FAA airworthiness directives
Airbus A321 airworthiness directives
411 FAA ADs name the Airbus A321: 285 in force, 56 recurring. Newest first.
AD 2026-18-03
Effective 2026-09-18
Airbus SAS Airplanes
This AD was prompted by a quality escape identified in the production assembly line on the main landing gear (MLG) support rib 5 lugs, which resulted in tool mark damage in the bore of the forward and aft lugs.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4), certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2026-0142, dated July 20, 2026 (EASA AD 2026-0142). (1) Model A318-112 airplanes. (2) Model A319-115, -132, and -133 airplanes. (3) Model A32...
AD 2026-17-04
Effective 2026-10-01
Airbus SAS Airplanes
This AD was prompted by reports of jamming of, or inability to open, the main landing gear (MLG) door during maintenance operations.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, -171N, and -173N airplanes. (3) Model A320-211, -212, -21...
AD 2026-14-04
Effective 2026-08-14
Airbus SAS Airplanes
This AD was prompted by a report that found corrosion and cracks on the broadband antenna adapter plate during an inspection.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (6) of this AD, certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, - 252N, -253N, -271N, -272N, and -273N airplanes. (3...
AD 2026-12-02
Effective 2026-07-14
Airbus SAS Airplanes
This AD was prompted by a report that cracks were detected on frame (FR) 16 and FR20 web holes and passenger door intercostal fitting holes at the door stop fitting locations, and a determination that a certain compliance time must be clarified.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025- 0111, dated May 14, 2025 (EASA AD 2025-0111). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112,...
AD 2026-11-04
Effective 2026-06-15
Airbus SAS Airplanes
This AD was prompted by aeroelastic stability assessments that indicate that reduced stability margins may exist due to accumulation of additional mass from rudder repainting or repairs.
This AD applies to all Airbus SAS Model A319-111, -112, -113, - 114, -115, -131, -132, -133, -151N, -153N, -171N, and -173N airplanes; Model A320-211, -212, -214, -216, -231, -232, -233, - 251N, -252N, -253N, -271N, -272N, and -273N airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, ...
AD 2026-10-17
Effective 2026-07-06
Airbus SAS Airplanes
This AD was prompted by reports of broken bolts in the affected seat rail connections of certain frames.
This AD applies to Airbus SAS Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2026-10-15
Effective 2026-07-06 · recurring
Airbus SAS Airplanes
This AD was prompted by the detection of a deviation from the manufacturing process during a review of the cold working process in the assembly line.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4), certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0078, dated April 9, 2025 (EASA AD 2025-0078). (1) Model A318-111, -112, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115,...
AD 2026-09-17
Effective 2026-06-18
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 4, 2024. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2026-09-16
Effective 2026-06-18
Airbus SAS Airplanes
This AD was prompted by a review of the cold working process on the assembly line that detected a deviation to the manufacturing process.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0066, dated March 28, 2025 (EASA AD 2025-0066). (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airpla...
AD 2026-09-03
Effective 2026-06-12
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 4, 2024. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mod...
AD 2026-03-10
Effective 2026-04-08
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 4, 2024. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2025-24-51
Effective 2026-01-06
Airbus SAS Airplanes
This emergency AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this emergency AD, certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, -171N, and -173N airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, - ...
AD 2025-23-09
Effective 2026-01-13
Airbus SAS Airplanes
This AD was prompted by a report that cracks were found on the web horizontal flange and inner cap on frame (FR) 68, left-hand (LH) and right-hand (RH) sides, at stringer (STGR) 22, and at the door stop fitting number 1 holes at FR 68.
This AD applies to Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0210, dated October 29, 2024 (EASA AD 2024-0210). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-1...
AD 2025-20-19
Effective 2026-01-02 · recurring
Airbus SAS Airplanes
This AD was prompted by the need to complete certain mandated programs intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0147R1, dated August 7, 2024 (EASA AD 2024-0147R1). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-...
AD 2025-20-15
Effective 2026-01-02
Airbus SAS Airplanes
This AD was prompted by reports that, during inspections accomplished as specified in certain airworthiness limitation items (ALIs), cracks were detected in the double joggle areas at frame (FR) 16 and FR20 in the nose forward fuselage.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0217, dated November 18, 2024 (EASA AD 2024-0217). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-1...
AD 2025-19-08
Effective 2025-12-30
Airbus SAS Airplanes
This AD was prompted by a report that cracks were found following fatigue tests for the new lower wing cover material on airplanes equipped with sharklets.
This AD applies to all Airbus SAS Model airplanes, certificated in any category, as identified in paragraphs (c)(1) through (3) of this AD. (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (3) Model A321-211, -212, -213, -2...
AD 2025-18-03
Effective 2025-10-20
Airbus SAS Airplanes
This AD was prompted by a report that a production deficiency of some SafeLav gaseous oxygen container (SLGOC) batches was identified during production testing of newly manufactured oxygen containers, and by the determination that additional airplanes are affected by the unsafe condition.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (6) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -2...
AD 2025-17-17
Effective 2025-09-17
Airbus SAS Airplanes
This AD was prompted by a determination that a batch of main landing gear (MLG) aft pintle pins did not have nickel plating applied to the inner bore during manufacturing.
This AD applies to all Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, -171N, and -173N airplanes. (3) Model A320-211, -212, -2...
AD 2025-17-07
Effective 2025-10-01 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes, in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before August 7, 2024. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112,...
AD 2025-16-10
Effective 2025-09-22
Airbus SAS Airplanes
This AD was prompted by a maintenance repair organization's report of deviations from the component maintenance manual acceptance test procedure for certain trimmable horizontal stabilizer actuators (THSAs).
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -2...
AD 2025-16-04
Effective 2025-09-18
Airbus SAS Airplanes
This AD was prompted by a heavy maintenance check that found elongation on the upper section of the vertical member's assembly at the frame (FR) 24A cargo panel sub-structure.
This AD applies to all Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, -171N, and -173N airplanes. (3) Model A320-211, -212, -2...
AD 2025-13-10
Effective 2025-08-14
Airbus SAS Airplanes
This AD was prompted by a determination that fatigue cracking may occur at the left-hand and right-hand wing manhole access panel attachment holes in the bottom wing skin panels 2, between rib 13 and rib 23, on airplanes with Sharklets or their structural reinforcements installed.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, - 252N, -253N, -271N, -272N, ...
AD 2025-10-12
Effective 2025-07-02 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that found corrosion and cracks on the broadband antenna adapter plate during an inspection.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (6) of this AD, certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, - 252N, -253N, -271N, -272N, and -273N airplanes. (3...
AD 2025-10-07
Effective 2025-06-26
Airbus SAS Airplanes
This AD was prompted by reports of cracks on the main landing gear (MLG) door hinge fitting and actuator fitting on the keel beam.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (7) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0097R2, dated July 12, 2024 (EASA AD 2024-0097R2). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2025-09-05
Effective 2025-06-05
Airbus SAS Airplanes
This AD was prompted by cracks being found during full-scale fatigue testing of the keel beam bottom panel between the edge profile and stringer run-out at frame 46 and stringer 37, left- and right-hand sides.
This AD applies to the Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD and in European Union Aviation Safety Agency (EASA) AD 2024-0135, dated July 10, 2024 (EASA AD 2024-0135). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -1...
AD 2025-03-07
Effective 2025-03-21 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 6, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2025-03-06
Effective 2025-03-21 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4), certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before December 19, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112...
AD 2025-03-08
Effective 2025-02-26
Airbus SAS Airplanes
This AD was prompted by reports of trimmable horizontal stabilizer actuators (THSAs) being delivered to operators having erroneous information (accumulated life) in the authorized release certificate.
This AD applies to all Airbus SAS Model airplanes, certificated in any category, as identified in paragraphs (c)(1) through (6) of this AD. (1) Airbus SAS Model A318-111, -112, -121, and -122 airplanes. (2) Airbus SAS Model A319-111, -112, -113, -114, -115, -131, - 132, -133, -151N, -153N, -171N, and -173N airplanes. (...
AD 2025-02-04
Effective 2025-03-17
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 6, 2023. (1) A318-111, -112, -121, and -122 airplanes. (2) A319-111,...
AD 2025-01-02
Effective 2025-03-11
Airbus SAS Airplanes
This AD was prompted by a full-scale fatigue test that found cracks on the main landing gear (MLG) bay rear skin panel at the stringer run-out at Frame 46 and Stringer 32 on the left-hand and right-hand sides.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0089, dated April 15, 2024 (EASA AD 2024-0089). (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airpla...
AD 2024-26-05
Effective 2025-03-11
Airbus SAS Airplanes
This AD was prompted by reported occurrences of chemical oxygen generators failing to activate in service and during maintenance activities.
This AD applies to all Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (8) of this AD. (1) Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, C4-605R Variant F, F4-605R, and F4-622R airplanes. (2) Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplane...
AD 2024-26-04
Effective 2025-02-18
Airbus SAS Airplanes
This AD was prompted by a report that certain overheat detection system (OHDS) sensing elements installed at certain positions might not properly detect thermal bleed leak events due to a quality escape during the manufacturing process.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2024-25-12
Effective 2025-03-07
Airbus SAS Airplanes
This AD was prompted by a determination that a damage-tolerance and fatigue reassessment of nose landing gear (NLG) repairs is necessary for certain parts fitted on airplanes approved for operation in the Commonwealth of Independent States (CIS).
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, and -153N airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, - 252N, -253N, -271N, -272N, and -27...
AD 2024-25-06
Effective 2024-12-30 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of jamming of, or inability to open, the main landing gear (MLG) door during maintenance operations.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2024-24-10
Effective 2025-01-13
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 6, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2024-24-09
Effective 2025-01-13
Airbus SAS Airplanes
This AD was prompted by a report that damage (including delamination of work deck and corroded and cracked retainer blocks) was found during inspection of certain galleys.
This AD applies to all Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -2...
AD 2024-19-15
Effective 2024-11-26
Safran Aerosystems (Formerly AVOX Systems Inc.; Scott Aviation) Oxygen Cylinder and Valve Assemblies, and Oxygen Valve Assemblies
This AD was prompted by reports of cylinder and valve assemblies having oxygen leakage from the valve assembly vent hole, caused by the absence of a guide that maintains appropriate spacing between certain parts, and by the manufacturer identifying additional assemblies and parts affected by the unsafe condition.
This AD applies to Safran Aerosytems (formerly AVOX Systems Inc.; Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794050, 89794077, 89794015, 891511-14, 806835- 01, 807982-01, 808433-01, or 891311-14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206-01. These asse...
AD 2024-19-13
Effective 2024-11-26 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before December 15, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model...
AD 2024-12-01
Effective 2024-08-13
Airbus SAS Airplanes
This AD was prompted by a report that, during a center fuselage certification full-scale fatigue test, cracks were found on the front spar vertical stringer at a certain frame.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0205, dated November 21, 2023 (EASA AD 2023-0205). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2024-11-01
Effective 2024-07-03 · recurring
Airbus SAS Airplanes
This AD was prompted by a report that repetitive disconnection and reconnection of certain Ni-Cd batteries during airplane parking or storage could lead to a reduction in capacity of those batteries.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (14) of this AD, certificated in any category, equipped with any parts manufacturer approval (PMA) part approved for the type design nickel cadmium (Ni-Cd) batteries having a part number identified in Figure 1 to the introductory text of pa...
AD 2024-08-08
Effective 2024-06-06 · recurring
Airbus SAS Airplanes
This AD was prompted by a report that repetitive disconnection and reconnection of certain nickel-cadmium (Ni-Cd) batteries during airplane parking or storage could lead to a reduction in capacity of those batteries.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (14) of this AD, certificated in any category. (1) Model A300 B4-2C, B4-103, and B4-203 airplanes. (2) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (3) Model A300 B4-605R and B4-622R airplanes. (4) Model A300 C4-605R variant...
AD 2024-06-07
Effective 2024-05-22
Airbus SAS Airplanes
This AD was prompted by reports of incomplete installations of the over wing panel lug attachments in the production assembly line and a determination that additional airplanes are subject to the unsafe condition.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022-0111R1, dated July 26, 2023 (EASA AD 2022-0111R1). (1) Model A319-115 airplanes. (2) Model A320-214, -216, -232, -251N, a...
AD 2024-04-07
Effective 2024-04-22
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes, identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before May 12, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-1...
AD 2024-04-04
Effective 2024-04-22
Airbus SAS Airplanes
This AD was prompted by reports of early cracking on the four holes of the crossbeam splicing at certain fuselage frames (FR).
This AD applies to Airbus SAS Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2024-04-03
Effective 2024-04-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before May 12, 2023. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111...
AD 2023-25-09
Effective 2024-02-07 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that a production deficiency of some SafeLav gaseous oxygen container (SLGOC) batches was identified during production testing of newly manufactured oxygen containers.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (6) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -2...
AD 2023-23-11
Effective 2024-01-23 · recurring
Airbus SAS Airplanes
This AD was prompted by a determination that cracks were found in the main landing gear (MLG) sliding tubes due to certain manufacturing defects that might not be identified using the current on-wing scheduled inspections.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all manufacturer serial numbers (MSNs). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, ...
AD 2023-23-08
Effective 2024-01-05 · recurring
Airbus SAS Airplanes
This AD was prompted by a report of cracks found during maintenance inspections on certain 10VU rack fitting lugs, and a determination that certain compliance times need to be revised.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus modification 157335 has been embodied in production. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -11...
AD 2023-20-12
Effective 2023-11-21
Airbus SAS Airplanes
This AD was prompted by a report that during re-engineering of galley G5, a 9G forward full scale qualification test was performed, and the door of the waste compartment opened before the required load was reached, and by reports of finding container/galley end stop bumpers damaged in service.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0029, dated February 1, 2023 (EASA AD 2023-0029), except where the Applicability of EASA AD 2023-0029 refers to certain g...
AD 2023-18-02
Effective 2023-10-24
Airbus SAS Airplanes
This AD was prompted by a report of cracking found on the frame of the right-hand side sliding window in the flight deck, and a determination that certain compliance times need to be reduced.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0009, dated January 16, 2023 (EASA AD 2023-0009). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2023-13-11
Effective 2023-09-05 · superseded or removed
AVOX Systems Inc. (Formerly Scott Aviation) Oxygen Cylinder and Valve Assemblies; and Oxygen Valve Assemblies
This AD was prompted by reports of cylinder and valve assemblies having oxygen leakage from the valve assembly vent hole, caused by the absence of a guide that maintains appropriate spacing between certain parts.
This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794077, 89794015, 891511-14, 806835-01, 807982-01, 808433-01, or 891311-14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206-01. These assemblies might be installed on, ...
AD 2023-13-10
Effective 2023-09-05 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 10, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2023-13-03
Effective 2023-09-05
Airbus SAS Airplanes
This AD was prompted by reports where the passenger door external handle mechanism was not allowing the flap handle to return to its normal, flush position when the door was being closed.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, and A319-171N ...
AD 2023-13-01
Effective 2023-07-12
Airbus SAS Airplanes
This AD was prompted by a determination that airplanes fitted with a certain fuel pump other than the fuel pumps identified in AD 2008-23-01 can be subject to cavitation erosion on the wiring conduit.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -23...
AD 2023-09-11
Effective 2023-07-10
Airbus SAS Airplanes
This AD was prompted by a report that during a maintenance check, cracks were found in the horizontal upper stiffener of the lateral window frame at the frame 4 upper attachment, and a determination that certain compliance times need to be revised.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022- 0151, dated July 26, 2022 (EASA AD 2022-0151). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112...
AD 2023-09-01
Effective 2023-06-26 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that certain overheat detection system (OHDS) sensing elements installed at certain positions might not properly detect thermal bleed leak events due to a quality escape during the manufacturing process.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2023-06-08
Effective 2023-05-18
Airbus SAS Airplanes
This AD was prompted by widespread fatigue damage (WFD) evaluations and full-scale fatigue testing that revealed several broken frames in certain areas of the cargo compartment, and by the determination that additional work is needed for certain airplanes.
This AD applies to Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category, as identified in European Aviation Safety Age...
AD 2023-05-14
Effective 2023-05-12
Airbus SAS Airplanes
This AD was prompted by reports of damaged lower lateral fittings of the 80VU rack and a determination that the compliance times must be revised.
This AD applies to all Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111 and -112 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (4) ...
AD 2023-05-02
Effective 2023-04-18 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that additional new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 18, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A3...
AD 2023-04-06
Effective 2023-04-10 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 18, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model...
AD 2023-01-01
Effective 2023-03-08
Airbus SAS Airplanes
This AD was prompted by a report of a nose landing gear (NLG) sliding tube rupture leading to an NLG collapse.
This AD applies to all Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -23...
AD 2022-24-13
Effective 2023-01-18
Airbus SAS Airplanes
This AD was prompted by a quality control review, which determined that the wrong aluminum alloy was used to manufacture several structural parts and by the issuance of an updated list of suspected parts, including those that may have been improperly heat treated.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 air...
AD 2022-24-05
Effective 2023-01-09 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that damage (including delamination of work deck, and corroded and cracked retainer blocks) was found during inspection of certain galleys.
This AD applies to all Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -2...
AD 2022-22-10
Effective 2022-12-30 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 2, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mode...
AD 2022-22-04
Effective 2022-12-30
Airbus SAS Airplanes
This AD was prompted by reports of fatigue damage in the structure for the door stop fittings on certain fuselage frames, and new analysis by the manufacturer, which resulted in optimized compliance times for the inspections.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0242, dated November 8, 2021 (EASA AD 2021-0242). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2022-18-09
Effective 2022-10-20 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that during re-engineering of galley G5, a 9G forward full scale qualification test was performed, and the door of the waste compartment opened before the required load was reached, and by reports of finding container/galley end stop bumpers damaged in service.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022-0026, dated February 16, 2022 (EASA AD 2022-0026). (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airpl...
AD 2022-18-05
Effective 2022-10-13
Airbus SAS Airplanes
This AD was prompted by unclear and incomplete placard instructions for the doghouse door lock, which could lead to incorrect operation of the doghouse door lock.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) All Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) All Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, and A3...
AD 2022-12-05
Effective 2022-09-02
Airbus SAS Airplanes
This AD was prompted by reports of cracks found on main landing gear (MLG) sliding tubes that may have been subject to improperly performed magnetic particle inspection.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 air...
AD 2022-15-05
Effective 2022-08-31 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that cracks were found on the web horizontal flange and inner cap on frame (FR) 68, left-hand (LH) and right-hand (RH) sides, at stringer (STGR) 22.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022- 0030, dated February 25, 2022 (EASA AD 2022-0030). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -...
AD 2022-14-10
Effective 2022-08-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that, during a center fuselage certification full-scale fatigue test, cracks were found on the front spar vertical stringer at a certain frame.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0241, dated November 8, 2021 (EASA AD 2021-0241). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111...
AD 2022-14-01
Effective 2022-08-18
Airbus SAS Airplanes
This AD was prompted by a report that taperloks used in the wing-to-fuselage junction at rib 1 were found to be non-compliant with the applicable specification, resulting in a loss of pre- tension in the fasteners; and a determination that, for certain airplanes, the compliance time for the initial inspection is inadequate and must be revised and additional actions are required.
This AD applies to Airbus SAS Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2022-09-16
Effective 2022-06-30
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 10, 2020. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mod...
AD 2022-08-08
Effective 2022-05-26 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports that, during inspections accomplished as specified in certain airworthiness limitation items (ALIs), cracks were detected in the double joggle areas at frame (FR) 16 and FR20 in the nose forward fuselage.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0227, dated October 11, 2021 (EASA AD 2021-0227). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2022-07-15
Effective 2022-05-02 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by the detection of several channel failures on a newly developed braking and steering control unit (BSCU), inducing, in case of dual channel failures, loss of anti- skid function together with the reversion to the alternate braking mode, and the loss of nose wheel steering.
This AD applies to the Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) All Model A318-111, -112, -121, and -122 airplanes. (2) All Model A319-111, -112, -113, -114, -115, -131, -132, - 133, -151N, -153N, and -171N airplanes. (3) All Model A320-211, -212, -...
AD 2022-07-08
Effective 2022-05-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that a more restrictive airworthiness limitation is necessary for the carbon friction disks on the no-back brake (NBB) of the trimmable horizontal stabilizer actuator (THSA).
This AD applies to all Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (7) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 ai...
AD 2022-06-21
Effective 2022-05-10
Airbus SAS Airplanes
This AD was prompted by a report that additional affected configurations were identified to be subject to widespread fatigue damage at certain stringer attachments and, for certain airplanes, it was determined that additional modification work is necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021- 0167, dated July 14, 2021 (EASA AD 2021-0167). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112...
AD 2022-06-02
Effective 2022-04-26 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of damaged lower lateral fittings of the 80VU rack, and reports of new damage on airplanes on which certain optional service information had been accomplished.
This AD applies to all Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111 and -112 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (4) ...
AD 2022-04-08
Effective 2022-04-11
Airbus SAS Airplanes
This AD was prompted by reports of low halon concentration in the forward and aft cargo compartments due to air leakage through cargo compartment door seals, and the certification of improved cargo door seals.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, equipped with any parts manufacturer approval (PMA) part approved for the type design forward and aft cargo compartment door seal part number (P/N) D5237106020400, including but not limited ...
AD 2022-04-09
Effective 2022-04-04 · superseded or removed
AVOX System Inc. (Formerly Scott Aviation) Oxygen Cylinder and Valve Assemblies and Oxygen Valve Assemblies
This AD was prompted by reports of cylinder and valve assemblies having oxygen leakage from the valve assembly vent hole, caused by the absence of a guide that maintains appropriate spacing between certain parts.
This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794077, 89794015, 891511-14, 806835-01, 807982-01, or 808433-01; and oxygen valve assemblies (body and gage assemblies) having P/N 807206-01. These assemblies might be installed on, but not lim...
AD 2022-04-03
Effective 2022-03-30
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before December 9, 2020. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2022-02-11
Effective 2022-03-15 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that cracks were detected on frame (FR)16 and FR20 web holes and passenger door intercostal fitting holes at the door stop fitting locations, and a determination that a certain compliance time needs to be clarified.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2018- 0289R1, dated February 10, 2021 (EASA AD 2018-0289R1). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2021-25-14
Effective 2022-01-05 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by the determination that fatigue cracking may occur at the left-hand and right-hand wing manhole access panel attachment holes in the bottom wing skin panels 2, between rib 13 and rib 23, on airplanes with Sharklets or its structural reinforcements installed.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD and certificated in any category. (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (3) Model A321-111, -112, -131, -211, -21...
AD 2021-23-15
Effective 2022-01-10
Airbus SAS Airplanes
This AD was prompted by a report that during re-engineering of galley G5, a 9G forward full scale qualification test was performed, and the door of the waste compartment opened before the required load was reached.
This AD applies to Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; as identified in European Aviation Safety Age...
AD 2021-22-04
Effective 2021-12-27 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a quality control review, which determined that the wrong aluminum alloy was used to manufacture several structural parts and by the issuance of an updated list of suspected parts, including those that may have been improperly heat treated.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 air...
AD 2021-21-02
Effective 2021-12-20 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that repetitive disconnection and reconnection of certain PMA Ni-Cd batteries during airplane parking or storage could lead to a reduction in capacity of those batteries.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (7) of this AD, certificated in any category, equipped with any parts manufacturer approval (PMA) part approved for the type design nickel cadmium (Ni-Cd) batteries identified in Figure 1 to paragraph (c) of this AD. [GRAPHIC] [TIFF OMITTED...
AD 2021-20-08
Effective 2021-11-18 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that repetitive disconnection and reconnection of certain nickel-cadmium (Ni-Cd) batteries during airplane parking or storage could lead to a reduction in capacity of those batteries.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (7) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -2...
AD 2021-18-04
Effective 2021-10-20
Airbus SAS Airplanes
This AD was prompted by reports of low halon concentration in the forward and aft cargo compartments due to air leakage through cargo door seals, and the certification of improved cargo door seals.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -23...
AD 2021-17-04
Effective 2021-10-05
Airbus SAS Airplanes
This AD was prompted by a report of false drill starts found around the latch hook mounting holes of certain door frames of the fuselage due to erroneous manufacturing processes.
This AD applies to Airbus SAS Model A321-211, -231, and -232 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0222, dated October 14, 2020 (EASA AD 2020-0222).
AD 2021-16-01
Effective 2021-09-28
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the following Airbus SAS airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 10, 2020: (1) Model A318-111, -112, -121, and -122 airplanes; (2) Model A319-111, -112, -113, -114, -115, -131, -132, -...
AD 2021-11-06
Effective 2021-06-04
Airbus SAS Airplanes
This AD was prompted by the loss of a windshield in flight, and the consequent rapid depressurization of the flight deck, which caused damage to flight deck items and systems and subsequent thermal shock and overheat, damage to windshield structural plies, and impaired structural integrity of the windshield.
This AD applies to the Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) All Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) All Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, and A...
AD 2021-10-04
Effective 2021-04-29
Airbus SAS Airplanes
This AD was prompted by a potential quality issue in the fuel pump that includes a locking key of the impeller drive shaft found loose in the cavity under the impeller.
This AD applies to the Airbus SAS airplanes, certificated in any category and identified in paragraphs (c)(1) through (4) of this AD. (1) All Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) All Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, an...
AD 2021-09-01
Effective 2021-06-01
Airbus SAS Airplanes
This AD was prompted by reports of missing overhead stowage compartment (OHSC) X-fixation brackets or brackets that were incorrectly installed during assembly.
This AD applies to Airbus SAS Model A320-271N, A321-211 and A321-271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0122, dated May 29, 2020 (EASA AD 2020-0122).
AD 2021-08-13
Effective 2021-06-01
Airbus SAS Airplanes
This AD was prompted by reports that certain oxygen supply solenoid valves are a potential source of increased flow resistance within the flightcrew oxygen system.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, and A319-133 airplanes. (3) Model A320-211, A32...
AD 2021-07-01
Effective 2021-05-10
Airbus SAS Airplanes
This AD was prompted by a report that the oil used to protect the nose landing gear (NLG) main fittings for transportation and storage was not removed before final heat treatment of the affected parts, possibly generating sub-surface cavities during heat treatment of the affected parts.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2021-05-20
Effective 2021-04-21 · recurring
Airbus SAS Airplanes
This AD was prompted by a report of a production quality deficiency on the inner retainer installed on link assemblies of the aft engine mount, which could result in failure of the retainer.
This AD applies to all the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111 and -112 airplanes. (2) Model A319-111, -112, -113, -114, and -115 airplanes. (3) Model A320-211, -212, -214, and -216 airplanes. (4) Model A321-111, -112, -211, -212,...
AD 2021-02-17
Effective 2021-03-30
Airbus SAS Airplanes
This AD was prompted by the results of laboratory tests on non- rechargeable lithium batteries installed in emergency locator transmitters (ELT), which highlighted a lack of protection against currents of 28 volts DC or 115 volts AC that could lead to thermal runaway and a battery fire.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319...
AD 2021-03-05
Effective 2021-02-22
Airbus SAS Airplanes
This AD was prompted by a report that following accomplishment of tap tests on rudders that were modified using the procedures in certain previously issued service information, disbonding of the rudder was found close to the lightning protection plate.
This AD applies to all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2020-26-15
Effective 2021-02-02
Airbus SAS Airplanes
This AD was prompted by fatigue testing that determined that fatigue damage could appear on clips, shear webs, and angles at certain rear fuselage sections and certain frames.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020- 0153, dated July 10, 2020 (EASA AD 2020-0153). (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (...
AD 2020-25-03
Effective 2020-12-28 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that during airplane boarding a loud bang was heard.
This AD applies to all Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -2...
AD 2020-22-16
Effective 2020-12-10
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before January 17, 2020. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2020-21-11
Effective 2020-11-20 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 13, 2019. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model...
AD 2020-21-10
Effective 2020-11-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 7, 2019. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2020-21-09
Effective 2020-10-30
Airbus SAS Airplanes
This AD was prompted by reports of cracks on the main landing gear (MLG) sliding tubes.
This AD applies to all the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216...
AD 2020-20-05
Effective 2020-11-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before October 11, 2019. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2020-19-03
Effective 2020-10-27
Airbus SAS Airplanes
This AD was prompted by reports of crack findings in and around the fastener holes of the central and lateral window frame upper junction; those cracks were found on fastener holes outside of the inspection area specified in a certain airworthiness limitation item (ALI) task.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0019, dated February 5, 2020 ("EASA AD 2020-0019"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-11...
AD 2020-18-06
Effective 2020-10-08
Airbus SAS Airplanes
This AD was prompted by a report that cracks were detected on the left- and right-hand sides of the first rivet hole of the frame (FR) 43 foot coupling during scheduled maintenance.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0037, dated February 27, 2020; corrected February 28, 2020 ("EASA AD 2020-0037"). (1) Model A318-111, -112, -121, and -...
AD 2020-17-03
Effective 2020-10-02
Airbus SAS Airplanes
This AD was prompted by reports of fatigue cracks on continuity fittings at the lower framing of the front windshield on airplanes on which Airbus Production Modification 22058 (which is included in Airbus Modification 21999) has been embodied.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0005, dated January 13, 2020 ("EASA AD 2020-0005"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-...
AD 2020-17-01
Effective 2020-09-09
Airbus SAS Airplanes
This AD was prompted by reports of fuel leaks at the interface of the low pressure shut off valves on the pylon areas of engines 1 and 2 due to improperly installed parts during production.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0148, dated July 6, 2020 ("EASA AD 2020-0148"). (1) Model A319-115 and -153N airplanes. (2) Model A320-214, -216, -232, -...
AD 2020-16-01
Effective 2020-08-19 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of low halon concentration in the forward and aft cargo compartments due to air leakage through cargo door seals.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -23...
AD 2020-14-08
Effective 2020-08-07
Airbus SAS Airplanes
This AD was prompted by reports of main landing gear (MLG) torque link apex pin rupture in service.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -23...
AD 2020-07-18
Effective 2020-05-26
Airbus SAS Airplanes
This AD was prompted by a determination that aluminum alloy with inadequate heat treatment was used for certain structural parts, including additional structural parts not addressed in AD 2017-05- 12.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0196, dated August 14, 2019 ("EASA AD 2019-0196"). (1) Model A318-112 airplanes. (2) Model A319-111, -112, -115, -132, a...
AD 2020-06-18
Effective 2020-04-02 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a maintenance repair organization's report of deviations from the component maintenance manual acceptance test procedure for certain trimmable horizontal stabilizer actuators (THSAs).
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N, -153N, and -171N airplanes. (3) Mod...
AD 2020-06-10
Effective 2020-05-04 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report of cracking found on the frame of the right-hand side sliding window in the flight deck.
This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0173, dated July 18, 2019 ("EASA AD 2019-0173"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111...
AD 2020-05-16
Effective 2020-04-24 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of incomplete installations of the over wing panel lug attachments in the production assembly line.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0233, dated September 18, 2019; corrected September 19, 2019 ("EASA AD 2019-0233"). (1) Model A319-115 airplanes. (2) Mod...
AD 2020-05-15
Effective 2020-04-24
Airbus SAS Airplanes
This AD was prompted by a report of rupture of a hydraulic reservoir air pressurization hose on an in-service airplane, leading to air leakage that was undetectable during normal operation, and found during subsequent zonal inspection.
This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-131, -132, and -133 airplanes. (2) Model A320-231, -232, and -233 airplanes. (3) Model A321-131, -231, and -232 airplanes.
AD 2020-05-14
Effective 2020-04-20
Airbus SAS Airplanes
This AD was prompted by a report of a production line inspection finding of damage on a main landing gear (MLG) side stay attachment outboard lug.
This AD applies to Airbus SAS Model A320-214, -232, -271N airplanes, and Model A321-231 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0167, dated July 15, 2019 ("EASA AD 2019-0167").
AD 2020-03-15
Effective 2020-04-02
Airbus SAS Airplanes
This AD was prompted by a report of erroneous positioning of affected parts on the skin of the fuselage during the pre-drill phase, which could result in unwanted drill-starts.
This AD applies to Airbus SAS Model A321-211, -212, -213, -231, and -232 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0098, dated May 3, 2019 ("EASA AD 2019-0098").
AD 2020-02-20
Effective 2020-03-20
Airbus SAS Airplanes
This AD was prompted by a report of a crack found in the side box beam flange of the fuselage at the frame (FR) 43 level during a fatigue test campaign.
This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2019-0122, dated June 4, 2019 ("EASA AD 2019-0122"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113,...
AD 2019-26-11
Effective 2020-03-12 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of finding container/galley end stop bumpers damaged in service.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0106, dated May 15, 2019 ("EASA AD 2019-0106"). (1) Model A319-112, -115, and -132 airplanes. (2) Model A320-214, -216, -...
AD 2020-01-17
Effective 2020-02-14 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that during airplane boarding a loud bang was heard.
This AD applies all Airbus SAS airplanes, certificated in any category, as identified in paragraphs (c)(1) through (4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, - 151N and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -23...
AD 2020-01-12
Effective 2020-02-14
Airbus SAS Airplanes
This AD was prompted by the absence of a requirement to remove a certain Emergency Procedure in the existing Aircraft Flight Manual (AFM) after accomplishing a certain modification or replacement.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4), certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (4)...
AD 2019-24-01
Effective 2020-02-19 · recurring
Airbus SAS Airplanes
This AD was prompted by the FAA's analysis of fuel system reviews on the affected airplanes conducted by the manufacturer.
This AD applies to the Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (6) of this AD, except airplanes equipped with a flammability reduction means (FRM) approved by the FAA as compliant with the Fuel Tank Flammability Reduction (FTFR) requirements of 14 CFR 25.981(b) or 14 ...
AD 2019-24-13
Effective 2020-02-03 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that during a maintenance check, cracks were found in an upper stiffener of the lateral window frame at the frame 4 upper attachment.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019- 0067R1, dated September 11, 2019 ("EASA AD 2019-0067R1"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2019-23-01
Effective 2020-01-09
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before June 13, 2018. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
AD 2019-21-10
Effective 2019-12-24 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a quality control review, which determined that the wrong aluminum alloy was used to manufacture several structural parts.
This AD applies to all Airbus SAS Model A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes, certificated in any category.
AD 2019-20-10
Effective 2019-12-18 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that cracks were detected on frame (FR) 16 and FR 20 web holes and passenger door intercostal fitting holes at the door stop fitting locations.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2018-0289, dated December 21, 2018 ("EASA AD 2018-0289"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -1...
AD 2019-19-15
Effective 2019-11-14
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 30, 2018. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mode...
AD 2019-18-07
Effective 2019-10-31 · superseded or removed
Airbus SAS Airplanes
The FAA is issuing this AD to address cracking in the open tack holes and rivet holes at the cargo floor support fittings of the fuselage, which could affect the structural integrity of the airplane.
This AD applies to Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category, as identified in European Aviation Safety Age...
AD 2019-18-06
Effective 2019-10-31
Airbus SAS Airplanes
This AD was prompted by reports of missing or loosened fasteners on connecting brackets of overhead stowage compartments (OHSC) and pivoting OHSC (POHSC).
This AD applies to Airbus SAS Model A318-112, -121, and -122; A319-111, -112, -115, -131, -132, and -133; A320-214, -216, -232, - 233, -251N, and -271N; and A321-211, -212, -213, -231, -232, -251N, -253N, -271N, and -272N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (E...
AD 2019-17-03
Effective 2019-10-11
Airbus SAS Airplanes
This AD was prompted by a test of a new wall partition for a certain cabin attendant seat model that revealed the backrest was permanently deformed and did not allow the seat pan to return to a full-up position; investigation results identified that a heat treatment had not been applied on certain backframes.
This AD applies to Airbus SAS Model A320-214 and -271N airplanes and Model A321-211 and -231 airplanes, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2019- 0005, dated January 14, 2019 ("EASA AD 2019-0005").
AD 2019-14-03
Effective 2019-09-26
Airbus SAS Airplanes
This AD was prompted by reports of cracking of the aft fixed fairing (AFF) of the pylons due to fatigue damage of the structure and reports of cracks on a certain rib of a modified AFF of the pylons.
This AD applies to Airbus SAS Model A318-111, -112; Model A319- 111, -112, -113, -114, -115; Model A320-211, -212, -214, -216; and Model A321-111, -112, -211, -212, -213 airplanes, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2018-0137R1, dated January 9, 2019 ("EASA AD 2018-...
AD 2019-14-04
Effective 2019-08-29
Airbus SAS Airplanes
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 13, 2018. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model...
AD 2019-12-07
Effective 2019-08-01 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a determination that cracks were found in the main landing gear (MLG) sliding tubes due to certain manufacturing defects that might not be identified using the current on-wing scheduled inspections.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers (MSNs). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211,...
AD 2019-08-07
Effective 2019-06-26 · recurring
Airbus SAS Airplanes
This AD was prompted by reports of cracks at the lower riveting of the four titanium angles that connect the belly fairing to the keel beam side panels on both sides of the fuselage.
This AD applies to the Airbus SAS airplanes specified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320...
AD 2019-07-05
Effective 2019-05-24 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report of cracks found during maintenance inspections on certain 10VU rack fitting lugs.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, ...
AD 2019-05-08
Effective 2019-04-16
Airbus SAS Airplanes
This AD was prompted by a report of corrosion found during the manufacturing process for some oxygen pipe assemblies that are used to supply oxygen to the flight crew.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(5) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes, all manufacturer serial numbers. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes, all manufacturer serial nu...
AD 2019-03-25
Effective 2019-04-16 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report that taperloks used in the wing-to-fuselage junction at rib 1 were found to be non-compliant with the applicable specification, resulting in a loss of pre- tension in the fasteners.
This AD applies to Airbus SAS Model A318-111, -112, -121, and - 122 airplanes, Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes, Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes, certificated in any catego...
AD 2019-03-28
Effective 2019-04-15 · recurring
Airbus SAS Airplanes
This AD was prompted by reports of in-flight loss of fixed and hinged main landing gear (MLG) fairings, and reports of post- modification MLG fixed fairing assemblies that have wear and corrosion.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, A318-112, A318-121, and A318-122 airplanes. (2) Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, and A319-1...
AD 2019-03-17
Effective 2019-04-03
Airbus SAS Airplanes
This AD was prompted by a revision of an airworthiness limitation item (ALI) document, which requires more restrictive maintenance requirements and airworthiness limitations.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before June 13, 2018. (1) Model A318-111, -112, -121, and -122 airp...
AD 2019-03-03
Effective 2019-03-26
Airbus SAS Airplanes
This AD was prompted by reports of multiple angle of attack (AoA) probe blockages.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, ...
AD 2019-01-07
Effective 2019-03-19
Airbus SAS Airplanes
This AD was prompted by a report that during removal of left- hand (LH) gear rib 5, four failed fasteners (bolts attaching the gear rib to the wing inner rear spar) were discovered.
This AD applies to Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category, as identified in Airbus Service Bulletin A320-57-1167, Revision 02, dated August 14, 2018.
AD 2018-26-08
Effective 2019-01-15
Airbus SAS Airplanes
This AD was prompted by an investigation that revealed that the outer cylinder of a certain ram air turbine (RAT) actuator was not properly deburred in accordance with manufacturing specifications.
This AD applies to Airbus SAS Model A320-214, A320-232, A320- 233, A321-211, and A321-231 airplanes; certificated in any category; as identified in the European Aviation Safety Agency (EASA) AD 2018- 0256, dated November 28, 2018 ("EASA AD 2018-0256").
AD 2018-25-08
Effective 2019-02-01 · recurring
Airbus SAS Airplanes
This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the frame forks and outer skin on the forward and aft cargo compartment doors are subject to widespread fatigue damage (WFD), and a determination that a modification of the frame forks must be accomplished.
This AD applies to Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; manufacturer serial numbers through 0758 incl...
AD 2018-25-02
Effective 2019-01-10 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by an evaluation by the design approval holder, which indicates that principal structural elements and certain life-limited parts are subject to widespread fatigue damage (WFD).
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD; certificated in any category; with an original certificate of airworthiness or original export certificate of airworthiness issued on or before October 24, 2017. (1) Model A318-111, -112, -121, and -122 a...
AD 2018-23-02
Effective 2018-12-28 · recurring
Airbus SAS Airplanes
This AD was prompted by reports of missing assembly hardware on the trimmable horizontal stabilizer actuator (THSA).
This AD applies to Airbus SAS Model A318-111, A318-112, A318- 121, and A318-122 airplanes; Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, and A319-133 airplanes; Model A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, and A320-233 airplanes; and Model A321-111, A321-112, A321-131,...
AD 2018-23-11
Effective 2018-12-19
Airbus SAS Airplanes
This AD was prompted by investigations that revealed that the cover seal of the brake dual distribution valve (BDDV) was damaged and did not ensure efficient sealing.
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 26925 has been embodied in production, which introduces a modified alternate braking system that removes the brake dual dis...
AD 2018-23-03
Effective 2018-12-14
Airbus SAS Airplanes
This AD was prompted by reports of false resolution advisories (RAs) from certain traffic collision avoidance systems (TCASs).
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, if modified by H4 Aerospace Supplemental Type Certificate (STC) ST03708NY or PMV Engineering STC ST03835NY. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -...
AD 2018-21-05
Effective 2018-11-19
Airbus SAS Airplanes
This AD was prompted by reports of fan cowl door (FCD) losses during takeoff.
This AD applies to Airbus SAS Model A319-131, A319-132, A319- 133, A320-231, A320-232, A320-233, A321-131, A321-231, and A321-232 airplanes, certificated in any category, if modified by Bombardier Short Brothers, PLC Supplemental Type Certificate (STC) ST03076NY.
AD 2018-20-08
Effective 2018-10-17
Airbus SAS Airplanes
This AD was prompted by a determination that, when two angle of attack (AoA) sensors are adversely affected by icing conditions at the same time, data displayed on the back-up speed scale (BUSS) could be erroneous.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, ...
AD 2018-17-19
Effective 2018-10-05
Airbus SAS Airplanes
This AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before April 19, 2017. (1) Model A318-111, -112, -121, and -122 airplanes. (2) M...
AD 2018-17-21
Effective 2018-10-04
Airbus SAS Airplanes
This AD was prompted by a revision of an airworthiness limitations document that specifies more restrictive maintenance requirements and airworthiness limitations.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before April 6, 2017. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mo...
AD 2018-16-04
Effective 2018-09-14
Airbus SAS Airplanes
This AD was prompted by a revision of an airworthiness limitations document that specifies more restrictive maintenance requirements and airworthiness limitations.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before April 6, 2017. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Mo...
AD 2018-16-02
Effective 2018-09-13 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report of a production quality deficiency on the inner retainer installed on link assemblies of the aft engine mount, which could result in failure of the retainer.
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111 and -112 airplanes. (2) Model A319-111, -112, -113, -114, and -115 airplanes. (3) Model A320-211, -212, -214, and -216 airplanes. (4) M...
AD 2018-14-09
Effective 2018-08-23 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of early cracking on the four holes of the crossbeam splicing at certain fuselage frames (FR).
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes, certificated in any category,...
AD 2018-13-08
Effective 2018-08-22 · superseded or removed
Airbus Airplanes
This AD was prompted by a report that, during a center fuselage certification full-scale fatigue test, cracks were found on the front spar vertical stringer at frame (FR) 36.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2018-12-02
Effective 2018-07-13
Airbus Airplanes
This AD was prompted by a review of maintenance instructions for a blend repair of the diameter of the snout of the main beam assembly of the forward engine mount that would create an excessive gap between the bearing mono-ball and the snout.
This AD applies to all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, and -115 airplanes; Model A320- 211, -212, -214, and -216 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes; certificated in any category.
AD 2018-09-09
Effective 2018-06-11 · superseded or removed
Airbus Airplanes Republication
This AD was prompted by an evaluation by the design approval holder indicating that the holes of the upper cleat to upper stringer attachments at rib 2 through rib 7 of the left- and right- hand wings are subject to widespread fatigue damage.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2018-09-16
Effective 2018-06-15
Airbus Airplanes
This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the potable water and waste water service panel areas are subject to widespread fatigue damage (WFD).
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, except for those airplanes on which Airbus modification 160055 or modification 160056 has been embodied in production, and except for Model A319 series airplanes on which modification 28162, 28...
AD 2018-06-04
Effective 2018-05-03 · recurring
Airbus Airplanes
This AD was prompted by fatigue tests which revealed cracking around the fasteners attaching the pressure panel to the flexible bracket at frame (FR) 36, adjacent to the longitudinal beams on the left and right sides of the airplane, and by the discovery of additional cracks under the longitudinal beams at locations that are not included in the inspection area required by AD 2004-03-07.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, except for airplanes on which Airbus Modification 151574 was embodied in production. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132...
AD 2018-06-01
Effective 2018-04-30
Airbus Airplanes
This AD was prompted by reports of false TCAS resolution advisories.
This AD applies to Airbus airplanes, all manufacturer serial numbers, certificated in any category, as identified in paragraphs (c)(1) through (c)(11) of this AD; except those Model A318, A319, A320 and A321 series airplanes that have been modified by a supplemental type certificate (STC) that installs Honeywell traffi...
AD 2018-05-04
Effective 2018-04-11
Airbus Airplanes
This AD was prompted by reports of engine fan cowl door (FCD) losses on airplanes equipped with CFM56 engines due to operator failure to close the FCD during ground operations.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, -113, -114, and -115 airplanes. (3) Airbus Model A320-211, -212, and -214 airp...
AD 2018-04-05
Effective 2018-04-03
Airbus Airplanes
This AD was prompted by in-service experience and further analysis, which showed that the galley 5 without kick-load retainers was unable to withstand the expected loading during several flight phases or in case of emergency landing.
This AD applies to Airbus Model A319-112, A319-115, A320-214, A320-232, and A321-211 airplanes, certificated in any category, manufacturer's serial numbers 1479, 3096, 3693, 3713, 3739, 3791, 3896, 3902, 3907, 3931, 3949, 3969, 4030, 4045, 4049, 4059, 4066, 4077, 4083, 4124, 4146, 4158, 4188, 4198, 4206, 4209, 4218, 42...
AD 2018-03-12
Effective 2018-03-19 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of fatigue damage in the structure for the door stop fittings on certain fuselage frames (FR).
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-211, -212, -214, 231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manu...
AD 2018-03-09
Effective 2018-02-22
Airbus Airplanes
This AD was prompted by a determination that the flat-headed pin at the upper attachment point of the overhead stowage compartments (OHSCs) at a certain frame may not sustain the maximum weight load for each flight phase.
This AD applies to Airbus Model A321-211 and -231 airplanes, certificated in any category, manufacturer serial numbers 3191, 3217, 3241, 3251, 3267, 3334, 3459, 3493, 3507, 3552, 3566, 3587, 3645, 3681, 3764, 3784, 3847, 3867, 3920, 3934, 3938, 3951, 3981, 4058, 4074, 4099, 4103, 4116, 4148, 4184, 4189, 4194, 4217, 422...
AD 2018-02-18
Effective 2018-02-21 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that, when two angle of attack (AoA) sensors are adversely affected by icing conditions at the same time, data displayed on the back-up speed scale (BUSS) could be erroneous.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers on which Airbus modification 35871 has been embodied in production or Airbus Service Bulletin A320-34-1397 has been embodied in service, except airplanes on wh...
AD 2017-25-06
Effective 2018-01-16
Airbus Airplanes
This AD was prompted by reports of a vertical strut penetrating through the cabin floor during an emergency water landing and on airframe ground contact at certain speeds/accelerations.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 153724 was embodied in production. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model...
AD 2017-25-05
Effective 2018-01-16
Airbus Airplanes
This AD was prompted by reports of the escape raft inflation system not deploying when activated due to the rotation of the cable guide in a direction which resulted in jamming of the inflation control cable.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all...
AD 2017-25-04
Effective 2018-01-16 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that more restrictive maintenance instructions and airworthiness limitations are necessary.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before December 21, 2015. (1) Model A318-111, -112, -121, and -122 airp...
AD 2017-24-07
Effective 2018-01-05
Airbus Airplanes
This AD was prompted by an investigation that showed that when a certain combination of target/proximity sensor serial numbers is installed on a flap interconnecting strut, a "target FAR" signal cannot be detected when reaching the mechanical end stop of the interconnecting strut.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all man...
AD 2017-24-03
Effective 2018-01-02
Airbus Airplanes
This action applies to Airbus Model A319-115, A319-132, A320- 214, A320-232, A321-211, A321-213, and A321-231 airplanes, certificated in any category, as identified in Airbus Service Bulletin A320-52-1167, dated August 6, 2015. (d) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) A...
AD 2017-22-07
Effective 2018-01-02 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of cracks on the frame forks and outer skin on the forward and aft cargo compartment doors.
This AD applies to Airbus Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category, manufacturer serial numbers through 0758 inclusive.
AD 2017-20-10
Effective 2017-11-15
Airbus Airplanes
This AD was prompted by a report of a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(3) of this AD, all manufacturer serial numbers. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (3)...
AD 2017-19-24
Effective 2017-11-01 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that more restrictive maintenance instructions and airworthiness limitations are necessary.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD; certificated in any category; with an original certificate of airworthiness or original export certificate of airworthiness issued on or before December 21, 2015. (1) Model A318-111, -112, -121, and -122 airp...
AD 2017-19-23
Effective 2017-11-01 · recurring
Airbus Airplanes
This AD was prompted by reports of wear at different levels in the trimmable horizontal stabilizer actuator (THSA).
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-2...
AD 2017-18-21
Effective 2017-09-28
Airbus Airplanes
This AD was prompted by an evaluation by the design approval holder that indicates that the main landing gear (MLG) does not comply with certification specifications, which could result in a locking failure of the MLG side stay.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus...
AD 2017-16-12
Effective 2017-10-02 · recurring
Airbus Airplanes
This AD was prompted by a report indicating that an Airbus Model A321 airplane encountered a blockage of two Angle of Attack (AOA) probes during climb, leading to activation of the Alpha Protection (Alpha Prot) while the Mach number increased.
This AD applies to the Airbus airplanes listed in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A32...
AD 2017-14-12
Effective 2017-09-22
Airbus Airplanes
This AD was prompted by reports that certain maintenance messages were recorded within the post flight report (PFR) that indicated the loss of elevator servo control monitoring performed by spoiler and elevator computer (SEC) 1, SEC 2, or both, during the engine start.
This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-...
AD 2017-14-14
Effective 2017-08-23 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination from fatigue testing on the Model A321 airframe that cracks could develop in the cabin floor beam junction at certain fuselage frame locations.
This AD applies to Airbus Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes, certificated in any category, all manufacturer serial numbers.
AD 2017-14-11
Effective 2017-08-21 · recurring
Airbus Airplanes
This AD was prompted by a report of a fire in the auxiliary power unit (APU) air intake.
This AD applies to Airbus airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -...
AD 2017-13-12
Effective 2017-08-09 · superseded or removed
Airbus Airplanes
This AD was prompted by an evaluation by the design approval holder, which indicates that the main landing gear (MLG) does not comply with certification specifications, which could result in a locking failure of the MLG side stay.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus...
AD 2017-13-07
Effective 2017-08-09 · recurring
Airbus Airplanes
This AD was prompted by a report that a main landing gear (MLG) door could not be closed due to rupture of the actuator fitting.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers. (1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Model A320-211, -212, -214, -231, -232, and -233 airplanes. (3) Model A3...
AD 2017-13-08
Effective 2017-08-03
Airbus Airplanes
This AD was prompted by a determination that, in specific flight conditions, the allowable load limits on the vertical tail plane could be reached and possibly exceeded.
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-2...
AD 2017-12-10
Effective 2017-07-20 · recurring
Airbus Airplanes
This AD was prompted by a full scale fatigue test campaign on Airbus Model A321 series airplanes in the context of the extended service goal.
This AD applies to Airbus Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes, certificated in any category.
AD 2017-11-07
Effective 2017-07-11 · recurring
Airbus Airplanes
This AD was prompted by reports of cracks on the 3 o'clock and 9 o'clock pivot fittings of a CFM56 engine's thrust reverser (T/R).
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, -113, -114, and -115 airplanes. (3) Airbus Model A320-211, -212, and -214 airp...
AD 2017-10-23
Effective 2017-06-29 · recurring
Airbus Airplanes
This AD was prompted by a determination from fatigue testing on the Model A321 airframe that cracks could develop on holes at certain fuselage frame locations.
This AD applies to Airbus Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes, certificated in any category, all manufacturer serial numbers.
AD 2017-08-03
Effective 2017-05-22
Airbus Airplanes
This AD was prompted by the discovery of corroded circlips in fuel vent protectors (FVP) having a certain part number.
This AD applies to the airplanes specified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus ...
AD 2017-05-12
Effective 2017-04-17 · superseded or removed
Airbus Airplanes
This AD was prompted by a quality control review on the final assembly line, which determined that aluminum alloy with inadequate heat treatment had been delivered and used on several structural parts.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category; manufacturer serial numbers 4895, 4903, 4911, 4919, 4929, 4938, 4942, 4944, 4946, 4948, and 4951, 4956 through 5541 inclusive, 5544, 5547, 5550, 5551, 5553, 5556, 5559, 5561, 5562, 5563, 5565...
AD 2017-05-02
Effective 2017-04-07
Airbus Airplanes
This AD was prompted by a quality control review of the final assembly line which determined that the wrong aluminum alloy was used to manufacture several structural parts.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category; manufacturer serial numbers 3586, 3588, 3589, 3590, 3595, 3604, 3608, 3614, 3615, 3620, 3632, 3634, 3638, 3647, 3651, 3657, 3660, 3661, 3663, 3671, 3675, 3680, 3683 through 3687 inclusive, 36...
AD 2017-04-10
Effective 2017-04-03
Airbus Airplanes
This AD was prompted by a report of a production quality deficiency on the inner retainer installed on link assemblies of the aft engine mount, which could result in failure of the retainer.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, -113, -114, and -115 airplanes. (3) Airbus Model A320-211, -212, and -214 airpl...
AD 2017-01-11
Effective 2017-02-22
Airbus Airplanes
This AD was prompted by a report of a rupture of a main landing gear (MLG) sliding tube axle.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model...
AD 2017-01-06
Effective 2017-02-21
Airbus Airplanes
This AD was prompted by a report of certain tie rod assemblies installed on the hinged fairing assembly of the main landing gear (MLG) with no cadmium plating on the rod end threads.
This AD applies to Airbus Model A319-115, A319-132, A320-214, A320-232, A321-211, A321-213, and A321-231 airplanes, certificated in any category, as identified in Airbus Service Bulletin A320-52- 1167, dated August 6, 2015.
AD 2016-25-24
Effective 2017-01-03 · recurring
Airbus Airplanes
This AD was prompted by reports of broken battery retaining rods.
This AD applies to Airbus Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320- 212, A320-214, A320-231, A320-232, A320-233, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321- 231, and A321-232 airplanes, certificated in any category, ...
AD 2016-25-08
Effective 2017-01-20
Airbus Airplanes
This AD was prompted by reports of silicon particles inside the oxygen generator manifolds, which had chafed from the mask hoses during installation onto the generator outlets.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214...
AD 2016-20-12
Effective 2016-11-25 · superseded or removed
Airbus Airplanes
This AD was prompted by Airbus issuing more restrictive maintenance requirements and/or airworthiness limitations.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before July 19, 2014. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model ...
AD 2016-19-14
Effective 2016-11-22 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of cracks found during maintenance inspections on certain lugs of the 10VU rack side fittings in the cockpit.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category; except airplanes on which Airbus Modification 35869 has been embodied in production. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -1...
AD 2016-17-12
Effective 2016-09-30 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of a partial loss of the no- back brake (NBB) efficiency during endurance qualification tests on the trimmable horizontal stabilizer actuator (THSA).
This AD applies to Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, ...
AD 2016-17-03
Effective 2016-09-23
Airbus Airplanes
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-2...
AD 2016-16-14
Effective 2016-09-23
Airbus Airplanes
This AD was prompted by a determination that oxygen generators installed on a certain batch of passenger emergency oxygen container assemblies might become detached by extreme pulling of the mask tube at the end of the oxygen supply causing a high temperature oxygen generator and mask to fall down.
This AD applies to the Airbus airplanes, certificated in any category, specified in paragraphs (c)(1) through (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model...
AD 2016-16-02
Effective 2016-09-16
Airbus Airplanes
This AD was prompted by reports of premature aging of certain passenger chemical oxygen generators that resulted in the generators failing to activate.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD; certificated in any category; all manufacturer serial numbers, except those that have embodied Airbus modification 33125 (gaseous system for all oxygen containers) in production. (1) Airbus Model A318-111, -112, -12...
AD 2016-14-09
Effective 2016-08-16 · recurring
Airbus Airplanes
This AD was prompted by inspection results that have shown that the main cause of crack initiation in the aft engine mount retainers is the vibration dynamic effect that affects both retainers, either with "dull" or "bright" surface finishes.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, -113, -114, and -115 airplanes. (3) Airbus Model A320-211, -212, and -214 airpl...
AD 2016-14-03
Effective 2016-08-12 · superseded or removed
Airbus Airplanes
We are issuing this AD to prevent fatigue cracking of the forward pressure bulkhead, which could result in reduced structural integrity of the airplane.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes...
AD 2016-12-04
Effective 2016-07-20 · recurring
Airbus Airplanes
This AD was prompted by an evaluation by the design approval holder (DAH) indicating that certain structural repair manual (SRM) inspection requirements for the fuselage skin repairs are insufficient to detect cracks.
This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model ...
AD 2016-12-10
Effective 2016-06-29
Airbus Airplanes
This AD was prompted by reports of airspeed indication discrepancies during flight at high altitudes in inclement weather.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus...
AD 2016-09-07
Effective 2016-06-10 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of airspeed indication discrepancies while flying at high altitudes in inclement weather.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus...
AD 2016-08-02
Effective 2016-06-08
Airbus Airplanes
This AD was prompted by reports of incorrect installation of jiffy joint connectors on cables connected to certain passenger service units (PSU), which could cause the passenger oxygen container to malfunction if the connector becomes disengaged during flight due to vibration.
This AD applies to Airbus Model A320-214, -232, and -233 airplanes; and Airbus Model A321-211 and -231 airplanes, certificated in any category, having manufacturer serial numbers (MSNs) 5583, 5598, 5602, 5604, 5608, 5610, 5613 through 5622 inclusive, 5624 through 5627 inclusive, 5629 through 5632 inclusive, 5634 throug...
AD 2016-09-06
Effective 2016-06-06 · recurring
Airbus Airplanes
This AD was prompted by the results of an evaluation by the design approval holder.
This AD applies to all Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD. (1) Model A318-111 and -112 airplanes. (2) Model A319-111, -112, -113, -114, and -115 airplanes. (3) Model A320-211, -212, and -214 airplanes. (4) Model A321-111, -112, -211, -2...
AD 2016-07-23
Effective 2016-06-06 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of in-flight loss of fixed and hinged main landing gear (MLG) fairings, and reports of post- modification MLG fixed fairing assemblies that have wear and corrosion.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model...
AD 2016-07-14
Effective 2016-05-16 · superseded or removed
Airbus Airplanes
This AD was prompted by fatigue testing that determined that fatigue damage could appear on clips, shear webs, and angles at certain rear fuselage sections and certain frames.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 30975 has been embodied in production. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplan...
AD 2016-07-12
Effective 2016-05-10 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of cracking of the aft fixed fairing (AFF) of the pylons due to fatigue damage of the structure.
This AD applies to Airbus Model A318-111 and -112, airplanes; Model A319-111, -112, -113, -114, and -115 airplanes; Model A320- 211, -212, and -214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes; certificated in any category; all manufacturer serial numbers on which Airbus Modification 33844 has be...
AD 2016-07-04
Effective 2016-05-10
Airbus Airplanes
This AD was prompted by a report that, during the assembly process, several gaps between the two parts of the girt bar fittings for the aft passenger doors were found to exceed tolerances.
This AD applies to Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD, except those on which Airbus Modification 154966 has been embodied during production. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, ...
AD 2016-06-13
Effective 2016-05-03
Airbus Airplanes
This AD was prompted by investigations that revealed that the cover seal of the BDDV was damaged and did not ensure efficient sealing.
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 26925 has been embodied in production. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (...
AD 2016-06-03
Effective 2016-04-22
Airbus Airplanes
This AD was prompted by reports of forward engine mount attachment pins that were manufactured from discrepant raw material.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers. (1) Model A319-131, -132, and -133 airplanes. (2) Model A320-232 and -233 airplanes. (3) Model A321-131, -231, and -232 airplanes.
AD 2016-05-02
Effective 2016-04-13 · recurring
Airbus Airplanes
This AD was prompted by a determination that the inspection interval of the main landing gear (MLG) door opening sequence must be reduced.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-2...
AD 2016-02-02
Effective 2016-03-01
Airbus Airplanes
This AD was prompted by reports of cracked cadmium-plated lock nuts that attach the hinge to the fan cowl door.
This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, and -115 airplanes. (3) Airbus Model A320-214 airplanes. (4) Airbus Mode...
AD 2016-01-08
Effective 2016-02-17
Airbus Airplanes
This AD was prompted by a determination that additional work is necessary to adequately address the identified unsafe condition.
(1) This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all...
AD 2015-23-13
Effective 2015-12-29 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that, in specific flight conditions, the allowable load limits on the vertical tail plane could be reached and possibly exceeded.
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-2...
AD 2015-22-10
Effective 2015-12-15 · recurring
Airbus Airplanes
This AD was prompted by a report of skin disbonding on a composite side shell panel of a rudder.
This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model ...
AD 2015-22-06
Effective 2015-11-20 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of spoiler and elevator computer (SEC) latent failures; an undetected loss of a SEC in flight will result in loss in redundancy for elevator control.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Mode...
AD 2015-19-08
Effective 2015-10-27 · recurring
Airbus Airplanes
This AD was prompted by a determination that certain elevator servo-control parts that do not conform to the approved type design have been installed and may have the potential of cracks in the rod eye-end.
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-2...
AD 2015-17-14
Effective 2015-10-02 · superseded or removed
Airbus Airplanes
This AD was prompted by reports that, during a full scale fatigue test, several broken frames in certain areas of the cargo compartment have been found, especially on the cargo floor support fittings and open tack holes on the left-hand (LH) side.
This AD applies to Airbus Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers.
AD 2015-17-06
Effective 2015-09-24
Airbus Airplanes
This AD was prompted by reports that on airplanes equipped with sharklets, discretes (used to activate the load alleviation function) are connected on various flight computers using the same ground point.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers on which Airbus modification (mod) 160500 or mod 160023 has been embodied in production, and those that have been modified in service through the Airbus ...
AD 2015-15-13
Effective 2015-09-08 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of cracks that could be initiated at the waste water service panel area and the potable water service panel area.
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 160055 or Airbus Modification 160056 has been embodied in production. (1) Airbus Model A319-111, -112, -113, -114, -11...
AD 2015-15-10
Effective 2015-08-28 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of wear of the trimmable horizontal stabilizer actuator (THSA).
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-2...
AD 2015-12-08
Effective 2015-07-21 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of corrosion found during the manufacturing process for some oxygen pipe assemblies that are used to supply oxygen to the flightcrew.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214...
AD 2015-09-03
Effective 2015-06-04 · recurring
Airbus Airplanes
This AD was prompted by reports of cracks on the forward corner fittings of engine pylon aft secondary structures.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, except for airplanes on which Airbus Modification 33844 or Modification 33847, as applicable, has been embodied in production. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A...
AD 2015-05-02
Effective 2015-03-23 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that certain limitations required by AD 2014-23-15, Amendment 39-18031 (80 FR 3871, January 26, 2015), conflict with limitations required by AD 2014-26-10, Amendment 39-18061 (80 FR 2813, January 21, 2015).
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2015-02-14
Effective 2015-04-06 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of cracks on the main landing gear (MLG) door hinge fitting and actuator fitting on the keel beam.
This AD applies to the Airbus airplanes specified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers (MSNs). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A...
AD 2015-03-05
Effective 2015-03-25
Airbus Airplanes
This AD was prompted by a determination that more airplanes are subject to the identified unsafe condition.
(1) This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2014-23-15
Effective 2015-03-02 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that more restrictive limitations are necessary.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes.
AD 2014-25-51
Effective 2015-02-06
Airbus Airplanes
This AD was prompted by a report of Angle of Attack (AoA) probes jamming on an in-service Airbus Model A321 airplane.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD. (1) All Model A318-111, -112, -121, and -122 airplanes. (2) All Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) All Model A320-211, -212, -214, -231,...
AD 2014-26-10
Effective 2015-02-25 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that the maintenance actions for airplane systems susceptible to aging must be mandated.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2014-24-07
Effective 2015-01-09 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of a crack found in the side box beam flange of the fuselage at the frame (FR) 43 level during a fatigue test campaign.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2014-23-05
Effective 2014-12-26
Airbus Airplanes
This AD was prompted by a report of a circumferential crack at the gland retaining-ring groove of certain retraction actuators on the main landing gear (MLG).
This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model ...
AD 2014-22-08
Effective 2014-12-17 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that more restrictive airworthiness limitations are necessary.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2014-20-04
Effective 2014-11-07 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of cracks at the lower riveting of the four titanium angles that connect the belly fairing to the keel beam side panels on both sides of the fuselage.
This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model ...
AD 2013-25-07
Effective 2014-10-17 · recurring
Airbus Airplanes
This AD was prompted by a report of an airplane landing with the nose landing gear (NLG) turned 90 degrees from centerline, and from additional reports of upper support anti-rotation lugs of the NLG rupturing in service.
This AD applies to the Airbus airplanes listed in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-111, -211, -212, -2...
AD 2014-17-10
Effective 2014-09-12 · recurring
Airbus Airplanes
This AD was prompted by reports of spurious terrain ahead warning system (TAWS) alerts during approach and takeoff.
This AD applies to all Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(4) of this AD. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -231, -232, and -233 airplanes...
AD 2014-17-02
Effective 2014-09-09
Honeywell ASCa Inc. Emergency Locator Transmitters Installed on Various Transport Category Airplanes
This AD was prompted by a fire on a parked and unoccupied airplane; preliminary information indicated combustion in the area of the ELT TU.
This AD applies to Honeywell ASCa Inc. emergency locator transmitters (ELTs) Model RESCU 406AF and 406AFN with transmitter unit (TU) part numbers (P/Ns) 1152682-1, -2, and -3, installed on transport category airplanes, certificated in any category, but not limited to the airplanes identified in table 1 to paragraph (c)...
AD 2014-13-12
Effective 2014-09-09 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of silicon particles inside the oxygen generator manifolds, which had chafed from the mask hoses during installation onto the generator outlets.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; A320-111, -211, -212, -214, -231, -232, and -233 airplanes; A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial ...
AD 2014-15-16
Effective 2014-08-18
Airbus Airplanes
This AD was prompted by a report that when the cabin lining was removed during a cabin conversion it was discovered that fasteners were missing on the frame.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, manufacturer serial numbers (MSN) 5230 through 5300 inclusive, except MSN 5255 and 5295. (1) Model A319-111, -112, -115, -132, and -133 airplanes. (2) Model A320-214, -232, and -233 airp...
AD 2014-14-06
Effective 2014-08-27 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of broken aft engine mount retainers.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111 and -112 airplanes. (2) Airbus Model A319-111, -112, -113, -114, and -115 airplanes. (3) Airbus Model A320-111, -211, -212, and -214...
AD 2014-08-01
Effective 2014-05-14 · superseded or removed
Airbus Airplanes
This AD was prompted by a report that an investigation showed that when a certain combination of a target/proximity sensor serial number is installed on a flap interconnecting strut, a "target FAR" signal cannot be detected when reaching the mechanical end stop of the interconnecting strut.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any categor...
AD 2013-26-14
Effective 2014-05-02 · recurring
Airbus Airplanes
This AD was prompted by reports of cracks found in the forward lug of the main landing gear (MLG) support rib 5 fitting.
This AD applies to Airbus Model A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319- 131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321- 211, A321-212, A321-213, A321-231, and A321-232 airplanes, ce...
AD 2014-03-08
Effective 2014-03-26 · superseded or removed
Airbus Airplanes
This AD was prompted by a report that an investigation showed that when a certain combination of a target/proximity sensor serial number is installed on a flap interconnecting strut, a "target FAR" signal cannot be detected when reaching the mechanical end stop of the interconnecting strut.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2013-26-07
Effective 2014-02-10
Airbus Airplanes
This AD was prompted by reports of certain sliding windows that were difficult to operate after landing.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2013-25-06
Effective 2014-02-10
Airbus Airplanes
This AD was prompted by a determination that certain maintenance activities, such as repairs or the accumulation of paint layers, might cause the weight of an elevator to exceed the certified limits.
This AD applies to the Airbus airplanes, certificated in any category, listed in paragraphs (c)(1) through (c)(4) of this AD, all serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-111, -211, -212, -214, -231, -2...
AD 2013-25-11
Effective 2014-01-31 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of worn lower lateral fittings of the 80VU rack.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2013-24-08
Effective 2014-01-06
Airbus Airplanes
This AD was prompted by a report of several in-service incidents of wear and detachment of the top-stops from magnetic fuel level indicators (MFLI) in a wing fuel tank.
This AD applies to Airbus Model A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319- 131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321- 211, A321-212, A321-213, A321-231, and A321-232 airplanes; ce...
AD 2013-20-04
Effective 2013-12-05
Airbus Airplanes
This AD was prompted by a determination that certain special washers used in retraction jack anchorage fitting bearing installation in the main landing gear (MLG) were incorrectly manufactured.
This AD applies to the Airbus airplanes listed in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-111, -...
AD 2013-20-11
Effective 2013-12-02 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that oxygen generators, installed on a certain batch of passenger emergency oxygen container assemblies, might become detached by extreme pulling of the mask tube at the end of the oxygen supply causing a high temperature oxygen generator and mask to fall down.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category;...
AD 2013-19-09
Effective 2013-11-06 · superseded or removed
Airbus Airplanes
This AD was prompted by a determination that replacement of angle of attack (AoA) sensor conic plates is necessary to address the identified unsafe condition.
This AD applies to the Airbus airplanes listed in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A32...
AD 2013-18-09
Effective 2013-10-03 · superseded or removed
Honeywell ASCa Inc. Emergency Locator Transmitters Installed on Various Transport Category Airplanes
This AD was prompted by a fire on a parked and unoccupied airplane; preliminary information indicated combustion in the area of the ELT TU.
This AD applies to Honeywell ASCs Inc. emergency locator transmitters (ELTs) Model RESCU 406AF and 406AFN with transmitter unit (TU) part numbers (P/Ns) 1152682-1, -2, and -3, installed on transport category airplanes, certificated in any category, but not limited to the airplanes identified in table 1 to paragraph (c)...
AD 2013-16-18
Effective 2013-09-27
Airbus Airplanes
This AD was prompted by a report of a missing fastener between certain stringers of the fuselage frame that connects the frame to a tee.
This AD applies to Airbus Model A320-214, -232, and -233 airplanes; and Model A321-211, -213, and -231 airplanes; certificated in any category; manufacturer serial numbers 4338, 4371, 4374, 4375, 4377, 4381 through 4384 inclusive, 4386, 4387, 4388, 4390 through 4402 inclusive, 4404 through 4409 inclusive, 4411 through ...
AD 2013-16-09
Effective 2013-08-23 · recurring
Airbus Airplanes
This AD was prompted by a report of a main landing gear (MLG) failing to extend during landing, and a determination that a certain configuration of landing gear control interface unit (LGCIU) and actuators may result in masking of centralized fault display system messages that are necessary to mitigate risks associated with failure of MLG extension or down-locking.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-1...
AD 2013-13-04
Effective 2013-08-14 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of an uncommanded nose landing gear (NLG) retraction.
This AD applies to Airbus Model A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319- 131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321- 211, A321-212, A321-213, A321-231, and A321-232 airplanes; ce...
AD 2013-05-11
Effective 2013-07-26 · recurring
Airbus Airplanes
This AD was prompted by reports of surface defects on rudders that were the result of debonding between the skin and honeycomb core.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all serial numbers (S/N) having a rudder with a part number (P/N) and serial number listed in tables 1, 2, and 3, and figures 1 and 2, and 3 and 4 of this AD; and rudders P/N D55...
AD 2013-07-04
Effective 2013-05-20
Airbus Airplanes
We are issuing this AD to prevent failure of the attachment points of the YZ-latches, which could result in unrestrained cargo causing damage to the fire protection system, hydraulic system, electrical wiring, or other equipment located in the forward and aft cargo compartments.
This AD applies to Airbus Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, - 214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers.
AD 2013-06-03
Effective 2013-05-03
Airbus Airplanes
This AD was prompted by reports of oil residue between the stator and the rotor parts of the position resolvers of the angle of attack (AOA) vane, which was a result of incorrect removal of the machining oil during the manufacturing process of the AOA resolvers.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2012-26-51
Effective 2013-01-24 · superseded or removed
Airbus Airplanes
This AD was prompted by a report indicating that an airplane equipped with Angle of Attack (AoA) sensors (with conic plates installed) recently experienced blockage of all sensors during climb, leading to autopilot disconnection and activation of the alpha protection (Alpha Prot) when Mach number was increased.
This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category,...
AD 2012-26-15
Effective 2013-01-24 · superseded or removed
Honeywell International Inc. Air Data Pressure Transducers
This AD was prompted by a report of a pressure measurement error in the pressure transducer used in various air data systems, which translates into air data parameter errors.
This AD applies to air data pressure transducers, as installed in air data computers (ADC), air data modules (ADM), air data attitude heading reference systems (ADAHRS), and digital air data computers (DADC) having the part numbers and serial numbers identified in Honeywell Alert Service Bulletin ADM/ADC/ADAHRS-34- A01...
AD 2012-23-10
Effective 2012-12-31 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of the escape slide of the raft inflation system not deploying when activated due to the rotation of the cable guide in a direction which resulted in jamming of the inflation control table.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2012-20-07
Effective 2012-11-21 · superseded or removed
Airbus Airplanes
This AD was prompted by Airbus issuing more restrictive maintenance requirements and/or airworthiness limitations.
(1) This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any catego...
AD 2012-16-11
Effective 2012-09-21
Airbus Airplanes
This AD was prompted by reports that some nuts installed on the wing, including on primary structural elements, were found cracked.
This AD applies to Airbus Model A318-112 and -121 airplanes; Model A319-111, -112, -115, -132, and -133 airplanes; Model A320- 214, -232, and -233 airplanes; and Model A321-211, -212, -213, and - 231 airplanes; certificated in any category; serial numbers 3359, 3361, 3362, 3365, 3366, 3368, 3370 through 3508 inclusive,...
AD 2011-19-01
Effective 2012-08-22
Airbus Airplanes
This AD was prompted by reports of transient loss of certain systems and the potential for an inadvertent error by flightcrew to use the IDG switch instead of the GEN switch when doing a certain airplane flight manual (AFM) display unit failure procedure.
This AD applies to Airbus Model A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319- 131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321- 211, A321-212, A321-213, A321-231, and A321-232 airplanes; ce...
AD 2012-14-13
Effective 2012-08-27
Airbus Airplanes
This AD was prompted by reports of fuselage nuts found cracked.
This AD applies to Airbus Model A318-112 and -121 airplanes; Model A319-111, -112, -115, -132, and -133 airplanes; Model A320- 214, -232, and -233 airplanes; and Model A321-211, -212, -213, and - 231 airplanes; certificated in any category; manufacturer serial numbers 3339, 3340, 3350, 3355, 3360, 3367, 3369, 3372, 338...
AD 2012-09-12
Effective 2012-06-21
Airbus Airplanes
This AD was prompted by reports that the modification required by AD 2005-23-02, Amendment 39-14360 (70 FR 69067, November 14, 2005), was not fully effective.
This AD applies to Airbus airplanes listed in paragraphs (c)(1), (c)(2), and (c)(3) of this AD; certificated in any category; all serial numbers; if equipped with one or more additional center tank(s) (ACT) with a part number (P/N) listed in table 1 of this AD. This AD does not apply to airplanes already having receive...
AD 2012-09-07
Effective 2012-06-18 · superseded or removed
Airbus Airplanes
This AD was prompted by reports that corrosion was found on the overwing refueling aperture on the top wing skin, and that for certain airplanes, repairs made using primer coating may prevent proper electrical bonding provision between the overwing refueling cap adaptor and the wing skin.
This AD applies to Airbus Model A319-111, -112, and -132 airplanes; Model A320-111, -211, -212, -214 and -232 airplanes; and Model A321-111, -211, -212, and -231 airplanes; certificated in any category; having manufacturer serial numbers 0039, 0078, 0109, 0118, 0120, 0153, 0174, 0187, 0203, 0215, 0218, 0226, 0227, 0228...
AD 2012-06-11
Effective 2012-04-16
Airbus Airplanes
This AD was prompted by reports of incorrect installation of rib pads of the lower aft panel of the center wing box (CWB) due to poor clamping during drilling, and reports that metal chips trapped between panels and stiffeners could impact the fatigue life of CWB panels.
This AD applies to Airbus Model A321-131, -211, -212, and -231 airplanes; certificated in any category; manufacturer serial numbers 1293, 1299, 1307, 1333, 1356, and 1366.
AD 2011-21-08
Effective 2011-11-23 · recurring
Sicma Aero Seat Passenger Seat Assemblies Installed on Various Transport Category Airplanes
This AD applies to Sicma Aero Seat 88xx, 89xx, 90xx, 91xx, 92xx, 93xx, 95xx, and 96xx series passenger seat assemblies identified in Annex 1, Issue 2, dated March 19, 2004, of Sicma Aero Seat Service Bulletin 90-25-013, Issue 4, dated March 19, 2004, that have backrest links having part numbers (P/Ns) 90-000200-104-1 a...
AD 2011-19-04
Effective 2011-10-21 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category; ...
AD 2011-16-03
Effective 2011-09-09
Airbus Model A300 B4-600, A300 B4-600R, and A300 F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called Model A300-600 Series Airplanes); Model A310 Series Airplanes; Model A318 Series Airplanes; Model A319 Series Airplanes; Model A320-211, -212, -214, -231, -232, and -233 Airplanes; Model A321 Series Airplanes; Model A330-200 and A330-300 Series Airplanes; and Model A340-200, A340-300, A340-500, and A340-600 Series Airplanes
This AD applies to the Airbus airplanes listed in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD, certificated in any category. (1) Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes; and Model A310-203, -204, -221, -222, -304, -322, -...
AD 2011-14-06
Effective 2011-08-22 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, - 132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, - 232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any catego...
AD 2011-13-11
Effective 2011-07-12 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122, airplanes; Model A319-111, -112, -113, -114, -115, -131, - 132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, - 232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any categ...
AD 2011-10-15
Effective 2011-05-31
Airbus Model A318-112, A319-111, A319-112, A319-115, A319-132, A319-133, A320-214, A320-232, A320-233, A321-211, A321-213, and A321-231 Airplanes
This AD applies to Airbus Model A318-112, A319-111, A319- 112, A319-115, A319-132, A319-133, A320-214, A320-232, A320-233, A321-211, A321-213, and A321-231 airplanes, certificated in any category, manufacturer serial numbers (MSN) 3603, 3605, 3607, 3610, 3613, 3615 to 3619 inclusive, 3622 to 3627 inclusive, 3629, 3631 ...
AD 2010-02-05
Effective 2011-01-18
Airbus Model A300, A300-600, A310, A318, A319, A320, A321, A330-300, A340-200, A340-300, A340-500, A340-600, and A380-800 Series Airplanes; and Model A330-201, A330-202, A330-203, A330-223, A330-243 Airplanes
This AD was prompted by a report indicating that certain equipment on the flight deck door is defective.
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD. (1) Model A300 B2-1A, B2-1C, B4-2C, B2K-3C, B4-103, B2-203, B4- 203, B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4- 622R, and C4-605R Variant F airplanes...
AD 2010-26-12
Effective 2011-01-12
Airbus Model A321-211, -212, -231, and -232 Airplanes
This AD applies to Airbus Model A321-211, -212, -231, and - 232 airplanes, certificated in any category, with manufacturer serial numbers 3051, 3067, 3070, 3075, 3081, 3098, 3106, 3112, 3120, 3126, and 3130.
AD 2010-24-07
Effective 2011-01-11 · superseded or removed
Airbus Model A318-111 and A318-112 Airplanes and Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, A318-112, A319- 111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320- 232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes, certificated in any ca...
AD 2010-23-07
Effective 2010-12-10 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category, ...
AD 2010-18-07
Effective 2010-09-09 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category.
AD 2010-10-08
Effective 2010-06-21
Airbus A318, A319, A320, A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category; ...
AD 2010-09-14
Effective 2010-06-08 · recurring
CFM International, S.A. CFM56-5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B4/P1, -5B6/2P, -5B4/2P1, and -5B9/2P Turbofan Engines
We are issuing this AD to prevent high-pressure compressor stalls, which could prevent continued safe flight or landing.
This AD applies to CFM International, S.A. CFM56-5B1/P, - 5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, - 5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B4/P1, -5B6/ 2P, -5B4/2P1, and -5B9/2P turbofan engines. These engines are installed on, but not limited to, Airbus A318, A319, A320, and A32...
AD 2010-06-18
Effective 2010-04-22
International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines
This AD applies to International Aero Engines (IAE) V2500- A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines with high-pressure (HP) compressor stage 3-8 drums, part numbers (P/Ns) 6A4900, 6A5467, 6A6473, 6A7383, 6A7384, 6A7385, and 6A7401, installed. Th...
AD 2010-06-01
Effective 2010-04-15
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, - 214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers (MSN); equipped w...
AD 2009-21-10
Effective 2010-02-04
AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes
This AD was prompted by the reported rupture of a high- pressure gaseous oxygen cylinder, which had insufficient strength characteristics due to improper heat treatment.
This AD applies to the oxygen cylinder assemblies, approved under United States Department of Transportation Regulations for Type 3HT cylinders, identified in Table 1 of this AD. These oxygen cylinder assemblies may be installed on various transport airplanes, certificated in any category, identified in but not limited...
AD 2007-15-06
Effective 2009-12-14 · superseded or removed
Airbus Model A318-111 and -112 Series Airplanes, and Model A319, A320, and A321 Series Airplanes
We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
This AD applies to all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category.
AD 2009-23-05
Effective 2009-12-14
Airbus Model A318-111, -112, A319, A320, and A321 Series Airplanes
We are issuing this AD to prevent possible mid-air collisions due to lack of visibility of TCAS indications on the PFD.
This AD applies to Airbus Model A318-111, A318-112, A319- 111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320- 232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 series airplanes, certificated in...
AD 2009-22-06
Effective 2009-11-30
International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 Turbofan Engines
We are issuing this AD to prevent an uncontained failure of the HPC stage 9-12 disc assembly, resulting in an in-flight engine shutdown and possible damage to the airplane.
This AD applies to International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 turbofan engines. These engines are installed on, but not limited to, Airbus A320 and A321 series, and McDonnell Douglas Corporation MD-90 airplanes.
AD 2009-20-05
Effective 2009-11-03 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, all certified models, certificated in any category, all serial numbers up to manufacturer's serial number (MSN) 2850 inclusive, except MSNs 0115, 0184, 0782, 1151, 1190, 2650, 2675, 2706, 2801, and 2837.
AD 2009-18-01
Effective 2009-10-01 · recurring
CFM International, S.A. CFM56-5B1/P; -5B2/P; -5B3/P; -5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; -5B8/P; -5B9/P; -5B1/3; -5B2/3; -5B3/3; -5B4/3; -5B5/3; -5B6/3; -5B7/3; -5B8/3; -5B9/3; -5B3/3B1; and -5B4/3B1 Turbofan Engines
We are issuing this AD to detect low-cycle-fatigue cracks in the LP turbine rear frame, which could result in an engine separating from the airplane, causing damage to, and possibly leading to loss of control of the airplane.
This AD applies to: (1) CFM International, S.A. turbofan engines with a low-pressure (LP) turbine rear frame, part number (P/N) 338-171-703-0; 338-171- 704-0; 338-171-705-0; or 338-171-706-0 installed, as follows: (i) Commercial application CFM56-5B1/P; -5B2/P; -5B3/P; -5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; ...
AD 2009-17-04
Effective 2009-09-22 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320- 111, -211, -212, -214, -231, -232, -233; and A321-111, -112, -131, - 211, -212, -213, -231, and -232 series airplanes; certificated in any category; all manufacturer serial numbers.
AD 2009-15-07
Effective 2009-08-25
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-111, -211, -212, -214, -231, -232, and -233; and A321-111, -112, -131, -211, -212, -213, -231, and -232 series airplanes; certificated in any category; equipped with one conventional pre-Enhanced Manufacture and Maintainability...
AD 2009-09-05
Effective 2009-06-04
Airbus Model A318-100 and A319-100 Series Airplanes; A320-111 Airplanes; A320-200 Series Airplanes; and A321-100 and A321-200 Series Airplanes
We are issuing this AD to prevent contact between the horizontal hinge pin and the adjacent electrical wire harness, which could result in damage to electrical wires, and consequent arcing and/or failure of associated systems.
This AD applies to Airbus Model A318-111 and 112; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-111, -211, -212, -214, -231, -232, and -233; and A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category; all manufactured serial numbers; except for those airplanes on ...
AD 2009-09-01
Effective 2009-05-06
Airbus Model A318, A319, A320 and A321 Series Airplanes
This AD applies to Airbus Model A318-111, A318-112, A318- 121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320- 214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes; ce...
AD 2009-01-01
Effective 2008-12-31 · superseded or removed
CFM International, S. A. CFM56-5B Series Turbofan Engines
We are issuing this AD to prevent HPC stalls, which could prevent continued safe flight or landing.
This AD applies to CFM International, S. A. CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7, -5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, - 5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, - 5B3/2P1, -5B4/2P, -5B6/2P, -5B4/P1, -5B4/2P1, and -5B9/2P turbofan engines. These engines are installed on, but not limited ...
AD 2008-25-06
Effective 2008-12-26
Airbus Model A319, A320, and A321 Series Airplanes Equipped With International Aero Engines (IAE) Model V2500-A1 Engines or Model V25xx-A5 Series Engines
This AD applies to all Airbus Model A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-231, and A321-232 series airplanes, certificated in any category; all serial numbers equipped with International Aero Engine (IAE) Model V2500-A1 engines or Model V25xx-A5 series engines. (The "xx" is used in ...
AD 2008-22-10
Effective 2008-12-19
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category, all certified models; all serial numbers which have received an original French or German (as applicable) standard airworthiness certificate or original French or German (as applicable) export certificate of airwo...
AD 2008-17-12
Effective 2008-10-02
Airbus Model A318, A319, A320, and A321 Series Airplanes Equipped With Certain Northrop Grumman (Formerly Litton) Air Data Inertial Reference Units
We are issuing this AD to prevent failure of an ADIRU during flight, which could result in loss of one source of critical attitude and airspeed data and reduce the ability of the flightcrew to control the airplane.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category; equipped with at least one Northrop Grumman (formerly Litton) air data inertial reference unit (ADIRU), part number (P/N) 465020-0303-0307, -0308, - 0309, -0312, -0314, -0315, or -0316; except airplanes equipped w...
AD 2008-09-16
Effective 2008-06-06
Airbus A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus A318, A319, A320, and A321 series airplanes, certificated in any category, all certified models, all manufactured serial numbers (MSN) up to and including MSN 2860.
AD 2008-05-12
Effective 2008-04-16 · recurring
Airbus Model A318, A319, A320, and A321 Airplanes
We are issuing this AD to detect and correct wear of the inboard flap trunnions, which could lead to loss of flap surface control and consequently result in the flap detaching from the airplane.
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Airbus Model A318-111, -112, -121, and -122 airplanes on which Airbus Modification 26495 has been incorporated in production. (2) All Airbus Model A319-111, -112, -113, -114, -115, -131, - 132, and ...
AD 2008-04-20
Effective 2008-04-03
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category, all certified models, all serial numbers, on which Airbus A318/A319/A320/A321 Maintenance Review Board Report (MRBR) zonal tasks ZL-540-02 and ZL-640-02 (for MRBR up to Revision 7) or MRBR zonal task ZL-540-02-1 or ZL-5...
AD 2007-25-12
Effective 2008-01-14 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category, except those identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Manufacturer serial numbers (MSNs) 2389, 2392, 2393, 2396, 2398, 2403, 2405, 2407, 2409, 2410, 2411, 2413 through 2439, 2441, and MSNs above ...
AD 2007-17-14
Effective 2007-10-02 · recurring
Airbus Model A321 Series Airplanes
This AD applies to Airbus Model A321 series airplanes; all certified models; certificated in any category; equipped with Messier-Goodrich S.A. or Goodrich-Messier Inc., main landing gear (MLG) wheel assemblies having part number (P/N) C20500000 or P/N C20452000.
AD 2007-06-05
Effective 2007-03-30
Airbus Model A318, A319, A320 and A321 Airplanes
This AD applies to Airbus Model A318-111 and -112; A319-111, -112, -113, -114, and -115; A320-111, -211, -212, and -214; and A321-111, -112, -211, -212, and -213 airplanes; certificated in any category; all serial numbers, which have CFM International CFM56-5A or CFM56-5B series engines installed.
AD 2006-25-15
Effective 2007-01-19
Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
We are issuing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.
This AD applies to Sicma Aero Seat third occupant seat assemblies, 133 series, with the part numbers (P/Ns) and serial numbers (SNs) in the following Table 1: Table 1.--Applicable Seat Assemblies Seat P/N Seat SN 1330622-070: 1 through 212. 1330622-070-1: 1 through 212. 1330622-070-2: 1 through 6. 1330622-100: 1 throug...
AD 2006-25-01
Effective 2007-01-08 · recurring
International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 Turbofan Engines
We are issuing this AD to prevent failure of the No. 3 bearing, which could result in an IFSD and smoke in the cockpit and cabin.
This AD applies to International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines with engine serial numbers V10601 through V11335 inclusive and bearings part number (P/N) 2A1165 installed. These engines are installed on, but not limited to, Airbus Indust...
AD 2006-22-04
Effective 2006-12-04
Airbus Model A318-100 and A319-100 Series Airplanes; Model A320-111 Airplanes; Model A320-200, A321-200, A330-200, A330-300, A340-200, and A340-300 Series Airplanes; Model A340-541 Airplanes; and Model A340-642 Airplanes; Equipped With Certain Sogerma-Services Powered Seats
We are issuing this AD to prevent uncommanded movement of the pilot's or co-pilot's seat during takeoff or landing, which could result in interference with the operation of the airplane and consequent temporary loss of airplane control.
This AD applies to the airplanes identified in Table 1 of this AD, certificated in any category; equipped with any Sogerma- Services pilot or co-pilot seat identified in Sogerma-Services Service Bulletin TAAI1-25-617, dated February 1, 2005, excluding any seat having part number (P/N) TAAI3-03PE00-01, TAAI3-03PE01-01, ...
AD 2006-09-11
Effective 2006-06-16 · recurring
Airbus Model A319-100, A320-200, A321-100, and A321-200 Series Airplanes
We are issuing this AD to detect and correct corrosion and damage on the lower part of the lavatory walls, which could compromise the structural integrity of the CAS attachments, and cause injury to the cabin attendants during a crash landing.
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 231, -232, and -233 airplanes; Model A321-111, -112, and -131 airplanes; and Model A321-211 and -231 airplanes; certificated in any category; equipped with the lavatories in Table 1 of this AD...
AD 2006-08-03
Effective 2006-05-18
Sicma Aero Seat (Formerly Farner); Cabin Attendant Seats Series 150 Type FN and Series 151 Type WN
We are issuing this AD to prevent injury resulting from contact with the bottom folding mechanism.
This AD applies to Sicma Aero Seat (formerly Farner) cabin attendant seats series 150 type FN and 151 type WN, all part and serial numbers. These attendant seats are installed on, but not limited to, Airbus A319, A320, and A321 series airplanes.
AD 2006-07-09
Effective 2006-05-05 · superseded or removed
Airbus Model A318-100 and A319-100 Series Airplanes; Model A320-111 Airplanes; and Model A320-200, A321-100, and A321-200 Series Airplanes
This AD applies to all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; Model A321-111, -112, and -131 airplanes, and Model A321-211, -212, -213, -231 and -232 airplane...
AD 2006-07-05
Effective 2006-05-04
Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-131, -231, and -232 Airplanes
We are issuing this AD to prevent structural failure of the secondary load path of the forward engine mount, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane.
This AD applies to Airbus Model A319-131, -132, and -133 airplanes; Model A320-232 and -233 airplanes; and Model A321-131, - 231, and -232 airplanes; certificated in any category; as identified in Airbus All Operators Telex (AOT) A320-71A1036, Revision 1, dated June 28, 2005.
AD 2006-07-03
Effective 2006-05-04
Airbus Model A321-100 and -200 Series Airplanes
We are issuing this AD to prevent a punctured fuel tank, which could cause damage to the airplane or injury to passengers.
This AD applies to Airbus Model A321-111, -112, and -131 airplanes; and Model A321-211 and -231 airplanes; certificated in any category; including airplanes modified in production by Airbus Modification 24982, but excluding airplanes modified in production by Airbus Modification 30046.
AD 2006-06-15
Effective 2006-05-01
Airbus Model A318-100 Series Airplanes; Model A319-100 Series Airplanes; Model A320-111 Airplanes; Model A320-200 Series Airplanes; Model A321-100 Series Airplanes; and Model A321-200 Series Airplanes
This AD was prompted by a report indicating that, during a test of the fire extinguishing system, air leakage through the water drain valves in the forward and aft cargo doors reduced the concentration of fire extinguishing agent to below the level required to suppress a fire.
This AD applies to the Airbus airplanes identified in Table 1 of this AD, certificated in any category. Table 1.--Applicability But not having the following Having the following Or the following Airbus Airbus Airbus model-- Airbus modification service bulletin modification installed in production-- incorporated in serv...
AD 2006-06-14
Effective 2006-05-01 · superseded or removed
Airbus Model A318-100 and A319-100 Series Airplanes, A320-111 Airplanes, A320-200 Series Airplanes, and A321-100 and A321-200 Series Airplanes
We are issuing this AD to prevent an ignition source in the wing fuel tank in the event of a lightning strike, which could result in a fire or explosion.
This AD applies to Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; A320-111 airplanes; Model A320-211, -212, -214, -231, - 232, and -233 airplanes; Model A321-111, -112, and -131 airplanes; and Model A321-211, -212, -213, -231, and -232 airplanes; certif...
AD 2006-03-10
Effective 2006-03-16 · superseded or removed
Airbus Model A318-100 and A319-100 Series Airplanes; A320-111 Airplanes; A320-200 Series Airplanes; and A321-100 and A321-200 Series Airplanes
We are issuing this AD to prevent contact between the horizontal hinge pin and the adjacent electrical wire harness, which could result in damage to electrical wires, and consequent arcing and/or failure of associated systems.
This AD applies to Airbus Model A318-111 and -112; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-111, -211, -212, -214, -231, -232, and -233; and A321-111, -112, -131, -211 and -231 airplanes; certificated in any category; serial numbers (S/Ns) 1 through 2396 inclusive, except S/Ns 2104, 2143, 2248, 2270...
AD 2005-26-07
Effective 2006-01-11
Airbus Model A318-100, A319-100, A320-200, A321-100, and A321-200 Series Airplanes; and Model A320-111 Airplanes
This AD applies to all Airbus Model A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319- 132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, and A321-231 airplanes; certificated in any category.
AD 2005-24-06
Effective 2005-11-30 · superseded or removed
Airbus Model A318-100, A319-100, A320-200, A321-100, and A321-200 Series Airplanes, and Model A320-111 Airplanes
We are issuing this AD to prevent landings with the NLG turned 90 degrees from centerline, which could result in reduced controllability of the airplane.
This AD applies to all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, and -231 airplanes; certificated in any category.
AD 2005-23-05
Effective 2005-12-19 · recurring
Airbus Model A319-100, A320-200, and A321-100 and -200 Series Airplanes
This AD was prompted by development of a new, improved modification of the telescopic girt bar of the escape slide/raft assembly.
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-211, -212, -214, -231, -232, and - 233; and A321-111, -112, -131, -211, and -231 airplanes; certificated in any category; equipped with telescopic girt bars of the escape slide/raft assembly installed per Airbus Modification 20...
AD 2005-20-28
Effective 2005-11-16
Airbus Model A319-100 Series Airplanes; Model A320-111 Airplanes; Model A320-200 Series Airplanes, and Model A321-100 and -200 Series Airplanes
This AD was prompted by information that the existing system design for interconnection of the EPSUs of the FPEEPMS does not provide adequate floor path lighting and marking for safe evacuation of the airplane in the event of an emergency.
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, - 214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211 and -231 airplanes; certificated in any category; in which the floor proximity emergency escape path marking system (F...
AD 2005-20-17
Effective 2005-11-09
Airbus Model A319-100 Series Airplanes; Model A320-111 Series Airplanes; Model A320-200 Series Airplanes; and Model A321-100 and -200 Series Airplanes
This AD was prompted by a report of failure of the parking brake while the airplane was on the holding point of the runway before takeoff, leading to a runway departure.
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, - 214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211 and -231 airplanes; certificated in any category; except those modified in production by Airbus Modification 30062.
AD 2005-19-14
Effective 2005-10-26 · superseded or removed
Airbus Model A318-100, A319-100, A320-200, A321-100, and A321-200 Series Airplanes; and Model A320-111 Airplanes
This AD was prompted by results of fuel system reviews conducted by the manufacturer.
This AD applies to Airbus Model A318-111 and -112 airplanes; A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and A321-111, -112, -131, -211 and -231 airplanes; certificated in any category; except airplanes that have received Airbus Modificat...
AD 2005-17-08
Effective 2005-09-27 · recurring
Airbus Model A321 Series Airplanes
This AD was prompted by a report that an operator found it impossible to lock emergency doors 2 and 3 in the open position.
This AD applies to Airbus Model A321 series airplanes, certificated in any category; except for those airplanes that have received Airbus Modification 33426 in production.
AD 2005-12-19
Effective 2005-07-29
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report that, during a test of the fire extinguishing system, air leakage around the temperature sensor for the aft cargo compartment reduced the concentration of fire extinguishing agent to below the level required to suppress a fire.
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category; as identified in Table 1 of this AD. Table 1.--Applicability But not having Having the Or the following the following following Airbus Airbus service Airbus Airbus model modification bulletin modification installed in i...
AD 2005-12-07
Effective 2005-06-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report of a crack found in the forward lug of the right-hand main landing gear (MLG) rib 5 fitting during greasing of the MLG pintle bearings.
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category; except those on which Airbus Modification 32025 was done during production.
AD 2005-10-04
Effective 2005-06-15 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the MLG side-stay cuff lugs or down-lock spring attachments, which could result in improper down-lock of the MLG during a freefall extension, and possible collapse of the MLG.
Airbus Model A319, A320, and A321 series airplanes; certificated in any category; except those airplanes on which Airbus Modification 30648 has been installed.
AD 2005-07-14
Effective 2005-05-12
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by a report of a broken piston rod bearing of the spoiler servo control.
This AD applies to all Airbus Model A318, A319, A320, and A321 series airplanes; certificated in any category.
AD 2005-06-06
Effective 2005-04-22
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report of an explosion in the APU compartment which blew open the compartment doors.
This AD applies to Airbus Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any Hamilton Sundstrand Auxiliary Power Unit (APU) alternating current (AC) generator having part number 5906732, 5909006, or 5910047; with up to amendment 17 included; on which Airbus Modification 32614 h...
AD 2005-02-09
Effective 2005-03-03 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To ensure continued structural integrity of these airplanes.
AD 2004-26-07
Effective 2005-02-10
Airbus Model A318, A319, A320, and A321 Series Airplanes Equipped With Air Cruisers/Aerazur Forward and Aft Passenger Door Emergency Escape Slides
This AD was prompted by manufacturer testing that has shown contact between the inflation hose and fabric roll, within a short period of time after inflation of the emergency escape slides, can rupture the inflation hose at its end fittings.
This AD applies to Airbus Model A318-111 and -112 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 series airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 series airplanes; and Model A321-111, -112, -131, -211, and -231 series airplanes; certificated in any category; equi...
AD 2004-25-11
Effective 2005-01-13
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by underlying safety issues involved in fuel tank explosions on several large transport airplanes.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes; certificated in any category; except those airplanes on which Airbus Modification 33518 has been accomplished in production.
AD 2004-25-08
Effective 2004-12-22 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by a report indicating that an airplane lost the integrated standby instrument system (ISIS), then, during the same flight, lost all electronic instrument system (EIS) display units.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category; on which Airbus Modification 27620 (reference Airbus Service Bulletin A320-34-1261) has been done.
AD 2004-23-18
Effective 2005-01-03
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by data showing that the magnetic variation table installed in the Honeywell inertial reference system (IRS) is obsolete at certain airports.
This AD applies to Model A319, A320, and A321 series airplanes; certificated in any category; equipped with a Honeywell air data inertial reference unit (ADIRU) having any part number (P/ N) listed in Table 1 of this AD; on which Airbus Modification 30652, 30941, or 30942 has not been done. Table 1.--Honeywell ADIRU P/...
AD 2004-20-05
Effective 2004-10-15
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by reports of the brief but total loss of all liquid crystal display (LCD) units during cruise on airplanes equipped with a certain EIS2 standard of electronic instrument system.
This AD applies to airplanes, certificated in any category, that are listed in Table 1 of this AD. Table 1.--Applicability Modified by Airbus Or Airbus service Airbus model-- modification-- bulletin-- A318, A319, A320, and A321 30368 or 31495: A320-31-1193, dated series airplanes. October 1, 2003; or A320-31A1198, date...
AD 2004-15-14
Effective 2004-08-13
Airbus Model A319-131, -132, and -133; A320-231, -232, and -233; and A321-131 and -231 Series Airplanes
This AD was prompted by reports of intermittent interruption of the electrical power supply due to fretting and consequent arcing of the electrical harness of the integrated drive generator (IDG) at the pin-to-socket connector at the firewall.
This AD applies to Airbus Model A319-131, -132, and -133; A320-231, -232, and -233; and A321-131 and "231 series airplanes; certificated in any category; except those airplanes on which Airbus Modification 32943 has been incorporated in production.
AD 2004-14-23
Effective 2004-08-23
Airbus Model A319-111, -112, -113, and -114; A320-111, -211, -212, and -214; and A321-111, -112, and -211 Series Airplanes
To prevent inadvertent deployment of the thrust reverser door, which could result in reduced controllability of the airplane.
Model A319-111, -112, -113, and -114; A320-111, - 211, -212, and -214; and A321-111, -112, and -211 series airplanes; certificated in any category; powered by CFM56-5A or -5B engines having any thrust reverser blocker door actuator part number D23090000-6.
AD 2004-12-19
Effective 2004-07-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition of the input filter capacitors of the transformer rectifier unit (TRU) in position 2 of the avionics compartment, which could potentially result in smoke in the cockpit.
Model A319, A320, and A321 series airplanes, certificated in any category; except those airplanes on which Airbus Modification 30737 has been accomplished in production (reference Airbus Service Bulletin A320-24-1099, Revision 02, dated February 11, 2003, in service).
AD 2004-12-08
Effective 2004-07-23
International Aero Engines (IAE) AG V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
This airworthiness directive (AD) is applicable to International Aero Engines AG (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527- A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. These engines are installed on, but not limited to, Airbus Industrie A319, A320, and A321 series, and McDonne...
AD 2004-11-13
Effective 2004-06-23 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Model A318, A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-09-06
Effective 2004-06-02 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
All Model A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-07-02
Effective 2004-04-14 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
To detect and correct cracking in a main landing gear (MLG) sliding tube, which could result in failure of the sliding tube, loss of one axle, and consequent reduced controllability of the airplane.
All Model A318, A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-06-03
Effective 2004-04-22
Airbus Model A319, A320, and A321 Series Airplanes
To prevent jamming of the ram air turbine (RAT) actuator in an emergency which requires deployment of the RAT, and consequent loss of hydraulic and electrical power in the airplane.
Model A320 series airplanes which have received modification 27189; Model A319 series airplanes; and Model A321 series airplanes, provided that none has received modification 30978 or 28413; certificated in any category.
AD 2004-06-02
Effective 2004-04-22
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of a lower guide rod fitting, which could cause a rear passenger door to jam during opening, delaying an emergency evacuation and resulting in injury to passengers or crew members.
Model A319, A320, and A321 series airplanes; certificated in any category; on which Airbus Modification 30821 has not been accomplished.
AD 2004-03-33
Effective 2004-04-07
Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, A300 B4-600R, and A300 F4-600R Series Airplanes (Collectively Called A300-600); Model A310 Series Airplanes; Model A319, A320, and A321 Series Airplanes; Model A330-301, -321, -322, -341, and -342 Airplanes; and Model A340 Series Airplanes
To prevent loss or fluctuation of indicated airspeed, which could result in misleading information being provided to the flightcrew.
The series airplanes, certificated in any category, listed in Table 1--Applicability. Table 1.-- Applicability Excluding Airplanes Model and Series-- Excluding Airplanes Modified per-- Equipped With-- A300 B2 and A300 B4: Airbus Modification 12236 in service (reference None. Airbus Service Bulletin A300-34-0166, dated ...
AD 2004-03-02
Effective 2004-02-18 · superseded or removed
Airbus Model A321 Series Airplanes
To prevent roll oscillations during approach and landing in certain icing, crosswind, and turbulent conditions, which could result in reduced controllability of the airplane.
All Model A321 series airplanes, certificated in any category.
AD 2004-01-03
Effective 2004-02-13
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; certificated in any category; except those on which Airbus Modification 27142 has been incorporated during production.
AD 2003-26-03
Effective 2004-01-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes Equipped With Certain Litton Air Data Inertial Reference Units
To prevent failure of ADIRU 3 during flight, which could result in loss of one source of critical attitude and airspeed data and reduce the ability of the flightcrew to control the airplane.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with Litton air data inertial reference units (ADIRU) installed per Airbus Modification 24852, 25108, 25336, 26002, or 28218; except those airplanes on which Airbus Modification 30650 or 30872 has been accomplished.
AD 2003-25-04
Effective 2004-01-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition sources and consequent fire/explosion in the fuel tank.
Model A319, A320, and A321 series airplanes; certificated in any category; excluding those on which Airbus Modifications 27150, 27955, and 27472 have been installed.
AD 2003-18-06
Effective 2003-10-16 · superseded or removed
Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 Series Airplanes
To prevent separation of the engine fan cowl door from the airplane in flight, which could result in damage to the airplane and hazards to persons or property on the ground.
Model A319-131 and -132; A320-231, -232, and - 233; and A321-131 and -231 series airplanes; certificated in any category; except those airplanes on which the following have been incorporated: Airbus Modifications 21948/P6222 and 30869 in production; Airbus Modifications 24259/P6222 and 30869 in production; Airbus Modif...
AD 2003-17-14
Effective 2003-10-07
Airbus Model A300 B2 and B4; A300 B4-600, A300 B4-600R, and A300 F4-600R (Collectively Called A300-600); A310; A319; A320; A321; A330; and A340 Series Airplanes; Equipped With PPG Aerospace Windshields
To prevent failure of both structural plies of the windshield caused by overheating of the power lead wire, which could cause reduced structural integrity of the windshield assembly, and consequent loss of the windshield during flight.
Airplanes listed in Table 1 of this AD, certificated in any category, as follows: Table 1.--Applicability Equipped with PPG aerospace windshields having-- Model And serial numbers Part number (P/N) (S/N) as listed in A300 B2 and B4 series NP-175201-1, NP- Airbus All Operators airplanes. 175201-2, or NP- Telex A300-56A0...
AD 2003-16-07
Effective 2003-09-12 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent moisture ingression and delamination of the cockpit lateral fixed windows, which could result in the loss of the outer glass ply and consequent damage to the airplane and injury to people or damage to property on the ground.
Model A319, A320, and A321 series airplanes, certificated in any category, equipped with PPG Aerospace cockpit lateral fixed windows having part number (P/N) NP-165313-1 or NP- 165313-2, and having a serial number (S/N) below 95001H0001 (PPG Aerospace manufacturing date before January 1, 1995).
AD 2003-11-23
Effective 2003-06-20 · superseded or removed
International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, and V2530-A5 Turbofan Engines
This AD was prompted by reports of No. 3 bearing failures that resulted in in-flight shutdowns (IFSDs) and smoke in the cockpit and cabin.
This AD is applicable to International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, and V2530-A5 turbofan engines with a serial number (SN) from V10600 through V11250 inclusive. These engines are installed on, but not limited to, Airbus Industries A319, A320, and A321 series airplanes.
AD 2003-10-14
Effective 2003-06-09
Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-231 Series Airplanes; Equipped With International Aero Engines (IAE) V2500-A5 Series Engines
to prevent smoke caused by an oil filter clog from entering the cabin during flight.
All Airbus Model A319-131, -132, and -133; A320- 232 and -233; and A321-231 series airplanes; certificated in any category; equipped with International Aero Engines (IAE) V2500-A5 series engines.
AD 2002-18-01
Effective 2002-10-10
Airbus Model A320 and A321 Series Airplanes
To prevent damage caused by water ingress into the elevator, which could lead to debonding of the elevator skins and degradation of the initial protection and consequent reduced structural integrity of the airplane.
Model A320 and A321 series airplanes, certificated in any category; having elevator part and serial numbers listed in Airbus Service Bulletin A320-55-1024, dated January 13, 1999; excluding those modified per Airbus Modification 23558.
AD 2002-10-06
Effective 2002-06-24
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous display of decision height information to the flightcrew during final approach, which could result in an increased risk of collision with terrain.
Model A319, A320, and A321 series airplanes without Airbus Modification 26017; certificated in any category.
AD 2002-08-13
Effective 2002-05-08 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent loss of the yellow hydraulic system, which provides all the hydraulics for certain spoilers; elements of the hydraulics for flaps, stabilizer, pitch and yaw feel systems, pitch and yaw autopilot, and yaw damper; and elevator, rudder, and aileron.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2002-06-01
Effective 2002-05-28 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the pintle fitting bearing, and consequent collapse of the main landing gear (MLG) during landing.
Model A319, A320, and A321 series airplanes, certificated in any category, except those on which Airbus Service Bulletin A320-32-1213, dated March 21, 2000 (reference Airbus Modification 28903 or 30044) has been accomplished.
AD 2002-06-53
Effective 2002-04-29
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes Equipped With Certain Thales Avionics Digital Distance and Radio Magnetic Indicators (DDRMIs)
To prevent failure of the DDRMI, which could cause the loss of data from the affected computers to other systems and degradation or total failure of the computers, leading to reduced ability to control the airplane in adverse conditions.
Model A319, A320, and A321 series airplanes equipped with Thales Avionics Digital Distance and Radio Magnetic Indicators (DDRMIs) having part numbers specified in paragraph 3.2 of Airbus All Operator Telex (AOT) A320-34A1262, dated March 19, 2002; Model A330 series airplanes equipped with Thales Avionics DDRMIs having ...
AD 2002-03-11
Effective 2002-03-19 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the bonds of the vertical stabilizer spar box to the skin, which could lead to reduced structural integrity of the spar boxes.
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-55A1027, dated May 13, 2000, Revision 01, dated August 1, 2000, or Revision 02, dated February 13, 2001; except those airplanes on which Airbus Service Bulletin A320-55-1028, Revision 02, dated July 26, ...
AD 2002-01-18
Effective 2002-03-06
Airbus Model A319, A320, and A321 Series Airplanes
To prevent corrosion of the trigger spring on the slide bar of the forward and aft passenger doors, which could result in incorrect locking of the slide bar during deployment of the escape slide and lead to a delay in evacuating passengers in an emergency.
Model A319, A320, and A321 series airplanes; all serial numbers having received Airbus Modification 20234 (Airbus Service Bulletin A320-25-1055) (installation of telescopic girt bar for slide raft), but NOT having received Airbus Modification 28212 (Airbus Service Bulletin A320-52-1102, Revision 01, dated November 25, ...
AD 2002-01-14
Effective 2002-01-22
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-35-1022, dated June 27, 2001.
AD 2001-26-21
Effective 2002-02-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent faulty operation of the low-pressure solenoid valve for the oxygen supply, which could prevent oxygen from being supplied to the airplane crew when needed, such as in the event of smoke in the cabin or rapid depressurization of the airplane.
Model A319, A320, and A321 series airplanes; on which Modification 21946 (Airbus Service Bulletin A320-35-1003) or 21999 has not been accomplished; certificated in any category.
AD 2001-26-20
Effective 2002-02-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the inability of the flightcrew to open the left- or right-hand sliding window for evacuation in an emergency, due to a window jamming in the closed position.
Model A319, A320, and A321 series airplanes, certificated in any category, as listed in Airbus Service Bulletin A320-56-1007, Revision 01, dated February 9, 2001.
AD 2001-26-10
Effective 2002-01-11 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes, certificated in any category, having manufacturer serial numbers 1035 and 1384 inclusive.
AD 2001-24-05
Effective 2002-01-04
Airbus Model A319, A320, and A321 Series Airplanes
To prevent reduced controllability of the airplane, due to the failure of the rudder artificial feel unit to disengage properly from autopilot mode during approach and landing.
Model A319, A320, and A321 series airplanes, certificated in any category, on which Airbus Modification 28909 was not accomplished during production.
AD 2001-16-09
Effective 2001-09-24 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent excessive vibration of the elevators, which could result in reduced structural integrity and reduced controllability of the airplane.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2001-16-14
Effective 2001-08-31 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the escape slide/raft to deploy correctly, which could result in the slide being unusable during an emergency evacuation and consequent injury to passengers or airplane crewmembers.
Model A319, A320, and A321 series airplanes equipped with telescopic girt bars of the escape slide/raft assembly, as listed in Airbus Industrie All Operators Telex (AOT) A320-52A1111, Revision 01, dated July 23, 2001; certificated in any category.
AD 2001-15-22
Effective 2001-09-10
Airbus Model A319, A320, and A321 Series Airplanes
To prevent injection of 115 volt alternating current (VAC) into 28 volt direct current (VDC) wire bundles, which could result in high voltage conditions within the fuel tank and the potential for damage to equipment, electrical arcing, and fuel vapor ignition on the ground.
Model A319, A320, and A321 series airplanes; certificated in any category; except those on which Airbus Industrie Modification 28289 has been installed.
AD 2001-15-16
Effective 2001-09-04
Airbus Model A319, A320, and A321 Series Airplanes
To prevent blockage of the outer door handle flap in an intermediate pushed-in position, which may prevent a passenger door from opening from the inside of the airplane, thereby delaying an emergency evacuation.
Model A319, A320, and A321 series airplanes, up to and including manufacturer's serial number (MSN) 1261, certificated in any category.
AD 2001-15-06
Effective 2001-08-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the ingestion of sill support-log material into the aspirator of the escape slide which could result in failure of the escape slide to inflate.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any emergency evacuation slide having a part number (P/N) listed as: D31516-103 D31516-105 D31516-107 D31516-109 D31517-103 D31517-105 D31517-107 D31517-109
AD 2000-24-08
Effective 2001-01-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent electrical arcing of the fuel boost pump wire, which could result in wing structural damage, or fire and/or fuel vapor explosion.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2000-24-02
Effective 2001-01-08 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent chafing and resultant wear damage on the inboard flap drive trunnions or on the protective half-shells, which could result in failure of the trunnion primary load path, adversely affect the fatigue life of the secondary load path, and lead to loss of the flap.
Model A319, A320, and A321 series airplanes; certificated in any category; except airplanes on which Airbus Modification 26495 (reference Airbus Service Bulletin A320-27-1117) has been accomplished.
AD 2000-22-07
Effective 2000-12-06
International Aero Engines AG (IAE) V2500-A5 and -D5 Series Turbofan Engines
International Aero Engines AG (IAE) V2500-A5 and -D5 series turbofan engines listed by Serial Number (S/N) as follows: V10011 V10035 V10036 V10039 V10040 V10041 V10054 V10067 V10079 V10080 V10084 V10111 V10121 V10123 V10124 V10130 V10131 V10139 V10166 V10172 V10174 V10180 V10199 V10221 V10341 V20001 V20013 V20017 V2001...
AD 2000-14-15
Effective 2000-08-28 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition sources and consequent fire/explosion in the fuel tank.
Model A319, A320, and A321 series airplanes; certificated in any category; excluding those on which Modifications 27150 and 27955 have been installed.
AD 2000-12-13
Effective 2000-07-24
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous navigational calculations, which could result in an increased risk of collision with terrain or other airplanes.
Model A319, A320, and A321 series airplanes; certificated in any category; on which any of the Airbus modifications has been installed or any of the Airbus service bulletins has been accomplished, as listed in the following table; except those airplanes on which Airbus Modification 26716, 26799, 26968, or 27831 has bee...
AD 2000-12-04
Effective 2000-07-19 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent fatigue cracking of the fuselage frames and frame feet, and consequent reduced structural integrity of the fuselage.
Model A319, A320, and A321 series airplanes, certificated in any category; except those on which Airbus Modification 25896, 25592, or 25593, or Airbus Service Bulletin A320-53-1128, Revision 01, dated October 4, 1999, has been accomplished.
AD 2000-11-27
Effective 2000-06-28 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct disbonding of the vertical stabilizer structure, which could result in reduced structural integrity of the spar boxes of the vertical stabilizer.
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-55A1027, dated May 12, 2000.
AD 2000-11-21
Effective 2000-07-18
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the servocontrol piston rod, which could result in reduced controllability of the airplane.
The following models, certificated in any category, excluding those on which Airbus Service Bulletin A320-27- 1126, dated April 26, 1999 (for Model A319 and 321 series airplanes); or A320-27-1127, dated April 26, 1999, or Revision 01, dated October 6, 1999 (for Model A320 series airplanes); has been accomplished: Model...
AD 2000-11-09
Effective 2000-07-06 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent cracking of the sliding tube subassembly of the main landing gear (MLG), which could result in collapse of the MLG.
Model A319, A320, and A321 series airplanes; manufacturer serial numbers through 0875 inclusive; certificated in any category; except those on which Airbus Service Bulletin A320-32- 1189, dated December 23, 1998, has been accomplished; and except those on which it can be shown that one of the following conditions has b...
AD 2000-10-16
Effective 2000-06-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the bearing, and consequent collapse of the main landing gear (MLG) during landing.
Model A319, A320, and A321 series airplanes, certificated in any category, except those on which Airbus Service Bulletin A320-32-1213, dated March 21, 2000 (reference Airbus Modification 28903 or 30044), has been accomplished.
AD 2000-05-21
Effective 2000-04-27
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes
To prevent position and altitude errors due to bad oscillator warm-up characteristics of the GPSSU, which could result in navigational errors that may exceed 0.5 nautical mile.
Model A319, A320, A321, A330, and A340 series airplanes, certificated in any category, as follows: 1. Model A319, A320, and A321 series airplanes on which Airbus Modification 28578 (Airbus Service Bulletin A320-34-1191, dated July 12, 1999), or Airbus Modification 28579 (Airbus Service Bulletin A320-34-1196, dated July...
AD 2000-05-08
Effective 2000-04-12
Airbus Model A319 and A321 Series Airplanes
To prevent failure of the ram air turbine (RAT) to deploy in an emergency situation, and consequent loss of electrical and hydraulic systems.
Model A319 and A321 series airplanes, certificated in any category; except those on which Airbus Modification 27015 or Airbus Service Bulletin A320-29-1088, dated February 23, 1999, has been accomplished.
AD 2000-04-24
Effective 2000-05-08
Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) Series Auxiliary Power Units
To prevent an uncontained APU failure and damage to the airplane.
Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) series Auxiliary Power Units (APUs), with load compressor impellers, part numbers (P/Ns) 3822270-4, or 3822270-5, installed. These APUs are installed on but not limited to Airbus Industrie A319, A320, and A321 series; Boeing 737-30...
AD 2000-04-11
Effective 2000-03-10
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous display of decision height information to the flight crew during final approach, which could result in an increased risk of collision with the terrain.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with Rockwell Collins radio altimeter LRA 700 having part number (P/N) 622-4542-020; excluding those on which Airbus Modification 26017 (Airbus Service Bulletin A320-31-1106) has been installed.
AD 2000-04-06
Effective 2000-03-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the ingestion of sill support-log material into the aspirator of the escape slide which could result in failure of the escape slide to inflate.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any emergency evacuation slide having a part number (P/N) listed as: D31516-103 D31516-105 D31516-107 D31516-109 D31517-103 D31517-105 D31517-107 D31517-109
AD 2000-02-36
Effective 2000-03-13
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a simultaneous cutoff of the fuel supply to both engines, which could result in a loss of engine power and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; as listed in Airbus Service Bulletin A320-24-1092, Revision 03, dated September 16, 1998; certificated in any category.
AD 99-25-10
Effective 2000-01-12
Airbus Model A319, A320, and A321 Series Airplanes
To prevent structural failure of the forward engine mount secondary load path, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane.
Model A319-131 and -132, A320-232 and -233, and A321-131 series airplanes; except those on which Airbus Modification 27020 has been accomplished (reference Airbus Service Bulletin A320- 71-1021, Revision 01, dated June 10, 1998); certificated in any category.
AD 99-23-09
Effective 1999-12-17
Airbus Model A319, A320, and A321 Series Airplanes
To prevent uncommanded nose landing gear wheel rotation, due to defective seals in the wheel steering selector valve of the hydraulic control unit for the nose landing gear, which could result in reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; except those airplanes on which Airbus Modification 23740 was accomplished during production, and those airplanes on which Airbus Service Bulletin A320-32-1197, dated October 9, 1998, or Revision 01, dated February 11, 1999, has been accomplished; certificated in any categor...
AD 99-21-28
Effective 1999-11-22
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes Equipped With AlliedSignal RIA-35B Instrument Landing System Receivers
To detect and correct faulty ILS receivers and to ensure that the flightcrew is advised of the potential hazard of performing ILS approaches using a localizer deviation from a faulty ILS receiver, and advised of the procedures necessary to address that hazard.
Model A319, A320, A321, A330, and A340 series airplanes; certificated in any category; equipped with AlliedSignal RIA-35B Instrument Landing System (ILS) receivers, part number (P/N) 066-50006-0202; excluding airplanes on which RIA-35B ILS receiver P/ N 066-50006-1202 [Airbus Modification 27251 (for Model A319, A320, a...
AD 99-21-19
Effective 1999-11-17
Airbus Model A319-131, A320-232 and - 233, and A321-131 and -231 Series Airplanes
To prevent failure of the titanium thrust links due to the life limit of the thrust links, which in combination with other failures, could result in the separation of an engine from the airplane.
Model A319-131, A320-232 and -233, and A321-131 and -231 series airplanes; except those airplanes on which Airbus Modification 26506 (reference Airbus Service Bulletin A320-71-1020, dated May 25, 1998) has been accomplished in production; certificated in any category.
AD 99-21-17
Effective 1999-10-28
Airbus Model A321 Series Airplanes
To prevent the loss of structural integrity of the rear part of the fuselage structure in the event of an undetected tail scrape during landing or takeoff.
Model A321 series airplanes, certificated in any category; except those on which Airbus Modification 25791 has been incorporated in production, or on which Airbus Service Bulletin A320-53-1130, dated June 17, 1997, or Revision 01, dated July 8, 1998, has been accomplished in service.
AD 99-20-05
Effective 1999-10-29
Airbus Model A319, A320, and A321 Series Airplanes
To prevent damage to computer electrical connectors due to ingress of water into the avionics bay, which could result in malfunctioning of the avionics computers.
Model A319, A320, and A321 series airplanes, certificated in any category, on which Airbus Modification 25995 has not been accomplished.
AD 99-17-11
Effective 1999-09-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; except airplanes on which Airbus Modification 26495 has been installed in production, or on which Airbus Service Bulletin A320- 27-1117, dated July 31, 1997, or Revision 01, dated June 25, 1999, has been accomplished; certificated in any category.
AD 99-13-01
Effective 1999-06-25
International Aero Engines AG V2500-A1 and V2500-A5 Series Turbofan Engines
To prevent failure of the high pressure turbine (HPT) hardware due to ignition of oil trapped by the HPT stage 1 inner rotating airseal (TOBI ID seal), which could result in an uncontained engine failure and damage to the airplane.
International Aero Engines AG (IAE) V2500-A1 turbofan engines, all serial numbers (S/Ns), and V2500-A5 turbofan engines, with S/Ns V10079 and below, installed on, but not limited to, Airbus Industries A319, A320, and A321 series airplanes.
AD 99-04-03
Effective 1999-04-12
International Aero Engines AG (IAE) V2500-A5/-D5 Series Turbofan Engines
To prevent high pressure compressor (HPC) stage 9-12 drum failure, which could result in an uncontained engine failure and damage to the aircraft.
International Aero Engines AG (IAE) Models V2522- A5, V2524-A5, V2527-A5, V2527E-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5 turbofan engines, installed on but not limited to Airbus Industrie A319, A320, A321 series and McDonnell Douglas MD-90 series aircraft.
AD 99-02-04
Effective 1999-02-19
Airbus Model A320 and A321 Series Airplanes
To prevent failure of the slat and flap control computer (SFCC), which could result in uncommanded slat retraction during takeoff and consequent insufficient wing lift available to complete a successful takeoff.
Model A320 series airplanes, as listed in Airbus Service Bulletin A320-27-1096, Revision 01, dated January 14, 1998; and Model A321 series airplanes, as listed in Airbus Service Bulletin A320-27-1103, dated June 14, 1996; certificated in any category.
AD 99-01-13
Effective 1999-02-12
Airbus Model A319, A320, and A321 Series Airplanes
To prevent simultaneous loss of heating to pitot probes 1 and 3, which could result in incorrect airspeed indications to both the pilot's and first officer's airspeed indication systems, and reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; excluding airplanes on which Airbus Modification 26403 or Airbus Service Bulletin A320-30-1036, Revision 02, dated February 4, 1998, has been accomplished; certificated in any category.
AD 98-26-03
Effective 1998-12-31
Airbus Model A321 Series Airplanes
Model A321 series airplanes, except those on which Airbus Modification 27036 has been installed; or on which the action described in Airbus Industrie Service Bulletin A320-25-1199, dated March 25, 1998, has been accomplished; certificated in any category.
AD 98-20-10
Effective 1998-10-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a simultaneous cutoff of the fuel supply to both engines, which could result in a loss of engine power and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; on which Airbus Modification 26065 (reference Airbus Service Bulletin A320-24-1092, Revision 01, dated December 24, 1997) has not been accomplished; certificated in any category.
AD 98-19-08
Effective 1998-10-07
Airbus Model A321 Series Airplanes
To prevent the use of erroneous automatic roll-out guidance generated by the flight management and guidance computer, which could result in the airplane departing the runway upon landing.
Model A321 series airplanes, certificated in any category, as identified below: Model A321 series airplanes equipped with CFM engines, on which Airbus Modification 25199 (reference Airbus Service Bulletin A320-22-1045) has been installed, except for those on which Airbus Modification 25469 (reference Airbus Service Bul...
AD 98-20-04
Effective 1998-10-26
Airbus Model A319, A320, and A321 Series Airplanes
To prevent water contamination of the avionics computers, which could result in the display of erroneous or misleading information to the flightcrew, and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; equipped with Monogram rinse valves having part number (P/N) 15800- 348, Revision C; and on which Airbus Modification 26145 (reference Airbus Service Bulletin A320-38-1049) has not been accomplished; certificated in any category.
AD 98-16-12
Effective 1998-09-08
Airbus Model A320 and A321 Series Airplanes
To prevent blockage of fuel by the build-up of ice crystals, which could result in low fuel pressure, and consequent shutdown of the engine during critical phases of flight.
Model A320 and A321 series airplanes; as listed in Airbus Service Bulletin A320-28-1044, Revision 10, dated November 5, 1996; certificated in any category.
AD 98-15-06
Effective 1998-08-20 · recurring
Airbus Model A320 and Model A321 Series Airplanes
To prevent jamming of the passenger/crew door, which could delay or impede the evacuation of passengers during an emergency.
Model A320 and Model A321 series airplanes, as listed below, certificated in any category: On which Airbus Modification 24497 has not been installed in production. Or On which Airbus Service Bulletin A320-52-1027, Revision 2, dated February 18, 1993, Revision 3, dated December 10, 1993, or Airbus Service Bulletin A320-...
AD 98-14-11
Effective 1998-08-12 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the bearing, and consequent collapse of the main landing gear (MLG) during landing.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 98-09-18
Effective 1998-06-03
Airbus Industrie Model A320 and A321 Series Airplanes
To prevent situations that could lead to reduced controllability of the airplane due to adverse airplane-pilot coupling characteristics.
Model A320 and A321 series airplanes; as listed in Airbus Service Bulletin A320-27-1082, Revision 1, dated September 6, 1995; certificated in any category.
AD 98-04-11
Effective 1998-03-24
Airbus Model A320 and A321 Series Airplanes
To prevent possible delays in deceleration when landing with strong cross winds and/or on a contaminated runway, which could increase the potential for landing overrun.
Model A320 and A321 series airplanes on which Airbus Modification No. 24745 (Airbus Service Bulletin A320-27-1088, Revision 3, dated December 11, 1996) has not been accomplished, certificated in any category.
AD 98-02-04
Effective 1998-03-23
CFM International CFM56-5B/2P Series Turbofan Engines
To prevent a low cycle fatigue (LCF) failure of the LPT case, which could result in damage to the aircraft.
CFM International (CFMI) CFM56-5B1/2P, -5B2/2P, - 5B3/2P, and -5B4/2P turbofan engines, installed with low pressure turbine (LPT) case, Part Number (P/N) 338-117-004-0, installed on but not limited to Airbus A320 and A321 series aircraft.
AD 97-25-17
Effective 1998-01-20
Airbus Model A320 and A321 Series Airplanes
To prevent output of erroneous radio altimeter height information to the flightcrew and autopilot, due to inadequate antenna solder connections, which could result in reduced ability of the flightcrew to cope with adverse operating conditions.
Model A320 and A321 series airplanes equipped with Collins radio altimeter antennas having part number (P/N) 622- 8701-002 and a serial number below 2014, certificated in any category.
AD 97-23-13
Effective 1997-12-17
Airbus Model A320 and A321 Series Airplanes
To prevent the inability of the slide/slide raft to deploy due to a failure of the passenger door, which could delay or impede passengers when exiting the airplane during an emergency.
Model A320 and A321 series airplanes, as specified in French airworthiness directive 96-171-083(B), dated August 28, 1996, certificated in any category.
AD 97-22-13
Effective 1997-12-05
Airbus Model A320 and A321 Series Airplanes
To prevent severely reduced controllability of the airplane during approach.
Model A320 and A321 series airplanes, on which Airbus Modification 24612 or Airbus Service Bulletin A320-31-1080 has not been accomplished; certificated in any category.
AD 97-21-10
Effective 1997-11-03 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To ensure that the flightcrew detects and corrects an unintended flight path if certain software anomalies of the FMGS occur, which could result in an increased risk of collision with terrain or other airplanes.
Model A319, A320, and A321 series airplanes, certificated in any category; on which any of the following Airbus Modifications have been installed: Affected model(s) Airbus modification installed A319 and A321: 25469 (reference Airbus Service Bulletin A320-22-1054). A319, A320, and A321: 26093. A320: 24065 (reference Ai...
AD 97-03-06
Effective 1997-03-06
Auxiliary Power International Corporation Model APS3200 Auxiliary Power Units
To prevent an APU fire due to ECB malfunction, which could result in damage to the aircraft.
Auxiliary Power International Corporation (APIC) Model APS3200 Auxiliary Power Units (APUs), Assembly Part Number (P/ N) 4500000, incorporating Electronic Control Box (ECB), P/N 4500003E, with software version 2.0.2, and ECB, P/N 4500003F, with software version 3.2. These APUs are installed on but not limited to Airbus...
AD 97-01-09
Effective 1997-01-30 · recurring
Airbus Model A321 Series Airplanes
To prevent the loss of the left and right emergency evacuation slides at emergency exits Number 2 and 3 during flight, which could make these exits unusable in the event of an emergency and also could cause damage to the empennage.
Model A321 series airplanes; as listed in Airbus Industrie All Operator Telex (AOT) 25-11, Revision 01, dated January 8, 1996, and Airbus Service Bulletin A320-25-1167, dated June 24, 1996; on which Airbus Modification 25369 has not been installed; certificated in any category.
Airbus A321: price, specs and every tail
AD data from the Federal Register and the FAA. Data: Radar, FAA aircraft registry file of 2026-10-09.
Records & AD tracking by Radar
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