FAA airworthiness directives

Airbus A320-214 airworthiness directives

394 FAA ADs name the Airbus A320-214: 263 in force, 58 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 2026-17-01
Effective 2026-10-01
Airbus SAS Airplanes
This AD was prompted by a fatigue test that identified cracks in the area of the fastener holes at the forward and aft upper corner of the bulk cargo door at section 16 and 17.
This AD applies to Airbus SAS 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 Union Aviation Safety Agency (EASA) AD 2025-0193, dated September 8, 2025 (EASA AD 2025-019...
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 2025-16-06
Effective 2025-09-22
Airbus SAS Airplanes
This AD was prompted by rivet holes being left unplugged after bracket relocation or removal accomplished during certain modifications, potentially resulting in fatigue damage starting from those rivet holes.
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024- 0204, dated October 22, 2024 (EASA AD 2024-0204). (1) Model A319-112 and -132 airplanes. (2) Model A320-214, -232, -233, -251N,...
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 2024-05-02
Effective 2024-05-08
Airbus SAS Airplanes
This AD was prompted by a quality review of the forward cargo door frame-to-fuselage skin panel assembly identified several drillings as deviating from manufacturing requirements, creating oversized fastener holes.
This AD applies to Airbus SAS Model A320-214, A320-216, A320- 251N, A320-271N, and A321-253NX airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0179, dated October 11, 2023 (EASA AD 2023-0179).
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 2023-25-12
Effective 2024-02-07
Airbus SAS Airplanes
This AD was prompted by a report that the fatigue life limit of the motoreductor, installed on the on-board entrance stairs, is not demonstrated for the complete airplane design service goal (DSG).
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-112 airplanes. (2) Model A319-115, -132, -133, -151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -231, -232, -251N, -252N, -253N, -271N, -272N, and -273N airp...
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 2023-14-05
Effective 2023-09-13
Airbus SAS Airplanes
This AD was prompted by reports that damaged seat rail covers were detected in the forward and aft seat fixation area of some airplanes during initial delivery.
This AD applies to Airbus SAS Model A320-214, -251N, and -271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0166R1, dated December 22, 2022 (EASA AD 2021-0166R1).
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 2022-10-08
Effective 2022-06-07 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports that damaged seat rail covers were detected in the forward and aft seat fixation area of some airplanes during initial delivery.
This AD applies to Airbus SAS Model A320-214, -251N, and -271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0166, dated July 13, 2021 (EASA AD 2021-0166).
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 2017-17-03
Effective 2021-10-05
Airbus SAS Airplanes
This AD was prompted by a report of a crack found during an inspection of the pocket radius of the fuselage frame, and a determination that similar cracks may develop in nearby areas of the fuselage frame and that additional airplanes are subject to the unsafe condition.
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- 0280, dated December 14, 2020 (EASA AD 2020-0280). (1) Model A318-111, -112 and -122 airplanes. (2) Model A319-111, -112, -1...
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 2021-08-13
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 2020-26-01
Effective 2021-01-04 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of cracks that were found on main landing gear (MLG) sliding tubes after improperly performed magnetic particle inspections of the MLG sliding tubes were done.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) 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 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 2020-18-07
Effective 2020-10-09
Airbus SAS Airplanes
This AD was prompted by reports of additional chafing of the forward fuselage underneath the fairing structure.
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 2020-0030, dated February 18, 2020 ("EASA AD 2020- 0030"). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A31...
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 2020-12-16
Effective 2020-09-08
Airbus SAS Airplanes
This AD was prompted by a report that following the installation of a second cargo fire extinguishing bottle, insufficient clearance between the cargo compartment fire extinguishing pipes was found.
This AD applies to Airbus SAS Model A320-214, -216, -231, -232, -233, -251N, and -271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019- 0279R1, dated February 5, 2020 ("EASA AD 2019-0279R1").
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 2020-05-19
Effective 2020-04-24
Airbus SAS Airplanes
This AD was prompted by a report that a possible interference was identified between 1M and 2M wiring harnesses and the tapping units, and that the interference could adversely affect the lavatory smoke detection system and/or the passenger oxygen system.
This AD applies to Airbus SAS Model A319-112, -115, and -132 airplanes; and Model A320-214, -216, -232 and -233 airplanes; certificated in any category; as identified in European Union Aviation Safety Agency (EASA) AD 2019-0227, dated September 11, 2019 ("EASA AD 2019-0227").
AD 2020-05-17
Effective 2020-04-24
Airbus SAS Airplanes
This AD was prompted by a report of marginal clearance between certain fuel sensor covers on rib 24 and the crown of stringer 15 on both left-hand (LH) and right-hand (RH) wings.
This AD applies to Airbus SAS Model A318-112, A319-111, A319- 112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320- 233, A320-251N, and A320-271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (...
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 2020-05-14
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 2020-02-20
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 2019-22-12
Effective 2019-12-31
Airbus SAS Airplanes
This AD was prompted by a report of undetected contacts between certain harnesses of the common fuel quantity indicating system and the center tank structure.
This AD applies to Airbus SAS Model A320-214, -216, -232, and - 233 airplanes, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2018-0155, dated July 20, 2018 ("EASA AD 2018-0155").
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 2019-14-06
Effective 2019-08-23
Airbus SAS Airplanes
This AD was prompted by a report of the fracture of a main landing gear (MLG) sliding tube axle, and an investigation that determined the cause to be an incorrect repair.
This AD applies to Airbus SAS Model A319-111, -112, -115, and - 131 airplanes, and Airbus SAS Model A320-214 and -232 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) Emergency AD 2019-0151-E, dated June 28, 2019 ("EASA Emergency AD 2019-0151-E").
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 2019-03-18
Effective 2019-04-09 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of cracks that were found after improperly performed magnetic particle inspections of the main landing gear (MLG) sliding tubes were done.
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; and Model A320-211, -212, -214, -216, -231, - 232, and -233 airplanes, certificated in any category, all manufacturer serial numbers.
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 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 2018-20-08
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 2018-17-22
Effective 2018-10-04
Airbus SAS Airplanes
This AD was prompted by a report indicating that certain modified airplanes do not have electrical ground wires on the fuel level sensing control unit (FLSCU), which adversely affects the fuel gravity feeding operation.
This AD applies to Airbus SAS Model A319-115 and -132 airplanes, and Model A320-214, -216, -232, and -233 airplanes, certificated in any category, all manufacturer serial numbers on which Airbus modification 154327 has been embodied in production, except those on which Airbus modification 158740 has been embodied.
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 2018-16-12
Effective 2018-09-12
Airbus Airplanes
This AD was prompted by reports of battery retaining rod failures due to quality defects of the material used during parts manufacturing.
This AD applies to Airbus Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, - 216, -231, -232, -233, -251N, and -271N airplanes; and Model A321- 111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category, as identified in Airbus Service B...
AD 2018-15-05
Effective 2018-08-07
Airbus SAS Airplanes
This AD was prompted by reports of safety pins that had been installed on the inflation reservoirs of escape slides/slide rafts during production, but had not been removed and stowed in the stowage pocket of the soft cover of the pack assembly.
This AD applies to Airbus SAS Model A319-115, -132, and -133 airplanes; and Model A320-214, -216, -232, -233, -251N, and -271N airplanes; certificated in any category, having manufacturer serial numbers as identified in Airbus Alert Operators Transmission A25N012-17, Revision 02, dated May 29, 2018.
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 2018-09-09
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 2018-05-11
Effective 2018-03-26
Airbus Airplanes
This AD was prompted by a report that a dynamometric key, previously used for installing the cargo fire extinguishing bottle system, was out of tolerance.
This AD applies to Airbus Model A320-214, -251N, and -271N airplanes, certificated in any category, having manufacturer serial numbers 07126, 07141, 07189, 07200, 07221, 07226, 07235, 07245, 07251, 07256, 07264, 07272, 07279, 07319, 07337 and 07340.
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 2018-02-18
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 2017-25-01
Effective 2018-01-09 · recurring
Airbus Airplanes
This AD was prompted by a report indicating that the lower rib foot angle of the center wing box did not match with the bottom skin panel inner surface.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers on which Airbus Modification 39729 was embodied in production, except those airplanes on which Airbus Modification 152155 or Modification 152200 was embod...
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 2017-14-11
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 2017-12-13
Effective 2017-07-25 · superseded or removed
Airbus Airplanes
This AD was prompted by a report of a crack found during an inspection of the pocket radius of the fuselage frame.
This AD applies to the Airbus Model A320-212 airplane having manufacturer serial number (MSN) 1011; Airbus Model A320-214 airplanes having MSNs 1009, 1026 and 1030; the Airbus Model A320-232 airplane having MSN 0977; and Airbus Model A320-233 airplanes having MSNs 1007 and 1013; 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 2017-08-03
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 2017-06-12
Effective 2017-05-02
Airbus Airplanes
This AD was prompted by a report that fatigue cracking could appear at certain fastener locations in the longeron area below the emergency exit cut-outs.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, except those on which Airbus modification (mod) 152637 has been embodied in production. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes, all manufacturer serial ...
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 2016-25-23
Effective 2017-01-03
Airbus Airplanes
This AD was prompted by a report indicating that, for airplanes on which Airbus modification 154327 (which substitutes the pump fuel feed system from the center fuel tank with a jet pump transfer system) was done, the modified airplanes do not have electrical ground wires on the fuel level sensing control unit (FLSCU), which adversely affects gravity feeding operation.
This AD applies to Airbus Model A319-115 and -132 airplanes, and Model A320-214, -232, and -233 airplanes, certificated in any category, all manufacturer serial numbers on which Airbus modification 154327 has been embodied in production.
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 2016-18-09
Effective 2016-10-13 · superseded or removed
Airbus Airplanes
This AD was prompted by reports of chafing damage on the fuselage skin at the bottom of certain frames, underneath the fairing structure.
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 37878 has been embodied in production, or Airbus Service Bulletin A320-53-1281 has been done in service. (1) Airbus Mo...
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 2016-08-13
Effective 2016-06-08 · recurring
Airbus Airplanes
This AD was prompted by reports of fatigue cracking of the inner rear spar of the wing and also by a determination that the modification of the inner rear spar is necessary to address the unsafe condition.
This AD applies to Airbus Model A320-211, -212, -214, -231, - 232, and -233 airplanes, certificated in any category, all manufacturer serial numbers, except those on which Airbus modification (mod) 24591 has been embodied in production.
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 2016-07-04
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 2016-05-02
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 2015-22-08
Effective 2015-12-10 · superseded or removed
Airbus Airplanes
This AD was prompted by a cracked upper cardan in the main landing gear (MLG).
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) 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 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 2015-15-12
Effective 2015-09-08 · recurring
Airbus Airplanes
This AD was prompted by reports of cracks found during inspections of the in-flight entertainment system radome assembly.
This AD applies to the airplane models identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, with Live TV radomes having part number (P/N) 5063-100-XX (XX designates the color option) and a serial number in the range of 001 through 497 inclusive, and modified by supplemental type...
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 2015-08-08
Effective 2015-05-12 · recurring
Airbus Airplanes
This AD was prompted by a determination that certain airplanes were not included in the applicability of AD 2014-26-53, Amendment 39-18068 (80 FR 3155, January 22, 2015); and AD 2015-03-02, Amendment 39-18098 (80 FR 6897, February 9, 2015).
This AD applies to Airbus Model A319-115, A319-132, A319-133, A320-214, A320-232, and A320-233 airplanes, certificated in any category, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896, 5910, and 5918 and subsequent.
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 2015-03-02
Effective 2015-02-24 · recurring
Airbus Airplanes
This AD was prompted by reports of failure of certain fasteners on the main landing gear (MLG) support rib lower flange.
This AD applies to Airbus Model A319-115, A319-133, A320-214, A320-232, and A320-233 airplanes, certificated in any category, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896, and 5910, and MSNs 5918 and subsequent.
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 2014-26-53
Effective 2015-02-06 · recurring
Airbus Airplanes
This AD was prompted by reports of failure of certain fasteners located at the wing lower skin surface and inboard main landing gear (MLG) support rib lower flange.
This AD applies to Airbus Model A319-115, A319-133, A320-214, A320-232, and A320-233 airplanes, certificated in any category, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896, and 5910, and MSNs 5918 and subsequent.
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 2014-25-07
Effective 2015-01-20 · recurring
Airbus Airplanes
This AD was prompted by a report of cracking at the splice plate of the frame (FR) 47 butt joint crossing area found during full- scale fatigue testing.
This AD applies to Airbus Model A320-211, -212, -214, -231, - 232, and -233 airplanes, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 31012 has been embodied in production.
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 2013-17-09
Effective 2013-10-09 · recurring
Airbus Airplanes
This AD was prompted by reports that certain trimmable horizontal stabilizer actuators (THSA) were found with corrosion that affected the ballscrew lower splines between the tie-bar and screw-jack.
This AD applies to all Airbus Model A318-111, -112, -121, and - 122 airplanes; Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Airbus Model A320-111, -211, -212, -214, - 231, -232, and -233 airplanes; and Airbus Model A321-111, -112, - 131, -211, -212, -213, -231, and -232 airplanes; cert...
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 2013-15-21
Effective 2013-09-24 · recurring
Airbus Airplanes
This AD was prompted by reports of cracks on the side panels of the keel beams.
This AD applies to Airbus Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; and Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; certificated in any category; all manufacturer serial numbers, except those having embodied Airbus modification 30355 in production.
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 2013-13-03
Effective 2013-08-14
Airbus Airplanes
This AD was prompted by a report of two fatigue cracks on the left-hand and right-hand sides of the continuity fittings at the front windshield lower framing on a Model A319 series airplane.
This AD applies to Airbus Model A319-112, -113, and -132 airplanes; Model A320-211, -212, -214, -231, and -232 airplanes; and Model A321-111 and -131 airplanes; certificated in any category; manufacturer serial numbers 0259, 0260, 0264, 0266 through 0270 inclusive, 0275, 0276, 0278, 0287, 0296, 0300, 0303, 0312, 0320, ...
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 2013-07-02
Effective 2013-05-15
Airbus Airplanes
This AD was prompted by fuel system reviews conducted by the manufacturer, which revealed that certain fuel pumps under certain conditions can create an ignition source in the fuel tank.
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; and Model A320-111, -211, -212, -214, -231, -232, and -233 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 2012-21-17
Effective 2012-12-05 · recurring
Airbus Airplanes
This AD was prompted by reports that medium-head fasteners were installed in lieu of shear-head fasteners on a certain upper panel, which manufacturer fatigue and damage tolerance analyses demonstrated could have an effect on panel fatigue life.
This AD applies to Airbus Model A320-214 and -232 airplanes; certificated in any category; manufacturer serial numbers 3456, 3503, 3516, 3529, 3591, 3597, 3611, 3631, 3696, 3698, 3714, 3719, 3775, 3777, 3780, 3782, 3786, 3797, 3805, 3812, 3870, 3907, 3909, 3913, 3922, 3929, 3946, 3953, 3975, 3979, 3991, 4010, 4012, 401...
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 2012-18-12
Effective 2012-10-22
Airbus Airplanes
This AD was prompted by a report of a torn out aspirator due to the aspirator interfering with the extrusion lip of the OWS enclosure during the initial stage of the deployment sequence.
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; and Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; certificated in any category; all manufacturer serial numbers; except for airplanes on which off-wing es...
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 2012-14-05
Effective 2012-08-21
Airbus Airplanes
This AD was prompted by reports of unsuccessful slide deployments during scheduled deployment tests, and failed functional tests of the release travel of the slide release mechanism.
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; and Model A320-111, -211, -212, -214, -231, - 232, and -233 airplanes; certificated in any category; all serial numbers.
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 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 2011-17-02
Effective 2011-09-16
Airbus Model A320-214, -232, and -233 Airplanes
This AD applies to Airbus Model A320-214, -232, and -233 airplanes; all manufacturer serial numbers on which Airbus Modification 38310 has been accomplished in production; 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 2010-24-07
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 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 2009-24-19
Effective 2010-01-08
Airbus Model A320 Series Airplanes
to ensure continued compliance with the certification requirements, it is considered necessary to require compliance by means of an AD. Actions and Compliance (f) Unless already done.
This AD applies to Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 series airplanes, certificated in any category, all certified models, all serial numbers, equipped with Hamilton Sundstrand (formerly Dowty) Ram Air Turbine (RAT) Ejection Jack, Model ERPS13EJ, part number (P/N) 114160004A or 114160005, ex...
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 2009-15-07
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 2008-02-15
Effective 2008-02-28 · recurring
Airbus Model A319 and A320 Series Airplanes
This AD applies to Airbus Model A319 and A320 series airplanes, certificated in any category, all certified models, all serial numbers (MSN); except airplanes identified in paragraphs (c)(1) and (c)(2) of this AD. Model A320 series airplanes MSN 2164 through MSN 2688 that have partially received Airbus Modification 334...
AD 2007-06-17
Effective 2007-04-27
Airbus Model A320 Series Airplanes
We are issuing this AD to prevent rupture of a rudder actuator fitting, which could result in reduced controllability of the airplane.
This AD applies to Airbus Model A320 series airplanes, certificated in any category; except those on which Airbus Modification 21733 or 21999 has been incorporated in production.
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 2006-22-04
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 2006-07-09
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 2006-06-14
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 2005-22-10
Effective 2005-12-05
Airbus Model A320-111 Airplanes, and Model A320-200 Series Airplanes
To prevent excessive vibrations of the elevators, which could result in reduced structural integrity and reduced controllability of the airplane.
Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes, certificated in any category.
AD 2005-20-36
Effective 2005-11-16
Airbus Model A320-111 Airplanes; and Model A320-200, A321-100, and A321-200 Series Airplanes
This AD was prompted by the results of fuel system reviews conducted by the manufacturer.
This AD applies to Airbus 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 airplanes on which Airbus Modification 23645 has been incorporated in production.
AD 2005-19-16
Effective 2005-10-26 · superseded or removed
Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes
We are issuing this AD to prevent an ignition source for fuel vapor in the wing, which could result in fire or explosion in the adjacent wing fuel tank.
This AD applies to Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes, certificated in any category; except those airplanes on which Airbus Modification 25513 has been accomplished in production.
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 2005-17-07
Effective 2005-09-07
Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes
The FAA is issuing this AD to detect and correct missing locking bolts on the axle nuts of the MLG wheels.
This AD applies to Airbus Model A320-111 airplanes, and Model A320-211, -212, -214, -231, -232, and -233 airplanes; certificated in any category; with serial numbers 2275 through 2440 inclusive, 2442 through 2446 inclusive, 2448, 2450, 2452, 2454, 2456 through 2458 inclusive, 2460 through 2474 inclusive, 2476 through 2...
AD 2005-15-07
Effective 2005-08-30 · superseded or removed
Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes
This AD was prompted by the results of fuel system reviews conducted by the manufacturer.
This AD applies to Airbus Model A320-111 airplanes; and Model A320-211, -212, -214, -231, -232, and -233 airplanes; certificated in any category; except those modified in production by Airbus Modification 22626.
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 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 2004-25-03
Effective 2005-02-10 · recurring
Airbus Model A320 Series Airplanes
This AD was prompted by a full-scale fatigue survey on the Model A320 fleet.
This AD applies to Airbus Model A320-111, -211, -212, and - 231 series airplanes on which Airbus Modification 21202 has not been done, certificated in any category.
AD 2004-25-02
Effective 2005-02-10 · recurring
Airbus Model A320 Series Airplanes
This AD was prompted by a full-scale fatigue survey on the Model A320 fleet.
This AD applies to Airbus Model A320-111, -211, -212, and - 231 series airplanes on which Airbus Modification 21346 has not been done, certificated in any category.
AD 2004-23-04
Effective 2004-12-20
Airbus Model A319 and A320 Series Airplanes
To prevent overheating of the fuel probes due to a short circuit, and fuel leakage due to inadequate space for thermal expansion within the additional center tanks, which could result in fuel vapors or fuel contacting an ignition source.
Model A319 and A320 series airplanes, certificated in any category; as listed in Airbus Service Bulletin A320-28-1087, Revision 02, dated June 10, 2003; and Airbus Service Bulletin A320-28-1086, Revision 01, dated October 23, 2002.
AD 2004-19-11
Effective 2004-11-05 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking in certain areas of the rear spar of the wing, which may lead to reduced structural integrity of the wing and the main landing gear (MLG).
Model A320 series airplanes, certificated in any category, except those modified in accordance with Airbus Modification 24591 (Airbus Service Bulletin A320-57-1089, dated December 22, 1996; Revision 01, dated April 17, 1997; Revision 02, dated November 6, 1998; or Revision 03, dated February 9, 2001).
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 2004-13-06
Effective 2004-08-03 · superseded or removed
Airbus Model A319 and A320 Series Airplanes
To detect and correct fatigue cracks on the side panels of the keel beams, which could result in reduced structural integrity of the airplane.
Model A319 and A320 series airplanes, certificated in any category; except those airplanes on which Airbus Modification 30355 has been incorporated in production.
AD 2004-09-19
Effective 2004-06-09 · recurring
Airbus Model A319 and A320 Series Airplanes
Model A319 and A320 series airplanes, certificated in any category; except those on which Airbus Modification 31888 has been accomplished.
AD 2004-06-13
Effective 2004-04-30
Airbus Model A319 and A320 Series Airplanes
To prevent the loss of the emergency evacuation slides during flight, which could result in damage to the fuselage, and to prevent incorrect inflation of the emergency evacuation slides, which could result in the emergency exits being unusable during an emergency evacuation.
Model A319 and A320 series airplanes, certificated in any category; except airplanes that have Airbus Modifications 24850 and 25844 and 27275 installed in production; or that have Airbus Service Bulletin A320-25-1156, Revision 01, dated February 2, 1999; or Revision 02, dated October 26, 1999; and Airbus Service Bullet...
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 2004-05-04
Effective 2004-04-09
Airbus Model A319 and A320 Series Airplanes
To prevent the loss of fuel quantity indication (FQI) of the center fuel tank, and to reduce the potential for an ignition source and possible explosion within the center fuel tank due to electrical arcing between the FQI probes and the adjacent structure in the event that the airplane is struck by lightning.
Model A319 and A320 series airplanes, as listed in Airbus Service Bulletin A320-28A1096, Revision 03, dated August 27, 2002; certificated in any category.
AD 2004-03-06
Effective 2004-03-15 · superseded or removed
Airbus Model A319 and A320 Series Airplanes
To detect and correct fatigue cracks on the wing/fuselage joint cruciform fittings, which could result in reduced structural integrity of the wing/fuselage.
All Model A319 and A320 series airplanes, certificated in any category.
AD 2003-25-07
Effective 2004-01-22 · superseded or removed
Airbus Model A319 and A320 Series Airplanes Equipped With Elevator and Aileron Computer (ELAC) L80 Standard
To prevent activation of the high angle-of-attack protection during final approach for landing, which could result in loss of the ability to flare properly during landings.
Model A319 and A320 series airplanes; certificated in any category; equipped with Elevator and Aileron Computer (ELAC) L80 Standard having part numbers listed in Airbus Service Bulletin A320-27-1135, dated June 29, 2001.
AD 2001-20-16
Effective 2001-10-26
Airbus Model A319 and A320 Series Airplanes
To prevent the airplane from departing the end of the runway during a landing or a rejected takeoff due to reduced braking performance.
Model A319 and A320 series airplanes, certificated in any category, equipped with Goodrich carbon brakes having part number 2-1526-4, 2-1526-5, 2-1572, 2-1600-1, or 2-1600- 2.
AD 2001-17-14
Effective 2001-09-07 · superseded or removed
CFM International CFM56 Series Turbofan Engines
To prevent an LPT conical support from remaining in service beyond its certified cyclic life limit, which could result in an uncontained engine failure and damage to the airplane.
This airworthiness directive (AD) is applicable to CFM International (CFMI) CFM56-5C4/1 series turbofan engines with low pressure turbine (LPT) conical support, part number (P/N) 337-002- 407-0, installed. These engines are installed on, but not limited to Airbus Industrie A320 series airplanes.
AD 2001-08-26
Effective 2001-05-11 · superseded or removed
Airbus Model A319 and A320 Series Airplanes Equipped with Elevator and Aileron Computer (ELAC) L80 Standard
To prevent activation of the high angle-of-attack protection during final approach for landing, which could result in loss of the ability to flare properly during landings.
Model A319 and A320 series airplanes; certificated in any category; equipped with Elevator and Aileron Computer (ELAC) L80 Standard having part numbers listed in Airbus Operator Information Telex (OIT) 999.0036/01/CL, dated March 23, 2001.
AD 2000-14-14
Effective 2000-08-07 · recurring
BFGoodrich Main Brake Assemblies as Installed on Airbus Model A319 and A320 Series Airplanes
To detect and correct thermal oxidation of the main brake assemblies, which could result in deterioration of the main landing gear (MLG) brakes, and consequent reduced braking performance.
Model BFGoodrich main brake assemblies having part number (P/N) 2-1598-1 or P/N 2-1600-1, as installed on Airbus Model A319 and A320 series airplanes, certificated in any category.
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 2000-10-15
Effective 2000-06-30 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking in certain areas of the rear spar of the wing, which may lead to reduced structural integrity of the wing and the main landing gear (MLG).
Model A320 series airplanes, certificated in any category, except those on which Airbus Modification 24591 (Airbus Service Bulletin A320-57-1089, dated December 22, 1996; Revision 01, dated April 17, 1997; or Revision 02, dated November 6, 1998) has been accomplished.
AD 2000-07-27
Effective 2000-05-03
Various Transport Category Airplanes Equipped With Certain Honeywell Air Data Inertial Reference Units
To prevent loss of the main sources of attitude data, consequent high pilot workload, and a significant increase in the likelihood of pilot error.
Transport category airplanes including but not limited to those listed below, certificated in any category; equipped with any Honeywell air data inertial reference unit (ADIRU) having a serial number below 0841 and a part number (P/N) listed below: Airplane manufacturer Model ADIRU P/N Boeing: 757-300 HG2050AC02 737-60...
AD 99-26-22
Effective 2000-02-01 · superseded or removed
Airbus Model A319 and A320 Series Airplanes
To prevent the loss of the escape slides during flight, which could make the emergency exits located over each wing unusable and result in damage to the fuselage.
Model A319 and A320 series airplanes, certificated in any category; except airplanes on which Airbus Modifications 24850 and 25844 have been installed in production, or on which Airbus Service Bulletin A320-25-1156, Revision 01, dated February 2, 1999, has been accomplished.
AD 99-25-07
Effective 1999-12-23
BFGoodrich Main Brake Assemblies as Installed on Airbus Model A319 and A320 Series Airplanes
To prevent thermal oxidation of the main brake assemblies of the main landing gear (MLG), which could result in deterioration of the MLG brakes, and consequent reduced braking performance.
BFGoodrich main brake assemblies having part number (P/N) 2-1598 or 2-1600, as installed on Airbus Model A319 and A320 series airplanes, certificated in any category.
AD 99-25-03
Effective 2000-01-07 · recurring
International Aero Engines AG V2500-A1 Series Turbofan Engines
To prevent high pressure turbine (HPT) disk fracture, which could result in an uncontained engine failure and damage to the airplane.
International Aero Engines AG (IAE) V2500-A1 series turbofan engines, installed on but not limited to Airbus Industrie A320 series airplanes.
AD 99-21-29
Effective 1999-11-22 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent reduced controllability of the airplane due to the failure of the rudder artificial feel unit to properly disengage from autopilot mode.
Model A320 series airplanes, certificated in any category, except airplanes on which Airbus Industrie Modification 22624 has been accomplished or on which Modification 21999 was accomplished in production.
AD 99-20-06
Effective 1999-10-29
Airbus Industrie Model A320 Series Airplanes
To prevent malfunction of the low pressure non-return valve in the airborne ground check module (AGCM) of the ram air turbine (RAT), which could result in loss of the blue hydraulic system, and consequent loss of certain flight control and electrical systems.
Model A320 series airplanes, certificated in any category; except those airplanes on which Airbus Industrie Modification 27728 or 27189 has been installed in production, or on which Airbus Industrie Service Bulletin A320-29-1086 has been accomplished.
AD 99-06-16
Effective 1999-04-21
CFM International CFM56-5 Series Turbofan Engines
To prevent a low cycle fatigue failure of the high pressure turbine rotor (HPTR) front air seal, which could result in an uncontained engine failure and damage to the aircraft.
CFM International CFM56-5 series turbofan engines installed on, but not limited to, Airbus A319 and A320 series aircraft.
AD 99-06-09
Effective 1999-04-16
Airbus Model A320 Series Airplanes
To prevent incorrect distribution of fire extinguishing chemicals in the event of a fire in the cargo compartment, which, if unconfined, could spread beyond the cargo compartment.
Model A320 series airplanes having manufacturer serial numbers 002 through 402 inclusive, on which Airbus Modification 20071 (reference Airbus Service Bulletin A320-26-1020, Revision 1, dated January 4, 1993) has been accomplished; except those airplanes on which Airbus Service Bulletin A320-26-1034, dated May 9, 1995;...
AD 99-05-05
Effective 1999-04-30
International Aero Engines AG (IAE) V2500-A1 Series Turbofan Engines
To prevent a high pressure turbine (HPT) disk fracture, which could result in an uncontained engine failure, and damage to the airplane.
International Aero Engines AG (IAE) Models V2500- A1 turbofan engines, installed on but not limited to Airbus Industrie A320 series airplanes.
AD 99-02-10
Effective 1999-02-23
Airbus Model A320 Series Airplanes
To prevent leakage from hydraulic pipe fittings in the trimmable horizontal stabilizer (THS), which could result in failure of the THS and consequent reduced controllability of the airplane.
Model A320 series airplanes; serial numbers 002 through 008 inclusive, 010 through 014 inclusive, 016 through 078 inclusive, 080 through 104 inclusive, 106 through 363 inclusive, 365 through 384 inclusive, 386 through 411 inclusive, 413 through 433 inclusive, 435 through 457 inclusive, 459 through 467 inclusive, and 46...
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 99-02-03
Effective 1999-02-19
Airbus Model A320 Series Airplanes
To prevent the trickling of water into the avionics compartment, which could result in avionics computer and equipment malfunctions.
Model A320 series airplanes on which Airbus Modification 22119 or 21999 has not been accomplished, certificated in any category.
AD 99-01-19
Effective 1999-02-12 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes on which Airbus Modification 21346 (reference Airbus Service Bulletin A320-53-1031, dated December 9, 1994) has not been accomplished; certificated in any category.
AD 99-01-18
Effective 1999-02-12 · recurring
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes, having manufacturer's serial numbers 002 through 008 inclusive, 010 through 014 inclusive, 016 through 039 inclusive, 041 through 052 inclusive, 054, 056, and 057; on which Airbus Modification 21905 (reference Airbus Service Bulletin A320-53-1056, Revision 02, dated February 16, 1998) has n...
AD 99-01-17
Effective 1999-02-12 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes on which Airbus Modification 21202 (reference Airbus Service Bulletin A320-53-1033, Revision 3, dated July 4, 1994) has not been accomplished, certificated in any category.
AD 98-20-18
Effective 1998-11-30 · superseded or removed
International Aero Engines (IAE) V2500- A1 Series Turbofan Engines
To prevent an HPT disk fracture, an uncontained engine failure, and damage to the aircraft.
International Aero Engines (IAE) V2500-A1 series turbofan engines, with high pressure turbine (HPT) stage 1 disks, part number (P/N) 2A1801, serial numbers (S/Ns) P100430, P100421, P100621, and P100618; HPT stage 1 disk, P/N 2A1101, S/ N P100346; and HPT stage 2 disk, P/N 2A0902, S/N P100381, installed. These engines a...
AD 98-22-05
Effective 1998-11-27 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes on which Airbus Modification 22418 (reference Airbus Service Bulletin A320-57-1043, Revision 02, dated May 14, 1997) has not been accomplished, certificated in any category.
AD 98-21-01
Effective 1998-10-21
International Aero Engines AG (IAE) V2500-A1 Series Turbofan Engines
To prevent fan blade root cracks, which could result in fan blade root failure, an uncontained engine failure, and damage to the aircraft, for those engines that have not previously been inspected in accordance with IAE Service Bulletin (SB) No. V2500-ENG-72-0316, dated May 15, 1998; or No. V2500-ENG-72-0316, Revision 1, dated June 5, 1998; or No.V2500-ENG-72-0316, Revision 2, dated August 28, 1998.
International Aero Engines AG (IAE) V2500-A1 series turbofan engines, installed on but not limited to Airbus A320 series aircraft.
AD 98-20-31
Effective 1998-10-30 · recurring
Airbus Model A320 Series Airplanes
To detect and correct cracking in the pressurized floor pick-up angles at the rear spar of the wing, which could result in reduced structural integrity of the airframe.
Model A320 series airplanes, as listed in Airbus Service Bulletin A320-57-1090, Revision 01, dated June 10, 1997; certificated in any category.
AD 98-20-30
Effective 1998-10-30 · recurring
Airbus Model A320 Series Airplanes Equipped With a Bulk Cargo Door
To prevent fatigue cracking of the upper frame flanges, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes, equipped with a bulk cargo door (Airbus Modification 20029), certificated in any category.
AD 98-20-29
Effective 1998-10-30
Airbus Industrie Model A320 Series Airplanes
To prevent pitch-up of the airplane due to activation of the spoilers during an automatic landing, which, if not corrected, could result in tail strikes and structural damage to the airplane.
Model A320 series airplanes on which Airbus Industrie Modification 23132, 24348, or 24511 has not been accomplished; certificated in any category.
AD 98-19-23
Effective 1998-10-22
Airbus Model A320 Series Airplanes
To prevent the possible loss of data recorded on the DFDR as a result of vibrations and/or accelerations during flight.
Model A320 series airplanes; equipped with a LORAL Digital Flight Data Recorder (DFDR) F800 [part number (P/N) 17M800-251/-261], and on which Airbus Modification 24959 (Airbus Service Bulletin A320-31-1088, Revision 1, dated September 16, 1996) has not been accomplished; certificated in any category.
AD 98-19-18
Effective 1998-10-21
Airbus Model A310, A300-600, and A320 Series Airplanes
Model A310 and A300-600 series airplanes on which Airbus Modification 10156 has not been accomplished (reference Airbus Service Bulletin A310-26-2023 or A300-26-6024), and Model A320 series airplanes on which Airbus Modification 22561 (reference Airbus Service Bulletin A320-26-1017) or Airbus Modification 24548 (refere...
AD 98-18-24
Effective 1998-10-20 · superseded or removed
Airbus Industrie Model A320 Series Airplanes
To correct fatigue cracking in the inner flange of door frame 66, left and right, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes on which Airbus Modification 21778 (reference Airbus Service Bulletin A320-53-1072, dated November 7, 1995, as revised by Change Notice 0A, dated July 5, 1996) has not been accomplished, certificated in any category.
AD 98-18-26
Effective 1998-10-13 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking of the front spar vertical stringers on the wings, which could result in reduced structural integrity of the airframe.
Model A320 series airplanes on which Airbus Modification 21290 (reference Airbus Service Bulletin A320-57-1017, Revision 01, dated March 17, 1997) has not been installed, certificated in any category.
AD 98-18-16
Effective 1998-10-08
Airbus Model A320 Series Airplanes
To prevent structural damage to the tail section when it strikes the runway, which could result in depressurization of the fuselage during flight.
Model A320 series airplanes on which Airbus Modification 22764 has not been installed, certificated in any category.
AD 98-15-04
Effective 1998-08-19 · recurring
Airbus Model A320 Series Airplanes
To prevent fatigue cracking on the bottom flanges of the longitudinal floor beams at frame 43, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes, on which Airbus Modification 20904 (reference Airbus Service Bulletin A320-53-1008, dated March 31, 1995) has not been accomplished, certificated in any category.
AD 98-13-14
Effective 1998-07-30 · superseded or removed
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking of the former junction at frame 68, which could result in reduced structural integrity of the aft fuselage.
Model A320 series airplanes, as listed in Airbus Service Bulletins A320-53-1089 and A320-53-1090, both dated November 22, 1995; on which Airbus Modifications 21780 and 21781 (reference Airbus Service Bulletin A320-53-1090) have not been installed; certificated in any category.
AD 98-12-33
Effective 1998-07-20 · recurring
Airbus Model A320 Series Airplanes
To detect and correct fatigue cracking on the connecting angle between frame 56 and the right-hand frame support at stringer 38, which could result in reduced structural integrity of the airplane.
Model A320 series airplanes, on which Airbus Modification 20941 (reference Airbus Service Bulletin A320-53-1011, dated December 9, 1994) has not been accomplished, certificated in any category.
AD 98-06-20
Effective 1998-04-24
Airbus Model A320 Series Airplanes
To prevent reduced structural integrity of the fuselage, restricted operation of the main landing gear (MLG) free-fall system, and, consequently, reduced ability to use the MLG during an emergency.
Model A320 series airplanes, manufacturer's serial numbers 002 through 008 inclusive, 010 through 078 inclusive, and 080 through 107 inclusive; certificated in any category.
AD 98-04-49
Effective 1998-04-03 · superseded or removed
Airbus Model A320-111, -211, -212, - 214, -231, -232, and -233 Series Airplanes
To detect and correct fatigue cracks on the wing/fuselage joint cruciform fittings, which could result in reduced structural integrity of the wing/fuselage.
Model A320-111, -211, -212, -214, -231, -232, and -233 series airplanes, all serial numbers, certificated in any category.
AD 89-23-06
Effective 1998-01-28 · recurring
CFM International CFM56-2, -3, -3B, - 3C, and -5 Series Turbofan Engines
To prevent a No. 3 bearing failure and subsequent inflight engine shutdown.
CFM International (CFMI) CFM56-2, -3, -3B, -3C, and -5 series turbofan engines, installed on but not limited to Airbus A319 and A320 series, McDonnell Douglas DC-8 series, and Boeing 737 series aircraft.
AD 98-01-17
Effective 1998-02-17
Airbus Model A320 Series Airplanes
To prevent failure of the main landing gear (MLG) to retract properly as a result of failure of a capacitor in the landing gear circuitry and subsequent electrical power interruption.
Model A320 series airplanes on which Airbus Modification 21574 (Airbus Service Bulletin A320-32-1139, Revision 1, dated December 30, 1994) or 21999 has not been installed, certificated in any category.
AD 98-01-12
Effective 1998-02-17 · superseded or removed
Airbus Industrie Model A320 Series Airplanes
To prevent jamming of the upper safety locking pin on the passenger door, which could result in inability to open the passenger door and, consequently, could impede or delay passengers from exiting the airplane during an emergency.
Model A320 series airplanes on which Airbus Industrie Modification No. 24389 (Airbus Industrie Service Bulletin No. A320-52-1057, dated July 26, 1994) has not been accomplished, certificated in any category.
AD 97-11-01
Effective 1997-06-27 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent fatigue cracking in the area where the center fuselage joins the wing, which could reduce the structural integrity of this area and consequently result in rapid decompression of the fuselage.
Model A320 series airplanes as listed in Airbus Service Bulletin A320-53-1026, dated August 5, 1994; on which modifications 21281P1495 and 21680P1818 have not been installed; certificated in any category.
AD 97-07-14
Effective 1997-05-12 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent fatigue cracking in the rib flange of the front spar side of the wing center section, and consequent reduced structural integrity of fuselage frame 36 and the wing center section.
Model A320 series airplanes as listed in Airbus Service Bulletin A320-57-1013, Revision 1, dated September 29, 1992; certificated in any category.
AD 97-05-13
Effective 1997-06-03
CFM International CFM56-5 Series Turbofan Engines
To prevent an air turbine engine starter failure, which could result in damage to the engine electrical harnesses.
CFM International (CFMI) CFM56-5 series turbofan engines, installed with air turbine engine starter, Part Number 301- 781-201-0, installed on but not limited to Airbus A320 series aircraft.
AD 97-05-04
Effective 1997-04-03
Airbus Model A320 Series Airplanes
To prevent loss of the standby emergency generation system, which provides necessary back-up capability when both main generators fail.
Model A320 series airplanes; on which a generator control unit (GCU) having part number (P/N) 520915 has not been installed, or on which Airbus Modification 21052 (reference Airbus Service Bulletin A320-24-1022) and Airbus Modification 21736 (reference Airbus Service Bulletin A320-24-1035) have not been accomplished; c...
AD 97-02-04
Effective 1997-02-26
Airbus Model A300, A300-600, A310, and A320 Series Airplanes
To prevent the loss of brake effectiveness during a high energy rejected takeoff (RTO).
Model A300, A300-600, A310, and A320 series airplanes equipped with Messier-Bugatti, BFGoodrich, Allied Signal (ALS) Aerospace Company (Bendix), or Aircraft Braking Systems (ABS) brakes; certificated in any category.
AD 96-25-07
Effective 1997-01-27 · recurring
Airbus Industrie Model A320 Series Airplanes
To prevent the ram air turbine (RAT) from breaking away from its support leg, which could damage the airplane structure and systems, and could injure ground personnel.
Model A320-111, -211, -212, -214, -231, and -232 series airplanes; on which Airbus Industrie Modification 24701 (as described in Airbus Service Bulletin A320-29-1065, dated February 28, 1995) has not been installed; certificated in any category.
AD 96-25-04
Effective 1997-01-27 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent electrical short circuiting due to chafing of the wire bundles in the wing, horizontal stabilizer, or main landing gear (MLG) bay.
Model A320 series airplanes on which Airbus Modification No. 22109 (Airbus Service Bulletin A320-24-1045, Revision 3, dated June 10, 1993) has not been accomplished; certificated in any category.
AD 96-18-16
Effective 1996-12-09
CFM International CFM56-2/-2A/-2B/-3/- 3B/-3C/-5 Series Turbofan Engines
To prevent a low cycle fatigue (LCF) failure of the low pressure turbine rotor (LPTR) stub shaft and conical support, which could result in an uncontained engine failure and damage to the aircraft.
CFM International (CFMI) CFM56-2/-2A/-2B/-3/-3B/- 3C/-5 series turbofan engines installed on, but not limited to Airbus A319 and A320 series, McDonnell Douglas DC-8 series, and Boeing 737, as well as Boeing E-3, E-6, and KC-135 (military) series aircraft. Note: This airworthiness directive (AD) applies to each engine i...
AD 96-18-12
Effective 1996-10-09
Airbus Model A320 Series Airplanes
To ensure that the proper P-clips are installed.
Model A320 series airplanes, manufacturer's serial numbers 129 through 343 inclusive, 345 through 347 inclusive, and 349 through 363 inclusive; certificated in any category.
AD 96-04-06
Effective 1996-03-25
Airbus Model A320 Series Airplanes
To prevent an electrical overvoltage of the relays, which could result in the loss of the braking/steering control unit (BSCU) systems, and subsequent loss of the antiskid functions and nose wheel steering of the airplane.
Model A320 series airplanes on which Airbus Modification 23611 (reference Airbus Service Bulletin A320-32-1115) has not been installed, certificated in any category.
AD 95-24-08
Effective 1995-12-27
Airbus Model A320 Series Airplanes
To prevent deployment of a thrust reverser during flight, which could adversely affect the controllability of the airplane.
Model A320 series airplanes; as listed in Airbus Industrie Service Bulletin A320-29-1048, Revision 1, dated December 4, 1992, and Revision 2, dated September 1, 1994; certificated in any category.
AD 95-22-11
Effective 1995-11-24
Airbus Model A320 Series Airplanes
To prevent the initiation and propagation of fatigue cracking in fuselage frame 20, which could adversely affect the structural integrity of this area of the fuselage.
Model A320 airplanes; having manufacturer's serial numbers (MSN) 006, 008, 011, 017, 018, 039, 042, 045, 046, and 047; certificated in any category.
AD 95-22-10
Effective 1995-11-20
Airbus Model A320 Series Airplanes
To prevent the initiation and propagation of fatigue cracking in the pintle pins of the main landing gear (MLG), which could lead to the failure of the pintle pins and consequent collapse of the MLG.
Model A320 airplanes; as listed in Airbus Service Bulletin A320-32-1024, dated January 29, 1990; certificated in any category.
AD 95-17-12
Effective 1995-09-21 · superseded or removed
Airbus Model A320 Series Airplanes
To prevent loss of the pilot's ability to control the moveable surfaces of the THS.
Model A320 series airplanes on which Airbus Modification 22621 (reference Airbus Service Bulletin A320-27-1041) and Airbus Modification 23556 (reference Airbus Service Bulletin A320-29-1058) have not been installed, certificated in any category.
AD 95-04-12
Effective 1995-03-17 · recurring
Airbus Model A310, A300-600, and A320 Series Airplanes
To prevent failure of the lavatory smoke detection system to detect smoke in the lavatory.
Model A310 and A300-600 series airplanes on which Airbus Modification 10156 has not been accomplished, and Model A320 series airplanes on which Airbus Modification 22561 or Airbus Service Bulletin A320-26-1017 has not been accomplished; certificated in any category. This AD is not applicable to airplanes on which the a...

Airbus A320-214: price, specs and every tail

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