FAA airworthiness directives
Airbus A321-271NX airworthiness directives
140 FAA ADs name the Airbus A321-271NX: 108 in force, 20 recurring. Newest first.
AD 2026-15-13
Effective 2026-09-02
Airbus SAS Airplanes
This AD was prompted by occurrences of high-pressure bleed valve (HPV) butterfly seal retention clip rupture.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-151N, -153N, -171N, and -173N airplanes. (2) Model A320-251N, -252N, -253N, -271N, -272N, and -273N airplanes. (3) Model A321-251N, -252N, -253N, -271N, -272N, -251NX, -252NX,...
AD 2026-12-11
Effective 2026-08-03
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 A321-251NX, -252NX, -253NX, -271NX, and -272NX airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025- 0067, dated March 28, 2025 (EASA AD 2025-0067).
AD 2026-09-06
Effective 2026-05-26
Airbus SAS Airplanes
This AD was prompted by an Airbus supplier identifying a quality issue in production, which could result in potential deviations from the specified thickness of various fuselage panels delivered to Airbus.
This AD applies to Airbus SAS Model A319-153N airplanes; Model A320-251N, -252N, and -271N airplanes; and Model A321-251NX, -252NX, -271NX and -272NX airplanes; certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2026- 0055R1, dated April 14, 2026 (EASA AD 2026-0055R1).
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 2025-16-12
Effective 2025-08-29 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by occurrences of high-pressure bleed valve (HPV) butterfly seal retention clip rupture.
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-151N, -153N, -171N, and -173N airplanes. (2) Model A320-251N, -252N, -253N, -271N, -272N, and -273N airplanes. (3) Model A321-251N, -252N, -253N, -271N, -272N, -251NX, -252NX,...
AD 2023-25-05
Effective 2024-02-07
Airbus SAS Airplanes
This AD was prompted by the detection of several channel failures on the 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 loss of nose wheel steering.
This AD applies to the Airbus SAS airplanes, certificated in any category, identified in paragraphs (c)(1) through (3) of this AD. (1) All Model A319-151N, A319-153N, and A319-171N airplanes. (2) All Model A320-251N, A320-252N, A320-253N, A320-271N, A320- 272N, and A320-273N airplanes. (3) All Model A321-251N, A321-251...
AD 2023-10-07
Effective 2023-11-09
Airbus SAS Airplanes
This AD was prompted by a safety review of the airplane fuel system, which identified that the electrical harness routing of the engine low pressure shut off valve (LPSOV) is not adequately protected against uncontained engine rotor failure (UERF).
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 2022-0185, dated September 5, 2022 (EASA AD 2022-0185). (1) Model A319-151N, -153N and -171N airplanes. (2) Model A320-251N, -...
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 2023-02-11
Effective 2023-04-17
Airbus SAS Airplanes
This AD was prompted by an emergency exit slide deployment test on an Airbus Cabin Flex (ACF) overwing emergency exit, where the emergency exit slide did not deploy due to a disconnected slide release cable junction.
This AD applies to Airbus SAS Model A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022-0090, dated May 18, 2022 (EASA AD 2022-0090).
AD 2022-19-10
Effective 2022-10-19
Airbus SAS Airplanes
This AD was prompted by a determination that the quick release pin that is installed on the upper attachment of certain Smart HS- L41 and Smart HS-L42 lavatories is too short to lock on the bracket.
This AD applies to Airbus SAS Model A321-251N, A321-251NX, A321- 252NX, A321-253N, A321-253NX, and A321-271NX airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0263, dated November 19, 2021 (EASA AD 2021- 0263).
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 2021-18-08
Effective 2021-09-14 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by a report indicating that during inspection of the engines, two original rods installed to maintain an interface plate between the pylon and nacelle were found damaged at both rod-eye ends.
This AD applies to Airbus SAS Model A319-171N; Model A320-271N, -272N, and -273N airplanes; and Model A321-271N, -272N, -271NX, and -272NX airplanes; certificated in any category; as identified in European Union Aviation Safety Agency (EASA) AD 2021-0177, dated July 23, 2021 (EASA AD 2021-0177).
AD 2021-14-08
Effective 2021-07-01 · superseded or removed
Airbus SAS Airplanes
This AD was prompted by reports of an increasing number of operational disruptions due to airspeed discrepancies that have occurred due to the large number of airplanes returning to service after airplanes have been parked or stored (a large number of airplanes have been parked or stored due to the COVID-19 pandemic).
This AD applies to all Airbus SAS Model A319-151N, A319-153N, A319-171N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N and A321-272NX airplanes, certificated in any category.
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 2021-02-17
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 2020-22-08
Effective 2020-11-19
Airbus SAS Airplanes
This AD was prompted by reports of removable display units (RDUs) found undocked from the hosting display docking stations (DDS).
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (6) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020- 0155, dated July 14, 2020 ("EASA AD 2020-0155"). (1) Model A320-251N and -271N airplanes. (2) Model A321-251N, -271N, -272N...
AD 2020-07-10
Effective 2020-04-22
Airbus SAS Airplanes
This AD was prompted by a report of a gap found on an engine pylon nose fire seal during an inspection of an in-production airplane.
This AD applies to Airbus SAS Model A320-271N airplanes and Model A321-271N, -271NX, and -272N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2020-0053, dated March 10, 2020 ("EASA AD 2020-0053").
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 2019-15-02
Effective 2019-09-06
Airbus SAS Airplanes
This AD was prompted by analysis of the behavior of the elevator aileron computer (ELAC) L102 that revealed that excessive pitch attitude can occur in certain conditions and during specific maneuvers.
This AD applies to all Airbus SAS Model A321-251N, A321-252N, A321-253N, A321-271N, A321-272N, A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX 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 2018-11-15
Effective 2018-05-30
Airbus Airplanes
This AD was prompted by a report that, when operated at low speed and high engine thrust, an engine did not restart following a fuel interruption shorter than five seconds.
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, all manufacturer serial numbers (MSN). (1) Model A320-271N airplanes. (2) Model A321-271N, -271NX, -272N and -272NX airplanes.
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 2011-21-08
Effective 2011-11-23 · recurring
Sicma Aero Seat Passenger Seat Assemblies Installed on Various Transport Category Airplanes
This AD applies to Sicma Aero Seat 88xx, 89xx, 90xx, 91xx, 92xx, 93xx, 95xx, and 96xx series passenger seat assemblies identified in Annex 1, Issue 2, dated March 19, 2004, of Sicma Aero Seat Service Bulletin 90-25-013, Issue 4, dated March 19, 2004, that have backrest links having part numbers (P/Ns) 90-000200-104-1 a...
AD 2011-19-04
Effective 2011-10-21 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category; ...
AD 2011-16-03
Effective 2011-09-09
Airbus Model A300 B4-600, A300 B4-600R, and A300 F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called Model A300-600 Series Airplanes); Model A310 Series Airplanes; Model A318 Series Airplanes; Model A319 Series Airplanes; Model A320-211, -212, -214, -231, -232, and -233 Airplanes; Model A321 Series Airplanes; Model A330-200 and A330-300 Series Airplanes; and Model A340-200, A340-300, A340-500, and A340-600 Series Airplanes
This AD applies to the Airbus airplanes listed in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD, certificated in any category. (1) Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes; and Model A310-203, -204, -221, -222, -304, -322, -...
AD 2011-14-06
Effective 2011-08-22 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, - 132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, - 232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any catego...
AD 2011-13-11
Effective 2011-07-12 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122, airplanes; Model A319-111, -112, -113, -114, -115, -131, - 132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, - 232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any categ...
AD 2010-24-07
Effective 2011-01-11 · superseded or removed
Airbus Model A318-111 and A318-112 Airplanes and Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, A318-112, A319- 111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320- 232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes, certificated in any ca...
AD 2010-23-07
Effective 2010-12-10 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category, ...
AD 2010-18-07
Effective 2010-09-09 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category.
AD 2010-10-08
Effective 2010-06-21
Airbus A318, A319, A320, A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes; certificated in any category; ...
AD 2010-09-14
Effective 2010-06-08 · recurring
CFM International, S.A. CFM56-5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B4/P1, -5B6/2P, -5B4/2P1, and -5B9/2P Turbofan Engines
We are issuing this AD to prevent high-pressure compressor stalls, which could prevent continued safe flight or landing.
This AD applies to CFM International, S.A. CFM56-5B1/P, - 5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, - 5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B4/P1, -5B6/ 2P, -5B4/2P1, and -5B9/2P turbofan engines. These engines are installed on, but not limited to, Airbus A318, A319, A320, and A32...
AD 2010-06-18
Effective 2010-04-22
International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines
This AD applies to International Aero Engines (IAE) V2500- A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines with high-pressure (HP) compressor stage 3-8 drums, part numbers (P/Ns) 6A4900, 6A5467, 6A6473, 6A7383, 6A7384, 6A7385, and 6A7401, installed. Th...
AD 2010-06-01
Effective 2010-04-15
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, - 214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers (MSN); equipped w...
AD 2007-15-06
Effective 2009-12-14 · superseded or removed
Airbus Model A318-111 and -112 Series Airplanes, and Model A319, A320, and A321 Series Airplanes
We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
This AD applies to all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and - 233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, - 231, and -232 airplanes; certificated in any category.
AD 2009-23-05
Effective 2009-12-14
Airbus Model A318-111, -112, A319, A320, and A321 Series Airplanes
We are issuing this AD to prevent possible mid-air collisions due to lack of visibility of TCAS indications on the PFD.
This AD applies to Airbus Model A318-111, A318-112, A319- 111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320- 232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 series airplanes, certificated in...
AD 2009-22-06
Effective 2009-11-30
International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 Turbofan Engines
We are issuing this AD to prevent an uncontained failure of the HPC stage 9-12 disc assembly, resulting in an in-flight engine shutdown and possible damage to the airplane.
This AD applies to International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 turbofan engines. These engines are installed on, but not limited to, Airbus A320 and A321 series, and McDonnell Douglas Corporation MD-90 airplanes.
AD 2009-20-05
Effective 2009-11-03 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, all certified models, certificated in any category, all serial numbers up to manufacturer's serial number (MSN) 2850 inclusive, except MSNs 0115, 0184, 0782, 1151, 1190, 2650, 2675, 2706, 2801, and 2837.
AD 2009-18-01
Effective 2009-10-01 · recurring
CFM International, S.A. CFM56-5B1/P; -5B2/P; -5B3/P; -5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; -5B8/P; -5B9/P; -5B1/3; -5B2/3; -5B3/3; -5B4/3; -5B5/3; -5B6/3; -5B7/3; -5B8/3; -5B9/3; -5B3/3B1; and -5B4/3B1 Turbofan Engines
We are issuing this AD to detect low-cycle-fatigue cracks in the LP turbine rear frame, which could result in an engine separating from the airplane, causing damage to, and possibly leading to loss of control of the airplane.
This AD applies to: (1) CFM International, S.A. turbofan engines with a low-pressure (LP) turbine rear frame, part number (P/N) 338-171-703-0; 338-171- 704-0; 338-171-705-0; or 338-171-706-0 installed, as follows: (i) Commercial application CFM56-5B1/P; -5B2/P; -5B3/P; -5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; ...
AD 2009-17-04
Effective 2009-09-22 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318-111, -112, -121, and - 122; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320- 111, -211, -212, -214, -231, -232, -233; and A321-111, -112, -131, - 211, -212, -213, -231, and -232 series airplanes; certificated in any category; all manufacturer serial numbers.
AD 2009-15-07
Effective 2009-08-25
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-111, -211, -212, -214, -231, -232, and -233; and A321-111, -112, -131, -211, -212, -213, -231, and -232 series airplanes; certificated in any category; equipped with one conventional pre-Enhanced Manufacture and Maintainability...
AD 2009-09-01
Effective 2009-05-06
Airbus Model A318, A319, A320 and A321 Series Airplanes
This AD applies to Airbus Model A318-111, A318-112, A318- 121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320- 214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes; ce...
AD 2009-01-01
Effective 2008-12-31 · superseded or removed
CFM International, S. A. CFM56-5B Series Turbofan Engines
We are issuing this AD to prevent HPC stalls, which could prevent continued safe flight or landing.
This AD applies to CFM International, S. A. CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7, -5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, - 5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, - 5B3/2P1, -5B4/2P, -5B6/2P, -5B4/P1, -5B4/2P1, and -5B9/2P turbofan engines. These engines are installed on, but not limited ...
AD 2008-25-06
Effective 2008-12-26
Airbus Model A319, A320, and A321 Series Airplanes Equipped With International Aero Engines (IAE) Model V2500-A1 Engines or Model V25xx-A5 Series Engines
This AD applies to all Airbus Model A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-231, and A321-232 series airplanes, certificated in any category; all serial numbers equipped with International Aero Engine (IAE) Model V2500-A1 engines or Model V25xx-A5 series engines. (The "xx" is used in ...
AD 2008-22-10
Effective 2008-12-19
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category, all certified models; all serial numbers which have received an original French or German (as applicable) standard airworthiness certificate or original French or German (as applicable) export certificate of airwo...
AD 2008-17-12
Effective 2008-10-02
Airbus Model A318, A319, A320, and A321 Series Airplanes Equipped With Certain Northrop Grumman (Formerly Litton) Air Data Inertial Reference Units
We are issuing this AD to prevent failure of an ADIRU during flight, which could result in loss of one source of critical attitude and airspeed data and reduce the ability of the flightcrew to control the airplane.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category; equipped with at least one Northrop Grumman (formerly Litton) air data inertial reference unit (ADIRU), part number (P/N) 465020-0303-0307, -0308, - 0309, -0312, -0314, -0315, or -0316; except airplanes equipped w...
AD 2008-09-16
Effective 2008-06-06
Airbus A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus A318, A319, A320, and A321 series airplanes, certificated in any category, all certified models, all manufactured serial numbers (MSN) up to and including MSN 2860.
AD 2008-04-20
Effective 2008-04-03
Airbus Model A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category, all certified models, all serial numbers, on which Airbus A318/A319/A320/A321 Maintenance Review Board Report (MRBR) zonal tasks ZL-540-02 and ZL-640-02 (for MRBR up to Revision 7) or MRBR zonal task ZL-540-02-1 or ZL-5...
AD 2007-25-12
Effective 2008-01-14 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category, except those identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Manufacturer serial numbers (MSNs) 2389, 2392, 2393, 2396, 2398, 2403, 2405, 2407, 2409, 2410, 2411, 2413 through 2439, 2441, and MSNs above ...
AD 2007-17-14
Effective 2007-10-02 · recurring
Airbus Model A321 Series Airplanes
This AD applies to Airbus Model A321 series airplanes; all certified models; certificated in any category; equipped with Messier-Goodrich S.A. or Goodrich-Messier Inc., main landing gear (MLG) wheel assemblies having part number (P/N) C20500000 or P/N C20452000.
AD 2006-25-15
Effective 2007-01-19
Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
We are issuing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.
This AD applies to Sicma Aero Seat third occupant seat assemblies, 133 series, with the part numbers (P/Ns) and serial numbers (SNs) in the following Table 1: Table 1.--Applicable Seat Assemblies Seat P/N Seat SN 1330622-070: 1 through 212. 1330622-070-1: 1 through 212. 1330622-070-2: 1 through 6. 1330622-100: 1 throug...
AD 2006-25-01
Effective 2007-01-08 · recurring
International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 Turbofan Engines
We are issuing this AD to prevent failure of the No. 3 bearing, which could result in an IFSD and smoke in the cockpit and cabin.
This AD applies to International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines with engine serial numbers V10601 through V11335 inclusive and bearings part number (P/N) 2A1165 installed. These engines are installed on, but not limited to, Airbus Indust...
AD 2006-08-03
Effective 2006-05-18
Sicma Aero Seat (Formerly Farner); Cabin Attendant Seats Series 150 Type FN and Series 151 Type WN
We are issuing this AD to prevent injury resulting from contact with the bottom folding mechanism.
This AD applies to Sicma Aero Seat (formerly Farner) cabin attendant seats series 150 type FN and 151 type WN, all part and serial numbers. These attendant seats are installed on, but not limited to, Airbus A319, A320, and A321 series airplanes.
AD 2005-17-08
Effective 2005-09-27 · recurring
Airbus Model A321 Series Airplanes
This AD was prompted by a report that an operator found it impossible to lock emergency doors 2 and 3 in the open position.
This AD applies to Airbus Model A321 series airplanes, certificated in any category; except for those airplanes that have received Airbus Modification 33426 in production.
AD 2005-12-19
Effective 2005-07-29
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report that, during a test of the fire extinguishing system, air leakage around the temperature sensor for the aft cargo compartment reduced the concentration of fire extinguishing agent to below the level required to suppress a fire.
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category; as identified in Table 1 of this AD. Table 1.--Applicability But not having Having the Or the following the following following Airbus Airbus service Airbus Airbus model modification bulletin modification installed in i...
AD 2005-12-07
Effective 2005-06-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report of a crack found in the forward lug of the right-hand main landing gear (MLG) rib 5 fitting during greasing of the MLG pintle bearings.
This AD applies to Airbus Model A319, A320, and A321 series airplanes, certificated in any category; except those on which Airbus Modification 32025 was done during production.
AD 2005-10-04
Effective 2005-06-15 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the MLG side-stay cuff lugs or down-lock spring attachments, which could result in improper down-lock of the MLG during a freefall extension, and possible collapse of the MLG.
Airbus Model A319, A320, and A321 series airplanes; certificated in any category; except those airplanes on which Airbus Modification 30648 has been installed.
AD 2005-07-14
Effective 2005-05-12
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by a report of a broken piston rod bearing of the spoiler servo control.
This AD applies to all Airbus Model A318, A319, A320, and A321 series airplanes; certificated in any category.
AD 2005-06-06
Effective 2005-04-22
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by a report of an explosion in the APU compartment which blew open the compartment doors.
This AD applies to Airbus Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any Hamilton Sundstrand Auxiliary Power Unit (APU) alternating current (AC) generator having part number 5906732, 5909006, or 5910047; with up to amendment 17 included; on which Airbus Modification 32614 h...
AD 2005-02-09
Effective 2005-03-03 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To ensure continued structural integrity of these airplanes.
AD 2004-26-07
Effective 2005-02-10
Airbus Model A318, A319, A320, and A321 Series Airplanes Equipped With Air Cruisers/Aerazur Forward and Aft Passenger Door Emergency Escape Slides
This AD was prompted by manufacturer testing that has shown contact between the inflation hose and fabric roll, within a short period of time after inflation of the emergency escape slides, can rupture the inflation hose at its end fittings.
This AD applies to Airbus Model A318-111 and -112 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and - 133 series airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 series airplanes; and Model A321-111, -112, -131, -211, and -231 series airplanes; certificated in any category; equi...
AD 2004-25-11
Effective 2005-01-13
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by underlying safety issues involved in fuel tank explosions on several large transport airplanes.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes; certificated in any category; except those airplanes on which Airbus Modification 33518 has been accomplished in production.
AD 2004-25-08
Effective 2004-12-22 · recurring
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by a report indicating that an airplane lost the integrated standby instrument system (ISIS), then, during the same flight, lost all electronic instrument system (EIS) display units.
This AD applies to Airbus Model A318, A319, A320, and A321 series airplanes, certificated in any category; on which Airbus Modification 27620 (reference Airbus Service Bulletin A320-34-1261) has been done.
AD 2004-23-18
Effective 2005-01-03
Airbus Model A319, A320, and A321 Series Airplanes
This AD was prompted by data showing that the magnetic variation table installed in the Honeywell inertial reference system (IRS) is obsolete at certain airports.
This AD applies to Model A319, A320, and A321 series airplanes; certificated in any category; equipped with a Honeywell air data inertial reference unit (ADIRU) having any part number (P/ N) listed in Table 1 of this AD; on which Airbus Modification 30652, 30941, or 30942 has not been done. Table 1.--Honeywell ADIRU P/...
AD 2004-20-05
Effective 2004-10-15
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD was prompted by reports of the brief but total loss of all liquid crystal display (LCD) units during cruise on airplanes equipped with a certain EIS2 standard of electronic instrument system.
This AD applies to airplanes, certificated in any category, that are listed in Table 1 of this AD. Table 1.--Applicability Modified by Airbus Or Airbus service Airbus model-- modification-- bulletin-- A318, A319, A320, and A321 30368 or 31495: A320-31-1193, dated series airplanes. October 1, 2003; or A320-31A1198, date...
AD 2004-12-19
Effective 2004-07-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition of the input filter capacitors of the transformer rectifier unit (TRU) in position 2 of the avionics compartment, which could potentially result in smoke in the cockpit.
Model A319, A320, and A321 series airplanes, certificated in any category; except those airplanes on which Airbus Modification 30737 has been accomplished in production (reference Airbus Service Bulletin A320-24-1099, Revision 02, dated February 11, 2003, in service).
AD 2004-12-08
Effective 2004-07-23
International Aero Engines (IAE) AG V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
This airworthiness directive (AD) is applicable to International Aero Engines AG (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527- A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. These engines are installed on, but not limited to, Airbus Industrie A319, A320, and A321 series, and McDonne...
AD 2004-11-13
Effective 2004-06-23 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
This AD applies to all Model A318, A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-09-06
Effective 2004-06-02 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
All Model A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-07-02
Effective 2004-04-14 · superseded or removed
Airbus Model A318, A319, A320, and A321 Series Airplanes
To detect and correct cracking in a main landing gear (MLG) sliding tube, which could result in failure of the sliding tube, loss of one axle, and consequent reduced controllability of the airplane.
All Model A318, A319, A320, and A321 series airplanes, certificated in any category.
AD 2004-06-03
Effective 2004-04-22
Airbus Model A319, A320, and A321 Series Airplanes
To prevent jamming of the ram air turbine (RAT) actuator in an emergency which requires deployment of the RAT, and consequent loss of hydraulic and electrical power in the airplane.
Model A320 series airplanes which have received modification 27189; Model A319 series airplanes; and Model A321 series airplanes, provided that none has received modification 30978 or 28413; certificated in any category.
AD 2004-06-02
Effective 2004-04-22
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of a lower guide rod fitting, which could cause a rear passenger door to jam during opening, delaying an emergency evacuation and resulting in injury to passengers or crew members.
Model A319, A320, and A321 series airplanes; certificated in any category; on which Airbus Modification 30821 has not been accomplished.
AD 2004-03-33
Effective 2004-04-07
Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, A300 B4-600R, and A300 F4-600R Series Airplanes (Collectively Called A300-600); Model A310 Series Airplanes; Model A319, A320, and A321 Series Airplanes; Model A330-301, -321, -322, -341, and -342 Airplanes; and Model A340 Series Airplanes
To prevent loss or fluctuation of indicated airspeed, which could result in misleading information being provided to the flightcrew.
The series airplanes, certificated in any category, listed in Table 1--Applicability. Table 1.-- Applicability Excluding Airplanes Model and Series-- Excluding Airplanes Modified per-- Equipped With-- A300 B2 and A300 B4: Airbus Modification 12236 in service (reference None. Airbus Service Bulletin A300-34-0166, dated ...
AD 2004-03-02
Effective 2004-02-18 · superseded or removed
Airbus Model A321 Series Airplanes
To prevent roll oscillations during approach and landing in certain icing, crosswind, and turbulent conditions, which could result in reduced controllability of the airplane.
All Model A321 series airplanes, certificated in any category.
AD 2004-01-03
Effective 2004-02-13
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; certificated in any category; except those on which Airbus Modification 27142 has been incorporated during production.
AD 2003-26-03
Effective 2004-01-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes Equipped With Certain Litton Air Data Inertial Reference Units
To prevent failure of ADIRU 3 during flight, which could result in loss of one source of critical attitude and airspeed data and reduce the ability of the flightcrew to control the airplane.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with Litton air data inertial reference units (ADIRU) installed per Airbus Modification 24852, 25108, 25336, 26002, or 28218; except those airplanes on which Airbus Modification 30650 or 30872 has been accomplished.
AD 2003-25-04
Effective 2004-01-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition sources and consequent fire/explosion in the fuel tank.
Model A319, A320, and A321 series airplanes; certificated in any category; excluding those on which Airbus Modifications 27150, 27955, and 27472 have been installed.
AD 2003-17-14
Effective 2003-10-07
Airbus Model A300 B2 and B4; A300 B4-600, A300 B4-600R, and A300 F4-600R (Collectively Called A300-600); A310; A319; A320; A321; A330; and A340 Series Airplanes; Equipped With PPG Aerospace Windshields
To prevent failure of both structural plies of the windshield caused by overheating of the power lead wire, which could cause reduced structural integrity of the windshield assembly, and consequent loss of the windshield during flight.
Airplanes listed in Table 1 of this AD, certificated in any category, as follows: Table 1.--Applicability Equipped with PPG aerospace windshields having-- Model And serial numbers Part number (P/N) (S/N) as listed in A300 B2 and B4 series NP-175201-1, NP- Airbus All Operators airplanes. 175201-2, or NP- Telex A300-56A0...
AD 2003-16-07
Effective 2003-09-12 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent moisture ingression and delamination of the cockpit lateral fixed windows, which could result in the loss of the outer glass ply and consequent damage to the airplane and injury to people or damage to property on the ground.
Model A319, A320, and A321 series airplanes, certificated in any category, equipped with PPG Aerospace cockpit lateral fixed windows having part number (P/N) NP-165313-1 or NP- 165313-2, and having a serial number (S/N) below 95001H0001 (PPG Aerospace manufacturing date before January 1, 1995).
AD 2003-11-23
Effective 2003-06-20 · superseded or removed
International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, and V2530-A5 Turbofan Engines
This AD was prompted by reports of No. 3 bearing failures that resulted in in-flight shutdowns (IFSDs) and smoke in the cockpit and cabin.
This AD is applicable to International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, and V2530-A5 turbofan engines with a serial number (SN) from V10600 through V11250 inclusive. These engines are installed on, but not limited to, Airbus Industries A319, A320, and A321 series airplanes.
AD 2002-18-01
Effective 2002-10-10
Airbus Model A320 and A321 Series Airplanes
To prevent damage caused by water ingress into the elevator, which could lead to debonding of the elevator skins and degradation of the initial protection and consequent reduced structural integrity of the airplane.
Model A320 and A321 series airplanes, certificated in any category; having elevator part and serial numbers listed in Airbus Service Bulletin A320-55-1024, dated January 13, 1999; excluding those modified per Airbus Modification 23558.
AD 2002-10-06
Effective 2002-06-24
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous display of decision height information to the flightcrew during final approach, which could result in an increased risk of collision with terrain.
Model A319, A320, and A321 series airplanes without Airbus Modification 26017; certificated in any category.
AD 2002-08-13
Effective 2002-05-08 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent loss of the yellow hydraulic system, which provides all the hydraulics for certain spoilers; elements of the hydraulics for flaps, stabilizer, pitch and yaw feel systems, pitch and yaw autopilot, and yaw damper; and elevator, rudder, and aileron.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2002-06-01
Effective 2002-05-28 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the pintle fitting bearing, and consequent collapse of the main landing gear (MLG) during landing.
Model A319, A320, and A321 series airplanes, certificated in any category, except those on which Airbus Service Bulletin A320-32-1213, dated March 21, 2000 (reference Airbus Modification 28903 or 30044) has been accomplished.
AD 2002-06-53
Effective 2002-04-29
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes Equipped With Certain Thales Avionics Digital Distance and Radio Magnetic Indicators (DDRMIs)
To prevent failure of the DDRMI, which could cause the loss of data from the affected computers to other systems and degradation or total failure of the computers, leading to reduced ability to control the airplane in adverse conditions.
Model A319, A320, and A321 series airplanes equipped with Thales Avionics Digital Distance and Radio Magnetic Indicators (DDRMIs) having part numbers specified in paragraph 3.2 of Airbus All Operator Telex (AOT) A320-34A1262, dated March 19, 2002; Model A330 series airplanes equipped with Thales Avionics DDRMIs having ...
AD 2002-03-11
Effective 2002-03-19 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the bonds of the vertical stabilizer spar box to the skin, which could lead to reduced structural integrity of the spar boxes.
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-55A1027, dated May 13, 2000, Revision 01, dated August 1, 2000, or Revision 02, dated February 13, 2001; except those airplanes on which Airbus Service Bulletin A320-55-1028, Revision 02, dated July 26, ...
AD 2002-01-18
Effective 2002-03-06
Airbus Model A319, A320, and A321 Series Airplanes
To prevent corrosion of the trigger spring on the slide bar of the forward and aft passenger doors, which could result in incorrect locking of the slide bar during deployment of the escape slide and lead to a delay in evacuating passengers in an emergency.
Model A319, A320, and A321 series airplanes; all serial numbers having received Airbus Modification 20234 (Airbus Service Bulletin A320-25-1055) (installation of telescopic girt bar for slide raft), but NOT having received Airbus Modification 28212 (Airbus Service Bulletin A320-52-1102, Revision 01, dated November 25, ...
AD 2002-01-14
Effective 2002-01-22
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-35-1022, dated June 27, 2001.
AD 2001-26-21
Effective 2002-02-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent faulty operation of the low-pressure solenoid valve for the oxygen supply, which could prevent oxygen from being supplied to the airplane crew when needed, such as in the event of smoke in the cabin or rapid depressurization of the airplane.
Model A319, A320, and A321 series airplanes; on which Modification 21946 (Airbus Service Bulletin A320-35-1003) or 21999 has not been accomplished; certificated in any category.
AD 2001-26-20
Effective 2002-02-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the inability of the flightcrew to open the left- or right-hand sliding window for evacuation in an emergency, due to a window jamming in the closed position.
Model A319, A320, and A321 series airplanes, certificated in any category, as listed in Airbus Service Bulletin A320-56-1007, Revision 01, dated February 9, 2001.
AD 2001-26-10
Effective 2002-01-11 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes, certificated in any category, having manufacturer serial numbers 1035 and 1384 inclusive.
AD 2001-24-05
Effective 2002-01-04
Airbus Model A319, A320, and A321 Series Airplanes
To prevent reduced controllability of the airplane, due to the failure of the rudder artificial feel unit to disengage properly from autopilot mode during approach and landing.
Model A319, A320, and A321 series airplanes, certificated in any category, on which Airbus Modification 28909 was not accomplished during production.
AD 2001-16-09
Effective 2001-09-24 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent excessive vibration of the elevators, which could result in reduced structural integrity and reduced controllability of the airplane.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2001-16-14
Effective 2001-08-31 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the escape slide/raft to deploy correctly, which could result in the slide being unusable during an emergency evacuation and consequent injury to passengers or airplane crewmembers.
Model A319, A320, and A321 series airplanes equipped with telescopic girt bars of the escape slide/raft assembly, as listed in Airbus Industrie All Operators Telex (AOT) A320-52A1111, Revision 01, dated July 23, 2001; certificated in any category.
AD 2001-15-22
Effective 2001-09-10
Airbus Model A319, A320, and A321 Series Airplanes
To prevent injection of 115 volt alternating current (VAC) into 28 volt direct current (VDC) wire bundles, which could result in high voltage conditions within the fuel tank and the potential for damage to equipment, electrical arcing, and fuel vapor ignition on the ground.
Model A319, A320, and A321 series airplanes; certificated in any category; except those on which Airbus Industrie Modification 28289 has been installed.
AD 2001-15-16
Effective 2001-09-04
Airbus Model A319, A320, and A321 Series Airplanes
To prevent blockage of the outer door handle flap in an intermediate pushed-in position, which may prevent a passenger door from opening from the inside of the airplane, thereby delaying an emergency evacuation.
Model A319, A320, and A321 series airplanes, up to and including manufacturer's serial number (MSN) 1261, certificated in any category.
AD 2001-15-06
Effective 2001-08-27
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the ingestion of sill support-log material into the aspirator of the escape slide which could result in failure of the escape slide to inflate.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any emergency evacuation slide having a part number (P/N) listed as: D31516-103 D31516-105 D31516-107 D31516-109 D31517-103 D31517-105 D31517-107 D31517-109
AD 2000-24-08
Effective 2001-01-08
Airbus Model A319, A320, and A321 Series Airplanes
To prevent electrical arcing of the fuel boost pump wire, which could result in wing structural damage, or fire and/or fuel vapor explosion.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 2000-24-02
Effective 2001-01-08 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent chafing and resultant wear damage on the inboard flap drive trunnions or on the protective half-shells, which could result in failure of the trunnion primary load path, adversely affect the fatigue life of the secondary load path, and lead to loss of the flap.
Model A319, A320, and A321 series airplanes; certificated in any category; except airplanes on which Airbus Modification 26495 (reference Airbus Service Bulletin A320-27-1117) has been accomplished.
AD 2000-22-07
Effective 2000-12-06
International Aero Engines AG (IAE) V2500-A5 and -D5 Series Turbofan Engines
International Aero Engines AG (IAE) V2500-A5 and -D5 series turbofan engines listed by Serial Number (S/N) as follows: V10011 V10035 V10036 V10039 V10040 V10041 V10054 V10067 V10079 V10080 V10084 V10111 V10121 V10123 V10124 V10130 V10131 V10139 V10166 V10172 V10174 V10180 V10199 V10221 V10341 V20001 V20013 V20017 V2001...
AD 2000-14-15
Effective 2000-08-28 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent ignition sources and consequent fire/explosion in the fuel tank.
Model A319, A320, and A321 series airplanes; certificated in any category; excluding those on which Modifications 27150 and 27955 have been installed.
AD 2000-12-13
Effective 2000-07-24
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous navigational calculations, which could result in an increased risk of collision with terrain or other airplanes.
Model A319, A320, and A321 series airplanes; certificated in any category; on which any of the Airbus modifications has been installed or any of the Airbus service bulletins has been accomplished, as listed in the following table; except those airplanes on which Airbus Modification 26716, 26799, 26968, or 27831 has bee...
AD 2000-12-04
Effective 2000-07-19 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent fatigue cracking of the fuselage frames and frame feet, and consequent reduced structural integrity of the fuselage.
Model A319, A320, and A321 series airplanes, certificated in any category; except those on which Airbus Modification 25896, 25592, or 25593, or Airbus Service Bulletin A320-53-1128, Revision 01, dated October 4, 1999, has been accomplished.
AD 2000-11-27
Effective 2000-06-28 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct disbonding of the vertical stabilizer structure, which could result in reduced structural integrity of the spar boxes of the vertical stabilizer.
Model A319, A320, and A321 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A320-55A1027, dated May 12, 2000.
AD 2000-11-21
Effective 2000-07-18
Airbus Model A319, A320, and A321 Series Airplanes
To prevent failure of the servocontrol piston rod, which could result in reduced controllability of the airplane.
The following models, certificated in any category, excluding those on which Airbus Service Bulletin A320-27- 1126, dated April 26, 1999 (for Model A319 and 321 series airplanes); or A320-27-1127, dated April 26, 1999, or Revision 01, dated October 6, 1999 (for Model A320 series airplanes); has been accomplished: Model...
AD 2000-11-09
Effective 2000-07-06 · recurring
Airbus Model A319, A320, and A321 Series Airplanes
To prevent cracking of the sliding tube subassembly of the main landing gear (MLG), which could result in collapse of the MLG.
Model A319, A320, and A321 series airplanes; manufacturer serial numbers through 0875 inclusive; certificated in any category; except those on which Airbus Service Bulletin A320-32- 1189, dated December 23, 1998, has been accomplished; and except those on which it can be shown that one of the following conditions has b...
AD 2000-10-16
Effective 2000-06-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the bearing, and consequent collapse of the main landing gear (MLG) during landing.
Model A319, A320, and A321 series airplanes, certificated in any category, except those on which Airbus Service Bulletin A320-32-1213, dated March 21, 2000 (reference Airbus Modification 28903 or 30044), has been accomplished.
AD 2000-05-21
Effective 2000-04-27
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes
To prevent position and altitude errors due to bad oscillator warm-up characteristics of the GPSSU, which could result in navigational errors that may exceed 0.5 nautical mile.
Model A319, A320, A321, A330, and A340 series airplanes, certificated in any category, as follows: 1. Model A319, A320, and A321 series airplanes on which Airbus Modification 28578 (Airbus Service Bulletin A320-34-1191, dated July 12, 1999), or Airbus Modification 28579 (Airbus Service Bulletin A320-34-1196, dated July...
AD 2000-05-08
Effective 2000-04-12
Airbus Model A319 and A321 Series Airplanes
To prevent failure of the ram air turbine (RAT) to deploy in an emergency situation, and consequent loss of electrical and hydraulic systems.
Model A319 and A321 series airplanes, certificated in any category; except those on which Airbus Modification 27015 or Airbus Service Bulletin A320-29-1088, dated February 23, 1999, has been accomplished.
AD 2000-04-24
Effective 2000-05-08
Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) Series Auxiliary Power Units
To prevent an uncontained APU failure and damage to the airplane.
Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) series Auxiliary Power Units (APUs), with load compressor impellers, part numbers (P/Ns) 3822270-4, or 3822270-5, installed. These APUs are installed on but not limited to Airbus Industrie A319, A320, and A321 series; Boeing 737-30...
AD 2000-04-11
Effective 2000-03-10
Airbus Model A319, A320, and A321 Series Airplanes
To prevent erroneous display of decision height information to the flight crew during final approach, which could result in an increased risk of collision with the terrain.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with Rockwell Collins radio altimeter LRA 700 having part number (P/N) 622-4542-020; excluding those on which Airbus Modification 26017 (Airbus Service Bulletin A320-31-1106) has been installed.
AD 2000-04-06
Effective 2000-03-30 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent the ingestion of sill support-log material into the aspirator of the escape slide which could result in failure of the escape slide to inflate.
Model A319, A320, and A321 series airplanes; certificated in any category; equipped with any emergency evacuation slide having a part number (P/N) listed as: D31516-103 D31516-105 D31516-107 D31516-109 D31517-103 D31517-105 D31517-107 D31517-109
AD 2000-02-36
Effective 2000-03-13
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a simultaneous cutoff of the fuel supply to both engines, which could result in a loss of engine power and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; as listed in Airbus Service Bulletin A320-24-1092, Revision 03, dated September 16, 1998; certificated in any category.
AD 99-25-10
Effective 2000-01-12
Airbus Model A319, A320, and A321 Series Airplanes
To prevent structural failure of the forward engine mount secondary load path, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane.
Model A319-131 and -132, A320-232 and -233, and A321-131 series airplanes; except those on which Airbus Modification 27020 has been accomplished (reference Airbus Service Bulletin A320- 71-1021, Revision 01, dated June 10, 1998); certificated in any category.
AD 99-23-09
Effective 1999-12-17
Airbus Model A319, A320, and A321 Series Airplanes
To prevent uncommanded nose landing gear wheel rotation, due to defective seals in the wheel steering selector valve of the hydraulic control unit for the nose landing gear, which could result in reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; except those airplanes on which Airbus Modification 23740 was accomplished during production, and those airplanes on which Airbus Service Bulletin A320-32-1197, dated October 9, 1998, or Revision 01, dated February 11, 1999, has been accomplished; certificated in any categor...
AD 99-21-28
Effective 1999-11-22
Airbus Model A319, A320, A321, A330, and A340 Series Airplanes Equipped With AlliedSignal RIA-35B Instrument Landing System Receivers
To detect and correct faulty ILS receivers and to ensure that the flightcrew is advised of the potential hazard of performing ILS approaches using a localizer deviation from a faulty ILS receiver, and advised of the procedures necessary to address that hazard.
Model A319, A320, A321, A330, and A340 series airplanes; certificated in any category; equipped with AlliedSignal RIA-35B Instrument Landing System (ILS) receivers, part number (P/N) 066-50006-0202; excluding airplanes on which RIA-35B ILS receiver P/ N 066-50006-1202 [Airbus Modification 27251 (for Model A319, A320, a...
AD 99-21-17
Effective 1999-10-28
Airbus Model A321 Series Airplanes
To prevent the loss of structural integrity of the rear part of the fuselage structure in the event of an undetected tail scrape during landing or takeoff.
Model A321 series airplanes, certificated in any category; except those on which Airbus Modification 25791 has been incorporated in production, or on which Airbus Service Bulletin A320-53-1130, dated June 17, 1997, or Revision 01, dated July 8, 1998, has been accomplished in service.
AD 99-20-05
Effective 1999-10-29
Airbus Model A319, A320, and A321 Series Airplanes
To prevent damage to computer electrical connectors due to ingress of water into the avionics bay, which could result in malfunctioning of the avionics computers.
Model A319, A320, and A321 series airplanes, certificated in any category, on which Airbus Modification 25995 has not been accomplished.
AD 99-17-11
Effective 1999-09-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
Model A319, A320, and A321 series airplanes; except airplanes on which Airbus Modification 26495 has been installed in production, or on which Airbus Service Bulletin A320- 27-1117, dated July 31, 1997, or Revision 01, dated June 25, 1999, has been accomplished; certificated in any category.
AD 99-13-01
Effective 1999-06-25
International Aero Engines AG V2500-A1 and V2500-A5 Series Turbofan Engines
To prevent failure of the high pressure turbine (HPT) hardware due to ignition of oil trapped by the HPT stage 1 inner rotating airseal (TOBI ID seal), which could result in an uncontained engine failure and damage to the airplane.
International Aero Engines AG (IAE) V2500-A1 turbofan engines, all serial numbers (S/Ns), and V2500-A5 turbofan engines, with S/Ns V10079 and below, installed on, but not limited to, Airbus Industries A319, A320, and A321 series airplanes.
AD 99-04-03
Effective 1999-04-12
International Aero Engines AG (IAE) V2500-A5/-D5 Series Turbofan Engines
To prevent high pressure compressor (HPC) stage 9-12 drum failure, which could result in an uncontained engine failure and damage to the aircraft.
International Aero Engines AG (IAE) Models V2522- A5, V2524-A5, V2527-A5, V2527E-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5 turbofan engines, installed on but not limited to Airbus Industrie A319, A320, A321 series and McDonnell Douglas MD-90 series aircraft.
AD 99-02-04
Effective 1999-02-19
Airbus Model A320 and A321 Series Airplanes
To prevent failure of the slat and flap control computer (SFCC), which could result in uncommanded slat retraction during takeoff and consequent insufficient wing lift available to complete a successful takeoff.
Model A320 series airplanes, as listed in Airbus Service Bulletin A320-27-1096, Revision 01, dated January 14, 1998; and Model A321 series airplanes, as listed in Airbus Service Bulletin A320-27-1103, dated June 14, 1996; certificated in any category.
AD 99-01-13
Effective 1999-02-12
Airbus Model A319, A320, and A321 Series Airplanes
To prevent simultaneous loss of heating to pitot probes 1 and 3, which could result in incorrect airspeed indications to both the pilot's and first officer's airspeed indication systems, and reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; excluding airplanes on which Airbus Modification 26403 or Airbus Service Bulletin A320-30-1036, Revision 02, dated February 4, 1998, has been accomplished; certificated in any category.
AD 98-26-03
Effective 1998-12-31
Airbus Model A321 Series Airplanes
Model A321 series airplanes, except those on which Airbus Modification 27036 has been installed; or on which the action described in Airbus Industrie Service Bulletin A320-25-1199, dated March 25, 1998, has been accomplished; certificated in any category.
AD 98-20-10
Effective 1998-10-27 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To prevent a simultaneous cutoff of the fuel supply to both engines, which could result in a loss of engine power and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; on which Airbus Modification 26065 (reference Airbus Service Bulletin A320-24-1092, Revision 01, dated December 24, 1997) has not been accomplished; certificated in any category.
AD 98-19-08
Effective 1998-10-07
Airbus Model A321 Series Airplanes
To prevent the use of erroneous automatic roll-out guidance generated by the flight management and guidance computer, which could result in the airplane departing the runway upon landing.
Model A321 series airplanes, certificated in any category, as identified below: Model A321 series airplanes equipped with CFM engines, on which Airbus Modification 25199 (reference Airbus Service Bulletin A320-22-1045) has been installed, except for those on which Airbus Modification 25469 (reference Airbus Service Bul...
AD 98-20-04
Effective 1998-10-26
Airbus Model A319, A320, and A321 Series Airplanes
To prevent water contamination of the avionics computers, which could result in the display of erroneous or misleading information to the flightcrew, and consequent reduced controllability of the airplane.
Model A319, A320, and A321 series airplanes; equipped with Monogram rinse valves having part number (P/N) 15800- 348, Revision C; and on which Airbus Modification 26145 (reference Airbus Service Bulletin A320-38-1049) has not been accomplished; certificated in any category.
AD 98-16-12
Effective 1998-09-08
Airbus Model A320 and A321 Series Airplanes
To prevent blockage of fuel by the build-up of ice crystals, which could result in low fuel pressure, and consequent shutdown of the engine during critical phases of flight.
Model A320 and A321 series airplanes; as listed in Airbus Service Bulletin A320-28-1044, Revision 10, dated November 5, 1996; certificated in any category.
AD 98-15-06
Effective 1998-08-20 · recurring
Airbus Model A320 and Model A321 Series Airplanes
To prevent jamming of the passenger/crew door, which could delay or impede the evacuation of passengers during an emergency.
Model A320 and Model A321 series airplanes, as listed below, certificated in any category: On which Airbus Modification 24497 has not been installed in production. Or On which Airbus Service Bulletin A320-52-1027, Revision 2, dated February 18, 1993, Revision 3, dated December 10, 1993, or Airbus Service Bulletin A320-...
AD 98-14-11
Effective 1998-08-12 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To detect and correct a rotated, damaged, or missing lock bolt, which could result in disengagement of the pintle pin from the bearing, and consequent collapse of the main landing gear (MLG) during landing.
All Model A319, A320, and A321 series airplanes; certificated in any category.
AD 98-09-18
Effective 1998-06-03
Airbus Industrie Model A320 and A321 Series Airplanes
To prevent situations that could lead to reduced controllability of the airplane due to adverse airplane-pilot coupling characteristics.
Model A320 and A321 series airplanes; as listed in Airbus Service Bulletin A320-27-1082, Revision 1, dated September 6, 1995; certificated in any category.
AD 98-04-11
Effective 1998-03-24
Airbus Model A320 and A321 Series Airplanes
To prevent possible delays in deceleration when landing with strong cross winds and/or on a contaminated runway, which could increase the potential for landing overrun.
Model A320 and A321 series airplanes on which Airbus Modification No. 24745 (Airbus Service Bulletin A320-27-1088, Revision 3, dated December 11, 1996) has not been accomplished, certificated in any category.
AD 98-02-04
Effective 1998-03-23
CFM International CFM56-5B/2P Series Turbofan Engines
To prevent a low cycle fatigue (LCF) failure of the LPT case, which could result in damage to the aircraft.
CFM International (CFMI) CFM56-5B1/2P, -5B2/2P, - 5B3/2P, and -5B4/2P turbofan engines, installed with low pressure turbine (LPT) case, Part Number (P/N) 338-117-004-0, installed on but not limited to Airbus A320 and A321 series aircraft.
AD 97-25-17
Effective 1998-01-20
Airbus Model A320 and A321 Series Airplanes
To prevent output of erroneous radio altimeter height information to the flightcrew and autopilot, due to inadequate antenna solder connections, which could result in reduced ability of the flightcrew to cope with adverse operating conditions.
Model A320 and A321 series airplanes equipped with Collins radio altimeter antennas having part number (P/N) 622- 8701-002 and a serial number below 2014, certificated in any category.
AD 97-23-13
Effective 1997-12-17
Airbus Model A320 and A321 Series Airplanes
To prevent the inability of the slide/slide raft to deploy due to a failure of the passenger door, which could delay or impede passengers when exiting the airplane during an emergency.
Model A320 and A321 series airplanes, as specified in French airworthiness directive 96-171-083(B), dated August 28, 1996, certificated in any category.
AD 97-22-13
Effective 1997-12-05
Airbus Model A320 and A321 Series Airplanes
To prevent severely reduced controllability of the airplane during approach.
Model A320 and A321 series airplanes, on which Airbus Modification 24612 or Airbus Service Bulletin A320-31-1080 has not been accomplished; certificated in any category.
AD 97-21-10
Effective 1997-11-03 · superseded or removed
Airbus Model A319, A320, and A321 Series Airplanes
To ensure that the flightcrew detects and corrects an unintended flight path if certain software anomalies of the FMGS occur, which could result in an increased risk of collision with terrain or other airplanes.
Model A319, A320, and A321 series airplanes, certificated in any category; on which any of the following Airbus Modifications have been installed: Affected model(s) Airbus modification installed A319 and A321: 25469 (reference Airbus Service Bulletin A320-22-1054). A319, A320, and A321: 26093. A320: 24065 (reference Ai...
AD 97-03-06
Effective 1997-03-06
Auxiliary Power International Corporation Model APS3200 Auxiliary Power Units
To prevent an APU fire due to ECB malfunction, which could result in damage to the aircraft.
Auxiliary Power International Corporation (APIC) Model APS3200 Auxiliary Power Units (APUs), Assembly Part Number (P/ N) 4500000, incorporating Electronic Control Box (ECB), P/N 4500003E, with software version 2.0.2, and ECB, P/N 4500003F, with software version 3.2. These APUs are installed on but not limited to Airbus...
AD 97-01-09
Effective 1997-01-30 · recurring
Airbus Model A321 Series Airplanes
To prevent the loss of the left and right emergency evacuation slides at emergency exits Number 2 and 3 during flight, which could make these exits unusable in the event of an emergency and also could cause damage to the empennage.
Model A321 series airplanes; as listed in Airbus Industrie All Operator Telex (AOT) 25-11, Revision 01, dated January 8, 1996, and Airbus Service Bulletin A320-25-1167, dated June 24, 1996; on which Airbus Modification 25369 has not been installed; certificated in any category.
Airbus A321-271NX: price, specs and every tail
AD data from the Federal Register and the FAA. Data: Radar, FAA aircraft registry file of 2026-10-09.
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