Airbus Industrie Airworthiness Directives

133 ADs indexed for Airbus Industrie aircraft.

Models

Recent ADs

2010-01-07

final rule

Airworthiness Directives; Airbus (Type Certificate Previously Held by Airbus Industrie) Model A340-200, -300, -500, and -600 Series Airplanes

Unsafe Condition: Failure to comply with Revision 00 of AIRBUS A340 ALS Part 3 constitutes an unsafe condition, which is a safety-significant latent failure that could, in combination with other specific failures or...

Effective: Jan 27, 2010 Category: aircraft Compliance: Within 12 months of the effective date of the AD.

Why matched: Airworthiness Directives; Airbus (Type Certificate Previously Held by Airbus Industrie) Model A340-200, -300, -500, and -600 Series Airplanes

2005-06-07

final rule

Airworthiness Directives; General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes; Correction

Unsafe Condition: This document makes a correction to Airworthiness Directive (AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines. We published AD 2005-06-07 in the Federal Regis...

Effective: May 5, 2005 Category: aircraft Compliance: section is incorrect

Why matched: Airworthiness Directives; General Electric Company (GE) CF6-80A1/ A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2000-16-07

final rule

Airworthiness Directives; Airbus Industrie Model A300 B2 and B4 Series Airplanes

Unsafe Condition: Bonding delamination and cracking of the fuselage longitudinal lap joints, circumferential joints, stringers, and doublers, which could result in rapid decompression of the airplane.

Effective: Sep 20, 2000 Category: aircraft Compliance: Within 6 months after May 13, 1985, or as indicated by the applicable service bulletins.

Why matched: Airworthiness Directives; Airbus Industrie Model A300 B2 and B4 Series Airplanes

2000-12-12 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A300, A300-600, and A310 Series Airplanes

Unsafe Condition: Fatigue cracking in the lower spar axis of the nacelle pylon between ribs 9 and 10, which could result in reduced structural integrity of the lower spar of the pylon.

Effective: Jul 28, 2000 Category: aircraft Compliance: Within 500 landings after June 12, 1995, or prior to the accumulation of 9,000 total landings for...

Why matched: Airworthiness Directives; Airbus Industrie Model A300, A300-600, and A310 Series Airplanes

2000-10-18

final rule

Airworthiness Directives; Airbus Industrie Model A300, A300-600, and A310 Series Airplanes

Unsafe Condition: Fatigue cracking in the lower spar axis of the engine pylons between ribs 6 and 7, which could result in reduced structural integrity of the engine pylon's lower spar and possible separation of the...

Effective: Jun 30, 2000 Category: engine Compliance: Within 500 landings after June 28, 1996, or at specified intervals based on crack detection and r...

Why matched: Airworthiness Directives; Airbus Industrie Model A300, A300-600, and A310 Series Airplanes

Amdt-39-11336

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: Malfunction of the low pressure non-return valve in the AGCM of the ram air turbine (RAT) could result in loss of the blue hydraulic system, leading to loss of certain flight control and electrical...

Effective: Oct 29, 1999 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

99-20-06

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: 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...

Effective: Oct 29, 1999 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Amdt-39-11285 Recurring

final rule

Airworthiness Directives; General Electric Company CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes

Unsafe Condition: Inadvertent thrust reverser deployment, which could result in loss of control of the airplane.

Effective: Sep 24, 1999 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; General Electric Company CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes

Amdt-39-11236 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Unsafe Condition: Cracking in certain bolt holes of the rear spar, which could result in reduced structural integrity of the airplane.

Effective: Sep 1, 1999 Category: aircraft Compliance: Not specified.

Why matched: Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Amdt-39-10796

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: Pitch-up of the airplane due to activation of the spoilers during an automatic landing, which could result in tail strikes and structural damage.

Effective: Oct 30, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

98-20-29

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: Pitch-up of the airplane due to activation of the spoilers during an automatic landing, which could result in tail strikes and structural damage to the airplane.

Effective: Oct 30, 1998 Category: aircraft Compliance: Required as indicated, unless accomplished previously.

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Amdt-39-10793 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Unsafe Condition: Fatigue cracking of the wing top skin at the front spar joint could result in reduced structural integrity of the airplane.

Effective: Oct 29, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

98-24248 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: Fatigue cracking in the inner flange of door frame 66 could result in reduced structural integrity of the airplane.

Effective: Oct 20, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Amdt-39-10718

final rule

Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Unsafe Condition: Cracking in the vertical web of the center spar sealing angles adjacent to the pylon rear attachment and in the adjacent butt strap and skin panel.

Effective: Oct 1, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

98-09-18

final rule

Airworthiness Directives; Airbus Industrie Model A320 and A321 Series Airplanes

Unsafe Condition: Adverse airplane-pilot coupling characteristics could lead to reduced controllability due to uncommanded movements of the ailerons and pilot response.

Effective: Jun 3, 1998 Category: aircraft Compliance: Within 1 year after the effective date of this AD

Why matched: Airworthiness Directives; Airbus Industrie Model A320 and A321 Series Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Amdt-39-10499

final rule

Airworthiness Directives; Airbus Industrie Model A320 and A321 Series Airplanes

Unsafe Condition: Difficulty maintaining the intended flight path during landing in turbulent conditions due to adverse airplane-pilot coupling characteristics.

Effective: Jun 3, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A320 and A321 Series Airplanes

Amdt-39-10275

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition: Jamming of the locking pin due to moisture and migrated bushings in the guide fittings of the safety locking pins of the passenger doors.

Effective: Feb 17, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Amdt-39-10059 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Unsafe Condition: Fatigue cracks in the outer skin of the fuselage at certain frames could reduce structural integrity and cause rapid decompression.

Effective: Aug 4, 1997 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

97-10-01

final rule

Airworthiness Directives; Airbus Industrie Model A310 Series Airplanes

Unsafe Condition: Cracking of the hardened steel inner race, and broken or missing inner races of the steady bearing assemblies of the flap transmission system could cause failure of the steady bearing shafts during...

Effective: Jun 10, 1997 Category: aircraft Compliance: Prior to the accumulation of 2,000 total landings or within 500 flight hours after the effective ...

Why matched: Airworthiness Directives; Airbus Industrie Model A310 Series Airplanes

Amdt-39-10013 Recurring

final rule

Airworthiness Directives; Airbus Industrie Model A310 Series Airplanes

Unsafe Condition: Cracking of the hardened steel inner race, and broken or missing inner races of the steady bearing assemblies of the flap transmission system.

Effective: Jun 10, 1997 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Industrie Model A310 Series Airplanes

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