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FAA Airworthiness Directives Database

20111 ADs

AD Number Status Subject Effective Date Superseded By
2018-16-09 Active
Fuselage
2018-09-10
2018-16-05 Superseded
Wings
2018-09-10
2020-21-17
2018-17-01 Superseded
Engine Oil System and Aircraft Fuel System
2018-09-05
2019-09-02
2018-15-07 Active
Flight Controls
2018-09-04
2018-17-07 Active
Electric
2018-09-04
2018-15-08 Active
Nacelles/Pylons
2018-08-31
2018-16-01 Active
Equipment
2018-08-31
2018-17-05 Superseded
Flight controls
2018-08-30
2020-20-16
2018-14-12 Active
Turbine Section
2018-08-30
2018-15-03 Active
Engine Exhaust System
2018-08-27
2018-14-09 Superseded
Fuselage
2018-08-23
2024-04-04
2018-14-11 Superseded
ATA Code 05
2018-08-23
2021-03-03
2018-16-03 Active
Powerplant
2018-08-23
2018-13-06 Active
Wings
2018-08-22
2018-13-08 Superseded
Wings
2018-08-22
2022-14-10
2018-12-08 Superseded
Fuselage
2018-08-22
2018-18-16
2018-16-08 Active
Rotorcraft Cooling Fan System
2018-08-20
2018-14-06 Active
Wings
2018-08-17
2018-13-01 Active
Turbine Governor
2018-08-16
2018-14-07 Active
Placards and Markings
2018-08-16
2018-16-07 Superseded
Turbine Section
2018-08-15
2019-02-01
2018-14-02 Superseded
Equipment/furnishings
2018-08-13
2020-22-10
2018-14-05 Active
SUMMARY: We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by reports of fire incidents of the auxiliary power unit (APU) inlet, which caused tail cone damage after an initial failed APU start followed by two or more in-flight APU start attempts. This AD requires modification of the APU electronic control unit (ECU) wiring harness. We are issuing this AD to address the unsafe
2018-08-13
2018-15-06 Active
Time Limits
2018-08-13
2018-14-03 Active
Landing gear
2018-08-13
2018-14-04 Active
Fuel
2018-08-13
2018-12-03 Active
Fuel Controlling System
2018-08-09
2018-15-01 Superseded
Turbine Engine, Turbine Section
2018-08-07
2019-20-05
2018-13-07 Superseded
Turbine Engine Compressor Section
2018-08-07
2018-25-01
2018-15-05 Active
Equipment/furnishings
2018-08-07
2018-15-02 Superseded
Tail Rotor Control System
2018-08-03
2021-05-09
2018-14-08 Active
Fuel
2018-07-27
2018-13-05 Active
Turbine Engine Reduction Gear
2018-07-26
2018-13-04 Active
Oxygen
2018-07-25
2018-14-01 Active
Fuselage Skin
2018-07-25
2018-12-07 Active
Landing Gear
2018-07-23
2018-13-02 Active
Turbine Engine Combustion Section
2018-07-20
2018-12-06 Active
Air conditioning
2018-07-16
2018-12-02 Active
Powerplant
2018-07-13
2018-12-05 Active
Wings
2018-07-13
2018-11-12 Active
Landing gear
2018-07-12
2018-13-03 Active
Turbine Engine Compressor Section
2018-07-11
2018-11-09 Active
Flight controls
2018-07-10
2018-11-08 Active
Fuselage
2018-07-10
2018-11-13 Active
Wings
2018-07-10
2018-11-14 Superseded
Wings
2018-07-10
2026-16-06
2018-11-10 Active
Doors
2018-07-09
2018-11-06 Active
Wings
2018-07-03
2018-11-16 Superseded
Turbine Engine Compressor Section
2018-07-02
2019-03-04
2018-09-14 Active
SUMMARY: We are superseding Airworthiness Directive (AD) 2016-11-02, which applied to all Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes; Model CL-600-2D15 (Regional Jet Series 705) airplanes; Model CL-600-2D24 (Regional Jet Series 900) airplanes; and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. AD 2016-11-02 required repetitive inspections of the upper and lower engine pylons for protruding, loose, or
2018-06-28