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Civil aviation

9,266 news found

Civil aviationFAA AD on Boeing model 737 series airplanes

Washington, USA - To prevent an uncommanded rudder hardover event and consequent loss of control of the airplane due to inherent failure modes, including single-jam modes, and certain latent failures or jams combined with a second failure or jam

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-251-AD; Amendment 39-12940; AD 2002-20-07 R1] RIN... more

Civil aviationFAA AD on Pilatus Britten-Norman Limited airplanes

Washington, USA - Models BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-CE-21-AD; Amendment 39-12926; AD 2002-22-02] RIN... more

Civil aviationFAA AD on Honeywell International, Inc., LF507 and ALF502R series turbofan engines

USA - To prevent separation of the combustor dome baffle from the combustion chamber liner assembly and the flow of hot combustor gases on oil and fuel lines which could result in an engine fire, an in-flight shutdown, and damage to the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-21-AD; Amendment 39-12931; AD 2002-22-06] RIN... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes

Washington, USA - To prevent severe flap asymmetry due to fractures of the carriage spindles on an outboard mid-flap, which could result in reduced control or loss of controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-214-AD; Amendment 39-12929; AD 2002-22-05] RIN... more

Civil aviationFAA AD on Boeing model 757-200, -200CB, and -300 series airplanes

Washington, USA - To prevent failure of an escape slide to deploy or inflate correctly, which could cause the slide to be unusable during an emergency evacuation and result in consequent injury to passengers or crewmembers

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-392-AD; Amendment 39-12921; AD 2002-21-14] RIN... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes

Washington, USA - To prevent damage to the upper wing skin surface and its structure, due to prolonged short-circuit electrical arcing of the anti-ice system

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-216-AD; Amendment 39-12912; AD 2002-21-06] RIN... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-10, -20, - 30, -40, and -50 series airplanes

To prevent fatigue cracking of the internal doublers and frame structure of the fuselage skin of the cockpit enclosure window sill, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-57-AD; Amendment 39-12915; AD 2002-21-09] RIN... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on Britax Sell GmbH & Co. products installed on Airbus, Bombardier and Boeing airplanes

Washington, USA - To prevent a fire in the galley compartment due to inadequate crimping of the electrical terminal contact pins, which could result in smoke in the cockpit and cabin and loss of control of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NE-58-AD; Amendment 39-12907; AD 2002-21-01] RIN... more

Civil aviationFAA AD on Agusta model A109E helicopters

Washington, USA - To prevent failure of specified parts of the main transmission assembly and supports, the tail rotor assemblies, the main rotor control bolt, or the fuselage left-hand elevator, and subsequent loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-06-AD; Amendment 39-12918; AD 2002-21-12] RIN... more