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Civil aviation

11,114 news found

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

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

Civil aviationFAA AD on Gulfstream model G-V series airplanes

Washington, USA - To prevent the circuit breaker wiring from becoming pinched or damaged, causing arcing between the wire and attaching bracket, which could result in smoke and/or fire in the pilot's circuit breaker panel

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-255-AD; Amendment 39-12909; AD 2002-21-03] RIN 2120-AA64... more