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Civil aviation

11,458 news found

Civil aviationFAA AD on Eurocopter France model EC 155B helicopters

Washington, Usa - To prevent an electrical discontinuity in the grounding plane inside the SMD45H multi-functional display, which can result in overheating of the interconnection board, smoke in the cockpit, and subsequent loss of control of helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-11-AD; Amendment 39-12886; AD 2002-19-06] RIN 2120-AA64 Airworthiness... more

Civil aviationFAA AD on Turbomeca S.A. Makila models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A installed

Washington, Usa - To prevent the ejector from becoming loose from the exhaust pipe, resulting in damage to the main rotor and tail rotor and loss of helicopter control

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-42-AD; Amendment 39-12882; AD 2002-19-02] RIN 2120-AA64 Airworthiness... more

Civil aviationFAA AD on Boeing 737 (2002-19-51)

Washington, Usa - To prevent operation with one failed flight control module (FCM), which could result in reduced controllability of the airplane, or with two failed FCMs, which could result in loss of control of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-NM-248-AD; AD 2002-19-51 R1 Boeing Model 737 Series Airplanes PDF... more

Civil aviationFAA AD on Eurocopter France Model AS332C, L, L1, and Model SA330F, G, and J Helicopters

Washington, Usa - To detect excessive angular play in the gearbox and to prevent failure of a gearbox, loss of tail rotor drive, and subsequent loss of control of the helicopter, accomplish the following

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-SW-47-AD; Amendment 39-12880; AD 2002-18-06] RIN 2120-AA64 Airworthiness... more

Civil aviationFAA AD on Eurocopter France Model SA330F, SA330G, SA330J, AS332C, AS332L, and AS332L1 Helicopters

Washington, Usa - To prevent wear of a collector bearing, loss of tail rotor effectiveness, and subsequent loss of control of the helicopter, accomplish the following

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-SW-66-AD; Amendment 39-12879; AD 2002-18-05] RIN 2120-AA64 Airworthiness... more

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2002-18-02)

Washington, Usa - To prevent jamming of the first officer's control wheel due to the presence of a foreign object on the lower bearing support of the transfer mechanism for the aileron

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-344-AD; Amendment 39-12874; AD 2002-18-02] RIN... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 airplanes (2002-17-06)

Washington, Usa - To prevent chafing damage to the wire assembly, and consequent arcing and smoke and fire in the electrical power center, and to prevent damage to the wire assembly terminal lugs and overheating of the power feeder cables on the No. 3 an

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-195-AD; Amendment 39-12872; AD 2002-17-06] RIN... more

Civil aviationFAA AD on Boeing model 727 series airplanes (2002-17-05)

Washington, Usa - To find and fix discrepancies of the wire bundles and hydraulic tubing in the aft stairwell area, which could result in electrical arcing between the wiring and hydraulic tubing and consequent fire and damage to adjacent structure

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-154-AD; Amendment 39-12871; AD 2002-17-05] RIN... more

Civil aviationFAA AD on Ballonbau Worner model K-630/1-Stu manned free gas balloons (2002-17-04)

Washington, Usa - To prevent the chance of an electrostatic charge buildup between the steelwire loops of the basket and the balloon envelope, which could result in ignition of combustible lifting gas fumes in the balloon envelope

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-CE-35-AD; Amendment 39-12869; AD 2002-17-04] RIN... more

Civil aviationFAA AD on Diamond Aircraft Industries models HK 36 R "Super Dimona", HK 36 TC, HK 36 TS, HK 36 TTC, HK 36 TTC-ECO, HK 36 TTC-ECO (Restricted Category), and HK 36 TTS sailplanes (2002-15-01 R1)

Washington, Usa - to detect and correct damage in the long aileron push control rods, which could result in failure of the aileron push rods and decreased control

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-CE-11-AD; Amendment 39-12870; AD 2002-15-01 R1] RIN... more

Civil aviationFAA emergency AD on Boeing model 737-600, -700, -700C, -800, and -900 series airplanes; model 747 series airplanes; and model 757 series airplanes (2002-18-52)

Washington, Usa - To prevent fuel vapors from coming into contact with an ignition source in the center wing fuel tank, which could result in fire/explosion in the center fuel tank

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-NM-229-AD; AD 2002-18-52 Boeing Model 737-600,... more