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Civil aviation

11,114 news found

Civil aviationFAA AD on Airbus model A-320-111, -211, -212, and -231 series airplanes (2004-03-07)

Usa - To detect and correct fatigue cracking around the fasteners connecting the pressure panel to the flexible bracket at frame 36, adjacent to the longitudinal beams on the left and right sides of the airplane, which could result in reduced structural

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-107-AD; Amendment... more

Civil aviationFAA AD on Fokker model F-28 Mark 0070 and 0100 series airplanes

Usa - To ensure that the flightcrew is aware of the procedures required to prevent ice from contacting the ice impact panels on the engine fan case, which could result in a panel coming loose during flight and blocking the bypass flow through the engine

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-10-AD; Amendment... 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

Usa - To prevent internal overheating and arcing of circuit breakers and airplane wiring due to long-term use and breakdown of internal components of the circuit breakers, which could result in smoke and fire in the flight compartment and main cabin

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-82-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC-10A- and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F; and model MD- 11 and MD-11F airplanes

Washington, Usa - To prevent separation of the inboard flap outboard hinge from the wing structure and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-43-AD; Amendment... more

Civil aviationFAA AD on Dassault model Falcon 900EX series airplanes

To ensure that the flightcrew is aware of the potential for reductions in climb performance in certain situations while operating in icing conditions, and the actions they must take to avoid this condition, which could result in an inability to avoid low

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-276-AD; Amendment... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (Embraer) model EMB-135 and -145 series airplanes

Washington, Usa - To prevent ice from damaging the pitot drain valves, which could cause airspeed indication errors, resulting in display of erroneous or misleading information to the flight crew

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-330-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 and -11F airplanes (2004-01-17)

Washington, Usa - To prevent potential chafing of the power feeder cables of the integrated drive generator (IDG) in engine pylons No. 1 and No. 3 on the wings, and consequent arcing on the fuel lines in the engine pylons and possible fuel fire

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-164-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Washington, Usa - To prevent various failures of electric motor of the auxiliary hydraulic pump and associated wiring, which could result in fire at the auxiliary hydraulic pump and consequent damage to the adjacent electrical equipment and/or structure

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-55-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL- 604) series airplanes

Washington, Usa - To prevent cracking in the pressure bulkhead at frame station (FS) 409.00, which could result in uncontrolled depressurization of the airplane and/or reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-267-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes

Usa - To prevent peeling of the paint and markings from the dust covers for the flight data recorder (FDR) and cockpit voice recorder (CVR) equipment due to hydraulic mist from the actuators, which could result in the inability to identify the FDR and CV

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-112-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model EC-130B4 helicopters

Usa - To prevent failure of a forward fitting, an excess load on the other fittings, which could cause them to crack and break, which could result in loss of the air intake cowling in flight, and subsequent damage or loss of control of the helicopter

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-41-AD; Amendment... more