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Civil aviation

10,835 news found

Civil aviationFAA AD on McDonnell Douglas model DC-9-10, DC-9- 20, DC-9-30, DC-9-40, and DC-9-50 series airplanes (2006-07-08)

Washington, Usa - To detect and correct stress corrosion cracking of the main fuselage frame, which could result in extensive damage to adjacent structure and reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16201-16203] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318/100 and A-319/100; A-320/111; and A-320/200, A-321/100, A-321/200 (2006-07-09)

Washington, Usa - To ensure the integrity of the THSA's primary load path, which if failed, could result in an eventual failure of the THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16203-16206] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B4-600, B4-600R, and F4-600R series airplanes, and model C4-605R Variant F airplanes (2006-07-07)

Washington, Usa - To prevent crack formation in the sealing angles and lead to subsequent crack formation in the bottom skin of the wing, and resultant reduced structural integrity of the center spar section of the wing

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16206-16208] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Cirrus Design Corporation models SR-20 and SR-22 airplanes

Washington, Usa - To detect, correct, and prevent damage to the fuel line and wire bundles, which could result in fuel leaks. This failure could lead to unsafe fuel vapor within the cockpit and possible fire

Airworthiness Directive Federal Register Information [Federal Register: March 30, 2006 (Volume 71, Number 61)] [Page 16027-16029] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-319/131, -132, and -133; A-320/232 and -233; and A-321/131, -231, and -232 airplanes (2006-07-05)

Washington, Usa - To prevent structural failure of the secondary load path of the forward engine mount, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 30, 2006 (Volume 71, Number 61)] [Page 16025-16027] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330-200 and -300 series airplanes; and A-340-200 and -300 series airplanes (2006-06-13)

Washington, Usa - To prevent rupture of the inboard and outboard actuator fittings of the aileron servo controls, which could result in airframe vibration and consequent reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 27, 2006 (Volume 71, Number 58)] [Page 15020-15023] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318-100; A-319-100; A-320-111; A-320-200; A-321-100; and A-321-200 series airplanes (2006-06-15)

Washington, Usa - To prevent air leakage through the water drain valves, which could result in an insufficient concentration of fire extinguishing agent and consequent inability of the fire extinguishing system to suppress the fire

Airworthiness Directive Federal Register Information [Federal Register: March 27, 2006 (Volume 71, Number 58)] [Page 15017-15020] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Aerospatiale model ATR-72 airplanes

Washington, Usa - To prevent cracking of the upper arms of the secondary side brace assemblies of the MLG, which could result in collapse of the MLG during takeoff or landing, damage to the airplane, and possible injury to the flightcrew and passengers

Airworthiness Directive Federal Register Information [Federal Register: March 27, 2006 (Volume 71, Number 58)] [Page 15024-15027] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D series airplanes (2006-06-11)

Washington, Usa - To detect and correct cracking of the tension ties, shear webs, and frames of the upper deck, which could result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 22, 2006 (Volume 71, Number 55)] [Page 14367-14370] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-06-10)

Washington, Usa - To detect and correct cracks in the skin, bearstrap, and small steel doubler (if installed), which could propagate and result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 22, 2006 (Volume 71, Number 55)] [Page 14370-14374] Header Information DEPARTMENT OF TRANSPORTATION Federal... more