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Security

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SecurityFAA AD on Cessna Aircraft Company models 401, 401A, 401B, 402, 402A, and 402B airplanes (2009-04-04)

Washington, Usa - To detect and correct such cracks, which, if not corrected, could result in failure of the wing auxiliary spar web and cause landing gear collapse during normal landing

Airworthiness Directive Federal Register Information Federal Register: [Page 7552-7554] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket... more

SecurityFAA AD on Boeing model 737-600, -700, -700C, -800 and -900 series airplanes (2009-01-02)

Washington, Usa - To prevent frame cracking, which, if not corrected, could lead to a severed frame that, combined with cracking of the skin lap splice above stringer 10, could result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 4117-4119] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Air Tractor, Inc. models AT-200, AT- 300, AT-400, AT-500, AT-600, and AT-800 series airplanes (2008-26-01)

Washington, Usa - To prevent the front and rear connections of the overturn skid plate to the airplane from breaking, which could allow foreign debris to enter the cockpit during an airplane overturn

Airworthiness Directive Federal Register Information Federal Register: [Page 78944-78946] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on McDonnell Douglas model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43; DC-8-50; DC-8F-54 and DC-8F-55; DC-8-60; DC-8-60F; DC-8-70; and DC-8-70F airplanes (2008-26-07)

Washington, Usa - To prevent the loss of structural integrity of the wing

Airworthiness Directive Federal Register Information Federal Register: [Page 78946-78948] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Cessna Aircraft Company 172, 175, 177, 180, 182, 185, 188, 206, 207, 208, 210, 303, 336, and 337 series airplanes (2008-26-10)

Washington, Usa - To prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control

Airworthiness Directive Federal Register Information Federal Register: [Page 78939-78944] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on General Electric Company (GE) CT7-8A turboshaft engines (2008-26-02)

Washington, Usa - To prevent failure of the No. 3 bearing due to contamination by aluminum oxide, which could result in a possible in-flight shutdown of the engines and loss of control or forced landing of the aircraft

Airworthiness Directive Federal Register Information Federal Register: [Page 78175-78178] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Boeing model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes (2008-25-07)

Washington, Usa - To detect and correct cracks or fractures of the primary structural and fail-safe load paths of the inboard and outboard trailing edge flaps, which could result in the loss of a flap during takeoff or landing

Airworthiness Directive Federal Register Information Federal Register: [Page 75305-75307] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more