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Security

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SecurityFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes (2008-24-51)

Washington, Usa - To prevent extended dry-running of the fuel pump, which could lead to localized overheating of parts inside the fuel pump, and which could produce an ignition source inside the fuel tank

Airworthiness Directive Federal Register Information Federal Register: [Page 8155-8159] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

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