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Security

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SecurityFAA AD on Cessna Aircraft Company models LC40-550FG, LC41-550FG, and LC42-550FG airplanes (2009-09-09)

Washington, Usa - To detect and correct damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 19873-19876] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Airbus model A-318/100 and A-319/100; A-320/111; A-320/200; and A-321/100 and A-321/200 series airplanes (2009-09-05)

Washington, Usa - To prevent contact between the horizontal hinge pin and the adjacent electrical wire harness, which could result in damage to electrical wires, and consequent arcing and/or failure of associated systems

Airworthiness Directive Federal Register Information Federal Register: [Page 19876-19877] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on General Electric Company (GE) CF6-80A series turbofan engines (2009-08-06)

Washington, Usa - To prevent cracks developing at the aft chamfer of the blade dovetail slots that could propagate to a failure of the disk and cause an uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 69)] [Page 16754-16755] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Honeywell Flight Management Systems (FMSs) installed on various transport category airplanes (2009-08-01)

Washington, Usa - To prevent a shift in the FMS computed position, which could result in uncommanded deviations from the intended flight path of the airplane

Airworthiness Directive Federal Register Information [Federal register: (Volume 74, Number 67)] [Page 16121-16124] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Bell Helicopter Textron Canada Limited model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, and 430 helicopters (2009-08-03)

Washington, Usa - To prevent loss of a blade tip weight, loss of a blade, and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: [Page 16112-16114] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Hawker Beechcraft Corporation model BH-125 series 600A airplanes and model HS-125 series 700A airplanes modified in accordance with Supplemental Type Certificate (STC) SA-2271SW (2009-08-04)

Washington, Usa - To prevent smoke and fumes in the cockpit in the event that a blower motor seizes and overheats due to excessive current draw

Airworthiness Directive Federal Register Information Federal Register: [Page 16116-16117] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on McDonnell Douglas model DC-8-50; DC-8F-54 and DC-8F-55; DC-8-60; DC-8-60F; DC-8-70; and DC-8-70F series airplanes (2009-08-02)

Washington, Usa - To prevent pump inlet friction when the fuel pumps are continually run as the center wing fuel tank becomes empty, and/or electrical arc burnthrough, which could result in a fuel tank fire or explosion

Airworthiness Directive Federal Register Information Federal Register: [Page 15841-15842] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA (Correction) AD on Bombardier model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes equipped with a Cockpit Door Electronic Strike System (2008-26-03)

Washington, Usa - To prevent failure of this equipment, which could compromise flight safety

Airworthiness Directive Federal Register Information Federal Register: [Page 15665-15666] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines (2009-07-12)

Washington, Usa - To prevent the inability to restart both engines after flameout due to excessive friction of the 4-step seal, which could result in subsequent forced landing of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 14929-14931] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Piper Aircraft, Inc. models PA-46-350P and PA-46R-350T airplanes (2009-07-08)

Washington, Usa - To detect and correct incorrect installation of 35-amp and 250-amp current limiters, which could result in failure of the 35-amp current limiter if installed in the 250-amp location

Airworthiness Directive Federal Register Information Federal Register: [Page 14461-14463] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA (Revision) AD on Air Tractor, Inc. models AT-400, AT- 401, AT-401B, AT-402, AT-402A, and AT-402B airplanes (2006-08-08R1)

Washington, Usa - To prevent fatigue cracks in the wing lower spar cap, that if not detected and corrected, could result in wing separation and loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 14465-14471] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more