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Security

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SecurityFAA AD on Sikorsky Aircraft Corporation (Sikorsky) model S-92A helicopters (2010-10-03)

Washington, Usa - To prevent failure of the MGB filter bowl assembly due to failure of the mounting studs or the filter bowl, loss of oil from the MGB, failure of the MGB, and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register [Page 27409-27411] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Sikorsky Aircraft Corporation model S-76A, B, and C helicopters (2010-10-02)

Washington, Usa - To prevent degraded servo actuator performance as a result of piston head seal leaking and plasma spray flaking, which could result in subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: [Page 26885-26887] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on CFM International, SA CFM56-5B1/P, 5B2/P, 5B3/P, 5B3/P1, 5B4/P, 5B5/P, 5B6/P, 5B7/P, 5B8/P, 5B9/P, 5B1/2P, 5B2/2P, 5B3/2P, 5B3/2P1, 5B4/2P, 5B4/P1, 5B6/2P, 5B4/ 2P1, and 5B9/2P engines (2010-09-14)

Washington, Usa - To prevent two engines on an airplane from having greater than 80 °C of EGT margin deterioration

Airworthiness Directive Federal Register Information Federal Register: [Page 23574-23576] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on McDonnell Douglas Corporation model DC-10/10, DC-10/10F, DC-10/15, DC-10/30, DC-10/30F, DC-10/40, DC-10/40F, MD-10/10F, MD-10/30F, MD-11, and MD-11F airplanes (2010-09-12)

Washington, Usa - To prevent point-of-contact arcing or filament heating damage in the fuel tanks, which could result in fuel tank explosions and consequent loss of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 23571-23572] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA (Correction) AD on General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B series turbofan engines (2010-01-04)

Washington, Usa - To prevent failure of certain P/N and S/N fan blades and aft actuator head hoses, which could result in an under-cowl fire and subsequent damage to the airplane

Federal Aviation Administration Airworthiness Directive Federal Register Information Federal Register: [Page 1017-1020] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

SecurityFAA AD on Honeywell International Inc., Primus EPIC and Primus APEX Flight Management Systems, installed on, but not Limited to EMBRAER ERJ-170, ERJ-190 and Pilatus Aircraft Ltd. model PC-12/47E airplanes (2010-09-04)

Washington, Usa - To provide the flightcrew with procedures to recover from or work around these software anomalies during flight, which could lead to an airplane departing from its scheduled flight path

Airworthiness Directive Federal Register Information Federal Register: [Page 22519-22521] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on The Boeing Company model 747/200B series airplanes (2010-09-03)

Washington, Usa - To detect and correct cracking of the stringer 6 lap joints where certain external doublers were not installed, which could result in rapid decompression and loss of structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 75, Number 82)] [Page 22514-22516] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more