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Civil aviation

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Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, C4-605R Variant F, and F4-600R series airplanes; and model A-310 series airplanes

Usa - To prevent loss of the relevant alternating current (AC) bus bar, reduced structural integrity of the engine pylon, and consequent loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23090-23093] Header Information Header... more

Civil aviationFAA AD on Airbus model A-319, A-320, and A-321 series airplanes

To prevent leakage of hydraulic fluid from the parking brake operated valve (PBOV), which could cause the loss of the parking brake accumulator, and render the alternate braking system and the parking/emergency braking system inoperative, as well as caus

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23095-23097] Header Information Header... more

Civil aviationFAA AD on Boeing model 747-400 and -400D series airplanes

Usa - To prevent passenger service unit (PSU) panels from moving and falling from the PSU support rails during takeoff or landing, which could result in injury to passengers and could impede evacuation of the passengers in an emergency situation

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23098-23099] Header Information Header... more

Civil aviationFAA AD on Airbus model A-330/200 series airplanes

To prevent failure of the driving finger of the rudder servo control and consequent loss of the rudder servo control function in driving the rudder to its commanded position, which, if combined with an engine failure during takeoff or go around,

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 26, 2004 (Volume 69, Number 80)] [Page 22389-22392] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300B2 series airplanes; A-300B4 series airplanes; A-300B4-600, B4-600R, F4-600R, and C4-605R Variant F (Collectively Called A-300/600) series airplanes; and A-310 series airplanes

Washington, Usa - To detect and correct cracking of certain skin lap joints, which could result in reduced structural integrity and decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 21, 2004 (Volume 69, Number 77)] [Page 21397-21401] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300B2 and B4 series airplanes; A-300 B4-600, B4-600R, and F4-600R (Collectively Called A-300/600) series airplanes; and A-310 series airplanes

Usa - To prevent hard points in the throttle control system that could lead to jamming of the throttle control cable, which could result in an asymmetric thrust condition and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 19, 2004 (Volume 69, Number 75)] [Page 20811-20815] Header Information Header... more

Civil aviationFAA AD on Boeing model 767-300 series airplanes

Usa - To prevent interference of the A1 galley with the radial stiffener on the aft pressure bulkhead, which could result in fatigue crack propagation, leading to possible rapid decompression of the airplane or to damage and/or interference with theplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-125-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300 B4-600 and A-300 C4- 600 series airplanes

Usa - To detect and correct damage of the center tank fuel pumps and fuel pump canisters, which could result in separation of a pump from its electrical motor housing, loss of flame trap capability, and a possible fuel ignition source in the center fuel

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-80-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Usa - To detect and correct corrosion of the left- and right-hand horizontal stabilizer hinge fitting bolts, barrel nuts, and associated holes in the horizontal stabilizer structure, and the left- and right-hand elevator sector pinch bolts and associated

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-212-AD; Amendment... more

Civil aviationFAA AD on Fokker model F-28 Mark 0070 and 0100 series airplanes

Usa - To prevent fatigue cracking of the sliding member, which could result in possible separation of the MLG from the airplane and consequent reduced controllability of the airplane upon landing and possible injury to passengers

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-256-AD; Amendment... more