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Civil aviation

10,840 news found

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes (2004-07-10)

Usa - To prevent a malfunction of the aural warning for the landing gear, leading the crew to open the circuit breaker for the aural warning horn which stops the operation of other aural warnings of malfunctions in other systems and, thus, could jeopardi

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-101-AD; Amendment... more

Civil aviationFAA AD on Dassault model Mystere-Falcon 50, Mystere-Falcon 900, and Falcon 900 EX series airplanes

Usa - To prevent puncture of the fuel tank in the event of a belly landing, which could result in a post-landing fire if fuel leaking from the tank makes contact with the sparks from the airplane sliding on the ground

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-51-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-15, DC-9-31, and DC-9-32 airplanes

Usa - To detect and correct fatigue cracks in the corners and upper center of the door cutout of the aft pressure bulkhead, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-60-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747-400 and -400D series airplanes (2004-07-20)

Usa - To prevent possible interference between wire bundle W4489 and the receptacle housing of the chiller boost fan, drain tubes, and adjacent structure, which could result in damage to the wire bundle and consequent arcing and fire

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-01-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747-100, -100B, -100B SUD, -200B, -200C, -200F, -300, 747SR, and 747SP series airplanes equipped with Pratt & Whitney JT9D-3, -7, -7Q, and -7R4G2 series engines (2004-07-19)

Usa - To prevent improper connection of the cowl latch located in the left-hand side of the cowl panel assembly of each engine, which could result in separation of a cowl panel from the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-207-AD; Amendment... more

Civil aviationFAA AD on Boeing model 707 and 720 series airplanes (2004-07-06)

Washington, Usa - To detect and correct cracking and/or loss of the upper and lower barrel nuts and bolts that retain the aft trunnion support fitting, which could result in the collapse of the main landing gear upon landing

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-335-AD; Amendment... more

Civil aviationFAA AD on General Electric Aircraft Engines CT7 series turboprop engines

Usa - To prevent separation of PGB left-hand and right-hand idler gears, which could result in uncontained PGB failure and internal bulkhead damage, possibly prohibiting the auxiliary feathering system from fully feathering the propeller on certain PGBs

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-48-AD; Amendment... more

Civil aviationFAA AD on Construcciones Aeronauticas, SA (Casa), model C-212 series airplanes (2004-07-17)

Washington, Usa - To prevent failure of the auxiliary landing gear direction system, which could result in abnormal vibrations during takeoff and landing runs, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-262-AD; Amendment... more

Civil aviationFAA AD on Boeing model 767-400ER series airplanes

To prevent fatigue cracking in the aft lower lug run-out region of the deflection control track, which could result in the loss of the secondary load path for the outboard flap, resulting in loss of the outboard flap and consequent reduced controllabilit

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-287-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes

Usa - To prevent an inability to lower or retract the landing gear using the landing gear control handle, which could result in use of Emergency Procedures using the landing gear manual release

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-157-AD; Amendment... more

Civil aviationFAA AD on Construcciones Aeronauticas, SA (Casa), model C-235 series airplanes (2004-07-16)

Usa - To prevent the flight crew from being able to inhibit the aural warning for the landing gear up, and the possibility that the flight crew of the next flight or possibly of the same flight could inadvertently land the airplane with the landing gear

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-160-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes (2004-07-05)

Usa - To detect and correct fatigue cracking, which could result in major damage to the adjacent structure of the pylon aft spar upper cap, and consequent reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NM-255-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-14, DC-9- 15, DC-9-15F, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C- 9A, C-9B), DC-9-33F, DC-9-34, and DC-9-34F; DC-9- 21, DC-9-41, and DC-9-51 series airplanes (2004-07-04)

Washington, Usa - To prevent overheating of the ballast transformers due to aging fluorescent tubes that cause a higher power demand on the ballast transformers, which could result in smoke in the cockpit

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-58-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 (Regional Jet Series 700 & 701), and CL-600-2D24 (Regional Jet Series 900) series airplanes

Washington, Usa - To detect and correct cracking in the primary fuel ejector, which could cause fuel leakage into the center fuel tank, and result in engine shutdown during flight

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-41-AD; Amendment... more

Civil aviationFAA AD on Sikorsky Aircraft Corporation model S-76 A, B, and C helicopters

Washington, Usa - To prevent both autopilots from disengaging following a No. 2 DC generator failure, and subsequent loss of control of the helicopter during instrument meteorological conditions (IMC) flight

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-45-AD; Amendment... more

Civil aviationFAA AD on Dornier model 328-100 series airplanes

Usa - To prevent failure of the support arms of the ground spoiler assemblies due to cracking, which could result in loss of function and/or separation of the affected ground spoiler assemblies from the airplane, and consequent reduced controllability of

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-300-AD; Amendment... more

Civil aviationFAA AD on BAE Systems (Operations) Limited (Jetstream) model 4101 airplanes

Usa - To detect and correct damage of the horizontal and vertical stabilizer attachment fittings, which could result in reduced structural integrity of the horizontal and vertical stabilizers and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-63-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-330-301, -321, -322, - 341, and -342 series airplanes; A-340/211, -212, 213, -311, - 312, and -313 series airplanes

Usa - To prevent cracking of the wire harness slot on the inner rear spar of the wing, which could result in reduced structural integrity of the wing

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-380-AD; Amendment... more