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Civil aviation

11,419 news found

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes

Washington, USA - To prevent fluid contamination inside the fueling float switch or changing of the wiring to the in-tank conduit, which could generate an ignition source and consequent fire and explosion in the fuel tank

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-44-AD; Amendment 39-13006; AD 2002-26-18] RIN... more

Civil aviationFAA AD on McDonnell Douglas DC-9-10, -20, -30, -40, and -50 series airplanes

Washington, USA - To detect and correct cracking in the fuselage skin or doubler at the corner of the forward lower cargo doorjamb, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-78-AD; Amendment 39-12998; AD 2002-26-10] RIN... more

Civil aviationFAA AD on Saab model SAAB 2000, SAAB SF340A, and SAAB 340B series airplanes

Washington, USA - To prevent ice from blocking the pitot system, due to the pitot tube not having enough heating capacity to stay above freezing temperature, which could result in erroneous airspeed indications

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-104-AD; Amendment 39-13007; AD 2002-26-19] RIN... more

Civil aviationFAA AD on Boeing model 747 series airplanes

To detect and correct wear damage of the fuselage skin in the area at the interface between the vertical stabilizer and fuselage skin, which could result in thinning and cracking of the fuselage skin, and consequent in-flight depressurization of the plan

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-85-AD; Amendment 39-13003; AD 2002-26-15] RIN... more

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

USA - To detect and correct an insufficient over-center force in the corresponding thrust reverser operating lever, and incorrect setting of the thrust reverser selector switch (S9), which could result in uncommanded deployment of the thrust reversers

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-290-AD; Amendment 39-13004; AD 2002-26-16] RIN... more

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, -800, and -900 series airplanes; model 747 series airplanes; and model 757 series airplanes

Washington, USA - To require the flightcrew to maintain certain minimum fuel levels in the center fuel tanks, and to prohibit the use of the horizontal stabilizer fuel tank (747-400) and certain center auxiliary fuel tanks (747)

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-309-AD; Amendment 39-12992; AD 2002-24-51] RIN... more

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

Washington, USA - To prevent fuel from being sprayed throughout the APU compartment and drawn out of the APU exhaust duct due to a cracked APU fuel nozzle, which could result in a fire or explosion in the APU compartment during flight

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-269-AD; Amendment 39-12995; AD 2002-26-07] RIN... more

Civil aviationFAA AD on Dornier model 328-300 series airplanes

Washington, USA - To prevent operation in weight/altitude/temperature conditions that exceed the performance capabilities of the airplane, which could result in impact with terrain during engine out performance- limited operations

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-293-AD; Amendment 39-12994; AD 2002-26-06] RIN... more

Civil aviationFAA AD on Airbus model A-330 and A-340 series airplanes

To prevent leakage of the parking brake operated valve and consequent failure of the "blue" hydraulic system and alternate parking brake and emergency braking systems, which could affect elements of the hydraulics for flaps, stabilizer, spoilers elevator

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-67-AD; Amendment 39-12999; AD 2002-26-11] RIN... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-10, -20, - 30, -40, and -50 series airplanes; and C-9 (Military) airplanes

Usa - To prevent internal overheating and arcing of circuit breakers and airplane wiring due to long-term use and breakdown of internal components of the circuit breakers, which could result in smoke and fire in the flight compartment and main cabin

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NM-287-AD; Amendment 39-12979; AD 2002-25-04] RIN... more

Civil aviationFAA AD on Boeing model 747 series airplanes powered by General Electric (GE) CF6-80C2 series engines

Washington, USA - To find and fix discrepant fasteners of the diagonal brace fittings, which could result in reduced structural integrity of the diagonal brace-to-strut attachment, and possible separation of the strut and engine from the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-17-AD; Amendment 39-12968; AD 2002-24-03] RIN... more