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Civil aviation

9,747 news found

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
Collins AerospaceCollins Aerospace

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
Collins AerospaceCollins Aerospace

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

Usa - To prevent the loss of the emergency evacuation slides during flight, which could result in damage to the fuselage, and to prevent incorrect inflation of the emergency evacuation slides, which could result in the emergency exits being unusable

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-339-AD; Amendment... more

Civil aviationFAA AD on Saab model SAAB 2000 series airplanes

Usa - To prevent long-term damage to the engine mounting structure (EMS), and loss of redundancy on the EMS, which could result in possible separation of an engine from the airplane, reduced controllability of the airplane, and injury to persons or prope

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-115-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-100, -200, -300, -400, and -500 series airplanes

Usa - To prevent engine damage, airframe damage, and/or hazard to persons or property on the ground as a result of "blue ice" that has formed from leakage of the lavatory drain system or flush/fill systems and dislodged from the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 95-NM-111-AD; Amendment... more