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Civil aviation

11,047 news found

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

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

Civil aviationFAA Emergency AD on Boeing Defense and Space Group (Boeing) model 234 helicopters

Washington, Usa - To detect a crack in the upper shaft extension, which could result in catastrophic failure of the aft vertical shaft assembly and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2004-SW-09-AD; AD 2004-06-51... more

Civil aviationFAA AD on Airbus model A-319, A-320, and A-321 series airplanes (2004-06-02)

Usa - To prevent failure of a lower guide rod fitting, which could cause a rear passenger door to jam during opening, delaying an emergency evacuation and resulting in injury to passengers or crew members

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-18-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-200 series airplanes modified by supplemental Type Certificate ST00516AT (2004-05-27)

To eliminate the possibility that the airplane crew could be unable to remove power from the in-flight entertainment (IFE) system during a non-normal or emergency situation, which could result in the airplane crew's inability to control smoke or fumes in

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-238-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-14, DC-9-15, and DC-9-15F; DC-9-20, -30, -40, and -50; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes

Washington, Usa - To prevent uncommanded seat movement during takeoff and/or landing, which could result in interference with the operation of the airplane and consequent temporary loss of control of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2003-16647; Directorate... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes (2004-05-12)

Usa - To prevent excessive wear of the gearboxes and subsequent movement or jamming of the engine throttle; movement of the throttle towards the idle position brings it close to the fuel shut-off switch, which could result in an in-flight engine shutdown

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-20-AD; Amendment... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes (2004-05-21)

Usa - To prevent the mechanical disconnection of a flap actuator, which, if followed by failure of the flap panel's second actuator due to increased loading, could result in flap asymmetry and consequent loss of controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-258-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F airplanes

Usa - To prevent failure of the electric motors of the hydraulic pump and associated wiring, which could result in fire at the auxiliary hydraulic pump and consequent damage to the adjacent electrical equipment and/or structure

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-362-AD; Amendment... more