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Civil aviation

10,840 news found

Civil aviationFAA AD on McDonnell Douglas model MD-11 and -11F airplanes (2004-01-17)

Washington, Usa - To prevent potential chafing of the power feeder cables of the integrated drive generator (IDG) in engine pylons No. 1 and No. 3 on the wings, and consequent arcing on the fuel lines in the engine pylons and possible fuel fire

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-164-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Washington, Usa - To prevent various failures of electric motor of the auxiliary 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. 2003-NM-55-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL- 604) series airplanes

Washington, Usa - To prevent cracking in the pressure bulkhead at frame station (FS) 409.00, which could result in uncontrolled depressurization of the airplane and/or reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-267-AD; Amendment... more

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

Usa - To prevent peeling of the paint and markings from the dust covers for the flight data recorder (FDR) and cockpit voice recorder (CVR) equipment due to hydraulic mist from the actuators, which could result in the inability to identify the FDR and CV

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-112-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model EC-130B4 helicopters

Usa - To prevent failure of a forward fitting, an excess load on the other fittings, which could cause them to crack and break, which could result in loss of the air intake cowling in flight, and subsequent damage or 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. 2003-SW-41-AD; Amendment... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (Embraer) model EMB-135 and -145 series airplanes

Usa - To detect and correct oxidation of the pitot-true air temperature (TAT) relay, which could result in increased resistance and overheating of the relay and consequent smoke in the cockpit; and to detect and correct oxidation of the full authority di

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-336-AD; Amendment... more

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

Usa - To prevent jamming of the locking pin of the passenger door, which could result in inability to open the passenger door and delay of evacuation in an emergency, resulting in possible injury to passengers or crew

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-120-AD; Amendment... more

Civil aviationFAA AD on Boeing model 767-200, -300, and -300F series airplanes

Washington, Usa - To prevent loss of the fuse pin of the aft pitch load fitting of the diagonal brace, which could result in increased loads in the wing-to-strut joints and consequent separation of the strut and engine from the wing

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-152-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4 series airplanes; and A-300 B4-600, B4-600R, C4-605R Variant F, and F4-600R series airplanes

Washington, Usa - To find and fix cracking of the lower outboard flange of gantry No. 4, which could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-248-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-600, 737-700, 737-800, 757-200, and 757-300 series airplanes

Washington, Usa - To prevent a short circuit in a video distribution unit (VDU) connector and consequent arcing and damage to wiring within the connector, which could result in damage to adjacent systems or structure and possible smoke or fire in the air

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-374-AD; Amendment... more

Civil aviationFAA AD on Eurocopter Deutschland model MBB-BK-117 A-1, A-3, A-4, B-1, B-2, and C-1 helicopters

Washington, Usa - To prevent cracking, separation of the bearing cage, failure of a bearing, failure of the TR transmission or INT gearbox, 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. 2003-SW-21-AD; Amendment... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 and Avro 146-RJ series airplanes

Washington, Usa - To detect and correct corrosion and cracking of the inner webs and flanges at frames 15, 18, 41, and 43, which could result in 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. 2002-NM-144-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas MD-90-30 airplanes

Washington, 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 mai

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-103-AD; Amendment... more

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

Washington, Usa - To prevent rupture of the potable water tank during flight of the airplane, which could result in structural damage to the airplane and its inability to sustain flight loads

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-422-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model MD-90-30 airplanes

Washington, Usa - To ensure that the lanyards on the pressure relief door for the thrust reverser have adequate strength so that the door will not detach from the thrust reverser in the event that an engine bleed air duct bursts, which could result in th

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-169-AD; Amendment... more