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Civil aviation

11,114 news found

Civil aviationFAA AD on Boeing model 747-200B, -200C, -200F, and -400F series airplanes (2005-08-09)

Washington, Usa - To find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20273-20275] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-600, -700, and -800 series airplanes (2005-08-10)

Washington, Usa - To prevent flammable fluid (such as fuel or hydraulic fluid) from leaking onto a hot engine exhaust nozzle or into the engine core fire zone, and consequently causing an uncontrolled fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20275-20276] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Cessna model 680 airplanes

Washington, Usa - To prevent a simultaneous loss of data from all four cockpit display units, and loss of primary navigation instruments, autopilot, flight director, master caution/ warning lights, aural warnings, global positioning system position infor

Airworthiness Directive Federal Register Information [Federal Register: April 14, 2005 (Volume 70, Number 71)] [Page 19682-19685] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, -100B, 100B SUD, -200B, -200C, -200F, and -300 series airplanes; and model 747SP and 747SR series airplanes (2005-08-01)

Washington, Usa - To detect and correct fatigue cracks in the body frames, skin and other internal structure in fuselage section 41, which could lead to rapid decompression and loss of the structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18290-18294] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 777-200 and -300 series airplanes equipped with Rolls Royce model RB-211 Trent 800 engines (2005-07-24)

Washington, Usa - To prevent failure of a thrust reverser and adjacent components and their consequent separation from the airplane, which could result in a rejected takeoff (RTO) and cause asymmetric thrust and consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18285-18287] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes

Washington, Usa - To prevent a broken terminal stud on the main relay of an electrical power generator, which could reduce the redundancy of electrical power systems, result in increased pilot workload, and contribute to reduced controllability of the ai

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18275-18277] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Dassault model Falcon 10 series airplanes

Washington, Usa - To prevent collapse of the flexible hoses in the wing anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18282-18285] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-300 and -400ER series airplanes (2005-07-13)

Washington, Usa - To prevent failure of the IFE cooling card to configure itself correctly in response to input signals from airplane system interfaces during a forward cargo fire, which could result in the IFE cooling fan causing smoke to penetrate occ

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17598-17600] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-100, -200C, -300, - 400, and -500 series airplanes (2005-07-19)

Washington, Usa - To find and fix fatigue cracking in the fuselage skin, doubler, bearstrap, and frames, which could result in reduced structural integrity of the frames, possible loss of a cargo door, and consequent rapid decompression of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17600-17603] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-400ER, 777-200, and 777-300 series airplanes (2005-07-16)

Washington, Usa - To prevent a galley, purser work station, or closet from detaching from the tie-down fitting studs during an emergency landing, which could injure passengers or crewmembers, or obstruct escape routes and impede emergency evacuation

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17590-17591] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2005-07-12)

Washington, Usa - To detect and correct fatigue cracking of the aft frame and frame support structure of the forward galley door, which could result in a severed fuselage frame web, rapid decompression of the airplane, and possible loss of the forward ga

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17596-17598] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318, A-319, A-320, and A-321 series airplanes

Washington, Usa - To prevent breakage of the piston rod bearing, which could cause loss of the associated hydraulic system and spoiler extension, and could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17591-17594] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes (2005-07-15)

Washington, Usa - To prevent a negative pressure condition from developing in the APU enclosure when the APU is operating on the ground, which could create a potential fire hazard if flammable liquid leakage occurs inside the APU enclosure and cannot be

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17604-17606] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD (Revision) on Hartzell Propeller Inc. models HC-B3TN-2, HC-B3TN-3, HC-B3TN-5, HC-B4TN-3, HC-B4TN-5, HC-B4MN-5, and HC-B5MP-3 turbopropellers

Washington, Usa - To preclude propeller attaching bolt failures or improperly secured propellers, which could lead to separation of the propeller from the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 6, 2005 (Volume 70, Number 65)] [Page 17315-17317] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas Model DC-9-15F Airplanes; and model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9- 50 series airplanes in All-Cargo Configuration (2005-07-18)

Washington, Usa - To ensure that cargo in the main cabin is adequately restrained and to prevent failure of components of the cargo loading system, failure of the floor structure, or shifting of cargo

Airworthiness Directive Federal Register Information [Federal Register: April 6, 2005 (Volume 70, Number 65)] [Page 17312-17315] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on General Electric Company CF34-8E series turbofan engines

Washington, Usa - To prevent dual-channel electrical signal faults in the master VG actuator which will cause an uncommanded reduction of thrust to idle with a subsequent loss of the ability to advance thrust above idle, and will result in a multiengine

Airworthiness Directive Federal Register Information [Federal Register: April 5, 2005 (Volume 70, Number 64)] [Page 17199-17201] Header Information DEPARTMENT OF TRANSPORTATION Federal... more