It does not receive public funding
Editor in chief:
CLARA MOSCHINI

Facebook Twitter Youtube Instagram LinkedIn

Civil aviation

11,448 news found

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes (2004-22-27)

Washington, Usa - To prevent flammable fluid in the upper or rear pylon areas from leaking past unsealed areas and onto a hot engine nozzle, which could result in ignition of the fluid, causing an undetected and uncontrollable fire to spread into the eng

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2004 (Volume 69, Number 216)] [Page 64852-64853] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330, A-340/200, and A-340/300 series airplanes

Washington, Usa - To prevent loss of the sensor strut function, resulting in the inability to detect flap drive disconnection at flap track stations 4 and 5, which could lead to separation of the outboard flap from the airplane, and consequent reduced co

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2004 (Volume 69, Number 216)] [Page 64836-64839] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 series airplanes, and models 70 and 300 airplanes

Washington, Usa - To detect and correct cracks in the NLG fork, which could result in reduced structural integrity and inability of the NLG fork to carry design limit and ultimate loads

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2004 (Volume 69, Number 216)] [Page 64842-64846] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-310 series airplanes; and model A-300 B4-600, B4-600R, and F4-600R series airplanes; and model C4- 605R Variant F airplanes

Washington, Usa - To prevent rupture of the housing of the RAT ejection jack due to overpressure in the jack caused by overfilling the hydraulic fluid, and consequent failure of the RAT ejection jack

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2004 (Volume 69, Number 216)] [Page 64854-64856] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 and -11F airplanes (2004-22-17)

Washington, Usa - To prevent moisture from entering through the rear of the connector of the ODUs located in the overhead baggage stowage racks, which could result in a short, damage to the connector pins, and consequent smoke and/or fire in the cabin

Airworthiness Directive Federal Register Information [Federal Register: November 9, 2004 (Volume 69, Number 216)] [Page 64850-64852] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Saab model Saab SF-340A and Saab 340B series airplanes

Washington, Usa - To prevent the elevator and aileron trim-tab bearings from coming loose, which could result in excessive play in the elevator and aileron trim systems, and reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: November 5, 2004 (Volume 69, Number 214)] [Page 64482-64483] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Gulfstream model GV and GV-SP series airplanes

Washington, Usa - To prevent chafing of the electrical wires of the wiring harness against the crew oxygen bottle, which could result in electrical shorting and possible fire in the underfloor structure of the airplane

Airworthiness Directive Federal Register Information [Federal Register: November 4, 2004 (Volume 69, Number 213)] [Page 64255-64258] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-400 and -400D series airplanes

Washington, Usa - To prevent ceiling panels from falling into the passenger cabin area in the event of failure of certain latch assemblies on the ceiling panels, which could result in consequent injury to the flightcrew and passengers

Airworthiness Directive Federal Register Information [Federal Register: November 4, 2004 (Volume 69, Number 213)] [Page 64253-64255] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-400 and -400F series airplanes

Washington, Usa - To prevent cracked/fractured side guide support fittings in the lower lobe cargo compartments, which could result in unrestrained cargo shifting in flight and damaging the airplane structure or systems, and consequent reduced

Airworthiness Directive Federal Register Information [Federal Register: November 2, 2004 (Volume 69, Number 211)] [Page 63443-63445] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To detect and correct fatigue cracking of the wing trunnion fittings or adjacent structure, which could result in failure of the main landing gear, consequent damage to surrounding structure, and possible loss of control of the plane

Airworthiness Directive Federal Register Information [Federal Register: October 29, 2004 (Volume 69, Number 209)] [Page 63053-63054] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Dornier model 328-100 and -300 series airplanes

Washington, Usa - To prevent the failure of critical ice protection systems following a lightning strike, which could result in reduced controllability and degraded performance of the airplane in the event of an encounter with icing conditions

Airworthiness Directive Federal Register Information [Federal Register: October 28, 2004 (Volume 69, Number 208)] [Page 62805-62806] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Various Transport Category Airplanes on Which Cargo Restraint Strap Assemblies Have Been Installed per Supplemental Type Certificate (STC) ST01004NY

Washington, Usa - To prevent shifting or unrestrained cargo in the cargo compartment, which could cause an unexpected change in the airplane's center of gravity, damage to the airplane structure and/or flight control system, a hazard to the flightcrew,

Airworthiness Directive Federal Register Information [Federal Register: October 27, 2004 (Volume 69, Number 207)] [Page 62566-62567] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon (Beech) model MU-300-10, 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) model Beech MU-300 airplanes

Washington, Usa - To prevent the accumulation of fuel and/or fuel vapor in the spoiler mixer bay and/or the aft fuselage compartment, which could result in a fire in the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 27, 2004 (Volume 69, Number 207)] [Page 62570-62571] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To find and fix discrepancies of the fuselage skin, which could result in fatigue cracking due to cabin pressurization, and consequent rapid in-flight decompression of the airplane fuselage

Airworthiness Directive Federal Register Information [Federal Register: October 27, 2004 (Volume 69, Number 207)] [Page 62567-62569] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To prevent failure of the outer and inner hinge pins due to corrosion or cracking, which could allow the pins to migrate out of the joint and result in intermittent movement of the horizontal stabilizer structure and consequent loss o

Airworthiness Directive Federal Register Information [Federal Register: October 26, 2004 (Volume 69, Number 206)] [Page 57632-57636] Header Information DEPARTMENT OF TRANSPORTATION Federal... more