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

Facebook Twitter Youtube Instagram LinkedIn

Security

5,079 news found

SecurityFAA AD on MD Helicopters, Inc. model 369A, OH-6A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, and 369HS helicopters (2008-15-03)

Washington, Usa - To prevent disbonding and subsequent separation of an abrasion strip from a T/R blade, which could result in vibration, loss of the T/R, and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: July 30, 2008 [Page 44139-44140] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Bell Helicopter Textron Canada model 222, 222B, 222U, 230 and 430 helicopters (2008-14-01)

Washington, Usa - To prevent interruption of the fuel supply caused by failure of the fuel switch, which could result in loss of engine power and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: [Page 39569-39570] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes (2008-14-08)

Washington, Usa - To detect and correct broken or missing fasteners in the hinge segments with a single fastener row, which could lead to opening of the cargo door during flight and result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 39579-39580] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2008-13-12)

Washington, Usa - To detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap joint

Airworthiness Directive Federal Register Information Federal Register: [Page 38905-38908] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Airbus model A-330 airplanes and model A-340/200 and -300 series airplanes (2008-13-13)

Washington, Usa - To prevent the airplane from departing the runway during a CAT 2 or CAT 3 automatic landing or roll-out, due to differences between actual magnetic variation and the values in the ADIRU magnetic variation table

Airworthiness Directive Federal Register Information Federal Register: [Page 38895-38898] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on McDonnell Douglas model DC-9-81, DC-9-82, DC-9-83, DC-9-87, and MD-88 airplanes (2008-13-29)

Washington, Usa - To detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register: July 8, 2008 [Page 38883-38885] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Boeing model 777-200, -200LR, -300, and -300ER series airplanes approved for Extended-Range Twin-Engine Operational Performance Standards, ETOPS, (2008-14-11)

Washington, Usa - To prevent ETOPS operation with insufficient cargo fire suppression capability, which could result in an uncontained fire in the cargo compartment

Airworthiness Directive Federal Register Information Federal Register: July 8, 2008 [Page 38893-38895] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Lockheed model 382, 382B, 382E, 382F, 382G, and 382J series airplanes (2008-14-10)

Washington, Usa - To prevent failure of the upper engine mount bolts, which could result in reduced structural capability of an engine mount, and possible separation of a strut and engine from the airplane during flight

Airworthiness Directive Federal Register Information Federal Register: July 7, 2008 [Page 38311-38313] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Boeing model 757 airplanes equipped with Rolls Royce RB-211-535E engines (2008-13-20)

Washington, Usa - To prevent failure of the attachment bolts and consequent separation of a thrust reverser from the airplane during flight, which could result in structural damage to the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 37786-37789] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Hawker Beechcraft Corporation F-33 series and models G-33, V-35B, A-36, A-36TC, B-36TC, 95-B55, D-55, E-55, A-56TC, 58, 58P, 58TC, G-58, and 77 airplanes (2008-13-17)

Washington, Usa - To prevent failure of the circuit breaker toggle switch, which could result in smoke in the cockpit and the inability to turn off the switch

Airworthiness Directive Federal Register Information Federal Register: July 2, 2008 [Page 37783-37786] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Boeing model 767-200, -300, and -400ER series airplanes (2008-13-21)

Washington, Usa - To prevent the in-line flow indicators of the passenger oxygen masks from fracturing and separating, which could inhibit oxygen flow to the masks and consequently result in exposure of the passengers and cabin

Airworthiness Directive Federal Register Information Federal Register: July 2, 2008 [Page 37781-37783] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more