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Security

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SecurityFAA AD on McDonnell Douglas model DC-8-61, DC-8- 61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F airplanes (2008-16-11)

Washington, Usa - To detect and correct fatigue cracking of door jamb corners of the forward and aft service doors, which could adversely affect the structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 47043-47044] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR... more

SecurityFAA AD on Boeing model 737-600, -700, -700C, - 800, -900, and -900ER series airplanes (2008-16-13)

Washington, Usa - To prevent fracture of the elevator tab pushrod ends, which could result in excessive in-flight vibrations of the elevator tab, possible its loss, and consequent loss of controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register: August 5 ,2008 [Page 45350-45351] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

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