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Security

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SecurityFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2008-09-15)

Washington, Usa - To detect and correct cracking in the vinyl interlayer or damage to the structural inner glass panes of the flight deck No. 2, No. 4, and No. 5 windows, which could result in loss of a window

Airworthiness Directive Federal Register Information [Federal Register: (Volume 73, Number 86)] [Page 24151-24153] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Taylorcraft, Inc. models A, B, and F series airplanes (2008-09-18)

Washington, Usa - To detect and correct corrosion or cracks in the wing strut attach fittings, which could result in failure of the wing strut attach fittings and lead to wing separation and loss of control

Airworthiness Directive Federal Register Information [Federal Register: May 2, 2008 (Volume 73, Number 86)] [Page 24162-24164] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

SecurityFAA AD on McDonnell Douglas model DC-10-10, DC- 10-10F, DC-10-15, and MD-10-10F airplanes (2008-09-17)

Washington, Usa - To detect and correct corrosion, and cracking of the air filler valve bore on the MLG cylinder, which could result in landing gear failure, significant damage to the airplane, and injury to personnel

Airworthiness Directive Federal Register Information [Federal Register: May 2, 2008 (Volume 73, Number 86)] [Page 24155-24157] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

SecurityFAA AD on MD Helicopters, Inc. model MD-900 series helicopters (2008-08-11)

Washington, Usa - To prevent fatigue cracking in the welds that connect the directional control pedal to the pedal shaft, resulting in loss of directional control and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: [Page 22787-22789] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Air Tractor, Inc. models AT-300, AT- 301, AT-302, AT-400, and AT-400A airplanes (2008-09-10)

Washington, Usa - To detect and correct cracks in the wing centerline splice joint. If not detected and corrected, these cracks could result in the wing separating from the airplane during flight

Airworthiness Directive Federal Register Information Federal Register: [Page 22795-22800] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on McDonnell Douglas model DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43; DC-8-50; DC-8F-54 and DC-8F-55; DC-8-60; DC-8-60F, DC-8-70; and DC-8-70F airplanes (2008-09-04)

Washington, Usa - To prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which could result in a fuel tank explosion and consequent loss of plane

Airworthiness Directive Federal Register Information Federal Register: [Page 21523-21526] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Kelly Aerospace Power Systems Turbochargers (2008-08-17)

Washington, Usa - To prevent hazardous amounts of carbon monoxide from entering the cabin, an increase in under-cowl temperatures hampering engine and accessory function, which could lead to an in-flight fire and loss of control

Airworthiness Directive Federal Register Information Federal Register: [Page 21222-21225] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes (2008-08-22)

Washington, Usa - To prevent a fire near a composite drain mast and possible disruption of the electrical power system caused by a lightning strike on a composite drain mast, which could result in the loss of several functions

Airworthiness Directive Federal Register Information Federal Register: [Page 21227-21229] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model ERJ-170 airplanes and model ERJ-190 airplanes (2008-08-21)

Washington, Usa - To prevent the flightcrew from performing a takeoff with a partially deployed thrust reverser, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 21231-21233] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA (Correction) AD on Airbus model A-330/200, A-330/300, A-340/200, and A-340/300 series airplanes (2008-06-07)

Washington, Usa - To prevent failure of the elevator servo controls during certain phases of takeoff, which could result in an unannounced loss of elevator control and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 20367] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket... more

SecurityFAA AD on Turbomeca Makila 1A and 1A1 turboshaft engines (2008-08-16)

Washington, Usa - To prevent dual-engine continued operation at 65% N1 after reversion of the ECU to the 65% N1 back-up mode due to temporary loss of N2 speed signal, which could lead to inability to continue safe flight

Airworthiness Directive Federal Register Information Federal Register: [Page 20525-20526] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Boeing model 757 airplanes (2008-08-12)

Washington, Usa - To prevent failure of the anchor tab of the bulkhead seal assembly, which in icing conditions could result in insufficient airflow to the wing TAI system, subsequent ice on wings, reduced control of airplane

Airworthiness Directive Federal Register Information Federal Register [Page 19993-19995] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket... more

SecurityFAA AD on Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. (2008-04-14)

Washington, Usa - To prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 19977-19979] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket... more

SecurityFAA AD on Bombardier model CL-600-1A11, CL-600-2A12, CL-600-2B16 airplanes, and model CL-600-2B19 airplanes (2008-08-06)

Washington, Usa - To prevent possible loss of control on take-off resulting from even small amounts of frost, ice, snow, or slush on the wing leading edges or forward upper wing surfaces

Airworthiness Directive Federal Register Information Federal Register: April 14, 2008 [Page 19989-19993] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/ 114HCA-0, and C5JFR36C1104/L114HCA-0 (2008-08-01)

Washington, Usa - To detect cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: April 14 ,2008 [Page 19971-19972] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more