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SecurityFAA (Revision) AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-09-06 R1)

Washington, Usa - To detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 7, 2006 (Volume 71, Number 235)] [Page 70857-70859] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 Turbofan Engines (2006-25-01)

Washington, Usa - To prevent failure of the No. 3 bearing, which could result in an in-flight shutdown (IFSD) and smoke in the cockpit and cabin

Airworthiness Directive Federal Register Information [Federal Register: December 4, 2006 (Volume 71, Number 232)] [Page 70294-70297] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Air Tractor, Inc. models AT-502, AT- 502A, AT-502B, AT-602, AT-802, and AT-802A airplanes

Washington, Usa - To detect and correct loose fasteners; any cracks in the rudder or vertical fin skins, spars, hinges or brackets; and/or corrosion of the rudder and vertical fin hinge attaching structure

Airworthiness Directive Federal Register Information [Federal Register: November 16, 2006 (Volume 71, Number 221)] [Page 66661-66663] Header Information DEPARTMENT OF TRANSPORTATION Federal... more