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FAA AD on Airbus model A-300 B2 and B4 series airplanes; and A-300 B4-600, B4-600R, and F4-600R series airplanes

Washington, Usa - To detect and correct fatigue cracking of the upper radius of the forward fitting of fuselage frame 47, which could result in propagation of the cracking to the rear fitting and reduced structural integrity of frame 47

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-378-AD; Amendment 39-13091; AD 2003-06-04] RIN 2120-AA64 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; and A300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600) Series Airplanes PDF Copy (If Available): Preamble...

AVIONEWS - World Aeronautical Press Agency - 43153
Rome, Italy, 03/28/2003 14:18
AVIONEWS - World Aeronautical Press Agency

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