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FAA AD on McDonnell Douglas model 717-200 airplanes

Usa - To detect and correct fatigue cracking of certain safe-life structure and certain principal structural elements, which could adversely affect the structural integrity of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-325-AD; Amendment 39-13274; AD 2003-17-01] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation...

fra/pec - 52094
Rome, Italy, 08/27/2003 18:07
AVIONEWS - World Aeronautical Press Agency

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