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FAA AD on McDonnell Douglas model DC-9-31 and DC- 9-32 airplanes

Washington, Usa - To prevent fatigue cracking of the internal doublers and frame structure of the fuselage skin of the cockpit enclosure window sill, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-61-AD; Amendment 39-13324; AD 2003-20-06] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-9-31 and DC- 9-32 Airplanes PDF Copy (If Available): Preamble Information AGENCY: Federal...

fra/pec - 53261

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