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FAA AD on McDonnell Douglas model DC-9-10, -20, - 30, -40, and -50 series airplanes

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 the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-57-AD; Amendment 39-12915; AD 2002-21-09] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, - 30, -40, and -50 Series Airplanes PDF Copy (If Available): Preamble Information Regulatory Information 2002-21-09...

AVIONEWS - World Aeronautical Press Agency - 35170
Rome, Italy, 10/25/2002 12:26
AVIONEWS - World Aeronautical Press Agency

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