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FAA AD on Boeing model 767-200, -300, and -300F series airplanes (2004-19-06)

Usa - To detect and correct fatigue cracking or corrosion of the fail- safe straps, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: September 27, 2004 (Volume 69, Number 186)] [Page 57636-57638] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-263-AD; Amendment 39-13800; AD 2004-19-06] RIN 2120-AA64 Airworthiness Directives; Boeing Model 767-200, -300,...

fra/pec - 104134
Rome, Italy, 09/28/2004 15:42
AVIONEWS - World Aeronautical Press Agency

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