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FAA AD on Boeing Model 767-200, -300, and -300F Series

USA - To prevent fatigue cracking in primary strut structure, which could result in separation of the strut and engine from the airplane

Airworthiness Directives DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-186-AD; Amendment 39-13768; AD 2004-16-12] RIN 2120-AA64 Preamble Information AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule. SUMMARY: This amendment supersedes three existing airworthiness directives (AD); applicable to certain...

AVIONEWS - World Aeronautical Press Agency - 101858

AVIONEWS - World Aeronautical Press Agency
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