Airworthiness Directive 2000-19-09
one-timeAirworthiness Directives; Boeing Model 767 Series Airplanes Powered by Rolls-Royce RB211 Series Engines
What this AD requires
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 767 series airplanes powered by Rolls-Royce RB211 series engines. This action requires modification of the nacelle strut and wing structure. This action is necessary to prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut. This action is intended to address the identified unsafe condition.
Which aircraft AD 2000-19-09 applies to
Modify nacelle strut and wing structure (both sides) per Boeing SB 767-54-0082 (dated October 28, 1999), addressing fatigue cracking in primary strut structure, prior to 37,500 total flight cycles or 20 years since date of manufacture (or optional threshold formula), whichever is later, or within 3,000 flight cycles after the AD effective date. Prior/concurrent actions per Boeing SBs 767-29-0057, 767-54-0059, 767-54-0069 Rev 1, 767-54-0083, 767-54-0088 Rev 1, and 767-57-0053 Rev 2 also required.
Whether AD 2000-19-09 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.