Airworthiness Directive 85-17-01
one-timeAirworthiness Directives; the following within the next 30 days after the effective date of this AD or upon accumulation of 1000 flight hours on any engine,
Which aircraft AD 85-17-01 applies to
Within 30 days after the effective date or upon accumulation of 1,000 flight hours on any engine, whichever is later, inspect and repair wiring and terminals per Boeing Alert Service Bulletin 767 (bulletin number truncated in source text); special flight permits allowed to reposition aircraft for compliance.
Whether AD 85-17-01 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 →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.