Airworthiness Directive 89-17-01 R1
one-timeAirworthiness Directives; markings in accordance with McDonnell Douglas AOL 8-669, dated April 19, 1974, paragraph 7, and with one of the following McDonnel
Which aircraft AD 89-17-01 R1 applies to
Lock pin handle and latch actuating shaft markings per McDonnell Douglas AOL 8-669, dated April 19, 1974, paragraph 7, and one of the listed McDonnell Douglas drawings (revisions AV / E / C / A-H).
Whether AD 89-17-01 R1 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.