Airworthiness Directive 87-10-06 R1
one-timeAD 87-10-06 R1 · 1987-01-01 · reciprocating engine
Airworthiness Directives; AIRWORTHINESS DIRECTIVES FINAL RULES: 87-10-06 R1 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown
Which aircraft AD 87-10-06 R1 applies to
MakesAirworthiness Directives Final Rules 87-10-06 R1 Citation This Information Is Not Available Page Number Docket Number Unknown Amendment 39-6293 Ad Number 87-10-06 R1 Subject Heading Textron Lycoming
ModelsO-320-A, O-320-B, IO-320, O-360, IO-360-B, AEIO-360B, O-540, IO-540-C4B5, IO-540-C4D5D, IO-540-D4A5, IO-540-V4A5D, IO-540-W1A5D, IO-540-W3A5D, AEIO-540-D, TIO-540-AA1AD, TIO-540-AB1AD, O-320, O-320-H
Whether AD 87-10-06 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:
Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 87-10-06 R1 complied with on your aircraft?
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.