Airworthiness Directive 87-12-05

one-time
AD 87-12-05 · 1987-01-01 · turbine engine

Airworthiness Directives; engine failure, remove gas producer turbine (GPT) and power turbine (PT) disks and spacers from service, and replace with servicea

Which aircraft AD 87-12-05 applies to

Applicability depends on the aircraft’s type certificate — check it against the specific tail.

Whether AD 87-12-05 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Superseded by AD 06-63 — comply with the superseding directive.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 87-12-05 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.