Airworthiness Directive 87-24-11
one-timeAirworthiness Directives; GARRETT TURBINE ENGINE COMPANY: Applies to Garrett Model GTCP 85 series Auxiliary Power Units Equipped with One-Piece Cast Turbine
Which aircraft AD 87-24-11 applies to
Applies to Garrett Model GTCP 85 series Auxiliary Power Units equipped with one-piece cast turbine wheels. Amendment 39-5781. To prevent turbine wheel separation and resulting containment shroud breach.
Whether AD 87-24-11 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.