Airworthiness Directive 81-17-01
one-timeAirworthiness Directives; series helicopters Brantley (Hynes) Model B2 series helicopters Enstrom Model F28, F28A, F28F; 280, 280F helicopters, Model F28C a
Which aircraft AD 81-17-01 applies to
Concerns vibrator assemblies (stall warning) on Brantly B-2 series and Enstrom F28/280 series helicopters equipped with Avco Lycoming HIO-360 engine; source text truncated in available record.
Whether AD 81-17-01 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.