Airworthiness Directive 82-12-04

one-time
AD 82-12-04 · 1982-01-01 · appliance

Airworthiness Directives; DETROIT DIESEL ALLISON: Applies to Detroit Diesel Allison (DDA) Combined Power Turbine and Propeller Governor Assembly, DDA P/N 68

Which aircraft AD 82-12-04 applies to

MakesDetroit Diesel Allison
Models401, 401A, 401B, 402, 402A, 402B, 414, N22B, N24A, 250-B15G, 250-B17, 250-B17B, 250-B17C
Part-conditional6875708, 8210-018.

Amendment 39-4396. Applies to Detroit Diesel Allison (DDA) Combined Power Turbine and Propeller Governor Assembly, DDA P/N 6875708 (Woodward P/N 8210-018), with specified serial numbers, as installed on the referenced engine/airframe model designations (source text is a garbled scraped table cross-referencing Nomad TC Pty Ltd, Rolls-Royce Corporation, and Textron applications).

Whether AD 82-12-04 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 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 82-12-04 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.

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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.