Airworthiness Directive 82-16-04 R1

one-time
AD 82-16-04 R1 · 1982-01-01 · airframe

Airworthiness Directives; Service Bulletin F28/27- 136 and Menasco Service Bulletin 27-63. C. Applies to airplanes with S/N's 11003 through 11024, and 11991

Which aircraft AD 82-16-04 R1 applies to

MakesFokker
ModelsF28
Serial-conditional — narrows to serials 11003–11024, 11991–11992.

Applies to airplanes with the specified serial numbers; compliance required within 300 hours in accordance with Fokker Service Bulletin F28/27-27, Revision 5, dated April 2, 1979 (see also Fokker Service Bulletin F28/27-136 and Menasco Service Bulletin 27-63).

Whether AD 82-16-04 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 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 82-16-04 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.

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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.