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Airworthiness Directive 82-24-06 R1

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AD 82-24-06 R1 · 1982-01-01 · airframe

Airworthiness Directives; 1982. This Amendment 39-4559 becomes effective February 7, 1983. FOOTER: B-N Group Ltd. BN-2 BN-2A BN-2A-26 BN-2A-27 BN-2A-6 BN-2A

Which aircraft AD 82-24-06 R1 applies to

MakesB-N Group Ltd.Britten-Norman
ModelsBN-2, BN-2A, BN-2A-26, BN-2A-27, BN-2A-6, BN-2A-8, BN-2A-9, BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3

Footer list partially visible in this excerpt; docket also filed under BRITTEN-NORMAN (Amendment 39-4506) (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 82-24-06 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 82-24-06 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.