Airworthiness Directive 84-13-06 R2

one-time
AD 84-13-06 R2 · 1984-01-01 · propeller

Airworthiness Directives; grip, accomplish the following: (a) Within the next 10 hours time in service, inspect the tail rotor blade grip in accordance with

Which aircraft AD 84-13-06 R2 applies to

MakesAgusta
Models109

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 84-13-06 R2 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 84-13-06 R2 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.