Airworthiness Directive 76-08-02 R2
one-timeAD 76-08-02 R2 · 1976-01-01 · other
Airworthiness Directives; 310J-1 310K 310L 310N 310P 310Q 310R 320 320-1 320A 320B 320C 320D 320E 320F 340 401 401A 401B 402 402A 402B 411 411A 414 421 421A
Which aircraft AD 76-08-02 R2 applies to
Makes310J-1 310K 310L 310N 310P 310Q 310R 320 320-1 320A 320B 320C 320D 320E 320F 340 401 401A 401B 402 402A 402B 411 411A 414 421 421A 421B E310H E310J T310P T310Q T310R Textron \310 Textron \310A Textron \310B Textron \310C Textron \310D Textron \310E Textron \310F Textron \310G Textron \310H Textron \310I Textron \310J Textron \310J-1 Textron \310K Textron \310L
ModelsT310P, T310Q, T310R
Whether AD 76-08-02 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 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 76-08-02 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.
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.