Airworthiness Directive 69-14-01
one-timeAD 69-14-01 · 1969-01-01 · other
Airworthiness Directives; 401A 402 402A 411 411A 421 421A E310H E310J T310P Textron Aviation Inc.\310G Textron Aviation Inc.\310H Textron Aviation Inc.\310I
Which aircraft AD 69-14-01 applies to
Makes401A 402 402A 411 411A 421 421A E310H E310J T310P Textron \310G Textron \310H Textron \310I Textron \310J Textron \310K Textron \310L Textron \310N Textron \310P Textron \320A Textron \320B Textron \320C Textron \320D Textron \320E Textron \320F Textron \401 Textron \401A Textron \402 Textron \402A Textron
ModelsT310P
Whether AD 69-14-01 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 69-14-01 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.