Airworthiness Directive 64-14-05
one-timeAD 64-14-05 · 1964-01-01 · airframe
Airworthiness Directives; Lockheed P/N 800618, Has Accumulated More Than 5,000 Hours' Time in Service. Compliance required as indicated. To eliminate the po
Which aircraft AD 64-14-05 applies to
MakesLockheed P N 800618 Has Accumulated More Than 5 000 Hours' Time In Service Compliance Required As Indicated To Eliminate Possibility Of Jamming Main Landing Gear Accomplish ) Periodic Inspections Described In And May Be Discontinued When P N 800618-3 Is Replaced By P N 841275-101 And P N 800618-4 Is Replaced By P N 841275-102 Upon Request Of Applies To All
Models188A, 188C
Applies to all models of the make above.
Whether AD 64-14-05 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 64-14-05 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.