Is AD 2008-14-10 a recurring Airworthiness Directive?

No — AD 2008-14-10 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2008-14-10 apply to?

AD 2008-14-10 applies to Lockheed — models 382, 382B, 382E, 382F, 382G, 382J. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2008-14-10

one-time

Official AD 2008-14-10 · FR doc E8-15181 · 2008-07-07 · airframe

Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J Series Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for all Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J series airplanes. This AD requires, among other actions, an inspection to determine whether a certain upper engine mount bolt is installed, and replacement of any discrepant upper engine mount bolt with a new one. This AD results from a report indicating that several upper engine mount bolts manufactured by a certain supplier broke during installation. We are issuing this AD to prevent failure of the upper engine mount bolts, which could result in reduced structural capability of an engine mount, and possible separation of a strut and engine from the airplane during flight.

Which aircraft AD 2008-14-10 applies to

MakesLockheed

Models382, 382B, 382E, 382F, 382G, 382J

Whether AD 2008-14-10 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 2008-14-10 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 →Read the full directive (Federal Register)

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.