Airworthiness Directive 63-21-04

one-time
AD 63-21-04 · 1963-01-01 · appliance

Airworthiness Directives; -04 LOCKHEED: Amdt. 625 Part 507 Federal Register October 2, 1963. Applies to All Models L-18 and PV-1 Airplanes Equipped With Spa

Which aircraft AD 63-21-04 applies to

ModelsL-18, PV-1

Lockheed Model L-18 and PV-1 airplanes equipped with Spartan electrically actuated elevator trim tabs, to prevent runaway trim tab actuator operation; Model 18 airplanes with Spartan trim tab require installation per STC SA2-183.

Whether AD 63-21-04 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 63-21-04 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.