Airworthiness Directive 63-21-04
one-timeAirworthiness 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
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:
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.