Airworthiness Directive 58-21-01
one-timeAirworthiness Directives; accomplish the following: 1. Unless already accomplished per Lockheed wire FS/229080-W, within the next 50 flight hours thoroughly
Which aircraft AD 58-21-01 applies to
Bulkhead corrosion inspection per Lockheed wire FS/229080-W; examine aft side of bulkhead within next 50 flight hours, then recurring inspection at next block overhaul or within 4,000 flight hours (whichever occurs first); if corrosion found, unpressurized flight only pending repairs.
Whether AD 58-21-01 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:
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.