Airworthiness Directive 58-21-01

one-time
AD 58-21-01 · 1958-01-01 · airframe

Airworthiness 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:

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 58-21-01 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.