Airworthiness Directive 87-02-04

one-time
AD 87-02-04 · 1987-01-01 · airframe

Airworthiness Directives; Instructions" of BAe Air Weapons Division (AWD) Service Bulletin (S/B) No. 32-19 dated December 19, 1985. If cracks are found, bef

Which aircraft AD 87-02-04 applies to

MakesBritish Aerospace

Visual inspection per BAe Air Weapons Division (AWD) Service Bulletin No. 32-19, dated December 19, 1985; repair cracks before further flight. Repeat visual inspection at intervals of 300 landings; conduct eddy current inspection if crack indications are found.

Whether AD 87-02-04 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Superseded by AD 2014-09540 — comply with the superseding directive.

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 87-02-04 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.