Airworthiness Directive 87-02-04
one-timeAirworthiness 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
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Superseded by AD 2014-09540 — comply with the superseding directive.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:
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.