Airworthiness Directive 84-02-04
one-timeAirworthiness Directives; accordance with the instructions of Messier-Hispano-Bugatti (MHB) Service Bulletin 470-32-172, Revision 1, dated June 10, 1981, fo
Which aircraft AD 84-02-04 applies to
Sliding rod attachment fitting rework per Messier-Hispano-Bugatti (MHB) Service Bulletin 470-32-172 Rev 1, for aircraft with serial numbers specified in the referenced Airbus documents; applicability read from the AD teaser — confirm exact model/serial from the records
Whether AD 84-02-04 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
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.