Airworthiness Directive 84-23-04
one-timeAirworthiness Directives; bulletin. C. To eliminate leakage from the fluid dampers in the main and nose landing gear actuating rams, within 180 days after t
Which aircraft AD 84-23-04 applies to
Main/nose landing gear actuating ram fluid damper leakage per Service Bulletin F27/28-55 (applicability read from the AD teaser — confirm exact model/serial from the records.)
Whether AD 84-23-04 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.