Airworthiness Directive 80-18-51
one-timeAirworthiness Directives; and possible fire, accomplish the following: Prior to further flight, unless already accomplished within the last 50 hours time in
Which aircraft AD 80-18-51 applies to
Inspect electrical wires and hydraulic lines between fuselage stations 5295 and 5600 for chafing (fire risk); unless already done within the last 50 hours TIS, replace any chafed wires/lines before further flight; report defects to FAA AEU-100 (Europe, Africa, Middle East).
Whether AD 80-18-51 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.