Airworthiness Directive 80-18-51

one-time
AD 80-18-51 · 1980-01-01 · airframe

Airworthiness 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

ModelsSA-330

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:

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 80-18-51 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.