Airworthiness Directive 74-25-01

one-time
AD 74-25-01 · 1974-01-01 · turboshaft engine

Airworthiness Directives; REGULATORY TEXT: 74-25-01 GENERAL ELECTRIC COMPANY: Amendment 39-2009. Applies to General Electric Company CT58-140 engine fuel sy

Which aircraft AD 74-25-01 applies to

MakesGeneral Electric
ModelsCT58-140, CT58
Part-conditional3007T22P02.

applicability read from the AD teaser — confirm exact model/serial from the records Specific hose serial numbers are also called out for one dated production batch — confirm exact serial match from the full AD text before use.

Whether AD 74-25-01 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 74-25-01 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.