Airworthiness Directive 85-25-56 R1
one-timeAD 85-25-56 R1 · 1985-01-01 · turbine engine
Airworthiness Directives; SUBJECT HEADING: GENERAL ELECTRIC COMPANY Models CF6-50 and -45 Series Engines ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFO
Which aircraft AD 85-25-56 R1 applies to
MakesSubject Heading General Electric
ModelsCF6-50
Whether AD 85-25-56 R1 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 85-25-56 R1 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.
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.