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Airworthiness Directive 82-23-03 R1

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AD 82-23-03 R1 · 1982-01-01 · turbine engine

Airworthiness Directives; International Inc. TFE731-2 TFE731-2A TFE731-2B TFE731-2BR TFE731-2C TFE731-3 TFE731-3A TFE731-3AR TFE731-3B TFE731-3BR TFE731-3C

Which aircraft AD 82-23-03 R1 applies to

MakesGarrett Turbine Engine CompanyHoneywell International Inc.
ModelsTFE731-2, TFE731-2A, TFE731-2B, TFE731-2BR, TFE731-2C, TFE731-3, TFE731-3A, TFE731-3AR, TFE731-3B, TFE731-3BR, TFE731-3C, TFE731-3CR, TFE731-3D, TFE731-3DR, TFE731-3R, TFE731

Garrett Turbine Engine Company Model TFE731-2, -3, -3R, -3A, -3AR, -3B and -3BR series turbofan engines (footer lists Honeywell International Inc. as current holder of the TFE731 model line). To prevent failure of the high-pressure compressor [rotor, text truncated]; compliance required as indicated unless already accomplished. Effective December 9, 1983.

Whether AD 82-23-03 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 82-23-03 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.

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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.