Airworthiness Directive 2000-25-06

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Official AD 2000-25-06 · FR doc 00-31537 · 2000-12-14 · turbine engine

Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines.

What this AD requires

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Pratt & Whitney (PW) PW4000 turbofan engines with the current design low pressure turbine (LPT) 4th stage air seal installed. This action requires, based on engine model, replacement of the current design seal with a new design seal, or with a modified seal. This amendment is prompted by reports of cracks in LPT 4th stage air seals. The actions specified by this AD are intended to reduce stresses that could lead to LPT 4th stage air seal cracking, resulting in seal fracture, uncontained engine failure, and damage to the airplane.

Which aircraft AD 2000-25-06 applies to

MakesPratt & Whitney
ModelsPW4052, PW4056, PW4060, PW4060A, PW4062, PW4152, PW4156, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, PW4462, PW4000
Part-conditional50N478, 50N478-001.

Applies only to engines with low pressure turbine (LPT) 4th stage air seal P/N 50N478 or P/N 50N478-001 installed. Installed on but not limited to Boeing 747, 767, McDonnell Douglas MD-11, Airbus A300, A310, and A330 series airplanes.

Whether AD 2000-25-06 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 2000-25-06 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 →Read the full directive (Federal Register)

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.