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Airworthiness Directive 2000-21-07

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Official AD 2000-21-07 · FR doc 00-28090 · 2000-11-02 · turbine engine

Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2000-21-07 applicable to Pratt & Whitney JT8D-200 series turbofan engines that was published in the Federal Register on October 24, 2000 (65 FR 63540). The statement identifying AD 2000-21-07 as superseding AD 99-12-04, Amendment 39-11188 (64 FR 30382, dated June 8, 1999), was inadvertently omitted from the AD. This document corrects that statement. In all other respects, the original document remains the same.

Which aircraft AD 2000-21-07 applies to

MakesPratt & Whitney Jt8D-200

Whether AD 2000-21-07 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 2000-21-07 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.