Airworthiness Directive 02-22759

one-time
AD 02-22759 · 2002-09-09 · turbine engine

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

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2002-17-02 applicable to Pratt & Whitney JT8D series turbofan engines that was published in the Federal Register on August 28, 2002 (67 FR 55108). The first sentence in the amendatory language that states "2. Section 39.13 is amended by removing Amendment 39-11940 (65 FR 65731, November 2, 2000) and by adding a new airworthiness directive to read as follows:" is incorrect. This document corrects that sentence. In all other respects, the original document remains the same.

Which aircraft AD 02-22759 applies to

MakesPratt & Whitney Jt8D

Whether AD 02-22759 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 02-22759 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.