Airworthiness Directive 02-19034

one-time
AD 02-19034 · 2002-07-26 · turbine engine

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

What this AD requires

This document makes corrections to Airworthiness Directive (AD) 2002-13-09 applicable to Pratt & Whitney JT8D-200 engines that was published in the Federal Register on July 3, 2002 (67 FR 44527). In the regulatory information, Table part B., Parts Requiring Inspection, one item under Description and one item under Engine Manual are incorrect. This document corrects these items. In all other respects, the original document remains the same.

Which aircraft AD 02-19034 applies to

MakesPratt & Whitney Jt8D-200

Whether AD 02-19034 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 02-19034 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.