Airworthiness Directive 87-14-01 R1

one-time
AD 87-14-01 R1 · 1987-01-01 · turbine engine

Airworthiness Directives; effective on July 27, 1987. This amendment (39-6359, AD 87-14-01 R1) becomes effective on December 11, 1989. FOOTER: Pratt & Whitn

Which aircraft AD 87-14-01 R1 applies to

MakesPratt & Whitney Division
ModelsJT8D-1, JT8D-11, JT8D-15, JT8D-17, JT8D-1A, JT8D-1B, JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, JT8D

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 87-14-01 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 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 87-14-01 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.