Airworthiness Directive 87-15-04

one-time
AD 87-15-04 · 1987-01-01 · propeller

Airworthiness Directives; change rod failure which could result in loss of propeller control, accomplish the following: Replace the spring assembly, P/N B-8

Which aircraft AD 87-15-04 applies to

Part-conditionalB-831-54, B-831-64.

applicability gated to Hartzell propellers equipped with pitch-change spring assembly P/N B-831-54; confirm exact model/serial from the records

Whether AD 87-15-04 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 87-15-04 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.