Airworthiness Directive 87-08-07

one-time
AD 87-08-07 · 1987-01-01 · appliance

Airworthiness Directives; equipped with Goodyear main landing gear wheel assemblies, Part Number 5007897. Compliance required as indicated, unless previousl

Which aircraft AD 87-08-07 applies to

ModelsDC-9-81, DC-9-82, DC-9-83, DC-9
Part-conditional5007897, 5007897-1.

Applies to McDonnell Douglas DC-9-81, -82, and -83 airplanes equipped with Goodyear main landing gear wheel assemblies P/N 5007897; repetitive crack inspection, replace before further flight if cracked; replacement with P/N 5007897-1 is terminating action.

Whether AD 87-08-07 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 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 87-08-07 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.

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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.