Airworthiness Directive 75-05-05

one-time
AD 75-05-05 · 1975-01-01 · appliance

Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2

Which aircraft AD 75-05-05 applies to

ModelsDC-10-30, DC-10-30F, KC-10A, KDC-10, DC-10-40, DC-10-40F, DC-10
Part-conditional5000757-1, 5000757-2.

Applies to main wheel assemblies P/N 5000757-1 and -2, installed on DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40, and DC-10-40F aircraft. Defective bolts to be scrapped.

Whether AD 75-05-05 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 75-05-05 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.