Airworthiness Directive 76-22-05
one-timeAD 76-22-05 · 1976-01-01 · airframe
Airworthiness Directives; approved by the Chief, Aircraft Engineering Division, Federal Aviation Administration, Western Region. This amendment becomes effe
Which aircraft AD 76-22-05 applies to
MakesThe Boeing CompanyMcdonnell Douglas Corporation
ModelsDC-10-10, DC-10-10F, DC-10-30, DC-10-30F, KC-10A, KDC-10, DC-10-40, DC-10
Whether AD 76-22-05 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 76-22-05 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.
Look up a tail number →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.