Airworthiness Directive 60-26-05

one-time
AD 60-26-05 · 1960-01-01 · airframe

Airworthiness Directives; 829912, at airplane center line for evidence of free play as follows: with elevator blocked at extreme down position apply up and

Which aircraft AD 60-26-05 applies to

Part-conditional827020-1, 813612-1, 840404-1.

Compliance is gated to inspection/replacement of the specific Lockheed elevator control part numbers noted in the teaser — confirm applicable model from the full AD text before use.

Whether AD 60-26-05 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 60-26-05 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.