Airworthiness Directive 67-28-05

one-time
AD 67-28-05 · 1967-01-01 · turbine engine

Airworthiness Directives; ) For the purposes of this AD, the number of cycles equals the number of landings (including touch- and-go landings). (d) Upon sub

Which aircraft AD 67-28-05 applies to

MakesPratt & Whitney
ModelsJT3D-1, JT3D-1-MC6, JT3D-1-MC7, JT3D-3, JT3D-3B, JT3D

For purposes of this AD, the number of cycles equals the number of landings (including touch-and-go landings). Upon submission of substantiating data through an FAA maintenance inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may approve an alternate method of compliance. Effective October 24, 1967.

Whether AD 67-28-05 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 67-28-05 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.