Airworthiness Directive 67-26-01

one-time
AD 67-26-01 · 1967-01-01 · appliance

Airworthiness Directives; indicate that the yaw damper is deactivated (c) Adjust and modify the yaw-damper control as follows: (1) Adjust the yaw-damper act

Which aircraft AD 67-26-01 applies to

MakesBoulton Paul
ModelsBAC 1-11
Part-conditionalP185-45-10.

Adjust/modify yaw-damper actuator (Boulton Paul P/N P185-45-10) per Boulton Paul Modification Nos. P185/11 or P185/15, in accordance with BAC 1-11 Service Bulletin No. 27-PM 3191 or later ARB-approved issue, on BAC One-Eleven airplanes.

Whether AD 67-26-01 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 67-26-01 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.