Airworthiness Directive 67-26-01
one-timeAirworthiness 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
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:
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.