Airworthiness Directive 69-17-02
one-timeAirworthiness Directives; c. Remove and replace lever assemblies that have improper staked control bearings before further flight. This amendment becomes ef
Which aircraft AD 69-17-02 applies to
Remove and replace lever assemblies that have improperly staked control bearings before further flight, or comply by a method approved by the Chief, Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, FAA; amendment effective August 19, 1969. Source text footer references Bell.
Whether AD 69-17-02 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.