Airworthiness Directive 65-18-02
one-timeAirworthiness Directives; Instructions) of General Design Service Bulletin No. 12.0.2800, dated June 1965, or an equivalent approved by the Aircraft Enginee
Which aircraft AD 65-18-02 applies to
Turn and Bank Indicators; comply per General Design Service Bulletin No. 12.0.2800, dated June 1965, or an FAA-approved equivalent; effective August 17, 1965, revised October 30, 1965.
Whether AD 65-18-02 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.