Airworthiness Directive 65-03-03
one-timeAirworthiness Directives; operating limitation to the airplane flight manual: Do not exceed 2,100 r.p.m. engine speed when demonstrating or practicing power
Which aircraft AD 65-03-03 applies to
Add AFM operating limitation: do not exceed 2,100 rpm during power-on stalls; inspect crankshaft flange per Lycoming SB No. 300A before further flight after any acrobatic/spin flight or rpm-limit exceedance; if cracks found in the flange, remove engine.
Whether AD 65-03-03 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.