Airworthiness Directive 63-13-03
one-timeAirworthiness Directives; tolerance of + 1/2 degree is permissible) from each of the other blades, inspections in accordance with (e) shall be accomplished
Which aircraft AD 63-13-03 applies to
Blade tracking inspection (tolerance of +/- 1/2 degree from other blades) required before further flight regardless of total propeller time in service; remove cracked blades from service before further flight; shot-peen the blade shank per Hartzell Overhaul Manual No. 114 and Hartzell Service Bulletin No. 83. Specific propeller model not stated in excerpt.
Whether AD 63-13-03 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.