Airworthiness Directive 51-14-01
one-timeAirworthiness Directives; pump (identified by either a 1/8 inch red band around the pump body, or the suffix "H" in the pump serial number, in series with a
Which aircraft AD 51-14-01 applies to
Thompson TF-1100 engine-driven fuel pump identified by a 1/8 inch red band around the pump body or suffix 'H' in the pump serial number (or '2'/'M2' stamped after TF-1100 on nameplate), installed in accordance with Beech Installation Instructions (revised); aircraft model not stated in available text.
Whether AD 51-14-01 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.