Airworthiness Directive 81-15-51 R1
one-timeAirworthiness Directives; ROCKWELL Models NA-265-60 and NA-265-80 Airplanes
Which aircraft AD 81-15-51 R1 applies to
Applies to NA-265-60 airplanes modified per STC SA687NW and equipped with Lear Siegler Flap Actuation System, and NA-265-80 airplanes modified per STC SA847NW; to prevent improper flap motion from flap actuation system failure.
Whether AD 81-15-51 R1 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.