We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Piper
Model
PA46-500TP
Year
2001
Serial number
4697100
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A6BEA9
Engine
Make and model
P&W Pt6a Ser
Type
Turbo-prop
Power
750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2001 – 2015Individual ownerFalmouth, ME
until 1989Individual ownerdifferent airframe: Beechcraft K35 S/N D5803
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · destroyed
Jun 13, 2014 · White Plains, NY
The pilot's failure to maintain a positive climb rate after takeoff due to spatial disorientation (somatogravic illusion). Contributing to the accident was the pilot's self-induced pressure to depart and his decision to depart in low-ceiling and low-visibility conditions.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Power plant · shield · chafedMar 16, 2005
DURING NORMAL EVENT INSPECTION, IT WAS FOUND THAT THE AIR SHIELD WAS CHAFFING AGAINST THE UPPER RT ENGINE MOUNT LEG WHERE IT PASSES THROUGH THE BAFFLE SHIELD FOR THE PLENUM ASSY. RECOMMENDED THAT CLOSE INSPECTION BE GIVEN TO AREA WHERE BAFFLING COULD BE CUTTING INTO THE ENGINE MOUNT. BOTH TIMES…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · bolt · corrodedOct 4, 2002
DURING A TIRE REPLACEMENT ON THE RT MAIN WHEEL ASSEMBLY, ALL WHEEL THRU BOLTS FOUND WORN AND CORRODED. THERE WAS NO TYPE OF ANTI-SEIZE LUBRICANT ON THE BOLTS. PIPER MAINTENANCE MANUAL DOES NOT REQUIRE ANY ANTI-SEIZE LUBRICAN ON THE THRU BOLTS.
From FAA Service Difficulty Reports; matched by N-number and serial number.