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
PA-23-250
Year
1974
Serial number
27-7554025
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A6E235
Engine
Make and model
Lycoming Ti0-540 Ser
Type
Reciprocating
Power
310 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2003 – 2007Headwind Aviation LLCOshkosh, WI
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Feb 23, 1998 · Peoria, IL
an improper preflight inspection of the airplane by the pilot and the inadvertant stall/mush which was encountered. A factor associated with this accident was the pilot's decision to continue to use the emergency hydraulic hand pump rather than the CO2 bottle to extend the landing gear which resulted in the landing gear not fully extending.
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.
The New Piper Aircraft, Inc. Models PA-23-235, PA-23-250, and PA-E23-250 Airplanes
Feb 22, 2005
Airframe (PA-23-250)Only with: Equipped with Garrett (formerly AiResearch) turbosuperchargers installed under STC SA852WE, SA909WE, or SA978WE, or under Piper Aircraft Drawing Number 32016.
the New Piper Aircraft, Inc. Models PA-23, PA-23-160, PA-23-235, PA-23-250, and…
Jun 23, 2003
Airframe (PA-23-250)Certain serial numbers: PA-23 23-1–23-2046; PA-23-160 23-1–23-2046; PA-23-235 27-505–27-622; PA-23-250 27-1–27-504; PA-23-250 27-2000–27-8154030; PA-E23-250 27-2505–27-4916; …. Only with: Applies only to airplanes that do not incorporate P/N 17634-002 flap control torque tube or P/N 104622-002 or 104622-004 flap control torque tube assembly.
ENGINE WAS DISASSEMBLED AND INSPECTED DUE TO CRANKSHAFT FAILURE. FOUND NR3 CHEEK BROKEN. THIS FAILURE CAUSED EXCESSIVE DAMAGE TO THE CRANKCASE, CAMSHAFT, NR1 AND NR 2 CONNECTING ROD, AND THE ASSOCIATED TAPPET BODIES. CAUSE OF THE FAILURE COULD POSSIBLY BE A METALLURGIC DEFECT OR A FORM OF FATIGUE.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · switch · out of adjustJan 24, 1996
PILOT COULD NOT GET DOWN AND LOCKED INDICATION OF THE NOSE GEAR. UPON SUCCESSFUL LANDING (GEAR WAS, IN FACT, DOWN AND LOCKED), IT WAS NOTED THE SWITCH AND BRACKET ASSEMBLY WERE NOT MAKING CONTACT. SWITCH IS ADJUSTABLE AND SUBMITTER SUGGESTS CAREFUL INSPECTION BE MADE AT SCHEDULED INSPECTIONS TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.