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
1962
Serial number
27-2264
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
A68FE6
Engine
Make and model
Lycoming 0-540 Series
Type
Reciprocating
Power
250 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2017 – nowGv Air INCMedford, OR · current
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 · substantial damage
Mar 29, 1987 · Dover, DE
THE ROCKWELL WAS IN LEVEL FLIGHT AT 2800 FT AND THE PIPER WAS CLIMBING WHEN MIDAIR COLLISION OCCURRED. NEITHER ACFT WAS OPERATING UNDER ATC. NEITHER PLT SAW THE OTR AIRCRAFT BEFORE THE COLLISION OCCURRED. THE BOTTOM OF THE ROCKWELL CABIN AND THE LEFT TIPTANK OF THE PIPER COLLIDED. THE COLLISION ANGLE BETWEEN THE ACFT WAS 60 DEGREES. THE ROCKWELL PILOT WAS ABLE TO PROCEED TO HIS INTENDED…
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.
STABILIZER TORQUE TUBE HOLES FOR STABILIZER MOUNT WERE FOUND ELONGATED. THIS WAS DISCOVERED WHILE INSPECTING THE LEFT STABILIZER FOR A CREAKING NOISE THAT WAS DISCOVERED DURING PRE-FLIGHT. THE ELONGATION OF THE HOLES ALLOWED MOVEMENT OF THE STABILIZER. THIS ACTION WORE THE ATTACHMENT BOLTS FOR THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.