N14268Piper PA-23-250
Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Individual owner
- City, state
- Whitwell, TN
- Certificate issued
- Jun 5, 2025
- Expires
- Jun 30, 2032
- Airworthiness
- Standard · Normal
- Airworthiness date
- May 1, 1972
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 dataAirframe
- Manufacturer
- Piper
- Model
- PA-23-250
- Serial number
- 27-4828
- 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
- A0AD69
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- 2025 – nowIndividual ownerWhitwell, TN · current
- 1944Pan American-Grace Airways INCNew York, NY · different airframe: Douglas Dc2 S/N 1301
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (8)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-25-11 | Horizontal Stabilizer Structure | Jan 25, 2022 | Airframe (PA-23-250)Certain serial numbers: PA-23-250 27-7654001–27-7954121 |
| 2017-15-05 | Air Conditioning | Aug 28, 2017 | Airframe (PA-23-250) |
| 2009-13-06 R1 | Piper Aircraft, Inc. Airplanes | Nov 3, 2011 | Airframe (PA-23-250)Only with: Equipped with a baggage door in the fuselage nose section (nose baggage door). |
| 2005-01-10 | 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. |
| 2003-09-13 | 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. |
Show all 8 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 99-05-09 | The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series Airplanes | Mar 19, 1999 | Airframe (PA-23-250)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-01–27-2504; PA-24-180 24-103–24-3687; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5028; …. Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2). |
| 83-22-01 R1 | The New Piper Aircraft, Inc.; Models PA-23-235, PA-23-250, and PA-E23-250 Airplanes | Oct 22, 1998 | Airframe (PA-23-250)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-1–on; PA-E23-250 27-2505–27-7554168; PA-E23-250 27-7654001–on |
| 98-04-27 | The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250… | Mar 13, 1998 | Airframe (PA-23-250) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
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.
- Engine fuel and control · manifold · looseJan 3, 2000
FOUND FUEL LINE FITTING ON FUEL INJECTOR LOSE CAUSING FUEL STARVATION TO FUEL MANIFOLD. TIGHTENED FITTING AND RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026