N27CY1976 Piper PA-23-250
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply4 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Individual owner
- City, state
- Hastings, FL
- Airworthiness
- Standard · Normal
- Airworthiness date
- May 7, 1976
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
- Year
- 1976
- Serial number
- 27-7654118
- 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
- A2A46C
Engine
- Make and model
- Lycoming Io-540 Ser
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until nowIndividual ownerHastings, FL · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (10)
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). |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (IO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 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. |
Show all 10 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
| 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. |
| 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 (4)
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.
- Flight controls · tube · crackedMay 7, 1999
DURING INSPECTION PER AD 78-02-03, FOUND LEFT TUBE AND WT ASSY CRACKED THROUGH APPROXIMATELY 1.50 INCHES FORWARD OF TUBE ATTACHMENT PLATE. SUBMITTER STATED THIS IS THE FOURTH ONE IN PAST YEAR, ALL WERE MODIFIED PER SB 540A.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · balance weight · crackedJan 12, 1999
DURING 100-HOUR INSPECTION OF BALANCE WEIGHTS AND ARMS PER AD 78-02-03, FOUND BOTH ARMS CRACKED. REPLACED BOTH WITH SERVICEABLE PARTS. CAUSE UNKNOWN, POSSIBLE THAT ICE ACCUMULATION ON STABLIZER CAUSED SLIGHT FLUTTER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · hinge · wornOct 9, 1998
REMOVED TRIM TAB DUE TO WORN HINGE. INSPECTION FOUND HORN ASSY P/N 28372-02 LOOSE AND SKINS AROUND ATTACHMENT AREA CRACKED. SUBMITTER STATED LEFT UNREPAIRED COULD POSSIBLY SEPARATE IN-FLIGHT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Electrical power · alternator · failedAug 21, 1996
PILOT REPORTED LT ALTERNATOR LIGHT FLICKERED DURING TURBULENCE. LIGHT CAME ON STEADY ON THE WAY TO MAINTENANCE. REMOVED ALTERNATOR, HEARD SOMETHING RATTLING INSIDE. REMOVED COOLING SHROUD AND FOUND ONE BRUSH INSIDE. REMOVED BRUSH BLOCK AND FOUND A PIECE OF IT AROUND THE BRUSH HAD BROKEN AWAY.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026