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Aircraft record

N54MV1976 Piper PA-23-250

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply3 service difficulty reports

Registration
Valid
expires May 31, 2032
Based in
Santa Rosa, CA
owner city / state
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
8
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Neil Anthony Foster Holdings LLC
Owner type
LLC
City, state
Santa Rosa, CA
Certificate issued
May 1, 2025
Expires
May 31, 2032
Airworthiness
Standard · Normal
Airworthiness date
Jan 19, 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 data

Airframe

Manufacturer
Piper
Model
PA-23-250
Year
1976
Serial number
27-7654043
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
A6D6BA

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
  1. 2025 – nowNeil Anthony Foster Holdings LLCSanta Rosa, CA · 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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2021-25-11Horizontal Stabilizer StructureJan 25, 2022Airframe (PA-23-250)Certain serial numbers: PA-23-250 27-7654001–27-7954121
2017-15-05Air ConditioningAug 28, 2017Airframe (PA-23-250)
2009-13-06 R1Piper Aircraft, Inc. AirplanesNov 3, 2011Airframe (PA-23-250)Only with: Equipped with a baggage door in the fuselage nose section (nose baggage door).
2005-01-10The New Piper Aircraft, Inc. Models PA-23-235, PA-23-250, and PA-E23-250 AirplanesFeb 22, 2005Airframe (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.
2003-09-13the New Piper Aircraft, Inc. Models PA-23, PA-23-160, PA-23-235, PA-23-250, and…Jun 23, 2003Airframe (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 ADs
ADSubjectEffectiveApplies to
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (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 R1The New Piper Aircraft, Inc.; Models PA-23-235, PA-23-250, and PA-E23-250 AirplanesOct 22, 1998Airframe (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
98-04-27The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…Mar 13, 1998Airframe (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 (3)

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 · pump · failedApr 28, 2004

    FUEL LEAKING INTO MANIFOLD REFERENCE LINE. PILOT EXPERIENCED INFLIGHT ROUGH ENGINE WHEN AUXILIARY FUEL PUMP WAS TURNED ON. FUEL CONTINUED TO RUN ONTO THE GROUND AFTER ENGINE SHUTDOWN.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · pump · failedApr 28, 2004

    FUEL LEAKING INTO MANIFOLD REFERENCE LINE. PILOT EXPERIENCED INFLIGHT ROUGH ENGINE WHEN AUXILIARY FUEL PUMP TURNED ON. FUEL CONTINUED TO RUN ON GROUND AFTER ENGINE SHUTDOWN. PROBABLE CAUSE: MFG DEFECT: LEAKING DIAPHRAGM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · fuel cell · defectiveMay 18, 1995

    DURING ROUTINE PRE-FLIGHT, FUEL TANK SUMP TESTING AND WATER IN AMOUNTS OF 3 OUNCES OR MORE WOULD BE FOUND. FUEL CAP O-RINGS WERE INSPECTED AND FOUND SATISFACTORY. TOP OF FUEL CELL/ACCESS COVER WAS REMOVED ON LEFT INBOARD CELL. WATER IN THE AMOUNT OF 3 CUPS WAS FOUND TRAPPED IN WRINKLES AND AGAINST…

    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

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