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Aircraft record

N2240D1978 Piper PA-34-200T

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply5 service difficulty reports

Registration
Valid
expires Nov 30, 2032
Based in
Spokane, WA
owner city / state
Engine
TSIO-360 SER · 225 hp
Cont Motor
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
7
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Individual owner
City, state
Spokane, WA
Certificate issued
Nov 25, 2025
Expires
Nov 30, 2032
Airworthiness
Standard · Normal
Airworthiness date
Nov 10, 1978

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-34-200T
Year
1978
Serial number
34-7970032
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
7
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A1F239

Engine

Make and model
Cont Motor Tsio-360 Ser
Type
Reciprocating
Power
225 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 – nowIndividual ownerSpokane, WA · current
  2. 1964 – 1974Individual ownerdifferent airframe: Cessna 170b S/N 20392

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (7)

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
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-34-200T)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-34-200T)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; …
2005-15-10The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T…Aug 26, 2005Airframe (PA-34-200T)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump.
2005-13-16The New Piper Aircraft, Inc. PA-34 Series AirplanesAug 8, 2005Airframe (PA-34-200T)
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-34-200T)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).
Show all 7 ADs
ADSubjectEffectiveApplies to
97-01-01 R1The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series…Dec 8, 1998Airframe (PA-34-200T)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies.
98-04-27The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…Mar 13, 1998Airframe (PA-34-200T)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (5)

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.

  • Fuel · fuel tank · leakingSep 4, 2013

    PILOT REPORTED FUEL LEAKING FROM UNDER RT WING DEICER BOOT. REMOVED BOOT AND FOUND CORROSION HAD EATEN THROUGH THE L/E OF BOTH TANKS BEHIND THE DEICER BOOT. PROBABLE THAT WATER WAS BEHIND THE BOOT AND CREATED THE PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · fuel tank · leakingSep 4, 2013

    PILOT REPORTED FUEL LEAKING FROM UNDER RT WING DEICER BOOT. REMOVED BOOT AND FOUND CORROSION HAD EATEN THROUGH THE L/E OF BOTH TANKS BEHIND THE DEICER BOOT. PROBABLE THAT WATER GOT BEHIND THE BOOT AND CREATED THE PROBLEM. ACFT SPENDS MOST WEEKENDS IN SALT AIR AND SALT WATER ENVIRONMENT, HELPED TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · adapter · failedJan 25, 2001

    90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM, APPARENTLY VIBRATION INDUCED. SOME PROVISIONS SHOULD BE MADE TO REINFORCE UNIT , OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Engine indicating · adapter · failedJan 23, 2001

    90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOULD BE MADE TO REINFORCE UNIT OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · adapter · failedJan 23, 2001

    90 DEGREE TACH ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEMS APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOULD BE MADE TO REINFORCE UNIT, OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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