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Aircraft record

N4490F1976 Piper PA-34-200T

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 8, 2022.

Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply8 service difficulty reports

Registration
Deregistered
Last based in
Rantoul, KS
owner city / state
Engine
TSIO-360 SER · 225 hp
Cont Motor
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
7
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Dodson International Parts INC
Owner type
Corporation
City, state
Rantoul, KS
Certificate issued
Sep 2, 2015
Canceled
Jan 8, 2022
Airworthiness
Standard · Normal
Airworthiness date
Aug 24, 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-34-200T
Year
1976
Serial number
34-7670339
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
A56E6A

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. 2015 – 2022Dodson International Parts INCRantoul, KS

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 (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 (8)

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.

  • Stabilizers · rivets · shearedJun 23, 1997

    RIVETS ON LT SIDE (3 OUT OF 4) SHEARED WHERE AFT SPAR OF VERTICAL STABILIZER ATTACHES TO EMPENNAGE. THESE RIVETS HAVE BEEN REPLACED BEFORE, BUT COULD NOT DETERMINE T.I.S. SINCE REPAIR. SUBMITTER STATED THIS IS THE SECOND PA-34-200T IN FLEET FOUND WITH SHEARED RIVETS IN THIS AREA.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · heater · crackedDec 23, 1996

    HEATER FAILED P.D.T. PER AD 96-20-07. BURNER CAN CRACKED. TSOH TRACKED VIA AIRCRAFT FLIGHT TIME = (2966 HRS) (DIVIDED BY 2) = 1483 HRS ON HEATER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • pump · seizedNov 20, 1996

    LEFT ENGINE PNEUMATIC PUMP SEIZED AND FAILED DURING PNEUMATIC DE-ICE OPERATION DURING IFR/ICING CONDITIONS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Flight controls · bracket · crackedJul 16, 1996

    INSPECTION FOUND FLAP LEVER BRACKET IS CRACKED AT BOTH FORWARD BEND RADIUS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · latch rod · wornMar 19, 1996

    FORWARD BAGGAGE DOOR AFT LATCH ROD IS WORN PARTIALLY THROUGH JUST BEHIND COTTER PIN HOLE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · latch rod · wornMar 19, 1996

    FORWARD BAGGAGE DOOR, FORWARD LATCH ROD IS PARTIALLY WORN THROUGH JUST BEHIND COTTER PIN HOLE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · torque tube · holes elongatedApr 23, 1995

    INSPECTION FOUND RUDDER TORQUE TUBE HOLES ARE ELONGATED WHERE TORQUE TUBE FITTING ATTACHES. NOTE: PART HAS 1584 HOURS ON IT SINCE STEEL FITTING WAS INSTALLED PER SB 899.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · wheel · crackedApr 9, 1995

    FOUR INCH CRACK FOUND IN CURVED SIDE OF NOSE WHEEL.

    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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