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Aircraft record

N2190K1978 Piper PA-34-200T

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply10 service difficulty reports

Registration
Valid
expires Jul 31, 2029
Based in
Columbus, OH
owner city / state
Engine
TSIO-360 SER · 225 hp
Cont Motor
Owners
1
since 2016
NTSB events
None
since 1982
ADs may apply
7
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Individual owner
City, state
Columbus, OH
Certificate issued
Jul 12, 2016
Expires
Jul 31, 2029
Airworthiness
Standard

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
34-7970096
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
A1DD53

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. 2016 – nowIndividual ownerColumbus, OH · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (10)

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.

  • Equipment and furnishings · elt · malfunctionedDec 9, 2010

    (BIER) ELT REMOVED FOR INSP AND TESTING IAW CFR PART 91.207D. DURING BENCH TESTING OF ME-406 ELT, THE ELT WOULD NOT TURN OFF OR RESET. INTERNAL BATTERY HAD TO BE UNPLUGGED TO PREVENT ELT FROM REPEATED TRANSMITTION. ELT PN 453-6603, SN 14668 WAS SENT FOR NEEDED REPAIRS UNDER THEIR WO 34431, DATED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Equipment and furnishings · elt · failedSep 30, 2008

    ELT EMERGENCY LOCATOR TRANSMITTER WILL NOT TEST PROPERLY ON A CONSISTENT BASIS BY DISPLAYING CORRECT 3-DIGIT COUNTRY CODE OR 15 DIGIT HEX ID CODE. THIS ELT HAS BEEN TESTED WITH (2) DIFFERENT 406 MHZ TESTERS DISTRIBUTED BY PN 453-1000 AND PN 453-0131 (MEASURE MODEL MEZ 1000 AND PSION ORGANIZER II…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Equipment and furnishings · elt · no testSep 30, 2008

    ELT EMERGENCY LOCATOR TRANSMITTER WILL NOT TEST PROPERLY ON A CONSISTENT BASIS BY DISPLAYING CORRECT 3-DIGIT COUNTRY CODE OR 15 DIGIT HEX ID CODE. THIS ELT HAS BEEN TESTED WITH (2) DIFFERENT 406 MHZ TESTERS. DISTRIBUTED, PN 453-1000 AND 453-0131 AND THE PERFORMANCE OF THE 451 ELT HAS BEEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Landing gear · arm · wornJul 22, 2008

    NLG MOUNT ASSY ATTACHMENT POINT FOR STEERING ARM ASSY HAS EXCESSIVE WEAR AT LWR MOUNT HOLE, SRM DOES NOT SPECIFY AT FIX OR ALLOWABLE LIMIT FOR PN 95551-23. DISCREPANCY FOUND DURING INSP IAW SB 1123A & B AND ANNUAL INSPECTION IAW SRM INSPECTION GUIDE. SB 1123B GIVES THE SERVICE LIMITS TO THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · housing · brokenJun 29, 2004

    DURING SEARCH FOR OIL LEAK ONTO ALTERNATOR FOUND. OIL SCAVENGE PUMP HOUSING HAD BROKEN MOUNT LUG. REPLACED WITH NEW PART. CAUSE OF FAILURE BELIEVED TO BE WEAK CONSTRUCTION. AIRCRAFT FREON COMPRESSOR MOUNTS HERE. AIRCRAFT HAS HAD DYNAMIC PROP BALANCES. SECOND FAILURE THIS ENGINE WITHIN 400 HOURS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · torque tube · damagedDec 4, 2001

    WHILE INSPECTING RUDDER ON ANNUAL INSPECTION THE INSPECTOR FOUND LOOSENESS AT THE RUDDER TORQUE TUBE ATTACH BOLTS. TEARDOWN INSPECTION SHOWED BOLT HOLES OVERSIZE AND ELONGATED. NEW PARTS INSTALLED BECAUSE (AN 174) BOLTS WERE LARGEST SIZE BOLTS PERMITTED. MFG SB REFERS TO THIS PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · stop · damagedAug 27, 1998

    DURING AIRCRAFT INSPECTION, NOSE LANDING GEAR WAS FOUND BADLY DAMAGED DUE TO OVERSTEERING WHEN TOWING. PARTS HAD TO BE REPLACED. SUBMITTER SUGGESTED MFG INSTALL TOW LIMIT MARKING TO AID IN PREVENTING EXCEEDING TOW LIMITS. ALSO, FOUND P/ N 7853500 TILLER ARM BOLT AND ROLLER ASSY LOOSE. FOUND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine controls · valve · failedAug 27, 1998

    DURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTER STATED VALVES NEED TO BE OPS CHECKED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine controls · valve · failedAug 27, 1998

    DURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTER STATED VALVES NEED TO BE OPS CHECKED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · angle · corrodedAug 27, 1998

    WHILE C/W SB 977, CORROSION WAS FOUND ON TOP OF LEFT, AFT WING ATTACH AND LOWER CABIN DOOR POST ATTACH. SUSPECT WATER LEAKING IN AFT CABIN DOOR AT SOME PREVIOUS TIME. LEFT CABIN INTERIOR WAS REMOVED FOR AVIONICS INSTALL AND PROVIDED ACCESS FOR BETTER INSPECTION THAN CALLED OUT IN SB. IN THIS AREA…

    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

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