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Aircraft record

N2452CPiper PA-38-112

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jul 10, 2020.

Safety record in brief:1 NTSB accident (destroyed damage, Feb 2017)1 AD may apply1 service difficulty report

Registration
Deregistered
Last based in
Hartford, CT
owner city / state
Owners
1
since 2014
NTSB events
1
destroyed, 2017
ADs may apply
1
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
International Aviation LLC
Owner type
LLC
City, state
Hartford, CT
Certificate issued
Mar 13, 2014
Canceled
Jul 10, 2020
Airworthiness
Standard · Normal, Utility
Airworthiness date
Nov 13, 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-38-112
Serial number
38-79A0192
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A24533

Engine

Make and model
Lycoming 0-235 Series
Type
4 Cycle
Power
115 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. 2014 – 2020International Aviation LLCHartford, CT
  2. 1955 – 1956Rosario Exploration CoGrand Junction, CO · different airframe: Cessna 180 S/N 30752

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 (1)

Accident · destroyed

Feb 22, 2017 · East Haven, CT

The failure of the fuel selector valve in a position that restricted fuel flow to the engine, resulting in a total loss of engine power during initial climb due to fuel starvation. Also causal was the operator's failure to effectively detect and resolve the wear and progressive binding of the fuel selector valve before it failed due to excessive rotational force being applied. Contributing was…

Damage
Destroyed
Injuries
Fatal
Report
ERA17FA112

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA17FA112)

Accident history for this model

ADs published since 1998 that may apply (1)

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
98-03-16The New Piper Aircraft Corporation Model PA-38-112 AirplanesMar 16, 1998Airframe (PA-38-112)Certain serial numbers: PA-38-112 38-80A0166–38-82A0122

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

Service Difficulty Reports (1)

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 · rotor · wornFeb 5, 2018

    WORN ROTOR ULTIMATELY FAILED DURING FLIGHT, RESULTING IN A FATAL ACCIDENT. THE PILOT LIKELY HAD TO APPLY EXCESSIVE FORCE TO SWITCH FUEL TANKS WITH THE WORN ROTOR.

    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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