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Aircraft record

N245CH1983 Boeing-Vertol 234

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched6 service difficulty reports

Registration
Valid
expires Jul 31, 2028
Based in
Aurora, OR
owner city / state
Engine
AL5512 · 4075 hp
Lycoming
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Columbia Helicopters INC
Owner type
Corporation
City, state
Aurora, OR
Certificate issued
Jul 10, 2018
Expires
Jul 31, 2028
Airworthiness
Standard · Transport
Airworthiness date
Jul 18, 2018

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
Boeing-Vertol
Model
234
Year
1983
Serial number
MJ022
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
44
Engines
2
Max takeoff weight
20,000 and over lb
Type certificate data sheet
H9EA
Mode S code
A242CC

Engine

Make and model
Lycoming Al5512
Type
Turbo-shaft
Power
4075 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. 2018 – nowColumbia Helicopters INCAurora, OR · 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 (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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

Service Difficulty Reports (6)

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.

  • Main rotor · tie bar · crackedSep 17, 2020

    DURING DISASSEMBLY OF 234 FWD ROTOR HEAD ASSEMBLY P/N: 414R2001-18, S/N: A4-1425 ON SWO-060358-20, DISCOVERED GREEN TIE BAR ASSEMBLY HAS CRACK IN UPPER PLATE IN OUTER CIRCUMFERENCE OF OUTBOARD LUG AREA.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Rotor flight controls · beam · crackedMar 12, 2018

    AFT ROTOR HEAD WAS IN SHOP FOR A SCHEDULED CENTER ROTOR HUB REPLACEMENT. DURING DISASSEMBLY, HORIZONTAL PIN LOCKING BEAM FOUND TO BE CRACKED. RESEARCH REVEALS THE CRACKED LOCKING BEAM TO BE AN OUTLIER. REPLACED AND COMPONENT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · strap · crackedMay 13, 2015

    STRAP WAS FOUND BOWED AND HAD NINE BROKEN PLATES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Airborne auxiliary power · nut · crackedJul 26, 2013

    APU WAS REMOVED FROM ACFT FOR REPORTED "LOUD SCREECHING" AND OIL LEAKING FROM INLET. ONCE INLET HOUSING WAS SEPARATED FROM REDUCTION DRIVE HOUSING IT WAS NOTED THAT THE OIL SLINGER NUT WAS BROKEN & CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · connector · damagedJun 9, 2001

    DURING A CLIMB, CRUISE SITUATION, THE NR 1 ENGINE N2 SYSTEM, BEGAN TO OSCILLATE TOWARDS THE HIGH SIDE. THE NR 1 ENGINE WAS BROUGHT BACK TO GROUND POSITION AND THE HELICOPTER WAS RETURNED TO THE SERVICE LANDING. TROUBLESHOOTING FOUND A FAULTY CANNON PLUG ATTACHED TO THE NR 1 N2 ACTUATOR. THE CANNON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · harness · corrodedApr 23, 2001

    AT TAKEOFF AND INTO CRUISE FLIGHT, THE NR 2 ENGINE BEGAN OSCILLATING AND GOING TO HIGH SIDE. THE NR 2 ENGINE WAS BROUGHT BACK TO THE GROUND POSITION AND HELICOPTER WAS RETURNED TO THE SERVICE LANDING. TROUBLESHOOTING REVEALED CORROSION/ RESISTANCE IN THE NR 2 ENGINE, NR 2 DECK CANNON PLUG 103P17.…

    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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