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
107-II
Year
1962
Serial number
2002
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
20
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
1H16
Mode S code
A16865
Engine
Make and model
Ge Ct58-140-2
Type
Turbo-shaft
Power
1400 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2015 – 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 (1)
Accident · destroyed
Aug 20, 1983 · Shaver Lake, CA
THE ONLY WITNESS, THE HOOKER, WHO GETS LOGS READY FOR TRANSPORT BY THE HELICOPTER, STATED THAT HE HEARD NOISES AND THE ROTOR BLADES BEGAN COMING APART AS THE ACFT STARTED DOWNHILL WITH A LOG. EXAMINATION OF THE WRECKAGE REVEALED THAT #3 SYCHRONIZING SHAFT (BOEING P/N 10703141-13) HAD FAILED A FATIGUE CRACK ORIGINATING AT A RIVET HOLE. THE TOTAL TIME ON THE SHAFT WAS 17492 HOURS WITH 435 HOURS…
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.
General Electric Company T58 and CT58 Series Turboshaft Engines
Oct 18, 2001
Engine (CT58-140-2)
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
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.
Engine · engine · shutdownJun 22, 2026
DURING CRUISE FLIGHT, STRAIGHT AND LEVEL, ACFT SHUTTERED BRIEFLY THEN IN PILOTS HEADSETS HEARD AN AUDIBLE ENGINE OVER-TEMP ALARM. NG AND ENGINE OIL PRESSURE ON THE NR 1 ENGINE WERE AT ZERO AND PILOTS CONDUCTED SINGLE ENG FAILURE PROCEDURE. AFTER DEALING WITH THE ENG FAILURE & WE WERE ESTABLISHED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine · engine · inoperativeAug 13, 2013
PILOTS REPORTED THAT DURING A DESCENT, NR 1 ENGINE TORQUE WAS AT 25 PERCENT AND NR 2 ENGINE TORQUE WAS AT 7 PERCENT. PULLED IN POWER TO INCREASE TORQUE ON THE NR 2 ENGINE. DURING PULL IN OF POWER, NR 2 ENGINE TORQUE DECREASED TO 1 PERCENT MOMENTARILY PRIOR TO MATCHING UP ALL PARAMETERS (TORQUE…
From FAA Service Difficulty Reports; matched by N-number and serial number.