N191CH1962 Boeing V-Columbia Helicopters 107-II
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Columbia Helicopters INC
- Owner type
- Corporation
- City, state
- Aurora, OR
- Certificate issued
- Apr 17, 2015
- Expires
- Apr 30, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 18, 2009
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 dataAirframe
- Manufacturer
- Boeing V-Columbia Helicopters
- Model
- 107-II
- Year
- 1962
- Serial number
- 2003
- 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
- A16C1C
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, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2001-18-06 | 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.
- Main rotor · sprag clutch · brokenJun 25, 2013
ON STARTUP, AFTER ADVANCING THE ENGINES TO FLIGHT IDLE, DISCOVERED THAT NR 2 ENGINE NF WAS HIGHER THAN NR AND NR 2 ENGINE TORQUE WAS CLOSE TO 0 PERCENT. WHEN NR 1 ENGINE WAS RETARDED TO GROUND IDLE, WITH NR 2 ENGINE STILL AT FLIGHT IDLE, NR DROPPED AND NR 2 ENGINE WOULD NOT TAKE THE LOAD. SUSPECT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · piston · brokenJul 12, 2010
CAME TO A HOVER ABOVE THE HOOKER, AT THAT TIME WE FELT A LIGHT TO MODERATE LATERAL SHUFFLE. NO UNUSUAL NOISE. NOT KNOWING WHAT WAS CAUSING THE SHUFFLE, WE CHECKED THE SAS SYS, SINGLE, BOTH AND NO SAS WITH NO CHANGE IN THE SHUFFLE. PILOT APPLIED POWER AND IT GOT SLIGHTLY WORSE AND DECREASED POWER…
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