N6675D1962 Boeing-Vertol 107-II
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply8 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Columbia Helicopters INC
- Owner type
- Corporation
- City, state
- Aurora, OR
- Certificate issued
- Oct 4, 2017
- Expires
- Oct 31, 2027
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jun 8, 2007
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-Vertol
- Model
- 107-II
- Year
- 1962
- Serial number
- 5
- 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
- A8D145
Engine
- Make and model
- Ge Ct58-140-1
- 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- 2017 – 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.
Accident history for this modelADs published since 1998 that may apply (3)
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 |
|---|---|---|---|
| 2012-14-10 | Boeing Vertol (Type Certificate Currently Held by Columbia Helicopters, Inc. (CHI)) and… | Aug 7, 2012 | Airframe (107-II)Only with: Upper collective pitch control assembly P/N 107CK003-2 or 107CK002-2 installed. |
| 2005-24-05 | Boeing Vertol Model 107-II Helicopters | Dec 8, 2005 | Airframe (107-II)Only with: With quill shaft P/N 107D2067 (all dash numbers) and spiral bevel pinion gear P/N 107D2215 installed. |
| 2001-18-06 | General Electric Company T58 and CT58 Series Turboshaft Engines | Oct 18, 2001 | Engine (CT58-140-1) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (8)
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 controls · actuator · failedAug 25, 2019
DURING TAKEOFF, THE NR 1 ENGINE FREEZE FAILED, PILOT RESET IT AND SUBSEQUENTLY, THE ENGINE FAILED TO ACCELERATE PAST FLIGHT IDLE. AIRCRAFT RETURNED TO BASE. REMOVED AND REPLACED THE #1 ENGINE ECA. COMPLIED WITH POST MAINTENANCE GROUND, HOVER AND FLIGHT LOGIC SETUP. ALL OPERATIONAL CHECKS ARE GOOD.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire detector · defectiveJul 23, 2019
DURING CRUISE FLIGHT PILOTS NOTICED #1 T-HANDLE FLICKERING, VERIFIED IT WAS A FALSE INDICATION AND DID NOT NEED TO UTILIZE ANY EMERGENCY PROCEDURES. FIRE LIGHT THEN EXTINGUISHED WITHIN 30 SECONDS. RAR AFT LOWER OUTBOARD FLAME DETECTOR. AIRCRAFT RETURNED TO SERVICE. SUPPLEMENTAL INFORMATION; THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · detector · defectiveJul 21, 2019
DURING CRUISE FLIGHT PILOTS NOTICED #1 T-HANDLE FLICKERING, VERIFIED IT WAS A FALSE INDICATION AND DID NOT NEED TO UTILIZE ANY EMERGENCY PROCEDURES. FIRE LIGHT THEN EXTINGUISHED WITHIN 30 SECONDS. AIRCRAFT RETURNED TO AIRFIELD FOR A SCHEDULED STOP. RAR AFT UPPER INBOARD FLAME DETECTOR. AIRCRAFT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reportsShow fewer reports
- Main rotor drive · clutch · failedApr 3, 2018
DURING EVENING SHUTDOWN PRIOR TO SCHEDULED REMOVAL OF AFT XMSN(DUE FOR QUILL SHAFT INSPECTION) PILOT NOTICED THE NR DID NOT DROP LIKE NORMAL. GROUND MAINTENANCE VISUALLY SAW THE NR 2 ENG/MIX BOX WAS NOT DISCONNECTING IN A NORMAL MANNER. R&R AFT XMSN PER ORIGINALLY SCHEDULED MAINTENANCE ACTIVITY.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bearing · galledJan 18, 2018
AFT ROTOR HUB WAS REMOVED. ON DISASSEMBLY IT WAS REVEALED THAT THE YELLOW LAG BEARING WAS GALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedJan 5, 2018
WHILE PERFORMING A B3 INSPECTION, MAINTENANCE DISCOVERED A CRACK IN THE LT PYLON CAP ANGLE BS 410, WL -6,-10, AND -12. REPAIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire detector · defectiveNov 21, 2016
FIRE DETECTION WARNING LIGHT ILLUMINATED DURING FLIGHT (FLIGHT ILLUMINATION). THERE HAVE BEEN SEVERAL PREVIOUS OCCURRENCES (SEE SUBMITTED SDR'S). THE NR 2 AFT, INBOARD, FIRE DETECTOR WAS REPLACED AND DOCUMENTED ON LC-000973-75-16, DISC-000619-75-16. THERE HAVE BEEN NO FURTHER OCCURRENCES.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedOct 13, 2011
UPON INSPECTION DISCOVERED CRACKED ANTENNA MOUNT DOUBLER & SKIN.
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