- Registered owner
- Columbia Helicopters Inc
- Location
- Aurora, OR
- Owner type
- Corporation
- Serial number
- 5
- Year built
- 1962
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- June 8, 2007
- Certificate issued
- October 4, 2017
- Expires
- October 31, 2027
- Mode S code
- A8D145
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 35
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 2 |
|---|---|
| 1964 | 1 |
| 1966 | 2 |
| 1969 | 1 |
| 1970 | 1 |
| 1972 | 1 |
| 1974 | 2 |
| 1975 | 1 |
| 1976 | 3 |
| 1978 | 1 |
| 1980 | 3 |
| 1981 | 2 |
| 1983 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1991 | 1 |
| 1994 | 1 |
| 1997 | 2 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2008 | 1 |
| 2012 | 1 |
| 2015 | 1 |
| 2021 | 1 |
| 2023 | 1 |
| 2025 | 1 |
Airframe · Boeing-Vertol 107-II
AD 2025-07-01Air Data ComputerAD 2023-11-07Ground Proximity SystemAD 2012-14-10Main Rotor Mast/SwashplateInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N6675DMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing-Vertol 107-II aircraft
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CHIA201908254108Actuator · failedDURING 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 SSDR CHIA201907234035Fire Detector · defectiveDURING 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 SERSDR CHIA201907214031Detector · defectiveDURING 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 UPPSDR CHIR201804103241Clutch · failedDURING 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 ORIGINSDR CHIR11820183122Bearing · galledAFT ROTOR HUB WAS REMOVED. ON DISASSEMBLY IT WAS REVEALED THAT THE YELLOW LAG BEARING WAS GALLED.SDR CHIR0201801101105Angle · crackedWHILE PERFORMING A B3 INSPECTION, MAINTENANCE DISCOVERED A CRACK IN THE LT PYLON CAP ANGLE BS 410, WL -6,-10, AND -12. REPAIRED.SDR CHIR20161121001Fire Detector · defectiveFIRE 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 HASDR CHIA20111013002Skin · crackedUPON INSPECTION DISCOVERED CRACKED ANTENNA MOUNT DOUBLER & SKIN.
STCs that may be installed · 40
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Boeing-Vertol 107-II
STC SH3319NMInstallation of Precise Flight Pulselite Control Unit in the
Landing /Taxi Recognition Visual Control Light system,STC SH1040NWInstallation of Navigation & Communication System.STC SR00925DEInstallation of Garmin GTX 335/335R and GTX345/345R transponders to provide ADS-B Out and In functionality