N6682D1964 Boeing-Vertol 107-II
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply18 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Columbia Helicopters INC
- Owner type
- Corporation
- City, state
- Aurora, OR
- Certificate issued
- Aug 19, 2010
- Expires
- Jan 31, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jun 3, 2011
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
- 1964
- Serial number
- 101
- 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
- A8D493
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- 2010 – 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 (CT58-140-2) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (18)
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.
- Nacelles and pylons · stringer · corrodedApr 10, 2026
DURING THE CORROSION INSPECTION OF THE AFT PYLON, FOUND CORROSION IN TWO PLACES ON STRINGER P/N 107S8319-16 AT APPROXIMATELY WL-0 ST-418 AND 465. STRINGER WILL BE REMOVED AND REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support fitting · corrodedFeb 17, 2020
DURING THE NIGHT'S RAMP INSPECTION, FOUND INTERGRANULAR CORROSION ON THE STATION 410 R/H SUPPORT FITTING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · wire · chafedSep 27, 2017
#1 ENGINE F I RE WARNING LIGHT ILLUMINATED, BUT NO F I RE WAS PRESENT. AC RET U RNED T O BASE AT BAF. CHANGED #1 AFT L OWER F I RE EYE FOR C HAFED WI RE .SUPPLEMENTAL INFORMATION; THE DETECTORS IN THIS A/C HAVE BEEN REPLACED WITH P/N 477223 FLAME DETECTORS IAW COLUMBIA HELICOPTERS, INC. SERVICE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fire protection · wire · nickedOct 9, 2016
FIRE DETECTION WARNING LIGHT ILLUMINATED DURING FLIGHT. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND SUSPECTED FAULTY SPLICES. NO FURTHER REOCCURRENCES HAVE BEEN REPORTED. FAULTY PORTIONS OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · wire · nickedOct 8, 2016
NR 1 ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT (FALSE ACTIVATION). INSPECTED SYSTEM. NO FAULTS FOUND. REPLACED FWD UPPER & LOWER DETECTORS FOR TROUBLESHOOTING. AIRCRAFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · wire · nickedOct 7, 2016
NR 1 ENGING FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. INSPECTED SYSTEM. NO FAULTS FOUND. REPLACED BOTH AFT UPPER & LOWER FIRE DETECTORS. SYSTEM TESTED. AIRCRAFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · wire · nickedOct 6, 2016
DURING CRUISE FLIGHT, THE NR 1 ENGINE FIRE DETECTION LIGHT FALSE ACTIVATED. SYSTEM INSPECTED. NO FAULTS FOUND. CHANGED THE SYSTEM AMPLIFIER FOR TROUBLESHOOTING. ACFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · wire · nickedOct 3, 2016
NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. FALSE FIRE WARNING. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND SUSPECTED FAULTY SPLICES. NO FURTHER REOCCURRENCES HAVE BEEN REPORTED. SUPPLEMENTAL INFORMATION; THE DETECTORS IN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuel · transmitter · false indicationSep 23, 2016
NR 2 FUEL PRESSURE READING FLUCTUATES AT SHUT DOWN. FOR TROUBLESHOOTING. INSTALLED 5 SEPERATE FUEL PRESSURE INDICATORS. THE FIRST INDICATOR INSTALLED P/N: SRD-3F S/N:30 SHOWED NO INDICATION OF WORKING. THE NEEDLES DID NOT MOVE. THE NEXT 4 INDICATORS ALL READ APPROXIMATLY 180 DEGREES OUT. THE ISSUE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · garlock seal · failedJun 6, 2016
DURING AN INSPECTION, MECHANIC REMOVED AFT TRANSMISSION LUBE FILTER AND NOTICED LARGE METALLIC CHIPS IN THE FILTER HOUSING AND ON THE FILTER PACKS. DISASSEMBLED FILTER AND FOUND MORE CHIPS. REMOVED BLOWER DRIVE SHAFT AND INPUT COVER ON THE TRANSMISSION TO DETERMINE WHETHER THE CHIPS CAME FROM THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 18 reports.
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