- Registered owner
- Columbia Helicopters Inc
- Location
- Aurora, OR
- Owner type
- Corporation
- Serial number
- 2002
- Year built
- 1962
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- July 5, 2012
- Certificate issued
- February 26, 2015
- Expires
- February 29, 2028
- Mode S code
- A16865
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 33
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 | 1 |
| 1969 | 1 |
| 1970 | 1 |
| 1972 | 1 |
| 1974 | 2 |
| 1975 | 1 |
| 1976 | 3 |
| 1978 | 1 |
| 1980 | 3 |
| 1981 | 2 |
| 1983 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20120809020429IChester, CAAccording to the pilot and copilot statements, during a dip for water there was some miscommunication between the crew that allowed the aircraft to get to close to a tree and the forward rotor blades contacted a tree. After returning to the airport,…Accident 19830820074729AHovering · Shaver Lake, CA#3SYN chronizing shaft failed on lifting a external load. Caused main rotors to collide. Rivet hole fatigue cracks.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CHIA2026062210939Engine · shutdownDURING 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 TSDR CHIR20131608001Engine · inoperativePILOTS 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
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