- Registered owner
- Columbia Helicopters Inc
- Location
- Aurora, OR
- Owner type
- Corporation
- Serial number
- 2003
- Year built
- 1962
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- February 18, 2009
- Certificate issued
- April 17, 2015
- Expires
- April 30, 2028
- Mode S code
- A16C1C
Boeing V-Columbia Helicopters 107-IITCDS 1H16Airframe · Boeing V-Columbia Helicopters 107-IITCDS 1E3Engine · GE CT58-140-2
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 V-Columbia Helicopters 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
No NTSB investigations matched to N191CHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing V-Columbia Helicopters 107-II aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CHIR201306250058Sprag Clutch · brokenON 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 ESDR CHIR07122010001Piston · brokenCAME 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 GSDR CHI2002F00002Link · crackedCREW CHIEF NOTIFIED OF A POSSIBLE CRACK ON THE FORWARD ROTOR HEAD GREEN GLADE EXTENSION LINK AT THE HORIZONTAL PIN LAG BORE 6 OCLOCK POSITION. UPON DISASSEMBLY OF THE ROTOR HEAD IT WAS CONFIRMED THAT THE EXTENSION LINK WAS CRACKED. THE CRACK EXTENDED APPROX.
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 V-Columbia Helicopters 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