# N192CH: 1967 Kawasaki Vertol KV107-11 - Status: Valid registration - Airframe: [Kawasaki Vertol KV107-11](https://openairdocs.org/model/kawasaki-vertol-kv107-11) (registry code 4820101, 39 seats) - Engine: [GE CT58-140-2](https://openairdocs.org/engine/ge-ct58-140-2) (registry code 30129) - Data sheets: [TCDS H1PC](https://openairdocs.org/tcds/H1PC) (Kawasaki Heavy Industries Limited), [TCDS 1E3](https://openairdocs.org/tcds/1E3) (General Electric Company) (OpenAirDocs) - Serial number: 4011 - Year built: 1967 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: March 5, 2009 - Certificate issued: March 18, 2015 - Expires: March 31, 2028 - Mode S code: A16FD3 - Registered owner: [Columbia Helicopters Inc](https://openairdocs.org/faa-owner/COLUMBIA%20HELICOPTERS%20INC) - Location: [Aurora, OR](https://openairdocs.org/faa-place/OR/Aurora) - Owner type: Corporation - Owner's area on the map: 45.2403° N, 122.7936° W: Placed by OpenAirDocs at the center of ZIP code 97002, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=192CH - Page: https://openairdocs.org/aircraft/N192CH From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 14 in force ### Matched by airframe (Kawasaki Vertol KV107-11) None in force. ### Matched by engine (GE CT58-140-2) - [AD 2015-20-09](https://openairdocs.org/ad/2015-20-09): Life-limited rotating parts · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Nov 18, 2015 - [AD 2005-04-10](https://openairdocs.org/ad/2005-04-10): Stage 1 compressor disks · General Electric T58-GE-100, T58-GE-10, T58-GE-5 and 2 more. Effective Mar 29, 2005 - [AD 2004-04-06](https://openairdocs.org/ad/2004-04-06): Fuel flow divider assemblies · General Electric T58-GE-402, T58-GE-100, T58-GE-10 and 8 more. Effective Mar 9, 2004 - [AD 2001-12-07](https://openairdocs.org/ad/2001-12-07): Fuel Flow Divider Assemblies · General Electric T58-GE-402, T58-GE-100, T58-GE-10 and 4 more. Effective Jul 2, 2001 - [AD 97-21-08](https://openairdocs.org/ad/97-21-08): Stage 1 forward cooling plate · General Electric T58-GE-100, T58-GE-10, T58-GE-8F and 6 more. Effective Dec 19, 1997 - [AD 97-19-17](https://openairdocs.org/ad/97-19-17): Critical rotating parts · General Electric T58-GE-100, T58-GE-10, T58-GE-5 and 6 more. Effective Nov 28, 1997 - [AD 94-07-05](https://openairdocs.org/ad/94-07-05): Turbine Wheels · General Electric CT58-110-1, CT58-110-2, CT58-140-1 and 1 more. Effective Apr 19, 1994 - [AD 81-18-03](https://openairdocs.org/ad/81-18-03): Fuel Controls · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Sep 17, 1981 - [AD 81-02-02](https://openairdocs.org/ad/81-02-02): Stage One Turbine Wheels · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Feb 2, 1981 - [AD 78-26-08](https://openairdocs.org/ad/78-26-08): Lube Pump Drive Shaft · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Dec 19, 1978 - [AD 67-01-02](https://openairdocs.org/ad/67-01-02): Rotor Discs · General Electric CT58-100-1, T58-GE-5, T58-GE-1 and 5 more. Effective Aug 24, 1976 - [AD 76-13-02](https://openairdocs.org/ad/76-13-02): Oil Cooler-To-Fuel Filter Hose · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Jul 6, 1976 - [AD 74-25-01](https://openairdocs.org/ad/74-25-01): Fuel System Hose · General Electric CT58-140-1 and CT58-140-2. Effective Dec 10, 1974 - [AD 69-17-03](https://openairdocs.org/ad/69-17-03): First and Second Stage Turbine Rotor Discs · General Electric T58-GE-5, T58-GE-1, CT58-100-2 and 4 more. Effective Aug 27, 1969 ### Historical (superseded or no longer in force) - [AD 2008-22-16](https://openairdocs.org/ad/2008-22-16) (historical): Repetitive heavy lift (RHL) · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Dec 1, 2008 - [AD 2001-18-06](https://openairdocs.org/ad/2001-18-06) (historical): Engine Life-limited Rotating Parts · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Oct 18, 2001 - [AD 69-23-02](https://openairdocs.org/ad/69-23-02) (historical): Stage 2 Compressor Rotor Disc Shafts · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more. Effective Oct 15, 1970 - [AD 79-23-04](https://openairdocs.org/ad/79-23-04) (historical): Turboshaft Engines Rotating Components · General Electric CT58-100-2, CT58-110-1, CT58-110-2 and 2 more ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N192CH. ## FAA accident and incident reports None matched to N192CH. ## Service difficulty reports (2) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHIR201208281020](https://openairdocs.org/sdr/CHIR201208281020), Aug 22, 2012: ENGINE. LEAKING. AIRCRAFT WAS ON AN ACTIVE FIRE MISSION WHEN FLYING BACK TO THE WATER DIP SIGHT CO-PILOT NOTICED THE NR 2 ENGINE OIL PRESSURE DROP TO ZERO, SECONDS LATER THE NG - [SDR CHI1753](https://openairdocs.org/sdr/CHI1753), Mar 20, 1997: BLADE. VACUUM LEAK. EVACUATED BLADE SPAR INDICATOR SYSTEM (ISIS) SHOWED POSITIVE. BLADE REMOVED FROM SERVICE TO INVESTIGATE SOURCE OF LEAK. THE LEAK WAS DETERMINED COMING FROM A SM ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Kawasaki Vertol KV107-11 aircraft: https://openairdocs.org/model/kawasaki-vertol-kv107-11/aircraft.md - The GE CT58-140-2 engine: https://openairdocs.org/engine/ge-ct58-140-2.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.