# N207CJ: 1990 Beech 1900C, registration cancelled 2005-06-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 28, 2005 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Beech 1900C](https://openairdocs.org/model/beech-1900c) (registry code 1154161) - Engine: [Pratt & Whitney Canada PT6A-60A](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-60a) (registry code 52043) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs) - Serial number: UC-107 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: April 19, 1990 - Certificate issued: June 8, 2005 - Last registry action: June 8, 2005 - Mode S code: A1AC3F - Owner when cancelled: [Specialized Aircraft Services Inc](https://openairdocs.org/faa-owner/SPECIALIZED%20AIRCRAFT%20SERVICES%20INC) - Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - Owner type: Corporation - Owner's area on the map: 37.7038° N, 97.2793° W: Placed by OpenAirDocs at the center of ZIP code 67208, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N207CJ - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=207CJ - Page: https://openairdocs.org/deregistered/N207CJ-2005-06-28 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Beech 1900C: https://openairdocs.org/model/beech-1900c.md ## Service difficulty reports (13) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 297031](https://openairdocs.org/sdr/297031), Oct 22, 2003: CIRCUIT CARD. MALFUNCTIONED. DURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TO INDICATE THAT BOTH THE LEFT AND RIGHT GEN TIES WERE OPEN ONE ATTEMPT WAS MADE TO RESET. DID NOT RESET, THE TAK - [SDR 1850301](https://openairdocs.org/sdr/1850301), Jul 2, 2003: HANDLE. OUT OF ADJUST. EMERGENCY EXIT LOOSE IN LOCKED POSITION. ADJUSTED EXIT DOOR HANDLE TENSION. - [SDR NSVA200300016](https://openairdocs.org/sdr/NSVA200300016), Mar 3, 2003: DOOR LATCH. SEIZED. LEB-Crew reported door handle stiff with door open or closed and button stuck on handle for airstair door. MX R&R Airstair door latch and lock assembly IAW Beec - [SDR NSVA200300006](https://openairdocs.org/sdr/NSVA200300006), Feb 19, 2003: ODOR. DETECTED. DURING FLIGHT THE LIGHTS/FLIGHT CIRCUIT BREAKER POPPED OUT. CIRCUIT BREAKER WAS RESET AND THEN POPPED AGAIN. THEN A STRONG ODOR OF ELECTRICAL DISCHARGE. THE BAC - [SDR NSVA200300003](https://openairdocs.org/sdr/NSVA200300003), Jan 22, 2003: HANDLE. LOOSE. IN FLIGHT, INSIDE DOOR HANDLE FELL OFF. - [SDR NSVA200200001](https://openairdocs.org/sdr/NSVA200200001), Oct 17, 2002: CHECK VALVE. FAILED. BOS- AFTER TAXIING TO GATE THE LT ENGINE WOULD NOT SHUT DOWN. FIRE T-HANDLE WAS PULLED, NO EFFECT. THE ENGINE CONTINUED TO RUN. MAINTENANCE VERIFIED THE FIREWAL - [SDR NSV2002F00000](https://openairdocs.org/sdr/NSV2002F00000), Dec 31, 2001: LINE. CHAFED. MECHANIC FOUND EVIDENCE OF FUEL DRIPPING FROM LEFT ENGINE NACELLE. REMOVED AND REPLACED FUEL LINE, RAN UP, LEAK CHECKED GOOD. (CONTROL NR NSVA 02-03) - [SDR NSVA0109](https://openairdocs.org/sdr/NSVA0109), Aug 20, 2001: FCU. MALFUNCTIONED. EN ROUTE FROM BOS-BHB, CREW NOTED THE FOLLOWING DISCREPANCY IN FIGHT LOG; LEFT ENGINE PARAMETERS DID NOT CHANGE WITH POWER LEVER CHANGES. AT THAT TIME THE CREW - [SDR NSVA20003](https://openairdocs.org/sdr/NSVA20003), Aug 20, 2000: CABLE. BROKEN. IN ACK AIRCRAFT WAS BOARDED BY CREW AND PASSENGERS. WHEN CREW CLOSED AIRSTAIR DOOR THEY NOTICED AN IRREGULARITY WITH THE HANDLE. CREW THEN TRIED TO OPEN DOOR AN - [SDR NSVA20002](https://openairdocs.org/sdr/NSVA20002), Aug 4, 2000: ROD. MISINSTALLED. AFTER TAKEOFF FROM ACK ADJUSTED AILERON TRIM WHICH CAUSED THE LEFT POWER LEVER TO MOVE AFT (RETARD). LEFT ENGINE TORQUE DECREASED APPROXIMATELY 500 LBS. DIVERTE - [SDR 98ZZZX4682](https://openairdocs.org/sdr/98ZZZX4682), Oct 17, 1998: LINE. LEAKING. THIS FUEL LINE GOES FROM THE FCU TO THE FUEL FLOW TRANSMITTER. THE DUCT FROM THE COWL TO THE STARTER/GENERATOR RUBS ON THIS LINE. THIS IS ONLY ON THE LEFT ENGIN - [SDR NSVA97013](https://openairdocs.org/sdr/NSVA97013), Oct 1, 1997: ACTUATOR. FAILED. ON TAXI, PART OF THE NOSE GEAR STEERING ACTUATOR FAILED CAUSING LOSS OF ASSISTED NOSE WHEEL STEERING. MAINTENANCE INSPECTED THE AIRCRAFT AND SECURED ALL LOOSE I - [SDR NSVA97012](https://openairdocs.org/sdr/NSVA97012), Oct 1, 1997: WINDOW. FAILED. ON TAKEOFF CLIMB, THE LEFT WINDSCREEN STARTED SMOKING WITH THE WINDSHIELD HEAT ON. THE CREW TURNED OFF THE WINDOW HEAT AND MADE AN UNEVENTFUL LANDING AT THEIR D ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19981013040159I](https://openairdocs.org/incident/19981013040159I), Oct 13, 1998: Beech 1900C (N207CJ), Beckley, WV, Minor damage. (-5)Aircraft hit deer on landing with left engine at bkw. Damage to left propeller, three blade tips were cut-off, on blade was split up the middle. Eleven… ## Other aircraft with N207CJ - [Registered now](https://openairdocs.org/aircraft/N207CJ): Textron 525C, S/N 525C0207 --- 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.