# N122GL: 1990 Beech 1900C, registration cancelled 2014-09-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 5, 2014 - Status when cancelled: Valid registration - Airframe: [Beech 1900C](https://openairdocs.org/model/beech-1900c) (registry code 1154161) - Engine: [Pratt & Whitney Canada PT6A-65B](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-65b) (registry code 52115) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs) - Serial number: UC-122 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: December 14, 2005 - Certificate issued: May 29, 2014 - Last registry action: May 29, 2014 - Mode S code: A05BC1 - Owner when cancelled: [Mtw Aerospace Inc](https://openairdocs.org/faa-owner/MTW%20AEROSPACE%20INC) - Location: [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery) - Owner type: Corporation - Owner's area on the map: 32.3391° N, 86.4011° W: Placed by OpenAirDocs at the center of ZIP code 36108, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N122GL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=122GL - Page: https://openairdocs.org/deregistered/N122GL-2014-09-05 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HSYA2012113012](https://openairdocs.org/sdr/HSYA2012113012), Nov 30, 2012: WIRE. BROKEN. PILOT REPORTED DURING A MX CHECK FLIGHT THAT THE GEAR REMAINED DOWN WITH ALL THREE GREEN LIGHTS ILLUMINATED WHEN THE GEAR HANDLE WAS MOVED TO THE UP POSITION. A - [SDR HSYA2010110310](https://openairdocs.org/sdr/HSYA2010110310), Nov 3, 2010: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT -COME UP-AFTER CYCLING THE GEAR STILL WOULD NOT COME UP AND WAS STILL INDICATING 3 GREEN IN THE DOWN POSITION. - [SDR HSYA2010060210](https://openairdocs.org/sdr/HSYA2010060210), Jun 2, 2010: CABLE. LOOSE. AFTER ROTATION, CAPTAIN REPORTED AN UNCOMMANDED RT ENGINE AUTO FEATHER. THE ACFT RETURNED TO THE AIRPORT WITHOUT FURTHER INCIDENT ARRIVING BACK IN THE BLOCKS FO - [SDR HSYA2010050810](https://openairdocs.org/sdr/HSYA2010050810), May 8, 2010: VENT. CONTAMINATED. PILOT REPORTED TO MX AFTER LANDING, THAT A BURNING PLASTIC/RUBBER SMELL IN CABIN WITH BLEEDS ON, CABIN TEMP SET TO COLD. MX TROUBLESHOT ACFT AND FOUND RUBBISH U - [SDR HSYA2009082109](https://openairdocs.org/sdr/HSYA2009082109), Aug 21, 2009: ENGINE. MALFUNCTIONED. ON ROTATION RT ENG TORQUE WENT TO 4000 LBS. FOR APPROXIMATELY 2 SECONDS. ENG STARTED TO AUTOFEATHER & PILOT PULLED THROTTLE BACK & SHUTDOWN ENG. PERFORM A BORES - [SDR HSYA20070702](https://openairdocs.org/sdr/HSYA20070702), Jul 1, 2007: AIRSTAIR. CRACKED. DURING PREFLIGHT INSPECTION, CREW REPORTED A CRACK ON THE AIRSTAIR DOOR NEAR THE HINGE. MX FOUND A CRACK ON THE INNER DOOR SKIN NEAR THE AFT END DOOR HINGE. UPO - [SDR HSY2005F00002](https://openairdocs.org/sdr/HSY2005F00002), Jan 24, 2005: HOSE. LEAKING. (MRR NR 02-012405) LOSS OF HYDRAULIC PRESSURE AND QUANTITY LED TO THE INABILITY TO OPERATE THE LANDING GEAR WITH NORMAL PROCEDURES. LANDING GEAR HAD TO BE EXTEN - [SDR GLBA20030617](https://openairdocs.org/sdr/GLBA20030617), Apr 26, 2004: CIRCUIT BREAKER. TRIPPED. GEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOOD - [SDR GLBA2001149](https://openairdocs.org/sdr/GLBA2001149), Jul 7, 2001: CAM. WORN. FLAPS WOULD NOT RETRACT ON T/O. REPLACED SAFETY SWITCH CAM. - [SDR GLBA2001038](https://openairdocs.org/sdr/GLBA2001038), Feb 15, 2001: ELEVATOR. FLUTTER. PILOT REPORTED ELEVATOR FLUTTER ON DESCENT AND CLIMB. INSPECTED FLIGHT CONTROLS, PERFORMED TEST FLIGHT. COULD NOT DUPLICATE, OPS CHECKED GOOD. RETURNED TO SERVI - [SDR GLBA2001011](https://openairdocs.org/sdr/GLBA2001011), Jan 24, 2001: COWLING. SEPARATED. RETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWLING. RETURNED TO SERVICE. - [SDR 20010112SG041](https://openairdocs.org/sdr/20010112SG041), Dec 2, 2000: ALTIMETER. MALFUNCTIONED. CAPTAINS ALTIMETER STUCK AT 10,200 FEET, AIR TURN BACK. CAPTAINS ALTIMETER REMOVED AND REPLACED. SYSTEM TESTED OK. (M) - [SDR 20010112SG038](https://openairdocs.org/sdr/20010112SG038), Nov 30, 2000: ALTIMETER. FAILED. CAPTAINS ALTIMETER FLAGGED AND ALTITUDE ALERTER FAILED AFTER TAKEOFF. RETURNED TO AIRPORT. CAPTAINS. CAPTAINS ALTIMETER WAS REMOVED AND REPLACED. TESTED OK. (M) - [SDR GLBA97064](https://openairdocs.org/sdr/GLBA97064), Apr 8, 1997: DOWNLOCK SWITCH. OUT OF ADJUST. SPI - GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH IN FLIGHT. MAINTENANCE ADJUSTED NOSE GEAR DOWNLOCK SWITCH. (M) - [SDR GLBA96233](https://openairdocs.org/sdr/GLBA96233), Nov 26, 1996: UPLOCK SWITCH. FAILED. SPI - AFTER RETRACTION, RED INTRANSIT LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK SWITCH. ALL SWITCHES WERE LATER ADJUSTED. TEST FLIGHT SATISF - [SDR GLBA96170](https://openairdocs.org/sdr/GLBA96170), Jul 31, 1996: TRUSS. CRACKED. SPI - RIGHT TRUSS CRACKED AT AREA 'A'. REMOVED AND REPLACED RIGHT TRUSS. (M) - [SDR GLBA96151](https://openairdocs.org/sdr/GLBA96151), Jul 12, 1996: WINDSHIELD. ARCING. MBL - AT 10,000 FEET DURING MODERATE RAIN, SMOKE IN COCKPIT WITH WINDSHIELD FUEL VENTS, ALT STATIC, PITOT AND STALL HEAT ON AND THE ENGINE ANTI-ICE ON. MAINTENA - [SDR GLBA96111](https://openairdocs.org/sdr/GLBA96111), Jun 3, 1996: ACTUATOR. FAILED. ORD - LEFT MLG SLOW TO INDICATE DOWN AND LOCKED. REMOVED AND REPLACED LEFT MLG ACTUATOR. OPS CHECKS GOOD. (X) - [SDR GLBA96099](https://openairdocs.org/sdr/GLBA96099), May 24, 1996: DOWNLOCK SWITCH. FAILED. ORD - CREW SELECTED GEAR DOWN, BUT RECEIVED NO 'DOWN AND LOCKED' INDICATION ON LT GEAR. ON SECOND ATTEMPT, LT GEAR LIGHT ILLUMINATED AND CREW LANDED UNEVENTFULL - [SDR GLBA96090](https://openairdocs.org/sdr/GLBA96090), May 12, 1996: AILERON. DAMAGED. ORD -CREW FOUND DAMAGE ON TRAILING EDGE OF LEFT AILERON DURING WALK AROUND INSPECTION. MAINTENANCE REMOVED AND REPLACED LEFT AILERON. FLIGHT TEST WAS GOOD. (M) - [SDR GLBA96004](https://openairdocs.org/sdr/GLBA96004), Feb 5, 1996: WARNING SYSTEM. ACTIVATED. UC-122 HAD FLAPS IN TAKEOFF POSITION, GEAR DOWN AND LOCKED WITH 3 GREEN INDICATED. THE RED LIGHTS ILLUMINATED IN THE GEAR HANDLE AND AURAL WARNING SOUNDED. THE - [SDR GLBA96027](https://openairdocs.org/sdr/GLBA96027), Jan 31, 1996: WARNING SYSTEM. MALFUNCTIONED. OSH - CREW REPORTED THAT THE GEAR INTRANSIT LIGHT AND HORN WOULD NOT EXTINGUISH WHEN GEAR SELECTED UP. CREW ELECTED TO DO AN AIR TURN BACK AND MADE AN UNEVENTFU - [SDR 96ZZZM78](https://openairdocs.org/sdr/96ZZZM78), Nov 14, 1995: ELEVATOR. DAMAGED. DEN - AIRCRAFT NR 159GL AND N122GL, CONTACTED ELEVATORS ON THE GROUND. MAINTENANCE REPLACED THE RIGHT ELEVATOR DUE TO TIP DAMAGE. (M) - [SDR 95ZZZM513](https://openairdocs.org/sdr/95ZZZM513), Aug 30, 1995: ENGINE. FAILED. ORD-BRL - FLT NR 5927 - THE LEFT ENGINE FAILED AND WAS SECURED. THE CREW DIVERTED TO GBC ON SINGLE ENGINE AND COMPLETED AND UNEVENTFUL LANDING. MAINTENANCE CHAN - [SDR 95ZZZX1964](https://openairdocs.org/sdr/95ZZZX1964), Mar 21, 1995: SKIN. CRACKED. SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND DORSAL FIN CRACKED ON LT SIDE AT REAR PRESSURE BULKHEAD ATTACH POINT. THE CRACK WAS BETWEEN TWO RIVET HOLES. - [SDR 95ZZZX1963](https://openairdocs.org/sdr/95ZZZX1963), Mar 20, 1995: TRUSS. CRACKED. SPW - DURING SCHEDULED VISUAL INSPECTION REQUIRED BY AD 95-02-18 IAW BEECH SB 2255R6, AREA OF THE RT ENGINE TRUSS WAS FOUND CRACKED. REPLACED TRUSS WITH SERVICE ## FAA accident and incident reports (4) 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 19980506012969I](https://openairdocs.org/incident/19980506012969I), May 6, 1998: Beech 1900C (N122GL), Denver, CO, Minor damage. Narrative: at approximately 05:45, 5/6/98, united airlines tug #CT4612, operated by uala employee william lett, accidentally ran into the left wing of air… - [Incident 19970408007489I](https://openairdocs.org/incident/19970408007489I), Apr 8, 1997: Beech 1900C (N122GL), Springfield, IL. Narrative: on April 8, 1997, great lakes aviation, ltd. flight 5859 was enroute from chicago, IL to decatur, IL. The nose landing gear did not indicate down… - [Incident 19950830031829I](https://openairdocs.org/incident/19950830031829I), Aug 30, 1995: Beech 1900C (N122GL), Galesburg, IL. During cruise left engine blew up. Secured. Diverted to gbg. - [Incident 19930421013649I](https://openairdocs.org/incident/19930421013649I), Apr 21, 1993: Beech 1900C (N122GL), Des Moines, IA. Unsafe gear light after departed. Manually extended gear at destination. Landed safely. ## Other aircraft with N122GL - [Cancelled 2025-04-01](https://openairdocs.org/deregistered/N122GL-2025-04-01): Boeing 737-800, S/N 28636. Owner: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) --- 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.