# N141UE: 1991 Beech 1900C, registration cancelled 2009-04-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 2, 2009
- Status when cancelled: Valid registration
- Airframe: [Beech 1900C](https://openairdocs.org/model/beech-1900c) (registry code 1154161)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: UC-141
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: January 16, 1991
- Certificate issued: May 4, 2000
- Last registry action: December 10, 2008
- Mode S code: A0A82E
- Owner when cancelled: [Raytheon Aircraft Credit Corp](https://openairdocs.org/faa-owner/RAYTHEON%20AIRCRAFT%20CREDIT%20CORP)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.7687° N, 97.2202° W: Placed by OpenAirDocs at the center of ZIP code 67226, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N141UE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=141UE
- Page: https://openairdocs.org/deregistered/N141UE-2009-04-02

From the FAA registry file of November 5, 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 (11)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR GUU2001F00006](https://openairdocs.org/sdr/GUU2001F00006), Apr 10, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGH
- [SDR GUU2001F00005](https://openairdocs.org/sdr/GUU2001F00005), Apr 10, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT 
- [SDR GLBA97012](https://openairdocs.org/sdr/GLBA97012), Jan 19, 1997: DOWNLOCK SWITCH. SHORTED. MKG - GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH GEAR UP. MAINTENANCE FOUND NOSE DOWNLOCK SWITCH SHORTED. (M)
- [SDR GLBA96255](https://openairdocs.org/sdr/GLBA96255), Dec 30, 1996: PRSOV. MALFUNCTIONS. CIU - LEFT AND RIGHT ENVIRONMENTAL FAIL ANNUNCIATOR IN FLIGHT. MAINTENANCE SWAPPED PRSOV VALVES FOR TROUBLESHOOTING. RIGHT SIDE OPERATES NORMALLY. DEFERRED LEFT
- [SDR GLBA96208](https://openairdocs.org/sdr/GLBA96208), Oct 14, 1996: FRAME. CRACKED. DEN - CABIN DOOR FRAME CRACKED. REPAIRED 1.75 INCH CRACK AT SNUBBER ATTACH POINT. (M)
- [SDR GLBA96159](https://openairdocs.org/sdr/GLBA96159), Jul 22, 1996: FILLET. PUNCTURED. DVL - REPAIRED HOLE ON FUSELAGE ON RIGHT WING FILLET IAW SRM 51-70-00. (M)
- [SDR GLBA96125](https://openairdocs.org/sdr/GLBA96125), Jun 21, 1996: EVA TUBE. DAMAGED. MSP - LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED DURING CLIMB-OUT. MX REPAIRED HOLE IN EVA TUBING. (M)
- [SDR GLBA96130](https://openairdocs.org/sdr/GLBA96130), Jun 19, 1996: MOTOR. FAILED. GFK - GEAR WILL NOT RETRACT. MX REMOVED AND REPLACED LANDING GEAR POWER PACK MOTOR. (M)
- [SDR GLBA96089](https://openairdocs.org/sdr/GLBA96089), May 13, 1996: BRACKET. BENT. LAN - CREW REPORTED, NOSE GEAR GREEN LIGHT DOES NOT ILLUMINATE WITH GEAR SELECTED DOWN. MAINTENANCE STRAIGHTENED NOSE DOWNLOCK SWITCH CONTACT BRACKET. SYSTEM OP
- [SDR GLBA96041](https://openairdocs.org/sdr/GLBA96041), Feb 29, 1996: INTRANSIT LIGHT. MALFUNCTIONED. SPW - CREW REPORTED, THE GEAR INTRANSIT LIGHT DID NOT EXTINGUISH FOLLOWING TAKEOFF. THEY MADE AN AIR TUN BACK AND AN UNEVENTFUL LANDING. MAINTENANCE CYCLED GEAR
- [SDR GLBA96038](https://openairdocs.org/sdr/GLBA96038), Jan 24, 1996: PROP GOVERNOR. MALFUNCTIONED. MIE - CREW REPORTED, THE LEFT PROP WENT TO GROUND IDLE IN FLIGHT. MAINTENANCE PERFORMED GROUND RUN BUT COULD NOT DUPLICATE PROBLEM DURING OPS CHECK. AIRCRAFT RE

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW94IA139](https://openairdocs.org/ntsb/FTW94IA139), Apr 27, 1994: Beech 1900C (N141UE), Cheyenne, WY, incident, minor damage. Probable cause: A PARTIAL FAILURE OF THE LEADING EDGE TIP PORTION OF ONE OF THE LEFT ENGINE PROPELLER BLADES DUE TO PREVIOUS IMPACT DAMAGE FROM AN UNKNOWN SOURCE.

## 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 19940427016589I](https://openairdocs.org/incident/19940427016589I), Apr 27, 1994: Beech 1900C (N141UE), Denver, CO, Minor damage. Lost part of left propeller in flight. Shut engine down. Diverted to Denver.

---
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.