# N254GL: 1996 Raytheon 1900D, registration cancelled 2026-04-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 21, 2026
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Raytheon 1900D](https://openairdocs.org/model/raytheon-1900d) (registry code 7150005)
- 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: UE-254
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: November 15, 1996
- Certificate issued: March 27, 2026
- Last registry action: March 27, 2026
- Mode S code: A266FB
- Owner when cancelled: [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N254GL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=254GL
- Page: https://openairdocs.org/deregistered/N254GL-2026-04-21

From the FAA registry file of November 4, 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 Raytheon 1900D: https://openairdocs.org/model/raytheon-1900d.md

## Service difficulty reports (75, newest 50)

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

- [SDR 2022F00509](https://openairdocs.org/sdr/2022F00509), Dec 9, 2022: RIB. CRACKED. CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT THE FOLLOWING LOCATION
- [SDR GLBA2017050800653](https://openairdocs.org/sdr/GLBA2017050800653), May 5, 2017: SNUBBER. CRACKED. MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR SNUBBER GLASS WAS CRACKED. REMOVED AND REPLACED THE AIRSTAIR SNUBBER STRUT ASSEMBLY IAW MM 52-10-01, OPS CHECKED GOO
- [SDR GLBA2017050800652](https://openairdocs.org/sdr/GLBA2017050800652), May 5, 2017: CABLE. BROKEN. MAINTENANCE REPORTED THAT THE UPPER FORWARD AIRSTAIR DOOR CABLE WAS BROKEN. REMOVED AND REPLACED THE CABLE IAW MM 52-10-02.
- [SDR GLBA2016080300602](https://openairdocs.org/sdr/GLBA2016080300602), Aug 3, 2016: STRINGER. CORRODED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 16 DEEPLY PITTED WITH CORROSION AT BS 198.25. MAJOR REPAIR.
- [SDR GLBA2016071500599](https://openairdocs.org/sdr/GLBA2016071500599), Jul 15, 2016: BULKHEAD. CRACKED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACKED BULKHEAD AT BS 588.1 AND STRINGER 8L ON THE BULKHEAD FLANGE, .5" IN LENGTH. MAJOR REPAIR.
- [SDR GLBA2016071500598](https://openairdocs.org/sdr/GLBA2016071500598), Jul 15, 2016: BULKHEAD. CRACKED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACKED BULKHEAD AT BS 588.1 AND STRINGER 8R ON THE BULKHEAD FLANGE, .4" IN LENGTH. MAJOR REPAIR.
- [SDR GLBA2016071400597](https://openairdocs.org/sdr/GLBA2016071400597), Jul 14, 2016: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK AT THE FUSELAGE FRAME AT BS 456, STRINGER 10R. MAJOR REPAIR
- [SDR GLBA2016071100594](https://openairdocs.org/sdr/GLBA2016071100594), Jul 11, 2016: SKIN. CORRODED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND EVIDENCE OF BELLY CORROSION BETWEEN STRINGERS 15 - 16L ALONG FRAME AT BS 198.25. MAJOR REPAIR.
- [SDR GLBA2016040800579](https://openairdocs.org/sdr/GLBA2016040800579), Apr 5, 2016: AUTOFEATHER SYS. UNKNOWN. PILOT REPORTED THAT THE LT ENG AUTO FEATHER CYCLED SEVERAL TIMES ON APPROACH. COMPLIED WITH FCD 1900-08-61-01, NO DEFECTS NOTED.
- [SDR GLBA2015091100536](https://openairdocs.org/sdr/GLBA2015091100536), Sep 9, 2015: AUTOFEATHER SYS. UNKNOWN. SIG EVENT, PILOT REPORTED THAT THE LT PROP AUTO FEATHERED WHEN INTRODUCING POWER FROM FLIGHT IDLE. TESTED AUTO FEATHER SYS SEVERAL TIMES IAW MM 61-21-00, SYS OP
- [SDR GLBA2013071200715](https://openairdocs.org/sdr/GLBA2013071200715), Jul 11, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE AFT FUSELAGE FRAME AT BS 509.5 AND STRINGER 3L IN THE FLANGE BEND RADIUS, 1.25" IN LENGTH. REPAIRED I
- [SDR GLBA2013071200714](https://openairdocs.org/sdr/GLBA2013071200714), Jul 11, 2013: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .375" IN LENGTH. REPAIRED
- [SDR GLBA2013071200713](https://openairdocs.org/sdr/GLBA2013071200713), Jul 11, 2013: RIB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT WING INBD RIB (JUNCTION WITH WING SPAR), RIB FLANGE AND DOUBLE, .75" IN LENGTH. REPAIRED IAW EO 13
- [SDR GLBA2013071100712](https://openairdocs.org/sdr/GLBA2013071100712), Jul 11, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE RT FRAME AT FS 451 AND STRINGER 10R IN THE BEND RADIUS, 1.3" IN LENGTH. REPAIRED IAW EO 13-1900-53-04
- [SDR GLBA2013030400192](https://openairdocs.org/sdr/GLBA2013030400192), Mar 1, 2013: BULB. BURNED OUT. PILOT REPORTED THAT THE EMERGENCY LIGHT ON F/O'S SIDE IS INOPERATIVE, EMERGENCY AND INDIRECT MODE. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2013012800163](https://openairdocs.org/sdr/GLBA2013012800163), Jan 27, 2013: DOWNLOCK SWITCH. DIRTY. PILOT REPORTED THAT WHILE EXTENDING THE GEAR, THE LT GEAR INDICATOR DID NOT ILLUMINATE, IN TRANSIT LIGHT WAS NOT ILLUMINATED, RAN QRH CK LIST AND MANUALLY PUMPE
- [SDR GLBA2012112800119](https://openairdocs.org/sdr/GLBA2012112800119), Nov 27, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS ON THE LT FWD SPAR CAP ANGLE ON VERTICAL STABILIZER, ONE CRACK GOING DOWN TO THE FIRST FASTENER HOLE AND 
- [SDR GLBA2012102900093](https://openairdocs.org/sdr/GLBA2012102900093), Oct 27, 2012: LIGHT. INOPERATIVE. PILOT REPORT THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX OPS CHECKED GOOD.
- [SDR GLBA201209032](https://openairdocs.org/sdr/GLBA201209032), Sep 2, 2012: TERMINAL. DIRTY. EMERGENCY LIGHTS WILL NOT COME ON DURING TEST. MX CLEANED CORROSION AND SECURED THE CONNECTION ON THE HOT BUSS BAR.
- [SDR GLBA2012041803](https://openairdocs.org/sdr/GLBA2012041803), Apr 18, 2012: SUPPORT. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACKED ON THE LT SIDEWALL FLANGE AT FS 327 STRINGER 9A LT IN THE FLANGE BEND RADIUS, 1.8" IN LENGTH. REPAIRED THE 
- [SDR GLBA2012041802](https://openairdocs.org/sdr/GLBA2012041802), Apr 18, 2012: SUPPORT. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT SIDEWALL FLANGE AT FS 288 & STRINGER 9AR IN THE BEND RADIUS OF THE FWD FLANGE, 1.4" IN LENGTH. RE
- [SDR GLBA2012041801](https://openairdocs.org/sdr/GLBA2012041801), Apr 18, 2012: SUPPORT. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT SIDEWALL FLANGE AT FS 327 & STRINGER 9AR, 1.2" IN LENGTH AT THE AFT FLANGE BEND RADIUS. REPAIRED 
- [SDR GLBA2012041202](https://openairdocs.org/sdr/GLBA2012041202), Apr 12, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 BETWEEN STRINGERS 3L & 4L, AT THE CARGO DOOR STRUT MOUNT, UPPER INBD NUTPLA
- [SDR GLBA2012041201](https://openairdocs.org/sdr/GLBA2012041201), Apr 12, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FUSELAGE FRAME AT FS 509 AND BETWEEN STRINGERS 4L & 5L AT THE CARGO DOOR STRUT MOUNT, UPPER INBD NU
- [SDR GLBA2012041002](https://openairdocs.org/sdr/GLBA2012041002), Apr 10, 2012: SPAR. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE HORIZONTAL STAB REAR SPAR WEB AT 10, 2, 5, & 7 O`CLOCK POSITION VIEWING FWD, TOTAL L
- [SDR GLBA2012041001](https://openairdocs.org/sdr/GLBA2012041001), Apr 10, 2012: DOOR FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE AIR STAIR DOOR ENTRANCE LWR FRAME AT THE LWR AFT CORNER, FS 173, 1.3" IN LENGTH. REPA
- [SDR GLBA20110826J](https://openairdocs.org/sdr/GLBA20110826J), Aug 25, 2011: CONNECTOR. DIRTY. PILOT REPORTED THAT THE MASTER CAUTION DID NOT ILLUMINATE WHEN THE AUTOFEATHER WAS RUN OFF. MX REMOVED PCB A127 INSPECTED AND CLEANED CONNECTIONS, REINSTALLED P
- [SDR GLBA20110826H](https://openairdocs.org/sdr/GLBA20110826H), Aug 25, 2011: CONNECTOR. DAMAGED. PILOT REPORTED THAT THE MASTER CAUTION DID NOT ILLUMINATE WHEN THE AUTOFEATHER WAS RUN OFF DURING RUN UP. MX RESECURED PIN 18 ON PCB A127, REF MI 24-01, OPS CHE
- [SDR GLBA20110808L](https://openairdocs.org/sdr/GLBA20110808L), Aug 7, 2011: CIRCUIT BOARD. MALFUNCTIONED. PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR DOES NOT TRIP THE MASTER CAUTION. MX RERACKED A126 PCB, IAW AIM CH 10 MI 24-01, OPS CHECKED GOOD.
- [SDR GLBA20110801F](https://openairdocs.org/sdr/GLBA20110801F), Jul 28, 2011: SEAL. WORN. MX REPORTED THAT DURING PRESSURIZATION THE CABIN DOOR WHISTLES. MX REPLACED THE DOOR SEAL IAW BMM 52-10-04, PN: 129-4000375, OPS CHECKED GOOD.
- [SDR GLBA20110729G](https://openairdocs.org/sdr/GLBA20110729G), Jul 28, 2011: SEAL. OUT OF POSITION. PILOT REPORTED THAT THE CABIN DOOR WAS SQUEALING IN FLIGHT. MX REPOSITIONED AND CLEANED THE DOOR SEAL, NO OTHER DEFECTS NOTED.
- [SDR GLBA20110728F](https://openairdocs.org/sdr/GLBA20110728F), Jul 27, 2011: CIRCUIT BOARD. INOPERATIVE. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR IS INOP, WORKS WITH THE PRESS TO TEST. MAINTENANCE REPLACED PCB PN: 129-364079-7 SN OFF 631-J-95 AND REPAIRED WIR
- [SDR GLBA20110706K](https://openairdocs.org/sdr/GLBA20110706K), Jul 3, 2011: DOOR. MISINSTALLED. PILOT REPORTED THAT DURING AN INSPECTION THE RT SIDE DOOR, 4C WAS NOT SEATED PROPERLY. MX REMOVED AND REINSTALLED THE EMERGENCY EXIT DOOR PROPERLY IAW BMM 52-20
- [SDR GLBA20110705J](https://openairdocs.org/sdr/GLBA20110705J), Jul 1, 2011: PCB. INOPERATIVE. "SUP" - SIG EVENT - PILOT REPORTED THAT THE LANDING GEAR HORN WAS INOPERATIVE. MX REPLACED PCB A119 PN: 112-3CY, OPS CK GOOD.
- [SDR GLBA20110606F](https://openairdocs.org/sdr/GLBA20110606F), Jun 5, 2011: CABLE. BROKEN. MX FOUND THE AIRSTAIR DOOR UPPER FWD CABLE BROKEN AND THE AFT UPPER CABLE COVER TORN. MX REPLACED BOTH CABLES IAW BMM.
- [SDR GLBA20101020](https://openairdocs.org/sdr/GLBA20101020), Oct 19, 2010: SKIN. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE BELLY SKIN CORRODED AT FS 213.25 BETWEEN STR 16 AND STR 15R. MAINTENANCE REPAIRED THE AFFECTED ARE
- [SDR GLBA2010102010](https://openairdocs.org/sdr/GLBA2010102010), Oct 19, 2010: SKIN. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE BELLY SKIN CORRODED AT FS 228.25 BETWEEN STR 16 AND STR 15R. MAINTENANCE REPAIRED THE AFFECTED AREA
- [SDR GLBA20101018F](https://openairdocs.org/sdr/GLBA20101018F), Oct 18, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A 1.7" CRACK IN THE RT HEAVY ANGLE FROM FS 288 GOING AFT 1.7" IN BEND RADIUS. MAINTENANCE REPAIRED THE
- [SDR GLBA20100330F](https://openairdocs.org/sdr/GLBA20100330F), Mar 30, 2010: SKIN. BUCKLED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, THE BELLY SKIN WAS FOUND BUCKLED IN NUMEROUS SPOTS BETWEEN THE FWD AND AFT SPAR FROM APPROX FS 288 TO 335, 32" FROM 
- [SDR GLBA20100113F](https://openairdocs.org/sdr/GLBA20100113F), Jan 10, 2010: SKIN. DAMAGED. MAJOR REPAIR - DURING ROUTINE TOWING OF ACFT ON 01/10/2010 THE RT WING CAME INTO CONTACT WITH ANOTHER ACFT RESULTING IN DAMAGE TO THE RT WING BETWEEN WS 183 & W
- [SDR GLBA20091030F](https://openairdocs.org/sdr/GLBA20091030F), Oct 27, 2009: SKIN. DAMAGED. WHILE TOWING THE ACFT INTO HANGAR IN "FMN" THE ELEAVATOR WAS DAMAGED. UPON INSP OF THE ACFT, DAMAGE WAS FOUND ON THE RT ELEVATOR T/E. BOTH THE TOP AND BOTTOM SK
- [SDR GLBA20090926A](https://openairdocs.org/sdr/GLBA20090926A), Sep 26, 2009: PCB. LOOSE. ON FINAL APPROACH INTO ALS WITH GEAR DOWN AND FLAPS 35 DEG RT PROPELLER TRIED TO AUTOFEATHER RT OIL PSI WAS AROUND 95-100. MAINTENANCE REMOVED AND RE-INSTALLED 
- [SDR GLBA20090423F](https://openairdocs.org/sdr/GLBA20090423F), Apr 20, 2009: SKIN. CRACKED. DURING A SCHEDULED STRUCTURAL INSP, A CRACK WAS FOUND IN THE BELLY SKIN AT FS 303 AND BL29 APPROX 5.6 INCH IN LENGTH. MX REPAIRED THE BELLY SKIN AT FS 303 AND B
- [SDR GLBA20061040](https://openairdocs.org/sdr/GLBA20061040), Dec 11, 2007: SKIN. DAMAGED. DAMAGE TO SKIN AT FS 163.975 AND STRINGER 2L AND 3L. MAINTENANCE REPAIRED SKIN AT FS 163.975 AND STRINGER 2L AND 3L IAW SRM 51-70. REPAIR DIMENSIONS APPROXIMATE
- [SDR GLBA20061033](https://openairdocs.org/sdr/GLBA20061033), Dec 6, 2007: ANGLE. CRACKED. LT HEAVY ANGLE CRACKED AT FUEL BEND RADIUS AT FS 288.0. LENGTH APPROXIMATELY 1.5 INCHES. MAINTENANCE REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53-90. REPAIR ARE
- [SDR GLBA20061035](https://openairdocs.org/sdr/GLBA20061035), Dec 6, 2007: SKIN. DELAMINATED. AIRSTAIR DOOR SKIN DELAMINATED AROUND EXTERIOR DOOR HANDLE. MAINTENANCE REMOVED CORROSION AROUND DOOR HANDLE AREA AND ACCOMPLISHED MINIMUM DAMAGE REPAIR I.A.W. 
- [SDR GLBA20061031](https://openairdocs.org/sdr/GLBA20061031), Dec 3, 2007: FRAME. CRACKED. FRAME CRACKED AT F.S. 164.4 AND STRINGER 9R. CRACK APPROXIMATELY .750 INCH IN LENGTH. MAINTENANCE REPAIRED FRAME CRACK AT F.S. 164.4 AND STRINGER 9R IAW SRM 51-
- [SDR GLBA20061029](https://openairdocs.org/sdr/GLBA20061029), Nov 16, 2007: SKIN. CORRODED. EXFOLIATION REPORTED ON BELLY OF THE AIRCRAFT AT STA. 212 AT BL3.5L TO BL 8.0L APPROXIMATELY 3 INCHES. MAINTENANCE REPLACED STRINGER 15L BETWEEN F.S. 183.25 TO 
- [SDR GLBA20061028](https://openairdocs.org/sdr/GLBA20061028), Nov 16, 2007: SKIN. DENTED. DENT ON FUSELAGE ABOVE AIRSTAIR DOOR FROM STA. 156-164 AND BL 10L TO BL18 APPROXIMATLEY .2500 INCH DEEP. MAINTENANCE REPAIRED DAMAGED FRAME AT F.S. 163.975 I.A.
- [SDR GLBA20060736](https://openairdocs.org/sdr/GLBA20060736), Apr 20, 2006: PCB. INTERMITTENT. RAT PROPELLER CYCLED IN AND OUT OF FEATHER SEVERAL TIMES, WITH AUTO FEATHER IN THE OFF POSITION IT OPERATED NORMALLY - REPLACED OVERSPEED GOVERNOR PAN 210961C S

All 75: https://openairdocs.org/deregistered/N254GL-2026-04-21/reports.md

## 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 DEN04IA024](https://openairdocs.org/ntsb/DEN04IA024), Nov 10, 2003: Beech 1900D (N254GL), Denver, CO, incident, minor damage. Probable cause: the ground personnel’s failure to maintain aircraft clearance, resulting in the collision. Contributing factors include ground communications not coordinated by the ground personnel, the flight…

## FAA accident and incident reports (2)

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 20130127000619I](https://openairdocs.org/incident/20130127000619I), Jan 27, 2013: Raytheon Aircraft Company 1900D (N254GL), North Platte, NE, No damage. On January 27, 2013 at 14:39 CST, N254GL, Beechcraft 1900D operated by great lakes aviation ltd, (glba) made an emergency landing on runway 30 at the North…
- [Incident 20031110028709I](https://openairdocs.org/incident/20031110028709I), Nov 10, 2003: Beech 1900D (N254GL), Denver, CO, Minor damage. (-23) Aircraft was being marshalled to parking position A52J on concourse a east ramp. Distance between painted aircraft parking spots on this section of the…

## Other aircraft with N254GL

- [Cancelled 1971-05-13](https://openairdocs.org/deregistered/N254GL-1971-05-13): Gates Lear Jet 24C, S/N 234. Exported to Argentina. Owner: [Gates Learjet Corporation](https://openairdocs.org/faa-owner/GATES%20LEARJET%20CORPORATION), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

---
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.