# Service difficulty reports: N254GL, cancelled Apr 21, 2026

A list on [N254GL, cancelled Apr 21, 2026](https://openairdocs.org/deregistered/N254GL-2026-04-21.md).

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

Page 1 of 2 · 75 reports

- [SDR 2022F00509](https://openairdocs.org/sdr/2022F00509.md): Rib · cracked · Dec 9, 2022 · N254GL · Beech 1900D · Wing, Rib/Bulkhead
  > 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 LOCATIONS; BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.
- [SDR GLBA2017050800653](https://openairdocs.org/sdr/GLBA2017050800653.md): Snubber · cracked · May 5, 2017 · N254GL · Beech 1900D · Passenger/Crew Doors
  > 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 GOOD.
- [SDR GLBA2017050800652](https://openairdocs.org/sdr/GLBA2017050800652.md): Cable · broken · May 5, 2017 · N254GL · Beech 1900D · Passenger/Crew Doors
  > 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.md): Stringer · corroded · Aug 3, 2016 · N254GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > 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.md): Bulkhead · cracked · Jul 15, 2016 · N254GL · Beech 1900D · Fuselage Main, Bulkhead
  > 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.md): Bulkhead · cracked · Jul 15, 2016 · N254GL · Beech 1900D · Fuselage Main, Bulkhead
  > 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.md): Frame · cracked · Jul 14, 2016 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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.md): Skin · corroded · Jul 11, 2016 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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.md): Autofeather Sys · unknown · Apr 5, 2016 · N254GL · Beech 1900D · Propeller Feathering/Reversing
  > 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.md): Autofeather Sys · unknown · Sep 9, 2015 · N254GL · Beech 1900D · Propeller Feathering/Reversing
  > 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 OPERATED NORMAL.
- [SDR GLBA2013071200715](https://openairdocs.org/sdr/GLBA2013071200715.md): Frame · cracked · Jul 11, 2013 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 IAW EO 13-1900-53-048.
- [SDR GLBA2013071200714](https://openairdocs.org/sdr/GLBA2013071200714.md): Spar Cap · cracked · Jul 11, 2013 · N254GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > 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 IAW EO 13-1900-55-018.
- [SDR GLBA2013071200713](https://openairdocs.org/sdr/GLBA2013071200713.md): Rib · cracked · Jul 11, 2013 · N254GL · Beech 1900D · Wing, Rib/Bulkhead
  > 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 13-1900-57-012.
- [SDR GLBA2013071100712](https://openairdocs.org/sdr/GLBA2013071100712.md): Frame · cracked · Jul 11, 2013 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 13-1900-53-049.
- [SDR GLBA2013030400192](https://openairdocs.org/sdr/GLBA2013030400192.md): Bulb · burned out · Mar 1, 2013 · N254GL · Beech 1900D · Emergency Lighting
  > 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.md): Downlock Switch · dirty · Jan 27, 2013 · N254GL · Beech 1900D · Landing Gear Position and Warning
  > 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 PUMPED THE GEAR DOWN, STILL DID NOT RECEIVE 3 GREENS, PERFORMED GPWS TEST HAD NO WARNING HORN, LANDED WIT
- [SDR GLBA2012112800119](https://openairdocs.org/sdr/GLBA2012112800119.md): Spar Cap · cracked · Nov 27, 2012 · N254GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > 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 1 NEXT TO THE SECOND FASTENER HOLE, 0.875" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02580
- [SDR GLBA2012102900093](https://openairdocs.org/sdr/GLBA2012102900093.md): Light · inoperative · Oct 27, 2012 · N254GL · Beech 1900D · Emergency Lighting
  > PILOT REPORT THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX OPS CHECKED GOOD.
- [SDR GLBA201209032](https://openairdocs.org/sdr/GLBA201209032.md): Terminal · dirty · Sep 2, 2012 · N254GL · Beech 1900D · Light System Wiring
  > 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.md): Support · cracked · Apr 18, 2012 · N254GL · Beech 1900D · Fuselage Miscellaneous Structure
  > 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 AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-025. MAJOR REPAIR.
- [SDR GLBA2012041802](https://openairdocs.org/sdr/GLBA2012041802.md): Support · cracked · Apr 18, 2012 · N254GL · Beech 1900D · Fuselage Miscellaneous Structure
  > 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. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-024. MAJOR
- [SDR GLBA2012041801](https://openairdocs.org/sdr/GLBA2012041801.md): Support · cracked · Apr 18, 2012 · N254GL · Beech 1900D · Fuselage Miscellaneous Structure
  > 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 THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-023. MAJOR REPAIR.
- [SDR GLBA2012041202](https://openairdocs.org/sdr/GLBA2012041202.md): Frame · cracked · Apr 12, 2012 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 NUTPLATE, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1
- [SDR GLBA2012041201](https://openairdocs.org/sdr/GLBA2012041201.md): Frame · cracked · Apr 12, 2012 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 NUTPLATE MOUNT, 1.8" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW E
- [SDR GLBA2012041002](https://openairdocs.org/sdr/GLBA2012041002.md): Spar · cracked · Apr 10, 2012 · N254GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > 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 LENGTH 1". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55
- [SDR GLBA2012041001](https://openairdocs.org/sdr/GLBA2012041001.md): Door Frame · cracked · Apr 10, 2012 · N254GL · Beech 1900D · Fuselage Main, Structure
  > 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. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 12-1900-53-020. MAJOR REPAIR.
- [SDR GLBA20110826J](https://openairdocs.org/sdr/GLBA20110826J.md): Connector · dirty · Aug 25, 2011 · N254GL · Beech 1900D · Propeller/Propulsor System Wiring
  > PILOT REPORTED THAT THE MASTER CAUTION DID NOT ILLUMINATE WHEN THE AUTOFEATHER WAS RUN OFF. MX REMOVED PCB A127 INSPECTED AND CLEANED CONNECTIONS, REINSTALLED PCB IAW MI 24-01, PERFORMED ENGINE RUNS AND AUTOFEATHER CHECKS, SYS OPS CK GOOD.
- [SDR GLBA20110826H](https://openairdocs.org/sdr/GLBA20110826H.md): Connector · damaged · Aug 25, 2011 · N254GL · Beech 1900D · Propeller Feathering/Reversing
  > 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 CHECKED GOOD.
- [SDR GLBA20110808L](https://openairdocs.org/sdr/GLBA20110808L.md): Circuit Board · malfunctioned · Aug 7, 2011 · N254GL · Beech 1900D · Propeller Feathering/Reversing
  > 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.md): Seal · worn · Jul 28, 2011 · N254GL · Beech 1900D · Passenger/Crew Doors
  > 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.md): Seal · out of position · Jul 28, 2011 · N254GL · Beech 1900D · Passenger/Crew Doors
  > 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.md): Circuit Board · inoperative · Jul 27, 2011 · N254GL · Beech 1900D · Door Warning System
  > 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 WIRES F2639 IAW 24-57-00, OPS CK GOOD.
- [SDR GLBA20110706K](https://openairdocs.org/sdr/GLBA20110706K.md): Door · misinstalled · Jul 3, 2011 · N254GL · Beech 1900D · Emergency Exits
  > 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 52-20-00.
- [SDR GLBA20110705J](https://openairdocs.org/sdr/GLBA20110705J.md): Pcb · inoperative · Jul 1, 2011 · N254GL · Beech 1900D · Landing Gear Position and Warning
  > "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.md): Cable · broken · Jun 5, 2011 · N254GL · Beech 1900D · Passenger/Crew Doors
  > 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.md): Skin · corroded · Oct 19, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-059. MATERIALS UTILIZED ARE INCLUDED
- [SDR GLBA2010102010](https://openairdocs.org/sdr/GLBA2010102010.md): Skin · corroded · Oct 19, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-059. MATERIALS UTILIZED ARE INCLUDED
- [SDR GLBA20101018F](https://openairdocs.org/sdr/GLBA20101018F.md): Frame · cracked · Oct 18, 2010 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-058. MATERIALS UTILI
- [SDR GLBA20100330F](https://openairdocs.org/sdr/GLBA20100330F.md): Skin · buckled · Mar 30, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 CENTERLINE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900
- [SDR GLBA20100113F](https://openairdocs.org/sdr/GLBA20100113F.md): Skin · damaged · Jan 10, 2010 · N254GL · Beech 1900D · Wing, Plate/Skin
  > 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 & WS 236. UPON EVALUATION OF THE DAMAGE, THE AREA WAS DETERMINED TO REQUIRE A MAJOR REPAIR. MX REPAIRE
- [SDR GLBA20091030F](https://openairdocs.org/sdr/GLBA20091030F.md): Skin · damaged · Oct 27, 2009 · N254GL · Beech 1900D · Elevator, Plate/Skin
  > 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 SKINS AND RIBS DAMAGED 11" INBD OF TAB CUTOUT BENT DOWN 3" AND SKIN BUCKLED 23.5"L. MX REPAIRED THE
- [SDR GLBA20090926A](https://openairdocs.org/sdr/GLBA20090926A.md): Pcb · loose · Sep 26, 2009 · N254GL · Beech 1900D · Propeller/Propulsor System Wiring
  > 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 THE A123 PRINTED CIRCUIT BOARD AND PERFORMED AN OPERATIONAL CHECK WICH WAS GOOD IAW MM 61-21-00-001
- [SDR GLBA20090423F](https://openairdocs.org/sdr/GLBA20090423F.md): Skin · cracked · Apr 20, 2009 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 BL29 IAW EO 09-1900-53-005. MATERIALS UTILIZED INCLUDE.050 INCH 2024-T3 AL ALCLAD,.040 INCH 2024-T
- [SDR GLBA20061040](https://openairdocs.org/sdr/GLBA20061040.md): Skin · damaged · Dec 11, 2007 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 APPROXIMATELY 13.5 BY 13.2500. RII INSPECTION COMPLIED IAW GLA TASKCARD 8.2.1.
- [SDR GLBA20061033](https://openairdocs.org/sdr/GLBA20061033.md): Angle · cracked · Dec 6, 2007 · N254GL · Beech 1900D · Fuselage Miscellaneous Structure
  > 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 AREA APPROXIMATELY 13.5 INCHES. RII INSPECTION COMPLIED IAW GLA TASKCARD 8.2.1.
- [SDR GLBA20061035](https://openairdocs.org/sdr/GLBA20061035.md): Skin · delaminated · Dec 6, 2007 · N254GL · Beech 1900D · Entrance Stairs
  > AIRSTAIR DOOR SKIN DELAMINATED AROUND EXTERIOR DOOR HANDLE. MAINTENANCE REMOVED CORROSION AROUND DOOR HANDLE AREA AND ACCOMPLISHED MINIMUM DAMAGE REPAIR I.A.W. B1900D SRM 52-10. RII C/W PER GLA TASKCARD 8.2.1.
- [SDR GLBA20061031](https://openairdocs.org/sdr/GLBA20061031.md): Frame · cracked · Dec 3, 2007 · N254GL · Beech 1900D · Fuselage Main, Frame
  > 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 51-70. REPAIR APPROXIMATELY 5.5 BY 2.5 INCHES. 2024-T3.O71 INCHES RII INSPECTION COMPLIED IAW GLA TAS
- [SDR GLBA20061029](https://openairdocs.org/sdr/GLBA20061029.md): Skin · corroded · Nov 16, 2007 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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 F.S. 258.25 I.A.W. BEECH 1900D E.O. 07-UE254-01. MATERIAL APPROXIMATELY 5" LONG OF 2014 T6511 EXTRU
- [SDR GLBA20061028](https://openairdocs.org/sdr/GLBA20061028.md): Skin · dented · Nov 16, 2007 · N254GL · Beech 1900D · Fuselage Main, Plate/Skin
  > 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.W. BEECH 1900D E.O. 07-UE254-02. REPAIR AREA APPROXIMATELY 17" LONG. RII C/W PER GLA TASKCARD 8.2.1.
- [SDR GLBA20060736](https://openairdocs.org/sdr/GLBA20060736.md): Pcb · intermittent · Apr 20, 2006 · N254GL · Beech 1900D · Propeller Controlling System
  > 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 SON 11446450 AND AUTO FEATHER PUB 129-364091-9 SON 925B94.

Next page: https://openairdocs.org/deregistered/N254GL-2026-04-21/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N254GL' AND deregistration_id = 'N254GL-2026-04-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N254GL-2026-04-21/reports

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