# Service difficulty reports: N255GL

A list on [N255GL](https://openairdocs.org/aircraft/N255GL.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 · 77 reports

- [SDR GLBA2016111400615](https://openairdocs.org/sdr/GLBA2016111400615.md): Cable · broken · Nov 12, 2016 · N255GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABLE BROKE BETWEEN THE CABIN DOOR AND THE SNUBBER. MAINTENANCE REPLACED THE AIRSTAIR DOOR CABLE FROM THE SNUBBER TO THE DOOR.
- [SDR GLBA2015050800519](https://openairdocs.org/sdr/GLBA2015050800519.md): Fastener · loose · May 8, 2015 · N255GL · Beech 1900D · Passenger/Crew Doors
  > SIG EVENT, MX REPORTED THAT THE CABIN DOOR WILL NOT CLOSE FROM THE OUTSIDE OF ACFT. FOUND LOOSE HARDWARE AT THE INTERNAL HANDLE BELL CRANK. SECURED HARDWARE IAW AIM 12.15.0. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014091900443](https://openairdocs.org/sdr/GLBA2014091900443.md): Skin · corroded · Sep 18, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION FOUND SKIN CORROSION & BULGING, 6 INCH AREA, RUNNING LATERALLY ALONG FORMER RING UNDER CARGO BAY AREA AT APPROX FS 497.00 & APPROX WL 76.00 RUNNING APPROX RBL 9.00 TO RBL 15.00. THE CORROSION & BULGING SKIN HAS CAUSED A.5 INCH
- [SDR GLBA2014050600412](https://openairdocs.org/sdr/GLBA2014050600412.md): Skin · cracked · May 5, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, MX FOUND A CRACK AT THE EMERGENCY EXIT, RT FWD, BONDED SKIN AT THE LWR AFT CORNER, 1.3" IN LENGTH. REPAIRED IAW EO 14-1900-52-004.
- [SDR GLBA2014042800411](https://openairdocs.org/sdr/GLBA2014042800411.md): Rib · cracked · Apr 28, 2014 · N255GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT WING INBD RIB FLANGE & DOUBLER FLANGE AT FS 288 & BL 29.06, FROM OTBD EDGES INWARD TO BEND RADIUS OF THE RIB FLANGE & DOUBLER FLANGE, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUI
- [SDR GLBA2014042400410](https://openairdocs.org/sdr/GLBA2014042400410.md): Frame · cracked · Apr 24, 2014 · N255GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.25 BETWEEN STRINGER 2R & 3R AT THE INBD LOWER CORNER AT AIR DUCT CUTOUT FROM A FASTENER TO THE BEND RADIUS,.2 INCHES IN LENGTH. MAJOR REPAIR, REPAIRED THE AFFECTED AREA AND PERFOR
- [SDR GLBA2014041500408](https://openairdocs.org/sdr/GLBA2014041500408.md): Skin · cracked · Apr 15, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND 3 CRACKS AT FS 163.97 & STRINGER 1, AT FASTENERS ON LT & RT SIDE OF STRINGER 1,.35 INCHES IN TOTAL LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-024.
- [SDR GLBA2014031700404](https://openairdocs.org/sdr/GLBA2014031700404.md): Tire · blown · Mar 16, 2014 · N255GL · Beech 1900D · Tire
  > PILOT NOTED THAT BOTH LT MAIN TIRES BLEW ON LANDING. R & R NR 1 & NR 2 MAIN WHEEL ASSEMBLIES IAW TASK CARD 1900-3240-01. PN 5006028-5, NR 1 SN ON 56/917, SN OFF 1601, NR 2 SN ON 561 431, SN OFF 284 1930. PERFORMED VISUAL INSPECTION OF LT MLG HUBS, BRAKES &
- [SDR GLBA2014030300398](https://openairdocs.org/sdr/GLBA2014030300398.md): Channel · cracked · Mar 3, 2014 · N255GL · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT HAT SECTION OF THE UPPER FLANGE FROM FWD FASTENER TO FLANGE LE, VSS 84.10 & 206 CHORD,.35 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-002.
- [SDR GLBA2013030700199](https://openairdocs.org/sdr/GLBA2013030700199.md): B-Nut · loose · Mar 6, 2013 · N255GL · Beech 1900D · Hydraulic System, Main
  > PILOT REPORTED THAT WHILE EXTENDING THE GEAR, MAINS SHOWED DOWN AND LOCKED, NOSE DID NOT SHOW GREEN INDICATION, GEAR HANDLE IN TRANSIT, REMAINED ILLUMINATED, RAN CHECKLIST, MANUALLY PUMPED GEAR DOWN, HAD 3 GREEN INTRANSIT LIGHT EXT, LANDED WITH NO FURTHER INCI
- [SDR GLBA2012121100133](https://openairdocs.org/sdr/GLBA2012121100133.md): Stabilon · damaged · Dec 11, 2012 · N255GL · Beech 1900D · Horizontal Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT STABILON AFT OTBD CORNER HAS FIBERGLASS DAMAGE MEASURING APPROX 4" X 3". REPAIRED IAW EO 13-1900-55-001. MAJOR REPAIR
- [SDR GLBA2012102400087](https://openairdocs.org/sdr/GLBA2012102400087.md): Spar Cap · cracked · Oct 24, 2012 · N255GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE FROM UPPER FASTENER HOLE TO UPPER EDGE OF ANGLE,.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-050. MAJOR REPAIR.
- [SDR GLBA2012102200086](https://openairdocs.org/sdr/GLBA2012102200086.md): Frame · cracked · Oct 22, 2012 · N255GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON FRAME AT FS 183.25 AND STRINGER 1, DOWNWARD TO THE EDGE OF THE FRAME, 2.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-057. MAJOR REPAIR.
- [SDR GLBA2012102200083](https://openairdocs.org/sdr/GLBA2012102200083.md): Web · cracked · Oct 20, 2012 · N255GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB AT THE 2 O'CLOCK POSITION,.125" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-049. MAJOR REPAIR.
- [SDR GLBA2012101900081](https://openairdocs.org/sdr/GLBA2012101900081.md): Spar · cracked · Oct 19, 2012 · N255GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT, STARTING AT TOP FASTENER AT FSS 84.18 MOVING DOWN TO THIRD FASTENER AT FSS 84.16, 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-048.
- [SDR GLBA2012092400068](https://openairdocs.org/sdr/GLBA2012092400068.md): Cam · out of adjust · Sep 24, 2012 · N255GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR IS DIFFICULT TO OPEN. MX ADJUSTED 2 AFT LOWER CAM'S IAW BMM 52-10-00, OPS CK GOOD.
- [SDR GLBA20111130K](https://openairdocs.org/sdr/GLBA20111130K.md): Wheel · out of balance · Nov 29, 2011 · N255GL · Beech 1900D · Wheel/Ski/Float
  > PILOT REPORTED THAT WHEN THE GEAR WAS RETRACTED, A STRONG VIBRATION WAS FELT FOR ABOUT 10 SECONDS. MX PERFORMED GEAR SWINGS IAW AIM CHAP 10 32-01, NO DEFECTS NOTED, REPLACED NOSE WHEEL PN: 114-8001-35, SN: 2345 IAW TC. 1900-3240.00 R2, OPS CK GOOD.
- [SDR GLBA20110913F](https://openairdocs.org/sdr/GLBA20110913F.md): Lanyard · broken · Sep 12, 2011 · N255GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIR STAIR DOOR LANDYARD BROKE. MX REPLACED THE DOOR SNUBBER CABLE, PN: 129-514119-1GLA, IAW BMM 52-12-01, OPS CHECKED GOOD.
- [SDR GLBA20110818G](https://openairdocs.org/sdr/GLBA20110818G.md): Cover · torn · Aug 18, 2011 · N255GL · Beech 1900D · Passenger/Crew Doors
  > MX FOUND THE AIRSTAIR DOOR UPPER FWD CABLE COVER TORN. MX REPLACED THE CABLE IAW MM 52-10-02, PN: 1440-40GLA.
- [SDR GLBA20110818F](https://openairdocs.org/sdr/GLBA20110818F.md): Cover · torn · Aug 18, 2011 · N255GL · Beech 1900D · Passenger/Crew Doors
  > MX FOUND THE AIRSTAIR DOOR LOWER FWD CABLE COVER TORN. MX REPLACED THE CABLE IAW MM 52-10-02, PN: 1440-43GLA.
- [SDR GLBA20110817J](https://openairdocs.org/sdr/GLBA20110817J.md): Propeller · malfunctioned · Aug 16, 2011 · N255GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE RT PROP GOES INTO FEATHER BEFORE TAKING BEYOND FEATHER GATE, GOES INTO FEATHER IN THE TAXI POSITION. MX RAN ENGINES, PROP DIDN'T GO INTO FEATHER UNTIL THE LEVER REACHED THE FEATHER STRIP ON THE QUADRANT, SYS OK FOR SERVICE.
- [SDR GLBA20110518G](https://openairdocs.org/sdr/GLBA20110518G.md): Tire · failed · May 18, 2011 · N255GL · Beech 1900D · Tire
  > PILOT REPORTED THAT DURING SIGNIFICANT LEFT QUARTERING CROSSWIND LANDING BOTH RT MAIN TIRES BLEW AND BECAME FLAT. MAINTENANCE R&R NR 3 AND NR 4 MAIN TIRES IAW TC 1900-3210.01,
- [SDR GLBA20110405G](https://openairdocs.org/sdr/GLBA20110405G.md): Frame · cracked · Apr 5, 2011 · N255GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FWD FUSELAGE FRAME AT F.S. 456 CRACKED AT THE GAS STRUT MOUNT UPPER IB NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INS
- [SDR GLBA20110405J](https://openairdocs.org/sdr/GLBA20110405J.md): Skin · chafed · Apr 5, 2011 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > "SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND RH OB FWD CORNER OF FUSELAGE BELLY SKIN AT F.S. 258.25 CHAFFED THROUGH, AREA OF CHAFE 2.2" BY.6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS
- [SDR GLBA20110404F](https://openairdocs.org/sdr/GLBA20110404F.md): Frame · cracked · Apr 4, 2011 · N255GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CUTOUT IS CRACKED AT THE IB LWR CORNER OF THE COUTOUT, CRACK IS.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQU
- [SDR GLBA20100628G](https://openairdocs.org/sdr/GLBA20100628G.md): Circuit Board · dirty · Jun 27, 2010 · N255GL · Beech 1900D · Propeller Feathering/Reversing
  > SUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE LT AUTO FEATHER SYS DISENGAGED REPEATEDLY IN ALL POWER SETTINGS. MX REMOVED THE A123 PRINTED CIRCUIT BOARD, CLEANED CONTACTS, RE-INSTALLED THE A123 PRINTED CIRCUIT BOARD IAW MX INSTRUCTION 24-01. MX RAN THE ENGI
- [SDR GLBA20100611G](https://openairdocs.org/sdr/GLBA20100611G.md): Skin · damaged · Jun 10, 2010 · N255GL · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - REF GLBA20100611F, FOUND UNDERLYING DAMAGE DURING REPAIR OF LEFT WING LEADING EDGE STRINGER AT LEFT WS 201 HAS REPAIR DAMAGE WITH MISSING MATERIAL. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900
- [SDR GLBA20100611F](https://openairdocs.org/sdr/GLBA20100611F.md): Structure · cracked · Jun 10, 2010 · N255GL · Beech 1900D · Wing, Plate/Skin
  > PILOT REPORTED A CRACK ON THE LEFT WING UPPER FORWARD SIDE AT APPROXIMATELY WS 194, FURTHER EVALUATION DISCOVERED THE CRACK TO BE AERODYNAMIC FILLER ONLY, BUT DID FIND AN UNDERLYING REPAIR THAT REQUIRES REWORK. MAJOR REPAIR - MAINTENANCE REPAIRED THE AFFECTED
- [SDR GLBA201005162](https://openairdocs.org/sdr/GLBA201005162.md): Unknown · smoke · May 16, 2010 · N255GL · Beech 1900D · Air Distribution System
  > HAD SMOKEY LOOK IN ROW 2 FROM PAX MODE CONTROL IN MANUAL, SHUT SYS DOWN, MX RAN NR 1 ENG AND WITH BLEED AIR ON, OPERATED THE ENVIRONMENTAL SYS IN MANUAL AND MANUAL COOL MODES. OPERATED THE BLOWERS IN HIGH AND AUTO. COULD NOT DUPLICATE SMOKE. NO UNUSUAL ODORS D
- [SDR GLBA200910251](https://openairdocs.org/sdr/GLBA200910251.md): Bulb · inoperative · Oct 25, 2009 · N255GL · Beech 1900D · Emergency Lighting
  > FO'S EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OF THE LIGHT WAS GOOD.
- [SDR GLBA20091026F](https://openairdocs.org/sdr/GLBA20091026F.md): Bulb · inoperative · Oct 20, 2009 · N255GL · Beech 1900D · Emergency Lighting
  > EES - PILOTS REPORTED THAT THE FIRST OFFICERS EMERGENCY INSTRUMENT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OF
- [SDR GLBA20090918F](https://openairdocs.org/sdr/GLBA20090918F.md): Frame · cracked · Sep 16, 2009 · N255GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK IN THE AIRSTAIR DOOR LOWER FUSELAGE FRAME AT F.S. 173.41 AND STRINGER 11L. CRACK LENGTH APPROXIMATELY.750" IN LENGTH. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER FUSELAGE FRAME IAW E.O
- [SDR GLBA20090606A](https://openairdocs.org/sdr/GLBA20090606A.md): Valve · inoperative · Jun 6, 2009 · N255GL · Beech 1900D · Air Distribution System
  > PILOTS REPORTED THAT THE RT ENVIRO FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. MX REMOVED AND REPLACED THE RT PRE-COOLER VALVE IAW MM 21-11-00. THE OPS CHECK WAS GOOD.
- [SDR GLBA20090405B](https://openairdocs.org/sdr/GLBA20090405B.md): Connector · loose · Apr 5, 2009 · N255GL · Beech 1900D · Propeller/Propulsor System Wiring
  > PILOTS REPORTED THAT EXPERIENCED A DROP IN THE RIGHT HAND PROPELLER RPM AND THAT IT HAD DROOPED TO 1620 RPM ON TAKEOFF. MAINTENANCE CLEANED THE CONNECTOR ON THE RIGHT HAND PROPELLER TACH GENERATOR AND RE-INSTALLED. REFERENCE BEECH 1900 MM 77-10-00.
- [SDR GLBA20090304H](https://openairdocs.org/sdr/GLBA20090304H.md): Switch · out of adjust · Mar 3, 2009 · N255GL · Beech 1900D · Propeller Feathering/Reversing
  > FLT 5106 - ON APPROACH THE PILOTS REPORTED THAT THE NR 2 ENGINE CYCLES IN AND OUT OF FEATHER AT APPROXIAMTELY 1000 LBS. OF TORQUE AS THEY INCREASED POWER ON FINAL. THEY WERE NOT SURE OF THE N1 AT THE TIME. MAINTENANCE REMOVED AND REPLACED THE PROP OVERSPEED G
- [SDR GLBA20090228A](https://openairdocs.org/sdr/GLBA20090228A.md): Engine · out of rig · Feb 28, 2009 · N255GL · Beech 1900D · Power Lever
  > POWER LEVERS SEEM OUT OF ADJUSTMENT. THERE IS A LARGE SPLIT BETWEEN LEVERS IN FLIGHT, THE LANDING GEAR WARNING HORN GOES ON AT ABOUT 2100 LBS OF TORQUE, AND THE ENGINES IDLE AT ABOUT 74% N1 WITH THE POWER LEVERS AT IDLE. MAINTENENANCE RIGGED THE NR 1 & 2 ENG
- [SDR GLBA20090220B](https://openairdocs.org/sdr/GLBA20090220B.md): Pressure Switch · inoperative · Feb 20, 2009 · N255GL · Beech 1900D · Engine (Turbine/Turboprop)
  > ON SHORT FINAL, RT ENGINE HAD ABOUT 5 TO 6 POWER SURGES. DURING THE SURGES, RT TORQUE FLUCTUATED BETWEEN APPROX 500LB-1200LB. FIRST POWER SURGES OCCURED AT APPROX 500LB OF TORQUE AS THE F/O ADVANCED POWER ON BOTH POWER LEVERS FROM 500LB TO 700LB OF TORQUE.
- [SDR GLBA200902040](https://openairdocs.org/sdr/GLBA200902040.md): Pressure Switch · worn · Jan 25, 2009 · N255GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOTS REPORTED THAT UPON FINAL APPROACH WITH PROPELLERS FULL FORWARD IDLE POWER, THE LT ENGINE CYCLED IN AND OUT OF AUTO FEATHER WITH 500 LBS. OF TORQUE CHANGE. THE ISSUE CEASED TO OCCUR AFTER POWER WAS INCREASED. MX R&R THE LT LOW PRESSURE SWITCH IAW 61-21
- [SDR GLB2008F00012](https://openairdocs.org/sdr/GLB2008F00012.md): Wire · chafed · Jul 24, 2008 · N255GL · Beech 1900D · Landing Gear System Wiring
  > ACFT 255GL - AIR RETURN - FLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE OF TIMES AND IT WOULDN’T COME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CIRCUIT BREAKER POPPED
- [SDR GLB2008F00011](https://openairdocs.org/sdr/GLB2008F00011.md): Landing Gear · malfunctioned · Jul 24, 2008 · N255GL · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE OF TIMES AND IT WOULDN’T COME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CIRCUIT BREAKER POPPED. PUSHED IN, GEAR CAME UP
- [SDR GLB2008F00010](https://openairdocs.org/sdr/GLB2008F00010.md): Control Handle · malfunctioned · Jul 24, 2008 · N255GL · Beech 1900D · Landing Gear Selector
  > LANDING GEAR EXTENSION-AIRCRAFT N255GL FLIGHT 5212 "STL" - PILOTS REPORTED THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED WHEN GEAR HANDLE WAS PUT TO THE DOWN POSITION. RE-SET, BROUGHT GEAR UP, THE PUMP KICKED IN AND BROUGHT THE GEAR UP. WHEN PUT HANDLE BACK
- [SDR GLBA20061092](https://openairdocs.org/sdr/GLBA20061092.md): Bulkhead · cracked · Apr 25, 2008 · N255GL · Beech 1900D · Fuselage Main, Bulkhead
  > FWD PRESSURE BULKHEAD CRACKED AT FS 84.0 AT RT AVIONICS BAY AT INTERSECTION A OF ANGLE AT WL 92.0 AND STIFFNER AT RBL 15.75. MAINTENANCE REPAIRED CRACK IN FORWARD PRESSURE BULKHEAD IAW SERVICE BULLETIN STEPS 3 THROUGH 8 & STEPS 1- THROUGH 22 AT F.S. 84.0. REPA
- [SDR GLBA20061090](https://openairdocs.org/sdr/GLBA20061090.md): Angle · cracked · Apr 22, 2008 · N255GL · Beech 1900D · Fuselage Miscellaneous Structure
  > RT WING TO FUSELAGE HEAVY ANGLE CRACKED ATH FWD BEND RADIUS APPROX 1.125 INCH IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. SRM 53-90-23. REPAIR ANGLE 13.5 ". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
- [SDR GLBA20061089](https://openairdocs.org/sdr/GLBA20061089.md): Skin · corroded · Apr 22, 2008 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN CORRODED AT FS 228.25 STRINGERS 15L AND 16L. MAINTENANCE REPAIRED BELLY SKIN AT F.S. 228.25 I.A.W. BEECH 1900D SRM 51-70. REPAIR APPROXIMATELY 7.5" BY 9.5. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
- [SDR GLBA20060866](https://openairdocs.org/sdr/GLBA20060866.md): Spar · cracked · Nov 1, 2006 · N255GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABLIZER, MAIN SPAR WEB CRACKED.
- [SDR GLBA20060864](https://openairdocs.org/sdr/GLBA20060864.md): Stringer · cracked · Oct 31, 2006 · N255GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 10R CRACKED AT FS 451.00 APPROXIMATELY.5 INCH.
- [SDR GLBA20060863](https://openairdocs.org/sdr/GLBA20060863.md): Frame · cracked · Oct 31, 2006 · N255GL · Beech 1900D · Fuselage Main, Frame
  > FRAME CRACKED AT STRINGER 10R FS 451.00, APPROXIMATELY.7500 INCH.
- [SDR GLBA20060865](https://openairdocs.org/sdr/GLBA20060865.md): Skin · corroded · Oct 30, 2006 · N255GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN CORROSION ON STRINGERS 15L AND 14L FROM APPROXIMATELY FS 243.25 TO 250.75.
- [SDR GLBA20030717](https://openairdocs.org/sdr/GLBA20030717.md): Engine · failed · Sep 10, 2004 · N255GL · Beech 1900D · Engine (Turbine/Turboprop)
  > RT ENGINE FAILED ON POWER UP FOR TAKEOFF, R&R ENGINE.
- [SDR GLBA20030528](https://openairdocs.org/sdr/GLBA20030528.md): Connector · dirty · Jan 8, 2004 · N255GL · Beech 1900D · Engine RPM Indicating System
  > 104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.

Next page: https://openairdocs.org/aircraft/N255GL/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 = 'N255GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N255GL/reports

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