# Service difficulty reports: N257GL

A list on [N257GL](https://openairdocs.org/aircraft/N257GL.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 · 68 reports

- [SDR GLBA2016081000603](https://openairdocs.org/sdr/GLBA2016081000603.md): Tire · flat · Aug 9, 2016 · N257GL · Beech 1900D · Tire
  > PILOT REPORTED THAT DURNG LANDING ROLL OUT, IT BECAME HARD TO KEEP THE ACFT ON THE CENTERLINE. AFTER EXITING THE RUNWAY, CAPTAIN SAW THAT BOTH LT MAIN TIRES WERE FLAT. OPEN.
- [SDR GLBA2015040300510](https://openairdocs.org/sdr/GLBA2015040300510.md): Brake · frozen · Apr 2, 2015 · N257GL · Beech 1900D · Brake
  > PILOT REPORTED THAT AFTER DE-ICING THE BRAKES FELT VERY INEFFECTIVE, VERY WEEK STOPPING ACTION, EVEN WHEN APPLIED FIRMLY. MX BRAKES FROZE UP, UNFROZE BRAKES BY APPLYING DE-ICE FLUID. OPERATIONS CHECKED GOOD IAW MM 32-40-00.
- [SDR GLBA2014022800388](https://openairdocs.org/sdr/GLBA2014022800388.md): Actuator · faulty · Feb 26, 2014 · N257GL · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT ON APPROACH TO LANDING WITH LG HANDLE IN THE DOWN POSITION, ONLY NOSE & RT MAIN GEAR GREEN LIGHTS ILLUMINATED. LG RELAY CB TRIPPED, RAN ALL APPROPRIATE CHECKLISTS & LANDING GEAR MANUALLY EXTENDED NORMALLY. MX R & R THE LT MAIN ACTUATOR IA
- [SDR GLBA2013121700361](https://openairdocs.org/sdr/GLBA2013121700361.md): Structure · cracked · Dec 17, 2013 · N257GL · Beech 1900D · Emergency Exits
  > DURING A SCHEDULED INSPECTION, FOUND EMERGENCY EXIT 4C LOWER AFT CORNER OF BONDED ASSEMBLY, CRACKED APPROXIMATELY 1 5/8 INCHES. REPAIRED IAW EO 13-1900-52-003.
- [SDR GLBA2013121800362](https://openairdocs.org/sdr/GLBA2013121800362.md): Skin · debonded · Dec 17, 2013 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN BETWEEN STRINGER 15-16L BS 290 CORRODED & DEBONDED. REPAIRED IAW EO 13-1900-53-081.
- [SDR GLBA2013121300355](https://openairdocs.org/sdr/GLBA2013121300355.md): Spar · cracked · Dec 13, 2013 · N257GL · Beech 1900D · Wing Spar
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT INBD WING INBD RT FLANGE ANGLE AT FS 288.00 & WING SPAR, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-57-020.
- [SDR GLBA2013121300356](https://openairdocs.org/sdr/GLBA2013121300356.md): Rib · cracked · Dec 13, 2013 · N257GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT INBD WING RIB & FLANGE ANGLE. REPAIRED IAW EO 13-1900-57-021.
- [SDR GLBA2013121300357](https://openairdocs.org/sdr/GLBA2013121300357.md): Stringer · cracked · Dec 13, 2013 · N257GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN STRINGER 9L AT BULKHEAD BS 588.1 THAT HAVE CONVERGED TO FORM A TRIANGLE SHAPED PIECE, 1.3 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-57-020.
- [SDR GLBA2013121300358](https://openairdocs.org/sdr/GLBA2013121300358.md): Stringer · cracked · Dec 13, 2013 · N257GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE STRINGER 9R AT BULKHEAD BS 588.1, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-079.
- [SDR GLBA2013121300359](https://openairdocs.org/sdr/GLBA2013121300359.md): Frame · cracked · Dec 13, 2013 · N257GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME FLANGE BS 107 STRINGER 8R. THE CRACK RADIATES TO THE END OF THE FRAME & DOWN APPROXIMATELY.3 INCHES FROM THE UPPER FASTENER,.9 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-080.
- [SDR GLBA2013041100229](https://openairdocs.org/sdr/GLBA2013041100229.md): Door · misinstalled · Apr 10, 2013 · N257GL · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE EMERGENCY DOOR AT 6C WAS NOT PROPERLY SEATED. MX REINSTALLED THE EMER DOOR.
- [SDR GLBA2013040900228](https://openairdocs.org/sdr/GLBA2013040900228.md): Cable · broken · Apr 9, 2013 · N257GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. MX REPLACED THE LOWER FWD AIRSTAIR DOOR ACTUATOR CABLE, OPS CHECKED GOOD.
- [SDR GLBA2013040800228](https://openairdocs.org/sdr/GLBA2013040800228.md): Cable · broken · Apr 9, 2013 · N257GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. OPEN
- [SDR GLBA2013030500196](https://openairdocs.org/sdr/GLBA2013030500196.md): Stringer · cracked · Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN A STRINGER AT FS 588.1 AND STRINGER 9R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-022. MAJOR REPAIR.
- [SDR GLBA2013030500195](https://openairdocs.org/sdr/GLBA2013030500195.md): Bulkhead · damaged · Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND BULKHEAD AT FS 588.1 DAMAGED JUST UNDER STRINGER 8R, PROTRUDING OUT OF A RIVET APPROX.25". REPAIRED IAW EO 13-1900-53-021. MAJOR REPAIR.
- [SDR GLBA2013030500194](https://openairdocs.org/sdr/GLBA2013030500194.md): Frame · cracked · Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS AT FS 588.1 STRINGER 9L, 1.25 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-019. MAJOR REPAIR.
- [SDR GLBA2013030500193](https://openairdocs.org/sdr/GLBA2013030500193.md): Skin · cracked · Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 588.1 STRINGER 8L, PROTRUDING UPWARD, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-020. MAJOR REPAIR.
- [SDR GLBA2013030100191](https://openairdocs.org/sdr/GLBA2013030100191.md): Skin · damaged · Mar 1, 2013 · N257GL · Beech 1900D · Horizontal Stabilizer, Plate/Skin
  > RT ELEVATOR OTBD EDGE & OTBD T/E DAMAGE APPROX 13" X 15.5". T/E ALSO BUCKLED JUST INBD OF OTBD HINGE ATTACH POINT APPROX 4" X 7". REPAIRED IAW TC 1900-2730.00. MAJOR REPAIR.
- [SDR GLBA2012111400109](https://openairdocs.org/sdr/GLBA2012111400109.md): Spar Cap · cracked · Nov 13, 2012 · N257GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE TOP TWO RIVETS, 1.25" IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-057. MAJOR REPAIR.
- [SDR GLBA2012111400110](https://openairdocs.org/sdr/GLBA2012111400110.md): Spar Cap · cracked · Nov 13, 2012 · N257GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE TOP TWO RIVETS, 2 INCHES IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-056. MAJOR REPAIR.
- [SDR GLBA201206151](https://openairdocs.org/sdr/GLBA201206151.md): Pump · failed · Jun 14, 2012 · N257GL · Beech 1900D · Fuel Boost Pump
  > LT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. TURNED ON THE STANDBY PUMP AND THE ANNUNCIATOR WENT OUT. NO FUEL LEAK NOTED ON POST FLIGHT. MX REPLACED THE LT LOW PRESSURE PUMP IAW BMM 73-10-00, OPS CHECKED GOOD.
- [SDR GLBA2012060401](https://openairdocs.org/sdr/GLBA2012060401.md): Frame · cracked · Jun 1, 2012 · N257GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT SIDEWALL FS 456 AND STRINGER 10R, FRAME AT STRINGER CUTOUT,.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-032. MAJOR REPAIR
- [SDR GLBA2012053101](https://openairdocs.org/sdr/GLBA2012053101.md): Frame · cracked · May 31, 2012 · N257GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 456 BETWEEN STRINGER 3 & 4L, FWD CARGO DOOR CUTOUT. REPAIRED IAW EO 12-1900-53-031. MAJOR REPAIR
- [SDR GLBA2012050101](https://openairdocs.org/sdr/GLBA2012050101.md): Spar · cracked · Apr 28, 2012 · N257GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB AFT SPAR WEB, CRACKS RADIATE FROM LIGHTNING HOLE AT 2, 5, 7& 10 O'CLOCK POSITIONS, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1
- [SDR GLBA20120109F](https://openairdocs.org/sdr/GLBA20120109F.md): Frame · corroded · Jan 7, 2012 · N257GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON THE FRAME AT FS 228.25 APPROX 2" INBD OF STRINGER 14R NEXT TO AN EXISTING REPAIR. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-002. MATERIALS UTILIZED ARE INCLUDED
- [SDR GLBA20111222F](https://openairdocs.org/sdr/GLBA20111222F.md): Cable · torn · Dec 21, 2011 · N257GL · Beech 1900D · Passenger/Crew Doors
  > SIG EVENT - PILOT REPORTED THAT THE AIR STAIR DOOR ROPE HAS TORN RUBBER SHEATHING. MX REPLACED THE UPPER AFT CABLE IAW BMM 52-10-02, PN: 1440-40GLA.
- [SDR GLBA201109011](https://openairdocs.org/sdr/GLBA201109011.md): Wire · damaged · Aug 1, 2011 · N257GL · Beech 1900D · Light System Wiring
  > CABIN LIGHT PARTIAL OPERATION. MAINTENANCE REPAIRED WIRES TO D436 SPLICE TO 4C AND 6C EMERGENCY LIGHTS IAW BMM 33-20-00, OPS CHECKED GOOD.
- [SDR GLBA20110413F](https://openairdocs.org/sdr/GLBA20110413F.md): Skin · delaminated · Apr 13, 2011 · N257GL · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND EROSION DAMAGE TO THE TOP OF L/E TIP OF THE RT WINGLET, DELAMENATION ON THE INBD SIDE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-003. MATERIALS UTILIZED
- [SDR GLBA20100105F](https://openairdocs.org/sdr/GLBA20100105F.md): Frame · cracked · Jan 5, 2011 · N257GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 303 IN THE BEND RADIUS, 1.1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-064 AND EO 11-1900-53-001. MATERIALS UTILIZ
- [SDR GLBA20101229F](https://openairdocs.org/sdr/GLBA20101229F.md): Angle · cracked · Dec 29, 2010 · N257GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MX FOUND A 1.5" CRACK IN THE BEND RADIUS AT THE RT HEAVY ANGLE AT FS 288. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP EO 10-1900-53-064. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA201002181](https://openairdocs.org/sdr/GLBA201002181.md): Relay · failed · Feb 18, 2010 · N257GL · Beech 1900D · Landing Gear Retraction/Extension System
  > UPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR DID NOT EXTEND AND THE CIRCUIT BREAKER POPPED. THEY THEN PERFORMED A MANUAL EXTENSION. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE HYDRAULIC POWER PACK WOULD NOT SHUT OFF CAUSING THE CIRCUIT BREA
- [SDR GLBA20090901F](https://openairdocs.org/sdr/GLBA20090901F.md): Skin · corroded · Aug 28, 2009 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING ROUTINE SCHEDULED MX CORROSION WAS FOUND ON THE BELLY SKIN BETWEEN STR 15L AND 15R AT FS 243.25. MAINTENANCE REMOVED CORROSION AND REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-0015. RII INSPECTION COMPLIED WITH IAW EO 09-1900-53-0015. INSPECTION SATISF
- [SDR GLBA20090831F](https://openairdocs.org/sdr/GLBA20090831F.md): Skin · cracked · Aug 28, 2009 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON THE SKIN DOME AT FS 150 BETWEEN STR 1 AND 2 R. CRACK APPROX.3 INCH IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA OF THE DOME SKIN AT F.S. 150 IAW EO 09-1900-53-013. RII INSPECTION COMPLIED WITH IAW EO 09
- [SDR GLBA20090828G](https://openairdocs.org/sdr/GLBA20090828G.md): Stringer · cracked · Aug 26, 2009 · N257GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK 2.9 INCHES WAS FOUND ON THE BELLY SKIN AT F.S. 303.25 2 INCHES INBOARD FROM RIGHT HAND EDGE OF BELLY SKIN PANEL. REPAIRED THE AFFECTED AREA AT F.S. 243.25 AND CUT AND SPLICED THE STRINGER IAW EO 09-
- [SDR GLBA20090828F](https://openairdocs.org/sdr/GLBA20090828F.md): Skin · cracked · Aug 25, 2009 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK 2.9 INCHES WAS FOUND ON THE BELLY SKIN AT F.S. 303.25 2 INCHES INBOARD FROM RIGHT HAND EDGE OF BELLY SKIN PANEL. MAINTENANCE REPAIRED THE AFFECTED AREA AT F.S. 303.25 I.A.W. E.O. 09-1900-53-012. RII
- [SDR GLBA200905031](https://openairdocs.org/sdr/GLBA200905031.md): Bulb · burned out · May 3, 2009 · N257GL · Beech 1900D · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AN INSTRUMENT EMERGENCY LIGHT WAS FOUND BURNED OUT. MAINTANENANCE REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA200904282](https://openairdocs.org/sdr/GLBA200904282.md): Annunciator · false activation · Apr 28, 2009 · N257GL · Beech 1900D · Door Warning System
  > CABIN DOOR ANNUNCIATOR ILLUMINATED DURING TAXI OUT AND ONTO RUNWAY. TAKEOFF ABORTED. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECK OF CABIN DOOR ANNUNCITOR. NO DEFECTS NOTED THIS CLEARS DML 34909 ALL PLACARD REMOVED. REF MM 52-70-00.
- [SDR GLBA20090326F](https://openairdocs.org/sdr/GLBA20090326F.md): Skin · dented · Mar 23, 2009 · N257GL · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - LT OUTBOARD WING LEADING EDGE BIRDSTRIKE REPAIR AT APPROXIMATELY WS 281 TO 301. DENT APPROXIMATELY 5/8TH INCH DEEP. MAINTENANCE REPAIRED THE LT OUTBAORD LEADING EDGE AT WS 281 TO 301 IAW EO 09-UE257-01. SKIN REPAIRED OUT OF PN 118-110047-81.
- [SDR GLBA20090227C](https://openairdocs.org/sdr/GLBA20090227C.md): Squat Switch · dirty · Feb 27, 2009 · N257GL · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT 5189 - PILOTS REPORTED THAT AFTER TAKEOFF THE STALL HEAT ANNUNCIATOR ILLUMINATED AND THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND SQUAT SWITCH IAW MM 32-60-05. NO DEFECTS WERE NOTED AND THE OPERATIONAL CH
- [SDR GLBA200811121](https://openairdocs.org/sdr/GLBA200811121.md): Skin · dented · Nov 3, 2008 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING ROUTINE DAILY LINE ENVIRONMENT CONDITIONS A TUG COLLIDED WITH THE AIRCRAFT LEAVING FOUR DENTS BELOW THE CARGO DOOR BETWEEN FS 447.0 TO APPROXIMATELY FS 472.7 BETWEEN STRINGER 11L & 12L. MAINTENANCE REPAIRED AFT FUSELAGE SKIN BETWEEN FS 4
- [SDR GLBA20061068](https://openairdocs.org/sdr/GLBA20061068.md): Skin · corroded · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. MAINT REPAIRED BELLY SKIN 15R TO 13L AT/FROM FS 213.25 TO FS 228.25 IAW SRM 51-70. REPAIR DIMENSION 26.250 INCHES X 33.5
- [SDR GLBA20061067](https://openairdocs.org/sdr/GLBA20061067.md): Frame · cracked · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 177.35 AND STR 9R CRACKED APPROX.500 INCHES IN LENGTH. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR**
- [SDR GLBA20061066](https://openairdocs.org/sdr/GLBA20061066.md): Frame · cracked · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 163.97 AND STR 9L CRACKED APPROX.40 INCH IN LENGTH. RII REQUIRED TC 8.2.1. MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE F.S. 163.97 AND STRINGER 9L IAW SRM 51-70. REPAIR APPROX 5 INCHES X 2.7 INCHES. 2024-T3.071. RII C/W IAW TC 8.2.1
- [SDR GLBA20061065](https://openairdocs.org/sdr/GLBA20061065.md): Skin · corroded · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY CORROSION FS 213.25 AND FS 228.25 AT STRINGERS 15R, 16R, 14L/13L AT FS 213.25 AND 15L/14L AT FS 228.25. MAINT REPAIRED DEBONDED STR 15R,15L,14L, FOR FS 213.25 TO FS 228.25 IAW SRM 53-90. STR REPAIR DIMENSIONS APPROX 10.5 INCHES. 2024 T-3. RII C/W IAW TA
- [SDR 20061068](https://openairdocs.org/sdr/20061068.md): Skin · corroded · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. OPEN
- [SDR 20061067](https://openairdocs.org/sdr/20061067.md): Frame · cracked · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 177.35 AND STRINGER 9R CRACKED APPROX.500 INCH IN LENGTH. OPEN
- [SDR 20061066](https://openairdocs.org/sdr/20061066.md): Frame · cracked · Feb 11, 2008 · N257GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 163.97 AND STR 9R CRACKED APPROX.40 INCH IN LENGTH - RII REQUIRED TC 8.2.1. OPEN
- [SDR GLBA20060833](https://openairdocs.org/sdr/GLBA20060833.md): Angle · cracked · Oct 5, 2006 · N257GL · Beech 1900D · Fuselage Miscellaneous Structure
  > RT HEAVY DOUBLERS CRACKED (ANGLE) AT F.S. 288.0 PN NR 114-430002-7180 (RT)
- [SDR GLBA20060840](https://openairdocs.org/sdr/GLBA20060840.md): Stringer · cracked · Oct 5, 2006 · N257GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 8R - 8L CRACKED, CANTED BULKHEAD F.S. 588.10 - REPAIR PENDING
- [SDR GLBA20060832](https://openairdocs.org/sdr/GLBA20060832.md): Skin · corroded · Oct 5, 2006 · N257GL · Beech 1900D · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON BELLY OF AIRCRAFT FS 223-75 TO 232.75, 3.5 INCHES O/B OF STRINGER 15R TO 4 INCHES LEFT OF STRINGER 16, REPAIR PENDING.

Next page: https://openairdocs.org/aircraft/N257GL/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 = 'N257GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N257GL/reports

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