# Service difficulty reports: N261GL

A list on [N261GL](https://openairdocs.org/aircraft/N261GL.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 · 67 reports

- [SDR GLBA2017121800698](https://openairdocs.org/sdr/GLBA2017121800698.md): Coupling · leaking · Dec 15, 2017 · N261GL · Beech 1900D · Fuel Storage
  > CREW REPORTED THAT THERE WAS A HYDRAULIC LEAK IN THE RIGHT FRONT PART OF THE RIGHT WHEEL [WELL]. 6-7 INCH PUDDLE BUT COULD SEE NO ACTUAL DRIPS. MAINTENANCE TROUBLESHOT AND FOUND FUEL LEAKAGE AT THE RIGHT OUTBOARD WING VENT BOX TRANSFERRING TO WHEEL WELL THROUG
- [SDR GLBA2016120900623](https://openairdocs.org/sdr/GLBA2016120900623.md): Handle · corroded · Dec 8, 2016 · N261GL · Beech 1900D · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CORROSION AROUND AND THROUGH BOLTS OF INTERIOR HANDLE BELLCRANK ASSY. ON AIRSTAIR DOOR, THE BELLCRANK ATTACHMENT HAS BEEN MODIFIED BY SB 129-4020-1 USING KIT 129-4020, (ONCE THEY OPEN IT UP IT MIGHT BE A PART RE
- [SDR GLBA2016111800617](https://openairdocs.org/sdr/GLBA2016111800617.md): Frame · cracked · Nov 18, 2016 · N261GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE FRAME AT BS 183.25 BETWEEN STRINGERS 2R AND 3R CRACKED AT THE INBOARD LOWER CORNER AREA OF DUCT CUTOUT, FRAME COMPLETELY CRACKED, 2" IN LENGTH. MAJOR REPAIR.
- [SDR GLBA2015011100492](https://openairdocs.org/sdr/GLBA2015011100492.md): Elbow · cracked · Jan 11, 2015 · N261GL · Beech 1900D · Engine Oil Distribution (Airframe Furnished)
  > WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN PWR, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMCK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMS. SECURE
- [SDR GLBA2015011200492](https://openairdocs.org/sdr/GLBA2015011200492.md): Unknown · malfunctioned · Jan 11, 2015 · N261GL · Beech 1900D · Engine Oil Distribution (Airframe Furnished)
  > WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN POWER, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMER CHECK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMS
- [SDR GLBA2014070300419](https://openairdocs.org/sdr/GLBA2014070300419.md): Line · ruptured · Jul 2, 2014 · N261GL · Beech 1900D · Hydraulic System, Main
  > LANDING GEAR FAILED TO EXTEND NORMALLY, GEAR INTRANSIT LIGHT ILLUMINATED, WITH GEAR SELECTED DOWN. TRANSIT LIGHT FAILED TO EXTINGUISH NORMALLY, HYD FLUID LOW ANNUNCIATOR ILLUMINATED. PERFORMED MANUAL GEAR EXTENSION, GEAR IND WERE NORMAL. ON LANDING, FOUND
- [SDR GLBA2013102300344](https://openairdocs.org/sdr/GLBA2013102300344.md): Stringer · corroded · Oct 23, 2013 · N261GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 AT FS 243.25, RUNS APPROX 6 INCHES. REPAIRED IAW EO 13-1900-53-075. MAJOR REPAIR.
- [SDR GLBA2013102200343](https://openairdocs.org/sdr/GLBA2013102200343.md): Skin · corroded · Oct 22, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORRODED AT FS 243.25 AND STRINGER 16. REPAIRED IAW EO 13-1900-53-076. MAJOR REPAIR.
- [SDR GLBA2013082100295](https://openairdocs.org/sdr/GLBA2013082100295.md): Skin · damaged · Aug 20, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CHAFED, FWD OF FS 370.25 BETWEEN STRINGER 15--16L. REPAIRED IAW EO 13-1900-53-056.
- [SDR GLBA2013082100298](https://openairdocs.org/sdr/GLBA2013082100298.md): Skin · damaged · Aug 20, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND STRINGER 15L FLANGE DAMAGED AT 2 LOCATIONS FROM THE VENT BLOWER BRACKET, CHAFED AT FS 368.25 AND 370.25, CHAFED HALF WAY THROUGH STRINGER FLANGE. REPAIRED IAW EO 13-1900-53-056. MAJOR REPAIR.
- [SDR GLBA2013082100297](https://openairdocs.org/sdr/GLBA2013082100297.md): Skin · damaged · Aug 20, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND STRINGER 16 CHAFED AT FOUR LOCATIONS FROM THE VENT BLOWER DUCT HARDWARE-SCREWS, DAMAGE AT TOP OF STRINGER BETWEEN BS 370.25 AND 378.25. REPAIRED IAW. EO 13-1900-53-056. MAJOR REPAIR.
- [SDR GLBA2013082100296](https://openairdocs.org/sdr/GLBA2013082100296.md): Skin · damaged · Aug 20, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AT FS 368.25 - 370.25 HAS TWO HOLES WORN THRU SKIN, HOLES NEXT TO STRINGER 15L, FWD AREA, HOLE J SHAPED IS.85" IN LENGTH, AFT WORN AREA HOLE IS.3" IN LENGTH. REPAIRED AREA IAW EO 13-1900-53-056. MAJOR REPAIR.
- [SDR GLBA2013052000251](https://openairdocs.org/sdr/GLBA2013052000251.md): Skin · cracked · May 20, 2013 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT LOWER BELLY SKIN OVER THE WING SPAR AT FS 288, 2.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-041. MAJOR REPAIR.
- [SDR GLBA2013051600250](https://openairdocs.org/sdr/GLBA2013051600250.md): Spar Cap · cracked · May 15, 2013 · N261GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE SPAR CAP, RT VERT STAB, SECOND FASTENER DOWN FROM THE TOP,.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-015. MAJOR REPAIR.
- [SDR GLBA2013051600249](https://openairdocs.org/sdr/GLBA2013051600249.md): Rib · chafed · May 15, 2013 · N261GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND CHAFED AREA ON THE LT RIB 1 AT JUNCTION WITH WING SPAR, FLANGE PORTION OF RIB 1 WORN DOWN TO DOUBLER FLANGE, 1.5"*.75" AREA. REPAIRED IAW EO 13-1900-57-011. MAJOR REPAIR.
- [SDR GLBA2013051600248](https://openairdocs.org/sdr/GLBA2013051600248.md): Frame · cracked · May 15, 2013 · N261GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AT THE INTERSECTION OF LONGERON UNDER RT FINGER DOUBLER,.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-040. MAJOR REPAIR.
- [SDR GLBA2013011400150](https://openairdocs.org/sdr/GLBA2013011400150.md): Diode · failed · Jan 12, 2013 · N261GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INST EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE INSTRUMENT EMERGENCY LIGHT SWITCH. MX REPLACED DIODES, OPS CHECKED GOOD.
- [SDR GLBA2013010800148](https://openairdocs.org/sdr/GLBA2013010800148.md): Fuse · inoperative · Jan 7, 2013 · N261GL · Beech 1900D · Indicating/Recording System
  > PILOT REPORTED THAT THE EMERGENCY INSTRUMENT LIGHTS ARE INOPERATIVE. MX REPLACED THE HOT BATTERY FUSE, OPS CHECKED GOOD.
- [SDR GLBA2012112600117](https://openairdocs.org/sdr/GLBA2012112600117.md): Current Limiter · failed · Nov 26, 2012 · N261GL · Beech 1900D · Air Conditioning System
  > PILOT REPORTED THAT 2 MINUTES INTO CRUISE, HAD SMOKE AND FUMES IN COCKPIT AND COMING FROM THE EYEBALL VENTS IN CABIN, CLOSED LT BLEED AIR AND SMOKE CLEARED, DECLARED EMERGENCY, LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE CURRENT LIMITER AND AFT BLOWER, OP
- [SDR GLBA2012111200105](https://openairdocs.org/sdr/GLBA2012111200105.md): Bulb · missing · Nov 9, 2012 · N261GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT BULB IS MISSING. MX REPLACED THE BULB, OPS CK GOOD.
- [SDR GLBA2012091700057](https://openairdocs.org/sdr/GLBA2012091700057.md): Skin · cracked · Sep 17, 2012 · N261GL · Beech 1900D · Vertical Stabilizer, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE VERTICAL STAB RT SIDE AFT LWR SPAR SKIN 8.5" UP FROM BOTTOM, 3" IN LENGTH. REPAIRED IAW EO 12-1900-55-038. MAJOR REPAIR.
- [SDR GLBA2012091700056](https://openairdocs.org/sdr/GLBA2012091700056.md): Attach Fitting · cracked · Sep 17, 2012 · N261GL · Beech 1900D · Elevator Tab, Attach Fittings
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SPAR CAP ON VERTICAL STAB AT HORIZONTAL STAB ATTACHMENT FITTING AT 2ND FASTENER FROM TOP, VSS 84.10 AT 20 PERCENT CHORD,.875" IN LENGTH. REPAIRED IAW FR-CO-02526, REV 1, STEP 1. MAJOR REPAIR.
- [SDR GLBA2012022102](https://openairdocs.org/sdr/GLBA2012022102.md): Spar · cracked · Feb 21, 2012 · N261GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND 4 CRACKS ON THE HORIZONTAL STAB REAR SPAR WEB AROUND ACCESS HOLE AT HSS. 00.0. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO
- [SDR GLBA20120214F](https://openairdocs.org/sdr/GLBA20120214F.md): Skin · corroded · Feb 14, 2012 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSP FOUND BELLY CORROSION AT FS 198.25 BETWEEN STRINGER 15 AND 16L, AREA BETWEEN A DOUBLE ROW OF FASTENERS, AREA.75" BY.5". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-011. MATERIALS U
- [SDR GLBA20120214G](https://openairdocs.org/sdr/GLBA20120214G.md): Door Frame · cracked · Feb 14, 2012 · N261GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE A/S DOOR ENTRANCE LOWER FRAME CRACKED IN THE AFT CORNER AT FS 176 AND STRINGER 11L,.1250" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 12-1900-53-010. MATERIALS UT
- [SDR GLBA201112052](https://openairdocs.org/sdr/GLBA201112052.md): Door · open · Dec 2, 2011 · N261GL · Beech 1900D · Emergency Exits
  > DURING THE PASSENGER BRIEFING (WITH ENGINES NOT RUNNING), A PASSENGER OPENED UP THE 6C EMERGENCY EXIT DOOR. MX REINSTALLED THE EMERGENCY EXIT DOOR.
- [SDR GLBA20111027G](https://openairdocs.org/sdr/GLBA20111027G.md): Seal · dirty · Oct 26, 2011 · N261GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR WAS SQUEELING IN FLIGHT. MX CLEANED THE DOOR SEAL, PRESSURIZATION CHECKS GOOD, OK FOR SERVICE.
- [SDR GLBA20110420G](https://openairdocs.org/sdr/GLBA20110420G.md): Door Frame · cracked · Apr 19, 2011 · N261GL · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER GARGO DOOR FUSELAGE FRAME AT FS 460 AND STRINGER 3L CRACKED 1.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53
- [SDR GLBA20110214F](https://openairdocs.org/sdr/GLBA20110214F.md): Blower · worn · Feb 13, 2011 · N261GL · Beech 1900D · Air Distribution Fan
  > PILOT REPORTED THAT WHEN BLOWER IS PLACED TO AUTO, IT GAVE OFF AN ELECTRICAL ODOR, WHEN TURNED OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE FORWARD BLOWER ASSY IAW AIM 21-02 AND CW CORROSION INSPECTION.
- [SDR GLBA201010311](https://openairdocs.org/sdr/GLBA201010311.md): Bulb · missing · Oct 31, 2010 · N261GL · Beech 1900D · Passenger Compartment Lighting
  > PILOT REPORTED THAT ONE OF THERE EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE IS MISSING A BULB. MAINTENANCE REPLACED THE MISSING BULB PN 1864 AND FILTER PN D165-100-2 IAW BMM 33-10-04, OPERATIONAL CHECKS GOOD.
- [SDR GLBA201009141](https://openairdocs.org/sdr/GLBA201009141.md): Engine · low torque · Sep 14, 2010 · N261GL · Beech 1900D · Engine (Turbine/Turboprop)
  > INCREASING POWER ON APPROACH, LT ENGINE REMAINED AROUND 500 LBS TORQUE, DID NOT RESPOND TO POWER LEVER INPUT WHILE RT ENGINE SPOOLED TO APPROX 1200 TORQUE. LT ENGINE AUTOFX TRIGGERED AND TOOK APPROX 2-3 INCHES OF POWER LEVER MOVEMENT TO GET LT ENGINE TO RESPON
- [SDR GLBA20100830F](https://openairdocs.org/sdr/GLBA20100830F.md): Skin · cracked · Aug 30, 2010 · N261GL · Beech 1900D · Emergency Exits
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE LOWER FWD SKIN ON THE 6A EMERGENCY EXIT DOOR, 1.2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-52-005. MATERIALS UTILIZED A
- [SDR GLBA20100827F](https://openairdocs.org/sdr/GLBA20100827F.md): Frame · cracked · Aug 27, 2010 · N261GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A THE CARGO PARTITION FUSELAGE ATTACH POINT HOLES ARE WORN, TOP LEFT, TOP CENTER, AND TOP RIGHT. MAINTENANCE INSPECTED AND FOUND THE REPAIR TO BE A MINOR REPAIR - REPAIRED PARTITION ATTACH POINTS, TOP, T
- [SDR GLBA20100826G](https://openairdocs.org/sdr/GLBA20100826G.md): Frame · cracked · Aug 26, 2010 · N261GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK ON THE LT HEAVY FRAME ANGLE AT FS 288 FWD BEND RADIUS, 1.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-053. MATERIALS UTILIZED
- [SDR GLBA20100309G](https://openairdocs.org/sdr/GLBA20100309G.md): Skin · dented · Mar 8, 2010 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO 10-1
- [SDR GLBA100307001](https://openairdocs.org/sdr/GLBA100307001.md): Skin · dented · Mar 7, 2010 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO10-1900-53-008. MATE
- [SDR GLBA20090921G](https://openairdocs.org/sdr/GLBA20090921G.md): Door Latch · lack of lube · Sep 18, 2009 · N261GL · Beech 1900D · Emergency Exits
  > DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 6C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR I.A.W. BMM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND I.A.W. 52-20-01 STEP D FOR LUBING. NO RIGG
- [SDR GLBA20090921F](https://openairdocs.org/sdr/GLBA20090921F.md): Door · stiff · Sep 18, 2009 · N261GL · Beech 1900D · Emergency Exits
  > DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 4C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR IAW MM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND IAW 52-20-01 STEP D FOR LUBING. NO RIGGING WAS
- [SDR GLBA20090512F](https://openairdocs.org/sdr/GLBA20090512F.md): Handle · misaligned · May 12, 2009 · N261GL · Beech 1900D · Landing Gear Selector
  > FLT 5091 - ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE J-HOOK DID RELEASE. THEY TRIED A COUPLE TIME TO GET THE GEAR TO COME UP. MAINTENANCE RE-STOWED THE EMERGENCY HANDLE AND INSPECTED THE LT AND RIGHT SAFETY SWITCHES. GEAR SWIN
- [SDR GLBA20090420G](https://openairdocs.org/sdr/GLBA20090420G.md): Frame · cracked · Apr 16, 2009 · N261GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED STRUCTURAL CHECK, MX DISCOVERED A CRACK ON THE RT HEAVY ANGLE AT FA 288.0. LENGTH OF CRACK APPROX 1.5 INCH LONG. MX REPAIRED THE RT HEAVY ANGLE AT FA 288.0. IAW. EO-09-1900-53-003. REPAIR AREA APPROXIMATELY 13.5 INCH LONG OUT OF PN 114-430
- [SDR GLBA20090420F](https://openairdocs.org/sdr/GLBA20090420F.md): Skin · cracked · Apr 16, 2009 · N261GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED STRUCTURAL CHECK MX DISCOVERED A CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25. CRACK APPROXIMATELY 2.250 INCHES IN LENGTH. MX REPAIRED THE CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOT
- [SDR GLBA20061085](https://openairdocs.org/sdr/GLBA20061085.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N NR 129-440044-75.
- [SDR GLBA20061087](https://openairdocs.org/sdr/GLBA20061087.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-71.
- [SDR GLBA20061086](https://openairdocs.org/sdr/GLBA20061086.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73
- [SDR 20061087](https://openairdocs.org/sdr/20061087.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS. 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. PN 129-440044-71.
- [SDR 20061086](https://openairdocs.org/sdr/20061086.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73.
- [SDR 20061085](https://openairdocs.org/sdr/20061085.md): Frame · bent · Mar 28, 2008 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N 129-40044-75.
- [SDR GLBA20061009](https://openairdocs.org/sdr/GLBA20061009.md): Hinge Fitting · damaged · Oct 8, 2007 · N261GL · Beech 1900D · Cargo/Baggage Doors
  > CARGO DOOR HINGE HALF FORWARD AND AFT LUGS MISSING AND SEVERAL LOOSE RIVETS. MAINTENANCE REPLACED HINGE HALF ON CARGO DOOR IAW SRM 52-90. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. IWO NR 94171, L/P NR 207464.
- [SDR GLBA20061007](https://openairdocs.org/sdr/GLBA20061007.md): Stringer Splice · corroded · Oct 1, 2007 · N261GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > BELLY CORROSION FOUND AT APPROXIMATELY FS 246 TO FS 250 ON STRINGER 15R. MAINTENANCE REPLACED DAMAGED STRINGER SECTION PER ENGINEERING ORDER 07-UE261-01. APPROXIMATE STRINGER REPLACEMENT 15" WITH 11" NEW STRINGER SPLICE. PART NUMBER 131686. RII INSPECTION COM
- [SDR GLBA20061008](https://openairdocs.org/sdr/GLBA20061008.md): Frame · cracked · Oct 1, 2007 · N261GL · Beech 1900D · Fuselage Main, Frame
  > FRAME CRACKED AT STRINGER CUTOUT FS 177 AT STRINGER 9AR. REPAIRED FRAME AT STRINGER RELIEF HOLE FS 177 AND STRINGER 9AR IAW 1900D SRM 51-70. REPAIR DIMENSIONS 4.5 BY 2.5. 2024 T-3.080. RII COMPLIED WITH IAW TASKCARD 8.2.1.

Next page: https://openairdocs.org/aircraft/N261GL/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 = 'N261GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N261GL/reports

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