# Service difficulty reports: N170GL

A list on [N170GL](https://openairdocs.org/aircraft/N170GL.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 · 95 reports

- [SDR TIMA2020090982003](https://openairdocs.org/sdr/TIMA2020090982003.md): Governor · leaking · Aug 29, 2020 · N170GL · Beech 1900D · Engine Oil Indicating System
  > LEVELED OFF IN CRUISE AT 14000' STARTED CRUISE CHECKS AND NOTICED OIL PRESS ON NR 2 ENGINE AT 60 PSI. PRESSURE EVENTUALLY DROPPED BELOW 60, SHUT DOWN ENGINE, MADE EMERGENCY LANDING IN BIL.
- [SDR GLBA2017082400681](https://openairdocs.org/sdr/GLBA2017082400681.md): Cable · worn · Aug 22, 2017 · N170GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE UPPER AFT DOOR CABLE NEEDS TO BE REPLACED. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE IAW MM 52-10-01.
- [SDR GLBA2017041800649](https://openairdocs.org/sdr/GLBA2017041800649.md): Pin · broken · Apr 17, 2017 · N170GL · Beech 1900D · Entrance Stairs
  > MAINTENANCE REPORTED THAT THE LOWER AIRSTAIR DOOR STRUT PIN WAS BROKEN. REMOVED AND REPLACED THE LOWER DOOR SNUBBER BRACKET ASSEMBLY (P/N: 129-514117-9) BY REMOVING ATTACHING HARDWARE BY TURNING ALL SCREWS COUNTER-CLOCKWISE UNTIL REMOVED AND SLIDING THE BRACKE
- [SDR GLBA2015122100561](https://openairdocs.org/sdr/GLBA2015122100561.md): Bolt · unsecure · Dec 20, 2015 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT A BOLT FELL OUT OF THE AIR STAIR DOOR COUNTER BALANCE. REPLACED THE BOLT & WASHER.
- [SDR GLBA2015092200548](https://openairdocs.org/sdr/GLBA2015092200548.md): Bulkhead · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Fuselage Main, Bulkhead
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 2 CRACKS AT CANT BULKHEAD, AT FS 588.10 AT JUNCTION WITH STRINGER 8R, CANT BULKHEAD AT FIRST FASTENER TOP SIDE AT STRINGER 8R & AT FIRST FASTENER BELOW STRINGER 8R, BOTTOM CRACK RADIATES UPWARD & DOWNWARD FROM
- [SDR GLBA2015092200547](https://openairdocs.org/sdr/GLBA2015092200547.md): Skin · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT BELLY SKIN AT APPROX FS 303.25 & BL 29.06, 1.25" IN LENGTH. REPAIRED IAW EO 15-1900-53-017.
- [SDR GLBA2015092200546](https://openairdocs.org/sdr/GLBA2015092200546.md): Skin · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 3 CRACKS IN THE LT FUSELAGE SKIN, AT THE LT VORTEX GENERATOR, LOCATED BETWEEN FS 232.25 & 248.25, LOCATED AT THE BOTTOM OF STRINGER 12L, TOTAL 3.35" IN LENGTH. REPAIRED IAW EO 15-1900-53-016.
- [SDR GLBA2015092200545](https://openairdocs.org/sdr/GLBA2015092200545.md): Skin · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Emergency Exits
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK AT THE EMERGENCY EXIT 6A SKIN, AT THE INNER LOWER FWD CORNER,.55" IN LENGTH. REPAIRED IAW EO 15-1900-52-001.
- [SDR GLBA2015092200544](https://openairdocs.org/sdr/GLBA2015092200544.md): Skin · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE SKIN CRACKED AT FS 100.500, JUST BELOW FIRST OFFICERS WINDSHIELD, BOTTOM OTBD CORNER,.625" IN LENGTH. REPAIRED IAW EO 15-1900-53-15.
- [SDR GLBA2015092200543](https://openairdocs.org/sdr/GLBA2015092200543.md): Skin · cracked · Sep 22, 2015 · N170GL · Beech 1900D · Emergency Exits
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EMERGENCY EXIT 6C SKIN, CRACKED AT THE INNER LOWER AFT CORNER,.8" INCHES LENGTH. REPAIRED IAW EO 15-1900-52-002.
- [SDR V0DR20150922003](https://openairdocs.org/sdr/V0DR20150922003.md): Cover · worn · Sep 22, 2015 · N170GL · Beech 1900D · Fuel Injector Nozzle
  > FUEL NOZZLE SHEATHS HAVE SIGNS OF CONTACTING THE TOP OF THE FUEL NOZZLE & THE SHEATH DOME AREA.
- [SDR GLBA2015092100542](https://openairdocs.org/sdr/GLBA2015092100542.md): Bulkhead · dented · Sep 21, 2015 · N170GL · Beech 1900D · Fuselage Main, Bulkhead
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND DENTS AT BULKHEAD AT FS 84.00, BETWEEN THE FIRST & SECOND DOUBLER FROM THE LT OTBD EDGE. DENT AREA IS 4" FROM LT TO RT & 6.7" UP & DOWN, DEEPEST DENTED AREA MEASURES AT APPROX.23". ALSO FOUND TWO SMALL DENT
- [SDR GLBA2015091800541](https://openairdocs.org/sdr/GLBA2015091800541.md): Door Frame · cracked · Sep 18, 2015 · N170GL · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE AIRSTAIR DOOR FRAME LOWER FWD CORNER AREA, FS 150 & STRINGER 11L, IS CRACKED APPROX.50 INCHES IN LENGTH. CRACK RADIATES OTBD FROM THE CUT OUT. THE CUT OUT IS APPROX 3 INCHES UPWARD FROM THE LOWER E
- [SDR GLBA2015091800540](https://openairdocs.org/sdr/GLBA2015091800540.md): Angle · cracked · Sep 18, 2015 · N170GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE ANGLE LOCATED AT FS 150.60 IS CRACKED IN AN AREA AT THE AIRSTAIR DOOR STRUT UPPER MOUNT BRACKETS, LOWER AFT SCREW HOLE. REPAIRED IAW EO 15-1900-53-009.
- [SDR GLBA2015091800539](https://openairdocs.org/sdr/GLBA2015091800539.md): Skin · cracked · Sep 18, 2015 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INNER SKIN AT FS 150.60, BETWEEN STRINGERS 7L & 6L IS CRACKED, APPROX 1.5" IN LENGTH AT THE AIR STAIR DOOR STRUT'S UPPER MOUNT BRACKETS, LOWER AFT ATTACHING SCREW HOLE ACCESS. SUPPLEMENTAL INFORMATION WIL
- [SDR GLBA2015091000535](https://openairdocs.org/sdr/GLBA2015091000535.md): Skin · corroded · Sep 10, 2015 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 243.25 & STRINGER 15L. REPAIRED IAW EO 15-1900-52-012.
- [SDR GLBA2015091000534](https://openairdocs.org/sdr/GLBA2015091000534.md): Frame · cracked · Sep 9, 2015 · N170GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK ON THE FWD FRAME FLANGE AT FS 177.35 BETWEEN STRINGER 14L & 13L, 1" IN LENGTH. REPAIRED IAW EO 15-1900-53-011.
- [SDR GLBA2014111700465](https://openairdocs.org/sdr/GLBA2014111700465.md): Control Cable · broken · Nov 14, 2014 · N170GL · Beech 1900D · Aileron Control System
  > PILOT REPORTED THAT THE RUDDER AILERON INTERCONNECT CABLE BROKE. REPLACED THE AILERON RUDDER INTERCONNECT CABLE PN NAS323-13-0250 IAW MM 27-10-08.
- [SDR GLBA2013092600324](https://openairdocs.org/sdr/GLBA2013092600324.md): Wire Harness · damaged · Sep 25, 2013 · N170GL · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT WITH ANTI-SKID ON BRAKES TOTALLY INOPERATIVE. BRAKES WORK NORNALLY WITH ANTI-SKID OFF. FOUND LT TRANSDUCER HARMESS DAMAGED. R & R WIRE HARNESS AND TRANSDUCER CONNECTIONS IAW AIM 14 PARA 14.3.9 OPS CHECKED GOOD.
- [SDR GLBA2013070100266](https://openairdocs.org/sdr/GLBA2013070100266.md): Motor · inoperative · Jun 28, 2013 · N170GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND WHEN GEAR HANDLE WAS SELECTED TO DOWN POSITION, NO INTRANSIT LIGHT INDICATION AND NO GREEN LIGHTS, RAN CHECKLIST AND MANUALLY EXTENDED GEAR. MX R & R THE POWER PACK MOTOR AND TIME DELAY PCB, OPS CHECKED GO
- [SDR GLBA2012122400143](https://openairdocs.org/sdr/GLBA2012122400143.md): Skin · corroded · Dec 22, 2012 · N170GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSP FOUND BELLY SKIN CORROSION AT FS 228.25 AND STRINGER 16. REPAIRED IAW EO 12-1900-53-076. MAJOR REPAIR
- [SDR GLBA2012122400142](https://openairdocs.org/sdr/GLBA2012122400142.md): Stringer · corroded · Dec 22, 2012 · N170GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND STRINGER 16 CORRODED BETWEEN FS 228.25 AND 213.25. REPAIRED IAW EO 12-1900-53-077. MAJOR REPAIR.
- [SDR GLBA2012122000137](https://openairdocs.org/sdr/GLBA2012122000137.md): Attach Angle · cracked · Dec 20, 2012 · N170GL · Beech 1900D · Wing, Attach Fittings
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING, LOWER INBD ATTACH ANGLE, JUST FWD OF FWD WING SPAR AT BL 29, 1.1" IN LENGTH. REPAIRED IAW EO 12-1900-57-012. MAJOR REPAIR.
- [SDR GLBA2012122000136](https://openairdocs.org/sdr/GLBA2012122000136.md): Web · cracked · Dec 20, 2012 · N170GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB, 0.125" IN LENGTH. REPAIRED IAW EO 12-1900-558-070. MAJOR REPAIR.
- [SDR GLBA2012122000135](https://openairdocs.org/sdr/GLBA2012122000135.md): Spar Cap · cracked · Dec 20, 2012 · N170GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE RT SPAR CAP ON VERTICAL STAB AT TOP HOLE,.5" IN LENGTH. REPAIRED IAW EO 12-1900-55-069. MAJOR REPAIR.
- [SDR GLBA2012091800063](https://openairdocs.org/sdr/GLBA2012091800063.md): Spar Cap · cracked · Sep 18, 2012 · N170GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE, (1) RADIATES UPWARD FROM THE UPPER FASTENER TO THE EDGE OF THE SPAR CAP ANGLE, RADIATES DOWNWARD FROM THE SECOND FASTENER, VSS 84.10 AT 20 PERCENT CHORD,.875"
- [SDR GLBA201208131](https://openairdocs.org/sdr/GLBA201208131.md): Bulb · burned out · Aug 13, 2012 · N170GL · Beech 1900D · Instrument Panel
  > CAPTAIN'S SIDE INSTRUMENT EMERGENCY LIGHTS BURNED OUT AND 1 INST INDIRECT LIGHT BULB. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2012032300001](https://openairdocs.org/sdr/GLBA2012032300001.md): Damper · worn · Mar 22, 2012 · N170GL · Beech 1900D · Nose/Tail Landing Gear
  > EXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TO AT APPX V1. CONTINUED UNTIL SHORTLY AFTER GEAR RETRACTION. MX REPLACED THE NLG TIRE IAW TC 1900-3240.00 AND REPLACED SHIMMY DAMPER IAW MM 32-20-03.
- [SDR GLBA2012032301](https://openairdocs.org/sdr/GLBA2012032301.md): Spar · cracked · Mar 22, 2012 · N170GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0,.73" IN LENGTH.
- [SDR GLBA20111025F](https://openairdocs.org/sdr/GLBA20111025F.md): Placard · dislodged · Oct 24, 2011 · N170GL · Beech 1900D · Placards and Markings
  > PILOT REPORTED THAT THE EMERGENCY PLACARD FELL OFF AT 3C. MX REPLACED THE PLACARD IAW AIM 5-16-0.
- [SDR GLBA20111003G](https://openairdocs.org/sdr/GLBA20111003G.md): Seal · leaking · Oct 1, 2011 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE DOOR SEAL IS LEAKING IN FLIGHT. MX SEAL, LEAK CHECKED GOOD IAW BMM 52-10-06.
- [SDR GLBA20111003F](https://openairdocs.org/sdr/GLBA20111003F.md): Seal · worn · Sep 30, 2011 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SEAL MAKES EXCESSIVE NOISE WITH CABIN PRESSURIZED ABOVE 3.5 PSID. MX INSPECTED AND FOUND A BAD SEAL ON THE NR1 ADF ANTENNA, REPLACED SEAL, IAW TC 1900-3411.00-3, LEAK CHECKS GOOD.
- [SDR GLBA20110914002](https://openairdocs.org/sdr/GLBA20110914002.md): Seal · failed · Sep 14, 2011 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SQUEALS IN FLIGHT. EXCESSIVE AMOUNT OF SEALANT ON DOOR SEAL, REMOVED SEALANT AND RESEALED THE DOOR SEAL, IAW BMM 52-10-04.
- [SDR GLBA20110913002](https://openairdocs.org/sdr/GLBA20110913002.md): Cable · damaged · Sep 13, 2011 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE UPPER DOOR CABLE SHEATHING IS PEALING. MX REPLACED THE CABLE IAW BMM 52-10-02.
- [SDR GLBA20110913001](https://openairdocs.org/sdr/GLBA20110913001.md): Seal · unsecure · Sep 13, 2011 · N170GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SQUEALS IN FLIGHT. MX RESECURED THE DOOR SEAL IAW BMM 52-10-04.
- [SDR GLBA20110816F](https://openairdocs.org/sdr/GLBA20110816F.md): Frame · cracked · Aug 16, 2011 · N170GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE FRAME AT FS 183.25 AND STRINGER CUTOUT 9AR,.3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-051 MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR
- [SDR GLBA20110711G](https://openairdocs.org/sdr/GLBA20110711G.md): Solenoid · dirty · Jul 9, 2011 · N170GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT WHEN THE POWER IS PULLED BACK TO IDLE DURING THE FLARE THE NR 2 PROP STAYS AT 1700 RPM AND WHILE THE NR 1 COMES DOWN THROUGH 1600 RPM. MX CLEANED, INSP, AND LUBED THE FLIGHT IDLE STOP SOLENOID, OPS CHECKED GOOD IAW RUN SHEET, ALL CHECKS GO
- [SDR GLBA20110711F](https://openairdocs.org/sdr/GLBA20110711F.md): Solenoid · dirty · Jul 8, 2011 · N170GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT WHEN THE POWER IS PULLED BACK TO IDLE DURING THE FLARE THE NR 2 PROP STAYS AT 1700 RPM AND WHILE THE NR 1 COMES DOWN SLOWLY. MX CLEANED THE LOW PITCH SOLENOID, PERFORMED ENGINE RUN SHEET 1900-RUN-WORKSHEET FEG 212, OPS CK GOOD.
- [SDR V0DR2011007](https://openairdocs.org/sdr/V0DR2011007.md): Bearing · seized · Apr 8, 2011 · N170GL · Beech 1900D · Air Distribution Fan
  > DURING SCHEDULED BRUSH, CHANGE THE REPAIR THE TECH NOTED NOISE FROM THE BEARINGS. INSP REVEALED THE ARMATURE, 1 OF THE (COMMUTATOR END) BEARINGS HAD FAILED. A VISUAL INSP OF THE BEARING REVEALED THE GREASE HAD SEEPED PAST THE SEALED AREA AND THE BEARING WOUL
- [SDR GLBA20101028A](https://openairdocs.org/sdr/GLBA20101028A.md): Autofeather Sys · malfunctioned · Oct 28, 2010 · N170GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THE THE RIGHT ENGINE CYCLED IN AND OUT OF FEATHER MULTIPLE TIMES ON SHORT FINAL, STARTED WITH TORQ AT 1K AND STOPPED WHEN BROUGHT ABOVE 2K TORQ, N1 AT 90-91% AT THAT TIME. MAINTENANCE INSPECTED THE LOW PITCH SOLONOID IAW MM 61-20-00, PERFORMED O
- [SDR GLBA201008232](https://openairdocs.org/sdr/GLBA201008232.md): Holder · failed · Aug 20, 2010 · N170GL · Beech 1900D · Light System Wiring
  > RT SIDE INST EMERGENCY LIGHTS DO NOT TURN ON WITH SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.
- [SDR GLBA201008201](https://openairdocs.org/sdr/GLBA201008201.md): Holder · corroded · Aug 20, 2010 · N170GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE RT SIDE INSTRUMENT EMERGENCY LIGHTS DO NOT TURN ON WITH THE SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.
- [SDR GLBA20100315F](https://openairdocs.org/sdr/GLBA20100315F.md): Frame · cracked · Mar 15, 2010 · N170GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE BEND RADIUS OF A FRAME AT FS 451 JUST ABOVE STRINGER 10R. CRACK IS APPROX.9" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-012. MATER
- [SDR GLBA20100315G](https://openairdocs.org/sdr/GLBA20100315G.md): Frame · cracked · Mar 15, 2010 · N170GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN A FRAME AT FS 456 AND STR 10R. CRACK IS APPROX.3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-011. MATERIALS UTILIZED ARE INCLUDED IN
- [SDR GLBA20100312H](https://openairdocs.org/sdr/GLBA20100312H.md): Angle · cracked · Mar 12, 2010 · N170GL · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING ROUTINE SCHEDULED MX THE RT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.3" IN LENGTH. A CRACK AT FS 303 WAS ALSO PRESENT.5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL
- [SDR GLBA2010312G](https://openairdocs.org/sdr/GLBA2010312G.md): Angle · cracked · Mar 12, 2010 · N170GL · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W EO 10-190
- [SDR GLBA100312002](https://openairdocs.org/sdr/GLBA100312002.md): Angle · cracked · Mar 12, 2010 · N170GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE THE LEFT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FORWARD END OF THE ANGLE AT F.S. 288.0. THE CRACK IS APPROXIMATELY 1.5" IN LENGTH.
- [SDR GLBA20100312F](https://openairdocs.org/sdr/GLBA20100312F.md): Skin · debonded · Mar 12, 2010 · N170GL · Beech 1900D · Passenger/Crew Doors
  > DURING ROUTINE SCHEDULED MX THE AIRSTAIR DOOR AREA FROM THE TOP STEP HINGE TO THE LOWER EDGE. THE INNER SKIN IS DEBONDED. MX R & R THE AIRSTAIR DOOR BOND ASSY IAW MM 52-10-03.
- [SDR GLBA200909292](https://openairdocs.org/sdr/GLBA200909292.md): Switch · faulted · Sep 29, 2009 · N170GL · Beech 1900D · Landing Gear Retraction/Extension System
  > AIR TURNBACK - PILOTS REPORTED THAT UPON TAKEOFF AND CLIMBING THAT THE GEAR HANDLE IN TRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE NOSE AND RIGHT HAND MAIN UPLOCK SWITCHES. MAINTENANCE RIGGED THE SWITCHES AND T
- [SDR GLBA20090409G](https://openairdocs.org/sdr/GLBA20090409G.md): Switch · dirty · Apr 8, 2009 · N170GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOTS REPORTED THAT THE RT ENGINE NR 2 PROPELLER VIOLENTLY CYCLES IN AND OUT OF FEATHER. PROPS WERE FULL FWD, IDLE SLOWLY INCREASING, CAUSED YAWING AT 1500 FT ON APPROACH. MX CLEANED POWER LEVER AUTOFEATHER MICROSWITCHES AND PERFORMED OPSL CHECK OF AUTOFEATHE

Next page: https://openairdocs.org/aircraft/N170GL/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 = 'N170GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N170GL/reports

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