# Service difficulty reports: N122GL, cancelled Sep 5, 2014

A list on [N122GL, cancelled Sep 5, 2014](https://openairdocs.org/deregistered/N122GL-2014-09-05.md).

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

- [SDR HSYA2012113012](https://openairdocs.org/sdr/HSYA2012113012.md): Wire · broken · Nov 30, 2012 · N122GL · Beech 1900C · Landing Gear System Wiring
  > PILOT REPORTED DURING A MX CHECK FLIGHT THAT THE GEAR REMAINED DOWN WITH ALL THREE GREEN LIGHTS ILLUMINATED WHEN THE GEAR HANDLE WAS MOVED TO THE UP POSITION. ACFT RETURNED TO DEPARTURE UNEVENTFULLY. MX TROUBLESHOT THE GEAR SYS AND THE FOLLOWING MX WAS PERFO
- [SDR HSYA2010110310](https://openairdocs.org/sdr/HSYA2010110310.md): Landing Gear · malfunctioned · Nov 3, 2010 · N122GL · Beech 1900C · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT -COME UP-AFTER CYCLING THE GEAR STILL WOULD NOT COME UP AND WAS STILL INDICATING 3 GREEN IN THE DOWN POSITION. CREW ADVISED THE TOWER AND DECLARED AN EMERGENCY TO LAND. ACFT LANDED WITH NO FURTHER INCIDENT. MX
- [SDR HSYA2010060210](https://openairdocs.org/sdr/HSYA2010060210.md): Cable · loose · Jun 2, 2010 · N122GL · Beech 1900C · Power Lever
  > AFTER ROTATION, CAPTAIN REPORTED AN UNCOMMANDED RT ENGINE AUTO FEATHER. THE ACFT RETURNED TO THE AIRPORT WITHOUT FURTHER INCIDENT ARRIVING BACK IN THE BLOCKS FOR MX TROUBLESHOOTING AND EVALUATION AT 1355Z. MX TROUBLESHOT ACFT AND FOUND BETA VALVE OUT OF ADJUST
- [SDR HSYA2010050810](https://openairdocs.org/sdr/HSYA2010050810.md): Vent · contaminated · May 8, 2010 · N122GL · Beech 1900C · Air Distribution System
  > PILOT REPORTED TO MX AFTER LANDING, THAT A BURNING PLASTIC/RUBBER SMELL IN CABIN WITH BLEEDS ON, CABIN TEMP SET TO COLD. MX TROUBLESHOT ACFT AND FOUND RUBBISH UNDER PILOT SEAT AIR VENT. REMOVED RUBBISH AND CLEANED AIR VENT IAW MM 12-20-00. MX OPS CHECKS PERFOR
- [SDR HSYA2009082109](https://openairdocs.org/sdr/HSYA2009082109.md): Engine · malfunctioned · Aug 21, 2009 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)
  > ON ROTATION RT ENG TORQUE WENT TO 4000 LBS. FOR APPROXIMATELY 2 SECONDS. ENG STARTED TO AUTOFEATHER & PILOT PULLED THROTTLE BACK & SHUTDOWN ENG. PERFORM A BORESCOPE INSPECTION OF ENGINE, NO DEFECTS NOTED. PERFORMED REMOVAL & INSPECTION OF OIL FILTER & HOUSING
- [SDR HSYA20070702](https://openairdocs.org/sdr/HSYA20070702.md): Airstair · cracked · Jul 1, 2007 · N122GL · Beech 1900C · Entrance Stairs
  > DURING PREFLIGHT INSPECTION, CREW REPORTED A CRACK ON THE AIRSTAIR DOOR NEAR THE HINGE. MX FOUND A CRACK ON THE INNER DOOR SKIN NEAR THE AFT END DOOR HINGE. UPON INITIATION OF A REPAIR TO AFFECTED AREA, MX FOUND CORROSION ON THE INNER DOOR SKIN, CLOSURE AND ME
- [SDR HSY2005F00002](https://openairdocs.org/sdr/HSY2005F00002.md): Hose · leaking · Jan 24, 2005 · N122GL · Beech 1900C · Hydraulic System, Main
  > (MRR NR 02-012405) LOSS OF HYDRAULIC PRESSURE AND QUANTITY LED TO THE INABILITY TO OPERATE THE LANDING GEAR WITH NORMAL PROCEDURES. LANDING GEAR HAD TO BE EXTENDED MANUALLY WITH THE HAND PUMP. NOTE: THIS WAS A PILOT TRAINING FLIGHT ONLY. FAILED LANDING GEAR
- [SDR GLBA20030617](https://openairdocs.org/sdr/GLBA20030617.md): Circuit Breaker · tripped · Apr 26, 2004 · N122GL · Beech 1900C · Landing Gear System
  > GEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOOD
- [SDR GLBA2001149](https://openairdocs.org/sdr/GLBA2001149.md): Cam · worn · Jul 7, 2001 · N122GL · Beech 1900C · Trailing Edge Flap Control System
  > FLAPS WOULD NOT RETRACT ON T/O. REPLACED SAFETY SWITCH CAM.
- [SDR GLBA2001038](https://openairdocs.org/sdr/GLBA2001038.md): Elevator · flutter · Feb 15, 2001 · N122GL · Beech 1900C · Elevator Control System
  > PILOT REPORTED ELEVATOR FLUTTER ON DESCENT AND CLIMB. INSPECTED FLIGHT CONTROLS, PERFORMED TEST FLIGHT. COULD NOT DUPLICATE, OPS CHECKED GOOD. RETURNED TO SERVICE.
- [SDR GLBA2001011](https://openairdocs.org/sdr/GLBA2001011.md): Cowling · separated · Jan 24, 2001 · N122GL · Beech 1900C · Nacelle/Pylon, Plate/Skin
  > RETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWLING. RETURNED TO SERVICE.
- [SDR 20010112SG041](https://openairdocs.org/sdr/20010112SG041.md): Altimeter · malfunctioned · Dec 2, 2000 · N122GL · Beech 1900C · Altimeter, Barometric/Encoder
  > CAPTAINS ALTIMETER STUCK AT 10,200 FEET, AIR TURN BACK. CAPTAINS ALTIMETER REMOVED AND REPLACED. SYSTEM TESTED OK. (M)
- [SDR 20010112SG038](https://openairdocs.org/sdr/20010112SG038.md): Altimeter · failed · Nov 30, 2000 · N122GL · Beech 1900C · Altimeter, Barometric/Encoder
  > CAPTAINS ALTIMETER FLAGGED AND ALTITUDE ALERTER FAILED AFTER TAKEOFF. RETURNED TO AIRPORT. CAPTAINS. CAPTAINS ALTIMETER WAS REMOVED AND REPLACED. TESTED OK. (M)
- [SDR GLBA97064](https://openairdocs.org/sdr/GLBA97064.md): Downlock Switch · out of adjust · Apr 8, 1997 · N122GL · Beech 1900C · Landing Gear Position and Warning
  > SPI - GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH IN FLIGHT. MAINTENANCE ADJUSTED NOSE GEAR DOWNLOCK SWITCH. (M)
- [SDR GLBA96233](https://openairdocs.org/sdr/GLBA96233.md): Uplock Switch · failed · Nov 26, 1996 · N122GL · Beech 1900C · Landing Gear Position and Warning
  > SPI - AFTER RETRACTION, RED INTRANSIT LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK SWITCH. ALL SWITCHES WERE LATER ADJUSTED. TEST FLIGHT SATISFACTORY. (X)
- [SDR GLBA96170](https://openairdocs.org/sdr/GLBA96170.md): Truss · cracked · Jul 31, 1996 · N122GL · Beech 1900C · Engine Mount Section
  > SPI - RIGHT TRUSS CRACKED AT AREA 'A'. REMOVED AND REPLACED RIGHT TRUSS. (M)
- [SDR GLBA96151](https://openairdocs.org/sdr/GLBA96151.md): Windshield · arcing · Jul 12, 1996 · N122GL · Beech 1900C · Windshield/Door Rain/Ice Removal
  > MBL - AT 10,000 FEET DURING MODERATE RAIN, SMOKE IN COCKPIT WITH WINDSHIELD FUEL VENTS, ALT STATIC, PITOT AND STALL HEAT ON AND THE ENGINE ANTI-ICE ON. MAINTENANCE DEFERRED WINDSHIELD HEAT IAW MEL 30-7. FOUND RIGHT WINDSHIELD GROUND BLOCK PULLED AWAY FROM WI
- [SDR GLBA96111](https://openairdocs.org/sdr/GLBA96111.md): Actuator · failed · Jun 3, 1996 · N122GL · Beech 1900C · Landing Gear Actuator
  > ORD - LEFT MLG SLOW TO INDICATE DOWN AND LOCKED. REMOVED AND REPLACED LEFT MLG ACTUATOR. OPS CHECKS GOOD. (X)
- [SDR GLBA96099](https://openairdocs.org/sdr/GLBA96099.md): Downlock Switch · failed · May 24, 1996 · N122GL · Beech 1900C · Landing Gear Position and Warning
  > ORD - CREW SELECTED GEAR DOWN, BUT RECEIVED NO 'DOWN AND LOCKED' INDICATION ON LT GEAR. ON SECOND ATTEMPT, LT GEAR LIGHT ILLUMINATED AND CREW LANDED UNEVENTFULLY. MAINTENANCE REMOVED LT GEAR DOWNLOCK SWITCH. OPS CHECK WAS GOOD. (X)
- [SDR GLBA96090](https://openairdocs.org/sdr/GLBA96090.md): Aileron · damaged · May 12, 1996 · N122GL · Beech 1900C · Ailerons
  > ORD -CREW FOUND DAMAGE ON TRAILING EDGE OF LEFT AILERON DURING WALK AROUND INSPECTION. MAINTENANCE REMOVED AND REPLACED LEFT AILERON. FLIGHT TEST WAS GOOD. (M)
- [SDR GLBA96004](https://openairdocs.org/sdr/GLBA96004.md): Warning System · activated · Feb 5, 1996 · N122GL · Beech 1900C · Landing Gear Position and Warning
  > UC-122 HAD FLAPS IN TAKEOFF POSITION, GEAR DOWN AND LOCKED WITH 3 GREEN INDICATED. THE RED LIGHTS ILLUMINATED IN THE GEAR HANDLE AND AURAL WARNING SOUNDED. THE AIRCRAFT WAS FERRIED TO SPI FROM ORD FOR REPAIRS. THE GEAR SWING COMPLETED IN SPI REVEALED NO DUP
- [SDR GLBA96027](https://openairdocs.org/sdr/GLBA96027.md): Warning System · malfunctioned · Jan 31, 1996 · N122GL · Beech 1900C · Landing Gear Position and Warning
  > OSH - CREW REPORTED THAT THE GEAR INTRANSIT LIGHT AND HORN WOULD NOT EXTINGUISH WHEN GEAR SELECTED UP. CREW ELECTED TO DO AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE JACKED AIRCRAFT AND PEFORMED FOUR COMPLETE GEAR SWING CYCLES. SYSTEM OPS C
- [SDR 96ZZZM78](https://openairdocs.org/sdr/96ZZZM78.md): Elevator · damaged · Nov 14, 1995 · N122GL · Beech 1900C · Elevator Structure
  > DEN - AIRCRAFT NR 159GL AND N122GL, CONTACTED ELEVATORS ON THE GROUND. MAINTENANCE REPLACED THE RIGHT ELEVATOR DUE TO TIP DAMAGE. (M)
- [SDR 95ZZZM513](https://openairdocs.org/sdr/95ZZZM513.md): Engine · failed · Aug 30, 1995 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)
  > ORD-BRL - FLT NR 5927 - THE LEFT ENGINE FAILED AND WAS SECURED. THE CREW DIVERTED TO GBC ON SINGLE ENGINE AND COMPLETED AND UNEVENTFUL LANDING. MAINTENANCE CHANGED ENGINES. SUSPECT BEARING FAILURE. (M)
- [SDR 95ZZZX1964](https://openairdocs.org/sdr/95ZZZX1964.md): Skin · cracked · Mar 21, 1995 · N122GL · Beech 1900C · Vertical Stabilizer
  > SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND DORSAL FIN CRACKED ON LT SIDE AT REAR PRESSURE BULKHEAD ATTACH POINT. THE CRACK WAS BETWEEN TWO RIVET HOLES. INSTALLED REPAIR IAW BEECH 1900 SRM 51-70-00, PAGE 17.
- [SDR 95ZZZX1963](https://openairdocs.org/sdr/95ZZZX1963.md): Truss · cracked · Mar 20, 1995 · N122GL · Beech 1900C · Engine Mount Section
  > SPW - DURING SCHEDULED VISUAL INSPECTION REQUIRED BY AD 95-02-18 IAW BEECH SB 2255R6, AREA OF THE RT ENGINE TRUSS WAS FOUND CRACKED. REPLACED TRUSS WITH SERVICEABLE.

## 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 = 'N122GL' AND deregistration_id = 'N122GL-2014-09-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N122GL-2014-09-05/reports

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