N122GL, cancelled Sep 5, 2014

Service difficulty reports · 26

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR HSYA2012113012Wire · brokenPILOT 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 PERFONov 30, 2012 · N122GL · Beech 1900C · Landing Gear System WiringSDR HSYA2010110310Landing Gear · malfunctionedAFTER 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 Nov 3, 2010 · N122GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR HSYA2010060210Cable · looseAFTER 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 ADJUSTJun 2, 2010 · N122GL · Beech 1900C · Power LeverSDR HSYA2010050810Vent · contaminatedPILOT 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 PERFORMay 8, 2010 · N122GL · Beech 1900C · Air Distribution SystemSDR HSYA2009082109Engine · malfunctionedON 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 Aug 21, 2009 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)SDR HSYA20070702Airstair · crackedDURING 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 MEJul 1, 2007 · N122GL · Beech 1900C · Entrance StairsSDR HSY2005F00002Hose · leaking(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 GEARJan 24, 2005 · N122GL · Beech 1900C · Hydraulic System, MainSDR GLBA20030617Circuit Breaker · trippedGEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOODApr 26, 2004 · N122GL · Beech 1900C · Landing Gear SystemSDR GLBA2001149Cam · wornFLAPS WOULD NOT RETRACT ON T/O. REPLACED SAFETY SWITCH CAM.Jul 7, 2001 · N122GL · Beech 1900C · Trailing Edge Flap Control SystemSDR GLBA2001038Elevator · flutterPILOT REPORTED ELEVATOR FLUTTER ON DESCENT AND CLIMB. INSPECTED FLIGHT CONTROLS, PERFORMED TEST FLIGHT. COULD NOT DUPLICATE, OPS CHECKED GOOD. RETURNED TO SERVICE.Feb 15, 2001 · N122GL · Beech 1900C · Elevator Control SystemSDR GLBA2001011Cowling · separatedRETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWLING. RETURNED TO SERVICE.Jan 24, 2001 · N122GL · Beech 1900C · Nacelle/Pylon, Plate/SkinSDR 20010112SG041Altimeter · malfunctionedCAPTAINS ALTIMETER STUCK AT 10,200 FEET, AIR TURN BACK. CAPTAINS ALTIMETER REMOVED AND REPLACED. SYSTEM TESTED OK. (M)Dec 2, 2000 · N122GL · Beech 1900C · Altimeter, Barometric/EncoderSDR 20010112SG038Altimeter · failedCAPTAINS ALTIMETER FLAGGED AND ALTITUDE ALERTER FAILED AFTER TAKEOFF. RETURNED TO AIRPORT. CAPTAINS. CAPTAINS ALTIMETER WAS REMOVED AND REPLACED. TESTED OK. (M)Nov 30, 2000 · N122GL · Beech 1900C · Altimeter, Barometric/EncoderSDR GLBA97064Downlock Switch · out of adjustSPI - GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH IN FLIGHT. MAINTENANCE ADJUSTED NOSE GEAR DOWNLOCK SWITCH. (M)Apr 8, 1997 · N122GL · Beech 1900C · Landing Gear Position and WarningSDR GLBA96233Uplock Switch · failedSPI - AFTER RETRACTION, RED INTRANSIT LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK SWITCH. ALL SWITCHES WERE LATER ADJUSTED. TEST FLIGHT SATISFACTORY. (X)Nov 26, 1996 · N122GL · Beech 1900C · Landing Gear Position and WarningSDR GLBA96170Truss · crackedSPI - RIGHT TRUSS CRACKED AT AREA 'A'. REMOVED AND REPLACED RIGHT TRUSS. (M)Jul 31, 1996 · N122GL · Beech 1900C · Engine Mount SectionSDR GLBA96151Windshield · arcingMBL - 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 WIJul 12, 1996 · N122GL · Beech 1900C · Windshield/Door Rain/Ice RemovalSDR GLBA96111Actuator · failedORD - LEFT MLG SLOW TO INDICATE DOWN AND LOCKED. REMOVED AND REPLACED LEFT MLG ACTUATOR. OPS CHECKS GOOD. (X)Jun 3, 1996 · N122GL · Beech 1900C · Landing Gear ActuatorSDR GLBA96099Downlock Switch · failedORD - 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)May 24, 1996 · N122GL · Beech 1900C · Landing Gear Position and WarningSDR GLBA96090Aileron · damagedORD -CREW FOUND DAMAGE ON TRAILING EDGE OF LEFT AILERON DURING WALK AROUND INSPECTION. MAINTENANCE REMOVED AND REPLACED LEFT AILERON. FLIGHT TEST WAS GOOD. (M)May 12, 1996 · N122GL · Beech 1900C · AileronsSDR GLBA96004Warning System · activatedUC-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 DUPFeb 5, 1996 · N122GL · Beech 1900C · Landing Gear Position and WarningSDR GLBA96027Warning System · malfunctionedOSH - 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 CJan 31, 1996 · N122GL · Beech 1900C · Landing Gear Position and WarningSDR 96ZZZM78Elevator · damagedDEN - AIRCRAFT NR 159GL AND N122GL, CONTACTED ELEVATORS ON THE GROUND. MAINTENANCE REPLACED THE RIGHT ELEVATOR DUE TO TIP DAMAGE. (M)Nov 14, 1995 · N122GL · Beech 1900C · Elevator StructureSDR 95ZZZM513Engine · failedORD-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)Aug 30, 1995 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZX1964Skin · crackedSPW - 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.Mar 21, 1995 · N122GL · Beech 1900C · Vertical StabilizerSDR 95ZZZX1963Truss · crackedSPW - 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.Mar 20, 1995 · N122GL · Beech 1900C · Engine Mount Section
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