N45GL

Service difficulty reports not matched to an aircraft · 41

They name N45GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N45GL' AND registry_match IS NULL
  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 051003Circuit Breaker · inoperativePILOT REPORTED THAT HE HAD TO MANUALY EXTEND THE LANDING GEAR.May 10, 2003 · N45GL · Beech 1900C · Landing Gear System WiringSDR 2004F00019Spring · brokenLOW FUEL PRESSURE LIGHT CAME ON IN FLT, ELECTRIC BOOST PUMP WAS TURNED ON AND EXTINGUISHED LIGHT. MAINTENANCE REMOVED THE LOW PRESSURE FUEL PUMP AND FOUND THE DRIVESHAFT HAD SHEARED. THE PUMP WAS REPLACED. DISASSEMBLY OF THE PUMP DISCLOSED THAT THE POPPET VJan 21, 2003 · N45GL · Beech 1900C · Fuel Injector NozzleSDR 2004F00023Actuator · failedON LANDING IN AKN, NOSE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. FERRY TO ANCHORAGE AFTER VERIFYING GEAR DOWN AND LOCKED, GREEN LIGHT CAME ON DURING TAXI OUT. COULD NOT DUPLICATE FAILURE ON GROUND. REPLACED NOSE GEAR ACTUATOR FOR T/S. (M)Dec 24, 2002 · N45GL · Beech 1900C · Landing Gear ActuatorSDR 2004F00016Relay · contaminatedON APPROACH TO LANDING IN ANCHORAGE, THE PILOT SELECTED LANDING GEAR DOWN TWICE WITH NO EFFECT. THE GEAR WAS EXTENDED MANUALLY AND THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE CONFIRMED THAT THE HYDRAULIC PUMP RELAY WAS FREEZING, HIGH MOISTURE CONTENT IN UNDec 3, 2002 · N45GL · Beech 1900C · Landing Gear System WiringSDR 2004F00013Connector · damagedAT LANDING IN ANCHORAGE, PILOT REPORTED MLG WAS SLOW TO GO DOWN, THE LANDING GEAR WARNING HORN WOULD NOT SILENCE AND INTRANSIT LIGHTS REMAINED ON WITH THREE GREEN SAFE LIGHTS ALSO ON. MAINTENANCE COULD NOT DUPLICATE. REPLACED PCB FOR WARNING HORN FAULT, RESENov 21, 2002 · N45GL · Beech 1900C · Landing Gear System WiringSDR ACE0822021Relay · contaminatedON APPROACH TO LANDING, THE LANDING GEAR WOULD NOT NORMALLY EXTEND. THE FLIGHT CREW USED THE ALTERNATE HAND PUMP FOR EXTENSION AND PERFORMED AND UNEVENTFUL LANDING. MAINTENANCE CONFIRMED THAT THE LANDING GEAR HYDRAULIC MOTOR RELAY WOULD FREEZE AND NOT OPERATAug 26, 2002 · N45GL · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR YAD2003F00002Connector · shortedDURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHT TURNED ON. TROUBLESHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. ALSO DISCOVERED THAT THE ELEVATOR ELECTRIC TRIM SERVO WIAug 20, 2002 · N45GL · Beech 1900C · Exterior LightingSDR ACE0820021Connector · shortedDURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHTS TURNED ON, TROUBLE SHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. DISCOVERED THAT THE ELEVATOR ELECTRIC TRIM SERVO WIRES TAug 20, 2002 · N45GL · Beech 1900C · Light System WiringSDR ACE0729021Oil Cooler · crackedMAINTENANCE FOUND OIL LEAKING FROM THE RIGHT ENGINE COWLING. INVESTIGATION REVEALED A CRACKED OIL COOLER. OIL COOLER WAS REPLACED. THE REMOVED OIL COOLER WAS INSPECTED AND A CRACK ALONG THE END PLATE WELD SEEM WAS LOCATED. THIS DEFECT IS COMMON WITH THIS PJul 31, 2002 · N45GL · Beech 1900C · Engine Oil CoolerSDR ACE0603021Relay · burnedON APPROACH, THE LANDING GEAR WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY, GIVING THREE GREEN SAFE INDICATIONS. MOMENTS AFTER GETTING THE GEAR DOWN AND SAFE INDICATION, THE LANDING GEAR PUMP CIRCUIT BREAKER POPPED. THE AIRCRAFT MADE AN UNEVENTFUL LANDINJun 4, 2002 · N45GL · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR ACE0510021Windshield · crackedON CLIMB OUT, RT WINDSHIELD CRACKED. AIRCRAFT IMMEDIATELY RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. WINDSHIELD REPLACED.May 10, 2002 · N45GL · Beech 1900C · Flight Compartment WindowsSDR ACE0206021Downlock Switch · inoperativePILOT REPORTED THAT ON APPROACH TO ANCHORAGE, WHEN THE LANDING GEAR WAS SELECTED DOWN. THE NOSE GEAR, GREEN DOWN AND LOCK LAMP FAILED TO ILLUMINATE (THE GEAR UNSAFE LIGHTS WERE NOT ILLUMINATED). THE GEAR WAS CYCLED AND AFTER A 30 SECOND DELAY, THE NOSE GEAR Feb 6, 2002 · N45GL · Beech 1900C · Landing Gear Position and WarningSDR ACE0119021Line · crackedFLIGHT CREW REPORTED THAT THE NR 2 ENGINE FLAMED OUT EN ROUTE. ATTEMPTED RESTART WAS UNSUCCESSFUL. THE ENGINE WAS SECURED AND ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE LOCATED A CRACKED P3 ENGINE CONTROL AIR LINE AND REPLACED SAME. MAINTENANCE ALSO DETEJan 19, 2002 · N45GL · Beech 1900C · Fuel Controlling SystemSDR ACE0117021Relay · burnedTHE PILOT REPORTED THAT AFTER DEPARTURE FROM HPB, THE LANDING GEAR SELECTOR HANDLE WAS INOPERATIVE AND WOULD NOT RAISE THE LANDING GEAR. THE FLIGHT CONTINUED, WITH THE GEAR EXTENDED. AN UNEVENTFUL LANDING WAS MADE AND MAINTENANCE REPLACED THE LANDING GEAR POJan 18, 2002 · N45GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR ACE1024011Relay · burnedON ARRIVAL, THE LANDING GEAR MOTOR CIRCUIT BREAKER POPPED, THE LOW HYDRAULIC LEVEL ENUNCIATOR CAME ON AND THE GEAR HAD TO BE MANUALLY EXTENDED. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND THE HYDRAULIC PUMP MOTOR VERY HOT AND THE CONTACTS IN THE MOTOR Oct 24, 2001 · N45GL · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR ACE1018011Landing Gear · icedON ARRIVAL, THE LANDING GEAR SELECTOR HAD TO BE CYCLED MULTIPLE TIMES TO ACHIEVE GEAR DOWN AND SAFE INDICATION. MAINTENANCE COULD NOT DUPLICATE THE FAULT AND INSPECTED THE SYSTEM, INCLUDING MULTIPLE SATISFACTORY CYCLES. THE POSSIBILITY THAT THE FAULT WAS ICIOct 18, 2001 · N45GL · Beech 1900C · Landing Gear SystemSDR YAD2001F00008Switch · failedCABIN ALTITUDE WAS NOTED AT 16,000 FT (DUE IMPACT - DAMAGE TO FUSELAGE) IN FLIGHT - CREW STATED USING SUPPLEMENTAL OXYGEN AT THIS POINT. CABIN ALTITUDE WARNING DID NOT FUNCTION, WARNING LIGHT SHOULD COME ON AT 12,250 FT. REPLACED DEFECTIVE SWITCH. WARNING Jul 25, 2001 · N45GL · Beech 1900C · Ground Proximity SystemSDR 20010425CW012Engine · failedON RETURN LEG OF ROUND TRIP, PILOT NOTICED AN ORANGE FLASH FRO THE RIGHT HAND ENGINE. ENGINE ITT STARTED RISING AND THE POWER STARTED RISING AND THE POWER STARTED SURGING. THE ENGINE WAS SECURED AND FEATHERED 45 MINUTES OUT. MADE UNEVENTFUL LANDING. NO DETJan 21, 2001 · N45GL · Beech 1900C · Engine (Turbine/Turboprop)SDR 20010601CW002Windshield · crackedWINDSHIELD CRACKED A FL20. THE FLIGHT CREW CANCELED THE INTENDED FLIGHT AND RETURNED TO ANCHORAGE, WITHOUT FURTHER PROBLEMS.Sep 8, 2000 · N45GL · Beech 1900C · Flight Compartment WindowsSDR 20010601CW006Switch · disconnectedWHILE PERFORMING ENGINE FIRE EXTINGUISHER SYSTEM TEST IAW B1900C MM CAMP NR2 INSPECTION TEMP REVISION 26-1, FOUND NR 1 AND NR 2 ENGINE SQUIB POWER SWITCH DISCONNECTED FROM ANNUNCIATOR/ ACTUATOR ASSEMBLY. THIS A RECURRENT PROBLEM WITH THIS STYLE SWITCH ASSEMBLAug 31, 2000 · N45GL · Beech 1900C · Fire DetectionSDR 20010425CW016Clamp · unsecureNR 1 ENGINE POWER FAILED TO REDUCE BELOW 2200 LBS. TORQUE FOR LANDING. THE ENGINE WAS SHUT DOWN IN FLIGHT JUST PRIOR TO LANDING. A NON EVENTFUL LANDING WAS ACCOMPLISHED AND THE ENGINE WAS RESTARTED FOR TAXI TO HANGAR. MAINTENANCE WAS UNABLE TO VERIFY THE CAJul 17, 2000 · N45GL · Beech 1900C · Engine Air Intake SystemSDR 20010607CW007Switch · disconnectedWHILE PERFORMING A NEW INSPECTION REQUIREMENT, FOUND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENGINE FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FNov 23, 1999 · N45GL · Beech 1900C · Extinguishing SystemSDR 2000ZZZX423Switch · disconnectedWHILE PERFORMING 'NEW' INSP REQUIREMENT, FND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FND ON HALF OF INSPECTNov 23, 1999 · N45GL · Beech 1900C · Extinguishing SystemSDR 99ZZZX4654Annunciator · failedFAILURE OF NON-FIELD REPLACEABLE IFR GPS 'LEG' ANNUNCIATION. THIS COMPONENT IS THE INDICATOR/SWITCHING UNIT OF A CERTIFIED IFR GPS NAVIGATION SYSTEM.Nov 3, 1999 · N45GL · Beech 1900C · Visual Omnirange (VOR) SystemSDR 20000502AP014Bulkhead · crackedDURING A ROUTINE ACE CAMP INSPECTION NR 6, HEAVY AFT FUSELAGE AND EMPENNAGE, FOUND MULTIPLE CRACKS IN CANTED BULKHEAD, STATION 588.10, IN EXCESS OF CRACK LIMITS PROVIDED IN BEECHCRAFT SERVICE BULLETIN 2564, REV 1 INCORPORATION OF SB 2564 KIT NR 129-4005-1S BEIJul 12, 1999 · N45GL · Beech 1900C · Fuselage Main, BulkheadSDR 99ZZZX1147Fuel Pump · failed67.6 HOURS AFTER OVERHAUL, DRIVESHAFT BROKE. PUMP TURNS NORMAL, NO DAMAGE DETECTED INSIDE PUMP.Mar 2, 1999 · N45GL · Beech 1900C · Engine Fuel PumpSDR 99ZZZM184Line · rupturedPILOT REPORTED CAPTAINS LEFT BRAKE VERY WEAK. BRAKE SYSTEM BLEED, OPS CHECKED GOOD. THE NEXT DAY, THE FLEXIBLE BRAKE LINES (UPPER) IN THE GEAR WELLS, LEFT AND RIGHT, WERE FOUND TO BE LEAKING THROUGH THE HOSE. REPLACED UPPER FLEX LINE. (M)Jan 25, 1999 · N45GL · Beech 1900C · Landing Gear Brake SystemSDR 98ZZZX3399Relay · contaminatedLANDING GEAR FAILED TO EXTEND WITH GEAR HANDLE SELECTION. LANDING GEAR EXTENDED USING HAND PUMP SYSTEM, GEAR INDICATIONS WERE NORMAL. FOUND LANDING GEAR PUMP RELAY CONTAMINATED WITH WATER AND SUSPECT UNIT FROZE IN-FLIGHT AND FAILED TO POWER ELECTRIC PUMP. SAug 27, 1998 · N45GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 98ZZZX3397Spar Cap Assy · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS SPAR JUST ABOVE THE EDGE OF THE SEALAug 20, 1998 · N45GL · Beech 1900C · Wing SparSDR 98ZZZX1871Fuel Line · chafedON NR 1 ENGINE - STARTER/GENERATOR COOLING DUCT HOSE CAME IN CONTACT WITH AN ENGINE FUEL LINE AND CHAFED A HOLE THROUGH THE TUBING WALL THICKNESS CAUSING FUEL TO LEAK INTO THE ACCESSORY SECTION OF THE ENGINE COMPARTMENT. P&WC SB 13250 ADDRESSES THIS PROBLEM AApr 26, 1998 · N45GL · Beech 1900C · Engine Fuel DistributionSDR 97ZZZX4834Terminal · separatedAIRCRAFT DEPARTED ANC FOR FAI. CLLIMBING OUT OF 8,000 FEET, NR 2 PROPELLER AUTOFEATHERED. FLIGHT CREW SECURED NR 2 ENGINE AND RETURNED TO ANC. LANDING WAS NORMAL. MAINTENANCE FOUND PUSH/PULL TERMINAL AT FORWARD END OF PROPELLER REVERSING CONTROL HAD SEPARAAug 11, 1997 · N45GL · Beech 1900C · Propeller Controlling SystemSDR GLBA96222Relay · failedORD - GEAR DID NOT EXTEND. EXTENDED GEAR MANUALLY. REMOVED AND REPLACED LANDING GEAR RELAY. OPS CHECKS GOOD. (X)Nov 11, 1996 · N45GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR GLBA96209Prop Governor · malfunctionedBMG - DURING LANDING AT 110 KTS THE RIGHT PROP RPM DECREASES TO 900 AND THE LEFT STAYS AT 1400. RIGHT TORQUE INCREASES SLIGHTLY AND AIRCRAFT YAWS HEAVY TO THE LEFT. MAINTENANCE CLEANED LOW PITCH SOLENOIDS. LUBED PROP AND BETA CABLES. REMOVED ADN REPLACED ROct 24, 1996 · N45GL · Beech 1900C · Propeller Controlling SystemSDR GLBA96039Motor Relay · failedESC - THE CREW REPORTED LANDIGN GEAR WOULD NOT EXTEND AND HAD TO MANUALLY EXTEND GEAR. AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR MOTOR RELAY. OPS CHECK WAS GOOD. (M)Feb 26, 1996 · N45GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZM483Truss · crackedESC - DURING THE ROUTINE TRUSS INSPECTION REQUIRED BY AD95-02-18, A .75 INCH CRACK WAS FOUND NEAR THE LINSEED OIL PLUG OF THE INBOARD AREA 'A' OF THE RIGHT TRUSS. THE TRUSS WAS REPAIRED IAW BEECH KIT 129-9006, REPAIR NR 2.Aug 15, 1995 · N45GL · Beech 1900C · Engine Mount SectionSDR 95ZZZM489Receiver/Trans · intermittentDVL - THE CREW ELECTED AN AIR TURNBACK AFTER THE WEATHER RADAR PICTURE SHRUNK AND THE HORIZONTAL WAS INTERMITTENT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED FOLLOWED BY THE REPLACEMENT OF THE RADAR R/T.Jul 27, 1995 · N45GL · Beech 1900C · Weather Radar SystemSDR 95ZZZX2508Aileron · dentedORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, THE LEFT WING TIP AND OUTBOARD TRAILING EDGE WERE DENTED BY A BAG CART TOW TRACTOR. MAINTENANCE REMOVED THE AILERON AND WING TIP AND INSPECTED THOSE AREAS FOR FURTHER DAMAGE. A SERVICEABLE AILERON AND WING TIP Apr 2, 1995 · N45GL · Beech 1900C · AileronsSDR 95ZZZX2509Engine Oil · lowDLH - INBOUND TO DLH, CREW EXPERIENCED THE RT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 40-100 PSI ACCOMPANIED BY THE ILLUMINATION OF THE RT OIL PRESSURE ANNUNCIATOR. THE RT ENGINE WAS SECURED AFTER WHICH AN UNEVENTFUL LANDING WAS COMPLETED. MAINTENANCE INSPECApr 1, 1995 · N45GL · Beech 1900C · Turbine Engine Oil SystemSDR 95ZZZX2021Rivet · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 4 RIVETS IN RT FUEL TANK TOP SIDE BETWEEN THE NACELLE AND STALL FORCE LOOSE AND LEAKING FUEL. THE RIVETS WERE REPLACED, THE TANK SEALED, AND LEAK CHECK OKAY.Mar 25, 1995 · N45GL · Beech 1900C · Wing, Plate/SkinSDR 95ZZZX1965Te Skin · crackedSPW - DURING ROUTINE MAINTENANCE, RUDDER TRAILING EDGE FAIRING WAS FOUND CRACKED AND HAD SEVERAL WORKING RIVETS. THE CRACK WAS REPAIRED AND RIVETS WERE REPLACED IAW DER APPROVED FROM 8110-3. RUDDER BALANCE CHECKED AND RESINSTALLED.Mar 25, 1995 · N45GL · Beech 1900C · Rudder, Plate/SkinSDR 95ZZZZ103Rivets · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RIGHT WING SEEPING FUEL OUTBOARD OF THE NACELLE ALONG THE SPAR. SEVERAL RIVETS WERE REPLACED AND THE AREA WAS SEALED WITH MIL-S-8802F SEALANT.Jan 30, 1995 · N45GL · Beech 1900C · Wing, Plate/Skin
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