N245GL

Service difficulty reports · 81

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 = 'N245GL' AND registry_match = 'registration'
  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 2022FA0000757Rib · crackedCRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FORWARD AND AFT FLANGES AT FUSELAGE STATION 303 BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80May 17, 2022 · N245GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2017120100693Clevis · bentMAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CLEVIS WAS BENT. REMOVED AND REPLACED LOWER FORWARD HANDRAIL IAW AMM 52-10-02-201, OPS CHECK GOOD. P/N ON/OFF: 1440-43GLA.Nov 30, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017051900657Control Handle · inoperativeTHE CREW REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND NORMALLY, LANDING GEAR CIRCUIT RELAY CIRCUIT BREAKER WAS TRIPPED, EXTENDED GEAR MANUALLY. ALL INDICATIONS WERE GREEN. MAINTENANCE PERFORMED GEAR CYCLES 5 TIMES IAW AIM MI 32-01. COULD NOT DUPLICATE THEMay 18, 2017 · N245GL · Beech 1900D · Landing Gear SelectorSDR GLBA2017041000647Cable · wornMAINTENANCE REPORTED THAT THE MAIN CABIN DOOR FORWARD TOP CABLE IS WORN. REMOVED AND REPLACED THE UPPER FORWARD AIRSTAIR DOOR HANDRAIL CABLE IAW BMM 52-10-02.Apr 8, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017033100645Cable · looseMAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE WAS TOO LOOSE. RESECURED UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE WITH PROPER TENSION IAW BMM 52-10-02.Mar 29, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017032400644Cable · brokenMAINTENANCE NOTED THAT THE FWD LOWER AIRSTAIR DOOR CABLE WAS BROKEN. REPLACED FORWARD LOWER AIRSTAIR DOOR CABLE, AND AFT LOWER CABLE P/N 1440-43GLA IAW AMM 52-10-02. OPS CHECKED GOOD.Mar 23, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017031700643Cable · looseMAINTENANCE NOTED THAT THE UPPER FORWARD AIRSTAIR DOOR HANDRAIL CABLE HAS IMPROPER TENSION. ADJUSTED THE CABLE IAW MM 52-10-02.Mar 15, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017022100633Cable · looseMAINTENANCE REPORTED THAT THE UPPER FORWARD PAX DOOR HANDRAIL CABLE TENSION IS TOO LOW. SECURED THE CABLE WITH PROPER TENSION IAW BMM 52-10-02.Feb 18, 2017 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016110700621Warning System · malfunctionedSIG EVENT, PILOT REPORTED THAT WHEN EXTENDING THE LANDING GEAR, LT MAIN GEAR ANNC FAILED TO ILLUMINATE WITH GEAR DOWN, LANDING GEAR INTRANSIT LIGHT DID NOT ILLUMINATE, ANNC ILLUMINATES WITH PUSH TO TEST. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLDec 7, 2016 · N245GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2016052700589Warning System · false activationTHE CABIN DOOR ANNC ILLUMINATED IN FLIGHT, CREW DECLARED AN EMER, INDICATION SYS WAS MEL'D. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 23, 2016 · N245GL · Beech 1900D · Door Warning SystemSDR GLBA2015111700560Warning System · false activationPILOT REPORTED THAT WHILE IN CRUISE, THE DISCHARGE LIGHT ON THE NR 1 FIRE EXTINGUISHER ILLUMINATED. REPLACED SOFT SPLICE, PN M81714/11-20D, ON WIRE W23B22 IAW EO 13-1900-26-001. OPERATIONAL CHECK OF DISCHARGE INDICATION GOOD.Nov 16, 2015 · N245GL · Beech 1900D · Extinguishing SystemSDR GLBA2015100500555Connector · dirtyPILOT REPORTED THAT THE NR 1 ENG EXTINGUISHER ANNC DISCHARGE NR 1 LIGHT ILLUMINATED, ON CLIMB OUT. FOUND NO CONTINUITY BETWEEN PIN M OF CONNECTOR P281 & THE FIRE BOTTLE SQUIB, CLEANED CONNECTOR P281, OPERATIONS CHECKED GOOD.Nov 2, 2015 · N245GL · Beech 1900D · Fire Protection System WiringSDR GLBA2014112600470Skin · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT SIDE BELLY SKIN AT BL 29.06 & WING SPAR, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-047.Nov 26, 2014 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014111700466Frame · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME FLANGE AT FS 177.35 BETWEEN STRINGERS 13L & 14L IN THE FRAME FLANGE BEND RADIUS AT OTBD END OF FRAME, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTNov 17, 2014 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2014111300464Skin · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE EMER EXIT 6A EXTERIOR BONDED SKIN CRACKED AT THE INTERIOR LOWER AFT CORNER, 1.2 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-52-006.ENGINEERING ORDENov 12, 2014 · N245GL · Beech 1900D · Emergency ExitsSDR GLBA2014091600438Skin · crackedDURING A SCHEDULED INSPECTION FOUND A 7/8 INCH LONGITUDINAL CRACK ON THE UPPER FUSELAGE AT APPROX FUSELAGE STATION 214.25 ON FUSELAGE SKIN 27 APPROX 2 INCHES RIGHT OF UPPER CTR LINE & APPROX 2 INCHES LEFT OF COMM 1 ANTENNA IN LINE WITH THE LE OF THE ANTENNA BASep 16, 2014 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014071400421Uplock Switch · faultyPILOT REPORTED THAT ON MLG EXTENSION THE CREW HEARD THE MOTOR RUN FOR APPROX 15 SECONDS THEN THE CB NEXT TO THE GEAR HANDLE POPPED. RAN CHECKLIST & MANUALLY EXTENDED GEAR, ALL INDICATIONS WERE NORMAL. REPLACED THE RT MLG UPLOCK SWITCH & RIGGED IAW TC 1900-32Jul 12, 2014 · N245GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2014070100418Uplock Switch · malfunctionedPILOT REPORTED THAT THE CIRCUIT BREAKER TRIPPED ON THE LANDING GEAR CONTROL, RAN CHECKLIST, PROCEEDED TO DESTINATION & USED THE MANUAL EXTENSION. MAINTENANCE R & R RT UPLOCK SWITCH IAW TC 1900-3260.00 REV 2.Jul 1, 2014 · N245GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2013120500353Hydraulic System · contaminatedPILOT REPORTED THAT AFTER SELECTING GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RAN THROUGH CHECK LIST, MANUALLY EXTENDED GEAR, ALL INDICATIONS SHOWED GEAR WAS DOWN AND LANDED SAFELY. MAINTENANCE INSPECTED RETRACTION AND EXTENSION OF LANDING GEAR Dec 4, 2013 · N245GL · Beech 1900D · Hydraulic System, MainSDR GLBA2013112200351Handle · separatedPILOT REPORTED THAT THE AIR STAIR DOOR HANDLE CAME OFF. INSTALLED A NEW SNAP RING & REINSTALLED DOOR HANDLE, IAW BMM 52-10-05, OPS CHECKED GOOD.Nov 21, 2013 · N245GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2013112100350Terminal · out of positionPILOT REPORTED THAT SPARKS WERE COMING OUT FROM BEHIND THE ICE PROTECTION PANEL. THE RT PITOT TERMINAL CONTACTING THE MOUNTING STRUCTURE REPOSITIONS THE RT PITOT TERMINAL END FOR CLEARANCE, ALL CHECKED GOOD.Nov 20, 2013 · N245GL · Beech 1900D · Pitot/Static Anti-Ice SystemSDR GLBA2013091300309Actuator · failedPILOT REPORTED THAT THEY LOWERED GEAR HANDLE, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, GEAR DID NOT MOVE, HYD POWER PACK DID NOT START AND LANDING GEAR HANDLE RED LIGHT DID NOT ILLUMINATE, MANUALLY EXTENDED GEAR, HANDLE RED LIGHT DID ILLUMINATED, GEAR DID Sep 12, 2013 · N245GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2013011500158Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT THE AFT LOWER CARGO DOOR FRAME AT FS 509.5, 2 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-002.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013011500157Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT FS 107, LT SIDE FRAME BEHIND FINGER DOUBLER IN THE BEND RADIUS, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-004.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013011500156Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND SKIN CRACKED AT FS 438 AND JUST ABOVE STRINGER 8L PROTRUDING OUT OF RIVET, .25" IN LENGTH. REPAIRED IAW EO 13-1900-53-003.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013011400155Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT VERTICAL STAB FWD SPAR CAP ANGLE BY THE TOP RIVET GOING TOWARDS THE BEND RADIUS, 1" IN LENGTH. REPAIRED IAW EO 13-1900-55-003.Jan 14, 2013 · N245GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013011400154Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING, INBD LOWER AFT CORNER BY SPAR RIB FLANGE , 1" IN LENGTH. REPAIRED IAW EO 13-1900-57-003.Jan 14, 2013 · N245GL · Beech 1900D · Wing Main, Frame StructureSDR GLBA2013011400153Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORRODED BETWEEN STRINGERS 14R AND 15R AT FRAME LOCATION AT FS 243.25. REPAIRED IAW EO 13-1900-53-001.Jan 14, 2013 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012103000096Oil System · leakingPILOT REPORTED THAT THE OIL PRESSURE ON NR 1 ENGINE DROPPED TO 50 PSI REDUCED POWER TO IDLE OIL PRESSURE CONTINUED TO DROP TO 40 PSI LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED SHUT ENGINE DOWN OBSERVED OIL PRESSURE AT 20 PSI JUST PRIOR TO ENGINE SHUTDOWN. MAINTOct 29, 2012 · N245GL · Beech 1900D · Turbine Engine Oil SystemSDR GLBA2012083100042Attach Fitting · crackedVERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10. CRACK IS .7500 INCH IN LENGTH, BEGINNING AT THE SECOND FASTENER HOLE ON LT FORWARD HORIZ STABILIZER ATTACH FITTING. REPAIRED IAW FR-00-02506, REV 1, STEP 1.Aug 30, 2012 · N245GL · Beech 1900D · Vertical Stabilizer, Attach FittingsSDR GLBA2012042301Circuit Board · damagedPILOT REPORTED THAT THE LT AUTOFEATHER SYS DISARMED AND REARMED REPEATEDLY DURING FLIGHT. MX REPLACED THE PCB A123, OPS CHECKED GOOD.Apr 20, 2012 · N245GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2012022401Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL STAB FWD SPAR WEB JUST INBD OF RT HSS 5.000 OTBD UPPER CORNER. REPAIRED IAW EO 12-1900-55-003. MAJOR REPAIR.Feb 24, 2012 · N245GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012022002Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT A SCREW HOLE ON THE AFT PRESSURE BULKHEAD, BEHIND AFT WALL AT 1 O`CLOCK POSITION, 1" IN LENGTH. REPAIRED IAW EO 12-1900-53-012. MAJOR REPAIRFeb 20, 2012 · N245GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012022001Stringer · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AT STRINGER 10L AND FS 165.4 AND WS 236 FROM A SCREW HOLE, EA CRACK .375 EACH. REPAIRED IAW EO 12-1900-55-001. MAJOR REPAIRFeb 20, 2012 · N245GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20111229ABulb · inoperativeONE INSTRUMENT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.Dec 29, 2011 · N245GL · Beech 1900D · Emergency LightingSDR GLBA201112024Pump · leakingFUEL LEAKING OUT OF MAIN DRAIN LT NACELLE. MX R & R LT LOW PRESSURE FUEL PUMP.Nov 30, 2011 · N245GL · Beech 1900D · Fuel Boost PumpSDR GLBA20111017FSwitch · out of adjustPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE RIGGED CABIN DOOR ANNUNCIATOR CENTER LATCH SWITCH IAW BMM 52-70-02, OPS CHECKED GOOD.Oct 15, 2011 · N245GL · Beech 1900D · Door Warning SystemSDR GLBA20110923FSkin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON AN REPAIR AT FS 164.415 AND STRINGER 9R, .75" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-057. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJORSep 23, 2011 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110921JDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE CARGO DOOR FRAME, FWD SIDE, FS 456, BETWEEN STRINGER 3L AND 4L, .7" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-056. MATERIALSSep 21, 2011 · N245GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20110921GStringer · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON 2" OF STRINGER 16 AT FS 228.25, BELLY OF FUSELAGE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-53-055. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Sep 20, 2011 · N245GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20110921FSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND BELLY CORROSION AT FS 228.25 MEASURING 7.5", 13" INBD OF LT TRANSPONDER ANTENNA, 12" INBD OF RT TRANSPONDER ANTENNA, BETWEEN STRINGERS 16 & 15L. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RIISep 20, 2011 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR V0DR2011010Slip Ring · deterioratedDURING SCHEDULED MX, A MECHANIC NOTED THAT DURING CLEANING OF THE PROP DEICE SLIP RING THAT THE DIELECTRIC FILLER IN BETWEEN COPPER RINGS APPEARED TO BE DETERIORATING. THE PROPELLER WAS REMOVED FROM SERVICE. THE PROP DEICE SLIP RING WAS R & R AND THE PROP REMay 3, 2011 · N245GL · Beech 1900D · Propeller Deice Boot SectionSDR GLBA20100630KSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP FOUND CORROSION ON BELLY SKIN AT FS 213.25 BETWEEN STRINGER 16L AND 15L, WITH AN AREA OF 1" BY .75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-042. MATERJun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100630JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 288.00 AT STRINGER 4R CUTOUT, .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-041. MATERIALS UTILIZEDJun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100630FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 177.35 AT STRINGER 6R CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-038. MATERIALS UTILIZED Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100630HStringer · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND AT FS 451 ON THE STRINGER 10R ON THE HORIZONTAL PORTION OF THAT STRINGER, .45" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-5Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20100630GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-039. MATERIALS UTILIZED Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100113GSkin · crackedMAJOR REPAIR - DURING A ROUTINE DE-ICE REPLACEMENT, A CRACK WAS FOUND ON THE RT WING AT WS 190.74 AT THE WING BOOT TUBE CONNECTION HOLE, PROTRUDING INBD. CRACK LENGTH APPROX 1.250" IN LENGTH. MX REPAIRED THE CRACK IAW EO 10-1900-87-001. RII INSPECTIONS COMPLJan 13, 2010 · N245GL · Beech 1900D · Leading Edge DevicesSDR GLBA20090409ATransducer · malfunctionedAIR RETURN - PILOTS REPORTED A LIGHTNING STIKE ON THE NOSE WHICH RESULTED IN A RUNWAWAY RUDDER BOOST SITUATION IF THE RUDDER BOOST SWITCH WAS "ON". RUDDER BOOST ACTIVATES AND STAYED ACTIVATED. MAINTENANCE PLACED THE ISSUE ON MEL 22-2 CAT.C C/N 34624 AT THE TIMApr 9, 2009 · N245GL · Beech 1900D · Autopilot SystemSDR GLBA20090408FSwitch · out of adjustSIGNIFICANT EVENT-SUSPECTED AUTOFEATHER -PILOTS REPORTED THAT THE NR 2 ENGINE PROPELLER FEATHERED VIOLENTLY IN AIR WITH PROPELLERS FULL FWD AND REDUCING POWER. AUTO FEATHER SWITCH WAS IN THE ARMED POSITION 500 FT ABOVE THE GROUND. MX GROUND RUNS SHOWED THE LT Apr 7, 2009 · N245GL · Beech 1900D · Propeller Feathering/Reversing
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