Beech 1900D

Service difficulty reports · 7,152

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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 aircraft_model_key = '1900D'
  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 GUUA95627101010ATorque Tube · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE IS CORRODED. REPLACED RIGHT ELEVATOR TORQUE TUBE.Oct 10, 2010 · N81556 · Beech 1900D · Elevator Control SystemSDR V0DR967YCBearing · failedBEARING FAILURE AT TSO:282.1. CAUSED ARMATURE TO STATOR CONTACT.Oct 7, 2010 · Beech 1900D · Starter-GeneratorSDR GUUA93532100510AButton · inoperativePILOT REPORTED LANDING GEAR WARNING HORN SILENCE BUTTON WILL NOT SILENCE GEAR HORN WITH FLAPS 0 AND GEAR UP. REPLACED GEAR WARNING HORN SILENCE BUTTON OPS CHECK GOOD.Oct 5, 2010 · N81535 · Beech 1900D · Landing Gear Position and WarningSDR CA101008002Relay · burnedAFTER ABC STRUCTURAL INSP AND FOLLOWING SEVERAL ENGINE RUNS, WHEN THE ACFT WAS CONNECTED TO GROUND POWER DURING SERVICING IN THE HANGAR, THE AME WORKING ON THE ACFT NOTED DENSE SMOKE COMING OUT OF THE ENGINE NACELLE AND LANDING GEAR AREA. ACFT POWER WAS REMOVOct 2, 2010 · Beech 1900D · Waste Disposal SystemSDR GLBA2010100410FSkin · dentedMAJOR REPAIR - MAINTENANCE FOUND DAMAGE ON AN LEFT ELEVATOR THAT WAS PURCHASED, TRAILING EDGE DENT ON OUTER 9" INCLUDING TIP AND 5" FROM TRAILING EDGE FORWARD, INCLUDES OUTBOARD RIB DAMAGE, TRAILING EDGE PUSHED IN 11.5" TO 14" OF OUTBOARD EDGE AND .25" FORWARDSep 30, 2010 · Beech 1900D · Elevator, Plate/SkinSDR GLBA20101001FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A .5" CRACK IN THE SKIN 5" LEFT OF BOTTOM CENTERLINE OF FUSELAGE AT F.S. 228.25. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-057. MATERIALSSep 28, 2010 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100927GSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE .7" BY 1" DEEP IN THE T/E OF THE LT ELEVATOR, JUST INBD OF CAP AT OUTER STATIC WICK, AT OUTER STATIC WICK, AND A DAMAGED RIVET ON TOP OF THE CAP. MAINTENANCE REPLACED THE RT ELEVASep 26, 2010 · N240GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA20100926FSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE .5" BY .5" DEEP IN THE T/E OF THE RT ELEVATOR, JUST INBD OF THE CAP AT THE OUTER STATIC WICK. OPENSep 26, 2010 · N240GL · Beech 1900D · Elevator, Plate/SkinSDR GUUA93857092210ASkin · damagedFLIGHT 5401 PILOT REPORTED BIRD STRIKE ON RIGHT WING. REMOVED DAMAGED SECTION OF SKIN AT RIGHT WING OUTBOARD LEADING WS 189.0 AND INSTALLED A DOUBLER REPAIR AND SKIN FILLER.Sep 22, 2010 · N81538 · Beech 1900D · Wing, Plate/SkinSDR GUUA95552092110AHandle · lack of lubeDURING SCHEDULED ROUTINE MX DISCOVERED 6A EMERGENCY EXIT HANDLE HARD TO OPEN. LUBRICATED 6A EMERGECNY EXIT HANDLE OPS CK OK.Sep 21, 2010 · N87555 · Beech 1900D · Emergency ExitsSDR GLBA20100920FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE FRAME AT THE STRINGER CUTOUT 4R AT FS 288, .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-056. MATERIALS UTILIZED ARE INCLUDED INSep 20, 2010 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GUUA95132091810ALight · looseDURING FLIGHT, LANDING GEAR "H" GREEN LIGHTS LOOSE AND FLICKERED ON AND OFF WHEN LANDING GEAR DOWN OR PRESS TO TEST. RESECURED LANDING GEAR "H" GREEN LIGHTS, OPS CHECK NORMAL.Sep 18, 2010 · N87551 · Beech 1900D · Landing Gear Position and WarningSDR GUUA95752091610AHandle · stickingDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT OUTER HANDLE STICKING. LUBED LT EMERGENCY EXIT OUTER HANDLE.Sep 16, 2010 · N87557 · Beech 1900D · Emergency ExitsSDR GLBA20100916GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT STRINGER CUTOUT 10R AND FS 456, .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-054. MATERIALS UTILIZED ARE INCLUDED INSep 16, 2010 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100916FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME ANGLE AT STRINGER 13L AND FS 177.35, UNDER THE AIRSTAIR ENTRANCE FLOOR, 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-055Sep 16, 2010 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93352091510ADoor · lack of lubeDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT DOOR IS HARD TO LOCK. LUBRICATED LT EMERGENCY DOOR OPS CHECK NORMAL.Sep 15, 2010 · N81533 · Beech 1900D · Emergency ExitsSDR GUUA93332091510AWire · looseDURING APPROACH, LANDING GEAR DOWN, NO 3 GREEN LIGHT INDICATION. RECONNECTED LOOSE WIRE AT LIGHT SENSOR ASSY. OPS CHECK GOOD.Sep 15, 2010 · N81533 · Beech 1900D · Landing Gear System WiringSDR GLBA20100915FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND CRACK IN FRAME AT FS 327.63, 1" BELOW FLOORBOARD ON RT SIDE, 2.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO10-1900-53-060. MATERIALS UTILIZED ARE INCLUDED IN Sep 15, 2010 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA201009141Engine · low torqueINCREASING POWER ON APPROACH, LT ENGINE REMAINED AROUND 500 LBS TORQUE, DID NOT RESPOND TO POWER LEVER INPUT WHILE RT ENGINE SPOOLED TO APPROX 1200 TORQUE. LT ENGINE AUTOFX TRIGGERED AND TOOK APPROX 2-3 INCHES OF POWER LEVER MOVEMENT TO GET LT ENGINE TO RESPONSep 14, 2010 · N261GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20100914FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE 6A EMERGENCY EXIT DOOR SKIN, LOWER FWD RADIUS, 1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-52-006. MATERIALS UTILIZED ARE INCLUDED IN TSep 14, 2010 · N153GL · Beech 1900D · Emergency ExitsSDR GUUA93832091310AAnnunciator · loosePILOT REPORTED NOSE GEAR LIGHT INOPERATIVE. PUSHED NOSE GEAR ANNUNCIATOR IN THE SOCKET.Sep 13, 2010 · N81538 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94352091310AHandle · bindingDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR HANDLE. OPS CHECK OK.Sep 13, 2010 · N49543 · Beech 1900D · Emergency ExitsSDR GUUA93732091210AAnnunciator · intermittentPILOT REPORTED CTR LANDING GEAR DOWN GREEN LIGHT INTERMITTENT. REPLACED CENTER LANDING GEAR DOWN GREEN LIGHT ANNUNCIATOR. OPS CHECK NORMAL.Sep 12, 2010 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR CA100921005Engine · failedLOSS OF TORQUE/IFSD DURING FLIGHT, THE PILOT REPORTED ENGINE NOISES AND OBSERVED TORQUE INDICATION DECREASING. HE ELECTED TO SHUTDOWN THE ENGINE AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. POST FLIGHT INSP FOUND DAMAGES TO THE COMPRESSOR.Sep 10, 2010 · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20100910GSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A BURN HOLE IN THE RIGHT ELEVATOR 4" INBOARD OF OUTBOARD EDGE, .75" WIDE BY .625" DEEP. MAINTENANCE REPLACED THE RIGHT ELEVATOR, IAW BMM TC 1900-2730-00. REMOVED IN SERVICABLE CONDITION FSep 10, 2010 · N211GL · Beech 1900D · AileronsSDR GUUA94232091010ACircuit Breaker · poppedDURING APPROACH LANDING GEAR CIRCUIT BREAKER POPPED. INSPECTED HYD POWER PACK AND WIRING NO DEFECTS NOTED COMPLIED WITH LANDING GEAR EXTEND/RETRACT SYS INSP CYCLED LANDING GEAR SEVERAL TIMES COULD NOT DUPLICATE.Sep 10, 2010 · N47542 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20100910FSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" BY .375" BURN HOLE IN THE T/E OF THE ELEVATOR 9" INBD OF THE OTBD EDGE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-27-004. MATERIALS UTILIZED ARE INCLUDSep 10, 2010 · N153GL · Beech 1900D · Elevator, Plate/SkinSDR GUUA94152090910AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Sep 9, 2010 · N17541 · Beech 1900D · Emergency ExitsSDR GLBA201009061Autofeather Sys · malfunctionedCYCLED IN DURING APPROACH LT ENGINE ENTERED FEATHER & OUT OF FEATHER. MX TROUBLESHOT AUTOFEATHER SYS, SYS FOUND TO OPERATE NORMALLY IAW BMM 61-21-00.Sep 6, 2010 · N100UX · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20100904ATube · leakingPILOT REPORTED THAT THEY NOTICED SMOKE/FUMES IN THE CABIN PRIOR TO TAKEOFF, SUSPECT VAPOR CYCLE SYSTEM LEAK. MAINTENANCE REPLACED THE TUBE FROM RECEIVER-DRIER TO CONDENSOR IAW BMM 21-52-00, REPLACED CONDENSER BLOWER IAW BMM 21-52-03, AND SERVICED SYSTEM IAW BMSep 4, 2010 · N154GL · Beech 1900D · Air Distribution SystemSDR GLBA201009031Wire · brokenPILOT REPORT THAT ONE OF THE CAPTAINS EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE INSPECTED THE SYSTEM, FOUND AND REPAIRED A BROKEN WIRE GOING TO THE CAPTAINS EMERGENCY LIGHTING IAW D436 INSTRUCTIONS, OPERATIONAL CHECKS GOOD, PN D436-36.Sep 3, 2010 · N219GL · Beech 1900D · Light System WiringSDR GLBA20100902FHandle · loosePILOT REPORTED THAT AFTER CLOSING THE AIR STAIR DOOR THE OUTSIDE HANDLE CAME OFF. MAINTENANCE REPLACED THE CABIN DOOR HANDLE SNAP RING PN MS16624-1075, REF MM 52-10-05 STEPS (A,B).Sep 2, 2010 · N173YV · Beech 1900D · Entrance StairsSDR GUUA93952090110BHandle · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT OUTER HANDLE BINDING. LUBRICATED RT FWD EMERGENCY EXIT HANDLE, OPS CHECK GOOD.Sep 1, 2010 · N82539 · Beech 1900D · Emergency ExitsSDR GUUA93952090110AHandle · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT INNER AND OUTER HANDLE BINDING. LUBRICATED RT AFT EMERGENCY EXIT OPS CHECK GOOD.Sep 1, 2010 · N82539 · Beech 1900D · Emergency ExitsSDR GLBA20100830FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE LOWER FWD SKIN ON THE 6A EMERGENCY EXIT DOOR, 1.2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-52-005. MATERIALS UTILIZED AAug 30, 2010 · N261GL · Beech 1900D · Emergency ExitsSDR GLBA20100827FFrame · crackedDURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A THE CARGO PARTITION FUSELAGE ATTACH POINT HOLES ARE WORN, TOP LEFT, TOP CENTER, AND TOP RIGHT. MAINTENANCE INSPECTED AND FOUND THE REPAIR TO BE A MINOR REPAIR - REPAIRED PARTITION ATTACH POINTS, TOP, TAug 27, 2010 · N261GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93853082710ASkin · crackedDURING SCHEDULED STRUCTURAL INSP, DISCOVERED CRACK IN SKIN 1.5 INCHES LONG AT APPROX FS 353 STRINGER 16. REMOVED DAMAGED SECTION OF SKIN, INSTALLED INSERTION PATCH AND EXTERNAL DOUBLER REPAIR.Aug 27, 2010 · N81538 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100827AConnector · dirtyLT ENGINE AUTOFEATHERED AS DESCENDING WHEN INCREASING TORQUE. MAINTENANCE CLEANED THE TORQUE TRANSMITTER CONNECTOR ON THE LT ENGINE AND PERFORMED GROUND RUNS, CHECKED LEFT ENGINE RIGGING, ALL OPERATIONAL CHECKS GOOD PER RUN SHEET.Aug 27, 2010 · N219GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20100826GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK ON THE LT HEAVY FRAME ANGLE AT FS 288 FWD BEND RADIUS, 1.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-053. MATERIALS UTILIZEDAug 26, 2010 · N261GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93852082510ACable · frayedDURING SCHEDULED STRUCTURAL INSP DISCOVERED AIRSTAIR DOOR AFT UPPER AND FORWARD UPPER CONTROL CABLES FRAYED. REPLACED UPPER AFT AND UPPER FORWARD AIRSTAIR DOOR CONTROL CABLES.Aug 25, 2010 · N81538 · Beech 1900D · Entrance StairsSDR GLBA20100826FValve · inoperativePILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, GEAR FAILED TO EXTEND AND LANDING GEAR RELAY TRIPPED, GEAR WAS MANUALLY EXTENDED SUCCESSFULLY WITH 3 GREEN LIGHTS INDICATED. MX REMOVED LANDING GEAR SERVICE VALVE PN 101-388008-3, SN 2206 Aug 25, 2010 · N231YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR CA100825005Insulator · cracked(CAN) DURING FLIGHT WHEN THE ACM WAS SELECTED TO THE FULL COLD POSITION, CABIN PRESSURIZATION WOULD BE LOST. DURING TROUBLESHOOTING, MX PERSONNEL FOUND A CRACK ON THE ACM INSULATOR. THE ACM WILL BE REPLACED PRIOR TO ACFT BEING RETURNED TO SERVICE.Aug 24, 2010 · Beech 1900D · Cabin Cooling SystemSDR GUUA93853082410BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT HEAVY ANGLE CRACKED AT FS 288 APPROX 1.875 INCHES LONG. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE,CLIP AND FASTNERS AS REQUIRED.Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA93853082410DStringer · corrodedDURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED CORROSION AT FS 348 STRINGER 16. REMOVED DAMAGED SECTION OF STRINGER 16, AND INSTALLED NEW SECTION STRINGER SPLICE.Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GUUA93853082410CFrame · crackedDURING SCHEDULED ROUTINE MX DISCOVERED ASD ANGLE CRACKED AT FS 150 STRINGER 5L APPROX. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, FrameSDR GLBA20100824GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT, TOP OF LEFT AILERON, 1.75" BY .75", 38.125" FROM OB EDGE AND .875" FROM TE. AND A .5" CRACK WAS FOUND RUNNING FWD TO AFT ON LOWER SKIN 37.125" FROM OB EDGE. MAINTENANCE REPAIRED THAug 24, 2010 · N173YV · Beech 1900D · AileronsSDR GUUA93853082410AStringer · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION AT STR 15L APPROX FS 250 TO 258. REMOVED DAMAGED SECTION OF STRINGER 15L,INSTALLED NEW SECTION AND INSTALLED EXTERNAL DOUBLER REPAIR.Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA201008231Powerpack · failedPILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, INTRANSIT LIGHT WAS ON AND NOTICED THAT THE GEAR RELAY CB POPPED, EXTENDED THE LANDING GEAR MANUALLY, LANDED SAFELY. MAINTENANCE CONFIRMED DISCREPANCY, TROUBLESHOT SYSTEM TO HYDRAULIC POWERAug 23, 2010 · N231YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20100823GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-052. MATERIAug 23, 2010 · N195GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100823FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP A, 2" CRACK WAS FOUND BETWEEN FS 300 TO 302, 28.5" OTBD OF THE CTR LINE ON THE RT SIDE AT WATER LINE 75.00. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-53-051. MATERIALS UTIAug 23, 2010 · N202UX · Beech 1900D · Fuselage Main, Plate/Skin
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