Beech 1900D

Service difficulty reports · 7,152

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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 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 GLBA20101213FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE DOME SKIN AT FS 150 AND RT OF STRINGER NR 1, .75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-063. MATERIALS UTILIZDec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101213GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 456 & STR 10R AT THE STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-062. Dec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, FrameSDR GUUA95552121310AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Dec 13, 2010 · N87555 · Beech 1900D · Emergency ExitsSDR GUUA52121310AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Dec 13, 2010 · N87555 · Beech 1900D · Emergency ExitsSDR GUUA95652121210ADoor · bindingPILOT REPORTED AIRSTAIR DOOR HARD TO OPEN, HANDLE CATCHES. RIGGED LOWER AIRSTAIR DOOR CAMS, OPS CHECK GOOD.Dec 12, 2010 · N81556 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93752120810AHandle · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT HANDLE DIFFICULT TO OPERATE. ADJUSTED UPPER STRIKER PLATES AND LOWER LUGS, OPS CHECK GOOD. ACFT DOWN FOR STRUCTURAL INSP.Dec 8, 2010 · N38537 · Beech 1900D · Emergency ExitsSDR GLBA20101206ABleed Air Sys · inoperativeCLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE FDec 6, 2010 · N210GL · Beech 1900D · Engine Bleed Air SystemSDR GUUA93652120610AHandle · stiffDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT OUTER HANDLE STIFF TO OPERATE. LUBRICATED LATCH MECHANISM ON RT AFT EMERGENCY EXIT OPS CHECK NORMAL.Dec 6, 2010 · N81536 · Beech 1900D · Emergency ExitsSDR GUUA93832120410AWarning Horn · malfunctionedPILOT REPORTED LANDING GEAR WARNING HORN SOUNDS WITH TORQUE SET AT 2000 LBS. INSPECTED GEAR WARNING SWITCH NO DEFECT NOTED TEST FLIGHT PERFORMED MARKED PEDESTAL. TEST FLIGHT SATISFACTORY.Dec 4, 2010 · N81538 · Beech 1900D · Landing Gear Position and WarningSDR GUUA95552120410ACable · frayedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD LOWER LATCH CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD LOWER LATCH CABLE OPS CHECK GOOD.Dec 4, 2010 · N87555 · Beech 1900D · Passenger/Crew DoorsSDR CA101206003Powerplant · failedPOWER LOSS-OPERATOR REPORTED AN IFSD OCCURRED FOLLOWING A LOUD NOISE. NO FURTHER DETAILS ARE AVAILABLE. POST FLIGHT INSP FOUND METALLIC DEBRIS IN THE EXHAUST. THE ENG WILL BE REPLACED.Nov 29, 2010 · Beech 1900D · Powerplant SystemSDR GUUA95652112610BHandle · out of adjustREPORT: DURING SCHEDULED ROUTINE INSP DISCOVERED RT FWD EMERGENCY EXIT INTERIOR HANDLE CLOSES TIGHT AGAINST UPHOLSTRY MAKING GRABBING HANDLE DIFFICULT. REMOVE. ADJUSTED FWD EMERGENCY EXIT DOOR ROD END OPSCHECK GOOD.Nov 26, 2010 · N81556 · Beech 1900D · Emergency ExitsSDR GUUA95652112610AAttach Fitting · out of adjustREPORT: DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DIFFICULT TO REMOVE. ADJUSTED EMERGENCY EXIT DOOR LUGS OPS CHECK GOOD.Nov 26, 2010 · N81556 · Beech 1900D · Emergency ExitsSDR GUUA95457112510AStringer · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON THE RT WING LOWER SKIN BONDED STRINGER AT WS 114.25 TO WS 124.25 CUT OUT 4.5 INCH SECTION ON CORRODED STRINGER. FABRICATED AND INSTALLED FROWARD REPAIR ANGLE AND AFT REPAIR ANGLE ON RIGHT WING LOWER BONDENov 25, 2010 · N87554 · Beech 1900D · Wing, Longeron/StringerSDR GUUA91252112410ACable · frayedDURING SCHEDULED ROUTINE INSP, DISCOVERED AIRSTAIR DOOR FWD UPPER INTERNAL CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD UPPER INTERNAL CABLE.Nov 24, 2010 · N45AR · Beech 1900D · Passenger/Crew DoorsSDR GLBA201011241Bulb · inoperativeEMERGENCY LIGHT BULB DID NOT TEST. MAINTENANCE REPLACED THE BULB PN 1864, REF MM 31-10-00, OPS CHECK GOOD.Nov 24, 2010 · N247GL · Beech 1900D · Emergency LightingSDR GUUA91253112110ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED 1 SHEARED RIVET AFT LOWER FUSELAGE BELLY FS 544.250 AFTER FURTHER INSP, DISCOVERED SKIN BULGING NEXT TO SHEARED RIVET. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR. ACFT DOWN FOR STRUCTURAL INSP.Nov 21, 2010 · N45AR · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101122FTerminal · loosePILOTS REPORTED THAT THEY NOTICED A SMOKE IN THE COCKPIT AFTER AN ODOR AND VISUAL LEAK OF SMOKE WAS NOTICED COMING FROM THE CAPTIANS WINDOW AT THE LOWER FWD CORNER. ENG ANTI-ICE AND ENGINE AUTO IGNITION WERE ON FOR TAKEOFF AND SHORTLY AFTER ALL ICE PROTECTIONNov 21, 2010 · N153GL · Beech 1900D · Window System WiringSDR GUUA93753111510ASkin · chafedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EXTERNAL SKIN CHAFE, APPROX AT FS 259-281 WS 30. REPAIRED LT EXTERNAL SKIN CHAFE INSTALLED EXTERNAL DOUBLER 1.5 X 22 INCHES COVER PATCH.Nov 15, 2010 · N38537 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA93753111410ADoor Frame · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED UPPER AFT CARGO DOOR FRAME HAS A 2.0 INCH CRACK APPROX AT FS 509.5, STRINGER 14L. REPAIRED CRACKED "L" ANGLE BY REMOVING 47.0 INCHESS OF ANGLE AND INSTALLING INSERTION OF THE SAME MATERIAL AND A 9.5 INCH REINFORCEMENTNov 14, 2010 · N38537 · Beech 1900D · Fuselage Main, StructureSDR GUUA94232111110ARelay · inoperativeDURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED ON GEAR EXTENSION. RESET BREAKER AND POPPED AGAIN. MANUALLY EXTENDED LANDING GEAR GOT DOWN LOCK INDICATION. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED 60AMP, LANDING GEAR CIRCUIT BREAKER AND LANDING GENov 11, 2010 · N47542 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA95632111110AUplock Switch · inoperativePILOT REPORTED WHEN LANDING GEAR WAS PUT UP " GEAR UNSAFE" LIGHTS REMAINED ILLUMINATED ALL GREEN "GEAR DOWN" LIGHTS EXTINGUISHED RAN QRH GEAR CAME UP NORMALY. REPLACED LT UP LOCK SWITCH OPS AND RIG CHECK GOOD.Nov 11, 2010 · N81556 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93572110910AEngine · sparksF/O REPORTED SPARKS SHOOTING OUT OF THE RT ENGINE EXHAUST NUMEROUS TIMES THROUGHOUT INITIAL CLIMB. INSPECTED RT ENGINE COMPRESSOR BLADES AND PERFORMED ENGINE PERFORMANCE RUN, NO DEFECTS NOTED.Nov 9, 2010 · N81535 · Beech 1900D · Engine (Turbine/Turboprop)SDR GUUA94532110810ASwitch · intermittentPILOT REPORTED GEAR WARNING HORN CANCELLATION BUTTON INTERMITTENTLY INOPERATIVE. REPLACED LANDING GEAR WARNING HORN SILENCE SWITCH. LANDING GEAR OPS CHECK GOOD.Nov 8, 2010 · N53545 · Beech 1900D · Landing Gear Position and WarningSDR ERAA201000006Blower Motor · failedCREW DISCOVERED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AIRPORT WHERE THEY EVACUATED THE ACFT AFTER LANDING. MX DETERMINED THAT THE FWD CABIN VENTILATION BLOWER HAD FAILED AND IT'S CURRENT LIMITER AS WELL. MX REPLACED THE UNIT WITNov 8, 2010 · N971EA · Beech 1900D · Air Distribution FanSDR GLBA20101105APressure Switch · malfunctionedLT SIDE PROP AUTOFEATHER W/ 1000LBS TQ SHORT FINAL. STOPPED AUTOFEATHERING ABOVE 1000 LBS TQ. MX INSPECTED THE SYS AND ADJUSTED THE FLIGHT IDLE TORQUE IAW AIM CH 7 SEC 2.5, PARA 2 AND REPLACED THE LOW PRESS SWITCH, RAN ENGINES, OPS CHECK GOOD IAW BMM.Nov 5, 2010 · N195GL · Beech 1900D · Propeller Feathering/ReversingSDR CA101216003Actuator · failed(CAN) SIGNIFICANT RESISTANCE FELT IN ELEVATOR TRIM WHEEL AT AFT END OF GREEN ARC DURING FLIGHT FOR TEN SECONDS AND EVERYTHING NORMAL AFTER THAT. AUTOPILOT TRIM FAIL- TRIM VERY DIFFICULT TO ADJUST UP/DOWN WHEN ABOVE 160 KIAS (OAT BELOW 0 C.) WITH ELECTRIC AND Nov 4, 2010 · Beech 1900D · Elevator Tab Control SystemSDR GUUA91252110410CHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Nov 4, 2010 · N45AR · Beech 1900D · Emergency ExitsSDR GUUA91252110410BHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED RT AFT EMERGENCY EXIT HANDLE.Nov 4, 2010 · N45AR · Beech 1900D · Emergency ExitsSDR GUUA91252110410AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED RT FWD EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED RT FWD EMERGENCY EXIT HANDLE.Nov 4, 2010 · N45AR · Beech 1900D · Emergency ExitsSDR CA101106001Skin · cracked(CAN) NOTED A 2 5/16 INCH CRACK IN LOWER LEFT FUSELAGE SKIN P/N 129-400031-51 DURING A SCHEDULED MAINTENANCE EVENT. THE CRACK IS LOCATED AT FS 303.25 WHICH IS A BULKHEAD JUST FORWARD OF THE 4TH LEFT CABIN WINDOW. THE CRACK EXTENDED FROM A RIVET HOLE AT THE BNov 3, 2010 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101101FSkin · tornMAJOR REPAIR - THE T/E OF A RT ELEVATOR WAS DAMAGED DURING SHIPPING, THE SKIN WAS TORN 46.5" TO 49.5" FROM INBD EDGE, .75" FROM T/E. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO10-1900-27-008, REV 1. MATERIALS UTILIZED ARE INCLUDED Nov 1, 2010 · N122UX · Beech 1900D · Elevator, Plate/SkinSDR GLBA201010311Bulb · missingPILOT REPORTED THAT ONE OF THERE EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE IS MISSING A BULB. MAINTENANCE REPLACED THE MISSING BULB PN 1864 AND FILTER PN D165-100-2 IAW BMM 33-10-04, OPERATIONAL CHECKS GOOD.Oct 31, 2010 · N261GL · Beech 1900D · Passenger Compartment LightingSDR GUUA93732103110ASwitch · inoperativePILOT REPORTED LANDING GEAR HAD TO BE RETRACTED BY BYPASSING THE "J" HOOK. REPLACED LANDING GEAR SWITCH OPS CHECK SATISFACTORY.Oct 31, 2010 · N38537 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94532102910APowerpack · inoperativeDURING APPROACH, WHEN THE LANDING GEAR HANDLE WAS LOWERED THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS RAISED, CIRCUIT BREAKER RESET, AGAIN WITH THE SAME RESULTS. MANUALLY EXTENDED THE LANDING GEAR THE GEAR ACCOMPOct 29, 2010 · N53545 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94535102910APowerpack · inoperativeDURING APPROACH WHEN THE LANDING GEAR HANDLE WAS LOWERED, THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS RAISED, CIRCUIT BREAKER RESET AGAIN WITH THE SAME RESULTS. MANUALLY EXTENDED THE LANDING GEAR. THE GEAR ACCOMOct 29, 2010 · N53545 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20101028AAutofeather Sys · malfunctionedPILOT REPORTED THE THE RIGHT ENGINE CYCLED IN AND OUT OF FEATHER MULTIPLE TIMES ON SHORT FINAL, STARTED WITH TORQ AT 1K AND STOPPED WHEN BROUGHT ABOVE 2K TORQ, N1 AT 90-91% AT THAT TIME. MAINTENANCE INSPECTED THE LOW PITCH SOLONOID IAW MM 61-20-00, PERFORMED OOct 28, 2010 · N170GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA95453102810ASkin · chafedDURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE LT PRESSURE PLATE AREA APPROX FS 258 AT WS 305. REPAIRED SKIN CHAFE INSTALLED DOUBLER 2.5 X 10.5 INCHES ON LT PRESSURE PLATE AREA AT FS 258, WS 305.Oct 28, 2010 · N87554 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101027GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" CRACK IN THE LT HEAVY ANGLE IN THE BEND RADIUS AT FS 303.25. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-061. MATERIALS UTILIZED ARE INCLUDED IN THEOct 27, 2010 · N184UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20101027FSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR DEBONDED AT THE HINDGE ATTACH AREA AND OUTER SKIN DEBONDED 3.5" TO 4" INWARD FROM EDGE OF DOOR. MX REPLACED THE AIRSTAIR DOOR IAW MM 52-10-03, OPS CHECK GOOD, COMPLIED WITH ALL RII REQOct 27, 2010 · N184UX · Beech 1900D · Passenger/Crew DoorsSDR GUUA95453102610ADoor Frame · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED CARGO DOOR FRAME UPPER FWD AREA CRACKED APPOX 2.5 INCHES AT FS 460 AT STRINGER 3L. STOP DRILLED ENDS OF CRACK AND INSTALLED DOUBLER REPAIR.Oct 26, 2010 · N87554 · Beech 1900D · Fuselage Main, StructureSDR GUUA93952102610AHandle · stickingDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT OUTER HANDLE STICKING. CLEANED AND LUBRICATED LT EMERGENCY EXIT OUTER HANDLE.Oct 26, 2010 · N82539 · Beech 1900D · Emergency ExitsSDR GUUA95453102510CAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR FWD ANGLE CRACKED AT LOWER SNUBBER ATTACH POINTS APPROX FS 150 AT STR 9L. REMOVED 28 INCH SECTION OF -3 ANGLE AND INSTALLED -3 FILLER ANGLE AND 8.5 INCH UPPER SPLICE AND 6.5 INCH LOWER -11 SPLICE ANGLE.Oct 25, 2010 · N87554 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA95453102510BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT HEAVY ANGLE CRACKED AT APPROX FS 288.0 IN RADIUS. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE CLIP AND FASTNERS AS REQUIRED.Oct 25, 2010 · N87554 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA95453102510AAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED RT HEAVY ANGLE CRACKED AT APPROX FS 288.0 IN RADIUS. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE CLIP AND FASTNERS AS REQUIRED.Oct 25, 2010 · N87554 · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20101020Skin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE BELLY SKIN CORRODED AT FS 213.25 BETWEEN STR 16 AND STR 15R. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-059. MATERIALS UTILIZED ARE INCLUDEDOct 19, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2010102010Skin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE BELLY SKIN CORRODED AT FS 228.25 BETWEEN STR 16 AND STR 15R. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-059. MATERIALS UTILIZED ARE INCLUDED Oct 19, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101018FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A 1.7" CRACK IN THE RT HEAVY ANGLE FROM FS 288 GOING AFT 1.7" IN BEND RADIUS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-058. MATERIALS UTILIOct 18, 2010 · N254GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93932101510AAnnunciator · malfunctionedPILOT REPORTED GREEN "NOSE" ANNUNCIATOR FOR LANDING GEAR FLICKERS. NO DEFECTS NOTED COULD NOT DUPLICATE. OPS CHECKS GOOD .Oct 15, 2010 · N82539 · Beech 1900D · Landing Gear Position and WarningSDR CA101102010Actuator · malfunctioned(CAN) DURING DESCEND PITCH TRIM VERY STIFF, ELECTRIC TRIM BEING INOP. MANUAL TRIM STIFF. TRIM SPRINGS BACK WHEN HANDWHEEL RELEASED. PITCH TRIM DID NOT FAIL ON GROUND.Oct 14, 2010 · Beech 1900D · Elevator Tab Control System
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