Raytheon 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 CA000128012Actuator · failed(CAN) ON APPROACH THE FLIGHT CREW SELECTED GEAR DOWN. THE NOSE LANDING GEAR ANNUNCIATOR DOWN & LOCKED INDICATION DID NOT ILLUMINATE. THERE WAS NO INTRANSIT LIGHT ILLUMINATING. THE NOSE GEAR ACTUATOR WAS REPLACED DUE TO AN INTERMITTANT INTERNAL MICROSWITCH.Jan 12, 2000 · Beech 1900D · Landing Gear ActuatorSDR AU000128012Actuator · failed(AU) ON APPROACH, THE FLIGHT CREW SELECTED GEAR DOWN. THE NOSE LANDING GEAR ANNUNCIATOR DOWN AND LOCKED INDICATION DID NOT ILLUMINATE. THERE WAS NO INTRANSIT LIGHT ILLUMINATING. THE NOSE GEAR ACTUATOR WAS REPLACED DUE TO AN INTERMITTANT INTERNAL MICROSWITCHJan 12, 2000 · Beech 1900D · Landing Gear Door ActuatorSDR C2XA00CL004Eva Tube · failedCLE - FLT 3221 - THE CREW REPORTED A LEFT BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT WHEN PASSING THROUGH 10,500 FEET ALTITUDE. THE LIGHT EXTINGUISHED WHEN THEY DESCENDED BELOW 6,500 FEET ALTITUDE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT.Jan 10, 2000 · N49543 · Beech 1900D · Engine DrainsSDR S2YA00001Motor · failedFLT 1120 - MKE-GRR - SHORTLY AFTER TAKEOFF, THE CREW SELECTED GEAR UP. THE RED GEAR HANDLE (INTRANSIT) LIGHT ILLUMINATED AND THE LANDING GEAR RELAY CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB AND IT POPPED AGAIN. THE CREW THEN SELECTED GEAR DOWN AND Jan 6, 2000 · N145SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 20000424AP041Encoder · failedCAPTAINS ALTIMETER FLAGGED IN FLIGHT. REMOVED AND REPLACED CAPTAINS ALTIMETER. BENCH TEST OF ALTIMETER COULD NOT DUPLICATE THE FLAGGING DISCREPANCY BUT DID REVEAL THAT THE ENCODER WAS NOT FUNCTIONING. (M)Jan 5, 2000 · N150UX · Beech 1900D · Altimeter, Barometric/EncoderSDR CA000120037Wire · broken(CAN) RPTED BY CREW THAT DIM POTENTIOMETER WAS NOT DIMMING LIGHTS FOR FLT CNTL PANELS & ANNUNCIATORS. WIRING BUNDLE BEHIND RADIO PANEL FOUND TO HAVE A BLACK DISCOLORATION. FURTHER INVESTIGATION FOUND WIRE TO BE BROKEN AS IT HAD BEEN CHAFFINGAGAINST CENTRE FOJan 3, 2000 · Beech 1900D · Light System WiringSDR 2000ZZZX450Gyro · intermittentNR 1 DIRECTIONAL GYRO PRECESSES INTERMITTENTLY IN THE FREE AND SLAVED MODES. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. COMP P/N DGS-65/622-6136-002.Jan 3, 2000 · N169GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 2000ZZZX470Seal · leakingPOST-FLIGHT INSPECTION FOUND OIL LEAKING FROM RT ENGINE LOWER FORWARD COWL. INSPECTION REVEALED THE SOURCE OF LEAK TO BE THE POWER SECTION OIL TRANSFER TUBE ELBOW. REPLACED 3 EACH PACKINGS. LEAK CHECK SATISFACTORY ON GROUND RUN.Dec 30, 1999 · N835CA · Beech 1900D · Engine Oil Distribution (Airframe Furnished)SDR 2000ZZZM88Yaw Damper · malfunctionedYAW DAMPER ENGAGED ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FLIGHT CONTROL PANEL. SYSTEM TESTS SATISFACTORY. (M)Dec 30, 1999 · N260GL · Beech 1900D · Autopilot SystemSDR CA000128063Bearing · worn(CAN) DURING REMOVAL OF THE COMPRESSOR SUPPORT ASSY FOUND PULLEY ) WAS CHAFFING AGAINST THE COMPRESSOR DRIVE SUPPORT ). BOTH PARTS WERE WORN DUE TO FRICTION.ALSO FOUND THEQUILL SHAFT TEETH BADLY DAMAGED AND THE BEARING EDGE WORN.SUSPECT THE BEARING LOCATED INDec 28, 1999 · Beech 1900D · Cabin Compressor SystemSDR CA000120001Control Cable · frayed(CAN) DURING INSPECTION OF CONTROL CABLES BENEATH FLOORBOARDS, IT WAS DISCOVERED THAT THE ELEVATOR DOWN CABLE WAS FRAYED AT STATION 522.5, LOCATED UNDER THE AFT CARGO FLOOR. THE CABLE HAD RUBBED THROUGH ITS PHENOLIC BUMPER ALLOWING IT TO RUB AGAINST THE EDGE Dec 28, 1999 · Beech 1900D · Elevator Control SystemSDR S2YA99031Harness · shortedFLT 1826 - MKE-CMH - THE STALL WARNING (HEAT) LIGHT ILLUMINATED. THE CREW CYCLED THE SWITCH SEVERAL TIMES AND THEN MADE AN AIRTURN BACK TO MKE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND HIGH RESISTANCE FOR THE GROUND WIRE ON THE LEFT SQUAT SWITCH. MAINTENADec 27, 1999 · N145SK · Beech 1900D · Landing Gear Position and WarningSDR 20000424AP040Gyro · intermittentNR 1 DIRECTIONAL GYRO INTERMITTENTLY FREEZES IN TURNS. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. (M)Dec 23, 1999 · N150UX · Beech 1900D · Directional Gyro and Indicating SystemSDR 2000ZZZX426Pump · leakingFUEL LEAK RIGHT ENGINE NACELLE. FOUND LOW PRESSURE FUEL PUMP LEAKING. REMOVED AND REPLACED UNIT, SYSTEM LEAK AND OPS CHECK SATISFACTORY.Dec 23, 1999 · N842CA · Beech 1900D · Engine Fuel PumpSDR 2000ZZZX424Gyro · stuckCAPTAIN'S HEADING INDICATOR STUCK. REPLACED DGS-65. SYSTEM CHECKS SATISFACTORY.Dec 23, 1999 · N843CA · Beech 1900D · Directional Gyro and Indicating SystemSDR 20000424AP039Gyro · intermittentNR 1 DIRECTIONAL GYRO INTERMITTENTLY FREEZED IN TURNS. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. (M)Dec 22, 1999 · N150UX · Beech 1900D · Directional Gyro and Indicating SystemSDR CA000118059Resistor · cracked(CAN) CREW REPORTED REDUCED AIRFLOW THROUGH CABIN VENTS. MAINTENANCE DISCOVERED FORWARD HEATER NOT WORKING. BLOWER ASSY REMOVED (P/N EM630-2/114-380028-5) AND UPON INSPECTION, FOUND TO BE VERY STIFF TO ROTATE. RESISTOR COVER REMOVED AND IT WAS DISCOVERED THDec 22, 1999 · Beech 1900D · Heating SystemSDR 2000ZZZX451Gyro · intermittentNR 1 DIRECTIONAL GYRO PRECESSES INTERMITTENTLY IN THE SLAVED MODE. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. COMPONENT P/N DGS-65/622-6136-002.Dec 22, 1999 · N169GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 2000ZZZX273Altimeter · malfunctionedALTIMETER FLAG IN VIEW. BENCH TEST CONFIRMED PROBLEM. ALTIMETER STAYS FLAGGED AT 1,000 FEET ABOVE THE PRESSURE ALTITUDE.Dec 22, 1999 · N253GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 2000ZZZX181Indicator · malfunctionedMILIBAR AND INCHES OF MERCURY SCALES DO NOT MATCH (I.E., 29.92 IN HG SHOWS 0993 MB INSTEAD OF 1013 MB).Dec 22, 1999 · N154GL · Beech 1900D · Altimeter, Barometric/EncoderSDR CA000118058Wire · failed(CAN) LOSS OF INSTRUMENT LIGHTING ON CPT AND COPILOT INSTRUMENT PANEL. LIGHTS CONTROLLED BY 2 SEPARATE POTENTIOMETERS ON OVERHEAD PANEL. PROBLEM ACTUATED C/B 21 LOCATED UNDER FLOOR WHICH FEEDS BOTH INSTRUMENT PANEL LIGHTS. MAINT FOUND THAT BEHIND AUDIO SELDec 21, 1999 · Beech 1900D · Light System WiringSDR 2000ZZZX425Governor · failedRIGHT ENGINE OVERSPEED GOVERNOR WILL NOT TEST. REPLACED GOVERNOR WITH OVERHAULED UNIT. OPERATIONAL AND LEAK CHECK SATISFACTORY.Dec 21, 1999 · N855CA · Beech 1900D · Propeller GovernorSDR S2YA99030Actuator · malfunctionedDURING APPROACH OF FLIGHT 1024, MKE-ATW, LT MAIN GEAR SAFE LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THEN MADE AN UNEVENTFUL LANDING. OUTSTATION MX INSPECTED AND PINNED THE GEAR. THE AIRCRAFT WAS FERRIED TO MKE AND INSPECTED BY Dec 20, 1999 · N92SK · Beech 1900D · Landing Gear ActuatorSDR CA991229035Indicator · malfunctioned(CAN) PILOT REPORTED R/H N1 GAUGE READING 115% IN SPITE OF NORMAL ENGINE PERFORMANCE. N1 INDICATOR WAS REPLACED.Dec 18, 1999 · Beech 1900D · Engine RPM Indicating SystemSDR C2XA99CL128Switch · failedCLE - FLT 3134 - AFTER TAKEOFF FROM CLE, LEFT AUTOFEATHER ADVISORY (GREEN) LIGHT AND REPEATER (AFX) FAILED TO ILLUMINATE. AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE LOW PRESSURE AUTOFEATHER SWITCH IAW BEECDec 17, 1999 · N81553 · Beech 1900D · Propeller Synchronizer SectionSDR 2000ZZZX94Indicator · failedCAPTAIN'S ALTIMETER FAILED ON TAKEOFF. REMOVED AND REPLACED NR 1 ALTIMETER. TESTED OK. COMPONENT P/N KEA3460663-3062-00. (X)Dec 16, 1999 · N96UX · Beech 1900D · Altimeter, Barometric/EncoderSDR CA000128062Drive Shaft · broken(CAN) AFTER LANDING THE PILOT SELECTED THE FLAP UP AND THEY JAMMED AT 17 DEGREES. INVESTIGATION FOUND THE RT OUTBOARD FLAP FLEX DRIVE WAS BROKEN APPROXIMATELY 24 INCHES FROM THE END.DAMAGED PARTS REPLACED.Dec 15, 1999 · Beech 1900D · Trailing Edge Flap ActuatorSDR AU000128062Flex Drive · broken(AU) AFTER LANDING , THE PILOT SELECTED THE FLAP UP AND THEY JAMMED AT 17 DEGREES. INVESTIGATION FOUND THE R/T OUTBOARD FLAP FLEX DRIVE WAS BROKEN APPROXIMATELY 24INCHES FROM THE END. DAMAGED PARTS REPLACED.Dec 15, 1999 · Beech 1900D · Trailing Edge Flap Control SystemSDR CA000118056Wire · broken(CAN) ON APPROACH TO GOOSE BAY, THE CREW NOTED THERE WAS NO DOWN AND LOCKED INDICATION (GREEN) FOR THE NOSE GEAR. MAINTENANCE DISCOVERED A BROKEN WIRE AT THE ENTRY INTO THE MICROSWITCH ON THE NOSE GEAR ACTUATOR. ACTUATOR REPLACED.Dec 7, 1999 · Beech 1900D · Landing Gear System WiringSDR CA991229034Actuator · failed(CAN) DURING APPROACH IN WAS DISCOVERED THAT THE NOSE LANDING GEAR LIGHT FAILED TO ILLUMINATE.UPON INSPECTION MAINTENANCE NOTED THE NOSE LANDING GEAR INTERNAL DOWNLOCK SWITCH HAD HIGH RESISTANCE. THE ACTUATOR (BY FRISBY) WAS REPLACED.Dec 6, 1999 · Beech 1900D · Landing Gear ActuatorSDR CA991229033Annunciator · inoperative(CAN) DURING APPROACH THE NOSE GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN. GEAR MANUALLY EXTENDED.THE ANNUNCIATOR WAS REPLACED.Dec 6, 1999 · Beech 1900D · Landing Gear Position and WarningSDR CA991229032Wire · chafed(CAN) DURING CRUISE THE 2 AMP MLG CONTROL CIRCUIT BREAKER TRIPPED AND WASN''T ABLE TO RESET. EXTENSIVE TESTING COULD NOT DUPLICATE FAULT. THE LANDING GEAR RELAY WAS REPLACED AND FAULT REAPPEARED ON TEST FLIGHT. EXTENSIVE INSPECTION OF WIRING FROM THE C/B TODec 4, 1999 · Beech 1900D · Landing Gear System WiringSDR C2XA99IA626Actuator · inoperativeCLE - FLT 3009, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW BEECH MM 32-30-10, AND THE AIDec 3, 1999 · N87557 · Beech 1900D · Landing Gear ActuatorSDR C2XA99CL127Actuator · failedCLE - FLT 3009 - AFTER TAKEOFF FROM CLE, THE LANDING GEAR WOULD NOT RETRACT. GREEN INDICATION LIGHTS REMAINED ON WITH NO INTRANSIT LIGHT. AIRCRAFT RETURNED TO CLE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAWDec 3, 1999 · N87557 · Beech 1900D · Landing Gear ActuatorSDR 2000ZZZM95Pump · leakingRIGHT ENGINE LOWER PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M)Nov 29, 1999 · N842CA · Beech 1900D · Fuel Boost PumpSDR 2000ZZZM94Pump · leakingLEFT ENGINE LOW PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M)Nov 29, 1999 · N842CA · Beech 1900D · Fuel Boost PumpSDR 2000ZZZM92Actuator · bindingNOSE WHEEL STEERING FAILS TO TURN FREE IN POWER OR CASTOR MODES. STEERING ACTUATOR REPLACED. (M)Nov 23, 1999 · N833CA · Beech 1900D · Steering UnitSDR 2000ZZZM90Anchor · brokenAIRSTAIR DOOR, FORWARD TOP CABLE ANCHOR BROKEN. REPLACED ANCHOR WITH NEW PART MANUFACTURED FROM WRONG MATERIAL. (M)Nov 23, 1999 · N846CA · Beech 1900D · Entrance StairsSDR 2000ZZZM93Blade · looseLEFT PROPELLER BLADE MOVEMENT OUTSIDE ALOOWABLE LIMITS IN HARTZELL SERVICE INSTRUCTIONS. PROPELLER REMOVED AND REPLACED. (M)Nov 22, 1999 · N855CA · Beech 1900D · Propeller Blade SectionSDR 2000ZZZM91Actuator · leakingNOSE WHEEL STEERING ACTUATOR LEAKS FLUID. REPLACED STEERING ACTUATOR. (M)Nov 22, 1999 · N836CA · Beech 1900D · Steering UnitSDR 99ZZZX4611Actuator · failedPILOT IN APPROACH LANDING NOTICED NOSE GEAR WAS NOT LOCKED. TALKED TO THE TOWER AND THEY CONFIRMED THAT, PILOT TRIED TO EXTEND BY EMERGENCY AND AGAIN COULD NOT LOCK NOSE GEAR. AIRCRAFT LANDED HARD AND NOSE GEAR LOCKED UP IN VERY LAST MOMENT AFTER PILOT PUT MNov 12, 1999 · N2FOR · Beech 1900D · Landing Gear ActuatorSDR CA991208063Dc Power · failed(CAN) COMPLETE DC POWER FAILURE DUE TO LIGHTNING STRIKE EXPERIENCED. PART TC: 6,665.Nov 10, 1999 · Beech 1900D · DC Power Distribution SystemSDR C2XA99CL122Thermocouple · failedCLE - FLT 3439 - THE CREW REPORTED THAT AFTER TAKEOFF THE RIGHT ITT WENT TO 810C WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TRIM THERMOCOUPLE IAW P/W MM 77Nov 8, 1999 · N87552 · Beech 1900D · Engine EGT/TIT Indicating SystemSDR CA000128064Pin · worn(CAN) DURING MAINTENANCE INSPECTION, FOUND PARTS OF THE INERTIAL ICE VANE CONTROL LINKAGE LYING ON THE BOTTOM OF THE COWLING JUST BELOW INLET SCREEN. HARDWARE REPLACED.Nov 7, 1999 · Beech 1900D · Air Intake Anti/De-Ice SystemSDR 99ZZZM796Engine · seizedUPON A NORMAL ENGINE START AT GATE, LEFT ENGINE EMITTED AN ABNORMAL PITCH NOISE FOLLOWED BY A DROP IN N1 SPEED AND A RISE IN ITT INDICATION. OTHER ENGINE INDICATIONS ALSO, INDICATED ABNORMAL INDICATIONS. ENGINE WAS REPLACED. (M)Nov 5, 1999 · N852CA · Beech 1900D · Engine (Turbine/Turboprop)SDR CA991116002Relay · pitted(CAN) THE LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN. MANUAL EXTENSION SELECTED, ALL GEAR LOCKS INDICATING GREEN. INSPECTION FOUND THE LANDING GEAR RELAY CONTACTS WERE PITTED AND ARCED. RELAY REPLACED.Nov 4, 1999 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR C2XA99IA573Switch · out of rigIAH - FLT 3695 - THE CREW ABORTED TAKEOFF DUE TO THE AUTO FEATHER SYSTEM NOT ARMING. MAINTENANCE ADJUSTED THE AFFECTED PEDESTAL MICROSWITCH IAW BEECHCRAFT 1900D MM 61-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Nov 3, 1999 · N17534 · Beech 1900D · Propeller Feathering/ReversingSDR AU991093Mount · worn(AUS) RIGHT ENGINE TRUSS CHAFED BY A CONNECTION ON THE AIR CONDITIONING COMPRESSOR SUCTION LINE.Nov 3, 1999 · Beech 1900D · Engine Mount SectionSDR 2000ZZZM233Nr 1 Bearing · failedDURING CLIMB-OUT AT 3000 FT, LEFT ENGINE EMITTED FLAMES FROM EXHAUST STACK, PRECEDED BY 'POP' NOISE. ENGINE WAS SECURED, EMERGENCY DECLARED AND THE AIRCRAFT RETURN TO FIELD WITHOUT INCIDENT. (M)Nov 3, 1999 · N862CA · Beech 1900D · Turbine Engine Compressor SectionSDR CA991112035Circuit Breaker · failed(CAN) CREW REPORTED BURNING ODOR IN THE COCKPIT WHICH WOULD DISSIPATE AFTER A FEW MOMENTS. IT WAS NOTED THAT THE LEFT PITOT HEATER CIRCUIT BREAKER HAD TRIPPED. INVESTIGATION FOUND ONE TERMINAL ON THE SELECTOR SWITCH WAS LOOSE AND SHOWED SIGNS OF EXCESSIVE HENov 1, 1999 · Beech 1900D · Pitot/Static Anti-Ice System
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