Raytheon 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 MASA00055Light · dislodgedFLT 109 - COS-DEN - HAD AN EMERGENCY EXIT SIGN ASSY FELL OFF IN THE PASSENGER CABIN. THE SIGN WAS REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 23, 2000 · N114YV · Beech 1900D · Emergency LightingSDR C2XA00CL049Skin · failedDURING A 1ST 200 HOUR INSPECTION, A 3 INCH CRACK WAS FOUND ON THE RIGHT SIDE EXTERIOR SKIN OF AIRCRAFT MIDSECTION INBOARD OF PANEL 611AB NEAR THE MAIN SPAR. MAINTENANCE REMOVED THE INTERIOR FOR INSPECTION OF THE SPAR AND SURROUNDING AREAS AND FOUND NO OTHER DJun 20, 2000 · N81536 · Beech 1900D · Fuselage Main, Plate/SkinSDR CA000726004Drive Shaft · worn(CAN) INITY MAINT NOTIFIED THAT WHEN SELECTING FLAPS TO UP POS (ON GROUND) THAT FLAP IND. SHOWING 20 DEGS&THAT FLAPS WERE NOT ABLE TO RETRACT ANY FURTHER. MAINT FOUND L/H INBOARD FLAP IN APPROX. 25DEGS DOWN POS,&THAT FLAP SPLIT SYS PREVENTING FURTHER FLAP-MOTJun 19, 2000 · Beech 1900D · Trailing Edge Flap ActuatorSDR CA000731023Cooler · cracked(CAN) PILOTS REPORT RT ENGINE RUNNING HOTTER THAN LT. RT PRECOOLER HAD CRACK IN IT, P3 AIR STRIKING OIL COOLER CAUSED LEAK. SMALL AMOUNT OF OIL COMING FROM OIL COOLER, P/N 114-3890005. THIS IS ONE OF TWO INSTANCES OF PRECOOLER BURNING INTO OIL COOLER THIS MONTJun 16, 2000 · Beech 1900D · Pneumatic Distribution SystemSDR CA000614059Tube · cracked(CAN) RT BLEED AIR FAIL WARNING LIGHT COME ON DURING FLIGHT. AFTER INVESTIGATION WE FOUND THAT LINE P/N 129-970032-1 WAS CRACKED AT WELDING JOINT OF THREADED FITTING.Jun 14, 2000 · Beech 1900D · Air Intake Anti/De-Ice SystemSDR S2YA00016Heater · inoperativeMKE-DSM - FLT 1843 - DURNG FLIGHT, THE LEFT WINDSHIELD STARTED TO DEVELOP ICE WITH THE WINDSHIELD HEAT SELECTED ON. THE FLIGHT CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE WINDSHIELD AND OP CHECKED IT. THE A/C WAS RETURNED Jun 14, 2000 · N108SK · Beech 1900D · Windshield/Door Rain/Ice RemovalSDR CA000706023Bulb · failed(CAN) ON APPROACH TO PENTICTION NOSE GEAR LIGHTS DID NOT ILLUMINATE. INTRANSIT LIGHT WAS EXTINGUISHED & NOSE LIGHTS DID NOT ILLUMINATE DURING PRESS TO TEST. PILOT DID FLYBY OF TOWER & ALL LOOKED GOOD. HE THEN ELECTED NOT TO LAND BUT RETURN TOCALGARY WHERE HE DJun 13, 2000 · Beech 1900D · Landing Gear Position and WarningSDR AU000583Flap · out of adj(AUS) FLAPS OUT OF ADJUSTMENT.Jun 13, 2000 · Beech 1900D · Trailing Edge Flap Control SystemSDR CA000713007Bearing · failed(CAN) CREW WAS ON CLIMB AT 8000 FT WHEN NR 1 ENGINE FLAMEOUT. THEY SECURED ENGINE & RETURNED TO BASE WHERE THEY PERFORMED AN UNEVENTFUL EMERG LDG. UPON NOTIFYING MAINT THEY WERE ASKED TO GO OUT & TRY A START CYCLE ON NR 1 ENGINE. START CYCLE WAS CARRIED OUT WJun 12, 2000 · Beech 1900D · Turbine SectionSDR S2YA00014Shutoff Valve · inoperativeFLT 1024 - MKE-CVG - DURING FLIGHT, THE CABIN ALT HI ANNUNCIATOR ILLUMINATED AT FL 230. THE FLIGHT CREW NOTED THE CABIN ALTITUDE WAS AT FL 100 AND CLIMBING. SO THE CREW DEPLOYED THE OXYGEN MASKS, DIVERTED TO FWA AND MADE AN UNEVENTFUL LANDING. THE CREW CONTJun 9, 2000 · N148SK · Beech 1900D · Cabin Pressure Control SystemSDR 20000816AP001Valve · leakingLANDING GEAR FAILED TO EXTEND ELECTRICALLY OR MANUALLY. AIRCRAFT SUSTAINED PROP AND AIRFRAME DAMAGE FROM GEAR UP LANDING. SUSPECT SERVICE VALVE MALFUNCTIONING AS THE PROBLEM. INCIDENT UNDER INVESTIGATION. (M)Jun 3, 2000 · N853CA · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 20000725AP001Skin · corrodedDURING INSPECTION, FOUND CORROSION WAS NOT NOTED UNDER THE FORWARD VENT BLOWER RESISTOR BLOCK. THE DAMAGE TO THE FUSELAGE SKIN WAS BEYOND LIMITS. THE DAMAGED AREA WAS REMOVED, AND REPAIRED IAW THE BEECHCRAFT STRUCTURAL REPAIR MANUAL. THE REMAINEDER OF THE FJun 2, 2000 · N101UX · Beech 1900D · Fuselage Main, Plate/SkinSDR S2YA00012Computer · inoperativeFLT 1090 - LSE-MKE - SHORTLY AFTER TAKEOFF, THE GPWS COMMANDED PULL UP, PULL UP. THE CREW CONTINUED TO CLIMB BUT THE GPWS WOULD NOT STOP, SO THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAINTENANCE WAS CONSULTED AND THE GPWS WAS PUT ON MEL. MAIJun 1, 2000 · N92SK · Beech 1900D · Ground Proximity SystemSDR C2XA00CL043Switch · failedCLE - FLT 3150 - THE CREW REPORTED AFTER TAKEOFF FROM CLEVELAND, THE GEAR HANDLE WOULD NOT MOVE. THE RED DOWN LOCK RELEASE BUTTON WAS DEPRESSED TO MOVE GEAR TO UP POSITION. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED ANDMay 29, 2000 · N69549 · Beech 1900D · Landing Gear SelectorSDR MASA00048Indicator · malfunctionedFLT 142 - COS-ABQ - DURING FLIGHT, THE CREW EXPERIENCED A ZERO OIL PRESSURE READING FROM THE LEFT ENGINE. AFTER LANDING MAINTENANCE RESEATED THE CONNECTOR AND SWAPPED GAUGES. OPS CHECK GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)May 27, 2000 · N104YV · Beech 1900D · Engine Oil Indicating SystemSDR 20000725AP007Controller · seizedDURING CLIMB-OUT FROM SYR, CREW DETECTED AND ELECTRICAL SHORT SMELL, FOLLOWED BY PRESSURIZATION FAILURE. AIRCRAFT RETURNED TO THE FIELD AND MAINTENANCE PERFORMED A THOROUGH INSPECTION OF CENTER CONSOLE WHERE PRESSURIZATION CONTROLLER IS MOUNTED. INSPECTION RMay 24, 2000 · N837CA · Beech 1900D · Cabin Pressure ControllerSDR 20000620SH013Gyro · inoperativeGYRO INOPERATIVE. (X)May 16, 2000 · N208GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 20000620SH012Gyro · precessesGYRO REMOVED FOR PRECESSING, NO FURTHER INFORMATION IS AVAILABLE. (X)May 16, 2000 · N153GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 20000620SH011Gyro · looseUNIT WAS REMOVED FOR LOOSE HARDWARE, NO FURTHER INFORMATION AVAILABLE. THE HARDWARE IN QUESTION WAS RELATED TO THE D-SUB CONNECTOR TIE-DOWNS MOUNTED TO THE CASE. (X)May 16, 2000 · N255GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 20000525SH002Gyro · malfunctionedDEN/GCC - FLIGHT DIVERTED TO CYS WHEN THE FIRST OFFICER''''S DIRECTIONAL GYRO BEGAN TO PRECESS AND STICK. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FIRST OFFICER''''S DIRECTIONAL GYRO. GROUND OPS CHECK WAS SATISFCTORY. SUBMITTER STATED THIS GYRO HAD PMay 14, 2000 · N228GL · Beech 1900D · Directional Gyro and Indicating SystemSDR EY2R56446AErosion Shield · debondedCRACKED AND DEBONDED FROM BLADE BENEATH DE-ICER BOOT. SEPARATED FROM BLADE AND REMAINED ATTACHED TO DE-ICER DURING REMOVAL OF DE-ICER.May 12, 2000 · Beech 1900D · Propeller Blade SectionSDR EY2R56446Bearing · corrodedBLADE BEARING CORRODED.May 12, 2000 · Beech 1900D · Propeller Blade SectionSDR C2XA00CL044Compressor · failedCLE - FLT 3377 - THE CREW REPORTED THE SMELL OF SMOKE AND UNUSUAL VIBRATION NOTED AFTER LANDING. THE CREW TURNED OFF THE MODE CONTROLLER AND THE SMELL OF SMOKE AND THE VIBRATION STOPPED. MAINTENANCE INSPECTED AND FOUND THE VCM COMPRESSOR FROZEN. THE AIRCRAFMay 11, 2000 · N69549 · Beech 1900D · Cabin Compressor SystemSDR 20000508SH027Gyro · malfunctionedPILOT REPORT WAS ''RED FLAG FO EA01'' AND GREEN TAG INFO WAS ''ROLLS''. (X)May 8, 2000 · N151UX · Beech 1900D · Attitude Gyro and Indicating SystemSDR C2XA00IA118Panel · malfunctionedIAH - DURING MAINTENANCE INSPECTION, DISCOVERED THE NR 1 ENGINE WOULD SPOOL UNCOMMANDED WHEN ELECTRICAL POWER WAS CONNECTED. MAINTENANCE REMOVED AND REPLACED THE NR 1 POWER SUPPLY PANEL IAW BEECH 1900 MM 24-30-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SMay 7, 2000 · N81556 · Beech 1900D · AC Power Distribution SystemSDR 20000620SH014Altimeter · reads highALTIMETER REMOVED FROM AIRCRAFT FOR RECERTIFICATION. ENCODER FUNCTIONED PROPERLY. ALTITUDE READOUT WAS 60 FEET TO 110 FEET HIGH IN REFERENCE TO A CALIBRATED PITOT STATIC TEST SET. THE ALTITUDE READOUT WAS OBSERVED HIGH PR AT -1,000 FEET TO 2,000 FEET. NO FMay 4, 2000 · N122UX · Beech 1900D · Altimeter, Barometric/EncoderSDR EY2R56379Fork · crackedFORWARD EARS OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 1 EACH CRACK.May 3, 2000 · Beech 1900D · Propeller AssemblySDR EY2R55536Fork · crackedFORWARD EARS OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 4 EACH CRACKS.May 3, 2000 · Beech 1900D · Propeller AssemblySDR EY2R56219ABracket · crackedBRACKET CRACKED AT MOUNTING HOLE.May 3, 2000 · Beech 1900D · Propeller AssemblySDR EY2R56219Fork · crackedFORWARD EARS OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 2 EACH CRACKS.May 3, 2000 · Beech 1900D · Propeller AssemblySDR C2XA00IA113Engine · malfunctionedAEX - FLT 3413 - CREW REPORTED THE NR 2 ENGINE WOULD NOT MAKE TAKEOFF POWER. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE NR 2 ENGINE BLEED AIR VALVE IAW PRATT & WHITNEY PT6 MM 75-30-00, AND AIRCRAFT WASMay 2, 2000 · N81556 · Beech 1900D · Engine (Turbine/Turboprop)SDR 20000517SH012Gyro · intermittentFREEZES UP IN TURNS INTERMITTENTLY.May 1, 2000 · N211UX · Beech 1900D · Attitude Gyro and Indicating SystemSDR C2XA00CL035Pressure Switch · failedCLE - FLT 3165 - THE CREW REPORTED THE NR 2 PROPELLER FEATHERED IN FLIGHT WITH THE AUTOFEATHER SWITCH IN THE ARM POSITION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMVOED AND REPLACED THE NR 2 ENGINE AUTOFEATHER LOW PRESSURE SWITCH IAW BEECApr 30, 2000 · N81553 · Beech 1900D · Propeller Feathering/ReversingSDR 20000703AP002Circuit Breaker · failedAFTER ENGINE START, CREW SMELLED ELECTRICAL SMOKE ODOR (NO SMOKE VISIBLE) THAT ORIGINATED AT THE CABIN BRIEFER CIRCUIT BREAKER. POWER WAS REMOVED FROM TEH CABIN BRIEFER AND THE AIRCRAFT WAS SHUT DOWN. CABIN BRIEFER CIRCUIT BREAKER WAS REPLACED AND THE CABIN Apr 28, 2000 · N100UX · Beech 1900D · Electrical Power SystemSDR 20000703AP007Radar · failedDURING CRUISE FLIGHT, CREW SMELLED ELECTRICAL SMOKE ODOR (NO SMOKE VISIBLE) FOLLOWED BY FAILURE OF THE WEATHER RADAR. RADAR SYSTEM WAS DEACTIVATED AND THE AIRCRAFT RETURNED TO DEN. MAINTENANCE PERSONNEL REPLACED THE WXP-840A RADAR CONTROL PANEL. OPS CHECKEDApr 24, 2000 · N254GL · Beech 1900D · Weather Radar SystemSDR 20000703AP006Gyro · malfunctionedFIRST OFFICERS EADI DISPLAY IS INTERMITTENT WITH ALL FLAGS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS VERTICAL GYRO. SYSTEM GROUND TESTED OK. (M)Apr 20, 2000 · N154GL · Beech 1900D · Attitude Gyro and Indicating SystemSDR 20000426SH012Rod · damagedDURING OVERHAUL PROCESS, MAG PARTICLE INSPECTION REVEALED AN INDICATION AT THE BASE OF THE PISTON NUT THREADS. INDICATION WAS DETERMINED TO BE AN INCLUSION IN THE BASE MATERIAL. (X)Apr 6, 2000 · Beech 1900D · Propeller AssemblySDR C2XA00CL033Brake · failedCLE - FLT 3372 - AFTER LANDING IN CRW, THE CREW REPORTED HIS LEFT BRAKE FAILED DURING TAXI TO THE GATE. THE AIRCRAFT CONTINUED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE BRAKE SYSTEM IAW BEECHCRAFT MM 12-10-00. PERFORMED AIRCRAFT TAXI ANApr 5, 2000 · N17541 · Beech 1900D · Landing Gear Brake SystemSDR C2XA00IA092Fire Loop · defectiveRIC - FLT 3056 - THE CREW REPORTED THAT THE NR 2 ENGINE FIRE LOOP LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO RIC WHERE IT LANDED WITHOUT INCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE BOTTLE. FLT 4378, WHEN TAKEOFF POWER WAS AApr 2, 2000 · N81546 · Beech 1900D · Fire DetectionSDR S2YA00008Pcu · malfunctionedFLT 1073 - GRB-CWA - DURING APPROACH, THE CREW SELECTED GEAR DOWN BUT THE GEAR DID NOT EXTEND AND THE LANDING GEAR CB POPPED. THE CREW MANUALLY PUMPED THE GEAR DOWN AND ACHIEVED THREE GREEN DOWN AND LOCKED INDICATION. THE CREW MADE AN UNEVENTFUL LANDING AND Mar 29, 2000 · N81SK · Beech 1900D · Landing Gear Position and WarningSDR 20000615AP002Circuit Board · inoperativeIN CRUISE FLIGHT CREW REPORTED DUAL ENVIRONMENTAL FAIL INDICATION. PRESSURIZATION SYSTEM FAILED. FOUND ENVIRONMENTAL SYSTEM PRINTED CIRCUIT BOARD INOPERATIVE. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. (M)Mar 29, 2000 · N195GL · Beech 1900D · Air Distribution SystemSDR 20000614AP010Wire · chafedLANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. CIRCUIT BREAKER FOR LANDING GEAR RELAY POPPED. FOUND WIRE G15G22 CHAFED IN FUSELAGE WHERE WIRE BUNDLE ENTERS FUSELAGE FROM LEFT WING. REPAIRED CHAFED WIRE. RETRACTION CHECK GOOD. (M)Mar 29, 2000 · N225GL · Beech 1900D · Landing Gear System WiringSDR 20000614AP009Warning System · activatedFIRE INDICATION DURING TAKEOFF, TAKEOFF WAS ABORTED. FIRE WAS EXTINGUISHED USING ENGINE FIRE EXTINGUISHER. AFTER REMOVAL OF THE COWLING THE REMAINS OF A PIECE OF PAPER TOWEL WAS FOUND. A PAPER TOWEL HAD BEEN LEFT ON TOP OF THE POWER SECTION DURING MAINTENANMar 29, 2000 · N262GL · Beech 1900D · Fire DetectionSDR 20000508SH029Altimeter · inaccuratePILOT WRITE-UP WAS ''GIVES ERRONEOUS READINGS AND FAILNG TCAS''. BENCH CHECK INDICATED ENCODER PULSES B4 AND C1 INOPERATIVE AND ALTIMETER IS 50 FEET HIGH (30 FEET OUT OF LIMITS) FROM -1,000 FEET TO 2,000 FEET. UNIT WAS SENT FOR REPAIR. (X)Mar 29, 2000 · N247GL · Beech 1900D · Altimeter, Barometric/EncoderSDR S2YA00007Engine · leakingFLT 1064 - SDF-MKE - THE LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 60-90 PSI. THE CREW DIVERTED TO IND AND HAD OUTSTATION MAINTENANCE SERVICE AND INSPECT THE LEFT ENGINE. THE A/C CONTINUED ONTO MKE AND MAINTENANCE INSPECTED THE ENGINE AGAIN. THE OIL CONSUMar 28, 2000 · N148SK · Beech 1900D · Turbine Engine Oil SystemSDR C2XAOOIA080Torque Tube · damagedIAH - DURING 200 HOUR INSPECTION, THE RIGHT ELEVATOR WAS FOUND TO HAVE PLAY AT THE TORQUE TUBE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TORQUE TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 27, 2000 · N47542 · Beech 1900D · Elevator StructureSDR 20001011SH007Skin · puncturedAIRCRAFT WOULD NOT PRESSURIZE. AFTER LANDING, FOUND TWO HOLES IN THE RIGHT SIDE OF THE FUSELAGE BELOW THE FLOORBOARD LEVEL. FOUND WHEEL ON RIGHT LANDING GEAR IN THE NR 4 POSITION HAD A PIECE MISSING FROM THE INNER WHEEL HALF (BRAKE SIDE). THE PIECE HAD BEENMar 26, 2000 · N226GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 20001011AP012Skin · puncturedAIRCRAFT WOULD NOT PRESSURIZE. AFTER LANDING FOUND TWO HOLES IN THE RIGHT SIDE OF THE FUSELAGE BELOW THE FLOORBOARD LEVEL. FOUND WHEEL ON RIGHT LANDING GEAR IN THE NR 4 POSITION HAD A PIECE MISSING FROM THE INNER WHEEL HALF (BRAKE SIDE). THE PIECE HAD BEEN TMar 26, 2000 · N226GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 20000619AP015Wheel · brokenAIRCRAFT WOULD NOT PRESSURIZE. AFTER LANDING TWO HOLES WERE FOUND IN THE RIGHT SIDE OF THE FUSELAGE BELOW THE FLOORBOARDS. MAINTENANCE FOUND THAT THE WHEEL ON THE RIGHT MAIN LANDING GEAR IN THE NUMBER 4 POSITION HAD A PIECE MISSING FROM THE FROM THE INNER WHMar 26, 2000 · N226GL · Beech 1900D · Wheel/Ski/FloatSDR 20000614AP008Indicator · failedCAPTAINS ALTIMETER, ALTITUDE PRESELECT, TRANSPONDER, AND TCAS FAILED ON DEPARTURE. LANDED AND RETURNED TO GATE. THIS IS THE SECOND REPORT OF THIS PROBLEM ON THIS AIRCRAFT IN 2 DAYS. MAINTENANCE PERSONNEL GROUND TESTED THE SYSTEM AND DETERMINED THAT THE ENCOMar 26, 2000 · N249GL · Beech 1900D · Altimeter, Barometric/Encoder
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