Raytheon 1900D
Service difficulty reports · 7,152
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR S2YA01001Altimeter · inoperativeFLT 2044 - MKE-CWA - DURING FLIGHT, THE CAPTAINS ALTIMETER FLAG APPEARED IN FLIGHT. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER, OPS CHECKED IT AND RETURNED THE AIRCRAFT TO SERVICE. (M)SDR C2XA0CL004Engine · failedLEX - FLT 3108 - THE CREW REPORTED NR 1 ENGINE LOST OIL PRESSURE IN FLIGHT AND THE ENGINE SHUT DOWN. THE AIRCRAFT DIVERTED AND LANDED IN CVG WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. (M)SDR CA010215010Bearing · failed(CAN) DURING CRUISE LT GENERATOR WARNING ANNUNCIATOR ILLUMINATED. CREW ATTEMPTED TO RESET BUT NO SUCCESS. INSPECTION OF THE STARTER GENERATOR REVEALED THE DRIVESHAFT END BEARING FAILED CAUSING EXCESSIVE ENDPLAY. GENERATOR OVERHAUL INTERVAL IS 1500 HOURS.SDR GLBA2001007Governor · malfunctionedABORTED T/O - RIGHT PROP RPM WENT TO 1900 ON T/O ROLL. INSPECTED INDICATING, SYSTEM COULD NOT DUPLICATE FAULT. SYSTEM OPS CHECKED GOOD. RETURNED TO SERVICE.SDR GLBA2001006Warning Light · illuminatedRETURN TO BLOCK - RIGHT BLEED AIR ANNUCIATOR ILLUMINATED ON CLIMBOUT. REPAIRED EVA TUBING.SDR 20010208CW010Fuel Cap · brokenUPON REMOVAL OF RT OUTBOARD FWD CAP, CAP FELL APART. PIN IN LOCKING TAP THAT SECURES CAP BODY TOGETHER IS LOOSE IN TAP AND FELL OUT, ALLOWING CAP TO FALL APART. REDESIGN OR MATERIAL CHANGE REQUIRED.SDR GLBA2001004Warning Light · illuminatedRETURN TO BLOCK - LEFT ENGINE BLEEDAIR FAIL INDICATION, RESEATED PCB OPS CHECKED SYSTEM GOOD RETURNED TO SERVICESDR GLBA2001003Generator · inoperativeRETURN TO BLOCK - RIGHT GEN FELL OFF LINE WOULD NOT RESET, R/R STARTER-GEN SYSTEM OPS CHECKED GOODSDR 20010515SG005Torque Tube · looseDURING SCHEDULED INSPECTION, DISCOVERED LOOSE RIVETS ON RT ELEVATOR TORQUE TUBE, RESULTING IN EXCESSIVE FREE PLAY OF ELEVATOR. INSPECTED CONTROL SYTEM FOR OTHER DEFECTS, NONE NOTED. REPLACED TORQUE TUBE WITH NEW UNIT. (M)SDR 20010208CW011Torque Tube · looseDURING SCHEDULED INSPECTION, RIGHT ELEVATOR WAS FOUND WITH EXCESSIVE, FREE PLAY,. LOOSENESS WAS THE RESULT OF LOOSE RIVETS ON TORQUE TUBE.SDR 20010208CW009Landing Gear · malfunctionedCLE FLIGHT 3231 THE CREW REPORTED THE LANDING GEAR FAILED TO EXTEND WHEN THE HANDLE WAS PLACED IN THE DOWN POSITION. THE GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE LANDING GEAR, HYDRAULIC ACCUMULATOSDR GLBA2001002Bulb · burned outEMERGENCY LIGHT INOP - R/R LIGHT BULB OPS CHECKED GOODSDR GLBA2001001Element · failedRETURN TO BLOCK - DUAL ENVIROMENTAL FAILURE, REPLACED TEMP SENSOR AND PRECOOLER BYPASS VALVE SYSTEM OPS CHECKED GOOD RETURNED TO SERVICESDR GLBA9191Altimeter · inoperativeRETURN TO BLOCK - #1 ALTIMETER FLAGGED ON CLIMB OUT, R/R ALTIMETER OPS CHECKED SYSTEM GOODSDR CA010103004Bearing · failed(CAN) IN FLIGHT PILOT NOTICED AN IMPORTANT VOLTAGE DIFFERENCE BETWEEN THE TWO GEN, SUDDENLY THE LT DC GENERATOR WENT OFF LINE. THE PILOT TRY TO RESET WITH NO SUCCESS. AFTER LANDING, MAINTENANCE CREW TRY TO START THE ENGINE WITH NO SUCCESS. THEY FOUND THE LT DCSDR CA010103007Bolt · broken(CAN) DURING THE REMOVAL OF RUDDER BELLCRANK ON CAPTAIN SIDE THE TOP INBOARD BOLT WAS FOUND BROKEN ON RUDDER PEDAL BELLCRANK SUPPORT. BOLT WAS STILL IN PLACE.REF RAYTHEON IPC 27-20-10 P8 ITEM 70, 71.SDR 20010112SG046Switch · shortedPROP SYNC SWITCH SHORTED CAUSING ELECTRICAL SMOKE IN COCKPIT. PULLED PROP SYNC CIRCUIT BREAKER AND SMOKE CLEARED. PROP SYNC SYSTEM DEACTIVATED AND DEFERRED PER MEL 61-1 PENDING RECEIPT OF SWITCH. REPLACED SWITCH AND TESTED SYSTEM. NO DISCREPANCIES NOTED. SDR S2YA00038Warning System · activatedFLT 1044 - MKE-GRB - DURING CLIMB-OUT, THE FO EFIS DISPLAY FAILED. THE CREW MADE AN AIR-TURN BACK AND AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED THE NR 2 DPU, OPS CHECKED IT AND RETURNED THE AIRCRAFT TO SERVICE. (M)SDR S2YA00037Switch · out of adjFLT 1221 - CVG-MKE - DURING CLIMB-OUT, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING IN CVG. THE CREW CONTACTED MX AND PUT THE ANNUNCIATOR ON MEL. MAINTENANCE READJUSTED THE BOTTOM ROLLER SWITCH ON THE CARGSDR 20010125SG005Connector · looseFLT 9401 - EYW/TPA - EN ROUTE TO TAMPA, LEFT ENGINE ITT ROSE TO 900 DEGREES. ITT DID NOT RESPOND WITH THROTTLE MOVEMENT. ALL OTHER INDICATIONS WERE NORMAL. ENGINE WAS SHUTDOWN AND SECURED. SECURED LEFT ENGINE ITT GAUGE CANNON PLUG. OPERATIONAL CHECK NORMASDR AU001190Socket · cracked(AUS) LT AND RT MAIN LANDING GEAR STRUT SOCKET ASSEMBLIES CRACKED INTHE AREA OF ATTACHMENT LUGS.SDR AU001189Socket · cracked(AUS) LT MAIN LANDING GEAR STRUT SOCKET ASSEMBLY CRACKED IN THE AREA OF ATTACHMENT LUGS. CRACK LENGTHS INBOARD 13.2MM (0.52IN) ANDOUTBOARD 12.7MM (0.5IN).SDR S2YA00034Windshield · crackedFLT 1021 - MKE-ATW - DURING CLIMB-OUT, THE WINDSHIELD STARTED TO CRACK. THE CREW LEVELED OUT THE A/C AND THE WINDSHIELD CONTINUED TO CRACK SO THEY MADE AN AIRTURN BACK AND AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED THE WINDSHIELD, OPS THE HEAT AND RESDR C2XA00CL101Indicator · failedCLE - FLT 3154 - THE CREW REPORTED THAT AFTER TAKEOFF THE NR 2 ENGINE TORQUE GAUGE DROPPED TO ZERO. ALSO REPORTED THAT ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 TSDR AU001205Strut · cracked(AUS) LT MAIN LANDING GEAR STRUCK BY A KANGAROO. INSPECTION FOUND THE LT MAIN LANDING GEAR AXLE AND TORQUE KNEE SOCKET CRACKED AT THE LOWER END OF THE TORQUE KNEE ATTACHMENT LUGS. CRACK LENGTH11.43MM (0.45IN).SDR 20010112SG025Windshield · bird strikeBIRD STRIKE ON BOTH LEFT AND RIGHT WINDSHIELDS. BOTH WINDSHIELDS BROKEN. REPLACED LEFT AND RIGHT WINDSHIELDS, P/N 1145043 & 101384025. (M)SDR 20010112SG024Control Handle · intermittentLANDING GEAR HANDLE HAD TO BE MOVED TO THE EXTEND POSITION SEVERAL TIMES BEFORE THE LANDING GEAR WOULD EXTEND. REPLACED THE LANDING GEAR SELECT HANDLE. RETRACTION/EXTENSION CHECKED GOOD. (M)SDR 20010112SG023Switch · shortedTHE PROPELLER SYNCHORNIZATION SWITCH SHORTED, RESULTING IN SMOKE IN THE COCKPIT. REPLACED THE PROPELLER SYNCHORNIZATION SWITCH. OPS CHECKED GOOD. (M)SDR C2XAOOCL100Packing · failedCREW REPORTED THE CAPTAINS LEFT BRAKE GOES ALL THE WAY TO THE FLOOR WITHOUT STOPPING ACTION. A/C TAXIED TO THE GATE WITHOUT FURTHER INCIDENT.MX INSPECTED AND FOUND THE LEFT INBOARD BRAKE SWIVEL TO BE LEAKING. THE BRAKE SWIVEL WAS REBUILT WITH NEW PACKINGS AND SDR C2XA00CL098Circuit Board · failedCLE-CREW REPORTED LANDING GEAR HANDLE FAILED TO MOVE TO UP POSITION AFTER TAKEOFF. CREW HAD TO USE THE DOWNLOCK RELEASE BUTTON ON LANDING GEAR CONTROL. A/C LANDED WITHOUT FURTHER INCIDENT.MX REMOVED/REPLACED THE A316 P.C. BOARD AND OPERATIONAL CHECKED IAW BEECSDR CA010104005Relay · failed(CAN) DURING AIRCRAFT TAXI CREW SELECTED FLAPS TO 17 DEGREES FOR TAKEOFF. FLAPS DID NOT OPERATE. FLAPS RE-SELECTED AND FLAPS MOVED TO SELECTED POSITION. CREW SELECTED FLAPS TO 0 DEGREE POSITION AND OPERATED ON THE M.E.L.MAINTENANCE WAS ABLE TO DUPLICATE FAULT SDR 20010112SG067Actuator · malfunctionedFLT 9330 - TPA-JAX - DURING APPROACH, WITH LANDING GEAR DOWN, LEFT SIDE GREEN ANNUNCIATOR WILL NOT ILLUMINATE. NO UNSAFE LIGHT OR HORN. REMOVED AND REPLACED LEFT LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. (M)SDR 20010112SG047Filter · failedSMOKE IN THE COCKPIT AND CABIN ON CLIMB, AIR RETURN. INSPECTED AND FOUND THAT THE FILTER ASSEMBLY ON THE VENT BLOWER ASSEMBLY HAD OVERHEATED AND FAILED. REMOVED AND REPLACED VENT BLOWER ASSEMBLY. (M)SDR C2XA00CL096Master Cylinder · failedAFTER LANDING THE CREW REPORTED THE CAPTAINS LEFT BRAKE PEDAL HAD NO RESISTANCE. A/C TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED THE CAPTAINS LEFT BRAKE MASTER CYLINDER IAW BEECHCRAFT MM 32-40-06. A/C WAS RELEASED FOR SERVICE.SDR CA001123004Bracket · broken(CAN) DURING GEAR RETRACTION IN CLIMB PILOT HEARD THUMP AT NOSE & TRANSIT LIGHT DID NOT EXTINCT GEAR CYCLED WITH SAME RESULT. GEAR LOWERED & SCREEN LIGHTS ON. PILOT COMMUNICATED WITH CNTL CENTRE & FLYBY TOWER REVEALED NOSE WHEEL TO BE OUT OF NORMAL STRAIGHT FSDR CA001122004Squat Switch · intermittent(CAN) FLIGHT 1790 DEPARTED CALGARY EN ROUTE TO KAMLOOPS, AIRCRAFT WOULD NOT PRESSURIZE AND RETURNED TO CALGARY. MAINTENANCE COULD NOT DUPLICATE DEFECT IN HANGAR AND AIRCRAFT WAS TEST FLOWN. PROBLEM REOCCURRED AND RETURNED TO HANGAR WHERE CONTINUITY TEST REVEALSDR C2XAOOCL091Bracket · brokenCREW REPORTED AFTER TAKEOFF FROM CLEVELAND THEY RECEIVED WARNING LIGHT FOR PASSENGER DOOR. A/C RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED/REPLACED PASSENGER DOOR MICROSWITCH BRACKET WHICH WAS FOUND TO BE BROKEN. PERFORMED OPERATIONSDR 20010112SG066Blower · shortedFLT 9449 - TPA-MIA - DURING FLIGHT, ELECTRICAL SMOKE SMELL IN REAR CABIN. REMOVED AND REPLACED AFT VENT BLOWER. OPERATIONAL CHECK NORMAL. (M)SDR 20010112SG065Connecting Rod · out of adjFLT 9137 - FLL - DURING FLIGHT, LEFT ENGINE SURGES THREE TIMES AT DIFFERENT POWER SETTINGS. ENGINE SHUTDOWN AND SECURED. ADJUSTED GOVERNOR INTERCONNECT ROD. OPERATIONAL CHECK NORMAL. (M)SDR 20010111SG034Controller · failedLANDING GEAR WOULD NOT COME DOWN WHEN SELECTED. THE LANDING GEAR WAS MANUALLY EXTENDED. REPLACED LANDING GEAR CONTROL AND TIME DELAY PC BOARD. LANDING GEAR RETRACTION TEST WAS GOOD. (M)SDR S2YA00033Indicator · malfunctionedFLT 1782 - MKE-MLI - AFTER TAKEOFF, THE RT N1 GAUGE BEGAN INDICATING IMPROPERLY. THE CREW MADE AN AIR TURN BACK TO MKE AND LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED AND OPS CHECK THE N1 GAUGE AND RETURNED THE AIRCRAFT TO SERVICE. (M)SDR 20010112SG016Gyro · inoperativePILOTS EHSI RED FLAGGED DURING THE TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 1 DIRECTIONAL GYRO AND THE SYSTEM TESTED GOOD. (M)SDR GLBA9137Altimeter · failedCAPTAINS ALTIMETER FAILED AFTER TAKEOFF. REMOVED AND REPLACED CAPTAINS ALTIMETER. SYSTEMS TESTS GOOD. (M)SDR AU001009Socket · cracked(AUS) RT MAIN LANDING GEAR TORQUE LINK ATTACHMENT LUG LOCATED ON THE SOCKET ASSEMBLY CRACKED. FOUND DURING UNSCHEDULED DOUBLE BRAKE UNIT CHANGE. AIRCRAFT HAD SUFFERED A WALLABY STRIKE ON LANDING ON THE PREVIOUS DAY.SDR 20010111SG031Hydraulic Line · rupturedLANDING GEAR RELAY CIRCUIT BREAKER POPPED AND THE HYDRAULIC LOW ANNUNCIATOR ILLUMINATED WHEN THE LANDING GEAR EXTENSION WAS SELECTED DOWN. THE LANDING GEAR HAD TO BE MANUALLY EXTENDED. FOUND THE AFT LEFT MLG ACTUATOR LINE RUPTURED. REPLACED THE LINE AND SERVSDR C2XA00CL083Motor · odorCLE - FLT 3231 - DURING TAXI, THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP MOTOR IAW BEECHCRAFT 1900D MM 27-50-03. OPERATIONAL CHECKS WERE GOOD IAW 27-5SDR 20010111SG008Switch · shortedPROP SYNC SWITCH SHORTED CAUSING ELECTRICAL SMOKE IN THE COCKPIT. PULLED PROP SYNC CIRCUIT BREAKER AND SMOKE CLEARED. PROP SYNC SYSTEM DEACTIVATED AND DEFERRED PER MEL 61-1 PENDING RECEIPT OF SWITCH. (M)SDR C2XA00CL080Fire Loop · damagedCLE - FLT 3320 - THE CREW REPORTED THEY HAD A NR 1 ENGINE FIRE WARNING IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE AFT FIRE LOOP IAW BEECHCRAFT 1900D MM 26-10-00. THE AIRCRAFT WASDR S2YA00032Actuator · failedIN APPROACH TO ESC THE CREW SELECTED GEAR DOWN BUT FAILED TO GET NOSE DOWN AND LOCKED INDICATION. THE CREW MADE SEVERAL ATTEMPTS TO EXTEND GEAR INCL. DOING FLY-BY & TALKING TO MX. AFTER NOT BEING ABLE TO ACHIEVE NOSE DOWN & LOCKED CRE DIVERTED TO GRB FOR BETTESDR C2XA00CL078Switch · failedCLE - FLT 3001 - THE CREW REPORTED THE NR 1 ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PULL HANDLE SWITCH ASSEMBLY IAW BEECHCRAFT MM 26-20-
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