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 95ZZZM61Elt · brokenDURING DETAILED INSPECTION, ELT MOUNTING TRAY (PLASTIC) P/N 452-3050 WAS DISCOVERED BROKEN IN NUMEROUS PIECES RENDERING ELT INOPERATIVE. MOUNTING TRAY WAS REPLACED WITH NEW UNIT. (M)SDR 95ZZZM221Elt · wetELT TRANSMITS CONTINUOUSLY. INVESTIGATION REVEALED THAT REMOTE SW WAS SHORTED DUE TO BEING WET. REMOVED AND REPLACED REMOTE SW P/N 118-34002-1 AND ELT BATTERY PACK P/N 452-0130. (M)SDR 95ZZZM140Control Module · failedMDT - PILOT REPORTED, THE LEFT ENVIRONMENTAL FAIL LIGHT ILLUMINATED AND THAT THERE WAS A HINT OF SMOKE IN THE COCKPIT. MAINTENANCE REPLACED FAULTY CONTROL MODULE PCB. OPS CHECKED GOOD.SDR S2YA950006Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 69.00 TO HAVE A CRACK 1.5 INCHES LONG ON THE TOP PORTION NEXT TO THE LOWER MOUNT HOLE OF THE MANUAL HYDRAULIC RESERVOIR BLEED VALVE, PN 114-388012-1. A REPAIR WAS MADE PER THE BEECH SRM.SDR S2YA950005Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 83.00 TO HAVE CRACKED ON THE BOTTOM PORTION BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS. THE CRACKS WERE APPROXIMATELY 3 INCHES AND 1 INCH LONG EXTENDING FROM THE CENTER OF THE RIB REISDR S2YA950003Volt/Freq Meter · knob missingTHE PUSH-TO-READ VOLT BUTTON ON THE A.C. VOLT/FREQUENCY METER EASILY BREAKS OFF OR BECOMES LOOSE AND FALLS OFF. SUBMITTER SUGGESTED THE DESIGN NEEDS TO BE IMPROVED. THREE INSTANCES OF THIS PROBLEM HAS OCCURRED ON DIFFERENT AIRCRAFT ON FLEET. (X)SDR 95ZZZX4165Elt · wetDURING DETAILED INSPECTION, DISCOVERED ELT INOPERATIVE. UNIT WAS CONTAMINATED WITH WATER AND MOUNTING TRAY WAS CRACKED. REMOVED AND REPLACED ELT ASSEMBLY.SDR 95ZZZM142Eva Tube · leakingISN - AFTER NOTING THAT THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED, THE CREW ELECTED AN AIR TURN BACK AND ACCOMPLISHED AND UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED EVA TUBING IN LEFT LEADING EDGE. LEAK CHECKED OK.SDR S2YA950002Ctr Bal Arm · crackedTHE CENTERBALANCE ARM WAS FOUND BENT. HAVE REPLACED 14 OF THE DASH 17 TYPES AND, SO FAR, 2 OF THE DASH 33 NEW DESIGNS BETWEEN 13 AIRCRAFT.SDR 95ZZZM63Elt · brokenELT TRANSMITTING (45 MINUTES). FOUND UNIT WET AND MOUNTING TRAY CRACKED. REMOVED AND REPLACED MOUNTING TRAY, P/N 452-3050.SDR S2YA950001Angle · crackedDURING AN INSPECTION, MAINTENANCE FOUND A 1.50 INCH CRACK ON THE ATTACH ANGLES OF BOTH THE LT AND RT VENTRAL FINS. THE LOCATION IS BELOW THE AFT PRESSURE BULKHEAD, FS 557.50 AND IS CAUSED BY THE LACK OF SHIMMING AT THE SKIN OVERLAP. THE CRACKS WERE REPAIRED.SDR 95ZZZM62Elt · wetELT TRANSMITS CONTINOUSLY. COMPLETE UNIT CONTAMINATED WITH MOISTURE. REMOVED AND REPLACED ELT ASSEMBLY.SDR 95ZZZW694De-Ice Boot · missingRIGHT PROPELLER, ONE DE-ICE BOOT MISSING. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL ON 1/18/95, AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, ITS APPARENT THAT THE PROBELM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOSDR 95ZZZX2510O-Ring · leakingISN - CREW REPORTED FUMES IN THE COCKPIT. MAINTENANCE FOUND AN O-RING UNDER THE RUDDER BOOST TRANSMITTER LEAKING OIL. THE O-RING WAS REPLACED AND LEAK CHECKED GOOD.SDR 95ZZZX2327Deice Boot · missingLEFT PROP, BLADE SN 521MA MISSING DEICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT'S APPARENT THAT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO BLADES PRIOR TO BOOT INSTALLASDR 95ZZZX2326Deice Boot · missingRIGHT PROP, BLADE SN 398MA, HALF OF DEICE BOOT MISSING. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT'S APPARENT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOTSDR 95ZZZX2512Fuel Control · leaksAFTER LANDING, PILOTS NOTED FUEL LEAK FROM ENGINE DRAIN. LEAK ISOLATED TO FCU/FUEL PUMP DRAIN. REMOVED AND REPLACED FCU/FUEL PUMP. AIRCRAFT RETURNED TO SERVICE.SDR 95ZZZX2339Torque Tube · loose rivetsDURING A SCHEDULED INSPECTION, LT ELEVATOR TORQUE TUBE ASSEMBLY FOUND TO HAVE LOOSE RIVETS. THE PART WAS REPLACED.SDR 95ZZZX2480Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER MID-RIB AT WS 83.00 TO HAVE A CRACK 5 INCHES LONG. THE CRACK WAS LOCATED IN THE TOP BEND RADIUS, EXTENDING DOWN AT AN ANGLE FROM THE FORWARD REINFORCEMENT ATTACH POINT. THE FORWARD REINFORCEMENT, PN 114-SDR 95ZZZX2479Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER SECTION MID-RIB AT WS 83.00 TO HAVE A CRACK 1.1250 INCH LONG. THE CRACK WAS ALONG THE TOP BEND RADIUS AT THE RIB CENTER STIFFENER ATTACH POINT. THE FORWARD REINFORCEMENT PN 114-120033-15 WAS ALSO CRACKEDSDR 95ZZZX2502Fuel Line · leakingDEN - UPON LANDING, CREW REPORTED A NOXIOUS ODOR IN THE COCKPIT WHEN THE LEFT BLEED VALVE WAS ON. MAINTENANCE FOUND FUMES CREATED BY A SMALL LEAK IN A FUEL LINE. THE LINE WAS REPLACED.SDR 95ZZZX3041Bearing · spalledTHE METAL OBSERVED IN THE POWER SECTION WAS BEING GENERATED BY THE NR 4 BEARING. THE CAUSE OF THE NR 4 BEARING SPALLING IS UNDER INVESTIGATION BY PRATT AND WHITNEY CANADA.SDR 95ZZZW588De-Ice Boot · missingDE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 361 HOURS AGO AT WHICH TIME BOOT WAS INSTALLED. SUBMITTER STATES UPON INSPECTION OF BOOT AREA ITS APPARENT THAT THE PAINT APPLIED TO THE BLADE PRIOR TO BSDR 95ZZZW587Lugs · wornRIGHT ENGINE RUBBING NOISE COMING FROM POWER SECTION AFTER SHUTDOWN AND THEN DISAPPEARS UPON COMPLETE COOL DOWN OF ENGINE. INVESTIGATION REVEALED THAT ANTI-ROTATION LUGS WERE WORN APPROXIMATELY .060. UNIT WAS NOT MODIFIED BY S/B 14206.SDR 95ZZZX2481Torque Tube · loose rivetsDISCOVERED LOOSE RIVETS ON LEFT ELEVATOR TORQUE TUBE DURING UNSCHEDULED MAINTENANCE ON TAIL. MAINTENANCE REMOVED AND REPLACED THE TORQUE TUBE ASSEMBLY.SDR 95ZZZZ224De-Ice Boot · missingDE-ICE BOOT SEPERATED FROM PROP DURING FLIGHT. PROBLEM APPEARS TO BE WITH ADHESION OF PAINT ON PROP BLADE. BOOT IS GLUED TO PAINTED SURFACE.SDR 95ZZZW529De-Ice Boot · missingLEFT PROP, ONE BLADE MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INVESTIGATION, ITS APPARENT THAT THE PROBLEM LIES WITH THE PAINT THAT IS APPLIED PRIOR TO BOOT INSTALLATION. (W)SDR 95ZZZX2338Display Unit · inopTHE FLIGHT CREW RETURNED TO THE POINT OF DEPARTURE DUE TO RT EFIS INTERMITTENLTY GOES ON AND OFF, LT EHSI WENT BLANK. MAINTENANCE REMOVED AND REPLACED COLLINS NR 1 DISPLAY PROCESSOR UNIT AND BOTH SYSTEMS CHECK GOOD.SDR 95ZZZX2478Flap Motor · inopPILOT REPORTED FLAPS COULD NOT BE SELECTED DOWN AND DURING DESCENT THEY HAD SMELL OF BURNING CARDBOARD OR SIMILAR MATERIAL. MAINTENANCE FOUND THE FLAP RELAY HOT DURING TROUBLESHOOTING. MAINTENANCE PULLED AND TY-WRAPPED BOTH FLAP MOTOR CIRCUIT BREAKERS AND MESDR 95ZZZZ214Fuel Flow Gauge · inoperativeFUEL FLOW INDICATOR ON RT SIDE INOPERATIVE. SUGGEST IMPROVEMENT OF INTERNAL COMPONENTS TO INCREASE RELIABILITY.SDR 95ZZZX2342Wire · chafedEFIS AUXILIARY POWER ANNUNCIATOR FLICKERED, WENT OUT, AND THEN WOULD NOT TEST. MAINTENANCE FOUND RELAY MODULES K103, K104, AND 5-AMP FUSE F033 INOP AND REPLACED THEM. LATER, DURING TROUBLESHOOTING FOR ANOTHER ELECTRICAL PROBLEM, FOUND A CHAFED WIRE J692007-JSDR 95ZZZX1770Deice Boot · missingDE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 198 HOURS AGO AT WHICH TIME THE BOOT WAS INSTALLED. UPON INSPECTION OF BOOT REMOVED, DISCOVERED THE PAINT APPLIED TO THE BLADE WAS STUCK TO GLUE ON THE BSDR 95ZZZX1962Eva Tubing · separatedISN - AFTER TAKEOFF, CREW ELECTED AN AIR TURN BACK WHEN THE LT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPAIRED THE SEPARATED EVA TUBING. FUNCTION CHECK OKAY.SDR 95ZZZX1725De-Ice Boot · missingDE-ICE BOOTS NOT MAINTAINING BOND TO PROPELLER BLADES. TWO DE-ICE BOOTS DISCOVERED MISSING FROM SAME PROPELLER ON TWO DIFFERENT OCCASIONS. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INVESTIGATION, IT IS APPSDR 95ZZZX1507Bearing · failedON ARRIVAL ALB, PIC NOTICED RIGHT INBOARD TIRE AND WHEEL, PN 40273A, ASSEMBLY MISSING. SUBJECT WHEEL ASSEMBLY WAS LATER FOUND AT ROC, THE LAST AIRPORT OF DEPARTURE. IT APPEARS OUTBOARD AND INBOARD BEARINGS FAILED. RETAINING NUT AND COTTER PIN WERE FOUND STISDR 95ZZZX1917De-Ice Boot · separatedTWO EACH PROP DE-ICE BOOTS ON RT PROP AND 1 EACH DE-ICE BOOT ON LEFT PROP. DE-ICE BOLTS SEPARATING FROM LEADING EDGE EROSION SHIELD DUE TO PAINT BENEATH SEPARATING FROM NICKEL TORSION SHIELD. SUGGEST IMPROVING INSTALLATION PROCEDURE FOR PAINT ON PROPS OR LEASDR 95ZZZW464De-Ice Boot · separatedTWO PROP DE-ICE BOOTS SEPARATING FROM LEADING EDGE EROSION SHIELD. PAINT ON SHIELD SEPARATED FROM SHIELD. SUBMITTER SUGGEST IMPROVING PAINTING PROCEDURES ON PROP BLADES OR LEAVING PAINT OFF OR EROSION SHIELD.SDR 95ZZZX2013Downlock Switch · frozenISN - AFTER TAKEOFF, CREW ELECTED AN AIR TURN BACK WHEN THE DOWNLOCK SWITCH WOULD NOT ACTIVATE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE THAWED OUT THE DOWNLOCK SWITCH AND ACCOMPLISHED A SATISFACTORY GEAR SWING.SDR 95ZZZX3040Shaft · galledTHE POWER SECTION WAS REPORTED AS HARD TO ROTATE. UPON DISASSEMBLY, FOUND PROP SHAFT AND SLEEVE WAS GALLED IN SUCH A WAY THAT IT COULD NOT ROTATE FREELY. IT HAS BEEN DETERMINED THE GALLING OCCURRED DUE TO FUEL OIL HEATER CONTAMINATING THE OIL SYSTEM WITH FUESDR 95ZZZX2483Torque Tube · loose rivetsDURING SCHEDULED INSPECTION, MAINTENANCE DISCOVERED THE RIGHT ELEVATOR TORQUE TUBE RIVETS LOOSE AND FRETTING. REPLACED THE TORQUE TUBE ASSEMBLY.SDR 95ZZZM285Motor · failedDEPARTED MONTROSE, PASSENGER COMPLAINED OF SMOKE IN CABIN. PILOT CALLED AN INFLIGHT EMERGENCY. RETURNED TO GATE WITHOUT INCIDENT. MECHANIC FOUND FLAP MOTOR AND WIRES BURNED. MEL'D FLAPS. PERFORMED GROUND RUN USING ALL ENVIRONMENTAL CHECKS TO ENSURE THERE SDR 95ZZZZ156Propeller Hub · leaking oilAIRCRAFT WAS EN ROUTE FROM BUF TO ALBANY NY, PILOT OBSERVED OIL PRESSURE DROPPING ON RIGHT ENGINE. THE AIRCRAFT DIVERTED TO SYR NY AND LANDED UNEVENTFUL. INVESTIGATION OF LOW OIL PRESSURE REVEALED OIL LEAKING FROM PROP. PROP REMOVED AND REPLACED AND UNIT RESDR 95ZZZX1957Circuit Board · failedISN - THE CREW ELECTED AN AIR TURN-BACK AFTER THE LEFT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE PC BOARD. RAN AIRCRAFT AND OPS CHECKED GOOD.SDR 95ZZZX3039Bearing · spalledBEARINGS NR 5, NR 6, AND NR 7 HAVE INDICATION OF ARCING AND SPALLING. POWER SECTION WAS REPORTED HAVING SUSTAINED A LIGHTNING STRIKE.SDR 95ZZZX2341Transfer Tube · chafedFOUND FUEL LEAKING FROM LT WHEELWELL, MAINTENANCE OPENED UP THE INNER FENDER ASSEMBLY AND FOUND MAIN GEAR UPLOCK SWITCH, WIRE BUNDLE HAD CHAFED THROUGH THE FUEL TRANSFER TUBE ASSEMBLY JUST INBOARD OF THE FUEL CROSS-TRANSFER VALVE. THE LINE WAS REMOVED ADN REPSDR 95ZZZX2482Torque Tube · loose rivetsRIGHT ELEVATOR TORQUE TUBE ASSEMBLY FOUND TO HAVE LOOSE RIVETS AT THE ELEVATOR ATTACH BRACKET. THE PROBLEM WAS FOUND AT A DETAIL NR 6 AND THE RIVETS WERE REMOVED AND REPLACED.SDR 95ZZZX1913Fire Loop · brokenMTH - AIRCRAFT DEPARTED. ON CLIMB AT APPROXIMATELY 9,000 FEET, YELLOW LOOP ANN FLICKERED AND RED FIRE T-HANDLE ILLUMINATED. PILOT MADE PRECAUTIONARY RT ENGINE SHUT-DOWN AND RETURNED TO MTH. INSPECTION REVEALED RT ENG AFT FIRE LOOP BROKEN, VIBRATION CAUSED.SDR 95ZZZX1811Bearing · spalledTHE NR 6 BEARING WAS FOUND WITH SPALLING ON ONE INNER RACE HALF AND SEVERAL OF THE BEARING BALLS. SUBMITTER BELIEVES THE SPALLING TO BE INTRODUCED BY THE STATIC PROBLEMS THAT ARE KNOWN TO BE ASSOCIATED WITH THE PROPELLER SYSTEM.SDR 95ZZZX732Limit Switch · out of adjustISN - AFTER DEPARTURE, CREW ELECTED AN AIR TURN-BACK WHEN THE GEAR HORN WOULD NOT SILENCE WITH GEAR IN UP POSITION. MAINTENANCE ADJUSTED THE FLAP LIMIT SWITCH. THE OPS CHECK WAS GOOD.SDR 95ZZZX664Trim Cable · separatedSUPPLEMENTAL SDR - 1-20-95. ISN - ON APPROACH, ELEVATOR TRIM CABLE SNAPPED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE IS INVESTIGATING THE FAULT. IN RE ELEVATOR TRIM TAB CABLE BREAK. MAINTENANCE INSPECTED ENTIRE CABLE RUN AND FOUND THE BROKEN CA
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