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 96ZZZX116Gas Shock · bentWHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK.SDR 95ZZZX6120Truss · chafedSPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE RT ENGINE TRUSS TOP INBOARD TUBE IN AREA 'A' CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1.SDR 95ZZZX5242Duct · brokenA THIRTY DEGREE SPLIT IN ITT WAS REPORTED WITH LEFT ENGINE RUNNING HIGHER THAN RIGHT. A POWER ASSURANCE RUN VERIFIED A PROBLEM WITH THE LEFT BLEED AIR CONTROL SYSTEM. FUNCTIONAL CHECKS OF THE LEFT BLEED SYSTEM WERE UNRELIABLE AND DID NOT AGREE WITH TROUBLESHSDR 95ZZZM511Ehsi · inopFAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M)SDR 95ZZZM510Vert Gyro · inopFAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M)SDR 95ZZZM494Wheel · brokenDURING TAXI ONTO RUNWAY A STEERING PROBLEM WAS NOTED. INSPECTION OF NOSE GEAR BY MAINTENANCE, REVEALED THAT THE INNER HALF OF NOSE WHEEL WAS BROKEN AROUND THE COMPLETE RADIUS OF WHEEL. NOSE WHEEL AND TIRE REPLACED. (M)SDR MASA9516Switch · out of adjustDURING APPROACH INTO DUBOIS, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED NOSE DRAG BRACE DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X)SDR 95ZZZM516Windshield · bird strikeSPW - DURING CLIMB-OUT AFTER DEPARTURE, THE CREW ENCOUNTERED A BIRD STRIKE. THE CREW ELECTED A PRECAUTIONARY AIR TURN BACK. AFTER AN UNEVENTFUL LANDING, MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION. NO FINDINGS WERE FOUND. (M)SDR 95ZZZX5161Blade · crackedRIGHT PROPELLER BLADE, SN 518MA, DE-ICE BOOT PARTIALLY MISSING AND LEADING EDGE CRACKED IN AREA OF BOOT OPERATION. REMOVED AND REPLACED PROPELLER WITH ZERO TIME OVERHAULED UNIT. (CRACK NOTED WAS IN LEADING EDGE ABRASION STRIP. THIS IS SECOND FAILURE OF THISSDR S2YA950020Rib · crackedDURING AN SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT WING CENTER MID RIB AT WS 83.00 TO HAVE A CRACK AT THE TOP APPROXIMATELY FIVE INCHES ACROSS. THE CRACK WAS LOCATED BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS AND A REPAIR WAS MADE. THE RIB REINFORSDR S2YA950019Generator · off lineAFTER THE FLIGHT CREW LEFT MKE ON FLT NR 1124, THEY FOUND THAT THE RT DC GENERATOR WAS OFF LINE. THEY PROCEEDED TO TURN BACK TO MKE. MAINTENANCE PARALLELED THE GENERATOR CIRCUIT PER BEECH MM AND OPS CHECK GOOD. (M)SDR S2YA950018Fire Loop · shortedTHE FLIGHT CREW HAD A RIGHT ENGINE FIRE INDICATION IN FLIGHT AFTER DEPARTING MKE ON FLIGHT NR 1026. THEY PROCEEDED TO SHUT DOWN THE RIGHT ENGINE IN FLIGHT AND DISCHARGED THE RT ENGINE FIRE BOTTLE. THEY DECLARED AN EMERGENCY, MADE A TURNBACK IN FLIGHT AND LANSDR S2YA950017Radar Contl Pnl · inopAFTER THE FLIGHT CREW DEPARTED ON FLIGHT NR 1822, THE WEATHER RADAR BECAME INOPERATIVE IN ALL MODES. THEY RETURNED TO MKE AND MAINTENANCE REPLACED THE RADAR CONTROL PANEL AND CLEARED THE DISCREPANCY. (M)SDR S2YA950016Boost System · malfunctionedDURING TAKEOFF ROLL OF FLIGHT NR 1120 THE CREW FELT LEFT RUDDER DEFLECTION AND VERIFIED THE RUDDER BOOST SYSTEM WAS MALFUNCTIONING. THEY ABORTED TAKEOFF, RETURNED TO MKE AND MAINTENANCE DEFERRED THE SYSTEM. SUBMITTER STATES, CONTACTED OPERATOR THIS WAS NOT ASDR 95ZZZX4047Air Sense Line · failedLAX/SMX - AIRCRAFT DEPARTED. APPROXIMATELY 10 MINUTES INTO FLIGHT AT 10,000 FEET, RT ENGINE STARTED TO SURGE IN POWER AND TORQUE DROPPED TO ZERO WITHIN 10 SECONDS. ALL OTHER PARAMETERS NORMAL. FLIGHT CREW SECURED RIGHT ENGINE AND DIVERTED TO BFL WITHOUT FURSDR 95ZZZX4045Deice Boot · missingRIGHT PROPELLER MISSING DEICE BOOT BLADE, S/N UNKNOWN. FURTHER INSPECTION FOUND 3 SEPARATE CRACKS IN LEADING EDGE OF 2 BLADES, S/N UNKNOWN. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL.SDR 95ZZZX4163Deice Boot · missingLEFT PROPELLER, BLADE, SERIAL NUMBER UNKNOWN, MISSING DEICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, SUBMITTER STATED THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES SDR 95ZZZM236Light Bulb · failedNOSE LANDING GEAR ANNUNCIATOR MODULE BULBS FAILED TO ILLUMINATE ON EXTENSION. INSPECTION OF MODULE FOUND P/N 951-F04 BULBS FAILED. (M)SDR 95ZZZM235De-Ice Boot · missingLEFT PROP, BLADE S/N 373MA, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT WAS APPARENT, SUBMITTER STATES, THAT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BSDR 95ZZZM234De-Ice Boot · missingRIGHT PROP, BLADE S/N 317MA, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, SUBMITTER STATES THE PROBLEM LIES WITH THE PAINT BEING APPLIED. THE BLADES PRIOR TO BOOT INSSDR 95ZZZM233De-Ice Boot · missingLEFT PROP, BLADE S/N UNKNOWN, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE. SUBMITTER STATES THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT SDR 95ZZZM480Display Unit · inoperativeFAR - THE CREW ELECTED AN AIR TURNBACK AFTER A RIGHT SIDE DISPLAY UNIT AND EFIS FAILURE. FOLLOWING AN UNEVENTFUL LANDING, MAINTENANCE RERACKED THE DISPLAY UNIT AND A GROUND CHECK WAS SATISFACTORY. (M)SDR 95ZZZM241De-Ice · missingDE-ICE BOOT NOT MAINTAINING BOND TO PROPELLER BLADE. ONE BOOT SEPARATED IN FLIGHT FROM BLADE S/N 409MA. BOOT WAS INSTALLED AT OVERHAUL BY HARTZELL ON 11/18/94 NEW BOOT WAS INSTALLED IAW CHAPTER 30 OF BEECH MANUAL. (M)SDR 96ZZZM1300Bearings · wornDURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M)SDR 95ZZZX4425Actuator · failedHYDRAULIC MAIN GEAR ACTUATOR ON RIGHT MAIN GEAR LEAKING FLUID FROM THREADED PISTON HOUSING NEAR FORWARD BOSS. REMOVED AND REPLACED MAIN GEAR ACTUATOR WITH NEW SERVICEABLE ACTUATOR PER BEECH MM, OPERATIONAL AND LEAK CHECK GOOD.SDR 95ZZZX4424Exhaust Stack · crackedLEFT ENGINE OUTBOARD EXHAUST STACK CRACKED ABOUT 1.50 INCHES LONG AT BLAST TUBE EXHAUST PORT. CRACK AT WELD BEAD PROGRESSING CIRCUMFERENTIALLY AROUND TUBE. REMOVED AND REPLACED EXHAUST STACK.SDR 95ZZZM540Exhaust Stack · crackedLEFT ENGINE INBOARD EXHAUST STACK CRACKED AT BLAST TUBE ATTACH WELD JOINT, PROGRESSING CIRCUMFERENTIALLY AROUND ATTACH WELD.SDR S2YA950015Volt/Ammeter · stickingMKE - FLT 1091.1 - AFTER FLIGHT CREW TOOK OFF, THEY NOTICED THE D.C. AMMETER STAYED AT ABOUT 60 AMPS. THEY DECIDED TO TURN BACK TO MKE TO HAVE MAINTENANCE CHECK IT. MAINTENANCE DETERMINED IT WAS A STICKING GAUGE MOVEMENT. VOLT/AMMETER WAS REPLACED. (X)SDR S2YA950014Fuel Sensor · failedAFTER TAKEOFF, RIGHT COLLECTOR TANK 'LOW' ANNUNCIATOR ILLUMINATED. THE CREW DECIDED TO RETURN TO MKE AND MEL'D THE SYSTEM. THE FLIGHT NUMBER WAS 1834.2. MAINTENANCE LATER TROUBLESHOT THE SYSTEM AND REMOVED AND REPLACED THE FUEL LEVEL SENSOR. (X)SDR 95ZZZX4166Elt · wetELT TRANSMITS CONTINUOUSLY. REMOVED AND REPLACED ELT ASSEMBLY. UNIT REMOVED WAS CONTAMINATED WITH WATER.SDR 95ZZZX3962O-Ring · cutISN - AFTER TAKEOFF, CREW OBSERVED AN OIL PRESSURE FLUCTUATION ON THE RIGHT ENGINE. THE ENGINE WAS SHUT DOWN FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN OIL LEAK CAUSED BY A CUT O-RING. SERVICED ENGINE WITH 4 QUARTS OIL AND LEAK CHECKED OK.SDR S2YA950013Deice Supp Line · chafedFOUND THE TAIL DEICE SUPPLY LINE CHAFED AT THE POINT OF EXIT FROM THE CLEAR PLASTIC ROUTING 'PROTECTION' TUBE. THE LOCATION IS THE BASE OF THE VERTICAL STABILIZER, LOWER ZONE 331. THE LINE WAS REPAIRED AND REST OF THE FLEET IS BEING CHECKED. (X)SDR 95ZZZX4168Rivets · looseRIVETS LOCATED IN RT WING OUTBOARD OF NACELLE TOP SPAR AREA LOOSE CAUSING FUEL LEAK. VERY COMMON OCCURRENCE WITH APPROXIMATELY A 6-10 RIVET LENGTH ALONG TOP WING SPAR.SDR 95ZZZX3416Torque Shaft Arm · looseRUDDER TORQUE SHAFT ARM, MOUNTING RIVETS (8) LOOSE.SDR 95ZZZM205De-Ice Boot · missingON RIGHT PROP, THREE INCHES MISSING FROM DE-ICE BOOT ON ONE BLADE. A SECTION OF LEADING EDGE METAL ABRASION STRIP WAS ALSO FOUND DETACHED FROM THE COMPOSITE BLADE. PROP WAS REMOVED AND REPLACED WITH AN AIRWORTHY UNIT. APPARENT CAUSE IMPROPER BONDING. (M)SDR 95ZZZX4164Elt · wetELT TRANSMITS CONSTANTLY, UNABLE TO SILENCE. REMOVED AND REPLACED ELT ASSEMBLY. UNIT REMOVED WET.SDR S2YA950012Switch · failedTHE PROP SYNCROPHASER BECAME INOP DUE TO AN ON/ON SWITCH BEING USED INSTEAD OF AN ON/OFF SWITCH. BEECH IS USING A THREE-POLE SWITCH AND THE ONE BARE UNPROTECTED TERMINAL HAS POWER SWITCHED TO IT WHEN YOU THINK IT IS SELECTED TO THE OFF POSITION. THIS HAS OCCSDR 95ZZZX4056Elt Tray · brokenDURING SCHEDULED MAINTENANCE AND ELT BATTERY TIME CHANGE, ELT MOUNTING TRAY WAS DISCOVERED BROKEN. REMOVED AND REPLACED MOUNTING TRAY AND BATTERY PACK.SDR 95ZZZM204Propeller · leakingDURING PREFLIGHT INSPECTION, CAPTAIN NOTICED EXCESSIVE AMOUNT OF OIL ON RIGHT ENGINE COWL. MAINTENANCE CONTROL NOTIFIED AND MAINTENANCE DISPATCHED TO AIRCRAFT TO INVESTIGATE. UPON INVESTIGATION DETERMINED OIL COMING FROM PROP BLADE AREA FORWARD OF SPINNER BUSDR S2YA950004Comp Bleed Valve · malfunctionedTHE CREW EXPERIENCED A VIBRATION ON TAKEOFF AND DURING CLIMB-OUT FOLLOWED BY A LOUD POP AND A YAW TO THE LEFT AS THEY WERE CLIMBING THROUGH 7,000 FEET ASL, THE LT PROP RPM WAS NOTICED TO DEVIATE AT THAT TIME. THE CREW RETURNED TO MKE WITHOUT INCIDENT. MAINTESDR 95ZZZX4009Bearing · damagedBEARING RECEIVED FROM HARTZELL IMPROPERLY PACKAGED. THE PACKAGING ALLOWED THE BEARING ASSY TO SEPARATE AND ALLOWED THE ROLLER PARTS TO IMPACT, THE BEARING RACE CAUSING THE ROLLERS TO BECOME DAMAGED. FIVE EACH BEARING BOXES RETURNED TO HARTZELL FOR CREDIT.SDR 95ZZZX4167Skin · delaminatedDURING AIRCRAFT REPOSITIONING FLIGHT FROM BRADFORD, PA TO JAMESTOWN, NY, PILOT FELT VIBRATION IN AIRFRAME. AIRCRAFT LANDED WITHOUT INCIDENT. DURING POST-FLIGHT INSPECTION, FOUND LT INBOARD WING PANEL (TOP) HAD STARTED TO DELAMINATE. REMOVED AND REPLACED PANSDR 95ZZZX4058Elt Mount · brokenDURING DETAILED PHASE NR 6 INSPECTION, FOUND ELT MOUNT AND FACE PLATE BROKEN. REPLACED ELT WITH NEW UNIT.SDR S2YA950011Hyd Fill Line · leakingFOUND HYRAULIC HAND PUMP SUCTION LINE CHAFING AGAINST THE LT SIDE OF THE AIR CYCLE MACHINE EXHAUST DUCT AT ZONE 511. MAINTENANCE REPAIRED THE LINE AND SUBMITTER IS IN THE PROCESS OF CHECKING THE REST OF FLEET. (X)SDR 95ZZZX4055Elt Tray · crackedDURING DETAILED PHASE NR 6 INSPECTION, ELT MOUNTING TRAY WAS DISCOVERED AS BEING CRACKED. UNIT WAS REPLACED WITH A NEW ELT ASSEMBLE.SDR S2YA950010Acm Inlet Duct · improper instlFOUND THE AIR CYCLE MACHINE INLET DUCT INSTALLED BACKWARDS ON THE BOTTOM OF THE LT WING PANEL WELD ASSEMBLY. REMOVED AND REINSTALLED THE LOUVER IN THE PROPER POSITION. THIS HAD ALSO OCCURRED ON AIRCRAFT S/N UE-145, BOTH FROM THE FACTORY. (X)SDR 95ZZZX4057Elt Harness · wetELT TRANSMITS CONSTANTLY - FOUND REMOTE SWITCH HARNESS SHORTED AND UNIT WAS WET. REMOVED AND REPLACED BATTERY PACK, PN 452-0130, AND REMOTE SWITCH HARNESS, PN 118-340002-1.SDR S2YA950009Axle · incorrect diaDISCOVERED BOTH INNER AND OUTER WHEEL BEARINGS, PN 13899, WERE FROZEN IN PLACE ON NLG STRUT ASSY AXLE SHAFT, PN 114-820026-1, WHILE TRYING TO REMOVE THE NOSE WHEEL AND TIRE ASSY. ATTEMPTED DRY ICE AND HEATING OF THE BEARING RACE TO FACILITATE REMOVAL, TO NO ASDR S2YA950008Radome · leaksTHE RADOME TO FUSELAGE MOUNT AREA AT FS 30.00 HAD TO BE SEALED TO PREVENT PREMATURE RADAR FAILURES DUE TO MOISTURE. AS THE RADAR TRANSIT/RECEIVER IS HIGHLY SUSCEPTIBLE TO ANY WATER. WE HAVE HAD MULTIPLE FAILURES DUE TO THIS PROBLEM. THE REST OF FLEET WAS SESDR S2YA950007Connector · looseTHE CREW REPORTED THEIR RADAR FAULTED SEVERAL TIMES DURING AN ATTEMPTED FERRY FLIGHT AND THEN FAILED. THEY THEN TURNED BACK TO THEIR ORIGINATION BECAUSE OF WEATHER CONDITIONS. MAINTENANCE RESEATED THE CANNON PLUGS AT THE COLLINS WX RADAR CONTROL PANEL, PN 62
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