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 GLBA001Tach Generator · looseNR 1 PROP RPM 1450 IDLE AT 600, TIGHTENED NR 1 N2 TACH GEN.Sep 1, 2003 · N96UX · Beech 1900D · Engine Indicating SystemSDR 255031Yoke · excess playEXCESSIVE PLAY IN ALL QUADRANTS IN CAPTAINS YOKE BOTH PITCH AND ROLL AXIS.Sep 1, 2003 · N136MJ · Beech 1900D · Control Column SectionSDR CA030905004Selector · failed(CAN) AIRCRAFT WENT ON LOCAL FLIGHT, WHEN GEAR SELECTED DOWN ON PREPARATION FOR LANDING GEAR DID NOT GO DOWN, CREW MANUALLY PUMPED GEAR DOWN AND RECEIVED 3 GREEN INDICATION. AFTER LANDING, AIRCRAFT WAS PLACED ON JACKS AND GEAR SWINGS CARRIED OUT. GEAR FUNCTIONAug 30, 2003 · Beech 1900D · Landing Gear SelectorSDR 8544318Bolt · looseDURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE.Aug 27, 2003 · N854CA · Beech 1900D · Rudder Control SystemSDR GLBA2003126Wire · brokenCABIN SIDE HEADSET GETS A LOT OF STATIC AND CUTS IN AND OUT, REPAIRED WIRING UNDER ENTRY FLOORBOARD BETWEEN CAPT'S PHONE JACK TO OBSERVE, PHONE JACK. OPS CK GOOD.Aug 27, 2003 · N201GL · Beech 1900D · Communications System WiringSDR GLBA2003125Indicator · inoperativeRT ITT INDICATOR NOT WORKING, REMOVED AND REPLACED INDICATOR.Aug 27, 2003 · N184UX · Beech 1900D · Engine EGT/TIT Indicating SystemSDR 53866Printed Ckt Board · faultyUPON APPROACH TO VPS LANDING GEAR WOULD NOT EXTEND. A SECOND ATTEMP WAS MADE WITH THE SAME THING NO DOWN AND LOCKED INDICATION FLY BY OF TOWER AT VPS. CONFIRMED GEAR WAS NOT DOWN. GEAR WAS THEN PUMPED DOWN AND LOCKED CONFIRMED BY GEAR DOWN AND LOCK INDICATIAug 26, 2003 · N176YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR CA030825015Indicator · shorted(CAN) DURING CURISE FLIGHT, CREW NOTED ELECTRICAL ODOR AND SMOKE IN COCKPIT AREA. THE AIRCRAFT RETURNED TO ORIGINAL DEPARTURE LOCATION. THE DURATION OF THE SMOKE/SMELL WAS VERY BRIEF. MAINTENANCE REPLACED THE AC VOLTMETER INDICATOR WHICH APPEARS TO HAVE SHORTAug 24, 2003 · Beech 1900D · AC Indicating SystemSDR GLBA2003124Door · openCABIN DOOR OPENED IN FLIGHT. REMOVED AND REPLACED AIRSTAIR DOOR RIG, CK AND LEAK CHECK GOOD.Aug 23, 2003 · N192GL · Beech 1900D · Entrance StairsSDR GLBA2003123Indicator · stuckRT TORQUE INDICATOR IS STUCK AT 300LB, REMOVED AND REPLACED RT TORQUE GAUGE. OPS CHECK GOOD.Aug 23, 2003 · N255GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GLBA2003122Controller · failedTRANSPONDER CONTROL WENT BLANK. REMOVED TRANSPONDER CONTROL P/N 622-9352-003, RE-SEATED IT, OPS CHECK GOOD.Aug 22, 2003 · N208GL · Beech 1900D · ATC Transponder SystemSDR CA030825014Shaft · broken(CAN) DURING CLIMB, CREW SELECTED FLAPS '0' BUT NOTED THAT PANEL NR 4 DID NOT APPEAR TO RETRACT ALL THE WAY UP. FLIGHT CONTINUED TO DESTINATION AND FLAPS WERE CONFIRMED TO BE ALL UP EXCEPT NR 4 WHICH WAS HANGING DOWN BY APPROX 4 DEGREES. THE .5000 & .7500 PANAug 21, 2003 · Beech 1900D · Leading Edge Slat Control SystemSDR AUS20030808Shaft · broken(CAN) DURING CLIMB, CREW SELECTED FLAPS '0' BUT NOTED THAT PANEL NR 4 DID NOT APPEAR TO RETRACT ALL THE WAY UP. FLIGHT CONTINUED TO DESTINATION AND FLAPS WERE CONFIRMED TO BE ALL UP EXCEPT NR 4 WHICH WAS HANGING DOWN BY APPROX 4 DEGREES. THE .5000 & .7500 PANAug 21, 2003 · Beech 1900D · Leading Edge Slat Control SystemSDR AMWA30Rib · crackedWHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA29Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA28Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA24Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA23Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA22Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA20Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 53738Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STABILIZER, THE RIB FLANGES AT CANTED STAB STA. 39.289 AND STAB STA. 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IAW STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03Aug 18, 2003 · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 53566Governor · failedAFTER TAKEOFF ON FLIGHT 5549 FROM PITTSBURGH PENSYLVANIA, THE LEFT PROP RPM ONLY SHOWED 1500 RPMS. THE CREW RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROP GOVERNOR. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE.Aug 15, 2003 · N144ZV · Beech 1900D · Propeller GovernorSDR GLBA2003121Trim Switch · out of adjustNR 2 ENG EXCEDED ITT TAKE OFF LIMITS 3392 ON TORQUE, READJUSTED TRIM STICK OHMS TO PROPER ADJUSTMENT.Aug 14, 2003 · N96UX · Beech 1900D · Engine EGT/TIT Indicating SystemSDR GLBA2003120Landing Gear · inoperativeLANDING GEAR WOULD NOT RETRACT, CND CHECK FLIGHT SATISFACTORY.Aug 14, 2003 · N94GL · Beech 1900D · Main Landing GearSDR AMWA21Bulkhead · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SHELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FWD PRESSURE BULKHEAD AT FS 84 BELOW THE SHELF. THE CRACK RUAug 13, 2003 · N139ZV · Beech 1900D · Fuselage Main, BulkheadSDR 2003F00575Pressure Blkhd · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FORWARD PRESSURE BULKHEAD AT FS. 84, BELOW SELF. THE CRACK RUNAug 13, 2003 · N139ZV · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2003119Fire Detector · malfunctionedLT FIRE LOOP ANNUNCIATOR ILLUMINATED FOLLOWED BY LT FIRE HANDLE FLICKERING, INSPECTION LT ENG FIRE LOOP AND CONNECTORS, OPS CK GOODAug 13, 2003 · N220GL · Beech 1900D · Fire DetectionSDR GLBA2003118Connector · looseWX RADAR DOES NOT TILT, SECURED LOOSE CONNECTOR ON ANTENNA.Aug 11, 2003 · N208GL · Beech 1900D · Weather Radar SystemSDR 53367Connector · dirtyUPON TAKEOFF ON FLIGHT 5576 THE WEATHER RADAR FAILED. THE CREW RETURNED TO THE FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND RESEATED THE ANTENNA CONNECTOR. NO PARTS WERE USED THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.Aug 8, 2003 · N13ZV · Beech 1900D · Weather Radar SystemSDR 2003F00561Truss · crackedAT SCHEDULED MAGNUFLUX INSPECTION, ENGINE TRUSS WAS DETERMINED TO HAVE A RADIAL CRACK IN THE LOWER RIGHT GUIDE PIN RADIUS. RAYTHEON AIRCRAFT COMPANY, THE MANUFACTURER, DETERMINED THAT THE BOSS GUIDE WAS NOT REPAIRABLE AND THAT ITS REPLACEMENT WOULD REQUIRE USAug 6, 2003 · N69549 · Beech 1900D · Engine Mount SectionSDR CA030808001Bearing · failed(CAN) AIRCRAFT DEPARTED. DURING THE END OF CLIMB OUT THE RT (NR 2) GENERATOR ANNUNCIATOR ILLUMINATED. GENERATOR WOULD NOT RESET, AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE CHECKS CARRIED OUT NR 2 ENGINE WOULD NOT TURN ON START, GENERATOR REMOVED, INSPECTED AND Aug 6, 2003 · Beech 1900D · Starter-GeneratorSDR 53300Rudder · malfunctionedAFTER DEPARTURE, ON FLIGHT 5530, THE CREW HAD A HARD RT THEN LAT UNCOMMANDED RUDDER BOOST. WHILE EXECUTING THE UNCOMMANDED RUDDER BOOST ACTIVATION EMERGENCY PROCEDURE CHECKLIST A THIRD SEVERE RUDDER BOOST ACTIVATION OCCURRED, FOLLOWED BY SEVERE OSCILLATIONS OAug 6, 2003 · N5YV · Beech 1900D · Rudder Control SystemSDR 53305Powerpack · failedWHILE ON APPROACH INTO PITTSBURGH PENNSYLVANIA ON FLIGHT 5557 THE CREW SELECTED THE LANDING GEAR DOWN AND THE GEAR DID NOT GO DOWN. THE LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW INFORMED AIR TRAFFIC CONTROL OF MISSED APPROACH AND PROCEEDED FOR A HOLD. TAug 6, 2003 · N144ZV · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR GLBA2003114Tire · separatedNR 2 TIRE TREAD CAME OFF. REMOVED AND REPLACED NR 1 & 2 WHEEL ASSY.Aug 5, 2003 · N261GL · Beech 1900D · TireSDR GLBA2003113Uplock Switch · malfunctionedGEAR INTRANSIT LIGHT DID NOT EXTINGUISH. REMOVED AND REPLACED RT MLG UPLOCK SWITCH.Aug 3, 2003 · N211GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2003111Receiver · incorrectNAV NEEDLE SHOWED 15 DEG ERROR BETWEEN EACH OTHER. REMOVED AND REPLACED NR 2 NAV RECEIVER.Aug 2, 2003 · N253GL · Beech 1900D · Navigation SystemSDR 53163Light · inoperativeDURING FLIGHT 2511 FROM DALLAS/FORT WORTH TEXAS TO ELDORADO ARKANSAS, THE CREW RETRACTED THE LANDING GEAR, THE RED INTRANSIT GEAR HANDLE LIGHTS DID NOT ILLUMINATE. PRESSED THE GEAR HANDLE LIGHT TEST SWITCH AND THE LIGHTS STILL DID NOT ILLUMINATE. CONTACTED MAug 1, 2003 · N26YV · Beech 1900D · Landing Gear Position and WarningSDR 53080Flap · malfunctionedAFTER TAKEOFF FROM PANAMA CITY FLORIDA ON FLIGHT 5445, THE FLAPS WERE SELECTED UP, STAY AT 17 DEGREES. THE CREW DECIDED TO RETURN TO PANAMA CITY FLORIDA WITH NO FURTHER INCIDENT. THE FLAPS WERE RETRACTED TO ZERO AND MEL'D. THE AIRCRAFT WAS RETURNED TO SERVIJul 30, 2003 · N165YV · Beech 1900D · Trailing Edge Flap Control SystemSDR 2003F00552Hose · leakingUNIDENTIFIABLE ODOR IN THE CABIN WHEN BLEEDS ARE ON. REMOVED AND REPLACED LEFT ENGINE FUEL PURGE PNEUMATIC HOSE. LEAK CHECK GOOD. (M)Jul 26, 2003 · N87551 · Beech 1900D · Pneumatic Distribution SystemSDR AMWA27Rivet · looseWHILE PERFORMING AN ABC STRUCTURAL INSPECTION, TWO RIVETS WERE FOUND TO BE LOOSE ON THE RIGHT SIDE OF THE FUSELAGE AT APPROXIMATELY FS 220.75, STRINGER 5R. REPAIR ACCOMPLISHED. NO TEAR DOWN REPORT WILL BE REQUIRED.Jul 24, 2003 · N131YV · Beech 1900D · FastenersSDR AMWA26Clip · crackedDURING ABC CHECK, A RIGHT HAND CLIP WAS FOUND CRACKED. REPLACED CLIP IN ACCORDANCE WITH BEECH SRM 53-90-23. NO TEAR DOWN REPORT WILL BE REQUIRED.Jul 24, 2003 · N131YV · Beech 1900D · Fuselage Miscellaneous StructureSDR AMWA25Hinge · crackedDURING ABC CHECK, THE CARGO DOOR HINGE WAS FOUND CRACKED. REPLACED HINGE IN ACCORDANCE WITH BEECH SRM 52-90-01. NO TEAR DOWN REPORT WILL BE REQUIRED.Jul 24, 2003 · N131YV · Beech 1900D · Fuselage, Door HingeSDR GLBA2003109Gyro · frozenNR 1 DG FROZE. REMOVED AND REPLACED NR 1 DG.Jul 21, 2003 · N240GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 52767AMWA01Governor · malfunctionedDURING TAKEOFF ON FLIGHT 5578 FROM READING PENNSYLVANIA TO PITTSBURGH, THE POWER ADDED TO THE RIGHT ENGINE WOULD NOT DEVELOPE MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE ANJul 20, 2003 · N144ZV · Beech 1900D · Propeller GovernorSDR 52767AMWA02Bleed Valve · inoperativeDURING TAKE OFF ON FLIGHT 5578, THE POWER ADDED TO THE RT ENGINE WOULD NOT DEVELOP MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKE OFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE AND THE PROP GOVERNOR. STILL AWAITING MORE INFJul 20, 2003 · N144ZV · Beech 1900D · Compressor Bleed ValveSDR 52767Bleed Valve · inoperativeDURING TAKE OFF ON FLIGHT 5578, THE POWER ADDED TO THE RT ENGINE WOULD NOT DEVELOP MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE AND THE PROP GOVERNOR. STILL AWAITING MORE Jul 20, 2003 · N144ZV · Beech 1900D · Compressor Bleed ValveSDR 52776AMWA1Generator · failedON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RT GENERATOR WOULD NOT STAY ONLINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. MAINTENANCE REMOVED AND REPLACED GENERATOR, GCU AND REPAIRED A WIREJul 20, 2003 · N237YV · Beech 1900D · DC Generating SystemSDR 52776Starter Gen · failedON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RIGHT GENERATOR WOULD NOT STAY ON LINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACEDJul 20, 2003 · N237YV · Beech 1900D · Starter-GeneratorSDR 52743Bleed Valve · failedON FLIGHT 5561, THE CREW WAS TAXING OUT WHEN THEY NOTICED THE RT ENGINE WOULD ONLY MAKE 1000 FT LBS TORQUE ON TAKE OFF. THE TAKE OFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE WITHOUT ANY FURUTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVEDJul 19, 2003 · N144ZV · Beech 1900D · Compressor Bleed ValveSDR 52753Bracket · out of positionON FLIGHT 5541 FROM LATROBE PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, AFTER TAXI OUT THE RIGHT AILERON TRAVEL HAS A CATCH AND A NOISE. THE CREW RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED THE COVERING IN THE COCKPIT OVER THE CONJul 19, 2003 · N174YV · Beech 1900D · Control Column Section
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