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 GUU2004F00011Bracket · corrodedAT SCHEDULED ROUTINE MAINTNANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.SDR GLBA2003039Connector · looseNR 1 NAV FAILED. TIGHTENED CONNECTION ON SPLITTER, OPS CHECK GOOD.SDR 049124Circuit Breaker · failedAFTER TAKE OFF FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 706,WHEN THE LANDING GEAR WAS SELECTED UP, SMOKE WAS DETECTED FROM THE RIGHT HAND CIRCUIT BREAKER PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. THE CREW RETURNED TO FASDR GLBA2003037Windshield · failedF/O`S WINDSHIELD SHATTERED. REMOVED AND REPLACED WINDSHIELD.SDR GLBA2003038Receiver · failedNR 1 NAV FAILED. REMOVED AND REPLACED NR 1 NAV VIR32.SDR GUU2004F00012Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.SDR GLBA2003036Wire · brokenLT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUM. REPAIRED BROKEN WIRE SPLICE ON LEFT ENG FIRE BOTTLE SQUIB.SDR GLBA2003035Altimeter#1 ALTIMETER RED FLAGGED, R&R ALTIMETERSDR NSVA20030021Drain Valve · brokenRT wing main fuel tank, outboard of Nacelle, drain valve came apart at insert and started leaking fuel. The drain valve consists of a housing and then an insert (which is the quarter turn drain assembly). These two units are held together with what appears tSDR CA030303001Engine · failed(CAN) DURING CRUISE, CREW NOTICED OIL PRESSURE DROPPING, PRIOR TO LOWER LIMIT, ENGINE WAS SECURED/SHUTDOWN. FLIGHT CONTINUED TO DESTINATION 20 MINUTES OUT AND LANDING COMPLETED WITHOUT INCIDENT. ENGINE STRIP INDICATES ANOTHER (BLACK OIL/CARBON IN OIL) ENGINESDR CA030324002Bearing Race · cracked(CAN) PROP REMOVED DUE TO EXCESSIVE BLADE RADIAL PLUS END PLAY. UPON DISASSEMBLY 2 OPPOSING BLADE BEARING WERE FOUND TO BE CRACKED. HUB FORWARDED TO HARTZELL FOR EVALUATION OF DAMAGE.SDR CA030318017Hose · cut(CAN) DURING A WALK AROUND, THE CREW NOTICED HYDRAULIC FLUID IN THE RT MAIN GEAR AREA.MAINTENANCE FOUND THAT THE RETRACT LINE HAD BEEN CUT CLOSE TO THE IDENTIFICATION CLAMP. THE CUT OCCURED NEAR THE CLAMP WHICH MAY INDICATE A CYCLIC FAILURE WITH THE CLAMP BEINSDR GLBA2003034Gyro · failedNR 2 EADI ROLL ANNUNCIATE. REMOVED AND REPLACED VERT GYRO, OPS CHECK GOOD.SDR GLBA2003033Meter · inoperativeRT DC LOAD METER INOP. REMOVED AND REPLACED RT DC LOAD METER.SDR GLBA2003032Switch · out of adjustCARGO DOOR ANNUN ILLUMINATED. ADJUSTED DOOR JAMB SWITCH, OPS CHECK GOOD.SDR 048803Solenoid · stuckUPON LANDING ON FLIGHT 5487 IN PHILADELPHIA PENNSYLVANIA, THE CREW THOUGHT IT WAS A DESTABILIZING FLARE DUE TO LEFT QUARTERING TAILWIND. THEY WENT AROUND TO LAND ON A DIFFERENT RUNWAY TO FIND IN THE FLARE IT WAS THE LEFT PROP THAT WAS IN GROUND FINE WHEN THE PSDR S2YA03011Downlock Switch · failedDURING APPROACH OF FLIGHT 1019, THE CREW DID NOT ACHIEVE A DOWN AND LOCKED INDICATION FOR THE RT MAIN GEAR. THE CREW MANUALLY EXTENDED THE GEAR. THE CREW STILL DID NOT GET THREE GREEN BUT THE IN-TRANSIT LIGHT EXTINGUISHED. THE CREW DID NOT DECLARE AN EMERGESDR AUS20030369Fitting · damaged(AUS) WING FORWARD ADAPTER PLATE DAMAGED. FASTENER HOLES ELONGATED. FRETTING AND CORROSION ALSO EVIDENT.SDR CA030312020Gyro · intermittent(CAN) AIRCREW AT GATE REPORTED DIFFICULTY IN HAVING CAPTAINS ATTITUDE INDICATOR COMING ON LINE. A/C WAS TAXIED TO HANGAR WHERE MAINT REPLACED NR 1 VERTICAL GYRO. SYSTEM WAS TESTED AND A/C RETURNED TO GATE. AT APPROX 10,000 FT CAPTAINS ATTITUDE INDICATOR FLAGGSDR S2YA03010Probe · faultyDURING TAKEOFF ROLL OF FLIGHT 1050, THE CREW NOTICED A FUEL QUANTITY ANNUCIATOR ILLUMINATED. THE CREW RETURNED TO GATE AND MEL-ED THE SYSTEM. ON 3/14/03 MECHANIC CLEARED THE MEL BY REPLACING A FUEL PROBE. MECHANIC RETURNED THE AIRCRAFT TO SERVICE WITH NO FUSDR 2003NSVA00020Support · brokenDuring taxi out the cabin door light illuminated. Crew taxied back to gate and FO was able to open the door without pushing in the door lock release button. Maintenance found the door handle upper support assembly broken. Replace the support and returned thSDR CA030312021Indicator · failed(CAN) DURING TAXI, FLIGHT CREW NOTED INCREASE IN OIL TEMPERATURE ON RIGHT ENGINE. CREW ELECTED TO RETURN TO GATE. MAINTENACE FOUND OIL TEMP PORTION OF DUAL INDICATOR (PRESSURE) AT FAULT. INDICATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 048548Gas Generator · failedCREW WAS ON TAKE OFF ROLL WHEN POWER WAS APPLIED TO THE NR 2 ENGINE. THE CREW HEARD A LOUD BANG FROM THE RIGHT SIDE OF THE AIRCRAFT. THEY ABORTED THE TAKE OFF AND TAXIED BACK DOWN TO THE GATE. THEY PROCEEDED TO PERFORM A CHECKLIST BY VISUALLY INSPECTING ENGINESDR AMWA17Finger Doubler · crackedWHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER. NO TEARDOWN REPORT WILL BE REQUIRED.SDR AMWA18Plate · damagedWHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE PER THE STANDARD REPAIR MANUAL 57-95-02. NO TEARDOWN REPORT WILL BE REQUIRED.SDR GLBA2003029Indicator · failedNR 1 ALTIMETER FLAGGED. PERFORMED PITOT-STATIC CHECK OF SYSTEM, OPS CHECK GOOD.SDR GLBA2003028Brush BlockLH PROP DEICE INOP, REPLACED BRUSH BLOCKSDR NSVA200300017Rivet · looseDURING ACCOMPLISHMENT OF NR 6 DETAILED INSPECTION FOUND THE LT ELEVATOR TORQUE TUBE RIVETS WORKING CAUSING EXCESSIVE PLAY AT ELEVATOR TRAILING EDGE. THE ELEVATOR WAS REMOVED AND THE TORQUE TUBE REPLACED. ELEVATOR REINSTALLED PER ALL MAINTENANCE MANUAL INSTRUSDR AMWA16Structure · damagedON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERTICAL AND SDR 048329Structure · bird strikeON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERITCAL AND SDR CA030305005Connector · cracked(CAN) CREW REPORTED THAT AUTOFEATHER DISABLE LIGHT WOULD ILLUMINATE DURING CLIMB AND DECENT PORTIONS OF FLIGHT. MAINTENANCE DID NUMEROUS ATTEMPTS TO DUPLICATE WITH SYSTEM PARTS BEING REPLACED FOR TROUBLESHOOTING PURPOSES. TEST FLIGHTS WHERE COMPLETED WITH THE SDR GLBA2003025Tube · disconnectedRIGHT BLEED AIR FAIL. RECONNECTED EVA TUBING ON LT INBOARD WING, OPS CHECK GOOD.SDR 048276Downlock Switch · failedUPON LANDING OF FLIGHT 5549 INTO MESSINA NEW YORK, THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR. THE CREW MADE SEVERAL ATTEMPS AND THEN LANDED AT THEIR DESTINATION WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SQUAT SWITCH. NO TEARDOWN REPOSDR GLBA2003026Windshield#1 WINDSHIELD CRACKED, REPLACED #1 WINDSHIELDSDR NSVA200300014DoorLGA: Passenger door sticking. MX lubricated exterior release switch on door with LPS Type 1.SDR AMWA15Spar · chafedUPON A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RIGHT SPAR CHAFED ON THE FORWARD SIDE. ALSO THE RT WING MAIN SPAR CHAFED BY FUEL PRESSURE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED OUT THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWNSDR GLBA2003024BoltCABIN DOOR INNER HANDLE LOOSE, R&R BOLTS OPS CHECK GOODSDR 2003F00384Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 2.75 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS REPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN RAYTHEON FIELD REPAIR FR-CO-00830 REV A. (M)SDR NSVA200300009Fire Loop · inoperativePWM-On take off roll, LH Fuel Fire-wall S/O Valve light in handle illuminated. Amp Detect (LH Side) fails to illuminate the fire-wall Fuel S/O valve handle. Take off was aborted, aircraft returned to gate. MX found no eveidence of fire. Trouble shooting of sysSDR 048076Keel · gougedWHILE DOING AN INSPECTION, MAINTENANCE DISCOVERED THE LT INBOARD MAIN LANDING GEAR KEEL WAS GOUGED. MAINTENANCE REPAIRED THE KEEL. NO TEARDOWN REPORT WILL BE REQUIRED.SDR GUU2003F00006Contactor · dirtyDURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS. CONTINUED TO DESTINATION. CLEANED CONTACTS AT LEFT FIRE BOTTLE. OPERATIONAL CHECK, OK.SDR GLBA2003019Switch · out of adjustRIGHT ANTI-ICE ANNUNCIATOR ILLUMINATED. ADJUSTED RT ICE VANE SENSE SWITCHES, OPS CK GOOD.SDR GLBA2003020Display · inoperativeNR 2 EADI SCREEN FAILED, REPLACED EADI OPS CHECKED SYSTEM SATISFACTORYSDR 048044Skin · delaminatedWHILE INBOUND FROM PONCA CITY, OKLAHOMA TO ENID OKLAHOMA ON FLIGHT 2501, SEAT 4F EMERGENCY EXIT OUTER SKIN PEELED OFF AND DEPARTED FROM THE AIRCRAFT WHILE INFLIGHT. THE CREW DECLARED AN EMERGENCY LANDING. THERE WAS NO FURTHER INCIDENT. MAINTENANCE FOUND HOLES SDR 048029Engine · leakingON FLIGHT 5427 FROM SHREVEPORT LOUISIANA TO NEW ORLEANS LOUISIANA, UPON TAKE OFF ROLL AT 60-70 KIAS, THE TORQUE SURGED TO MAXIMUM. THE LEFT PROP RPM DROPPED TO APPROXIMATELY 1000-1200 RPM. THE TAKE OFF WAS ABORTED. THE CREW RETURNED THE THE GATE WHERE MAINTENASDR AMWA13Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT SPAR CAP WAS CHAFING THE WHEEL WELL. BLENDED THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.SDR GLBA2003017Vane · stuckSTALL WARNING SOUNDED ON ROTATION, RELEASED STUCK VANE TEST FLIGHT OKSDR AMWA12Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP WAS CHAFFING. BLENDED OUT THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.SDR CA030224001Fastener · loose(CAN) UPON INSPECTION OF THE ELEVATOR SYSTEM AND TAIL AREA, THE LT ELEVATOR TORQUE TUBE FASTENERS WERE FOUND LOOSE. OUT OF THE 8 FASTENERS, 7 WERE LOOSE AND 1 HAD SHEARED OFF. NO OVERSIZE FASTENERS ARE APPROVED ON (SERIAL NUMBER UE-258) AIRCRAFT AND AFTER. SDR AMWA11Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP BEHIND INNER FENDER WAS CHAFED BY FUEL PRESSURE SWITCH LINE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED , ALODINED AND PRIMED THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIE
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