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 017041Powerpack · failedLANDING GEAR WOULD NOT EXTEND, MANUAL EXTENSION PERFORMED. REPLACED HYD POWER PACK IAW MM, OP AND LEAK CHECKED GOOD.SDR GLBA20030531Circuit Board · failedNR 1 AND NR 2 ENVIRO FAILS, REMOVED AND REPLACED A130 PCB. OPS CK GOOD.SDR 57841Downlock · inoperativeAFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQUIRED. OPS CK GOOD.SDR 57827Autofeather Sys · malfunctionedON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL.SDR CA040202011Handle · failed(CAN) DURING TAKEOFF ROLL THE AIRSTAIR DOOR EXTERIOR HANDLE SEPARATED FROM THE DOOR. FURTHER INSPECTION FOUND IMPACT DAMAGE TO LT PROPELLER AND LT IB FLAP. APPROXIMATELY ONE INCH MISSING FROM TIP OF ONE PROPELLER BLADE AND DENT IN LOWER SKIN OF IB FLAP. HANDLESDR CA040122004Bracket · cracked(CAN) DURING GROUND HANDLING, CREW ATTEMPTED TO OPEN DOOR FROM INSIDE AND THE MAIN HANDLE UPON APPLYING PRESSURE, RELEASED WITHOUT ACTUATING DOOR CAMS. MAINTENANCE FOUND THAT THE MAIN DOOR ACTUATION BRACKETHAD BROKEN INTO TWO PIECES. THE BRACKET WAS REPLACED ASDR GLBA20030528Connector · dirty104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.SDR GLBA2003528Connector · inoperative104 PERCENT N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.SDR GLBA20030527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONSDR GLBA2003527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONSDR GLBA20030525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.SDR GLBA20030524Indicator · intermittentCAPT HAS NO AIRSPEED INDICATION, ASI STARTED WORKING ABOUT HALF WAY ON FERRY FLIGHT. DID PITOT STATIC TEST OPS CK GOOD.SDR GLBA2003525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.SDR GLBA2003524Indicator · intermittentCAPT HAS NO AIRSPEED IND, ASI STARTED WORKING ABOUT HALF WAY TO DEN ON FERRY FLIGHT. DID PITOT STATIC TEST, OPS CK GOODSDR AMWA112Seal · crackedDURING INSPECTION RT ENGINE FIRE SEAL WAS FOUND TO BE CRACKED ON THE O/B CENTER WEB, IN CENTER AREA OF WEB APPROX 3.5 INCHES LONG. REPAIRED BY REPLACING WEB ASSY ACCORDANCE WITH SRM.SDR AMWA111Firewall · crackedDURING INSPECTION RT ENGINE FIRE WALL WAS FOUND CRACKED AROUND THE O/B SECTION OF WEB APPROX AT 5 INCHES LONG IN VERT POSITION. BEHIND ATTACH ANGLE FOR COWLING. THEN CRACK TURNS HORIZONTAL GOING I/B APPROX 2.5. REPAIRED DAMAGE AREA BY STOP DRILLING CRACK ENSDR GLBA20030523Antenna · malfunctionedBOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, R&R ANTENNASDR GLBA2003523Display · defectiveBOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, PENDING CORRECTIVE ACTION.SDR 57548Coupling · wornUPON APPROACH TO MCI LANDING GEAR WOULD NOT EXTEND. CREW AND MX CONTROL DECIDED TO HAVE AIRCRAFT RETURN TO LIT, AS IT WAS A REPOSITION FLIGHT. UPON ARRIVAL AT LIT, THE GEAR WAS PUMPED DOWN AND HAD 3 GREENS. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. SDR GLBA20030522Switch · out of adjustCARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, ADJUSTED DOOR AJAR SWITCH OPS CK GOODSDR GLBA20030521Warning Light · illuminatedPULLED O2 MASKS FOR PAX WITH CAB ALT HI ANNUNCIATORS COULD NOT DESCANT DUE TO ICING, REINSTALLED MASKS CAB ALT HIGH LIGHT CAME ON DUE TO RT BLEED SYS IN OFF. OPS CK GOOD.SDR 364032Switch · sparksWHEN THE NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON WAS PUSHED IT CAUSED ELECTRICAL SPARKS. REMOVED AND REPLACED NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON, SPARKS WHERE CAUSED BY LOOSE BUTTON WHICH SHORTED AGAINST YOKE.SDR 57453Brake · inoperativeUPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.SDR GLBA20030520Brush Block · inoperativeRT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5.SDR 2004F00360Brake · malfunctionedFLT 9227 - NAS-FLL - AFTER LANDING, BRAKES ARE SPONGY AND LOSE PRESSURE WHILE TURNING AND STOPPING. BLED BRAKES. LEAK CHECK OK. OPERATIONAL CHECK NORMAL. (M)SDR 364031Door Frame · wornWORN NOTCH IN CARGO DOOR FRAME LOWER EDGE MID SPAN, REMOVED DAMAGED AREA AND INSTALLED AN INSERTION REPAIR WITH SPLIT DOUBLER ON UNDERSIDE TO SUPPORT THE RIB IAW SRM SKIN DAMAGE ( NON PRESSURIZED AREA).SDR GLBA20030519Windshield · crackedCAPT WINDSHIELD CRACKED RETURN TO AIRPORT, REMOVED AND REPLACED WINDSHIELD PN 101-384025-17.SDR AMWA110Rib · crackedDURING INSPECTION FOUR CRACKS FOUND ON THIS RIB, TWO ON THE LT SIDE AND TWO ON THE RT SIDE LOCATED ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46 & 101-640000-38. LT STRINGER P/N 101-640000-39 & 101-640000-45.SDR AMWA109Rib · crackedDURING INSPECTION, FIVE CRACKS FOUND IN THIS RIB, THREE ON THE RT SIDE AND TWO ON THE LT SIDE LOCATED ON THE STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-45, 101-640000-42 & 101-640000-38. LT STRINGER P/N 101-640000-43, 10SDR AMWA107Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39.SDR AMWA108Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON RT SIDE ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46.SDR GLBA20030516Switch · dirtyCARGO DOOR ANNUNCIATOR LIGHT CAME ON IN FLIGHT, CLEANED CARGO DOOR WARNING SWITCHES & ADJUSTED CARGO DOOR AJAR SWITCH OPS CK GOODSDR 57206Brake · malfunctionedAFTER LANDING IN PIT. CREW REPORTED THAT THE LT BRAKE HAD VERY LITTLE PRESSURE ON TAXI. BLEED LT BRAKES SYS. IAW MM 32-40-00. OPS AND LEAK CK GOOD.SDR 57174Indicator · failedAFTER TAXING OUT FROM GATE. CREW NOTED LT TORQUE INDICATOR WENT TO ZERO ON INITIAL SPOOL UP FOR TAKEOFF. CREW THEN RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE INDICATOR.SDR 57171Gyro · inoperativeSHORTLY AFTER DEPARTURE FROM PIT CREW NOTICED CAPT'S GYROSCOPIC DIRECTIONAL COMPASS SYSTEM WASN'T WORKING CORRECTLY. SO DECEIDED TO RETURN TO PIT. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. T/S REPAIRED PINS 5 AND 7 OF CONNECTOR J203 AT NR 1 FLUX DETECTOSDR AMWA98Doubler · debondedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, ONE RIGHT BONDED DOUBLER WAS FOUND TO BE DISBONDED.SDR AMWA104Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 124 WAS FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA97Doubler · delaminatedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT DOUBLER WAS FOUND TO BE DISBONDED.SDR AMWA102Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENERS AT LWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA95Rivet · shearedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE HEAVY ANGLE HAD ONE SHEARED RIVET.SDR AMWA96Seat Track · damagedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE DAMAGED.SDR AMWA106Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 105 WERE FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA103Fastener · corrodedDURING SCHEDULED STRUCTURAL INSPECTION, TWO FASTENERS AT LWS 55 WERE FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA94Rivet · shearedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE WINDOW FINGER DOUBLER WAS FOUND TO HAVE ONE SHEARED RIVET.SDR AMWA105Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 128 WAS FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA100Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 124 WERE FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA99Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, SEVEN FASTENERS AT RWS 125-131 WERE FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA101Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, THREE FASTENERS AT RWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.SDR AMWA93Keelbeam · wornDURING A DETAIL INSPECTION, THE FORWARD LEFT INBOARD LOWER KEEL WAS WORN AT THE GRAVEL FENDER ATTACH BRACKET.SDR AMWA91Angle · crackedDURING AN ABC STRUCTURAL INSPECTION, THE RIGHT HEAVY ANGLE WAS FOUND TO BE CRACKED.
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