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 GUU2002F00021Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00020Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM.SDR AUS20020579Rib · corroded(AUS) RH WING CORRODED IN AREA OF LOWER AFT INBOARD CORNER. CORROSION AFFECTED LOWER WING SKIN, REAR SPAR AND THE UPPER SURFACE OF THEHORIZONTAL LEG OF THE CENTRE WING MAIN RIB.SDR GLBA2002080Transducer · intermittentSTALL WARNING INTERMITTENT. REPLACED TRANSDUCER.SDR GLBA2002078Indicator · malfunctionedNR 1 PROP INDICATOR FLUX. SWAPPED INDICATORS, OPS CHECKED SYSTEM SATISFACTORY. RETURNED TO SERVICE.SDR GLBA2002076Cable · brokenCABIN DOOR WILL NOT OPEN. REPLACED INNER DOOR CABLES, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2002074Bypass Valve · leakingLEFT ENVIRONMENTAL FAIL. REPLACED BYPASS VALVE.SDR GLBA2002077Probe · out of adjustRIGHT ENGINE TEMP LIMITED. ADJUSTED TRIM PROBE, OPS CHECKED SATISFACTORY.SDR GLBA2002075Lever · out of adjustBOTH PROPS WOULD NOT REACH 1700 RPM. ADJUSTED PROP RPM LEVER, OPS CHECKED SYSTEM SATISFACTORY.SDR GUU2002F00006Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM.SDR JJB2002F00001Bolt · bentDURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS, UNIT UNDER INVESTIGATION.SDR GLBA2002072Cable · brokenPAX DOOR WOULD NOT OPEN. INSPECTED FOUND INNER DOOR CABLE BROKEN. REPLACED INNER DOOR CABLES.SDR GLBA2002073Propeller · malfunctionedRIGHT PROP WOULD NOT ADJUST OR FEATHER ON GROUND. REPLACED PROPELLER ASSEMBLY.SDR GUU2002F00010Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GLBA2002071Warning System · malfunctionedRIGHT ENVIRONMENTAL FAIL ON T/O ROLL. RESET OVERPRESS LED ON BLEED AIR.SDR GUU2002F00014Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00015Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW BEECH MM.SDR GLBA2002070Altimeter · inoperativeCAPTAINS ALTIMETER FAILED ON T/O, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYSDR GUU2002F00013Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00012Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GLBA2002068Control Head · stripped#1 NAV SELECT BUTTON STRIPPED, REPLACED CONTROL HAEDSDR GUU2002F00011Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00009Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GLBA2002066Screw · loosePAX DOOR MAKING A POPPING SOUND WHEN PRESSURIZING. TIGHTENED CLOSET SCREWS, TEST FLIGHT SATISFACTORY.SDR GLBA2002065Hose · leakingLEFT FUEL LOW PRESSURE LIGHT ILLUMINATED, REPLACED HOSE ASSEMBLYSDR GLBA2002064Door · out of rigEMERGENCY EXIT HANDLE NEEDED CHECK. RIGGED DOOR, OPS CHECKED SATISFACTORY.SDR GLBA2002063Pressure Switch · failedLEFT ENVIRONMENTAL FAILURE ON T/O. REPLACED PRESSURE SWITCH.SDR GLBA2002062Latch · unsecureRIGHT ENGINE COWL LATCH OPENED ON T/O. RESECURED, OPS CHECKED SATISFACTORY.SDR 2002F00779Powerpack · malfunctionedAIRCRAFTS LEFT MAIN LANDING GEAR WOULD NOT RETRACT ON CLIMB-OUT. THE MAIN GEARS WAS THEN HAND PUMPED DOWN UNTIL THREE GREENS WERE INDICATED. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE FOR AIR MIDWEST REMOVED AND REPLACED THE HYDRAULIC POWER PACSDR CA020527011Socket · cracked(CAN) DURING INSPECTION OF MLG LOWER SOCKETS THEY WHERE FOUND TO BE CRACKED AS PER COMMUNIQUE NR 27 DATED FEB 1993. BLENDING IS ALLOWED UP TO .050 INCH BUT DUE TO LOW HOURS SINCE NEW THEY WHERE SENT TO AN OVERHAUL FACILITY FOR EVALUATION OF REPAIR OR REPLACE.SDR GUU2002F00008Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00007Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GLBA2002061Seal · tornCABIN DOOR SEAL LEAKING, REPLACED SEAL OPS CHECKED SATISFACTORYSDR GUU2002F00000Bolt · looseAT SCHEDULED ROUTINE INSPECTION VERTICAL SPAR SECURITY CHECK ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.SDR CA020605004Line · cracked(CAN) HEAVY FUEL LEAK OBSERVED ON LT ENGINE DURING GROUND RUN. AFTER INVESTIGATION, FOUND THAT THE PRESSURE LINE BETWEEN FCU AND FUEL FLOW DIVIDER WAS FOUND CRACKED AT THE B-NUT ON FCU SIDE. THE CRACK WAS PARALLEL TO THE WELDING OF THE B-NUT SEATING.SDR GLBA2002060Tube · damagedLEFT BLEED-AIR FAILURE. REPAIRED DAMAGED ENA TUBING AT WING, OPS GOOD.SDR GLBA2002059Switch · inoperativeLEFT ENGINE OIL PRESSURE ANNUNICATOR ILLUMINATED REPLACED PRESSURE SWITCHSDR GUU2002F00002Oil System · contaminatedAT SCHEDULED ROUTINE INSPECTION (LINE CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED OIL. CHANGE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH.SDR GLBA2002057Shutoff Valve · failedDUAL ENVIRONMENTAL FAILURE ON CLIMBOUT. REPLACED PRSOV VALVE.SDR CA020506003Socket · cracked(CAN) DURING A ROUTINE INSPECTION THE LT AXLE SOCKET ASSY WAS NOTED TO HAVE A SMALL CRACK IN THE AREA OF THE LOWER TORQUE KNEE LUGS. INVESTIGATION OF THE RT SOCKET ASSY REVEALED THE SAME CRACK IN THE SAME AREA.BOTH AXLE AND PISTON ASSY'S WERE REPLACED.SDR GUU2002F00005Power Unit · failedAT SCHEDULED ROUTINE INSPECTION THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED (BLACK OIL). REPLACE THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR.SDR GUU2002F00004Oil System · contaminatedAT SCHEDULED ROUTINE INSPECTION (A CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED "BLACK OIL". CHANGED THE ENGINE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH.SDR CA020506002Blower · seized(CAN) SMOKE SMELL IN CABIN & FLIGHT DECK AFTER LANDING.THIRTY MINUTE DELAY TO SWAP AIRCRAFT. INSPECTION REVEALED THAT THE FORWARD EVAPORATOR BLOWER HAD SEIZED, AND BLOWN THE CURRENT LIMITER, PROTECTING IT'S CIRCUIT. THE EVAPORATOR BLOWER ASSY WAS REPLACED ANSDR GLBA2002056A/C Pack · malfunctionedLEFT ENVIRONMENTAL FAILURE ON T/O. ENVIRONMENTAL SYSTEM OPS CHECK GOOD.SDR 2002F00630Pulley Bracket · looseAT SCHEDULED THIRD 200 HOUR INSPECTION, DISCOVERED THE AILERON LEFT DOWN CONTROL CABLE TO BE FRAYED. DETERMINED CABLE FRAYING CAUSED BY INCOMPLETE INSTALLATION OF PULLEY MOUNTING BRACKET. SECURED BRACKET , AND REPLACED PULLEY AND CABLE. (M)SDR S2YA02016Switch · sticksFLT 1454 - DAY-MKE - DURING TAKEOFF, THE RIGHT AUTO FEATHER DISABLE ANNUNCIATOR ILLUMINATED. THE CREW ABORTED THE TAKEOFF. THE A/C WAS FERRIED BACK TO MKE. MAINTENANCE REPLACED THE AUTO FEATHER SWITCHES IN THE POWER LEVER, OPS CHECK GOOD. (M)SDR GLBA2002067Rivet · shearedPILOT REPORTED THAT RUDDER PEDAL WAS VERY DIFFICULT TO ADJUST. INSPECTION FOUND THE TORQUE TUBE BEARING HOLDER OUTBOARD SIDE HAD ALL BUT ONE RIVET FASTENER SHEARED (3EA). REPLACED RIVETS AND RETURNED TO SERVICE.SDR 2002F00631Wire · looseFLT 9311 - SRQ-MIA - LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON NUMEROUS OCCASIONS. SECURED LOOSE WIRE AT LEFT FIRE BOTTLE. OPERATIONAL TEST NORMAL. (M)SDR 2002F00632Warning System · false activationFLT 9281 - RSW-TPA - LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON, FLICKERING NUMEROUS TIMES. INSPECTED SYSTEM. PERFORMED ENGINE RUN. NO DEFECTS NOTED. (M)SDR 2002F00633Fire Loop · faultyFLT 9428 - MCO-MIA - DURING FLIGHT, LEFT FIRE LOOP AMBER ANNUNCIATOR CAME ON. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP. OPERATIONAL TEST NORMAL. (M)
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