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 54885Indicator · fluctuatesDURING TAKE OFF RIGHT TORQUE WENT TO ZERO. TAKE OFF WAS ABORTED AND AIRCRAFT RETURNED TO MAINT. REMOVED AND REAPLCED GAUGE.P/N 114-3800-653 S/N 132.SDR GUU2004F00013Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT IB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT IB ELEVATOR HINGE BRACKET.SDR CA030928001Line · cracked(CAN) WHEN TRYING TO SERVICE OXYGEN SYSTEM ONLY THE LT BOTTLE WOULD FILL AND A LOUD LEAK COULD BE HEARD. AFTER INVESTIGATION BY MAINTENANCE THE FILLER INTERCONNECT LINE WAS FOUND TO BE CRACKED WHERE IT ATTACHES TO THE RT BOTTLE. THE LINE WAS REPLACED AND LEASDR 8483504Bolt · looseDURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE.SDR 54574Switch · out of adjustMASTER WARNING ILLUM WITH A CABIN DOOR ANNUNCIATOR. TAKEOFF WAS ABORTER AFT RETURNED TO GATE. ADJUSTED CABIN DOOR ANNUNCIATOR LIGHT SWITCH.SDR AMWA58Engine · fireFIRE STARTED IN LEFT ENGINE. FIRE WAS EXTINGUISHED BY MOTORING OF ENGINE.SDR CA030929003Pump · leaking(CAN) SIMILIAR TO A PREVIOUS SDR ON THE RT SIDE ON SEPT 18, 2003, THE LT HAND LOW PRESSURE FUEL PUMP BEGAN LEAKING IN FLIGHT ALLOWING ODOR AND FUEL ESCAPE FROMTHE AIRCRAFT. MAINTENANCE AGAIN REPLACED THE PUMP AND THE STRIP SHOWED THE SAME GASKET BLOW OUT ALLOWSDR GLBA2003135Governor · malfunctionedRT PROP STARTS TO FEATHER WHEN POWER LEVER IS BROUGHT BACK, REMOVED AND REPLACED PROP GOV.SDR AMWA55Rib · crackedFOUND TWO CRACKS ON RIB P/N 101-640000-59 AT THE RIVETS BESIDE THE STRINGERS INTERSECTIONS. THE STRINGER THAT INTERSECT THE RIB ARE P/N 101-640000-39 AND 101-640000-46. BOTH CRACKS WERE REAIRED IAW THE MFG STRUCTURAL REPAIR MANUAL.SDR CA030929002Pump · leaking(CAN) CREW NOTICED A FUEL ODOR IN AIRCRAFT AT ALTITUDE AND A PASSENGER NOTIFIED THAT FLUID APPEARED TO BE COMING FROM COWL AREA THAT NORMALLY PROVIDES EXHAUST AIR FROM THE STARTER GENERATOR. THE AIRCRAFT DIVERTED TO THE CLOSEST AIRPORT. MAINTENANCE FOUND THE RSDR GLBA2003134Wire · brokenGEAR WILL NOT GO UP WHEN SELECTED. REPAIRED BROKEN WIRE BY POWER PACK.SDR 54446AMWABrake · malfunctionedAFTER LANDING IN PNC, CAPT'S BRAKES WHERE SPONGING ON LANDING BRAKES WHERE WRITTEN UP MAINT WAS CALLED A/C WAS FERRIED TO LIT FOR REPAIR. BLEED BRAKES. NO TEARDOWN REPORT WILL BE REQUIRED.SDR GLBA2003133Transmitter · malfunctionedNR 1 ENG WILL NOT MAKE TAKE OFF POWER, R&R NR 1 TORQUE TRANSMITTERSDR GLBA2003132Indicator · failedNR 1 TORQUE GAUGE QUIT AFTER TAKEOFF, REMOVED AND REPLACED TORQUE INDICATOR.SDR 2003FA0000934Guide · brokenWHILE CHECKING ELEVATOR TRIM WE FOUND INTERMITENT BINDING OF ELEVATOR TRIM WHEN MANUALLY OPERATING TO NOSE DOWN DIRECTION. BINDING WAS OF SUCH THAT IT WOULD MOMENTARILY HANG BEFORE RELEASING. IT OCCURED AT PRETY MUCH THE SAME POSITION EACH TIME, (WHEN MOVING FSDR 54388AMWAReservoir · malfunctionedLANDING GEAR FAILED TO EXT & MANUAL EXTENDED (MSS). REMOVED AND REPLACED HYD RESERVOIR & POWER PACK ASSY TEST NORM.SDR GLBA2003131Flap · inoperativeFLAPS WOULD NOT RETRACT AFTER T/O, ADJUSTED LT SPLIT FLAP SWITCH OPS CK GOOD.SDR AMWA54255Propeller · unknownMAINTENANCE RECEIVED A CALL FROM CREW STATING PROP WOULD NOT GO INTO GROUND DURING FLIGHT. MAINTENANCE INSPECTED IT AND COULD NOT DUPLICATE THE PROBLEM ON GROUND. AIRCRAFT WAS FERRIED TO DUBOIS, PENNSYLVANIA AND WAS INSPECTED BY MAINTENANCE THERE AWAITING FOSDR AMWA57Rib · crackedFIVE CRACKS FOUND IN THE RIB IN JOGGLED PARTS OF RIB AT STRING INTERSECTIONS. STRING P/N 101-640000-46, 101-640000-39, 101-640000-45, 101-640000-38. CRACKS RUN HORIZONTAL TO RIB FROM LAST RIVET HOLE TO EDGE OF RIB.SDR AMWA56Rib · cracked2 CRACKS FOUND IN THE RIB. IN JOGGLED SECTION OVER STRNG AT LAST RIVET. CRACKS LOCATED AT STRNG P/N 101-640000-37 AND 10-640000-46.SDR GLBA2003130Turbine · failedRT ENGINE POWER TURBINE FAILED AT 1000 LBS TORQUE. REMOVED AND REPLACED RT ENGINE ASSY.SDR 2004F00216Turbine Blades · failedDURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. POWER SECTION HAS SDR 2004F00030Turbine Blades · damagedFLT 9240 - FLL - DURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. PSDR 54215Bulb · inoperativeUPON INITIATING GEAR DOWN CREW NOTICED THAT THE NOSE GEAR ANNUNCIATOR DIDN'T ILLUM. CREW PERFORMED AND NOTIFIED TOWER MANUAL GEAR EXT PROCEDURE WAS INITIATED AFTER COMPLETION OF CHECK LIST. IT WAS NOTED GEAR DOWN ANNUNCIATOR STILL DIDN'T ILLUM. SPARE BULB WAS SDR AMWA46Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46 (1EA CRACK ON THIS RIB)SDR AMWA45Rib · crackedRIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-37 AND STRG P/N 101-640000-39 (2EA CRACKS ON THIS RIB).SDR AMWA41Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-37 LT SIDE (1EA CRACK ON THIS RIB)SDR AMWA40Rib · crackedRIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-46 ON RT SIDE STRG P/N 101-640000-41 STRG P/N 101-640000-37 LT SIDE (4EA CRACK ON THIS RIB).SDR AMWA39Rib · crackedRIB 69.184 CS CRACKED AT STRG P/N 101-640000-45 (1EA CRACK ON THIS RIB) LT SIDE.SDR AMWA38Rib · crackedRIB AT CS 24.973 CRACKED AT STRG P/N 101-640000-39 LT SIDE (1EA CRACK ON THIS RIB).SDR AMWA37Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-45 STRG P/N 101-640000-39 (2EA CRACKS ON THIS RIB)SDR AMWA36Rib · crackedRIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 STRG P/N 101-640000-46 LT SIDE (3EA CRACKS ON THIS RIB)SDR AMWA35Rib · crackedRIB AT CSS 39.289 AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 ON RH SIDE AND STRG P/N 101-640000-39 STRG P/N 101-640000-37 (4EA CRACKS ON THIS RIB)SDR AMWA34Rib · crackedRIB AT CSS 54.026 CRACKED AT STRG. 101-640000-47 STRG. P/N 101-640000-42 RT SIDE AND STRG 101-640000-43 STRG P/N 101-640000-39 STRG P/N 10164000041 5 EA CRACKS ON THIS RIB)SDR AMWA33Rib · crackedRIB CRACKED AT CSS 69.184 AT STRG P/N 101-640000-46 RT AND STRG P/N 101-640000-45 LT SIDE (2EA CRACK AT THIS RIB).SDR AMWA32Rib · crackedRIB AT CS 54.026 CRACKED AT STRG. P/N 101-640000-46 STRG P/N 101-640000-47 ON RT SIDE AND STRG P/N 101-640000-39 LT SIDE (3EA CRACKS ON THIS RIB).SDR AMWA31Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-39, 1EA CRACK AT THIS RIB.SDR AMWA48Rib · cracked6 CRACKS FOUND ON THIS RIB LOCATED AT END RIVET OF RIB AREA THAT IS JOGGLED OVER STRG. STRG INTERSECTION LH P/N 101-640000-37, LT 101-640000-39, LH P/N101-640000-45 THEN RH P/N 101-640000-38, RH P/N 101-640000-46, RH P/N 101-640000-42.SDR AMWA47Rib · cracked2 CRACKS FOUND ON RIB NR 1 ON LT SIDE AT STRINGER INTERSECTION STRINGER P/N 101-64000-37 AND 1 ON RH SIDE AT STRG P/N 101-640000-46. CRACKS LOCATED AT THE END RIVET ON JOGGLE OVER STRINGER BOTH LOCATIONSSDR AMWA54Rib · crackedWHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE LT SIDE AT THE CENTER STRG,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03SDR AMWA53Rib · crackedWHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RT SIDE AT THE FWD SIDE,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03SDR AMWA52Rib · crackedWHILE PERFORMING INSP IN THE VERT. STAB., THE RIB FLNAGE AT CANTED STAB. STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RT SIDE NEAR THE FWD, CENTER, AND AFT STRG. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03SDR AMWA51Rib · crackedWHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLANGE AT CANTED STAB. STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE LT SIDE AT THE AFT STRG INTERSECTION AND ONE PLACE ON THE RT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021SDR AMWA50Rib · crackedWHILE PERFORMING AN INSP IN THE VERT. STAB., THE RIB FLANGE AT CANTED STAB. STA 54.026 WAS FOUND CRACKED IN 3 PLACES ON THE RT SIDE NEAR THE FWD, CENTER AND AFT STRG AND 2 PLACES ON THE LT. REPAIRED CRACKS TO THE RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-5SDR AMWA49Angle · crackedDURING AN ABCD STRUCTURAL INSPECTION, THE RT FUSELAGE CLOSING ANGLE WAS FOUND CRACKED 2.4 INCHES. THE CRACK WAS REPAIRED IN ACCORDANCE TO THE BEECH SRM 53-90-23 AND RAYTHEON AIRCRAFT COMPANY FIELD REPAIR FR-CO-00934SDR AMWA44Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46, STRG 101-640000-42 ON RT SIDE AND STRG P/N 101-640000-41, STRG P/N 101-640000-37 (4EA CRACKS TOTAL ON THIS RIB)SDR AMWA43Rib · crackedRIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 STRG P/N 101-640000-42 BOTH RT SIDE AND STRG P/N 101-640000-37 STRG P/N 101-640000-45 ON LT SIDE (4 EA TOTAL CRACKS ON THIS RIB)SDR AMWA42Rib · crackedRIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER.SDR 255032Handle · out of positionEMERGENCY EXIT DOOR OVER SEAT 6A OUTSIDE HANDLE NOT FLUSH WITH DOOR SKIN. OUTSIDE HANDLE IS RECESSED INTO DOOR WHEN CLOSED. REMOVED DOOR FROM OUTSIDE AND REINSTALLED DOOR. IAW MM 52-20-00 HANDLE IS FLUSH.SDR GLBA2003127Tach Generator · malfunctionedNR 1 PROP RPM 1450 IDLE AT 600, TIGHTENED NR 1 N2 TACH GEN.
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