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 7C7A2015041502Structure · crackedCRACKED FOUND AT STRUCTURAL INSPECTION. DAMAGED AREA REPAIRED BY FR CO 104023R1. PARTS REPLACED AND DOUBLERS INSTALLEDSDR 7C7A201504150001Structure · chafedCHAFE DAMAGE AT LT FRAME FS 288-363.25 AND RT FRAME FS318.25 378.25 438.25 451.0. CHAFES ARE BLENDED AND POLISHED. NDT INSPECTED TO ENSURE NO CRACKS HAVE FORMED AND REPAIRS APPLIED BEECHCRAFT FIELD REPAIR FR CO 104024R2SDR CA150417012Fire Detector · defective(CAN) RT TEE HANDLE ILLUMINATED IN FLIGHT. FIRE EXTINGUISHER WAS ACTUATED. ENGINE SHUTDOWN. MAINTENANCE DISCOVERED THAT THE RT LOOP-DETECTOR AFT WAS DEFECTIVE. REPLACED LOOP-DETECTOR AND FIRE EXTINGUISHER AND RETURNED ACFT TO SERVICE.SDR CA150408025Erosion Shield · cracked(CAN) PROPELLER BLADES EROSION SHIELD CHORDWISE CRACK WITHIN SIX INCHES OF OTBD EDGE OF DE-ICER.SDR GLBA2015040300510Brake · frozenPILOT REPORTED THAT AFTER DE-ICING THE BRAKES FELT VERY INEFFECTIVE, VERY WEEK STOPPING ACTION, EVEN WHEN APPLIED FIRMLY. MX BRAKES FROZE UP, UNFROZE BRAKES BY APPLYING DE-ICE FLUID. OPERATIONS CHECKED GOOD IAW MM 32-40-00.SDR CA150401002Hose · cracked(CAN) CREW REPORTED THAT THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. ACFT RETURNED TO ORIGIN. AFTER ACFT WAS POSITIONED IN THE HANGER ON JACKS A GEAR SWING WAS CARRIED OUT. DURING THE GEAR SWING A LARGE AMOUNT OF FLUID WAS FOUND DRIPPING NEAR THE RT MSDR GLBA2015033000508Acm · wornPILOT REPORTED THAT THE PRESSURIZATION OPERATIONS CHECKED GOOD DURING RUN-UP, UPON CLIMB PRESSURIZED TO APPROX DIFF OF 3.0 & FAILED TO FURTHER PRESSURIZE. CABIN ALTITUDE HIGH ANNUNCIATOR ILLUMINATED, DEPLOYED OXYGEN MASKS, DECLARED AN EMERGENCY & RETURNED. SDR GLBA2015032500507Fan · malfunctionedPILOT REPORTED THAT THERE WAS LIGHT SMOKE COMING FROM THE FLOOR VENTS. REPLACED THE AFT VENT BLOWER IAW AIM 21-07. OPERATIONS CHECKED GOOD.SDR CA150324005Duct · cracked(CAN) CREW REPORTED A RT ENVIRO FAIL LIGHT. THE ENVIOR FAIL LIGHT SNAG WAS RECTIFIED, BUT DURING THE TROUBLESHOOTING OF THIS SNAG MAINTENANCE FOUND A DUCT ASSEMBLY CRACKED FROM THE FLANGE. ALSO, A HOLE WAS ALSO DISCOVERED IN THE EVA TUBING ADJACENT TO THE CRASDR GLBA2015032300506Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE LT FUSELAGE SKIN UNDER THE VORTEX GEN MOUNT AREA. FWD SKIN CRACK IS .9" IN LENGTH AT FS 238.25, STRINGER 12L, & AFT SKIN CRACK IS 1.0" IN LENGTH AT FS 248.25, STRINGER 12L, CRACK 1.9" IN TOTAL LENGTH. RESDR CA150323004Connector · corroded(CAN) LT FIREWALL FUEL SHUTOFF VALVE WOULD NOT TEST. MAINTENANCE FOUND PINS 7 AND 1 OF CONNECTOR J108, PN 206036-3, FOUND SEVERELY CORRODED. PINS WERE REPLACED WITH NEW. SYSTEM FUNCTION CHECKED SERVICEABLE. ACFT WAS RETURNED TO SERVICE. REF WDMD SECTION 91-SDR GLBA2015032000505Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME REPAIR & FRAME AT FS 163.975, STRINGER 10R, FRAME CRACK BEYOND STOP DRILL, .65" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-004. MAJOR REPAIR.SDR GLBA2015031900503Channel · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.SDR GLBA2015031900504Frame · crackedDURING A SCHEDULED INSPECTION, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS AT THE OTBD END OF THE FRAME, 1.25" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-003. MAJOR REPAIR.SDR 7C7A201503210020Switch · false indicationLEFT FIRE PULL TEE HANDLE (LEFT RED LIGHT) PULSED ON CLUMB OUT OF VDZ. DIMMED ON THEN OFF 3 TIMES.SDR CA150319002Pitot System · intermittent(CAN) ON DEPARTURE PASSING THROUGH 3000-4000 FT, THE CREW ENCOUNTERED YD. RUDDER BOOST FAILURE. THE DECISION WAS MADE TO ACTION THE CHECKLIST ONCE CLEARED ON COURSE. SHORTLY AFTER THIS, THE FLIGHT DIRECTOR FAILED. ONCE CLIMBING THROUGH 10,000, IT WAS NOTICEDSDR CA150317005Stringer · debonded(CAN) DURING STRUCTURAL INSPECTION MAINTENANCE DISCOVERED DISBONDING AT STR 13 BS 393-408. STRINGER REPAIRED IAW SRM.SDR CA150317004Stringer · debonded(CAN) DURING STRUCTURAL INSPECTION CHECK MAINTENANCE FOUND DISBONDING AT STR 14L BETWEEN BS 213-243. OEM WAS CONTACTED. SUBJECT AREAS WERE REPAIRED IAW OEM APPROVED REPAIR INSTRUCTIONS.SDR CA150311003Starter Gen · failed(CAN) LEFT DC GEN ANNUNCIATOR ILLUMINATED IN FLIGHT. ACFT DIVERTED TO MX BASE FOR EVALUATION. STARTER GEN FOUND TO BE UNSERVICEABLE, BEARING FAILURE. GEN SPLINES INSPECTED IAW MM 24-30-01 & MM 72-00-00 SECTION 12. NO EVIDENCE OF ELEC DISCHARGE DAMAGE EVIDESDR CA150310005Tube · chafed(CAN) CREW REPORTED PNEUMATIC PRESSURE LOW. DID NOT GET ABOVE 15PSI. MAINTENANCE FOUND LT BLEED LINE PN 129-970040-1, FEEDING REGULATOR CHAFED THROUGH/LEAKING DUE TO CORROSION FOUND ON AREAS OF THE LINE AND CLAMPS. SERVICEABLE LINE/CLAMPS INSTALLED & CHECKESDR GLBA2015030900501Bulkhead · buckledDURING A SCHEDULED INSPECTION, FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO 12L. REPAIRED THE BULKHEAD IAW EO 15-120-53-001. MAJOR REPAIR.SDR CA150301001Hose · cracked(CAN) AFTER LANDING CREW NOTICED HYD FLUID ON GROUND UNDER LT LANDING GEAR. A FERRY FLIGHT PERMIT WAS INITIATED TO BRING THE ACFT TO A MAINTENANCE BASE FOR INSPECTION. DURING INSPECTION MX FOUND A HOLE IN THE LT MAIN GEAR EXTEND LINE PN 101-388017-5, JUST AFSDR GLBA2015022700500Master Cylinder · wornPILOT REPORTED THAT THE LT BRAKE WAS INOPERATIVE FROM THE CAPTAIN SEAT, EXTREMELY SOFT FROM THE FIRST OFFICER SEAT. REPLACED O RINGS ON THE SWIVEL FITTINGS ON THE NR 1 BRAKE. REPLACED THE CAPTAINS LT MASTER CYLINDER IAW BMM 32-40-06. OPERATIONS CHECK & LEAKSDR CA150223001Support · cracked(CAN) CREW REPORTED A CABLE LET GO INSIDE THE AIR STAIR DOOR DURING DEPLANING OF PASSENGERS. MAINTENANCE FOUND THAT THE UPPER/LOWER HANDLE SUPPORT ASSEMBLY WAS CRACKED IN FOUR (4) PIECES.SDR CA150318003Gps · intermittent(CAN) APPROXIMATELY 6 MILES FINAL THE GPS FLAGGED. CREW CALLED FOR A GO-AROUND. IN THE GO-AROUND THE GPS CAME BACK ON LINE. THE CREW THEN RECEIVED VECTORS FOR NDB APPROACH AND LANDED WITHOUT INCIDENT. IT WAS THOUGHT TO BE A LOSS OF RAIM-RECEIVER AUTONOMOUS SDR CA150223002Transducer · reads high(CAN) RT ENGINE OIL PRESSURE DURING THE CLIMB READING 150-160 PSI. CREW REQUESTED RETURN TO ORIGIN. NO EMERGENCY DECLARED. THE CREW COMPLETED A NORMAL APPROACH AND LANDED WITHOUT INCIDENT. AFTER EVALUATION BY MAINTENANCE IT WAS DISCOVERED THAT THE OIL PRESSUSDR GLBA2015021700499Circuit Board · failedTHE HAND MIC SMELLED HOT & STARTED SENDING STATIC TO THE INTERCOM SYS. PLUGGED INTO INTO FIRST OFFICER`S JACK. REPLACED PC BOARD PN ON & OFF 130-340097-1 IN THE AUDIO CONTROL PANEL, SN OFF UNKNOWN, SN ON 504-8-95. WORK ACCOMPLISHED IAW AIM 10-24-01. REPLACSDR CA150213001Flap System · inoperative(CAN) DURING TAKE OFF REPORTED THAT THE FLAPS WOULD NOT RETRACT FROM 17 DEGREES TO ZERO DEGREES DURING AIRCRAFT CLEAN UP. THE FLAPS REMAINED AT 17 DEGREES. THE CREW REQUESTED RETURN TO ORIGIN. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT.SDR CA150211002Fastener · loose(CAN) DURING PHASE 6 DETAILED INSPECTION MAINTENANCE FOUND LOOSE FASTENERS, JO-BOLTS AT CENTER HINGE "A" FRAME OF THE RUDDER LOOSE. DURING RUDDER REMOVAL IT WAS FOUND THAT UPPER AND CENTER RUDDER ATTACHING 8 BOLTS WERE SHANKED OUT. IT IS SUSPECTED THAT THE VISDR CA150211003Circuit Board · faulty(CAN) THE CREW OF A BEECH 1900D ON APPROACH NOTICED THE LANDING GEAR LIGHTS, 3 GREEN, DID NOT ILLUMINATE. EMERGENCY SERVICES WERE REQUESTED & THE ACFT LANDED WITHOUT INCIDENT. ACFT WAS REMOVED FROM SERVICE & INSPECTED BY MAINTENANCE. ANNUNCIATOR CONTROL PCBSDR CA150207001Oil System · overheated(CAN) EXCESSIVELY HIGH OIL TEMP ON RT ENG DURING CRUISE. TROUBLESHOOTING CARRIED OUT. THE FOLLOWING COMPONENTS WERE REPLACED, THERMOSTATIC BYPASS VALVE, ENGINE OIL TEMP BULB & OIL COOLER. TEST FLIGHT WAS CARRIED OUT WITH SATISFACTORY RESULTS & THE ACFT WAS SDR CA150203006Pulley Bracket · cracked(CAN) BRACKET IS CRACKED IN HALF, FOUND ON A ROUTINE DOOR CABLE INSPECTION.SDR GLBA2015012800494Strut · malfunctionedPILOT REPORTED THAT THE CABIN DOOR SNUBBER WAS INOPERATIVE. SERVICED THE PAX DOOR STRUT IAW MM 12-10-00. OPERATIONS CHECKED GOOD.SDR 8EKA20150123001Diode · burnedBEFORE START UP THE NR 1 COM CONTROL HEAD SHORTED OUT & STARTED TO SMOKE. POWER WAS SHUTDOWN & WE BEGAN TO TROUBLESHOOT. AFTER LOOKING AT THE WIRING DIAGRAM & CHECKING THE POWER CIRCUIT AT THE NR 1 COM CONTROL CONNECTOR, FOUND THERE WAS NO SHORT TO GND. INSSDR V0DR20150122001Liner · brokenA MAIN WHEEL ASSY WAS RECIEVED WITH A WORN TIRE. DURING DISASSEMBLY OF THE WHEEL THE TECH FOUND 6 OUT OF 7 KEYWAY LINERS THAT HAD BROKEN TANGS. THE TECH R & R ALL 7 KEYWAYS. THE TECH VISUALLY INSPECTED THE INBD WHEEL HALF FOR ADDITIONAL DAMAGE FROM THE THE SDR CA150113021Wire · chafed(CAN) CREW REPORTED THAT THE CABIN DOOR INTERNAL LIGHT AND AIRSTAIR LIGHTS WERE UNSERVICEABLE. AFTER INSPECTION BY MAINTENANCE IT WAS DISCOVERED THAT A WIRE WAS FOUND CHAFED AND ARCING AGAINST THE INTERCOSTAL. THIS CAUSED FUSE F126 TO BLOW. THIS FUSE IS HOT FRSDR 7C7A201502020002Seat Track · crackedCRACK IN LT OB SEAT TRACK AT BS 427.25SDR GLBA2015011200491Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND THE UPPER INBD RT WING SKIN TE CHAFED & CORRODED WITH SEVERAL ELONGATED HOLES AT BL 36. CHAFE 8.5 INCHES LONG, 2 INCHES WIDE AT THE WIDEST PART & .020 INCHES DEEP BEFORE CORROSION REMOVAL. FOUND TO BE A MINOR REPAIR IAW SDR GLBA2015011100492Elbow · crackedWHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN PWR, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMCK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMS. SECURESDR GLBA2015011200492Unknown · malfunctionedWHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN POWER, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMER CHECK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMSSDR CA150113023Panel · unserviceable(CAN) AIRCRAFT WAS SNAGGED FOR LT ENG UNABLE TO START. AFTER INVESTIGATION FOUND FEEDER WIRES, BETWEEN STARTER & GENERATOR & DC POWER PANEL WAS ARCING AT THE STUD OF THE POWER PANEL. THE NUT HOLDING THE FEEDER WIRE DOWN WAS LOOSE BUT NOT LOOSE. RING TERMINASDR GLBA2015010800490Skin · damagedDURING A SCHEDULED INSPECTION FOUND A BURN HOLE IN THE RT ELEVATOR TOP OTBD SKIN TE 1.5 INCH WIDE BY .75 INCHES LONG IN AN EXISTING PATCH. HOLE IS 4.5 INCHES FROM OTBD TIP & .5 INCHES FROM THE TE. REPAIRED IAW EO 14-120-53-002.SDR CA150107001Cowling · missing(CAN) MISSING PIECE OF COWLING. CLEARANCE WAS ISSUED. NO EMERGENCY DECLARED AND FLIGHT LANDED. ONCE INSPECTED BY MAINTENANCE IT WAS CONFIRMED THAT LT UPPER AFT COWLING PN 114-980078-21 WAS MISSING. IT WAS DETERMINED THAT THE COWLING WAS ONLY PUT IN PLACE BY SDR GLBA2015010200489Master Cylinder · leakingTHE LT BRAKE PEDAL IS MUSHY & IT MUST BE FULLY DEPRESSED TO ACTIVATE THE BRAKES. FOUND EVIDENCE TO SUSPECT THAT THE CAPTAIN'S LT BRAKE MASTER CYLINDER, SN 4112, WAS BYPASSING INTERNALLY. THE CAPTAIN`S BRAKE MASTER CYLINDER WAS R & R IAW BMM 32-40-06. DURINGSDR GLBA2015010200488Snubber · low pressureTHE AIR STAIR DOOR OPENS REALLY FAST & FOUND THAT THE DOOR SNUBBER PRESS READ 500 PSI. SERVICED THE AIR STAIR DOOR SNUBBER AS NEEDED IAW MI 52-01. OPERATIONS CHECKED GOOD AT THIS TIME.SDR GLBA2014123000487Line · looseTHE CAPTAIN`S LEFT BRAKE PEDAL WENT TO THE FLOOR. FOUND THE BRAKE LINE LOOSE AT CLUSTER FITTING BETWEEN 1 & 2 BRAKE. TIGHTENED BRAKE LINE & BLED BRAKES IAW TC 1900-3240.02 STEPS 6 - 9. OPS CHECKED GOOD.SDR GLBA2014122400486Strut · low pressureTHE CABIN DOOR SNUBBER IS READING 200 PSI LOW & THE DOOR IS HARD TO CLOSE. SERVICED THE CABIN DOOR STRUT AS NEEDED IAW AIM 3 4 0 STEP 23. OPERATIONS CHECKED GOOD.SDR GLBA2014121700480Skin · wornDURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT BS 220 & STRINGER 15L HAS A .25 INCH HOLE WORN THROUGH THE SKIN. WORN AREA IS FWD & AFT APPROX 25 INCHES IN LENGTH & WIDTH IS APPROX .065 INCHES. REPAIRED IAW EO 14-1900-53-054SDR GLBA2014121900484Skin · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE CARGO BAY LT INNER SKIN AT BS 509.5 & STRINGER 11L, .9 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-059.SDR GLBA2014121700483Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 460 & STRINGER 3L, 2.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-058.
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