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 GUU2005F00021Reservoir · lowLT BRAKE INOPERATIVE. FOUND BRAKE RESERVOIR LOW. SERVICED RESERVOIR. BLED LT BRAKE ASSEMBLY. (K)SDR CA050607002Control Valve · failed(CAN) AC LANDED AT INTENDED AIRSTRIP. PARKING BRAKE WAS SET AND ENGINES SHUTDOWN. WHEN AC WENT TO DEPART THE PARKING BRAKE WAS RELEASED BUT THE BRAKES STAYED ON. IT WAS FOUND THAT THE BRAKE CONTROL VALVE FAILED INTERNALLY, THE PLUNGER ACUTATOR SHAFT SHEAREDSDR 71141Spring · brokenCREW REPORTED DURING INTERMEDIATE CLIMB, IT TOOK FULL RIGHT AILERON TRIM TO KEEP THE AIRCRAFT WINGS LEVEL. CREW NOTED NO CONTROLLABILITY PROBLEMS. CRUISE TRIM SETTING APPEARED MORE NORMAL AT 3 RIGHT. AIRCRAFT REQUIRED NO AILERON RETRIMMING DURING DESCENT. SDR CA050607003Windshield · cracked(CAN) DURING CRUISE FLIGHT ,THE RT WINDSHIELD CRACKED. THE FLIGHT WAS COMPLETED AND THE OUTER PLY WAS FOUND TO BE CRACKED. THE DEFECT WAS WITHIN LIMITS SET OUT IN AFM, MM AND GMEL. IT WAS DEFERRED IAW GMEL AND SUBSEQUENT FLIGHTS COMPLETED IAW RESTRICTIONS UNTISDR CA050607004Windshield · cracked(CAN) DURING CRUISE FLIGHT ,THE RT WINDSHIELD CRACKED. THE FLIGHT WAS CONTINUED AND UPON LANDING THE OUTER PLY WAS FOUND CRACKED. THE DEFECT WAS FOUND TO BE WITHIN AIRWORTHINESS LIMITS FOR CONTINUED FLIGHT UNDER GMEL RESTRICTIONS. THE WINDSHIELD HAD BEEN INSTASDR 71138Diode · faultyEMERGENCY COCKPIT LIGHTING ON, OFF HOT BATTERY BUSS, MAIN BATTERY SWITCH OFF AND SWITCH FOR FLIGHT INSTRUMENT INDIRECT LIGHTS ON. ELECTRICAL ODOR IN COCKPIT AREA. MAINTENANCE REMOVED AND REPLACED DIODE.SDR S2YA05036Uplock Switch · out of adjustON CLIMBOUT OF FLIGHT, THE CREW REPORT THE LANDING GEAR HANDLE LIGHT WAS FLICKERING WITH THE HANDLE IN THE UP POSITION. THE CREW PERFORMED AN AIR-TURN-BACK TO DEPARTURE AIRPORT. MECHANIC ADJUSTED THE LT MAIN UPLOCK SWITCH AND RETURNED THE AC TO SERVICE. (K)SDR 71124Rheostat · burnedCREW CALLED IN AND REPORTED THAT WITH COCKPIT EMERGENCY LIGHTS ON, BATTERY OFF, INDIRECT LIGHTING ON, THERE WAS AN ELECTRICAL BURNING ODOR. MAINTENANCE REMOVED AND REPLACED INDIRECT LIGHT RHEOSTAT SWITCH.SDR CA050802001Truss · cracked(CAN) MULTIPLE CRACKS WERE FOUND EMITTING FROM TOOLING HOLES AND RIVETS IN BRACKETS A (220-050) AND B (220-051), IAW DRAWING NR 129-910047-13.SDR GUU2005F00020Brake · failedCAPTAIN`S SIDE LT BRAKE PEDAL WOULD NOT BRAKE. SERVICED BRAKE SYSTEM. NO LEAK NOTED. (K)SDR AMWA71073Indicator · failedUPON TAXI OFF ROLL, CREW OBSERVED LEFT PROP RPM INDICATOR STUCK AT 1300 RPM. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PROP TACH INDICATOR.SDR CA050531005Vertical Gyro · failed(CAN) ON ROLLOUT FOR TAKEOFF AT APPROX 60 KNTS THE CAPTAINS ATTITUDE INDICATOR FLAGGED OFF AND WENT BLANK. THE T/O WAS REJECTED AND THE AIRCRAFT RETURNED TO THE GATE. DURING THE TAXI THE UNIT CAME BACK ONLINE. THE CREW CONTACTED MAINTENANCE AND AS THE UNIT WASSDR GUU2005F00019Brake · unresponsiveLT TOE BRAKE DOES NOT WORK. HAVE TO PUMP UP PRESSURE. BLED LT BRAKE SYSTEM. OPS CHECK NORMAL. (K)SDR 71037Brake · malfunctionedON TAXI TO GATE BRAKES WERE SPONGY. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THEREFORE NO PARTS WERE USED.SDR 71033Strut Wiper · looseON A WALK AROUND (PREFLIGHT) THE CREW DISCOVERED THE STRUT WIPER WAS LOOSE. MAINTENANCE REMOVED AND REPLACED THE RT MAIN LANDING GEAR ASSEMBLY.SDR CA050705004Bearing · fractured(CAN) ENGINE ORIGINALLY OVERHAULED IN 2002, FIRST RUN. AT THAT TIME, A PROCESS TO CLEAN OIL JET NOZZLE 3 AND 4 WAS UTILIZED AS PER OEM MANUAL. OTHER OPERATORS HAD EXPERIENCED DIFFICULTY WITH THE 3/4 OIL NOZZLE AND IT WAS FOUND THAT PROPER AND THOROUGH CLEANINGSDR 20030850Powerpack · malfunctionedUPON APPROACH WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT EXTEND. FLIGHT CREW USED THE MANUAL GEAR DOWN HAND PUMP TO EXTEND GEAR SUCCESSFULLY AND LANDED. MAINTENANCE DISCOVERED HYDRAULIC POWER PACK CIRCUIT BREAKER WAS TRIPPED. RESET CIRCUIT BREAKER AND SDR CA050621003Engine · failed(CAN) DURING CRUISE SMOKE BECAME EVIDENT IN THE CABIN ACCOMPANIED BY HIGH ENGINE OIL TEMPERATURE AND LOW OIL PRESSURE INDICATIONS. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION FOUND OIL LEAKING FROM THE ENGINE INLET AREA. MFG WILL MONITOR THE ISDR 70891Connector · dirtyRT PROP WILL ONLY MAKE 1550 UNDER POWER. MAINTENANCE CLEANED OVERSPEED GOVERNOR CONNECTOR PLUG. THEREFORE NO PARTS WERE USED.SDR CA050518007Wire · chafed(CAN) DURING APPROACH, THE LANDING GEAR REPORTED AS (FAILED TO OPERATE RELIABLY) REQUIRING MULITIPLE EXTENSION ATTEMPTS. TROUBLESHOOTING FOUND CHAFED WIRED AT THE HYD PACK PRESSURE SWITCH THAT WERE REPAIRED.SDR 20030846Spar · crackedDURING ROUTINE INSPECTION, FOUR CRACKS APPROX .5 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH COMPANY EO. AIRCRAFT RETURNED TO SERVICE.SDR CA050518006Fire Loop · will not test(CAN) DURING START, CREW WAS RUNNING PREFLIGHT CHECKS AND FOUND LT FIRE LOOP WOULD NOT TEST. MAINTENANCE FOUND THE FWD FIREWALL CONNECTION WAS POOR AND WAS CORRECTED.SDR CA050517009Pcb · intermittent(CAN) ALL 3 GREEN GEAR INDICATIONS BLANKED OUT DURING FINAL APPROACH. AFTER CYCLING GEAR , LIGHTS RETURNED. PROBLEM FOUND WITH A125 PCB WHICH PROVIDES A COMMON GROUND FOR ALL 3 LIGHTS.SDR S2YA05032Engine · lowDURING FLIGHT, CREW REPORT THE RT OIL PRESSURE WAS FLUCTUATING BETWEEN 70 AND 80 PSI AND OCCASIONALY DROPPING TO 50 TO 60 PSI AND THEY WERE GETTING A RED WARNING LIGHT. THE CREW PERFORMED AN AIR-TURN-BACK. OUTSTATION MECHANIC INSPECTED ENGINE CHEC THE CHIP DSDR 70786Annunciator · inoperativeNLG WILL NOT INDICATE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THE PROBLEM IS IN THE ANNUNCIATOR ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE ANNUNCIATOR.SDR 20030842Fire Loop · false indicationDURING THE TAKEOFF ROLL, THE RT RED T-HANDLE ANNUNCIATOR AND YELLOW FIRE LOOP ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED THE DEFECTIVE REAR (AFT) FIRE LOOP. AIRCRAFT RETURNED TO SERVICE.SDR CA050503005Switch · failed(CAN) ACFT DEPARTED TERRACE AND WHEN GEAR WAS SELECTED UP IT DID NOT OPERATE. IT WAS CYCLED ONCE MORE WITH NO EFFECT. THE GEAR INDICATION SHOWED DOWN AND LOCKED SO THE CREW ELECTED TO LAND WHERE MAINTENANCE MAINTENANCE WAS AVAILABLE. LANDED UNEVENTFULLY AND SDR CA050503012Bolt · shearedAFTER T/O & GEAR UP SELECTED, CREW HEARD A LOUD THUD IN NOSE AREA. GEAR IND SHOWED AN UNSAFE CONDITION, GEAR SELECTED DOWN & 3 GREENS WERE OBTAINED FOR DOWN & LOCKED. DURING FLYBY, OBSERVED NLG TO BE PERPENDICULAR TO STRAIGHT. DECIDED TO FLY TO MAIN BASE. SDR CA050429003Duct · crackedTHE CREW HAD A BLEED AIR FAIL INDICATION IN FLIGHT, FOLLOWED PROCEDURES AND SHUT THE LT BLEED AIR VALVE OFF AND CONTINUED FLIGHT. UPON INSPECTION AT A MX BASE ,IT WAS FOUND THAT THE EVA TUBING IN THE AREA OF THE DUCT HAD MELTED. THE EVA TUBING WAS REPLACED ASDR 20030837Spar · crackedDURING ROUTINE INSPECTION, FOUR CRACKS APPROX .65 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH EO, AIRCRAFT RETURNED TO SERVICE.SDR GUUA94253042305ASkin · tornDURING SCHEDULED ROUTINE MX DISCOVERED SKIN TEAR AT FS 475.5 RUNNING FROM THE SKIN EDGE AT THE AFT CARGO DOOR LOWER DOOR SILL EXTENDING DOWN 2.5 INCHES. STOP DRILLED TEAR AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR 20030834Annunciator · false activationCARGO DOOR ANNUCIATOR ILLUMINATED IN FLT, CREW EXECUTED EMEGENCY CHECKLIST, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SYSTEM CHECKS AND COULD NOT DUPLICATE DISCREPENCY. AIRCRAFT RETURNED TO SERVICE.SDR CA050421004Yoke · cracked(CAN) DURING STRUCTURAL INSPECTIONS, THE AILERON YOKE INSPECTION REPEATING AT 3000 HOURS WAS ACCOMPLISHED AND IT WAS FOUND THAT BOTH THE LEFT AND RIGHT AILERON YOKE ASSEMBLIES WERE CRACKED. THE CRACKS EXTEND FROM THE BORE FOR SPIGOT INSERTION THROUGH THE OUTESDR CA050503001Spar · crackedRUDDER TORQUE TUBE P/N 101-630010-9 LOWER ATTACH BOLTS (3) FOUND LOOSE, HOLES IN TORQUE TUBE ELONGATED. RUDDER CONTROL HORN P/N 101-524059-1 DAMAGED AT CENTER ATTACH HOLE DUE BENT ATTACH BOLT, BEARING P/N MS28913-5C DAMAGED FROM BOLT. ALL ABOVE PARTS REPLACESDR 20030831B-Nut · leakingAFTER DEPARTURE, ON CLIMB-OUT FLT CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATIONS, FOLLOWED BY LOW LEFT OIL PRESSURE GAUGE INDICATION. SHORTLY AFTER LEFT OIL PRESSURE LOW ANNUNCIATION. FLT CREW DECLARED EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. MASDR 20030830Wire · chafedDURING CLIMB, FLT CREW REPORTED AFX DISABLE AND LEFT AND RIGHT AUTOFEATHER ANNUNCIATORS ILLUMINATED. FLT CREW RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRES AT LT MLG UPLOCK SWITCH. OP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2005F00081Brake Assy · malfunctionedRT BRAKE VERY SOFT. REQUIRED EXCESSIVE PUMPING TO CREATE PRESSURE AND INCREASE BRAKE EFFECTIVENESS. BLED LEFT AND RIGHT BRAKES. OPERATIONAL CHECK NORMAL. (M)SDR CA050527020Csd · malfunctionedDURING DESCENT, THE ENGINE EXPERIENCED SURGING AND THE PILOT ELECTED TO SHUT THE ENGINE DOWN IN FLIGHT. THE CONSTANT SPEED UNIT AND FUEL CONTROL UNIT WERE SUBSEQUENTLY REPLACED.SDR 70332Switch · out of adjustIN CRUISE, CARGO DOOR ANNUNCIATOR ILLUMINATED. RAN APPROPRIATE EMERGENCY CHECKLIST. DECLARED EMERGENCY WITH PHX/ABQ CENTER. LANDED AT PHX WITH NO INJURY TO AIRCRAFT OR PASSENGERS. SYSTEM MEL'D. MAINTENANCE ADJUSTED CARGO DOOR JAM SWITCH.SDR GUU2005F00009Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. (K)SDR S2YA05026Gyro · malfunctionedAFTER TAKEOFF, THE CREW REPORTD THE FO EHSI AND THE CA RMI FROZEN AT 320 DEGREE HEADING. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE AC BUT COULD NOT DUPLICATE THE PROBLEM. MECHANIC REPLACED THE NR 2 DIRECTIONAL GYRO FOR TROUBLESHOOTING AND SDR 20030826Skin · corrodedDURING ROUTINE INSPECTION, UNDER BELLY SKIN CORROSION WAS IDENTIFIED AT FS 225.5 TO FS 230.95 APPROX. 5.5 INCH BY 19.5 INCH. CORRODED SKIN WAS REPLACED AND REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE.SDR 2005F00076Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M)SDR CA050411002Flex Drive · failed(CAN) ON APPROACH FLAPS WERE SELECTED TO 17 DEG, FLAPS STARTED TO MOVE THEN STOPPED, AIRCRAFT LANDED SAFELY. INSPECTION OF THE FLAP SYSTEM SHOWED THAT THE RT FLAPS WERE IN A SPLIT FLAP CONDITION BETWEEN 0 DEG AND 17 DEG. FURTHER INVESTIGATION REVEALED THE RTSDR 20030814Rod End · brokenON TAKEOFF, AS SOON AS THE NOSEWHEEL LEFT THE GROUND THE CAPTAIN SIDE RUDDER PEDALS LOST EFFECTIVENESS. FO'S CONTROLS WERE WORKING NORMALLY AND CONTROL WAS TRANSFERRED AND AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERED RUDDER PEDAL INTERCONNECT RODEND WAS BRSDR 20030815Rod End · brokenDURING NON-ROUTINE INSPECTION, MAINTENANCE DISCOVERED LT RUDDER PEDAL INTERCONNECT ROD END WAS BROKEN AT RUDDER BELLCRANK. RODEND REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR 70122Brake · dirtyAFTER ARRIVING AT GATE IN DFW, CREW REPORTED LEFT BRAKE WEAK. MAINTENANCE CLEANED THE BRAKES. THEREFORE NO PARTS WERE USED.SDR 20030828Frame · crackedDURING ROUTINE INSPECTION, A .55 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 498.25 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE.SDR 20030827Frame · crackedDURING ROUTINE INSPECTION, A .63 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 482.75 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE.SDR 70056Annunciator · defectiveON APPROACH FOR LANDING IN ART WITH GEAR EXTENDED CREW NOTED NOSE GEAR DIDN'T INDICATE DOWN AND LOCKED. THEN PERFORMED EMERGENCY CHECKLIST AND PUMPED GEAR DOWN BY HAND. STILL NOSE DIDN'T INDICATE DOWN AND LOCKED. CREW DID FLYBY OF FIELD AND WERE REPORTED NO
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