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 = '340B' 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 = '340B' 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 SIMA200126005Indicator · malfunctionedCAPTAINS ALTITUDE INDICATOR HAD A RED FLAG ON TAKEOFF ROLL. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED OPS CHECK IAW SAAB AMM ON THE ADC OPS CHECK GOOD. (M)SDR SIMA200126004Gauge · faultyDFW - FLT 3685 - LEFT ENGINE TORQUE WENT TO ZERO ON TAKEOFF. LEFT TORQUE CIRCUIT BREAKER POPPED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT TORQUE GAUGE. OPS CHECK GOOD. (M)SDR SIMA200125901Switch · inoperativeLAX - FLT 3268 - AFTER LANDING GEAR WAS SELECTED DOWN THE LEFT DOWNLOCK LIGHT DID NOT ILLUMINATE. CREW DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED THE LEFT DOWNLOCK SWITCH IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVSDR PNSA010902Connector · dirtyON CLIMBOUT FROM ANC RT ENGINE ITT GAUGE STARTED FLUCTUATING NO OTHER UNUSUAL INDICATIONS. MAINTENANCE CONTACTED ON RADIO AND AIRCRAFT RETURNED TO ANC. MAINTENANCE CLEANED ITT YELLOW HARNESS CANNON PLUG AT ENGINE AND GROUND RUN AIRCRAFT OK.SDR MALA010720Seat Track · corrodedDuring 4K-check in CWA, found LH Center Aisle seat LBL 18.3 corroded. Mx Performed Repair from Sta 297 to 349 IAW EO S53060. Seat Track PN 7253799-383, Slice joint PN 7253799-379.SDR MALA010719Angle · corrodedDuring 4K-Inspcection found frome Top Flange and Angle corroded on bottom Frame at Sta 258. Maintenance replaced corroded Angle PN 7253722-001 and performed repair to Top Flange IAW EO S53102.SDR MALA010698Indicator · erraticDURING FLIGHT 2933, LT PROP RPM INDICATION ERRATIC. INDICATION VARIES FROM ACTUAL RPM AND ZERO INTERMITTENTLY. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT PROP INDICATOR P/N 522742, S/N ON 0387128, S/N OFF 9802872 IAW AMM 61-40-05-2. OPS CHECKSDR MALA010718Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT O/B ELEVATOR FWD FUSELAGE CABLE P/N 7227105-712.SDR MALA010717Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT I/B FWD ELEVATOR CABLE P/N 7227705-644 IAW SF340 AMM 27-31-15.SDR MALA010716Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B AILERON FWD FUSELAGE CABLE CHAFED. MX REPLACED LT O/B AILERON FUSELAGE CABLE P/N 7227105-623 IAW SF340 AMM 27-11-25-4.SDR MALA010715Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B FWD AILERON FUSELAGE CABLE IS CHAFED. MX REMOVED AND REPLACED LT I/B AILERON CABLE, P/N 7227105-623 IAW SF 340 AMM 27-11-15-4.SDR MALA010714Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED LT O/B RUDDER CABLE P/N 7227105-562 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4.SDR MALA010713Control Cable · chafedDURING 4K-CHECK IN CWA, LT RUDDER AFT SINGLE CABLE OF DUAL CIRCUIT I IS CHAFFED. MX REPLACED LT RUDDER AFT SINGLE CABLE CIRCUIT I P/N 7227105-582 IAW SF340 AMM 27-21-25-4.SDR MALA010712Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT I/B RUDDER CABLE P/N 7227105-571 IAW SF340 AMM 27-21-25-4.SDR MALA010711Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT O/B RUDDER CABLE P/N 7227105-562 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4.SDR MALA010710Control Cable · chafedDURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MX REPLACED RT RUDDER SINGLE CABLE P/N 7227105-582 OF CIRCUIT I IAW SF340 AMM 27-21-25-4.SDR MALA010709Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B AILERON FUSELAGE CABLE IS CHAFED. MX REPLACED RT I/B AILERON FWD FUSELAGE CABLE WITH NEW CABLE P/N 7227105-614 IAW SF340 AMM 27-11-25-4.SDR MALA010708Control Cable · chafedDURING 4-K CHECK IN CWA, RT O/B FWD AILERON FUSELAGE CABLE IS CHAFED. MX REPLACED RT O/B FWD FUSELAGE AILERON CABLE P/N 7227105-624.SDR MALA010707Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B FWD ELEVATOR FUSELAGE CABLE IS CHAFED. MX REPLACED RT I/B FWD FUSELAGE CABLE IAW SF340 AMM 27-31-15-4. P/N 7227705-644.SDR MALA010706Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED RT O/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712.SDR SIMA200125301Skin · crackedABI - DURING MBV INSPECTION, FOUND OUTER SKIN OF RIGHT ENGINE NACELLE CRACKED ON OUTBOARD SIDE. REPAIRED NACELLE SKIN IAW SAAB 340 SRM AND REPAIR STATEMENT SDS002401. (M)SDR MALA010681Indicator · faultyON CLIMBOUT NOTICED RT PROP OIL TEMP IN YELLOW ARC (>77 DEGREE, MAX LIMIT) AT 40 PERCENT TG IT WAS RIGHT AT THE MAX LIMIT OF 77 DEGREES. EVEN AT GROUND IDLE IT WAS AT MAX LIMIT. MAINTENANCE REMOVED AND REPLACED RT OIL PRESS/TEMP GAUGE WITH SERVICEABLE UNIT PSDR MALA010679Motor · failedAFTER DEPLANING FLIGHT 3180 GROUND OPS HOOKED UP EXTERNAL POWER. SHORTLY AFTER, VISIBLE SMOKE WAS SMELLED IN CABIN. MAINTENANCE VISUALLY INSPECTED CABIN AREA, FOUND SIDEWALL LIGHTS AT ROW 1-5 AND OVERHEAD LIGHTS AT ROWS 9A AND 10, SUSPECT BAD LIGHT SOCKET AND/SDR SIMA200125001Circuit Board · defectiveLAX - FLT 3202 - DURING CRUISE, FLIGHT ATTENDANT REPORTED ODOR OF BURNED ELECTRICAL INSULATION FROM GALLEY AREA BY COFFEE JUG. CIRCUIT BOARD IN PSU AT SEAT 3A FOUND DEFECTIVE. REMOVED AND REPLACED SEAT 3A PSU IAW SAAB 340 AMM. NO FURTHER BURNED ODORS NOTED. SDR SIMA200124903Light · malfunctionedSAN - FLT 3360 - EMERGENCY FLOOR PROXIMITY LIGHTING AT SEATS 6, 7, AND 8 EXTINGUISHES AFTER 15 SECONDS. MAINTENANCE PERFORMED OPS TEST OF THE EMERGENCY LIGHTING SYSTEM PER SAAB 340 AMM. PROBLEM COULD NOT BE DUPLICATED. (M)SDR SIMA200124905Frame · corrodedDURING MBV INSPECTION, FOUND FRAME 236.5 UNDER GALLEY AREA HAD CORROSION BEYOND SRM LIMITS. CORROSION WAS REMOVED FROM FRAME AND WAS REPAIRED IAW SAAB 340 SRM. (M)SDR 2001F00397Smoke Detector · malfunctionedDFW - CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CRUISE. NR 1 FIRE BOTTLE WAS ACTUATED. WARNING LIGHT WENT OUT WITHIN SEVERAL MINUTES AFTER BOTTLE WAS BLOWN. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS IAW SAAB 340 AMM. OPS CHESDR SIMA200124904Smoke Detector · malfunctionedDFW - CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CRUISE. NR 1 FIRE BOTTLE WAS ACTUATED. WARNING LIGHT WENT OUT WITHIN SEVERAL MINUTES AFTER BOTTLE WAS BLOWN. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS IAW SAAB 340 AMM. OPS CHESDR SIMA200124902Control Handle · faultyBGR - FLT 4929 - CREW INITIATED EMERGENCY LANDING DUE TO THE LEFT MAIN LANDING GEAR INDICATION NOT SHOWING DOWN AND LOCKED (GREEN) DURING APPROACH. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW SAAB 340 AMM. LANDING GEAR OPERATIONALLY AND SDR MALA010696Seat Track · corrodedDURING 4K-CHECK IN CWA, AFT PORTION OF LT CENTER IS SEAT TRACK LBL 18.3 HAS HEAVY CORROSION FROM APPROXIMATELY STA 686.5 TO 633 ON FLOORBOARD FLANGE. MAINTENANCE TREATED CORROSION AND REPAIRED SEAT TRACK IAW SRM 53-70-60, MAL EO S53078.SDR MALA010695Seat Track · corrodedDURING 4K-CHECK IN CWA, RT GALLEY SEAT TRACK PROFILE HAS HEAVY CORROSION. MAINTENANCE REMOVED AND INSTALLED NEW PROFILE P/N 7253721-495 AND RAIL P/N 7253721-459 IAW SRM CHAPTER 51.SDR SIMA200124801Light · inoperativeSYR - FLT 5062 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7BC TO BE INOPERATIVE. LIGHT PUT ON MEL AT THIS TIME. (M)SDR SIMA200124803Frame · corrodedABI - DURING MBV INSPECTIONS, FOUND UPPER FLANGE OF BOTTOM FRAME 225 HAD CORROSION BEYOND SRM LIMITATIONS. REMOVED CORROSION AND REPAIRED IAW SAAB 340 SRM. (M)SDR SIMA200124702Control Cable · failedCLL - FLT 3902 - DURING CLIMB, LEFT ENGINE TORQUE DROPPED TO 30 PERCENT. CREW DECLARED INFLIGHT EMERGENCY, SHUT ENGINE DOWN, AND RETURNED TO FIELD. REMOVED AND REPLACED LEFT WING PUSHPULL POWER CABLE FROM HMU TO NACELLE WHEEL WELL IAW SAAB 340 AMM 76-10-00. SDR MALA010694Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B ELEVATOR FUSELAGE CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT I/B ELEVATOR FUSELAGE CABLE P/N 7227705-643 IAW SF340 AMM 27-31-15.SDR MALA010693Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT I/B ELEVATOR FUSELAGE CABLE P/N 7227705-643 IAW SF340AMM 27-31-15.SDR MALA010692Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B FWD AILERON CABLE IN FUSELAGE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE IN FUSELAGE WITH NEW CABLE P/N 7227105-624 SF340 AMM 27-11-25-4.SDR MALA010691Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B FWD AILERON FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD AILERON CABLE IN FUSELAGE WITH NEW CABLE P/N 7227105-623 IAW SF340 AMM 27-11-25-4.SDR MALA010690Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B FWD AILERON FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED LT O/B FWD AILERON CABLE IN FUSELAGE WITH NEW CABLE P/N 7227105-613 IAW SF340AMM 27-11-25-4.SDR MALA010689Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B FWD ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR FUSELAGE CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15.SDR MALA010688Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25.SDR MALA010687Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B DUAL CIRCUIT I FUSELAGE RUDDER CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25.SDR 2001F00499Power Supply · dischargedSPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M)SDR 2001F00498Power Supply · dischargedSPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M)SDR 2001F00497Power Supply · dischargedSPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M)SDR 2001F00496Power Supply · dischargedSPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200124501. (M)SDR SIMA200124501Power Supply · dischargedSPS - FLT 3512 - CREW REPORTED EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNITS 20LN, 21LN, 22LN, 23LN, AND 24LN. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200124502Light · incorrectBOS - FLT 4915 - FLOOR PROXIMITY EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 14 AND WAS ISSUED MEL. FOUND INCORRECT BULB WAS INSTALLED BY MAINTENANCE. BULB WAS REMOVED AND REPLACED WITH CORRECT BULB P/N 3071PEGL. (M)SDR MALA010725Motor · failedDURING WALK-AROUND AFTER FLIGHT 2742, NOTICED SUPPLEMENTAL AIR CONDITIONING INOP. NOTICED UNUSUAL SMELL FROM SUPP A/C VENT. MAINTENANCE DEFERRING SUPP A/C IAW 1-16-125-60-5-12 AFT AIR CONDITIONING, AUX HEAT BLOWN CONTROL CIRCUIT BREAKERS PULLED AND COLLARED.SDR NSVA0110Pressure Switch · leakingPILOT REPORTED FUEL LEAKING OUT OF NR 1 ENGINE DRAIN. MAINTENANCE OPENED COWLING AS NECESSARY OBSERVE FOR LEAKS, DISCONNECTED COMPONENT DRAIN LINES AT OV FUEL FILTER AND PRESSURE DIFFERENTIAL SWITCH WHILE RUNNING BOOST PUMP. ISOLATED LEAK TO FUEL PRESSURE DI
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