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 MALA080208Skin · dentedSEVERAL DENTS NOTED IN CARGO DOOR OUTER SKIN. REPAIRED IAW EO NR S52028, S52151.SDR MALA080206Frame · chafedSEVERAL FUSELAGE FRAMES INNER FLANGES CHAFED. REPAIRED IAW EO NR S53641, S53642, S53152.SDR MALA080207Skin · gougedNUMEROUS DENTS AND GOUGES NOTED IN LT AND RT OUTER FUSELAGE SKIN. REPAIRED IAW EO NR S53640, S53005.SDR PNSA02Warning System · activatedLEFT OIL PRESSURE LIGHT CAME ON DURING TAKEOFF.SDR MALA080204Frame · chafedTOP FRAME, WHERE AIR STAIR SLIDES HAS TWO DEEP CHAFES AT STA 294. REPAIRED IAW EO NR S53362.SDR MALA080205Panel · damagedPANEL 193AL HAS COMPOSITE DAMAGE. REPAIRED IAW EO NR S51031.SDR MALA080192Skin · dentedSEVEN DENTS NOTED IN THE LT FLAP UPPER SKIN PANEL 541AT. REPAIRED IAW EO NR S57231.SDR MALA080203Skin · unknownPASSENGER ENTRANCE DOOR OUTER SKIN REPAIRED. REPAIRED IAW EO NR S52152.SDR MALA080195Seat Track · corrodedREPLACED SECTION OF RT INBD AISLE SEAT TRACK 31 5/8 LONG BEGINNING AT STA 294 TO STA 326 DUE TO CORROSION. REPAIRED IAW EO NR S53060.SDR MALA080194Seat Track · corrodedREPLACED FWD SEAT TRACK SPLICE BETWEEN STA 297 AND STA 330, LBL18.3 DUE TO CORROSION. REPAIRED IAW EO NR S53060.SDR MALA080191Angle · chafedSIX CHAFE SPOTS FOUND ON CABIN FRAME INNER FLANGES OR INNER FLANGE REINFORCEMENT ANGLES. REPAIRED IAW EO NR S53635 AND S53152.SDR NSVA2008042Warning Light · false activationDURING TAKE-OFF ROLL LEFT ENGINE TAIL-PIPE HOT LIGHT ILLUMINATED AND SUBSEQUENTLY ABORTED TAKE-OFF. OPS CHECK IAW AMM 26-11-00-05, PROCEDURE 1, NO DEFECTS NOTED.SDR MALA080196Frame · damagedFRAME DAMAGED AT STA 294 BETWEEN SL1617 AND SL1618. REPAIRED IAW EO NR S53152.SDR MALA080193Panel · dentedDENT NOTED IN PANEL 193AL. REPAIRED IAW EO NR S51031.SDR NSVA2008039Control Unit · defectiveTCAS TRANSPONDER WILL NOT POWER UP. SMOKE REPORTED. FOUND FAULTY CONTROL UNIT IAW SAAB AMM 34-54-00 & 34-00-00.SDR NSVA08038Power Supply · dischargedONE GROUP OF INTERIOR EMERGENCY LIGHTS WILL NOT TEST. REPLACED POWER SUPPLY 22LN BATTERY WAS EVIDENTLY DEAD.SDR NSVA08038ABattery · dischargedDURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK 3 FLOOR PROXIMITY AND 3 EMERGENCY COVE LIGHTS WERE FOUND NOT TO BE ILLUMINATING. EMERGENCY LIGHT POWER SUPPLY 22LN WAS REPLACED IAW COLGAN AIR WORK CARD 33-50-02S AND SYSTEM CHECKED SATISFSDR NSVA2008037Unknown · smokeSMOKE IN COCKPIT DURING DESCENT. NO ABNORMAL INDICATIONS AND FLIGHT ATTENDANT DID NOT SMELL THE SMOKE. CHECKED RT & LT ENG FOR OBVIOUS DAMAGE, NO FAULT FOUND. CHECKED BOTH RT & LT ACM OILS, FOUND FULL. CHECKED FOR POPPED C/B, NONE FOUND. RAN RT ENG FOR APSDR MAL2008F00051Pump · malfunctionedFLIGHT CALLED AROUND THE MBS AREA WITH A MAIN HYDRAULIC PUMP PROBLEM. MAIN HYDRAULIC ACCUMULATOR PRESSURE DROPS FROM 3000 TO 2000 PSI EVERY 35 SECONDS IN FLIGHT. CREW TALKED TO DISPATCH MXC AND RETURNED TO DTW. WORKED UP NRS FOR FLIGHT TO RETURN TO DTW. THSDR PNSA100802Warning System · malfunctionedYELLOW TCAS ALERT SHORTLY AFTER TURN RED ALERT. PULLED C/B AND RESET THE TCAS, WENT TO A NORMAL MODE. TESTED OK, CONTINUED THE FLIGHT.SDR MALA080190Skin · dentedDENT NOTED IN RT ELEVATOR UPPER SKIN. REPAIRED IAW EO S51031.SDR MALA080189Skin · gougedGOUGE NOTED IN LT FLAP UPPER SKIN. REPAIRED IAW EO S51031.SDR MALA080187Door · dentedDENTS NOTED IN RT EMERGENCY EXIT DOOR. REPAIRED IAW EO S52147 AND S52028.SDR MALA080186Bolt · missingNLG UPPER TORQUE LINK PIN BOLT MISSING HEAD. REPLACED BOLT P/N NAS1304-25D.SDR SIMA200829602Seat Track · corrodedDURING A HMBV INSPECTION THE SEAT TRACK AT BL 0.00 WAS FOUND TO BE CORRODED. REMOVED THE SEAT TRACK AND CUT, CLEANED ALODINED AND PRIMED ALL FASTENER HOLES. REPAIR DONE IAW SAAB SRM (SRM 72LKS3079 REV 50) CHAPTER 53-70-60. AIRCRAFT RETURNED TO SERVICE.SDR PNSA081001G Switch · failedWHILE IN CRUISE THE ELT TURNED ON, FLIGHT CREW ABLE TO RESET AND CONTINUED WITH FLIGHT. TWO DAY LATER THE SAME THING, ABLE TO RESET, WHEN FLIGHT ARRIVED BACK TO MAINTENANCE BASE ELT WAS CHANGED AND TESTED OK. TEAR DOWN REPORT INDICATED THAT G-SWITCH ACTIVATESDR SIMA200828201Seat Track · corrodedDURING A HMBV INSPECTION THE SEAT TRACK AT 18.3L WAS FOUND TO BE CORRODED FROM FS 296 TO FS 310. REMOVED A 31 INCH SECTION OF SEAT TRACK. CUT NEW SECTION OF SEAT TRACK MATERIAL P/N 7253799-381 AND U-BEAM MATERIAL 7253799-379. DRILLED, CLEANED AND TREATED RESDR SIM2008F00029Repair · corrodedDURING A HMBV INSP, AN OLDER REPAIR ON THE GALLEY FRAME AT FS 258 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR FILLER. FABRICATED A NEW FILLER. DRILLED, CLEANED AND TREATED NEW PART. REPAIR DONE IAW SAAB SRM (79LKS 3079 REV 50) CHAPTER 53-70-30. SDR MALA080185Fairing · dentedTWO DENTS NOTED IN THE WING TO FUSELAGE FAIRINGS. REPAIRED IAW EO S51031.SDR MALA080184Skin · dentedDENT NOTED ON LT SIDE OF RUDDER ASSY, 5.25 AFT OF FRONT SPAR AT WL 164.55. REPAIRED IAW EO S57226.SDR MALA080183Seat Track · corrodedSEAT TRACK HAS CORROSION BL 0.0 FROM STA 294 AND STA 373. REPAIRED IAW EO S53060.SDR MALA080182Seat Track · corrodedSEAT TRACK HAS CORROSION LBL 18.3 FROM STA 294 AND STA 373. REPAIRED IAW EO S53060.SDR MALA080181Seat Track · corrodedSEAT TRACK HAS CORROSION LBL 18.3 FROM STA 521 AND STA 686.888. REPAIRED IAW EO S53060.SDR MALA080180Seat Track · corrodedLT INBOARD FLOOR TRACK HAS CORROSION BETWEEN STA 319 AND STA 363. REPAIRED IAW EO S53627.SDR MALA080179Panel · dentedSIX DISBONDED DENTS NOTED IN FUSELAGE CENTER PANEL ASSEMBLY (193AL). REPAIRED DENTS IAW EO S51031.SDR CA081001002Terminal · melted(CAN) ACFT ARRIVED FROM CUSTOMER WITH EXTERNAL POWER INOP (MEL). AFTER INVESTIGATION, FOUND THE + TERMINAL MELTED AT THEN EXT PWR CONNECTOR. SHEET METAL REPAIR WAS PREVIOUSLY DONE AT THE EXT PWR CONNECTOR ATTACHMENT. BOTH TERMINALS WERE CRACKED HALF WAY.SDR NSV2008F00028Light · noneEMERGENCY LIGHTS ARE ON WITH SWITCH IN THE ARM POSITION AND ACFT POWERED FROM BATTERIES. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-50-00 AND WC 33-50-016. NO FAULT FOUND. NOTE: EMERGENCY LIGHTS SYSTEM IS DESIGNED TO ILLUMINATE IF SDR MAL2008F00044Skin · dentedDURING THE 2Y AND N4K NOTED DENT IN RT FUSELAGE AT STA 389. REPAIRED IAW EO# S53009.SDR MAL2008F00047Skin · puncturedDURING THE 2Y AND N4K THE RT ELEVATOR UPPER SKIN PUNCTURED AT HS68.66. REPAIRED IAW EO S53229.SDR MAL2008F00037Skin · dentedDURING THE 2Y AND N4K NOTED 4 DENTS IN TAIL CONE BETWEEN STA797 AND 803. 1 ABOVE AND 3 BELOW SL1604. REPAIRED IAW EO#S53620.SDR MAL2008F00049Skin · dentedDURING THE 2Y AND N4K NOTED THE LOWER FUSELAGE CENTER WING FAIRING AT STA562 HAS SEVERAL DENTS. REPAIRED DENTS ON LOWER FUSELAGE CENTER TRAILING COVER FAIRING IAW MAL EO S51031.SDR MAL2008F00046Skin · dentedDURING THE 2Y AND N4K NOTED 13 DENTS IN UPPER SKIN OF RT HORIZONTAL STABILIZER. REPAIRED IAW EO S55017 & S55160.SDR MAL2008F00042Skin · dentedDURING THE 2Y AND N4K NOTED 2 DENTS NOTED IN RT OVERWING EXIT EXTERIOR SKIN. REPAIRED IAW EO S52028 & S52139.SDR MAL2008F00041Skin · dentedDURING THE 2Y AND N4K NOTED 3 DENTS NOTED IN TAIL SECTION STA 622-853. REPAIRED IAW EO#S53229.SDR MAL2008F00040Skin · dentedDURING THE 2Y AND N4K NOTED 32 DENTS NOTED IN THE LT FUSELAGE STA 322-392 AND 5 DENTS NOTED ON THE RT FUSELAGE STA 353-392. REPAIRED IAW EO#S53619.SDR MAL2008F00033Indicator · malfunctionedFLAP CAUTION LIGHT WENT OFF 2 TIMES. RT FLAP INDICATOR MOVE DOWN, FLAP CAUTION LIGHT ILLUMINATED. SPLIT FLAP INDICATION GREEN LIGHT ON. FLAPS TEST 1 PANEL, NO CONTROL PROBLEMS EMERGENCY LANDING JAN. VISUALLY VERIFIED FLAPS IN UP POSITION AND INDICATED AGRESDR SIM2008F00023Adi · malfunctionedON FLIGHT 3275, AT CRUISE, CREW REPORTED NR 2 EADI FLICKERED AND EXTINGUISHED INOPERATIVE WITH SLIGHT ELECTRICAL ODOR WHICH SOON DISSIPATED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED EADI IAW AMM 34-24-10-04 COMPLIED WITH ADJUST TEST NO DEFECTS. ACFT RETSDR MAL2008F00034Unknown · odorON OVERHEAD PANEL, THE L PITOT LIGHT ILLUMINATED INFLIGHT WITH AN ELECTRICAL BURNING SMELL ASSOCIATED. RAN THE QRH AND SMELL PERSISTED. DIVERTED TO FARGO AND EMERGENCY DECLARED. DISCONNECTED BATTS AND CIRCUIT BREAKER J27 PULLED. R&R THE LT CURRENT SENSOR PSDR NSV2008F00023Structure · vibrationAIRPLANE SHAKES DURING CLIMBOUT AT SLOW SPEED AND DURING APPROACH. CAPTAINS CONTROL COLUMN SHAKES. MOVES APPROXIMATELY 3 INCHES. VIBRATION DIMINISHES SOME IN CRUISE FLIGHT. VIBRATION STOPPED COMPLETELY WHEN FLAPS SELECTED TO 15 DEG ON APPROACH.SDR SIMA200824604Unknown · unknownON FLIGHT 3248 CREW REPORTED ON ABORTED TAKE OFF DUE TO NO TORQUE INDICATING ON NR 2 ENGINE, NO BOTTOM GOVERNING AND PROP RPM WILL NOT COME ABOVE 1000 RPM. ACFT REMOVED FROM SERVICE. PERFORMED GROUND RUN IAW SAAB AND GE MM NO FAULTS FOUND ACFT RETURNED TO SER
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