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 = '7374K5' 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 = '7374K5' 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 K11A2024122400297Battery · inoperativeCAPTAIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED CAPTAINS EMERGENCY FLASHLIGHT BATTERY IAW B737 AMM 25-64-06. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME.SDR K11A2024121300296Indicator · out of limitsFLAP INDICATED AN ASYMMETRY, LEFT NEEDLE AT 9 O’CLOCK AND RIGHT NEEDLE AT 8 O’CLOCK WHEN SELECTING FLAPS 1, FLAPS WOULD NOT MOVE. THE FLAPS LOCKED OUT. DECLARED AN EMERGENCY COMPLETED THE QRH 4.35. WE WERE ABLE TO USE ALTERNATE FLAP EXTENSION TO FLAPS 2. PERSDR K11A2023121300246Battery · no testDURING CHECK EMERGENCY BATTERY PACK WAS FOUND INOP IN FWD GALLEYSDR K11A2023061600213Unknown · unknownRETURNED TO ROC AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT WITH CABIN OUTFLOW VALVE CLOSED AT ALL TIMES.SDR K11A2022081800156None · failed inspAT 340 (FL) FIRE WARNING FWD PIT, DECLARED EMERGENCY , STARTED DECENT TO KSTL, FIRE WARNING STOPPED AROUND FL 250, CONTINUED KSTL AND LANDED CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R SDU BATTERIES S/N E16238 IAW SECURA PLANE TECH. AMM SUP 26-15-01,SDR JR2R20220606188Skin · crackedLH LOWER FUSELAGE SKIN CRACKED 6 INCHES AFT OF LH AFT WTB FAIRINGSDR JR2R20220606324Flap · damagedLH I/B AFT FLAP LOWER SURFACE DAMAGEDSDR K11A2022042700125Controller · defectiveAIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R AND R THE PRESSURIZATION CONTROLLER IAW B737 AMM 21-31-31 & 21-31-00, OPS CHECK GOOD. NO DEFECTS NOTEDSDR K11A2021070200051Cabin Pressure · failedAIRCRAFT WOULD NOT PRESSURIZE IN FLIGHTSDR K11A2021052500050Bearing · bindingLEFT AND RIGHT INTERMITTENT BINDING ON AILERON CONTROLS, REMOVED AND REPLACED AILERON ARTIFICIAL FEEL CENTERING BEARING IAW B737 AMM 27-11-81 AND B737 SRM 51-40-04, OPS CHECK GOOD NO DEFECTS NOTEDSDR K11A2021051900049Trim Tab · looseABNORMAL VIBRATION ON TAKEOFFSDR EE4Y2020031111013Spar · corrodedRH WING FSS FWD SPAR LOWER CHORD WITH CORROSION. NOTE THAT THE RH WING FWD SPAR,LOWER CHORD AT FSS 571 WAS REPAIRED PER SERVICE REQUEST ID:4-4719754243 AND IAW COOPESA EO COO-EO-2020-10849 R00.(REF: JOB A1J003 ITEM 6-2)SDR Q2SA2019060427420Battery Pack · dischargedAIRCRAFT GROUNDED. EMERGENCY LIGHT OVER R1 DOOR INOP. REMOVED AND REPLACED RH EMERGENCY BATTERY PACK IAW B737 AMM 33-51-51. OPS CHECK GOOD.SDR Q2SA20190130402Actuator · blownAIRCRAFT GROUNDED. ENROUTE DOWNWIND, LOSS HYD SYSTEM "A". ACCOMPLISHED NON-NORMAL QRH PROCEDURE. FOUND NR 1 GROUND SPOILER TOP RIM OF CYINDER BLOWN APART. REPLACED NR 1 GROUND SPOILER ACTUATOR IAW AMM 27-62-94.SDR Q2SA20180216389Proximity Sensor · inoperativeNOSE GEAR INDICATED BOTH RED AND GREEN LIGHTS ON WHILE LANDING GEAR LEVER WAS MOVED TO UP POSITION. AIRCRAFT GROUNDED. TROUBLESHOT THE NOSE GEAR INDICATION IAW AMM 32-61-00 P101. FOUND A FAULTY NOSE GEAR PROXIMITY SNESOR. REMOVED AND REPLACED THE SENSOR IAWSDR Q2SA20180204388Battery · inoperativeEMERGENCY LIGHTS WILL NOT TEST. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-51, OPS TESTED GOOD.SDR EE4Y2017042703338Skin · canningDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND THE FUSELAGE SKIN WITH OIL CAN BETWEEN STA 500B AND STA 500B+10" AND BETWEEN STR 22L AND STR 23L. THE AFFECTED SKIN SECTION IS REPAIRED UNDER EO4502 INSTRUCTIONS AND APPROVED BY 8110-3.SDR EE4Y2017042703337Skin · canningDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND THE FUSELAGE SKIN WITH OIL CAN BETWEEN STA 480 AND STA 490 AND BETWEEN STR 22L AND STR 23L. THE AFFECTED SKIN SECTION IS REPAIRED UNDER EO4502 INSTRUCTIONS AND APPROVED BY 8110-3.SDR EE4Y2017042703339Beam · puncturedDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND AT THE STA 500B+10" BETWEEN STR 12L AND 13L LEVEL, THE SIDE BEAM AFT FACE WITH PUNCTURE. THE AFFECTED BEAM IS REPAIRED UNDER EO4412-9 INSTRUCTIONS AND APPROVED BY 8110-3.SDR EE4Y2017042703331Strap · damagedDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND AT THE UPPER FUSELAGE, MAIN CARGO DOOR SURROUND, B/S 500C, BETWEEN STR 6L AND STR 7L, FUSELAGE STRAP WITH AN ELONGATED FASTENER HOLE. THE AFFECTED STRAP IS REPAIRED UNDER EO4412-4 AND APPROVED BY 8110-3.SDR EE4Y2017042603303Frame · damagedDURING MAINTENANCE INSPECTION PROCESS IT WAS FOUND AT THE STA 847 STR 4R LEVEL, THE FRAME INNER FLANGE WITH OVERSIZED FASTENER HOLE, SPECIFICALLY AT THE CEILING SUPPORT CHANNEL ATTACHMENT POINTS. THE AFFECTED FRAME IS REPAIRED UNDER EO4412-8 INSTRUCTIONS AND ASDR Q2SA20161022262Attach Angle · corrodedCORROSION AT BS 351.2 STRINGER 17 ATTACH ANGLE. AIRCRAFT GROUNDED. R & R THE ATTACHED ANGLE IAW SRM 51-40-02 PGS 4-7 PARA 7D, 51-40-05 PG 6-10 FIG 4, 51-30-01 PGS 7-8,21 FIG 10.SDR Q2SA20151201229Warning Light · illuminatedL1 DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL WITH MASTER CAUTION LIGHT.SDR Q2SA20151117228Flap System · malfunctionedAMBER "L/E FLAPS TRANSIT" LIGHT ILLUMINATED AFTER FLAPS RETRACTED. OVERHEAD PANEL INDICATOR L/E DEVICE FLAPS NR 3 INDICATED DEPLOYED. QRH PROCEDURES FOLLOWED.SDR HN62002F00013Frame · corrodedBS 1088 BULKHEAD FORWARD SIDE, T-CHORD (FRAME) ON OUTBOARD SIDE OF APU DIFFUSER DUCT CUTOUT, HAS CORROSION. CAUSE: UNKNOWN.SDR HN62002F00012Skin · delaminatedRIGHT WING OUTBOARD AILERON TAB, OUTBOARD END IS DELAMINATED.SDR HN62002F00011Frame · corrodedCORROSION FOUND ON FRAME IN AFT CARGO BAY AT BS 847, RBL19 BETWEEN STR25R AND 26R.SDR HN62002F00008Stiffener · corrodedAPU COMPARTMENT RIGHT SIDE BULKHEAD, APU TORQUE BOX LINER CUTOUT, VERTICAL STIFFENER CORRODED, BS1126, RBL 15. CAUSE: UNKNOWNSDR HN62002F00007Cargo Track · corrodedCORROSION ON RIGHT HAND CARGO TRACK, FROM BS 500F TO BS 500G, RBL 14, WL 156.SDR HN62002F00006Angle · corrodedCORROSION ON AFT BULKHEAD LOWER SUPPORT DP714C ANGLE, BS 947, LBL 17, TO RBL 15, WL 179.SDR HN62002F00005Cargo Track · corrodedCORROSION ON LEFT HAND CARGO TRACK BETWEEN BS 500F AND 500G, LBL18, WL 156.SDR HN62002F00004Fitting · corrodedAFT GALLEY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTINGS HAS CORROSION.SDR HN62002F00003Frame · corrodedCORROSION ON FRAME AT BS 294, RBL 53, WL 208.SDR HN62002F00002Structure · crackedRIGHT ELEVATOR TAB, INBOARD HINGE CUTOUT, CRACKED AT LOWER OUTBOARD END.SDR HN62002F00001Fitting · corrodedAFT ENTRY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTING HAS CORROSION.SDR HN62002F00000Fitting · corrodedAFT ENTRY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTING HAS CORROSION. CAUSE: UNKNOWN
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