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 n_number = 'N652FE' 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 n_number = 'N652FE' 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 FDEA202510182050Grip · missingCAPTAINS SLIDING WINDOW HANDLE MISSING GRIP. REF IPC 56-12-11-03A ITEM 15 PART 18OCT25 16:30 SDF IDENTIFIED PARTS HANDLE FOR SLIDING WINDOW INSTALLED MISSING GRIP AND SET SCREW PER SMP. REF ERS 25-03162. PER MEM QA, GRIP INSTALLATION IS NOT RII. LH SDR FDEA202409251402Seat Track · damagedFLOOR SEAT TRACK DAMAGED AT POSITION 12R FOR LOCK. SEAT TRACK ADAPTER LOBES AT LOCK MT1673 BROKEN. INSTALLED SEAT TRACK SECTION AND REPAIR IAW SRM 53-10-16-201/FIG 201. INSTALLED FLOORBOARDS IAW AMM 53-10-25-04-02 AND HANDLING SYSTEMS IAW AMM 25-58-00-00.SDR FDEA202409251401Seat Track · damagedFLOOR SEAT TRACK DAMAGED AT POSITION 12R FOR LOCK. SEAT TRACK ADAPTER LOBES AT LOCK MT1673 BROKEN. INSTALLED SEAT TRACK SECTION AND REPAIR IAW SRM 53-10-16-201/FIG 201. FLOORBOARDS IAW AMM 53-10-25-04-02 AND HANDLING SYSTEMS IAW AMM 25-58-00-00. INSTALLEDSDR FDEA202308111550Rib · corrodedR/H WING SPOILER 4 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375735 P1,SEQ NO:863, TITLE: WINGS - ATTACH FITTINGS - RH WING #4 SPOILER JACK RIB AT STA ABX 10SDR FDEA202308101567Flange · wornRH MLG DOOR CENTER FITTING AFT SIDE IS WORN INSTALLED THE NEW CENTER HINGE FITTING WITH FASTENERS I.A.W A300-600F SRM 51-40-21-001, PARA.6~7, PAGE.7B-50 & 51-72-10-001, PAGE.2 "MAJOR REPAIR"SDR FDEA202308081566Rib · corrodedR/H WING SPOILER 3 BEAM O/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0375736 P1,SEQ NO:862, TITLE: WINGS - ATTACH FITTINGS - RH WING #3 SPOILER JACK RIB AT STA ABX31.SDR FDEA202308081565Rib · corrodedR/H WING SPOILER 3 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375736 P1,SEQ NO:862, TITLE: WINGS - ATTACH FITTINGS - RH WING #3 SPOILER JACK RIB AT STA ABX31.SDR FDEA202308081559Rib · gougedR/H WING SPOILER 5 BEAM I/B JACK RIB LWR BORE INNER FACE GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375737 P1,SEQ NO:865, TITLE:WINGS - ATTACH FITTINGS - RH WING #5 SPOILER JACK RIB AT STA ABX 175.8SDR FDEA202308081558Rib · corrodedR/H WING SPOILER 5 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375737 P1,SEQ NO:865, TITLE:WINGS - ATTACH FITTINGS - RH WING #5 SPOILER JACK RIB AT STA ABX 17SDR FDEA202308081549Rib · gougedR/H WING SPOILER 4 BEAM O/B JACK RIB UPR BORE INNER FACE GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0375735 P1,SEQ NO:863, TITLE: WINGS - ATTACH FITTINGS - RH WING #4 SPOILER JACK RIB AT STA ABX 103.7SDR FDEA202308061551Rib · corrodedLH WING NO.4 SPOILER I/B JACK RIB UPPER RIB BORE INNER SURFACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT LH#4 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375643 P1,SEQ NO:861, TITLE:WINGS - ATTACH FITTINGS - LH WING #4 SPOILER JACK RIB AT STA ABSDR FDEA202308061370Seat Track · wornFR54/FR54.2 LH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.27MM I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061369Seat Track · wornFR54/FR54.2 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.22MMSDR FDEA202308061368Seat Track · wornFR54/FR54.2 RH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.27MMSDR FDEA202308061367Seat Track · wornFR54/FR54.2 RH NO.4 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.44MM I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061366Seat Track · wornFR54/FR54.2 RH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.09MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061365Seat Track · wornFR38.2/FR40 LH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.06MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061364Seat Track · wornFR38.2/FR40 LH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.57MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061363Seat Track · wornFR38.2/FR40 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.47MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308061362Seat Track · wornFR38.2/FR40 RH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.09MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202308051525Flap · cracked2EA CRACKS (30MM & 4MM) WERE FOUND AT L/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGE REPAIR AND LOWER SKIN EXTERNAL DOUBLERS REPAIR (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX EA NO:T6-5750-T03283SDR FDEA202308051522Flap · cracked2EA CRACKS (30MM & 7MM) WERE FOUND AT L/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGES AND LOWER SKIN CUT OUT, REPAIRED WITH REPAIR ANGLES AND DOUBLERS (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX ESDR FDEA202308041390Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER7-12", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSSDR FDEA202308041389Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER10-24", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENSDR FDEA202308041388Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER10 6", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSSDR FDEA202308041387Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16 18", T/E-5.5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMESDR FDEA202308041386Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR57-57.2, Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,SDR FDEA202308041385Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR28-30, Y450 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, SDR FDEA202308041384Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR28-30, Y0 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSDR FDEA202308041377Angle · crackedAFT CGO COMP'T CEILING PANEL SUPPORT ANGLE CRACK NEAR UPR FWD CORNER AREA BETWEEN FR60~61 POSITION. REMOVED CRACKED SUPPORT ANGLE AND INSTALLED NEW ONE. I.A.W A300-600F SRM 51-72-10- 001, PAGE.2 AND 51-40-21-001, PARA .6, PAGE.7B-23SDR FDEA202308031383Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LH I/B FLAP LWR SKIN AT T/E RIB 14A,T/E-10" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202308031382Aileron · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 2~3,T/E-7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202308031381Aileron · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 11~13,T/E-2.7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14SDR FDEA202308031380Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 9~10,REAR SPAR DATUM 12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRSDR FDEA202308031378Support · damagedAFT CGO CMPTR RH FR59A FOUND 1EA WIRE CONDUIT SUPPORT BROKEN REMOVED BROKEN WIRE CONDUIT SUPPORT, AND INSTALLED NEW ONE. I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND 51-40-21-001, PARA.13, PAGE.149-156SDR FDEA202308011488Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR 19~20, STGR 52~54L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202308011379Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR 27, BTW STGR 32~34R COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.SDR FDEA202307301575Fitting · crackedTHE MDC DOOR ACTUATOR YOKE BOTH SUPPORT FRAME WERE FOUND CRACK & BROKEN FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO:T6- 5230-T0375508 P1, SEQ NO:857, TITLE:DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARING FITTINSDR FDEA202307301414Fitting · crackedAVIONICS COMP'T ACCESS DOOR STOP OMEGA FITTING CRACK. REPLACED FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-PAGE.23SDR FDEA202303210479Fitting · cracked(EA # 6-5315-T0328356 D P2) UPON OPEN-HOLE HFEC OF FR44RL FOOT, FOUND HOLE # H1 CRACKED WITHIN THE FWD FRAME LAYER AT THE 4:00 CLOCK POSITION, AS VIEWED LOOKING AFT: MARKED IN RED. COMPLIED WITH EA T-6-5315-T0328356 E P3 FUSELAGE-FRAME FOOT CRACK,FRAME FEESDR FDEA202207311831Pump · failedAT GEAR RETRACTION, HYDRAULIC GREEN PUMP #2 LOW PRESSURE ANNUNCIATOR ON ECAM. GEAR RETRACTED SLOWER THAN NORMAL. AFTER GEAR FULLY UP AND RETRACTED THE LOW PRESSURE CAUTION WENT AWAY. REPEAT SQUAK. REPLACED #2 GREEN HYD. EDP IAW A300-600 AMM CH. 29-11-3SDR FDEA202201070022Bulkhead · damagedMDIS 652 53-10 4930 05JAN22 FNT OPEN U AFT PRESSURE BULKHEAD PUNCTURED AT LEFT SIDE, MAIN DECK FLOOR LEVEL, BY GUIDE BAR LEFT ABOARD FROM ONLOADING COMMANDER. SHGN 05JAN22 18:14 FNT U REMOVED MDC AFT LEFT BULKHEAD PARTITION TO ACCESS AND SDR FDEA202201060149None · unknownL1 AND R1 ESCAPE SLIDE INDICATOR WARNING LIGHTS WILL NOT TEST REPLACED ASPSU IAW AMM 52-73-18-04-0, OPS CKS GOOD, MEL REMOVEDSDR FDEA202112073042Battery · failedR1 DOOR SLIDE WILL NOT ARM. . RELEASED FOR SERVICE PER MEL : 52-XX-XX CATEGORY : C EXPIRATION : 15DEC21 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURSDR FDEA202105201319Elevator · damaged1. 2 EA WATER TRAPPED AREAS (50MM X 50MM)(50MM X 50MM) WERE FOUND AT NO.22 & NO.28 FASTENER OF LH ELEVATOR UPPER SKIN PANEL. 2. 2 EA WATER TRAPPED AREAS WERE FOUND AT NO.2 & NO.7 FASTENER OF LH ELEVATOR LWR SKIN PANEL. THE MAX WATER TRAPPED AREA IS 50MM XSDR FDEA202105201314Elevator · damaged1.1EA WATER TRAPPED AREA(120MM*75MM) WAS FOUND AT NO.22 FASTENER OF LH ELEVATOR LWR SKIN PANEL. 2.2EA WATER TRAPPED AREA WERE FOUND AT NO.27 & NO.38 FASTENER OF LH ELEVATOR UPR SKIN PANEL. THE MAX WATER TRAPPED AREA IS 70MM*65MM. THE FASTENER NO COUNTISDR FDEA202105191297Skin · crackedRH WING ALL SPEED AILERON UPR SURFACE GOT A NICK AT T/E O/B SECTION AS MARK I.A.W. EA #6-5750-155229A PART:2 (P2) TITLE: WINGS - FLIGHT SURFACES - ALL SPEED AILERON UPPER AND LOWER SKIN REPAIRS ACCOMPLISHED THE WORK.SDR FDEA202105191295Floor Panel · dentedTHE #132PG FLOOR PANEL OF LOWER FWD CARGO COMPPARTMENT WAS FOUND LOWER SURFACE SEVERAL DENT WITH MARK REPAIRED THE DAMAGED AREA WITH RESIN AND FIBERGLASS I.A.W A300-600F SRM 53-10-20- 201 PARA8B FIG203 SHEET1SDR FDEA202105181263Floor Panel · brokenTHE #131PG FLOOR PANEL OF LOWER FWD CARGO COMPPARTMENT WAS FOUND BROKEN REPAIRED THE DAMAGED AREA WITH RESIN AND FIBERGLASS I.A.W A300-600F SRM 53-10-20- 201 PARA.8B FIG.203 SHEET1.SDR FDEA202105181283Floor Panel · damagedTHE #241PF FLOOR PANEL OF MAIN DECK COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK REPAIRED THE FLOOR PANEL I.A.W A300-600F SRM 53-10-20-201 P201~205 & P208 & FIG201
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