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 jasc_code = '5755' 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 jasc_code = '5755' 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 IPXA2024081693530Rod End · crackedCRACK - FITTING, L/H WING NO.3 SPOILER ACTUATOR ROD END FITTING. (REPLACE). .I.A.W AMM 27-61-02-404-012 REV.111 STEP 3.I ADJUST NO.3 SPOILER TO FLAP CLEARANCE. COMPLETED RII CHECK FOR INSTALL NO.3 SPOILER REF WORK ACTION 3 & 6.SDR IPXA2024082166239Support Fitting · cracked**SUPPLEMENTAL SDR** FAULT - AGING A/C INSPECTION : FOUND NO.8 SPOILER SUPPORT FITTING COLLAR CRACK. (REPLACE) INSTALL NEW FASTENER I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B11642 SH.1 REV.G. REVIEWEDSDR IPXA2024081466239Support Fitting · cracked**SDR FILED OPEN**FAULT - AGING A/C INSPECTION : FOUND NO.8 SPOILER SUPPORT FITTING COLLAR CRACK. (REPLACE) REVIEWEDSDR NACA2024071200003Doubler · damagedDURING NRC CA1559/206 CORRECTIVE ACTION FOUND CORROSION AT NO.9 SPOILER OB HINGE FITTING DOUBLER GROUND POINT. INSTALLED DOUBLER VIA METAL BOND REPAIR METHODSDR NACA2024070500007Skin · bulgedLH WING NO.2 SLAT OUTER SKIN BULGE AROUND FASTENER HOLE AT SLAT STA 183.03. CUTOUT DAMAGED AREA, MADE FILLER AND DOUBLER AND INSTALLED IAW NAC EO 737-57-0043SDR NACA2024070500006Rib · corrodedRH WING NO.9 SPOILER O/B END RIB CORRODED. ALL CORROSION REMOVED FROM RIB, REPLACED THE OB SPOILER #9 RIB WITH BOND METAL METHOD IAW NAC EO 737-57-0047 REV1RSDR FDEA202407040931Skin · damagedRH WING NO.13 SPOILER FOUND 2 EA HOLE AT 34 IN AWAY FROM IB AND 4.25 IN AWAY FROM AFT EDGE, 48 IN AWAY FROM IB AND 5 IN AWAY FROM AFT EDGE. REPAIRED RH WING NO.13 SPOILER 2 EA HOLE AT 34 IN AWAY FROM IB AND 4.25 IN AWAY FROM AFT EDGE, 48 IN AWAY FROM IB ASDR IPXA2024061299251Skin · debondedDISBOND - SKIN , R/H WING NO.8 SPOPILER UPPER SURFACE AREA , WS 724. (REPAIR) 1.REMOVE THE DAMAGED MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (L:12", W:1", 19" FROM AFT EDGE AND 90" FROM INBD EDGE AT NO.8 SPOILER) IAW SRM 57-70-01-2R-1 REFER TO SRM 51-70-05-SDR SWAA2024060698487Hinge Bracket · cracked#6 GRD SPOILER INBD HINGE SUPPORT FITTING BRACKET BENT AND BOTH SUPPORT CLIPS CRACKED. REMOVED #6 GRD SPOILER INBD HINGE SUPPORT FITTING BRACKET IAW SRM 51-40-02. BRACKET INSTALLED ON STEP 12 OF EA 24-53-01529.SDR SWI202408210700Skin · dentedTRANSFER FROM EAML 1352997 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 30 DENTS ON RH FLIGHT SPOILER UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH FLIGHT SPOILER IN REFERENCE WITH AMM 27-64-05. OPS CHECKED GOOD AT SDR FDEA202405290957Rib · gougedL3 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379359 P1, SEQ NO:001239, WRI: 57409742, TITLE: WINGS- ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT STA ABX 31.SDR FDEA202405290956Rib · gougedL3 SPOILER O/B JACK RIB UPPER & LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379359 P1, SEQ NO:001239, WRI: 57409742, TITLE: WINGS- ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT SSDR FDEA202405290955Rib · gougedL6 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #6 SPOILER O/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379363 P1, SEQ NO:001241, WRI: 57409744, TITLE: WINGS- ATTACH FITTINGS-LH WING #6 SPOILER JACK RIB AT STA SP1X 31SDR FDEA202405290954Rib · gougedL6 SPOILER I/B JACK RIB UPPER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #6 SPOILER I/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379363 P1, SEQ NO:001241, WRI: 57409744, TITLE: WINGS- ATTACH FITTINGS-LH WING #6 SPOILER JACK RIB AT STA SP1X 31SDR FDEA202405290953Rib · gougedL4 SPOILER O/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #4 SPOILER O/B JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379361 P1, SEQ NO:001240, WRI: 57409743, TITLE: WINGS- ATTACH FITTINGS-LH WING #4 SPOILER JACK RIB AT STA ABXSDR FDEA202405290951Rib · gougedR6 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #6 SPOILER JACK RIB I.A.W FEDEX EA NO: T6- 5740-T0379403 P1, SEQ NO:001245, WRI: 57409748, TITLE: WINGS- ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X 3SDR FDEA202405290918Rib · gougedR3 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0379398 P1, SEQ NO:001242, WRI:57409745, TITLE:WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX31.SDR FDEA202405290917Rib · gougedR3 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0379398 P1, SEQ NO:001242, WRI:57409745, TITLE:WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX31.6SDR FDEA202405290915Rib · gougedR5 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0379407 P1, SEQ NO:001244, WRI:57409747, TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIBS AT STA ABX SDR FDEA202405290913Rib · gougedR5 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0379407 P1, SEQ NO:001244, WRI:57409747, TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX17SDR FDEA202405290897Rib · gougedR4 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH WING #4 SPOILER JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379401 A P1, SEQ NO:001243, WRI: 57409746, TITLE: WINGS- ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STASDR FDEA202405290896Rib · gougedR4 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH WING #4 SPOILER JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379401 A P1, SEQ NO:001243, WRI: 57409746, TITLE: WINGS- ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STASDR FDEA202405280738Skin · delaminatedNO. 7 SPOILER LWR SURFACE FROM OB TO IB 17 INCH CROSS TE TO LE 29.5 INCH FOUND DELAMINATION.` EVALUATED NO .7 SPOILER LOWER SURFACE FROM OB TO IB 17 INCH CROSS TE TO LE 29.5 INCH DELAMIINATION DAMAGE SIZE LXW=0.6"X0.4" WITHIN ALLOWABLE LIMIT AS PER B777 SRSDR CALA2024060401698Plate · crackedREF AMES NON ROUTINE 171415-0500-0009. GENERATING ITEM: 171415- 0500-0001. RT WING TE TRANSITION WIGGLE PLATE CRACKED. LOCATED JUST I/B OF #8 SPOILER. TAG# 34152 REMOVED OLD AND INSTALLED NEW WIGGLE PLATE IAW BH757-200 SRM 51-40-02.SDR CALA2024060401697Plate · crackedLEFT WING TE TRANSITION WIGGLE PLATE CRACKED. LOCATED JUST I/B AND BELOW #5 SPOILER. REMOVED OLD AND INSTALLED NEW WIGGLE PLATE IAW B757-200 SRM 51-40-02.FOR MORE DETAILS UNITED FORM # 46-0024 SSFR C/W.SDR CALA2024052701594Rib · crackedLHW NO.6 SPOILER LOWER FITTING UPPER CHORD FOUND CRACK REF TO HAECO NON-ROUTINE NO. 9486159, ORIGINATED BY EMP V916669, SPEC NO. B787-57-3-0014. PERFORMED BY EMP V909250 AND RII BY EMP V916669 - LHW NO.6 SPOIL ER LOWER FITTING (IN BOARD FIXED T/E AUX D RIB) CRSDR FDEA202405190690Skin · delaminatedLH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 30MM*15MM, DEPTH: 1.51MM. COMPLIED WITH EA: 6-5750-T0379154 P1. TITLE: WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WISDR SWAA2024061186939Bracket · crackedLEFT WING UPPER SHELF PANEL I/B OF #5 SPOILER LOWER ANGLE BRACKET CRACKED ON FWD SIDE (MARKED)<[01] REMOVED AND REPLACED ANGLE BRACKET WITH FASTENERS PER SRM 51-40-02;[02] REMOVED AND REPLACED ANGLE BRACKET WITH FASTENERS PER SRM 51-40-02. INSPECTION C/W.SDR AALA202405243304Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #5 SPOILER PREVIOUS REPAIRS HAVE DELAMINATION AND ARE COMING LOOSE. MAINTENANCE REPLACED THE SPOILER AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L00027024.SDR FDEA202405120653Skin · delaminatedLH WING #4 SPOILER CENTER O/B HINGE ARM LWR SKIN FOUND DELAMINATION. SIZE: 17MM*9MM. DEPTH: 2.00MM COMPLIED WITH EA 6-5750-T0379097 P1, ACCOMPLISHED THE MODIFICATION OF SB A300-57-6082 R03 ON THE LH WING #4 SPOILER AND ALLOWED TO LEAVE THE DELAMINATION AS SDR FDEA202405120644Skin · crackedRH WING SPOILER #7, LOWER SURFACE, AT WBL 167.54 APPROX, SKIN WITH PUNCTURE. RH WING SPOILER #7, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01-2R REP 1 PAG 1-4 AND SRM 51-70-17-0G PAR C FIG 11 REV 88 DEC 15/2023SDR FDEA202405100749Rib · wornRH WING #5 SPOILER ACTUATOR O/B JACK RIB I/B FACE SURROUNDING BOLT HOLE LOCATION 3 (O/B LWR) AREA FOUND NICK ACCOMPLISHED THE REINFORCED REPAIR AT RH WING #5 SPOILER O/B JACK RIB LOWER HOLE I.A.W FEDEX EA NO:T6-5740-T0379208 P1, SEQ NO:769, TITLE: WING-ATTSDR FDEA202405100748Rib · wornRH WING #5 SPOILER ACTUATOR O/B JACK RIB I/B FACE SURROUNDING BOLT HOLE LOCATION 1 (O/B UPR) AREA LOSS OF PROTECTION ACCOMPLISHED THE REINFORCED REPAIR AT RH WING #5 SPOILER O/B JACK RIB UPPER HOLE I.A.W FEDEX EA NO:T6-5740-T0379208 P1, SEQ NO:769, TITLE: SDR IPXA2024051079464Skin · dentedRIGHT WING NR 12 SPOILER UPPER SURFACE FOUND DENT, DIA:0.94", DEPTH:0.006", 26.5" FROM T/E, 12.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR RESDR IXXA2024050601Skin · cracked#9 SPOILER LE AROUND 1 FASTENER CRACKEDSDR AALA202405085288Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #5 SPOILER INBOARD HINGE FITTING ON THE REAR SPAR AT RIB 19 IS CRACKED. REPLACED HINGE FITTING PER SRM 51-42-11.SDR IPXA2024051096662Skin · dentedRIGHT WING NR 12 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.86", DEPTH : 0.008", 31.5" FROM T/E, 3.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJORSDR IPXA2024051096630Skin · dentedRIGHT WING NR 12 SPOILER UPPER SURFACE FOUND DENT,1.DIA:0.65",DEPTH:0.005",14" FROM T/E,21.5" FROM OUTBD EDGE.2.DIA:0.53",DEPTH:0.001",14.25" FROM T/E,17.75" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SSDR IPXA2024051096433Skin · dentedRIGHT WING NR 12 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.93", DEPTH : 0.015", 1.5" FROM T/E, 24.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJORSDR IPXA2024051096403Skin · dentedRIGHT WING NR 12 SPOILER UPPER SURFACE FOUND DENT, DIA : 1.33", DEPTH : 0.011", 35.5" FROM T/E, 23" FROM INBD EDGE. (REPAIR) RREPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR SDR IPXA2024051096287Skin · dentedRIGHT WING NO.12 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.95", DEPTH : 0.006", 13.5" FROM T/E, 17.5" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJORSDR IPXA2024051096899Skin · dentedRIGHT WING NR 11 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.88", DEPTH : 0.01", 2.25" FROM T/E, 29" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR RSDR IPXA2024051096752Skin · dentedRIGHT WING NR 11 SPOILER UPPER SURFACE FOUND DENT, DIA : 1.23", DEPTH : 0.014", 22" FROM T/E, 7.5" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR RSDR IPXA2024051096740Skin · dentedRIGHT WING NR 11 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.88", DEPTH : 0.006", 25" FROM T/E, 16.5" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR RSDR IPXA2024051096728Skin · dentedRIGHT WING NR 11 SPOILER UPPER SURFACE FOUND DENT, DIA : 0.87", DEPTH : 0.007", 13" FROM T/E, 14.25" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR SDR IPXA2024051096717Skin · dentedRIGHT WING NR 11 SPOILER UPPER SURFACE FOUND DENT, DIA : 1.2", DEPTH : 0.018", 9" FROM T/E, 2.5" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPASDR IPXA2024051697030Skin · dentedRIGHT WING NR 7 SPOILER UPPER SURFACE FOUND DENT, DIA : 1.1", DEPTH : 0.008", 23.9" FROM T/E, 39.6" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL III). REPAIR CLASSIFICATION: MAJOSDR IPXA2024051696990Skin · dentedRIGHT WING NR 7 SPOILER UPPER SURFACE FOUND DENT, DIA : 1.4", DEPTH : 0.0125", 14.5" FROM T/E, 37.8" FROM OUTBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL III). REPAIR CLASSIFICATION: MAJSDR IPXA2024051696941Skin · dentedLEFT WING NR 6 SPOILER UPPER SURFACE FOUND DENT, 1. DIA : 2.6", DEPTH : 0.004", 26" FROM T/E, 16.2" FROM INBD EDGE. (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-4 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL III). REPAIR CLASSIFICATION: MAJORSDR IPXA2024051474380Skin · dentedRIGHT WING NR 10 SPOILER UPPER SURFACE FOUND DENT, DIA:1", DEPTH:0.01", 6", FROM T/E, 73" FROM INBD EDGE (REPAIR) REPAIR I/A/W: B747-400F (REV. 100) SRM 51-70-10-2R-2 AND 51-70-10-2R-0 PER SRM 57-20-01-2R-1 (DETAIL I). REPAIR CLASSIFICATION: MAJOR REPAIR PER G
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