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 = '5711' 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 = '5711' 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 YENA2022080200734Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB14 T O RIB15 ON LH WING REFER TO THE MPD TASK 572179-01; PERFORMED INTERIM REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 14 ON LH WING I.A.W. EC NO. A22-606-01, ANDSDR YENA2022080200733Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB13 TO RIB14 ON LH WING REFER TO THE MPD TASK 572179-01; B17030932, DUE DATE NOV-29-2022 ULTRASONIC PHASED ARRAY P/N: OMNI-MX; S/N: OMNI-102103; DUE DATE: JUL-30-2022. CSDR IXXA2022072901001Spar · corrodedR WING LEADING EDGE ABOVE PYLON, FLAKING CORROSION AT “OF. SS. 400.00”.SDR DALA2022071804967Frame · crackedSHIP 3229 CRACKS FOUND IN SEVERAL LOCATIONS AT FR 36 INTERFACE BTWN VERTICAL STIFFENERS AND FLOOR BEAMS (Y-765,Y-254,Y254, AND Y765) L. CORRECTIVE ACTION: REPAIRED PER ERA 600173-14AD. CONTINUE ON MON. (2325286)SDR JR2R20220712997Spar · crackedRH WING O/B SPAR 1 CRACKEDSDR R61A2023080100407Spar · unknownMAJOR****RH-OB-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P2. PERFORMED JC# 170EO-57-20-0050MA_1****MAJORSDR R61A2023080100406Spar · unknownMAJOR****LH-OB-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P1. PERFORMED JC# 170EO-57-20-0049MA_1****MAJORSDR JR2R20220711624Spar · crackedRH WING TIP FWD SPAR IS CRACKEDSDR JR2R20220711623Spar · crackedLH WING TIP FWD SPAR CRACKEDSDR DALA2022070404615None · noneSHIP 177 ERA 599988-14 ISSUED FOR REWORK TO STA 955 LH REAR SPAR WEB, FOL LOW ON ACTION IS REQUIRED, CORRECTIVE ACTION: ACCOMPLISH SECTION II EVERY 2844 FLIGHT CYCLES AFTER SECTION I. ASSOCIATED ER/A 00-599988. (2303345)SDR DALA2022063004582None · noneSHIP 178 RH MLG W/W STA 955 FOUND CORROSION AT IB GAP BETWEEN REAR SPAR BULKHEAD AND SIDE FRAME FITTING. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 599695-14 (2298247)SDR LR7A2022062403142Beam · corrodedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE CENTER WING FRONT BEAM WEB CORRODED, FS517, WL269. / REPAIRED IAW LAC MEA 382-57-22-020. NR# 1000690185.SDR EE4Y2022062015827Skin Panel · corrodedDURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-001 MPD, IT WAS FOUND AT LH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUT AFTER CORROSION REMOVAL WAS FOUNDSDR EE4Y2022062015828Skin Panel · corrodedDURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-002 MPD, IT WAS FOUND AT RH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7, RIB 15, RIB 21 AND RIB 22 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUTS AFTERSDR DALA2022062004282Skin · corrodedSHIP 3224 CORROSION UPPER SURFACE EXTERNAL SKIN REAR SPAR AREA FR24 TO FR26 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 599270-14 REV ORIGINAL. (2284870)SDR DALA2022062004281Skin · corrodedSHIP 3224 CORROSION TRAILING EDGE REAR SPAR UPPER SKIN LOC. BTW RIB 24 TO RIB26 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 599270-14 REV. ORIGINAL. (2284205)SDR AALA202206282152Web · crackedAIRCRAFT IN BASE MAINTENANCE: WING CENTER SECTION REAR SPAR WEB CRACKED AT STA 663.75, AND RIGHT BUTT LINE 15-25. REPAIRED WITH BONDED REPAIR WING CENTER SECTION REAR SPAR WEB PER SRM 51-70-04-2R.SDR DALA2022061704263Pickle Fork · corrodedSHIP 178 DURING HCK AT STAG, CORROSION WAS NOTED ON THE RH PICKLE FORK (SIDE FRAME FITTING), STA 955. ER/A 599695-14 SECTION I WAS ACCOMPLISHED, FOLLOW ON ACTION IS REQUIRED FOR SECTION II, CORRECTIVE ACTION: ACCOMPLISH ER/A 599695-14 SECTION II INSPECTION BEFSDR JR2R20220613520None · crackedRH WING FWD SPAR #1 CRACKEDSDR JR2R20220613584None · crackedLH WING SPAR 1 CRACKED AT WINGTIP ATTACH POINTSDR DALA2022061304141Spar Web · corrodedSHIP 1605 CORROSION FOUND ON THE GAP AREA BETWEEN THE RH SIDE WING CENTER SECTION REAR SPAR WEB AND THE SIDE FRAME BULKHEAD FITTING. CORRECTIVE ACTION: THE CORROSION AREA REPAIRED AS PER PRI 599482-14 REV 0 AND PRI 599482-14 (2273299)SDR DALA2022061004086Bulkhead · cracked(LOG 2270542) DURING INSPECTION FOUND CRACK FOUND ON LEFT WHEEL WELL FWD BULKHEAD BETWEEN 31.83 LBL AND ADJCENT O/B STIFFENER WITHIN POCKET AREA. FABRICATED DOUBLER AND DRILLED TO FINAL HOLE SIZE. ALODINED & PRIMED DOUBLER. INSTALLED REPAIR DOUBLER PER SRM 57-SDR DALA2022061004085Bulkhead · cracked(LOG 2270532) DURING INSPECTION FOUND CRACK ON LIFT WHEEL WELL FWD BULKHEAD BETWEEN 45.64 LBL AND ADJACENT I/B STIFFENER WITHIN POCKET AREA. FABRICATED REPAIR WEB FROM 0.16 IN 2024-T3 IAW B737 SRM 57-10-00 TABLE 202. TREATED AND PRIMED PARTS INSTALLED REPAIR ASDR R61A2022062500410Wing · crackedWHILE ACFT IN HEAVY CHECK MAINTENANCE FOUND A CRACK ON LH WING LOWER SKIN AT SPAR 2 BETWEEN RIB 15-16. COMPLIED WITH ETD2022-170-020076.SDR SWAA2022060713336Bracket · brokenRIGHT WING REAR SPAR I/B THROUGH ACCESS PANEL 651DB ATTACHED BRACKET TO SPAR IS BROKEN / [01] REMOVED DAMAGE BRACKET AT R/W REAR SPAR I/B THROUGH ACCESS PANEL 651DB PER REF B737-700 SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED DAMAGE BRACKET AT R/W REAR SPAR ISDR DALA2022051703401Bearing Support · corrodedSHIP 1818 LH MLD WHEEL WELL PICKLE FORK AREA BEARING PLATE FOUND CORROSION, CORRECTIVE ACTION: REAR SPAR WEB REPAIRED AS PER PRI: 597988-14 (2236517)SDR SIMA20220513005Spar · crackedLH WING SPAR 1 CRACKED AT OUTBD TIP.-C/A-RAR LH WING OUTBD SPAR 1 FITTING IAW EMB-175 SRM 51-40-08.SDR SIMA20220513004Spar · crackedRH WING SPAR 1 CRACKED AT OUTBD TIP. (MAJOR REPAIR)-C/A-REMOVED AND REPLACED WITH SERVICEABLE RH OUTBD SPAR 1 IAW EMB-175 SRM 51-40-08SDR DALA2022051303327Skin · wornSHIP 671 DURING THE ENABLING ACTIVITIES OF W.O 5725- 010006-01A, WEAR WAS FOUND IN THE AREA OF THE LOWER AFT WING SKIN, AFT EDGE AT THE FLAP TRACK NBR 2, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00255:WEAR IN THE AREA OF THE LOWER AFT WING SKIN , AFT EDGE ATSDR DALA2022051203299None · noneSHIP 671 DURING THE ENABLING ACTIVITIES OF W.O 5725- 010006-01B, WEAR WAS FOUND IN THE AREA OF THE LOWER AFT WING SKIN, AFT EDGE AT THE FLAP TRACK NBR 7, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00254:WEAR IN THE AREA OF THE LOWER AFT WING SKIN , AFT EDGE ATSDR FDEA202205091158Spar Cap · noneEXISTING REPAIR FOUND AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906. EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-03-2R REPAIR 1 FIGURESDR SIMA20220507003Spar · crackedRH WING SPAR 1 CRACKED AT OUTB TIP. MAJOR REPAIR. REPLACEMENT OF WING TIP INBOARD SPAR I WITH REINFORCED SPAR SECTION - RH WINGLET. PN 171-16240-408, SN 0000896457, WING TIP ASSYSDR DALA2022050603183None · noneSHIP 3223 CRACKS WERE FOUND AT HOLES IN FLOOR BEAM/ VERTICAL STIFFENER JUNCTION AT Y254, Y765, Y-254, Y-765, HOLES 1 AND 2 FOR EACH. CORRECTIVE ACTION: COMPLIED WITH ERA 598059-14AD. (2224101)SDR DALA2022050403119Spar · wornDISCOVERED WEAR ON THE PREVIOUS REPAIR AT THE RIGHT WING FIXED LEADING EDGE STA XIS 117. SUMMARY OF NRC 00055: WING FIXED LEADING EDGE STA XIS 117 WAS REPAIRED PER ER/A 599011-14 REV. ORIGINAL, SECTION I. PERMANENT REPAIR AND PER PRI 599011-14 REV 0. ASSOCIATESDR DALA2022050403116Doubler · wornFOUND WEAR ON THE FIXED LEADING EDGE REPAIR DOUBLER STA XOS 329 TO 335 AT LH WING (LW). SUMMARY OF NRC 00033: FIXED LEADING EDGE REPAIR DOUBLER STA XOS 329 TO 335 AT LH WING WAS REPLACED PER ER/A 551840-14 REV. ORIGINAL SECTION I. PERMANENT REPAIR. (LP #221844SDR DALA2022042903023None · noneSHIP 3249 CORROSION FOUND ON LH WING AFT SPAR/ACA (ANCHORAGE) FITTING INTERFACE. BOLTS IN HOLES 52,53,54 WERE FOUND SHEARED AND CORROSION AT HOLES 52,53,54,55, AND 81, PER SB A320-57-1089 NUMBERING. CORROSION ON AFT SPAR WEB AND ACA FITTING. CORRECTIVE ACTION:SDR JR2R20220425108Rib · crackedLH HORIZONETAL STAG FWD RIBS 11 AND 12 CRACKEDSDR IXXA2022042702Spar · crackedL/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX
LES 525. FAS WO N389AZ-02-01. N/R 00049.SDR IXXA2022042600001Spar · crackedL/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX LES 500.10. FAS WO N389AZ-02-01 NON ROUTINE 00050SDR KCSA202204191047Stiffener · corrodedFWD SPAR VERTICAL STIFFENER SHOWS EVIDENCE OF CORROSION AT OLES 1560SDR DALA2022060203868Floorbeam · crackedSHIP 3249 SEVERAL CRACKS WERE FOUND IN THE FLOORBEAMS AT VERTICAL STIFFENERS INTERFACE AT FR36, AND Y-765 H1, Y-254 H1 AND H2, Y254 H1 AND H2 Y765 H1 AND H2. CORRECTIVE ACTION: COMPLIED WITH ERA 596762-14AD. (2195259)SDR SWAA2022050394012Panel · delaminatedR/W FRONT SPAR L/E PANEL 621HB EDGE DELAMINATED / [01] MEASUREMENTS;[02] REPAIRED SMALL EDGE DAMAGE SIZE .750 DIA. ON R/W FRONT SPAR L/E LOWER ACCESS PANEL 621HB AS PER B737 SRM 51-70-04-2R-7 ; MATERIALS USED PO#11533636; PO#1690463 AND PO#1753794;[03] VERIFIESDR DALA2022041802636Shim · migratedSHIP 681 LAMINATED SHIM MIGRATION FROM REAR SPAR AND BODY SPLICE PLATE. BS 1040. DOT 99-051. CORRECTIVE ACTION: SUMMARY OF NRC 00082 - ACCOMPLISHED REPAIR AT CENTER WING REAR SPAR RBBL 70.50 AT STA 1040 TERMINAL FITTING, ALL CDCCL AND SFAR 88 REQUIREMENTS COMPSDR DALA2022041402609None · noneSHIP 681 REPAIR TO CENTER WING, LWR REAR SPAR, SOB SPLICE AT RBBL 70.5 REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598110-14AD. CORRECTIVE ACTION: REF ERA 598110-14AD. (2193618)SDR DALA2022040602368None · noneSHIP 1604 RH WING CENTER SECTION REAR SPAR WEB NEAR REAR SPAR BULKHEAD FITTING (PICKLE FORK) LH UPPER CORNER SUSPECT CORROSION, CORRECTIVE ACTION: THE CORROSION AREA REPAIRED AS PER PRI 597729-14 (2185418)SDR KCSA202204041036Stiffener · corrodedLH WING LE AT FSSO 1510 LE RIB ATTACH STIFFENER TO FRONT SPAR HAS CORROSIONSDR IXXA2022050401Rib · crackedCRACK INDICATION ON RH REAR SPAR LOWER CHORD AT RIB POST 10. ONE CRACK INDICATION ON THE OUTBOARD SIDE OF RIB 10 AFT/OUTBOARD FASTENER TRAVELING APPROX 1/4" LONG. FAS WO N431AZ-01-01 NON ROUTINE 00327SDR SWAA2022040487627Frame · crackedBS 502; LBL 69; WL 190; 2.25' CRACK IN L/H WING TO BODY FAIRING MOUNT FRAME. / [01] REMOVED CRACKED LH WING TO BODY FAIRING MOUNT FRAME IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW LH WING TO BODY FAIRING MOUNT FRAME PN 116A3118U9 ATAG A121005 IAW BOEINGSDR DALA2022032502013Spar · not reportedSHIP 179 ERA 597468-14 ISSUED FOR REPAIRS TO WING CENTER SECTION REAR SPA R WEB AND REAR SPAR BULKHEAD FITTINGS. CORRECTIVE ACTION: DTA DTE IS REQUIRED NO LATER THAN 37499 TOTAL FLIGHT CYCLES. (2169234)SDR DALA2022032201861Not Reported · not reportedCRACKS (3 EA) ON INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE (IN REF SETTLEMENT AREA OF REFUEL ACCESS PANEL LATCHES). SUMMARY OF NRC 00079: INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE WAS REPAIRED PER ERA 598025-14 REV. ORIGINAL, PRI REV. 0 AND SRM 57- 40-01 REP
Back to JASC 5711