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 CKSA96177Spar Cap · corrodedKOSC - DURING C-2 CHECK INSPECTION FOUND: RIGHT WING LEADING EDGE LOWER SPAR CAP CORRODED AT WS 1300. REMOVED CORRODED SPAR CAP AND REPAIRED IAW B747 SRM 57-30-03. CORROSION CARD NR C57-510-01. TASK CARD NR 85485.SDR UPS96421477Spar Web · crackedINSPECTION TYPE-C, MID-SPAR WEB INSPECTION, EO 747-5710-7893 FOUND CRACK IN WEB AT WS 453. CRACK IS APPROX 7 MM, STARTING AT FASTENER HOLE FROM SECOND ROW OF FASTENERS THAT ATTACH THE WEB TO THE UPPER CHORD. REPAIRED MID-SPAR WEB AT WS 453 ACC EO B747-5710-7SDR UPS96221437Spar · corrodedINSPECTION TYPE: C. WHILE CARRYING OUT REPAIR TO LEADING EDGE AT WS 349 ON RT WING, CORROSION FOUND ON UPPER SURFACE OF FRONT SPAR UPPER CHORD. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS. SEE SRS EO 96-35-005 REFERENCE UPS REPAIR AUTHORIZATION ENGINEERINGSDR CALA9601803Spar · corrodedINSPECTION FOUND CORROSION ON REAR SPAR AFT FACE AT WS 405. THE AREA WAS REPAIRED IAW SRM 5720-01551.SDR 9622109956Spar Web · crackedDURING SCHEDULED MAINTENANCE, FOUND A 1.7 INCH CRACK IN THE RIGHT WING REAR SPAR WEB UNDER THE REAR SPAR PANEL ATTACH FITTING WS 58. REPAIRED PER EM 57-10-00028.SDR ZIAA96049Spar · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING LE SPAR XFS 500. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR 96ZZZX5418Spar Cap · corrodedUPON PREPPING WINGS FOR RE-COVER, EXFOLIATION DISCOVERED IN STBD WING MAIN SPAR CAP UPPER. SEVERAL LAYERS OF VARIOUS TYPES OF TAPE HID THE CORROSION UNTIL REMOVED FOR INSPECTION. EXFOLIATION RUNS FULL LENGTH OF SPAR CAP, VARYING IN DEPTH TO .0625 INCH.SDR ABXA9700709Spar Car · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR TEE CAP DOUBLER CORRODED. REPAIRED LEFT WING REAR SPAR CAP IAW ABX REA D957-16504-MR.SDR ABXA9700708Spar Cap · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW ABX REA 957-16496-MR.SDR ABXA9700707Spar Cap · corrodedDURING ACCEPTANCE INSPECTION FOUND THE LEFT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW ABX REA D957-16496-MR.SDR UPS96221267Spar · crackedINSPECTION TYPE-D, CRACK IN REAR SPAR UPPER CHORD AT WS 290 RT. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-01.SDR 97ZZZX1416Spar Cap · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON RT WING LOWER CAP OF FRONT SPAR, WS 519, AFT OF NR 6 L/E SLAT ACTUATOR.SDR P5CA9600751Spar · corrosionLEVEL 1 CORROSION ON RIGHT WING FRONT SPAR LOWER CHORD AT NR 19 LEADING EDGE FLAP PANEL WELL. REMOVED LEVEL 1 CORROSION AND TREATED AREA PER BAC SRM 57-30-01.SDR 9621409178Spar Cap · crackedDURING H-CHECK, FOUND A 4 INCH CRACK IN THE CENTER WING REAR SPAR UPPER CAP AT THE VERTICAL KEEL PANEL. REPAIRED CAP (P/N 9911752-1) PER EA 91-111701.SDR 96ZZZX5598Spar · corrodedINSPECTION OF LT WING AFTER INCIDENCE OF STORM DAMAGE TO TIP BOW, FOUND HEAVY CORROSION TO BOTH SPARS. RT WING WAS THEN INSPECTED AND SPAR CORROSION WAS ALSO FOUND. LT WING CORROSION WAS ACCELERATED BY A LARGE BIRD NEST INSIDE. REPLACED SPARS WITH NEW.SDR 96ZZZX5597Spar · corrodedINSPECTION OF LT WING AFTER INCIDENCE OF STORM DAMAGE TO TIP BOW, FOUND HEAVY CORROSION TO BOTH SPARS. RT WING WAS THEN INSPECTED AND SPAR CORROSION WAS ALSO FOUND. LT WING CORROSION WAS ACCELERATED BY A LARGE BIRD NEST INSIDE. REPLACED SPARS WITH NEW.SDR DLL13962258Spar Web · crackedTHE RT WING REAR SPAR WEB AT THE UPPER CAP ATTACH AT IWS 310-330 AND UPPER WING SKIN HAS A CRACK. THE DAMAGE WAS REINFORCED WITH A REPAIR PLATE.SDR 96ZZZX5131Spar · corrodedDURING FUEL TANK REMOVAL FOR DETERIORATED HOSE REPLACEMENT, FOUND CORROSION ON WING SPAR.SDR 96ZZZX5434Spar · delaminatedFOUND SEVERE SPAR DELAMINATION ON UPPER OUTBOARD FUEL TANK ATTACH POINTS. SUBMITTER STATED APPEARS TO BE RESULT OF EXPOSURE TO SALT AIR NEAR SEACOAST IN FLORIDA. SUBMITTER SUGGESTS TANK REMOVAL AND INSPECTION OF AREA EVERY 5 YEARS. AIRCRAFT WAS BASED IN SALSDR 96FDEA01488Spar Chord · corrosionNR 0685 AND 034, UPON REMOVAL OF REAR SPAR WEB FOUND CORROSION ON LOWER 870 SPAR CHORD BS 870 LBL 50 TO RBL 50 WL 161. *S/D* REMOVED CORROSION ON BS 870 SPAR CHORD, FOUND CHORD IS OUT OF LIMITS PER FEDEX SRM 57-12-20. REMOVED AND REPLACED LOWER CHORD PER FEDSDR 97ZZZM523Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 520 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.SDR 97ZZZM522Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 420 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.SDR 97ZZZM521Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 410.0 L/E FORWARD LOWER SPAR CAP CORRODED. MECH REMOVED CORROSION BOTTOM OF FORWARD CHORD AT RIGHT WING STATION 410 IAW B727 SRM 51-10-6. CORROSION REMOVAL WENT OUT OF LIMITSSDR 97ZZZM511Spar · corrodedDURING SCHEDULED INSPECTION AT AERO COP IN LAKE CITY, FL, FOUND LT WING STATION 491.5 L/E SPAR AFT OF NR 4 SLAT ACTUATOR CORRODED APPROX 6 INCHES IN LENGTH. MECH REMOVED CORROSION AT WS 491.5 L/E SPAR IAW B727-SRM 51-10-6. REMOVED AT .091 METAL 14 INCHES ORISDR 97ZZZM508Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING STATION 546.5 L/E SPAR CORRODED FORWARD OF NR 4 SLAT ACTUATOR ARM. FOUND TO BE IN LIMITS.SDR 97ZZZM507Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 629, L/E SPAR CORRODED AT ACTUATOR ARM NR 7. FOUND TO BE IN LIMITS.SDR 97ZZZM503Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 738.5 LEFT FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMIT.SDR 96FDEA01477Spar Chord · corrodedNR 0661 AND 025, CORROSION AT BS 870 RBL 40 TO RBL 55, WL 190 UPPER CHORD. CORROSION IS OUT OF LIMITS AS PER FEDEX SRM. *S/D* REMOVED CORROSION ON UPPER STA 870 SPAR CHORD, FOUND SPAR CHORD IS OUT OF LIMITS PER FEDEX SRM 57-12-20. REMOVED AND REPLACED UPPESDR MWEA96503Spar · corrodedDURING INSP, RT WING REAR SPAR LOWER TEE CAP HORIZONTAL LEG BLEND OUT REPAIR AT STA XRS 179 REQUIRED EVALUATION. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-09, FIG 11.SDR MWEA96487Spar · corrodedDURING INSP, FOUND RT WING HAD EXFOLIATION CORROSION IN TWO PLACES ON FRONT SPAR FWD LOWER TANG AT STA XRS-167 AND XRS-200-210. COMPLETED REPAIRS IAW DAC TELEX DATED 6 AUG 96.SDR MWEA96486Spar Cap · corrosionDURING INSP, RT WING LOWER FWD FLANGE OF SPAR CAP WAS FOUND WITH SEVERE EXFOLIATION CORROSION FROM STA XRS 295 TO 324. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0630/RMK DATED 31 JULY 96.SDR MWEA96448Spar Cap · corrodedDURING INSPECTION, LT REAR SPAR CAP LOWER HORIZONTAL LEG WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. COMPLETED REPAIR IAW SRM 57-09, FIG. 11.SDR UPS96221088Stiffener · corrodedINSPECTION TYPE: C. CORROSION AT RWS 245.0 FRONT SPAR STIFFENER ON UPPER O/B END. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-10-01, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM'S 51-30-5, 51-30-2, MM 28-11-00.SDR P5CA9600700Spar Web · crackedCRACKED RIGHT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040.SDR P5CA9600699Spar Web · crackedCRACKED LEFT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040.SDR 96FDEA01448Spar Chord · corrodedNR 6047. RIGHT WING TOP TE PANEL OUTBOARD OF NR 5 SPOILER BULGING AT AFT SPAR STA XORS 782 - 827. SUBJECT CORROSION HAS BEEN REMOVED, AREA TREATED AND PAINTED PER 51-21-01.SDR 96FDEA01447Spar Chord · corrosionNR 5050 AND 505. LEFT WING REAR SPAR UPPER CHORD ANGLE AFT TANG BETWEEN STA XORS 670 TO 830 HAS NUMEROUS AREAS OF EXFOLIATION CORROSION. REMOVED CORROSION PER SRM 51-21-01.SDR TSAA9657068Spar · corrodedDURING HEAVY MAINTENANCE VISIT, RIGHT WING CORROSION NOTED ON BOTTOM SIDE OF LOWER CHORD OF FRONT SPAR, SS133 AND 145. REPAIRED PER ECO2135R1. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9657067Spar · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BULGE ALONG FRONT SPAR LOWER CHORD, SS 148 LEFT WING. REPAIRED PER ECO 2135R1. AIRCRAFT RETURNED TO SERVICE. (M)SDR 97ZZZM509Spar · corrodedWING STATION LEADING EDGE SPAR JUST FORWARD OF NR 2 SLAT ACT ROD HAS CORROSION AT 3 INCHES LONGERON. MECH REMOVED CORROSION AT WING STATION 616.5 LE SPAR IAW SRM 51-10-6. REMOVED AT .024 METAL 6 INCHES LONG ORIGINAL THICKNESS .225 MAX OUT ALLOWABLE .012 OUT SDR CA960910040Spar Cap · corroded(CAN) DURING CORROSION INSPECTION PER SB 190 (CAA AD 020-02-90) CORROSION WAS DETECTED ON FACE OF SPAR CAP LAMINATE. REPAIR SCHEME GIVEN BY FACTORY REP. DURING REPAIR, CORROSION FOUND BETWEEN LAMINATES EXTENDING PAST REPAIR SCHEME LIMITS. FINAL REPAIR ENTAILS SDR ABXA9700148Spar Cap · corrodedDURING C-CHECK, THE LEFT AND RIGHT WINGS REAR SPAR UPPER CAPS AT STATION XRS267 WERE FOUND CORRODED AT THE FLAP HINGE FITTING HOLES. THE SPAR CAPS WERE REPAIRED IAW REA D957-16147-MR.SDR 9619136615Spar Web · crackedDURING P-CHECK, FOUND CRACKS AND CORROSION IN THE RIGHT WING FRONT SPAR WEB AT THE UPPER CHORD FSSI 1087. REPAIRED PER EA 66-106376.SDR CKSA96118Vert Stiffener · corrodedDURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED APPROXIMATELY STATION XCW 29L. REPAIRED IAW DC8 SRM 57-2-0, 51-1-20 AND 51-1-8. TASK NR 80083, CORROSION CARD NR 2000-0551.SDR CKSA96117Spar Cap · corrodedDURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR LOWER CAP CORRODED AND CRACKED APPROXIMATELY STATION XCW 23L TO XCW 43L. REPAIRED IAW DC8 S/B 57-30R4 DRAWING NR SR08570012. TASK NR 80082, CORROSION CARD NR 2000-0551.SDR CKSA96116Angle · crackedDURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER LOWER ATTACH ANGLE CRACKED APPROXIMATELY STA XCW 35R. REPAIRED IAW DC8 DRAWING NR SR08570012. TASK NR 80081, CORROSION CARD NR 2000-0551.SDR CKSA96115Vert Stiffener · corrodedDURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED LOWER END APPROXIMATELY STA XCW 23R. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-8. TASK NR 80080, CORROSION CARD NR 2000-0551.SDR CKSA96114Spar · corrodedDURING C-2 CHECK, INSPECTION FOUND CENTER WING LOWER FRONT SPAR HAS HEAVY EXFOLIATION CORROSION FROM STATION XCW 17R TO XCW 405R AT PREVIOUS REPAIR. REPAIRED SPAR IAW DC8 S/B 57-30R4 AND DRAWING SR08570012. TASK NR 80079, CORROSION CARD NR 2000-0551.SDR 9621539756Spar · crackedDURING H-CHECK, FOUND A CRACK IN THE RIGHT WING REAR SPAR LOWER CAP AT XRS 164. REPAIRED CAP (P/N 5911301) PER EA 97-110758.SDR P5CA9600758Spar Chord · corrodedFOUND FRONT SPAR LOWER CHORD CORRODED IN CENTER TANK DRY BAY AT RBL 120. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 57-10-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.
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