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 UPS97823669Rib · crackedINSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 764. REPAIRED IAW SRM 57-2-0 AND 57-3-3.SDR UPS97823668Rib · crackedINSPECTION TYPE:D, L-WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 784. REPAIRED IAW SRM 57-2-0 AND 57-3-3.SDR UPS97823670Rib · crackedINSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 848. REPAIRED IAW SRM 57-2-0 AND 57-3-3.SDR 97ZZZX2902Spar · crackedWHILE C/W AMERICAN CHAMPION SL 406 RE: CRACKED SPARS. BOTH MAIN SPARS FOUND TO HAVE HAIRLINE CRACKS OPPOSITE THE UPPER INBOARD ATTACH BOLT FOLLOWING THE SPAR GRAIN. BOTH WINGS TO BE REPLACED WITH FACTORY NEW WINGS. 1974 CITABRIA 7GCBC 700 HRS TTSN. NEVER SDR 97ZZZX2901Spar · crackedWHILE C/W AMERICAN CHAMPION SL 406 RE: CRACKED SPARS. BOTH MAIN SPARS FOUND TO HAVE HAIRLINE CRACKS OPPOSITE THE UPPER INBOARD ATTACH BOLT FOLLOWING THE SPAR GRAIN. BOTH WINGS TO BE REPLACED WITH FACTORY NEW WINGS. 1974 CITABRIA 7GCBC 700 HRS TTSN. NEVER SDR MWEA97467Spar · crackedDURING C-CHECK, STA XRS164 LT WING REAR SPAR AFT FACE LWR TEE INBRD LWR BOLT HOLE CRACKED. MAINT REPAIR IAW ASB57-146R3 AND DAC DRWG J060271.SDR DLL13971184Spar Web · crackedTHE FS 1043, 1103 AND 1163 SPAR WEBS WERE FOUND TO BE MISSING A ROW OF ATTACH FASTENERS AT THE LBL AND RBL 116 END RIB ATTACH ANGLE. ONLY ONE ROW WAS INSTALLED SURING MANUFACTURE OF THE AIRCRAFT. SUBSEQUENT DYE PENETRANT INSPECTIONS REVEALED NUMEROUS CRACKS SDR DLL10971143Spar Cap · misdrilledTHE LT SPAR TO UPPER WEB ATTACH FASTENER HOLES WERE OVERSIZED AT TWO LOCATIONS. THE FIRST LOCATION IS AT APPRX. IWS 306. THE SECOND LOCATION IS AT APPROX IWS 378.SDR 9711726730Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB WS 1450 TO 1465. REPAIRED PER EA 67-150910.SDR CKSA97311Spar Cap · crackedDURING ACCOMPLISHMENT OF AD 90-16-05 SB 57-72 R-3, FOUND UPPER FRONT SPAR CAP FORWARD FLANGE RIGHT HAND WING HAS CRACKS OF 1 INCH LENGTH XFS 25, 1.75 INCH LENGTH XFS 40, .25 INCH LENGTH XFS 62.5 AND 1.5 INCH LENGTH XFS 67.500. UPPER CAP FORWARD FLANGE LEFT HASDR CKSA97310Spar Cap · crackedDURING ACCOMPLISHMENT OF AD 90-16-05 SB 57-30 R-4, FOUND LOWER FRONT SPAR CAP FORWARD FLANGE RIGHT HAND WING HAS TWO CRACKS OF .25 INCH LENGTH XFS 56 AND .125 INCH LENGHT XFS 58. COMPLIED WITH MODIFICATION OF LEFT HAND AND RIGHT HAND LOWER INBOARD FRONT SPAR SDR 97FDEA00332Spar · damagedDOUBLER AT LT WING TO CENTER SECTION AT FRONT SPAR HAS DEEP GOUGE CAUSED FROM WING/FUSELAGE FILLET RUBBING DOUBLER (AND 7309 SPLICE PLATE AT SCW = 118.20). BURNISHED GOUGE ON FRONT SPAR ANGLE AND WING DOUBLER. MEASURED GROOVE, DEPTH .020. REPAIRED AS PER EASDR 9711679156Spar · corrodedDURING L-CHECK, FOUND CORROSION ON RIGHT WING AFT SPAR AT APPROXIMATELY 24 INBOARD OF WING TIP. REPAIRED PER EA 91-112950.SDR P5CA9701096Spar Chord · crackedFRONT SPAR LOWER CHORD CRACKS AT FSSO 1440 AND 1425 RHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTIONS WITH NEW CHORD SECTIONS AND SPLICE STRAPS AT FSSO 1395 RHS PER RS NR 57-21-33404.SDR P5CA9701095Spar Chord · crackedFRONT SPAR LOWER CHORD CRACKS AT FSSO 1446 LHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTION WITH NEW CHORD SECTION AND SPLICE STRAP AT FSSO 1425 LHS AS PER RS NR R-57-21-33403.SDR 97ZZZX2813Spar · erodedAFTER DISASSEMBLING AIRCRAFT FOR REFURBISHMENT, RT WING MAIN SPAR ATTACH FITTING WAS FOUND ERODED. ADDITIONAL SIGNS OF FRETTING AND EROSION WERE DETECTED AT THE LOWER END OF THE LIFT STRUT. ALL WEAR WAS INDICATIVE OF A LIMITED FORE AND AFT 'SWING' OF THE ENTSDR IXXA9700113Spar Cap · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT WING UPPER AUXILIARY SPAR CAP WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP, FABRICATION AND INSTALLATION OF NEW SPAR CAP IN ACCORDANCE WITH DER APPROVED DRAWING 853-239-97, DOUGLAS AIRCRAFT DRAWING SDR ABXA9701372Spar Cap · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT WING UPPER FRONT SPAR CAP CORRODED AT XOS240. REPAIRED FRONT SPAR UPPER CAP IAW ABX REA D957-19643.SDR CALA9701038Spar · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING FRONT SPAR UPPER CHORD AT STA 335. THE CRACKED SECTION WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5710-01819 AND SRM 57-10-6.SDR AU970607Web · cracked(AUS) LH WING LOWER SPAR WEB ANGLE CRACKED IN THREE PLACES - CRACK LENGTHS 53.34MM (2.1IN), 66.04MM (2.6IN) AND 44.45MM (1.75IN) - FOUND FOLLOWING SPAR CAP REMOVAL FOR INSPECTION IAW SB-AG-39SDR AU970605Web · cracked(AUS) RH WING INBOARD SPAR LOWER WEB ANGLE CRACKED THROUGH RIVET HOLE - CRACK LENGTH 91.44MM (3.6IN) - ANOTHER CRACK FOUND ON UPPER WEB ANGLE - CRACK LENGTH 22.85MM (0.9IN) - FOUND DURING REMOVAL OF SPAR CAPS FOR INSPECTION IAW SB-AG-39SDR 9711739607Spar · corrodedDURING L-CHECK, FOUND CORROSION LOWER SPAR CAP LOWER AFT FLANGE AT WS 160. REPAIRED PER EA 96-112953.SDR AU970598Web · cracked(AUS) RH WING SPAR INBOARD WEB CRACKED - FOUND FOLLOWING REMOVAL OF SPAR CAPS FOR INSPECTION IAW SB-AG-39SDR 97ZZZX3405Spar · corrodedFOUND ON ANNUAL INSPECTION, INTERGRANULAR CORROSION ON CARRY-THROUGH SPAR. SOME SPOTS 2 INCHES AND .0625 INCH DEEP, PLUS OTHER CORROSION. SUBMITTER STATED THIS IS HARD TO SEE WITHOUT REMOVING HEADLINER.SDR P5CA9701088Spar · crackedLHW FRONT SPAR LOWER CHORD CRACK FOUND 9 INCHES LONG AT OLES 1440, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.SDR P5CA9701087Spar · crackedRHW FRONT SPAR LWR CHORD CRACK FOUND 2 INCH LONG AT OLES 1430, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.SDR 97ZZZX2716Spar · crackedINSPECTED SPAR IAW SL 406. FOUND RIGHT FORWARD SPAR CRACKED OUTBOARD, AFT SIDE OF STRUT ATTACH DOUBLER. CRACK VERY DIFFICULT TO SEE WITHOUT BENDING LEADING EDGE ALUMINUM UP TO GET A CLEAR VIEW OF TOP OF SPAR. THIS CRACK COULD NOT BE SEEN FROM BOTTOM OF WING SDR MWEA97429Spar Cap · corrodedDURING D-CHECK, XRS 426 TO 431 LT WING AFT SPAR LWR CAP, AFT TANG CORRODED. MAINT REPAIRED IAW SRM 57-09 PG 47.SDR MWEA97416Spar Strap · misrepairedDURING D-CHECK, XRS 445 LT WING FWD SPAR IMPROPER PREVIOUS REPAIR. MAINT REMOVED AND REPLACED IAW DAC DRWG 591938 AND SRM 51-30-5.SDR P5CA9700541Spar · corrodedLEVEL 1 LT WING L/E SPAR LOWER CHORD CAP HAS LIGHT CORROSION. REMOVED CORROSION WITHIN LIMITS. ALODINED AND PRIMED PER BOEING SRM 57-30-01.SDR 9710941154Spar · corrodedDURING L-CHECK, FOUND CORROSION ON UPPER T-CHORD OF AFT SPAR FROM XORS 1077 TO 1086. REPAIRED PER EA 11-150360.SDR MWEA97409Spar Tang · corrodedDURING D CHECK, STA 240-257 RT WING FWD LWR SPAR TANG IMPROPER PREV BLEND OUT. MAINTENANCE REPAIRED IAW TELEX SVC-MSP-0433/JLW.SDR MWEA97390Spar Tang · corrodedPREV REPAIR ON LT WING LEADING EDGE LOWER FWD SPAR TANG BETWEEN XRS164 AND XRS 189 CORROSION AT XRS 353. REMOVED AND REPLACED IAW TELEX SVC MSP 0387 KJC.SDR DLL10970990Spar Web · crackedWHILE ACCOMPLISHING DAL SPECIAL INSP 7-55740-12AD, REAR SPAR WEB INSPECTION FOR FATIGUE CRACKS, ONE FASTENER HOLE WAS OVERSIZED BEYOND THE MAX LIMITS DICTATED ON LAC DWG 1642705 REVISION E. THE HOLE, WAS PREVIOUSLY OVERSIZED AT LAST INSP TO REMOVE CRACKS TO A SDR P5CA9700992Spar Strap · crackedLT WING UPPER SURFACE FRONT SPAR UPPER STRAP CRACKED AT WS 485. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9700991Spar Strap · crackedLT WING UPPER SURFACE FRONT SPAR UPPER STRAP CRACKED AT WS 840. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9700832Spar Strap · corrodedLEVEL 1 CORROSION LT WING UPPER SURFACE FRONT SPAR UPPER STRAP BULGED UP AT WS 1454. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700831Spar Strap · corrodedLEVEL 1 LT WING UPPER SURFACE FRONT SPAR UPPER STRAP BULGED UP AT WS 485. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700830Spar Strap · shearedLT WING UPPER SURFACE FRONT SPAR UPPER STRAP ATT RIVETS (1 EA) SHEARED AT WS 450. REPLACED PER BOEING SRM 51-30-02.SDR P5CA9700829Spar Chord · corrodedLEVEL 1 LT WING UPPER SURFACE FRONT SPAR UPPER CHORD STRAP BULGED UP AT WS 395. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR DHL9770256DSpar Web · cutAT D-CHECK, CUT BS 740 ACCESS HOLE IN FRONT SPAR WEB FOR REMOVAL AND REPLACEMENT OF TERMINAL FITTING PER BOEING TELEX. REMOVED STIFFENERS AND FASTENERS, ACCOMP VISUAL AND HFEC INSP, CUT OUT WEB AT STA 740 RBL 13 TO 36 AND FROM 194.35 TO WL 181.35 PER BOEING TSDR 97FDEA00291Spar Chord · corrosionCORROSION (C53-132-02,1) ON UPPER REAR SPAR CHORD STA 870, RBL 65, LBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER SPAR CHORD STA 870, RBL 65, LBL 65, WL 178 PER FED-EX NR 7-5710-34044.SDR 97FDEA00290Spar Chord · corrodedNR 0476 016, CORROSION (SPEC C53-132-02,1) ON STA 870 LOWER REAR SPAR CHORD RBL 25, LBL 25, WL 138. *S/D* REMOVED DAMAGED LOWER REAR SPAR CHORD FROM RBL 70 TO LBL 70, WL 138, BS 870 AND INSTALLED NEW LOWER CHORD PER FED-EX EA 7-5710-34044.SDR AALA970928Spar · corrodedTUL - CORROSION ON LOWER FWD LEFT WING SPAN CHORD EXTENSION. REMOVED CORROSION, TREATED AREA, AND INSTALLED REPAIR STRAP PER SRM 57-30-00-2 FIG 1. TST: 55,741 HOURS. CYCLES, 34,503. (X)SDR TSAA9757126Spar Web · crackedDISCREPANCIES FOUND DURING C AND CP1 VISIT, CRACK IN WING CENTER SECTION FRONT SPAR WEB AT RBL 44. REPAIRED CRACKED CENTER SECTION FRONT SPAR AS FOLLOWS 1) CUTOUT CRACKED PORTION OF WEB. (2) CONFIRM CRACK REMOVAL BY HFEC INSPECTION. 3) FABRICATED 2024T3 .06SDR AU970615Stiffener · corroded(AUS) LH WING SPAR FORWARD STIFFENER PLATE AND SPAR TOP PLATE CONTAINED EXFOLIATION CORROSIONSDR 97ZZZX2350Spar · rivets workingRT WING, SPAR, LOWER, FORWARD, INBOARD - FOUND SEVERAL WORKING RIVETS WITH HEAVY BLACK STREAKING AFT OF THE RIVET HEADS. FURTHER INSPECTION REVEALED LEADING EDGE HINGE PIN SEVERELY WORN. REQUIRES REPLACEMENT OF SPAR ASSY AND LEADING EDGE HARDWARE ASSY. SUSPSDR AU970468Spar Cap · cracked(AUS) RH WING LOWER FORWARD SPAR CAP CRACKED FROM 6.35MM (0.25IN) HOLE- ONE CRACK 3.098MM (0.122IN) EXTENDED FORWARD AND ONE CRACK0.508MM (0.020IN) EXTENDED REARWARD - FOUND DURING MAGNETIC PARTICLE INSPECTION - SEE MDR 97/0459 FOR FURTHER INFORMATIONSDR AU970467Spar Cap · cracked(AUS) LH WING LOWER SPAR CAP CRACKED FROM 6.35MM (0.25IN) HOLE - ONECRACK 12.395MM (0.488IN) EXTENDS FORWARD AND ONE CRACK 7.975MM(0.314IN) EXTENDS REARWARDS - FOUND DURING MAGNETIC PARTICLE INSPECTION - SEE MDR 97/0447 FOR ADDITIONAL INFORMATIONSDR AU970459Spar Cap · cracked(AUS) RH WING LOWER SPAR CAP CONTAINED TWO CRACKS FROM 6.35MM (0.25IN)BOLT HOLE - ONE CRACK EXTENDS 3.048MM (0.120IN) FORWARD FROM THE HOLE AND ONE CRACK EXTENDS 0.508MM (0.020IN) REARWARDS - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW SB-AG-39
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