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 FDEA200906272351Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP OTBD OF NR 5 SPOILER PANEL INBD AROUND XORS 799. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272350Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP FWD OF NR5 SPOILER PANEL INBD AREA BETWEEN XORS 714 TO 738. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272335Spar · damagedRT WING T/E FALSE SPAR INBD REPAIR HAS LOOSE FASTENER IN THE UPPER SECTION WBL 118. FABRICATED REPAIR PARTS , NEW LOWER CHORD, ANGLE REPAIR , HEAT TREATED 7075 'O' TO T6 CONDITION IAW FAS ER 2-37153-801 REV A, NEW STRAP, TWO RADIUS FILLERS & NEW DOUBLER SDR FDEA200906272328Spar · corrodedEXFOLIATION CORROSION ON LT WING REAR SPAR WEB BETWEEN WS 150.5 TO WS 177.5 AT BOOST PUMP LWR MATING SURFACE. REPAIR CARRIED OUT ON LT WING REAR SPAR IAW EA F-5700-129607. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100.SDR FDEA200906262320Spar · crackedCRACK ANGLE LT WING FALSE SPAR AT NR 7 SPOILER ATTACH FITTING. CUT ANGLE AT LT WING FALSE SPAR IAW FX DWG SR 27-57-038 REV C. FABRICATED 2 ANGLES. HEAT TREATED ANGLES FROM 'O' TO T6 IAW FAS ENG REPORT NR 2-37153-801 REV A, FABRICATED DOUBLER, WEB, LOWER ANGSDR CA090626004Spar · cracked(CAN) DURING A 100 HR INSP, (3) CRACKS WERE VISUALLY FOUND IN THE AFT WING SPAR AFT UPPER RADIUS BETWEEN THE LT AND RT IB SEAT TRACKS. ON FURTHER INSP WITH EDDY CURRENT, IT WAS FOUND THAT FWD UPPER RADIUS OF AFT SPAR WAS CRACKED BETWEEN THE LT AND RT IB SEAT SDR 2009FA0000554Spar Cap · damagedLT WING AFT TRUSS PLATE ATTACH HOLES ARE DRILLED TO LARGE IN TRUSS PLATE AND IN AFT SPAR CAP AT WING STATION 102.1. DETERMINED TO HAVE OCCURRED DURING PRODUCTION. OBTAINED DER APPROVAL FOR DISPOSITION.SDR 2009FA0000546Spar Cap · damagedRT WING FWD SPAR CAP HAS A DOUBLE HOLE UNDER THE INBD ENGINE MOUNT SUPPORT. SUSPECT MIS-DRILLED DURING PRODUCTION. ENGINEERING DISPOSITION OBTAINED FOR REPAIR OF ELONGATED HOLE AREA.SDR DLM88091265Spar · crackedCRACK ON RT WING REAR SPAR STA XW=160 NEAR OUTBOARD FLAP INBOARD HINGE RT WING. CRACK WAS CUT OUT IAW ERA 475563-14 REV ORIG. REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ERA 475563-14 REV ORIG.SDR USAA2009071791870Spar · crackedSAL - Q3 - MAJOR REPAIR - CRACK ON LEFT WING REAR SPAR UPPER CHORD AT RSS224.14, WBL 157. REPAIRED LEFT WING REAR SPAR UPPER CHORD AT RSS224.14, WBL 157 IAW US AIRWAY EA 132503.SDR GUUA93757061709DSpar · corrodedDURING SCHEDULED INSP DISCOVERED LT WING FWD SPAR AFT FLANGE AREA 3 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA93757061709CSpar · corrodedDURING SCHEDULE INSP DISCOVERED LT WING FWD FRONT SPAR AREA 2 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA93757061709BSpar · corrodedDURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 FWD SPAR AFT FLANGE HAS CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.SDR SWAA093921Spar · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING FWD SPAR LOWER CHORD CRACKED AT NR 2 PYLON RT SKATE ANGLE, FWD FASTENER HOLE. REPAIRED SPAR PER SWA EA.SDR HALA2009061100031Spar · corrodedMODERATE CORROSION ON THE LT WING REAR SPAR LWR TANG AT ARS 164 (AREA I/B FLAP ACT FITTING). ACCOMPLISHED PERMANENT REPAIR AS PER MESSAGE HWI 09-0047-08B AND DWG NR J060271.SDR FDEA200905211762Spar · crackedCRACK ANGLE FALSE SPAR LT WING STA 244 AT NR 7 SPOILER ACTUATOR BRACKET. REMOVED DOUBLER AND WEB SECTION. CUT OUT DAMAGED ANGLE SECTION IAW DWG NR SR27-57-038 REV C. INSTALLED ALL PARTS IAW DRW NR SR27-57-038 REV. C.SDR AALA20090521TUL11Spar · corrodedRIGHT WING REAR SPAR CORRODED UNDER UPPER AND LOWER BONDING STRAPS FOR NUMBER TWO TANK AFT BOOST PUMP. CORROSION REMOVED PER EA B737-57-006285.SDR AALA20090521TUL10Spar · corrodedLEFT WING REAR SPAR CORRODED UNDER LOWER BONDING STRAP FOR NUMBER ONE FUEL TANK BOOST PUMP. CORROSION REMOVED PER EA B737-57-006285.SDR FDEA200905171701Spar · crackedLT WING FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. CUTOUT SECTION, FABRICATED NEW SECTION, FABRICATED WEB, FABRICATED 2 ANGLES, HEAT TREAT ANGLES IAW FASI ER 2-32153-801 REV. A, FABRICATED STRAP, 2 RADIUS FILLERS, LOCATED AND DRILLED NEW PARTS, ALODINED ANSDR 2009FA0000500Spar · crackedON 5/15/2009, DURING AN ANNUAL INSPECTION IT WAS NOTED THERE IS A COMPRESSION CRACK AT REAR STRUT ATTACH POINT TOP SIDE OF SPAR AT END OF DOUBLER. WHING TIP IMPACKED GROUND DURING A WIND STORM. (K)SDR FDEA200905091596Spar · corrodedLT LWR FWD CTR TANK SPAR CORRODED AT STA 744 LBL 20 TO LBL 30. DISPLACED SEAL AT BS 740, OPENED FUEL PANELS NR 7540 AND 7340 FOR ACCESS IAW SRM 51-30-2, MM 51-30-011-4 AND 28-11-021-4, REMOVED SEAL RETAINER , CORNER FITTINGS AND PANELS NR 3445, 6402R AND 630SDR 2009FA0000423Spar · separatedTHIS IS AN EXPERIMENTAL ACFT. INVESTIGATION REVEALED THAT IT APPEARS THE LT REAR WING SPAR SEPARATED AT THE WING, CAUSING THE LT WING TO FAIL. FURTHER EXAMINATION OF WOOD (DOUGLAS FIR ACCORDING TO THE AIRCRAFT RECORDS)USED IN THE CONSTRUCTION OF THE SPAR RETRISDR 22AA20090505Spar · crackedON PRE FLIGHT FOUND FUEL LEAK BY LEFT WING ROOT FORWARD OF WHEEL WELL. UPON FURTHER INVESTIGATION THE LEFT REAR SPAR WAS FOUND CRACKED.SDR FDEA200905091590Spar · crackedRIGHT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT. WING T/E FALSE SPAR LOWER CHORD IAW DRAWING SR27-57-038 REV. C (STD REWORK DRAWING INBD SPOILER SUPT. BEAM CRACK REPAIR).SDR FDEA200905091588Spar · crackedLEFT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT WING T/E FALSE SPAR LOWER CHORD ANGLE IAW DRAWING SR27-57-038 REV C.SDR FDEA200905041499Frame · crackedFOUND CRACK ON C 45 RT IN AREA 1(SEE EO 6-5310-7-5015 PT1), CENTER WING SECTION. REPAIR PERFORMED BY NDT FOR FURTHER CRACKS AND ACCOMPLISHMENT OF REPAIR IAW EO 6-5310-7-5015 PT 2, APPROVED BY RAS 70519824/005/2009 ISS A AND EA 6-5710-129119.SDR FDEA200904281460Spar · crackedRIGHT WING T/E FALSE SPAR CHORD ANGLE CRACKED. REMOVED & REINSTALLED TORQUE BOX FITTING TO ACCESS WEB, CUT-OUT DAMAGED AREA. FABRICATED NEW WEB, FABRICTATED NEW CHORD SECTION, FABRICATED 2 ANGLES, FABRICATED 2 RADIUS FILLER, AND FABRICATED NEW DOUBLER. HEATSDR FDEA200904271445Spar · crackedLT WING T/E FALSE SPAR LOWER CHORD ANGLE CRACKED, WBL 118. REMOVED DAMAGED SECTION OF FALSE SPAR IAW DWG SR27-57-038. FABRICATED NEW SPAR SECTION, WEB, 2 SUPPORT ANGLES, STRAP, DOUBLER, ALL IAW DWG SR 27-57-038 REV. C. INSTALLED ALL REPAIR PARTS IAW SR 27-57SDR GUUA93957042209ASpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION AT RT FWD SPAR FLANGE JUST BEHIND DRAIN PLUG WS 126.5. BLENDED OUT CORROSION AT RT FWD MAIN SPAR FLANGE JUST BEHIND DRAIN PLUG.SDR GUUA93957042109ASpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT WING FWD SPAR FLANGE WS 125.25. REMOVED SURFACE CORROSION AT LEFT WING FORWARD SPAR WS 125.25 AND INSTALLED REPAIR DOUBLER STRAP.SDR FDEA200904211368Spar · damagedCENTER WING BOX REAR SPAR FR 47 OVERSIZED HOLES. COMPLIED WITH EA 6-5710-127940.SDR DHLA2009801005Spar Cap · crackedLT LWR WING FRONT SPAR CAP AT L/E ATTACH HOLE SHOWS A 0.500 INCH LENGTH CRACK, STA XFE 523.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-7-09, EVA D857-00261 REV IA DATED 04-27-09, REPAIR SKETCH 200904200125 DWG J060232, JCT04316 REMSDR FDEA200904091244Spar · crackedRT WING T/E FALSE SPAR LOWER CHORD ANGLE CRACKED WBL 118 REPAIRED RT WING T/E SPAR LOWER CHORD ANGLE IAW FEDEX DRAWING SR27-57-038 REV C, STD REWORK DRAWING INBD SPOILER SUPPORT BEAM CRACK REPAIR.SDR MZZA2009041000049Spar · corrodedLEFT WING CENTER SECTION CORROSION FOUND UNDER DRAG BRACE BETWEEN SL20 AND SL21 AT STA 540 (WBL 52). REPAIR CARRIED OUT IAW EC/RA 5710-02160, PART 1-INTERIM REPAIR.SDR MZZA2009041000047Spar · corrodedRIGHT WING CENTER SECTION CORROSION FOUND UNDER DRAG BRACE BETWEEN SR20 AND SR21 AT STA 540 (WBL52). REPAIR CARRIED OUT IAW EC/RA 5710-02160, PART 1-INTERIM REPAIR.SDR FDEA200904091233Rib · chafedFOUND OLD DRILLING MARKS IN RT WING REAR SPAR RIBS IN THE TRAILING EDGE AREA. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009148/2009 ISS A, APPROVED BY EA 6-5710-129140.SDR CA090504008Spar · corroded(CAN) CORROSION FOUND, CENTER WING, MAIN SPAR, FWD FLANGE APRROX LBL 16 TO RBL 16. DURING SCHEDULED STRUCTURAL INSP, FOUND CORROSION BUBBLING UP FROM UNDER PRC COATING THAT COVERS THE SPAR CAP CORNER RADIUS. REMOVAL OF THE PRC FOUND PITTED CORROSION ON THE SPSDR CA090402002Spar · corroded(CAN) WHILE PERFORMING C1 CHECK ON THE AIRPLANE ,VISUAL INSP DISCLOSED SEVERE CORROSION AT THE LWR SECTION OF THE FRONT SPAR AT STATION 120 AND 175 JUST BELOW THE NACELLE. WAITING E/O TO COMPLETE THE JOB.SDR AALA20090406TUL03Spar · corrodedLEFT WING REAR SPAR CORRODED. REPAIRED IAW EA B757-57-005721.SDR CA090302006Adapter · corroded(CAN) DURING INSP THE REAR SPAR ADAPTER WAS FOUND HEAVILY CORRODED. MORE INFO TO FOLLOW.SDR QXEA2009030500163Spar · corrodedPDX - C1 - FWD SPAR ATTACH FLANGE FOR PANELS 261CT AND 261LT HAS FRETTING ON OTBD ENDS. BLENDED FRETTING AT FWD SPAR ATTACH FLANGE FOR PANELS 261CT AND 261LT. REF RD 8/4-53-451 GENERAL NOTES STEP 1. HFEC INSP BLENDS FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01SDR QXEA2009030300146Spar · corrodedPDX - C1 - TURTLE BACK PNL AFT SPAR ATTACH FLANGE HAS FRETTING ALONG ITS ENTIRE LENGTH. REPAIRED AFT TURTLEBACK PANEL, AFT SPAR ATTACH FLANGE ALONG ENTIRE LENGTH BY BLENDING IAW RD 8/4-53-451. MEASURED THICKNESS AND FOUND LOWEST POINT TO BE .90, FOUND FLANGESDR FDEA200903020788Spar · looseNR 8 RIGHT WING FALSE SPAR LOWER CHORD ABOVE MLG HAS LOOSE FASTENERS AND FOUND CRACKED. REPAIRED IAW STANDARD REPAIR DRAWING SR27-57-038 REV. C.SDR IPXA09654975Bracket · crackedINSPECTION TYPE:C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (CRACK 1.125 INCH LENGTH). RT WING LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40SDR IPXA09654974Bracket · crackedINSPECTION TYPE:C LT WING - L/E LES 580 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (CRACK 1.75 INCH LENGTH). LT WING LES 580 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-SDR EIAA20090036Spar · corrodedRT WING REAR SPAR UPPER SURFACE HAS CORROSION FROM WS 565 TO 575. REPAIRED PER 742-EO-53-2848. FAA APPROVAL THROUGH FAA FORM 8100-9 ISSUED BY BOEING.SDR GUUA95157022009ESpar · corrodedDURING SCHEDULED INSP, DISCOVERED CORROSION ON RT WING J STRINGER FWD FLANGE AND RT FWD SPAR, FD FLANGE BETWEEN WS 124.58 TO 135.86. CLEANED CORROSION SPOT ALLOWABLE DAMAGE WITHIN LIMITS ALSO CLEANED AND TREATED AND PRIMED SURFACE AREA AT RIGHT WING J STRINGESDR GUUA95157022009DSpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON RT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND K STRINGER FWD FLANGE BETWEEN WS 114.25 TO 124.25. CLEANED CORROSION AT RIGHT FORWARD AFT FLANGE MATERIAL LOSS IS STILL ABOVE DESIGN MINIMUM STRENGTH.CLEANED CSDR GUUA95157022009CSpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING FWD SPAR FWD FLANGE AND J STRINGER FWD FLANGE BETWEEN WS 124.58 TO 135.86. REMOVED CORROSION AND INSTALLED FILLER AND REPAIR DOUBLER ON LEFT FORWARD SPAR FORWARD FLANGE AND INSTALLED EXTERNAL STRAP ON J STSDR GUUA95157022009ASpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND J STRINGER AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION INSTALLED INTERNAL STRAP ON LEFT FORWARD SPAR FLANGE AND EXTERNAL STRAP ON J STRINGER.
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