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 1060106041ASpar Cap · corrodedCORROSION RIGHT SPAR CAP NEAR WS 124.588. FOUND DURING INSPECTION.SDR 06FDEA0653Spar Cap · corrodedLEFT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1044-1047. LEFT HAND WING REAR SPAR UPPER CAP CORROSION AT XORS 1044-1047 AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90754, TITLE: WINGS - LEFT HAND REAR SPAR UPPER CAP CORROSION AT STATIONS XORSSDR 1060106041Spar Cap · corrodedCORROSION LEFT MAIN SPAR CAP FWD FLANGE NEAR WS 124.588. FOUND DURING INSPECTION.SDR UPS06446378Spar · crackedINSPECTION TYPE:C RT WING FRONT SPAR WEB AT FSSI 688 FOUND 2EA FASTENER HOLES CRACKED, CRACK LENGTH .5 INCH & .125 INCH. RT WING FRONT SPAR WEB REPAIRED AS PER RS R57-21-35443 JUST BETWEEN FSSI 670 & FSSI 695 AND UPS EO B747-5720-23833-A.SDR CA060221001Spar · crackedDURING MAINTENANCE (WING REMOVAL) FRONT SPAR WEB FOUND CRACKED AT ROOT FITTING. ONCE DOUBLER WAS REMOVED, THE CRACK WAS FOUND TO HAVE BEEN STOP DRILLED.SDR UPS06846383Spar Cap · crackedINSPECTION TYPE:C2 LT WHEEL WELL LOWER SPAR CAP HAS A 16 INCH CRACK. REPAIRED LT LWR SPAR CAP FS 857 IAW SRO 8570009.SDR EIA2006025Spar · corrodedDURING B-CHECK, EXFOLIATION CORROSION ON LT WING FORWARD SPAR WEB AT LES 949 ON WEB AND STIFFENER. REMOVE DAMAGE, NDT AREA, FABRICATE AND INSTALL REPAIR PER ECRA 478-57-175-2.SDR EIA2006020Spar · crackedDURING B-CHECK, CRACK FOUND ON THE RT LWR FRONT SPAR CHORD FROM FSS 1387 - 1391 (LES 1422-1438). REMOVED AFFECTED AREA AND REPLACED WITH SPLICE. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST, WAITING FOR FINAL REPAIR INFORMATIONSDR UPS06846382Spar Cap · crackedINSPECTION TYPE:C2 RT WW LWR SPAR CAP CRACKED 1 INCH LONG RBL 30. REPAIRED LWR SPAR CAP STA 857 RBL 30 IAW SRO 8570009.SDR 06FDEA0537Spar · tool damageRT WING FRONT SPAR LOWER CHORD PLATE HAS A MISSED DRILLED HOLE LOCATED DIRECTLY BELOW THE NR 4 K-FLAP ACTUATOR. REPAIRED MISSDRILLED HOLE IAW FED EX EA 7-5710-96565.SDR CA060303002Spar · crackedCENTER SECTION FUSELAGE REAR WING CARRY-THRU SPAR CRACKED 3/4" FROM TOP OF SPAR RUNNING DOWNWARD AT EDGE OF REINFORCEMENT INSIDE FUSELAGE AT REAR LT FLOAT FITTING STATION NR 199.5 BULKHEAD NR 8.SDR CA060201001Spar · crackedA 100 HR INSPECTION WAS STARTED A CRACK WAS DISCOVERED AT THE RIGHT FRONT SPAROUT BOARD END WHERE IT ATTACHES TO THE SUB SPAR. THE CRACK IS VERTICAL RUNNING APPROXIMATELY 1 1/2 TO TWO INCHES IN LENGTH. THE CRACK STARTS AT THE TOP AND RUNS DOWN THROUGH A RIVESDR 06FDEA0404Spar · corrodedRT WING FRONT SPAR HAS AREAS OF CORROSION AT LES 340-345. REPAIRED PER FED EX EA 7-5710-96562.SDR EIA2006015Spar · corrodedLT WING FRONT SPAR LOWER SKIN EXTENSION FOUND CORRODED AT OLES 1354. BLEND OUT CORROSION, REPAIR FITTING AND PLUG INSTALLED PER SRM 57-30-03, FIG 4.SDR QXEA200600423Spar · corrodedPDX: LT WING FWD SPAR LWR FLANGE FRETTED AT APPROX STA YW 45.00 (INBOARD END OF LEADING EDGE 511AL). MAINTENANCE REPAIRED IAW Q400 SRM 51--21-00-350-801, NDTM PART 6, 51-00-02, SRM 51-21-10-380-801, HORIZON EA 6-57-430 AND RD 8/4-57-614.SDR QXEA200600422Spar · corrodedPDX: LT WING FWD SPAR TOP FLANGE HAS FRETTING AT APPROX YW 45.00. MAINTENANCE REPAIRED IAW Q400 SRM 51-21-00-350-801, NDTM PART 6, 51-00-02, SRM 51-21-10-380-801, HORIZON EA 6-57-430 AND RD 8/4-57-614.SDR 23JAN2006Spar · corrodedDURING MAINTENANCE, WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 5 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE RT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 359 TO 422. THE MEASURED COSDR AMTA200600045Spar · corrodedLT WING OVERWING IWS 241.08 TO 372.64 TE REAR SPAR DOUBLER IS RUSTY. CLEANED MINOR RUST CORROSION IAW SRM 51-10-02. CORROSION CLEANED ARE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW 51-50-01 FIG 01. CADMIUN PLATED CLEANUP AREA IAW LCCP 77-1237A. (M)SDR 06FDEA0195Spar Cap · corrodedLEFT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1044. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90724.SDR 06FDEA0194Spar Cap · corrodedRIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1045. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90728.SDR 06FDEA0193Spar Cap · corrodedRIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 683.4 AND XORS 700. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90727.SDR UPS06846196Spar Cap · crackedINSPECTION TYPE:C1, NDT FOUND CRACK APPROX 8" LONG ON LT LOWER SPAR CAP AT BL 47-55 ON HORIZONTAL LEG STA 857. REPAIRED LT LWR SPAR CAP STA 857 BL47-55 IAW SRO 8530009 AND EA 008-5710-01-A0039.SDR UPS06846105Spar · crackedINSPECTION TYPE:C1 3 POSSIBLE CRACKS ON FWD SIDE OF STA.680 BETWEEN FASTENERS COMMON LOWER SPAR AT RBL 13,18 AND 31. CUT OUT DAMAGED WEB. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS AND FINGER DOUBLER AT WEB STA. 680 IAW SRM 53-2-5 FIG 13, 51-1-21 AND SDR 06FDEA0093Spar Cap · damagedTWO (2) EACH FASTENER HOLE AT LOWER REAR SPAR CAP AT STA XORS 1062, FOUND ELONGATED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-94587.SDR 06FDEA0092Spar Cap · crackedRIGHT WING, LOWER REAR SPAR CAP AT STA XORS 1048 FOUND WITH APPROX 1.25 INCH CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-94587.SDR AMTA200600012Spar · crackedLEFT WING UPPER SKIN AT IWS 390 AFT OF REAR SPAR FOUND CRACKED. STOP DRILLED END OF CRACK IAW L1011 SRM 57-32-00 PAGE 822 FIG 811 CRACK UNDER 2 INCHES (1.87 INCHES). (M)SDR MJYA0601004Spar · corrodedWING CENTER SECTION REAR SPAR LOWER CHORD WAS REPAIRED DUE TO CORROSION.SDR EA01BQVA0106ASpar · corrodedDURING MAINTENANCE WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 8 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE LT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 340 TO 406. THE LARGEST PATCSDR EA0123JAN2006Spar · corrodedDURING MAINTENANCE WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 8 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE LT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 340 TO 406. THE LARGEST PATCSDR CA051230004Spar · crackedWING MAIN SPAR EXTRUSION CRACKED AT MAIN LANDING GEAR SIDESTAY SUPPORT BRACKETS, LT AND RT SIDES. CRACKS RUN SPANWISE IN FILLET RADIUS AND IN WEB. TWO CRACKS VISIBLE IN EACH SIDE, LONGEST CRACK IS ABOUT 1.25" LONG. CRACKS EXTEND THROUGH FULL THICKNESS OF THSDR DHL2006752503Spar · corrodedDISCREPANCY FOUND NR 110621; RT/WING AT WS 170 APPRX L/E CAVITY FRONT SPAR LWR CHORD HAS CORROSION. REMOVED CORR ON RT/WING LWR SPAR AT WS 170 ORIGINAL THICKNESS .413 MAT REMOVED .109 MATL REMAINING IS .304 AND IS OUT OF LIMITS IAW SRM 57-10-1 FIG2 FABBED DSDR 2005FA0001648Spar Cap · corrodedSEVERE INTERGRANULAR CORROSION OF MAIN WING SPAR WEB AND UPPER SPAR CAP AFT OF ENGINE FIREWALL. REQUIRES REMOVAL OF ENGINE, ENGINE MOUNT, FIREWALL. SUSPECT SOURCE OF CORROSION TO BE FIRE SHEATH INSTALLED OVER FUEL LINES BEHIND FIREWALL. SB 61 ADDRESSES INSPSDR UPS05845899Spar · crackedINSPECTION TYPE:SV LT WING REAR SPAR UPPER CAP AFT FLANGE IS CRACKED APPROX. 7".(XW736.5). REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 894-928513.SDR AU510002132Rivet · missingWING REAR SPAR ATTACHMENT PLATE RIVETS (7OFF) MISSING. INVESTIGATION CONTINUING.SDR AU510001979Spar · corrodedRT WING SPAR CHANNEL HEAVILY CORRODED IN AREAS ON THE MATING FACE BETWEEN THE CHANNEL AND THE SPAR ANGLE.SDR AU510001978Angle · corrodedRT WING SPAR ANGLE CONTAINED AREAS OF HEAVY CORROSION BETWEEN THE MATING FACES OF THE ANGLE AND SPAR CHANNEL AND THE ANGLE AND THE SPAR STRAP. CORROSION WAS MAINLY LOCATED IN THE AREA OF THE TANK BAY.SDR AU510001977Spar · corrodedRT WING SPAR STRAP CONTAINED AREAS OF HEAVY CORROSION BETWEEN THE MATING FACES OF THE SPAR ANGLE AND SPAR STRAP LOCATED MAINLY IN THE TANK BAY AREA.SDR AU510001777Spar · faultyLT AND RT WING REAR SPARS PNO 108-100000-23 (LT) AND P/N 108-100000-24 (RT) FAULTY. EVIDENCE OF WING MOVEMENT AT SKIN INTERSECTIONS ON TOP OF EACH WING.SDR CA051222004Spar · corrodedA/C IN FOR 5 YR WING BOLT REPLACEMENT AND MAIN SPAR LWR FITTING VISUAL INSPECT. LWR FWD LT WING BOLT DIFFICULT TO REMOVE AND UPON REMOVAL MODERATE CORROSION WAS OBSERVED IN BOLT BORES. LOOKING AT BOLT BORES FROM FRONT, GREATEST CORROSION APPEARED TO BE AFT ASDR AU510001580Frame · cracked(AUS) FUSELAGE FRAMES PN P1756-02/1 AND PN P1756-01/1 LOCATED IN WING FORWARD SPAR CARRY THROUGH SECTION CRACKED. FOUND DURING INSPECTION IAW AD. (CASA NR 510001580)SDR AUCR200500004Spar Cap · corrodedRT WING UPPER FORWARD SPAR CAP W.S.73 (PREVIOUS PROCESSING BY PARTY UNKNOWN) OF THE FORWARD FLANGE HAS EXCEEDED MAXIMUM NEGLIGIBLE LIMITS FOR DAMAGE LOCATION. DUE TO THE RELATIVE LOCATION OF THE WING ATTACH CORNER FITTING THIS DAMAGE CANNOT BE REPAIRED AND WILSDR AUCR200500003Spar Cap · corrodedRT WING REAR SPAR UPPER CAP WS178 AT NACELLE AFT ATTACH PLATE. DISSIMILAR METAL CORROSION ATTACKING UPPER CROWN AND AND VETICAL LEG OF THE SPAR CAP. CORROSION WAS VISUALLY DETECTED AT SCHEDULED DEPOT LEVEL INSPECTION. CORROSION EXCEEDED MAXIMUM NEGLIGIBLE LIMISDR AUCR200500002Spar Cap · corrodedLT WING UPPER REAR SPAR CAP WS178, AT NACELLE AFT ATTACH PLATE. DISSIMILAR METAL CORROSION ATTACK UPPER CROWN AND VERTICAL LEG. CORROSION WAS VISUALLY DETECTED AT DEPOT LEVEL SCHEDULED INSPECTION. CORROSION WAS FOUND TO EXCEED NEGLIGIBLE DAMAGE LIMITS.SDR 20051129Tube · crackedWING SPAR CARRY THRU P/N 295-030-401 IS CRACKED ON LT VERTICAL TUBE, TOP, FRONT SIDE.SDR MASA200500955Spar · cracked"MAJOR REPAIR TO RT WING LEADING EDGE SPAR OUTBOARD OF STN. YW423.0 PER REPAIR ORDER DHC82-57-1054." INSPECTION OF REMAINING SPAR FOR CRACKS AND SPLICING C/W. REMOVED AND REPLACED DAMAGED SPAR SECTION - OUTB’D OF APPROXIMATELY YW41 1.SDR USAA051409Spar · crackedLBL 135.5, 12 INCHES FWD FROM REAR SPAR CRACKED. MAJOR REPAIR, REMOVED DAMAGE, INSTALLED REPAIR TEE, FILLERS, AND VERT STIFFENER IAW EA 97047. DEFECT SIZE: 1.5 INCH.SDR SWIA200515945Spar · crackedRT WING; LOWER WING PLANK; REAR SPAR LOWER FLANGE IS CRACKED, WS 148.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV G & REO 601R-57-21-131 REV NC & RII 57-401.SDR 05FDEA03768Spar · crackedRT WING, TRAILING EDGE HAS A TWO INCH LONG CRACK IN FITTING AT XORS, 14 INCHES AFT OF INNER REAR SPAR. REMOVED AND REPLACED SUPPORT FITTING ARCO472-42, ( PO# 509448.1) IAW DC10-30 SRM 51-33-01 VOLII. TIMCO MECHANIC 7921, QC INSPECTOR #QC35.SDR DJFA2005163Spar · corrodedDURING AN UNSCHEDULED MAINTENANCE VISIT, WHILE INVESTIGATING A FUEL LEAK, CORROSION WAS DISCOVERED ON BOTH FORWARD AND BOTH AFT WING SPAR SPLICES ON THE UNDERSIDE OF THE WING DIRECTLY ABOVE THE SKID RAILS.SDR 2005UALA01247Spar · crackedLEFT WING FRONT SPAR IS CRACKED, PUNCTURED AT NR 1 LEADING EDGE SLAT, INBD AUX TRACK. DETERMINED SLAT SENSOR TARGET WAS PREVIOUSLY INSTALLED 180 DEGREES OUT, CAUSING DAMAGE. LEFT WING FRONT SPAR WAS FOUND CRACKED, PUNCTURED AT THE NR 1 LEADING EDGE SLAT, INB
Back to JASC 5711