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 EE4Y2019100109886Spar · crackedRH WING RSS 224.14 REAR SPAR UPPER CHORD OPEN FASTENER HOLE CRACKED. NOTE: REAR SPAR UPPER CHORD WAS REPAIRED AS PER SRM 57-20-10 REPAIR 4 INSTRUCTIONS.SDR SIMA20190928007Attach Fitting · crackedL/H ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP.-C/A-REMOVED, REPAIRED, AND REINSTALLED L/H WINGTIP IAW ERJ-175 AMM 57-30-00 AND ERS-EJ-57MR-1151 PART A; BONDING CHECKS GOOD, AND OPERATIONAL CHECKS OF LIGHTS GOOD. 3EA STATIC DISCHARGERSDR SCNA2019100194178Spar · cracked11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDITSDR FDEA201909202783Spar Cap · corrodedLEFT WING REAR SPAR UPPER CAP. SHOWING LIGHT SURFACE CORROSION ON CAP SURFACE. FROM APPROX. WING STA. XORS1050 - XORS1060 AREA MARKED DOT 60 REPAIRED PER EA 1-5710-T0350190 WING- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK.SDR R61A2019100598186Spar · cracked***AIRCRAFT IS IN HEAVY CHECK***R/H WING TIP ASSY SPAR 1 FOUND CRACKED. REPLACED R/H WING TIP ASSY IAW AMM 57-30-00-000-801-A.***AIRCRAFT REMAINS IN HEAVY CHECK***SDR R61A2019100591885Spar · cracked***AIRCRAFT IS IN HEAVY CHECK***L/H WING TIP ASSY SPAR 1 FOUND CRACKED. REPLACED WING TIP ASSY IAW AMM 57-30-00-000-801-A.***AIRCRAFT REMAINS IN HEAVY CHECK***SDR 9WGA2019091809Spar · corrodedRT WING OUTBOARD AFT TRAILING EDGE SPAR CORROSION PULLING THRU FASTENERS STA. XORS 433.00- XORS 418.60. NON-ROUTINES 1573, 1574.SDR FDEA2019101762676Former · crackedLEFT WING - FORWARD SPAR - SUPPORTING STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). STOP DRILLED CRACK AND INSTALLED A .090 REPAIR DOUBLER IAW SRM 57-00-00 FIG 209 SHEET 1.SDR SIMA20190914006Attach Fitting · crackedRT ENHANCED WING TIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-PERFORMED REPAIR OF RT ENHANCED WING TIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151.SDR SIMA20190914005Attach Fitting · crackedLT ENHANCED WING TIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-REMOVED AND REPLACED LT ENHANCED WING TIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151. SEE TURNOVER FOR DETAILS.SDR CALA2019091701550Spar Web · corroded@ WING STA 675 CORROSION ON AFT SPAR WEB. CORROSION MEASURES AT 1" WIDE X .25" TALL. LOCATED AT UPPER EDGE OF WEB. ADJACENT TO NEAREST FASTENER OF WEB ADJACENT TO NEAREST FASTENER. CORROSION MEASURES AT 1" WIDE X .25" TALL. LOCATED AT UPPER EDGE REMOVED CORROSSDR CALA2019091701549Spar Web · corroded@ WING STA 687, CORROSION ON AFT SPAR WEB. (MKD) CORROSION MEASURES AT .375" WIDE X .5" TALL. 1.25" FROM LOWER EDGE OF WEB. ADJACENT TO NEAREST FASTENER AND TO STIFFENER ANGLE. SUBMIT FOR ENGENEERING PER THEIR REQUEST. CORROSION SHOWING. REF SRM 57-20-10. DOCUSDR CALA2019091701548Spar Web · corroded@ WING STA 713, CORROSION ON AFT SPAR WEB. CORROSION MEASURES .75" WIDE X .5" TALL. 1.5" FROM UPPER EDGE OF WEB. .25" FROM NEAREST FASTENER. CORROSION SHOWING. REF SRM 57-20-10. DOCUMENTED DIMENSIONS TO SUBMIT FOR ENGENEERING PER THEIR REQUEST. REMOVED CORROSISDR IPXA2019091846944Stiffener · crackedINSPECTION TYPE:4C RT WING FIXED L/E RIB (STIFFENER) IS CRACKED O/B OF SLAT ACTUATOR ACCESS PANEL 618FB. REMOVED AND REPLACED CRACKED RT WING FIXED L/E RIB (STIFFENER) O/B OF SLAT ACTUATOR ACCESS PANEL 618FB IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2019091846943Stiffener · crackedINSPECTION TYPE:4C LT WING FIXED L/E RIB (STIFFENER) IS CRACKED O/B OF SLAT ACTUATOR ACCESS PANEL 518FB. REMOVED AND REPLACED CRACKED LT WING FIXED L/E RIB (STIFFENER) O/B OF SLAT ACTUATOR ACCESS PANEL 518FB IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR ABXR201909050313Attach Angle · corrodedPANEL ATTACH ANGLE AT LEFT WING LOWER SPAR WAS CORRODED AT WS 460. REPAIRED PER 47385REA01.SDR SIMA20190905003Attach Fitting · crackedRT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-REMOVED AND REPLACED RT ENHANCED WINGTIP SPAR1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 PART B.SDR SIMA20190905002Attach Fitting · crackedLT ENHACED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-REMOVED AND REPLACED LT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 PART A.SDR SWAA2022031841507Web · corrodedLEFT WING FORWARD SPAR IS CORRODED AT BONDING STRAP LOCATION FOR NUMBER 1 FUEL FWD BOOST PUMP. / REMOVED CORROSION ON LH WING FWD SPAR WEB AT THE BONDING STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; ORIGINAL .485' LOSS .126' REMIANING .SDR SWAA2022031841437Spar · corrodedLEFT WING REAR SPAR BOOST PUMP TANK 1 AFT HAS CORROSION AT UPPER BONDING JUMPER IFSS 145 8.5' FROM UPPER CHORD / REMOVED CORROSION ON L/H WING REAR SPAR BOOST PUMP AT UPPER BONDING JUMPER ATTACH POINT IFSS 145 IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; SDR SWAA2022031841438Spar · corrodedLEFT WING REAR SPAR BOOST PUMP TANK 1 AFT HAS CORROSION AT LOWER BONDING JUMPER IFSS 145 8.5' FROM LOWER CHORD / REMOVED CORROSION ON L/H WING REAR SPAR BOOST PUMP AT LOWER BONDING JUMPER ATTACH POINT IFSS 145 IAW SRM 51-10-02-0G-0. VERFIED ALLOWBLE LIMITS; ORSDR HALA2019090600376Spar · corrodedLEFT WING REAR SPAR LOWER TANG SERVERE CORROSION STATION 360 - 366 (M) O/B OF O/B FLAP HINGE. 1. REPAIRED PER E105-491102-PERM VER A.SDR HALA2019090600375Spar · corrodedLEFT WING REAR SPAR LOWER TANG MODERATE CORROSION STATION XRS 184 - 188 (M) 1. REMOVED CORROSION PER SRM 51-10-04. 2. HFEC OK. CHORD 1.0 SPAN 3.75 ADJ .173 REM .119, M66 SUBMITTED 3. COMPLETED REPAIR PER E105-491103-PERM.SDR SIMA201908196002Spar · crackedRH WING TIP FWD FITTING CRACKED INSIDE 651AB. FOUND ON CLOSE UP. ACCOMPLISHED PERMANENT REPAIR TO RH WINGTIP FWD SPAR 1 IAW ENVOY ERS-EJ-57MR-1151SDR FDEA201908151888Former · crackedLEFT WING LEADING EDGE COMPARTMENT FORMER AT STATION XOS 911 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB 2921 REVISION A. INSTALLED FABRICATED FORMER AT LEFT HAND WING LEADING EDGE COMPARTMENT ATSDR FDEA201908151887Former · crackedLEFT WING LEADING EDGE OUTBOARD COMPARTMENT FORMER AT STATION XOS 1025 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED FORMER AT LEFT HAND WING LEADING EDGE OSDR Q5QA20190815243Spar Web · crackedREAR SPAR CARRY THROUGH IS CRACKED.THE CRACK RADIATES FROM THE LOWER RIGHT MOST OUTBOARD FASTENER OF THE FUSELAGE REAR WING ATTACH FITTING. THE LENGTH OF THE CRACK IS APPROXIMATELY 5/16" AND CAN BE SEEN WITHOUT MAGNIFICATION. THE CRACK WAS CONFIRMED WITH EDDY SDR 2019FA0000252Spar · corrodedDURING INSPECTION OF WING CARRY THROUGH SPAR PER CESSNA SEL-57-06. I WAS NOT DUE FOR INSPECTION BASED ON ACTT, BUT BASED ON FIELD FEEDBACK WE PERFORMED VISUAL INSPECTION AND FOUND EXTENSIVE CORROSION. I CAN PROVIDE PICTURES. THE DAMAGE ON MINE IS SIGNIFICANTLYSDR COEA201910234919Spar · corrodedWO 198966 NR 500035 HEAVY CHECK COE/MAJOR REPAIR: L/H WING REAR SPAR UPPER STRIP SLAT HAS LEVEL 2 CORROSION AROUND FASTENER HOLES BETWEEN RIBS 13-21 ON THE UPPER SURFACE. CORRECTIVE ACTION: REPAIRED PER SRAS S572K0006...15229 ISSUE B, DATED 10/16/2019.SDR CALA2019081201350Spar · damagedLT WING L/E FRONT SPAR WEB FOUND DAMAGED AT OFSS1025 REF NRC 9131148 DVI SURROUNDING STRUCTURAL WITHIN 16'' NIL FINDINGS. HFEC INSP CARRIED OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND AT TRIM MED EDGE. HFEC OPEN HOLE INSP CARRIED OUT AT EXISTING FASTENER SDR COEA201910318919Spar · corrodedWO 198966 NR 600027 HEAVY CHECK COE/MAJOR REPAIR: R/H WING REAR SPAR UPPER STRIP SLAT HAS LEVEL 2 CORROSION AROUND FASTENER HOLES BETWEEN RIBS 13-21 ON THE UPPER SURFACE. CORRECTIVE ACTION: REPAIRED PER SRAS PCE-1900/17...11929 ISSUE C, DATED 10/16/2019.SDR FXGA201908051958Spar Web · corrodedCORRODED REAR SPAR WEB AT W/STA 359L. TO REPAIR A CORRODED REAR SPAR WEB AT W/STA 359L. CUT OUT CORRODED AREA AND REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-5.SDR FXGA2019080521957Spar · crackedCRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. TO REPAIR A CRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. PERFORM OUTER WING CENTER SPAR WEB REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-7.SDR HYIA20190724001Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND LOWER AFT SPAR CAP P/N: 5122041-23. THIS CORROSION IS LOCATED IN THE FORWARD RADIUS OF THE HORIZONTAL AND VERTICAL LEGS OF THE CAP AT APPROXIMATE LWS 228.71. THIS CORROSION HAS A DEPTH OF APPROXIMATESDR IPXA2019080525263Spar Cap · corrodedINSPECTION TYPE:4C, RT WING AFT SPAR UPPER CAP HAS CORROSION AT STA. XORS 810 - 826.5 AND STA. XORS 781 - 800. REPAIRED CORRODED RT WING AFT SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS 781.5 - XORS 826.5 IAW 011-5720-01-A7857 REV. IR AND EO MD11-5720-73486-A.SDR CA190719009Spar · corroded(CAN) DURING INSPECTION OF LOWER SPAR CARRY THRU FOR CORROSION, SEVERAL (5) SMALL SPOTS OF CORROSION FOUND ON UPPER SURFACE OF THE LOWER FORWARD SPAR FLANGE. SIZE OF CORROSION VARRIED FROM 5 MM TO 10 MM.APPEARS TO BE SURFACE ONLY. TEXTRON CESSNA CONTACTED AND SDR FDEA201907181626Spar · crackedCRACK SIGNAL WAS FOUND AT RH WING FRONT SPAR RIB9 "S" HOLE AFTER ROTO-TEST INSPECTION COMPLIED WITH FEDEX EA: 6-5710-T0347649 P1, TITLE: WINGS - BASIC WING STRUCTURE - RH WING RIB 9 HOLE S/163 CRACK INDICATION - REPAIR, EO 6-5710-7-5001, SB A300-57-6037. SDR IPXA2019080535277Spar Cap · corrodedINSPECTION TYPE:4CRT WING UPPER T/E HAS CORROSION FROM XORS 538-600.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 536 - XORS 600 IAW EA 011-5720-01-A7856 REV. IR AND EO MD11-5720-73483-A. (MINOR)SDR CA190718001Spar · cracked(CAN) ROUTINE INSPECTION BEFORE A/C WAS DEPARTING ON LONG CONTRACT AWAY BASE. CRACKS EMANATING FROM NAIL HOLES ON SPAR DOUBLER. (TC# 20190718001)SDR HYIA20190718001Spar Cap · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS IDENTIFIED ON THE HORIZONTAL LEG OF THE LEFT HAND UPPER OUTBOARD SPAR CAP (P/N: 5122041-21). THIS CORROSION IS LOCATED AT APPROXIMATE LEFT WING STATION 197.71 AND MEASURES APPROXIMATELY .022 INCHES DEEP. THIS IS IN ESDR SWAA2022031282953Spar · corrodedLH WING BOOST PUMP TANK 1 FWD UPPER GROUND STRAP ATTACH POINT CORRODED / REMOVED CORROSION ON L/H WING #1 FWD BOOST PUMP GROUND STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; ORIGINAL .485' LOSS .126' REMAINING .359' OUT OF LIMITS IAW SRMSDR JGVR20190415002Spar · corrodedNUMEROUS AREAS OF CORROSION AROUND FASTENERS ON RT WING, AFT SPAR ON BOTH SIDES ON OUTBOARD AILERON HINGE. MECHANICALLY BLENDED LEVEL 1 CORROSION RT WING AFT SPAR BETWEEN THE MIDDLE AND OUTBOARD AILERON HINGES, IAW SRM 51-10-01. EVALUATED BLENDED AREAS AND FOSDR HALA2019090500366Spar · corrodedLEFT WING REAR SPAR LOWER TANG SERVER CORROSION STATION 360. 366 (M) 0/B OF 0/B FLAP HINGE. TRIMMED OUT CORRODED FLANGE AT XRS 360 TO 366. PERFORMED HIGH FREQUENCY EDDY CURRENT(HFEC) INSPECTION FOR THE FLANGE AND OPEN HOLES IN THE EFFECTIVE AREA, NO CRACKS FOSDR FXGA201906261920Spar · corrodedCORROSION ON AFT WING SPAR LOWER CHORD BETWEEN LBBL 19.2 AND WS 210L. CORROSION WAS FOUND ON THE AFT WING SPAR LOWER CHORD CENTER SECTION AND LT SECTION. SPLICES WILL BE PERFORMED AT LBBL 19.2 ON THE CENTER WING SECTION AND AT WS 210 ON THE LT WING SECTION. SDR LR7A2019062402128Former · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND TRAILING EDGE FORMER CRACKED AT LH CWS220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6724.SDR LR7A2019062402119Spar · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTER WING FRONT SPAR WEB WITH CRACKS AT PIN RIVET HOLES OWS69. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6659.SDR LR7A2019062402118Spar · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTER WING FRONT SPAR WEB WITH 2 CRACKS AT OWS58 AND WL259-287. REPAIRED IAW SRM FIG. 57-030-22. NR# 6658.SDR LR7A2019062402116Spar Cap · damagedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, REPLACED RT CTR WING FRONT SPAR UPPER CAP AS PER LAC TASK 0150 REV A (BEYOND 2ND/3RD OVERSIZE FASTENER HOLES) DUE TO FRONT SPAR WEB RENEW AT CWS154.5-220. REPAIRED IAW SRM FIG. 57-030-15. NR# 6SDR LR7A2019062401988Spar Cap · damagedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING FRONT SPAR (FS517) RT WEB LOWER CAP WITH OVERSIZED HOLES AT CWS174R-180R; WL257. REPAIRED IAW MEA 382-57-18-211. NR# 6375.SDR LR7A2019062401987Stiffener · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING FRONT SPAR WEB CWS178L VERTICAL STIFFENER CRACKED. FS517, WL263-285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6374.
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