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 Q2S2010F00042Spar · corrodedWS NR 0912, WC NR 57-910-01-01. RT WING L/E FRONT SPAR LOWER CHORD AT OLES 1356 FOUND CORROSION. RT WING LOWER SKIN CORROSION AREA CUT AND REMOVED IAW SRM 57-30-03, FIG 9 REV 116 AT FRONT SPAR OLES 1356 TO 1362. HFEC CARRIED OUT AND FUND NO CRACK EVIDENT. SDR MZZA2010030800006Spar · corrodedFOR ESFR ENTRY, REF HANGER N/R 0974602, CORROSION REPAIR RT WING FWD LWR SPAR STRAP BELOW NR 7 I/B AUX TRACK. RT WING FWD LWR SPAR STRAP SECTION REPAIRED PER ECRA 5730-02588 AND FORM; 44.0008 ATTACHED ITEM 1 TO ITEM 38 ACCOMPLISHED.SDR GLBA20100302FASpar · damagedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX A LOCK FASTENER HOLE IN THE LT WING SPAR AT APPROX WS 93.250 WAS FOUND STEPPED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-57-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.SDR GLBA20100302FFrame · crackedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L. CRACK IS APPROX 2" LONG.SDR GUUA93957022810ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE MFG ACFT COMPANY KIT 118-4014-0003.SDR Q2S2010F00038Spar · corrodedWS NR 0630, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD EXTENSION AT APPROX OLES 1361 FOUND CORROSION. REPAIR CARRIED OUT IAW EN 1020-10. FORM 8100-9, DATED 22 MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00035Spar · corrodedWS NR 0631, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD AT APPROX OLES 1305 FOUND EXFOLIATION. REPAIR CARRIED OUT IAW EN NR 1020-10. FORM 8100-9 DATED 22, MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00020Strap · corrodedWORKSHEET NR 0628, WORKCARD 57-830-01-01. LT WING L/E FRONT SPAR UPPER CHORD STRAP AT APPROX OLES 1481 FOUND CORROSION. CORRODED STRAP REPLACED IAW SRM 51-30-02 REV 116. PN ON: 65B016877.SDR DALA104329872Spar · crackedDURING "H" CHECK FOUND LT WING L/E AT STA XLFS 254 WEB CRACKED AT UPPER SPAR CHORD. REPAIRED IAW SRM 51-10-2, 51-10-3,51-10-4,51-70-4 & 51-30-5.SDR 2010FA0000203Spar · crackedFOUND CRACK IN LT MAIN WOOD SPAR APPROX 16 " INBD OF LIFT STRUT.SDR CA100224009Fastener · missing(CAN) ACFT WAS ON SCHEDULED CHECK AND DURING INCORPORATION OF SB 57-3815/16 TO COMPLY WITH AD 2009-23-03. IT WAS DISCOVERED THAT THERE WAS A CONFLICT WITH THE SB DWG AND THERE WERE SOME MISSING FASTENERS (QTY 7) AT RWS 123 ON THE RT AFT WING SPAR THAT WERE MISDR MTNA0210001Spar Cap · corrodedLT AND RT FWD WING SPAR CAP AT RIB 10 AND RIB 12 HAS CORROSION. CORROSION REMOVED AND BLENDED IAW TEMPORARY REPAIR INSTRUCTIONS IAW ATR STRUCTURAL REPAIR APPROVAL SHEET DO/TS-802/10...5597 AND DO/TS-803-804/10...5596.SDR WRLA20100207341Spar Cap · corrodedDURING PERFORM TASK CARD WA5729 FOUND LEFT WING REAR SPAR UPPER CAP P/N ARB7413-1 CORROSION AT XW840 NRC. BLENDOUT THE CORROSION AREA AND THE DAMAGE WITHIN ALLOWABLE LIMITS IAW SRM 57-00-10 FIG 101 REV 42, APPLY PROTECTIVE COATING, COND CHECK NORMAL.SDR WRLA20100207340Spar Cap · corrodedDURING PERFORM TASK CARD WA5729, FOUND LEFT WING REAR SPAR UPPER CAP P/N ARB7413-1 CORROSION ST XW899 NRC. RE-IDENTIFY THE CORROSION AREA IS AT XORS 1052 AND PFM EI: W2010A57B-383 REV00 REPAIR CORROSION ON LT WING REAR SPAR UPPER CAP UPPER SURFACE AT XORS 105SDR 2010FA0000087Spar · corrodedSEVERE CORROSION ON LT AND RT AILERON MAIN SPARS BETWEEN SPAR AND BRACKETS. SPAR BULGES AROUND RIVETS ATTACHING THE BRACKETS TO THE SPAR. THIS CONDITION WAS FOUND WHEN INSPECTING AILERONS PRIOR TO RECOVERING. SUSPECT THEY MAY HAVE BEEN ON SEA PLANE OPERATED ONSDR FY4Y197M20100129Spar · corrodedTHE ACFT INPUT FOR 6C CHECK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE THICKNESS OF CORROSION REMOVED IS 0SDR FY4Y197M20100201Spar · crackedACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL: 0.370"; THICKNESS OF CORROSION REMSDR 2010FA0000078Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING VISUAL INSP BY INSPECTOR, THE LEVEL 2 CORROSION WAS FOUND ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE CHORD THICKNESS OF CORROSION REMOVED IS 0.040". PHOTO SDR 2010F00009Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL:0.370"; THICKNESS OF CORROSION REMOVEDSDR IPXA10658389Spar · crackedINSPECTION TYPE:6C, LT WING - L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB FRONT SPAR ANGLE FOUND CRACKED IN LENGTH 3/4" LT WING - L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB FRONT SPAR ANGLE REPLACED AND INSTALLED IAW SRM 57-10-02 AND 51-40-02 REV 46.SDR COEA2010012503819Strip · chafedHEAVY CHECK COE - MAJOR REPAIR: RT WING FRONT SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 5, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 6 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS.SDR COEA2010012502819Strip · chafedHEAVY CHECK COE - MAJOR REPAIR: LT WING FRONT SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 5, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 6 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS.SDR COEA2010011801819Spar · chafedHEAVY CHECK COE: MAJOR REPAIR: LT WING REAR SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 4, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 3 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS DO/TS-299/SDR USAA2010020590292Pan · crackedSAL - MAJOR REPAIR - C22 CHECK - CRACK ON LEFT WING FORWARD SPAR SEAL PAN ASSEMBLY AT WBL 190. REPLACED LEFT WING FORWARD SPAR SEAL PAN ASSEMBLY AT WBL 190 IAW B737 SRM 51-40-02 AND EA 132866.SDR FDEA201001120087Spar · corrodedRT WING REAR SPAR WEB CORRODED AT RT WING FUEL SHUTOFF VALVE AT VALVE MATING SURFACE AREA. ACCOMPLISHED EA NR F-5710-131557, WING RT REAR SPAR CORROSION AT FUEL SHUTOFF VALVE. MAJOR REPAIR.SDR IPXA10658109Spar · crackedRT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE FOUND CRACKED. RT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 45.SDR CA100125010Spar · corroded(CAN) CORROSION EXFOLIATION TYPE FOUND ON THE WEB OF THE SPAR ON THE RT REAR WING (WS 76.63) (ONLY THE WEB SITUATED AT THE EXTERIOR OF THE STA, WAS 7663 WAS AFFECTED, THE INSIDE WEB WAS INTACT) ACFT HAS ALREADY FLOWN WITHOUT THE GEAR DOORS INSTALLED (BEFORE 2SDR CA100127016Spar Cap · corroded(CAN) AFTER ACCOMPLISHING AD 94-04-14 IT WAS NOTED THAT THE WING LOWER SPAR CAP WAS CORRODED BEYOND THE SAFE LIMIT ACCORDING TO SB 208A. THE ACFT WAS GROUNDED.SDR IPXA10M58239Doubler · crackedINSPECTION TYPE:2C RT WING L/E INTERIOR AT UPPER SPAR CAP APPROX STA XOS496.5 BEADED DOUBLER IS CRACKED, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER, AND ANGLE REF SRM 57-40-02 REPAIR 9 FIG 203.SDR CA100108008Attach Fitting · corroded(CAN) LT WING REMOVED FOR REPAIR OF CRACKED RIB INTERNAL FLANGE OF REAR FORK ON THE LT REAR SPAR FUSELAGE ATTACH FITTING WAS FOUND CORRODED (SEE ATTACHED PICTURE). THIS DEFECT WAS NOT NOTICEABLE WITH THE WING INSTALLED ON THE FUSELAGE AND ONLY BECAME APPARENTSDR CA100127014Spar · cracked(CAN) ON INSP OF WING AD 78-09-05 WAS ACCOMPLISHED AND THE LT WING FWD SPAR AFT WEB WAS FOUND CRACKED.SDR CA100209010Spar · cracked(CAN) THE OTBD WING REAR SPAR WEB WAS FOUND CRACKED AT THE LAP JOIINT WS 110.11, THE LOCATION OF THE OTBD FLAP, INBD TRACK. THE RIVETS SECURING THE LOWER CLIPS TO THE FLAP TRACK FAILED. THE FORCES APPLIED TO THE FLAP TRACK WHEN THE FLAPS WERE LOWERED PULLED ONSDR USAA2009123193455Spar · corrodedBFM - MAJOR REPAIR - C4 CHECK - CORROSION ON LEFT WING REAR SPAR LOWER FACE AT RSS 219.51, WL 200. REPAIRED LEFT WING REAR SPAR LOWER FACE AT RSS 219.51, WL 200 IAW EA 134180.SDR 2010F00000Spar · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON RT WING FRONT SPART LOWER CHORD PLATE AT WS 482. AFTER REPAIRING TO THE FRON SPAR LOWER CHORD PLATE, FORM 337 WILL BE SUBMITTED TO FAA FOR FINAL RESULT OF CORRECTIVE ACTIONS DETAIL.SDR IXXA10WSAP016SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1076. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA. SDR IXXA10WSAP015SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1070. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA.SDR FDEA200912184486Spar · corrodedRT WING REAR SPAR WEB CORRODED AT RT FUEL SHUTOFF VALVE AT VALVE MATING SURFACE AREA. REPAIR IAW EA F-5710-131557. ACCOMPLISHED EA NR F-5710-131557 WING-RT REAR SPAR WEB CORROSION AT FUEL SHUTOFF VALVE, THIS IS A MAJOR REPAIR WITH NO FOLOW=UP INSPECTION RESDR AALA20091216TUL13Casting · crackedLEFT WING LEADING EDGE FRONT SPAR FRONT SIDE CASTING CRACKED AT STATION XRS 240. NEW CASTING INSTALLED PER SRM 51-30-05.SDR FDEA200912114414Frame · crackedRT WING FRAME 47, HOLE "E" HAS A CRACK INDICATION AT 6 O'CLOCK AT DEPTH 15/32. COMPLIED WITH EA 6-5710-135118.SDR 2009FA0001012Spar · corrodedLT WING REAR SPAR UPPER SPAR CHORD CORRODED OUT OF LIMITS AT WING STA70 - STA 189 AND CRACKED AT WING STA 177. REPLACE SPAR CHORD SECTION IAW SR NR 1-1446626958 WITH ATTACHED 8100-9.SDR GUUA94957120109ASpar · corrodedDURING SCHEDULED LT WING X-RAY INSP, DISCOVERED SURFACE CORROSION ON MAIN SPAR AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION AND INSTALLED AN INTERNAL REPAIR STRAP AND EXTERNAL DOUBLER REPAIR.SDR 2009FA0000995Spar · crackedDURING ROUTINE INSPECTION OF WINGS, CRACKS WERE NOTED IN SEVERAL OF THE FALSE SPAR ANGLES IN THE RIGHT WING. REFERENCE SERVICE BULLETIN SB-212-57-30 AND AD 98-12-28.SDR CA091207002Frame · cracked(CAN) A REPAIR INVOLING WELDING A CRACK APPROX 1 INCH LONG LOCATED JUST ABOVE THE LT REAR FLOAT ATTACHMENT PLATE, WITHIN THE CIRCLE OF C. FIG 2 OF SL NR 71 WAS CARRIED OUT. THE FOLLOWING DAY, NOTICED A CRACK APPROX 3/4 TO 1 INCH LONG IN THE WELD THAT RUNS ARSDR CA091203006Spar · damaged(CAN) UPON PULLING THE WINGS FOR A PAINT JOB, IT WAS NOTICED AT SOME POINT SOMEONE WHO WAS DRILLING A SCREW FROM THE WING ROOT FAIRING, DRILLED THROUGH THE WING ATTACH POINT FROM THE SPAR INTO THE WING BOLT.SDR GUUA94357112409ASpar · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED RT WING LWR AFT SPAR ON COLLECTOR TANK HAS SMALL SPOT OF SURFACE CORROSION BETWEEN WS 114.25 TO 124.25. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP. NOTE: PREVIOUSLY SUBMITTED, OPEN.SDR 2009FA0000989Spar · crackedIN THE PROCESS OF PERFORMING AN ANNUAL INSP, A FATIGUE CRACK INDICATION WAS DETECTED ON LT WING IN THE UPPER MAIN SPAR WEB JUST BELOW THE SPAR CAP RUNNING SPANWISE THE ENTIRE LENGTH OF THE EXTRUDED SPAR. REMOVAL OF LT MAIN TANK EASED INSP OF FULL LENGTH OF SPSDR K11A2009112372502Attach Angle · corrodedLOWER SPAR CAP FWD ATTACH ANGLE FLANGE HAS CORROSION AT LEFT WING FSS 415.SDR FDEA200911234136Spar · crackedRT WING T/E FALSE SPAR LWR CHORD CRACKED AT WBL 118. CUT-OUT DAMAGED SECTION IAW SRM 51-10-1. FABRICATED NEW WEB SECTION IAW DWG NR SR27-57-038 REV C. FABRICATED ANGLES IAW DWG NR SR27-57-038 REV C. FABRICATED WEB DOUBLER IAW DWG NR SR27-57-038 REV C. LOCSDR FDEA200911234135Spar · crackedLT WING T/E FALSE SPAR CRACKED AT WBL 118. CUT OUT SECTION 20 1/2" LONG AND WEB 9 1/2" X 12" IAW SRM 51-10-1 REV 101, FABRICATED WEB SECTION AND DOUBLER, 2 SPLICE ANGLES, , RADIUS FILLER, 2 FILLERS IAW DWG NR SR27-57-038 REC C, INSTALLED ALL REPAIR FILLERSDR SIMA200932704Bushing · damagedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT LOWER SPAR CAP INBOARD HOLE BUSHING DAMAGED IN TORQUE BOX 1. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT LOWER SPAR CAP INBOARD HOLE BUSHING IN TORQUE BOX 1 IAW EO EM-57MR-452. THE AIRCRAFT WAS R
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