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 = '5700' 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 = '5700' 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 VNAA202610060037Hinge Fitting · corrodedCORROSION ON HINGE FITTINGS (4 EA`S) WAS FOUND IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING. AREAS ON HINGE FITTINGS (4 EA`S) IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING WERE REPAIRED PER REO 690-57-51-556 REV --.SDR DALA2026082704877Structure · crackedA CRACK WAS FOUND AT HOLE 378. REPAIRED PER ERA 636140-14AD. (1779338) AIRCRAFT WAS GROUNDED.SDR CALA2026081918737Panel · damagedDURING INSPECTION FOUND PANEL 651DB AFT DOOR SUPPORT DAMAGED. REMOVED AND REPLACED WITH NEW SERVICEABLE PANEL ASS REF AMM 57-50-02-400-802.SDR IPXA2026092193152Spar · damagedRIGHT WING TO FUSELAGE UPPER AREA PANEL 677CT LOWER SUPPORT ANGLE HAS (8EA) ELONGTED HOLES. INSTALL NEW SPAR . NEW PART WAS INSTALLED IAW SRM 51-40-21-001.SDR IPXA2026072970144Splice Plate · crackedDURING PERFORM EO-76733-JIC2 STEP 247, FOUND NR 2 FASTENER HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98163-REQ1 REV.1 AND EGAT EI F2026A57M-1371 REV 3.SDR SWAA2026062913646Fairing · cutTWO ELONGATED HOLES ON AFT STRAKE FAIRING AT WINGLET SCIMITAR LT. REPAIRED AFT STRAKE FAIRING AT WINGLET SCIMITAR LT IAW SRM 51-70-04-2R-9 REPAIR 9.SDR IPXA2026061903908Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR REXA2026080401435Landing · crackedSECONDARY NRC FROM TC 900-57-580-503: AFTER REMOVING THE 584FB ACCESS PANEL, ELONGATED HOLE WAS FOUND IN THE SETTLEMENT AREA. SETTLEMENT AREA OF 584FB ACCESS PANEL WAS REPAIRED PER REO 690-57-52-595 REV: - -SDR DALA2026060903438Wing · no discrepancyACFT DUE LT AND RT WING INSPECTIONS AD 2024-21-01. C/W WORKCARDS 5720-01103-01A, AND 5720-01103-01B, FCN'S 95-0557- 8-0032, AND 95-0557-8-0035. OK FOR SVC. (8357674) (AIRCRAFT GROUNDED)SDR KCSA202606021048Structure · crackedCRACK IN LOWER T/E STRUCTURE, WS725 JUST AFT OF REAR SPARSDR IPXA2026051534276Bracket · missingMISSING BRACKET PN: A5796554820500 ON MOVABLE FAIRING 635BB. INSTALLED BRACKET P/N: A57965548205; TRAVELER #: T26/1865162 IN ZONE 600 ON MOVABLE FAIRING 635BB. IAW AIRBUS AIPC 27-51-65-11 ITEM 30, SRM 57-20-35-001 PAG.11 AND SRM 51-40-21-001.SDR KY7A2023FA0000158Wing · no discrepancyBIRD STRIKE AFTER TAKEOFF, BIRD MADE CONTACT WITH R WING. CLEANED THE REMAINS & PREFORMED BIRD STRIKE INSPECTION IAW FMB145 AMM 05-50-08 NO DAMAGE C\W RTS CHECKSDR SWAA2026051288257Nonskid · deterioratedLEFT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO LEFT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.SDR SWAA2026051288258Nonskid · deterioratedRIGHT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO RIGHT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.SDR IPXA2026050753105Bracket · damagedPANEL 672CB I/B ATTACH FITTING, HOLE ELOGATED 1EA. INSTALLED 2EA.BRACKETS ON PANEL 672CB IAW SRM 51-40 21-001.SDR IXXA2026040901Drain Line · dentedLEFT WING SURGE TANK DRAIN LINE IS DENTED AND GOUGED.SDR SWAA2026040784886Nonskid · peelingRIGHT WING INBD UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAY HAS AREAS OF PEELING PAINT. TOUCHED UP AREAS OF PEELING PAINT ON THE RIGHT WING I/B UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAY IAW AMM 51-21-97-370-801.SDR IPXA2026031861571Plate · damagedHOLES IN REINFORCING PLATE P/N: A57244651203 UNDERLYING STRUCTURE LOOKING FWD FOUND HOLE DIAMETER TO BE AT 0.250" 35(EA) WITH SHORT EDGE DISTANCE (1.5D). IT WAS FOUND OUT OF LIMITS. INSTALLED NEW REINFORCING PLATE P/N A57244651203 IAW SRM 51-40-21-001 AND SSDR R61A2026022700052Skin · crackedWHILE IN HEAVY CHECK - CRACK AT RT WING LOWER SKIN RIB 3A FWD EDGE OF MLG CUTOUT. CUT OUT DAMAGE, FABRICATED, LOCATED AND DRILLED, AND INSTALLED PERMANENT REINFORCING REPAIR REF ETD2026-170-003199.SDR COEA2026032610801Access Panel · corrodedWO 269490 NR 500039 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS PANEL 521DT FOIL FRETTED. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-4809/07...04337 ISSUE I, DATED 3/2/2026.SDR DALA2025120108775None · noneSHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)SDR CALA2025111711267Blowout Panel · detachedLEFT WING LE SLAT PANEL MISSING SDR FLAGGED NR 5 SLAT OTBD SADDLE BRACKET ATTACHED TO THE BLOWOUT PANEL MISSING ALONG WITH WITH BLOWOUT PANEL. ENGINEERINGS ASSISTANCE REQUESTED. REQUIREMENTS OF ECRA: 5743-02021 CARRIED OUT. NO ADDITIONAL FINDINGS FOUND, LEAK CSDR SWAA2025111333732Rib · crackedLEFT WING DEFLECTION CONTROL TAB, RIB CRACKED APPROX 2 FROM AFT EDGE. COMPLETED STEPS UP TO AND INCLUDING STEP 4.P OF LT WING INBD FIXED TE DEFLECTION CONTROL RIB REPAIR IAW SRM 57-51-02-2R-3, REPAIR 3. PERFORMED NDT STEP 4.G PER NDT PART 6 51-00-00 PROCEDSDR DALA2025110708136Panel · not reportedL/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852". REMOVED L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852" (1284968)SDR SWAA2025112028595Paint · degradedTHE LEFT WING UPPER INBD SURFACE EMERGENCY ESCAPE PATHWAY HAS HEAVILY DEGRADED PAINT. RESTORED FINISH PER AMM 51-21-97-370-802.;[02] INSPECTION C/WSDR F3LA202510230319Fitting · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION ON RH WING DRY BAY 674AB CORROSION WAS FOUND UNDER MULTIPLE NUTS. INSPECTION AND WORK PERFORMED AS PER EO-A32F-57-32466-01-FINAL. MX ACTION IS ACCEPTABLE.SDR F3LA202510230318Fitting · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION ON LH WING DRY BAY 574AB CORROSION WAS FOUND UNDER MULTIPLE NUTS. INSPECTION AND WORK PERFORMED AS PER EO A32F-57-32466-01-FINAL. MX ACTION IS ACCEPTABLE.SDR VNAA2025F00020Support · corrodedDISCREPANCY: THE LANDING FOR PANEL 642ET IS CORRODED. CORRECTIVE ACTION: REPAIRED LANDING IAW MHIRJ REO 670-57-21-1032 REV-- DATED 2025-1-13SDR AALA202510295385Rod · excess playAIRCRAFT WAS NOT GROUNDED: LEFT WING, BETWEEN SPOILER NUMBER 5 AND 6, AFT OF AFT SPAR, INBOARD SIDE BOTH RODS HAVE EXCESSIVE PLAY. REMOVED AND REPLACED BEAM ASSEMBLY AT LEFT WING. PER B737NG SRM 51-40-02, SRM 51-40-05, SRM 51-20-01.SDR DALA2025100807327Sealant · not reportedWORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717 51-24-00 & DWG'S. C/W STEP 19 OF ERA 629612-14AD (1239562)SDR DALA2025092406976Limiter · damagedON WAKEUP FOUND SPEED TAPE ON RH VORTILON. DAMAGE WITHIN LIMITER PER EAA 570743-14MA REV B APPLIED TEMP REPAIR. WILL NEED PERMINENT REPAIR WITHIN 100 FLIGHT HOURS.(7372557)SDR SWAA2025100213158Paint · peelingCORROSION SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING. PERFORMED DETAIL VISUAL INSPECTION ON SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING AND NO CORROSION FOUND, ONLY PEELING PAINT IAW SRM 51-10-02. NO MAINTENANCE ACTION IF SDR SWIA2025120200903Guide · wornDURING AAI AUDIT OF 2C TASK CARD 57-690-304, FOUND THE LT SIDE ROLLER GUIDE IS SHOWING SIGNS OF WEAR. COMPLIED WITH THE REPAIR OF THE LT SIDE ROLLER GUIDE IAW REO 690-57-51-467, REV -. OPS CHECK GOOD.SDR CALA2025082708186Tape · unsecureFA REPORTS ABNORMALLY LO UD WHISTLE FROM RIGHT OV ERWING EXIT. SECURED LOOSE TAPE ON RIGHT WING.SDR FDEA202508181494Repair · not reportedEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER BETWEEN STATION XOS 621 TO XOS 625 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER BETWEEN STATION XOS 621 TO XOS 625 EVALUATED AND FOUND REPAIRSDR DALA2025080505856Strut · looseLEFT WING INTERCONNECTING STRUT LOOSE. CORRECTIVE ACTION: REPLACED BEARING AT LH WING I/B FLAP INTERCONNECTING SUPPORT STRUT ATTACH FITTING IAW A319 CMM TASK 57-52-21-300-803-A01. (1122721).SDR DALA2025080505855Strut · looseRIGHT WING INTERCONNECTING STRUT WITH LOOSENESS. CORRECTIVE ACTION: REPLACED BEARING AT RH WING I/B FLAP INTERCONNECTING SUPPORT STRUT ATTACH PAINT IAW A319 CMM TASK 57-52-21-300-803-A01. (1122710).SDR FDEA202506140936None · noneAGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-8 BY FABRICATION) EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789SDR FDEA202506140935None · noneAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-7 BY FABRICATION) EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.6SDR FDEA202506140934None · noneAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD11 SRM 5SDR SWAA2025072180824Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB. REPAIRED ACCESS PANEL 661CB IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR UIEA2025060200713Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2025060604324Repair · not reportedSHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)SDR DALA2025051503762Not Reported · damaged(LOG 0963092) PERFORM PERMANENT REPAIR IN ACCORDANCE SRM 57-10-10-2R PROCEDURE 3. PERMANENT REPAIR IN ACCORDANCE B737-800 SRM 57-10-10-2R PROCEDURE 3, REPAIR 3 ALTERNATIVE 2 WAS PERFORMED.SDR 9WGA2025070154519Support · crackedDURING HEAVY MAINTENANCE LH FLAP HINGE SUPPORT WAS FOUND CRACKED.SDR DALA2025043003315Repair · not reported-AD- EXISTING REPAIR FOUND, CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHUR FLIGHT REF. FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FORSDR DALA2025043003314Repair · not reported-AD- EXISTING REPAIR FOUND, OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC I OF ERA 619064-14AD REV B. (LP #7184929)SDR UIEA2025042100557Fastener · not reportedWINGS - WING LEADING EDGE - UPPER SKIN PANEL - FASTENER CHANGE - SB 737-57-1336 R0 IAW PAR-B1920 REV.0.(<P>REPLACED FASTENER IAW ATLAS AIR PAR-B REV 0 DATED: 17JAN25 AND BOEING 737-800 BCF SRM 57-41-01-2R-7 REPAIR 7 PARG 4 TABLE 201 FIG 202, REV 23 DATED: 10MASDR CALA2025042104037Wing · smokeRAMP REPORTS SMOKE COMING FROM WINGS, BURNING SMELL. CONTACTED FIRE DEPARTMENT, NO HEAT SHOWN ON THERMAL IMAGING, NO BURNING SMELL, NO EVIDENCE OF HEAT DAMAGE FOUND. DROPPED FLAP/S SLATS ON GROUND REF AMM 27-50-00, INSPECTED, SMOKE APPEARS TO CONDENSATION WISDR VNAA20250528001Hinge Fitting · gougedRH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE. RH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE WAS REPAIRED PER REO 690-57-51-421 REV --.
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