JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, newest first.
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 = '5720' 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 = '5720' 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 ZZDA2010424Panel · crackedLEFT WING INBOARD BUTE DOOR, CRACKED. ACCOMPLISHED BUTE DOOR DOUBLER REPAIR PER EA 17-57-02514IR.SDR LR7A2010091400045Fitting · corrodedDURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT INBOARD LOWER FWD CORNER FITTING WITH PITTING CORROSION AT NODE FACE; THICKNESS VERY NEAR LIMIT. REPLACED CORNER FITTING IAW LOCKHEED SMP583 CHAP 51-60 & 51-70.SDR LR7A2010091400044Fitting · damagedDURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT INBOARD UPPER FWD CORNER FITTING NODE THICKNESS EXCEEDING LIMITS. REPLACED CORNER FITTING IAW LOCKHEED SMP583 CHAP 51-60 & 51-70.SDR UALA2010090703267Stiffener · brokenBROKEN OTBD TRACK SIDE PLATE STIFFENER ON LT WING NR5 SLAT TRACK WELL. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE IAW REO-L01268 AND RAS-BAE-1013919-2010. CAT "A" REPAIR.SDR SWAA105167Angle · brokenDURING SCHEDULED MV2 CHECK, FOUND RT WING STRUT PANEL 585R UPPER SUPPORT ANGLE FWD FASTENER BROKEN. REMOVED AND REPLACED ANGLE PER SRM AND EA.SDR UIEA2010083100149Rod · brokenDURING WALKAROUND INSP AT STN, DAMAGE WAS DISCOVERED AT RT WBL238.30. FIXED T/E UPPER RIB INSTALLATION CONSISTING IN BROKEN TIE ROD AND CLEVIS. (THE BROKEN ROD WAS REMOVED AND A DETAIL VISUAL INSP WAS PERFORMED TO ASSURE DAMAGE-FREE CONDITION TO THE SURROUNDSDR SWAA105049Support Angle · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING T/E SUPPORT ANGLE CRACKED AT WBL 85. REMOVED AND REPLACED ANGLE PER SRM AND DWG.SDR FDEA201008233104Structure · corrodedMAIN DECK - UPON REMOVAL OF FLOOR PANEL AT CTR TANK UPPER SURFACES AT STA 1226, BETWEEN X= -79 TO X= -82 FOUND WITH SURFACE CORROSION. MAIN DECK CENTER TANK UPPER SURFACES AT STATION 1226, BETWEEN X= -79 TO X= -82 SURFACE CORROSION REPAIR CARRIED OUT ASSDR FXGA9056RStructure · corrodedDEEP CORROSION FOUND AT MULTIPLE NUT PLATE HOLES ALONG THE NR 2 NACELLE FILLET FAIRING BETWEEN THE FRONT AND CENTER SPAR. REPAIRED PER EAC EO 1044 AND 8110-3 DATED 8/20/10.SDR IPXA10M62269Strap · crackedINSPECTION TYPE:1C, RT WING FIXED L/E SKIN SPLICE STRAP CRACKED XOS 791. REMOVED, FABRICATED, AND INSTALLED SKIN SPLICE STRAP IAW DWG ARB3954.SDR IPXA10M62268Strap · crackedINSPECTION TYPE:1C, RT WING L/E SKIN SPLICE STRAP AT XOS 669 CRACKED. REMOVED, FABRICATED ADN INSTALLED SKIN SPLICE STRAP IAW DWG ARB3954.SDR VGQY2010081200078Channel · crackedLEFT WING T/E REAR SPAR ADJACENT TO NR 6 SPOILER ACTUATOR AFT FACE / UPPER CHANNEL CORRODED. TRAILING EDGE BEAM UPPER CHORD 65B11614-7 FOUND WITH CORROSION CRACKING AT TWO LOCATIONS. CRACK LENGTHS ARE APPROX 3.5" INCH AND 1.75" AT THE RADAII. COMPLIED WITH SDR WRLA20100810436Rib · crackedCRACK ON THE SUPPORT RIB OF LT WING REFUELING ACCESS DOOR AT STA XOS643.SDR FDEA201008102900Doubler · corrodedNR 1 PYLON SPIGOT FITTING -TO -WING DOUBLER HAS CORROSION ON OTBD SIDE (APPROX 2" SQ, VISIBLE) BETWEEN OTBD SPIGOT ATTACH BOLTS. ALSO THIS DOUBLER HAD A GOUGE ON L/E - REF.N01074. REMOVED NR1 PYLON FROM LT WING TO ACCESS SPIGOT FITTING IAW AMM 54-50-00-4,SDR A6WA201040744Angle · crackedRT INBD FLAP HINGE OTBD FAIRING ANGLE ON INBD HINGE CRACKED REF 16 SRM 57-21-55. R & R WITH DUPLICATED PART IAW SRM.SDR IPXA10M62219Doubler · crackedINSPECTION TYPE:2C, IN LT WING OTBD L/E COMP AT XOS 610, THE CEILING HAS 2 EA SMALL CRACKS AT FASTERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203, REV 44.SDR FDEA201008092877Support Bracket · gougedLT WING, NR 2 SPOILER, INBD SUPPORT BRACKET IS GOUGED BY THE FLAP. REPAIRED GOUGED SUPPORT BRACKET IAW EA 8-5740-136702,SDR FDEA201008042803Support · corrodedLEFT WING LEADING EDGE FIRE BOTTLE SUPPORT LANDING HAS FRETTING. BLENDED AND CHECKED LIMITS OF FRETTING ON LEFT WING L/E FIRE BOTTLE DOOR LANDING IAW SRM 57-00-01, FIG 1A, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II AND PAINTED IAW SRM 51-21-01, VOL ISDR USAA2010080491587Fitting · crackedMCN - C2 - MAJOR REPAIR - CLIP CRACKED LEFT WING LOWER TRAILING EDGE AT WBL 83. REPLACED LEFT WING LOWER TRAILING EDGE ATTACH CLIP AT WBL 83 IAW B757 SRM 51-40-02.SDR U2RA227DHN009Rub Strip · corrodedRT WING PANEL NR 94A RUB STRIP CORRODED.
SDR GUUA95157072610BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE.SDR USAA2010073091548Angle · crackedCLT - Q1 - MAJOR REPAIR - CRACK ON ANGLE ON LEFT WING AT OUTBOARD SIDE OF NR 3 AILERON ATTACH HINGE FITTING. REPLACED ANGLE ON LEFT WING AT OUTBOARD SIDE OF NR 3 AILERON ATTACH HINGE FITTING IAW B737 SRM 51-40-02.SDR FDEA201007162558Support · misrepairedLT WING FIXED L/E LOWER PANEL SUPPORT STRIP AT STA XOS 906 FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING FIXED L/E LOWER PANEL SUPPORT STRIP AT STA XOS 906 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER AT LT WING FIXED L/E LSDR V0XR201007160001Angle · cracked(V0XR) RT AFT WING SPAR TO FUSELAGE CLOSING ANGLE CRACKED. R & R RT AFT WING SPAR ANGLE. W/C 2095SDR TAMF20100046SPlate · corrodedDURING "SC3" CHECKS INSP, FOUND CORROSION ON WING 111T1008-1 BEARING PLATE, STA 995.00 LBL 74.53 LH. REPAIR ACCOMPLISHED IAW EWO 767-57-061R2 AND SR 1-1626004867.SDR DALA1019970662Support Fitting · damagedWHILE ACCOMPLISHING EA 06-070332-03, AD REV J SPOT FACE DEPTH FOR HOLES MARKED 3 AND 4 ON NEW SUPPORT FITTING PN 012N8888-2 FOR THE RT WING WAS EXCEEDED TO ATTAIN 100 PERCENT SPOT FACE. COMPLIED WITH ER/A 484129-14 AD DURING HMV AT SAA ON N/R CARD 174576.SDR V0XR201007130001Angle · cracked(V0XR) FWD WING SPAR TO FUSELAGE CLOSING ANGLE AT 4L TO 6L IS CRACKED. REMOVED AND REPLACED WING SPAR TO FUSELAGE CLOSING ANGLE. W/C 2092SDR FDEA201007082418Stiffener · crackedLT WING T/E CAVITY UNDER PANEL 575 BB; UPPER PANEL SUPPORT IS CRACKED. RIB 6A-RIB 7. REMOVED CRACKED SUPPORT (STIFFENER) AND ADJACENT BRACKET IAW SRM 51-40-21, PARA 7. FABRICATED NEW STIFFENER IAW DWG A57241059 (-200). ALODINED AND PRIMED STIFFENER IAW SRSDR IPXA10M61198Structure · crackedINSPECTION TYPE:3C, RT WING OTBD L/E COMPARTMENT CEILING HAS CRACKS AT STA XOS 643. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG. 203.SDR ASAA1098038Support Angle · crackedRT WING TRAILING EDGE SEAL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE.SDR CA100706009Retainer · mismanufacturedPN C6W1130-39, SEAL, RETAINER, WING FENCE HAS BEEN MFG USING INCORRECT MATERIAL. INVESTIGATING TO DETERMINE IF FURTHER ACTION IS REQUIRED.SDR ASAA1098034Support Angle · crackedRT WING TRAILING EDGE SEAL SUPPORT ANGLE CRACKED.SDR ASAA1098032Support Bracket · crackedRIGHT WING PANEL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET.SDR IPXA10561161Channel · chafedINSPECTION TYPE:C4, RT WING LOWER FIXED T/E PANEL OTBD CHANNEL IS CHAFED BELOW NR 7 SPOILER (MARKED) R & R CHANNEL IAW SRM 57-51-02-1A 1. DWG 113N1620, SRM 51-40-02.08.SDR SIMA201018701Angle · damagedDURING MAINTENANCE BASE VISIT FOUND DAMAGE TO LEFT WING LOWER SKIN AND ANGLE DUE TO TIRE STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR OF DAMAGE TO LEFT WING LOWER SKIN AND ANGLE IAW EO-EM-57MR0488R3. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR V0XR20100701002Angle · cracked(V0XR) FWD WING SPAR TO FUSELAGE (CLOSING ANGLES). R & R FWD WING SPAR TO FUSELAGE, CLOSING ANGLES. W/C 2094SDR V0XR20100701001Angle · cracked(V0XR) FWD WING SPAR TO FUSELAGE (CLOSING ANGLES) AT 4R-6R CRACKED. REMOVED AND REPLACED FWD WING SPAR TO FUSELAGE, CLOSING ANGLES. W/C 2093SDR USAA2010070891368Support Fitting · crackedBFM - Q5 - MAJOR REPAIR - CRACK AT RIGHT WING UPPER AFT PANEL SUPPORT CLIP AFT OF REAR SPAR RSS236. REPLACED SUPPORT CLIP AFT OF REAR SPAR AT RSS236 IAW B737 SRM 51-40-02.SDR AALA20100627TUL03Support · shearedVVI - CREW REPORTED AIRFRAME VIBRATIONS ORIGINATING FROM AFT FUSELAGE. EMERGENCY DECLARED FLIGHT RETURNED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WING FAIRING INBOARD OF NUMBER 8 SPOILER WITH TWO HOLD DOWN SUPPORT RODS SHEARED OFF.SDR SWAA103757Support Angle · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING SUPPORT ANGLE UPPER SURFACE I/B SIDE CRACKED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.SDR SWAA103573Web · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING L/E WEB CRACKED. REMOVED AND REPLACED WEB PER SRM.SDR ASAA1057930Attach Angle · crackedLEFT WING TRAILING EDGE RSS 269 T/E SUPPORT AFT ATTACH ANGLE IS CRACKED AT THE LOWER FASTENER HOLE. REMOVED AND REPLACED CRACKED FASTENER HOLE.SDR A6WA201040572Seal · crackedSEAL ON OTBD SIDE OF LT FLIGHT SPOILER ATTACHED TO WING HAS A 5" CRACK. R & R WITH NEW SERVICEABLE SEAL IAW SRM 51-42-06 AND SRM 51-41-02.SDR FDEA201006142093Web · damagedLOOSE AND MISSING SCREWS BOTTOM AFT FALSE SPAR CHORD RIGHT WING AT NR 8 SPOILER FITTING CUT OUT DAMAGED WEB SECTION. TRIMMED LOWER CHORD DAMAGE. FABRICATED NEW WEB SECTION, NEW LOWER CHORD, & 2 ANGLES. HEAT TREATED PARTS IAW FASI ENG REPORT 2-37153-801 REV A,SDR FDEA201006141993Stiffener · crackedRT WING L/E STIFFENER IS CRACKED BETWEEN WING STATIONS XORS 560 AND XORS 565.SDR FDEA201006141992Stiffener · crackedRT WING L/E STIFFENER IS CRACKED BETWEEN WING STATIONS XORS 560 AND XORS 565. ACCOMPLISHED HFEC IAW NTSPM 06-10-01.001 TO VERIFY AND OF CRACK. REPAIRED CRACKED STRINGER IAW EA 8-5710-136667.SDR ASAA1057910Attach Bracket · crackedRIGHT WING DEFLECTION FITTING RSS 289 UPPER FWD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED CRACKED BRACKET AT RSS 289 DEFLECTION ROLLER FITTING.SDR ASAA1077914Angle · crackedOUTBOARD AFT ANGLE IS CRACKED UNDER INBOARD FIXED LEADING EDGE SKIN ON LT WING. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE.SDR CALA2010061400275Web · wornRIGHT WING AT APPROX RSS 500 HAS A WORN AREA ON I/B SIDE OF WEB ABOUT 3 INCHES AFT OF AILERON CABLE GROMMET. INSTALLED DOUBLERS REPAIR REF ECRA 5720-02138 PART 1. INITIATED DIP AS FOLLOW; "ACCOMPLISH PERMANENT REPAIR BEFORE 6-7-2012. PLANNING TO CONTACT ENGSDR ASAA1057903Support · crackedRIGHT WING TRAILING EDGE AFT PANEL SUPPORT CRACKED. REMOVED AND REPLACED FITTING ON THE RT WING T/E FIXED BULKHEAD.
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