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 SWAA2015121747256Angle · crackedRIGHT WING ANGLE CRACKED IN AILERON REAR SPAR BAY AT APPROX RSS 545. R & R ANGLE IAW SRM.SDR SWAA2015121747255Angle · crackedLEFT WING TE INTERIOR, FWD OF AILERON NR 2 HINGE, LT ANGLE CRACKED. R & R ANGLE IAW SRM.SDR SWAA2016021048904Bracket · crackedRIGHT WING BRACKET CRACKED AT RSS 234. R & R BRACKET IAW SRM & DWG.SDR DALA2017120408423Stiffener · corroded(AIRCRAFT 6821, L/P 2266204) MONITOR INSPECTION LOG REFERENCE ER/A 539845-14 REQUIRES STAGE II DTA APPROVAL WITHIN 24 MONTHS OF 04 DEC 2015. ACCOMPLISHED PERMANENT REPAIR IAW ER/A 539845-14 REV ORIG. CUT OUT CORROSION DAMAGE AND CUT THE STIFFENER AT LBBL 0.23"SDR SWAA2016012148247Support Angle · crackedRIGHT WING SUPPORT ANGLE CRACKED, BETWEEN BS 706 - 727, RBL 70.85. R & R ANGLE IAW SRM & DWG.SDR SWAA2016011147847Fitting · crackedRIGHT WING AFT SPAR WING SPAR, UPPER CHORD TO BODY BATH TUB FITTING AT RSS 70.85 CRACKED. R & R FITTING IAW SRM & DWG.SDR SWAA2015121547153Stiffener · crackedLEFT WING NR 3 INBD FLAP, OTBD TRACK FAIRING INBD SIDE, HOCKEY STICK, STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.SDR A6WA201543341Attach Angle · crackedRIGHT WING, LE PICOLO TUBE UNION SUPPORT WEB ATTACH ANGLE AT LE TRANSITION, WS 149.58 CRACKED. R & R RT WING PICOLO TUBE UNION SUPPORT WEB ATTACH ANGLE IAW SRM 51-42-10.SDR FDEA201512083950Adapter · corrodedFUEL TANKS, LT WING TANK OVERWING FILL PORT ADAPTER MATING SURFACE CORRODED. REMOVED CORROSION FROM LT OVERWING FILL PORT ADAPTER MATING SURFACE IAW SRM 51-10-02, OUT OF LIMITS IAW SRM 57-20-01-1A STEP 3E. REPAIRED LT WING TANK FILL PORT ADAPTER MATING SURFASDR SWAA2016011948154Fitting · crackedLEFT WING REAR SPAR AFT BEAM TO SPAR FITTING CRACKED AT FASTENER HOLE, UPPER ROW APPROX, RSS 223. REPAIRED FITTING IAW ER & EA.SDR SWAA2016011948141Fitting · crackedRIGHT WING REAR SPAR AFT BEAM TO SPAR FITTING CRACKED, AT UPPER ROW INBD HOLE. REPAIRED FITTING IAW ER & EA.SDR UIEA2015120900704Support · corrodedCORROSION BEAM, OLES 1341, RT WING LE COMPARTMENT LOWER SUPPORT. REMOVED DAMAGE & MEASURED REWORKED AREA, LENGTH 3.1 IN. WIDTH = 23.0IN. DEPTH =0.014; WITHIN THE ALLOWABLE DAMAGE IAW SRM 57-41-13, ALLOWABLE DAMAGE 1 REV 32 DETAIL DATA. PLEASE REFER TO JC ATTSDR UIEA2015120900713Fitting · corrodedCORROSION CLIP, LT WING LE TO FRONT SPAR, LOWER CLIP AT HOLES 1360. REMOVE DAMAGE PART IAW SRM 51-40-02-06-0 REV 32 & PART FABRICATION IAW EI NR T2015P57B-2567 SEQUENCE A REV 0 & 3. INSTALLED FABRICATE PART IAW SRM 51-40-02-06-0 REV 32 & JOB COMPLETED & CONDSDR SWAA2016011948125Web · crackedRIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, WEB CRACKED. REPAIRED WEB IAW EA.SDR SWAA2016011948124Fitting · crackedRIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, FITTING CRACKED. REPAIRED FITTING IAW EA.SDR SWAA2016011948123Web · crackedLEFT WING FASTENER HOLES AT WING RSS 223.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW EA.SDR SWAA2016011948115Fitting · crackedLEFT WING FASTENER HOLE INBD OF WING RSS 224.14, FITTING CRACKED. REPAIRED FITTING IAW EA.SDR SWAA2016011147861Fitting · crackedRIGHT WING AFT MLG FITTING CRACKED AT RSS 221, COMMON TO UPPER CHORD. R & R FITTING IAW EA.SDR SWAA2015123147550Fitting · crackedRIGHT WING CLIP CRACKED AT RSS 234. R & R CLIP IAW SRM.SDR SWAA2015123047508Strap · crackedLEFT WING REAR SPAR, UPPER STRAP AT STATION 236 CRACKED. R & R STRAP IAW SRM.SDR ABXA20151202215Support Beam · corrodedRIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B657-61840 IAW SRM 51-40-02 GENERAL PG 7 PARA 70. CORRODED LEVEL 2, PN 113T1913024, PART NAME PANEL SDR SWAA2015120846877Link Assy · looseLEFT WING NR 2 FLAP SUPPORT, FAIRING LINK ASSEMBLY LOOSE. R & R LINK ASSEMBLY IAW AMM.SDR FDEA201512023852Web · crackedRIGHT WING, INTERNAL WEB CRACKED AT STATION XORS 402 & APPROX STRINGER 39. REMOVED DOUBLER FROM RT WING INTERNAL WEB AT STATION XORS 402 & APPROX STRINGER 39 & REPAIRED IAW EA 8-5700-T0321488.SDR SWAA2016010747746Stiffener · crackedLEFT WING REAR SPAR, STIFFENER CRACKED AT RSS 194.04. REPAIRED STIFFENER IAW EA.SDR SWAA2016010747758Angle · crackedRIGHT WING UPPER SKIN HOLE AT REAR SPAR, CRACKED AT APPROX RSS 249, AFT ROW. R & R ANGLE IAW SRM & ACO.SDR FDEA201511293817Strap · crackedRIGHT WING TE LOWER CHORD STRAP SILL FOUND CRACK AT WING STATION XORS 402. REMOVED IAW SRM 51-31-01-0G. NEW STRAP SILL FABRICATED BY MACHINING IAW DWG ARC7008 REV C. NEW FABRICATED STRAP SILL INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMSDR SWAA2016011948112Attach Angle · crackedLEFT WING OTBD FIXED TE, UPPER SURFACE PANEL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG.SDR SWAA2015121647196Bracket · crackedLEFT WING BRACKET, COMMON TO UPPER SPAR CHORD, CRACKED AT RSS 235. R & R CHORD IAW DWG & EA.SDR FDEA201511273796Fitting · crackedRIGHT FUSE, CTR WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL. PERFORMED ROTATING PROBE INSPECTION FOUND HOLE F HAVE CRACK SIGNAL. REAMED THE AFFECTED HOLE F TO REMOVE THE CRACK IAW SRM 51-40-44. INSTALLED THE OVERSIZED FASTENER IAW SRM 51-40-21. MINOR SDR LR7A2015112600635Fitting · crackedDURING UNSCHEDULED VISUAL INSPECTION IAW SP-158, FOUND OWS241.6L VERTICAL STIFFENER TO FLAP TRACK FITTING HAD CRACKED. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583 SRM CH 57-10 AND DWG 348627.SDR LR7A2015112600634Stiffener · crackedDURING UNSCHEDULED VISUAL INSPECTION IAW SP-158, FOUND OWS173L HAD A CRACKED VERTICAL STIFFENER ON BACK OF NR 1 DRY BAY WALL. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH 57-10 AND DWG 348626.SDR SWAA2016010747752Web · crackedLEFT WING UPPER WEB INBD & OTBD, BETWEEN RSS 220.14 - 225.14 AT THE FASTENER HOLE. REPAIRED WEB IAW EA.SDR SWAA2016010747751Web · crackedRIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW EA.SDR SWAA2016010747748Web · crackedRIGHT WING FASTENER HOLE AT WING RSS 225.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW ER & EA.SDR REXA2015112101201Stop Fitting · brokenPANEL 594JB HAS BUTE DOOR STOP TAB BROKEN OFF THE END OF THE PANEL. REMOVED THE BROKEN DOOR STOP AT PANEL 594JB IAW SRM 51-42-06. RECEIVED NEW DOOR STOP, PN 600-10196-15. INSTALLED TO PANEL 594JB IAW SRM 51-42-06. WORK SUMMARY STATEMENT REQUIRED. R & R DSDR A6WA201543272Web · crackedRIGHT WING OTBD LE WEB IS CRACKED, BETWEEN ACCESS PANELS 630KZ & 630LZ. R & R RT OTBD LE WEB, BETWEEN ACCESS PANELS 630KZ & 630LZ IAW SRM 51-42-13.SDR A6WA201543274Drag Angle · crackedLEFT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R LT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & SUP 15-287.SDR A6WA201543275Drag Angle · crackedRIGHT MLG WW DRAG ANGLE COMMON TO BAT RIB IS CRACKED IN THE AFT RADIUS. R & R RT MLG DRAG ANGLE COMMON TO BAT RIB IAW SRM 51-42-21.SDR A6WA201543273Drag Angle · crackedRIGHT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R RT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & AWAC SUPPLEMENT 15-287.SDR SWAA2015112346275Support Bracket · crackedRIGHT WING UPPER TE PANEL, BETWEEN NR 7 & 8 SPOILERS AFT SUPPORT BRACKET, CRACKED AT OTBD ATTACH FASTENERS. R & R BRACKET IAW DWG & SRM.SDR ABXA20151117205Channel · corrodedWING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51-40-02 & REA B657-61805. CORRODED LEVEL 2, PN 113T1912-3, PART NAME CHORD CHANNEL, SN NSN, FS & BSSDR SWAA2015120246617Plate · crackedLEFT WING WIGGLE PLATE ATTACHED TO LOWER WING SKIN TE AT APPROX RSS 248 CRACKED. R & R WIGGLE PLATE IAW SRM.SDR E4EB20151115006Cap · corrodedLT WING INBD LE FUEL TANK UPPER TE TEE CAP HAS INTERGRANULAR CORROSION. BETWEEN XFS 30.000 - 57.000.SDR SIMA20151113002Attach Angle · crackedRIGHT WING LOWER LATERAL FAIRING ATTACHMENT ANGLE, 3RD FROM THE AFT IS CRACKED. REPLACED ANGLE IAW SRM 51-40-02.SDR ABXA20151111206Support · corrodedAT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-05 TABLE 3 & 51-40-02-7. CORRODED LEVEL 2, PN 113T1632-197, SN N/A, PART NAME RIB TE PANEL SUPPORTSDR CA151110005Gasket · missing(CAN) DRY BAY GASKETS AT PANEL 621BT, AND PANEL 521AT DISCOVERED NOT INSTALLED DURING C CHECK. NO ASSOCIATED DAMAGE FOUND AND NEW GASKETS INSTALLED.SDR SWAA2016012648390Support Fitting · crackedLEFT WING REAR SPAR GROUP OF 7 HOLES, HOLE NR 5, CRACKED IN AFT SUPPORT FITTING AT 9 O' CLOCK POSITION. REPAIRED FITTING IAW EA.SDR SWAA2015120946902Fitting · crackedRIGHT MLG BEAM, FWD FITTING CRACKED AT FASTENER HOLE, SECOND ROW FROM INBD, THIRD FROM TOP. R & R FITTING IAW ER & EA.SDR CA151109009Washer · missing(CAN) MISSING WASHER ON OTBD WING FAIRING BOLT DURING THE INVESTIGATION OF AN ISSUE IN SERVICE, IT WAS NOTICED A MISSING WASHER ON THE INSTALLATION OF THE MAIN ROD 1005751802 WITH THE FLAP-FAIRING ATTACHEMENT, 1005751893 ON IML STRUCTURE OF FLAP-FAIRING ON SOMSDR SWAA2015120946915Angle · crackedLEFT WING ANGLE CRACKED ON TE AT WBL 183.40. R & R ANGLE IAW SRM & DWG.
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