JASC 5710
Service difficulty reports · 4,461
Reports filed under 5710 · Wing Main, Frame 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 = '5710' 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 = '5710' 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 FDEA202212050327Skin · corrodedLH WING UPPER SURFACE - APPROX XORS 213 STR 16 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIRSDR FDEA202212050326Skin · corrodedLH WING UPPER SURFACE - APPROX XORS 213 STR 16 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIRSDR FDEA202212050325Skin · corrodedLH WING UPPER SURFACE - APPROX XORS 122 STR 19 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIRSDR SWAA2023021477039Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 RBL 40 (WL 167)<[01] VERIFIED ITEM 1 OF STEP 7;[02] VERIFIED ITEM 3 OF STEP 7;[03] VERIFIED ITEM 4 OF STEP 7;[04] VERIFIED ITEN 2 OF STEP 9;[05] MISS SPELLED INTERNAL NOT ENTERNAL;[06] CAP SEALED EXTERNAL FASTNERS COMMSDR DALA2022120107704Barrier · not reportedSHIP 659 SECTION I REPAIR TO RH WING DRY BAY BARRIER AT WSTA 286.5-313.5 REQUIRES SECTION II REPAIR WITHIN 24 MONTHS PER ERA 603572-14. CORRECTIVE ACTION: REF ERA 603572-14. (2516112)SDR DALA2022113007651Rub Strip · corrodedCORROSION FLAP TRACK FAIRING 633CB RUBBER STRIP H WING. COMPLIED WITH ER/A #603935-14 PRI REV.ORIGINAL.SDR ASAA2022112840978Gasket · leakingRH WING FUEL PANEL 632KB SMALL FUEL LEAK. GROUNDED - YES. REMOVED PANEL #632KB ON RH WING. REPLACED GASKET & REINSTALLED RH WING LOWER FUEL 632KB IN REF TO B737-900 AMM 28-11-11-400-801, TRANSFER FUEL BACK, SOAKED FOR A HOUR, NO LEAKS NOTED. OK FOR SERVICE.SDR FDEA202211253002Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACKS 3EA LOCATED BETWEEN STA X46 AND X-46/STR47 (015-04) REMOVED, FABRICATED AND INSTALLED 3 EA STRINGER SECTION INSIDE UPPER CENTER AUXILIARY TANK AT STA X46 AND X-46 ON STR 47 IAW SRM 57-10-03-2R FIG 201 REPAIR 1. ORIGSDR FDEA202211232847Stiffener · unknownSTIFFNER APB 7278-1 REQUIRES FABRICATION. 0003883811 : CORDOVA, CARLOS - 27-NOV-2022 07:15 FABRICATED STIFFENER P/N APB7278-1 IAW DOUGLAS DWG APB7278SDR FDEA202211203005Plate · gougedRH WING LE SLAT TRACK NO 19 CUT OUT TRACK I/B & O/B PLATE HAS GOUGED AS MARKED 74- 015 REMOVED, FABRICATED AND INSTALLED PLATE AT R/H WING L/E SLAT TRACK #19 STA XOS= 1158 IAW SRM 57-00-00-2R FIG 202 REPAIR 2 AND DWR ARB1977.SDR SWAA2022123072921Access Panel · damagedLEFT WING FWD UNDER WING FAIRING PANEL 191FL, SCREW HOLES ELONGATED. NO WATER NOTE ON REPAIR AREA IAW SRM 51-70-04-2R-9 PARAGRAPH 4. APPLIED THE GLASS FABRIC REPAIR PLIES AT ACCESS PANEL IAW SRM 51-70-04-2R-9, PARAGRAPH 4. PAINTED REPAIR AREA IAW SRM 51-7SDR SWAA2022123072302Panel · elongatedRIGHT WING LOWER O/B TRAILING EDGE PANEL 671BB, SCREW HOLES ELONGATED. REPAIRED DAMAGE ON R/W LOWER OTBD TE PANEL 671BB IAW SRM 51-70-04-2R-9.SDR SWAA2022123072303Panel · damagedRIGHT WING LOWER O/B TRAILING EDGE PANEL #671AB; SCREW HOLES ELONGATED. REPAIRED IAW SRM 51-70-04-2R-9.SDR SWAA2022122072209Support · crackedL/W T/E ACCESS PANEL 561AB SUPPORT STRUCTURE CRACK.<[01] REMOVED AND REPLACED L/W T/E PANEL 561AB SUPPORT STRUCTURE PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED TABLE;[03] VERIFIED STEP 1;2SDR SWAA2022122072212Support · corrodedL/W T/E ACCESS PANEL 561AB SUPPORT STRUCTURE HAS CORROSION AROUND FASTENER HOLES.<[01] THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00G3L8S - FOUND CRACKED WILL BE REPLACE.;[02] VERIFIED STEP #1SDR SWAA2022120970310Rail · corrodedCORROSION INTERNAL CAVITY LEADING EDGE ON RAIL LOCATED AT OFSS 288 AND SS 53 ON BOTTOM SURFACE AT LEVEL OF RIB 8 AT LT WING. REPLACED RAIL LOCATED LEADING EDGE AT OFSS 288 AND SS 53 ON BOTTOM SURFACE AT LEVEL OF RIB 8 AT LT WING IAW SRM 51-10-02 AND B737-700 SDR SWAA2022120970312Rail · corrodedCORROSION FIXED LEADING EDGE ON RAIL LOCATED BOTTOM SURFACE AT LEVEL OF OFSS 449 SS214 AND AT LEVEL OF RIB 14 AT LT WING 2022-632461 / [01] REMOVED AND REPLACED RAIL ON FIXED LEADING EDGE LOCATED BOTTOM SURFACE AT LEVEL OF OFSS 449 SS214 AND AT LEVEL OF RIB 14SDR SWAA2022120969873Rail · brokenBROKEN O/B FIXED LEADING EDGE RAIL LOCATED AT LEVEL OFSS 722 AND SS 487 AND BETWEEN RIB 24 TO RIB 25 ON BOTTOM SURFACE AT LT WING 2022-632427 / [01] REPLACED RAIL LOCATED O/B FIXED LEADING EDGE AT LEVEL OFSS 722 AND SS 487 AND BETWEEN RIB 24 TO RIB 25 ON BOTTOSDR SWAA2022111770017Attach Angle · crackedCRACK FOUND ON STA. 663 VERTICAL LEG OF ATTACH ANGLE COMMON TO DRAIN VALVE LOWER I/B NUTPLATE HOLE AT RBL 32 WL 193 / [01] VERIFIED CRACK FROM DRAIN CUTOUT TO INBD NUTPLATE HOLE ON LOWER ATTACH ANGLE VERTICAL LEG IAW B737 NDT PART 6 51-00-00 PROCEDURE 23. TOOLSDR SWIA202266930Structure · damagedFOUND HOLE IN UNDERLYING STRUCTURE IN THE FOOTPRINT OF PANEL 594UB TO BE DAMAGED REPAIRED THE STRUCTURE IAW REO 601R-57-51-1003, REV-.SDR FDEA202211092744Former · crackedR/H WING FORMER AT STA. 499 CRACKED. COMPLIED WITH E..A. H-5720-T0371575 REV P1.SDR FDEA202211092743Former · crackedR/H WING FORMER AT STA. 565 CRACKED. COMPLIED WITH E..A. H-5720-T0371575 REV.SDR FDEA202211082905Skin · corrodedBUSHING FOR DRAIN HOLE AT CENTER WING UPPER SKIN AT REAR SPA APPROX BETWEEN XCW 101 AND XCW 118 REQUIRES TO BE FABRICATED WITH DIM. AS FOLLOW: DIA = 0.750, HEIGHT = 0.675 FABRICATED BUSHING PER EA 1-5710-T0370445 P3 WINGS - PLATES AND SKIN - CENTER WING - SDR COEA2022120706807Landing · corrodedDURING HEAVY CHECK, RT UPPER WING CUTOUT 622CT HAS LEVEL 2 CORROSION ON LANDING. REPAIRED IAW SRAS DO/TS-3854/07_4243 ISSUE H,SDR YENA2022110101059Rib · crackedDURING HEAVY MAINTENANCE: CRACK ON LOWER SKIN PANEL RIB 10 LH WING; REF TOMX WO 1989- NR 00163; ACCOMPLISHED REPAIR OF SKIN PANEL RIB 10 LH WING E190-SRM 57-10-01 / REPAIR 54.SDR J7SA2022111000339Wedge · corrodedDISCOVERED CORROSION ON LEFT AND RIGHT WING WEDGE PANEL IB TRAILING EDGE BOX PANEL INTERFACE. GAINED ACCESS TO CORRODED LH AND RH WEDGE ANGLES. REPLACED MATCH DRILLED WEDGE ANGLES. WORK COMPLETED IAW GAC DRAWINGS 1159W40166 REV D. 1159W40003 REV N. AND 1159W20SDR J7SA2022103100337Wedge · corrodedDISCOVERED CORROSION ON LEFT AND RIGHT WING WEDGE PANEL IB TRAILING EDGE BOX PANEL INTERFACE. REPLACED RH WING TAPERED WEDGE FITTING. REPLACED LH WING TAPERED WEDGE FITTING. WORK COMPLETED IAW G450 SRM 51-41-00.SDR COEA2022122312807Fitting · damagedL/H WING FRONT SPAR LOWER FLANGE NACELLE ATTACH FITTING AT RIB 12 OUTBOARD BOLT HOLE HAS A FLAW INDICATION COMMON TO THE LOWER WING SKIN. CORRECTIVE ACTION: REPAIR PER SRAS ES_00204175_01...19870 ISSUE A,SDR IXXA2022112703Beam · corrodedCORROSION AREA ON BEAM PN 113T1911-40 BETWEEN WS841.20 & WS811.20 APPROX IN LENGTH 30".SDR SWAA2022111765810Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68 / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 TO BE CORRECT AND UPDATED MEASUREMENT TABLE;[09] RECIEVED REPAIR PARTS 1EA REPAIR DOUBLER MATERIAL USED 2024T3 CLAD 0.071' LOT# 1452482-1 SDR SWAA2022111765809Attach Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68 / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 TO BE CORRECT AND UPDATED MEASUREMENT TABLE;[09] RECIEVED REPAIR PARTS 1EA REPAIR DOUBLER MATERIAL USED 2024T3 CLAD 0.071' LOT# 1452482-1 SDR SWAA2022112264981Beam · crackedFOUND 2 E/A CRACK O N INTERNAL BEAM 2022-585731 / [01] REMOVED AND REPLACED SLAT 7 DUE TO 2 E/A CRACK FOUND ON INTERNAL BEAM IAW B737-700 AMM 27-81-21-000-801 AND 27-81-21-40-801; AND PERFORMED LEADING EDGE SLAT ADJUSTMENT IAW B737-700 AMM 27-81-00-820-803.SDR CALA2022102702943Attach Angle · crackedLOWER FUS CENTER WING R/H VAPOR BARRIER UPPER ATTACHED ANGLE CRACKED AT RBL 10 STA 663.75 REF AAR N/R 9512277 REPAIR LOWER FUSE CENTER WING R/H VAPOR BARRIER UPPER ATTACHED ANGLE AS PER REF B737 SRM 57-10-10-2R-5 REPAIR 5 MAT USED 2027-T3 0.071 AND 2024-T3 0.0SDR FDEA202210222644Former · crackedL/WING FLE OSS 499 HAS A CRACKED FORMER REPLACED FORMER B67-57-002-03 AT L/WING FLE OSS 499 USING EA H-5720-T0371261 AS REFERENCE.SDR SWAA2022111762416Support Bracket · brokenBROKEN SUPPORT BRACKET ON ACCESS PANEL 651FB, RT WING. REPLACED THE SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SDR SWAA2022111761875Support Bracket · crackedCRACK TRAILING EDGE BRAKET SUPPORT LOCATED IRSS 142, LT WING. REPLACED TRAILING EDGE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9.SDR SWAA2022102861936Angle · crackedSTA 663 CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARREIR IS CRACKED AT RBL 10 WL 170.85 / [01] ATTACH ANGLE BEEN REPAIRED ON N/R # TTG8Q00FJLLX I.A.W SRM 57-10-10-2R-5;[02] VERIFIED JOB COMPLETE; AUDIT C/WSDR DALA2022102106833Barrier · damagedSHIP 655 SECTION I REPAIR TO RH WING DRY BAY BARRIER AT WSTA 231.50- 258.50 REQUIRES SECTION II REPAIR WITHIN 24 MONTHS PER ERA 602946-14. CORRECTIVE ACTION: REF ERA 602946-14. (2459437)SDR SWAA2022102161184Barrier · crackedRIGHT MLG WHEEL WELL LOWER RIGHT VAPOR WEB BARRIER HAS A CRACK APPROXAMATLY 6 INCHES LONG BETWEEN RBL 32.00 AND RBL 36.00. CRACK INITIATES AT A FASTENER AT TERMINATES AT A FASTENER. / [01] AS PER AVIATION PARTNERS BOEING SRM SUPPLEMENT 57-10-10 ALLOWABLE DAMAGSDR SWAA2022102861077Attach Angle · crackedSTA 663 CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARREIR IS CRACKED AT RBL 50; WL 170.85 / [01] VERIFIED PARTIALS FOR STEPS 2 - 4;[02] VERIFIED STEPS 1; 5; 7 AND 8;[03] STEP 9 C/W;[04] STEP 11 C/W;[05] REPAIR PARTS BEEN INSTALLED I.A.W SRM 57-1010-2R-5 NSDR FDEA202210172589Former · crackedL/H FIXED LEADING EDGE FORMER CRACKED AT OSS 441 0000280794 : SHAEFFER, DAVID C - 18-OCT-2022 04:30 REPLACED CRACKED FORMER REF EA TH-5720-T0371169 P1SDR SWAA2022111660597Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING 2022-584665. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2001 SHEET 18 REV -.SDR SWAA2022112259778Panel · damagedRIGHT WING T/E PANEL 661BB HAD SEVERAL PULLED FASTENER HOLES. REPAIRED IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & E .;SDR IXXA20221306Support Beam · corrodedRIGHT WING T/E PANEL SUPPORT BEAM HAS CORROSION ON TOP APPROX W.S. 216.SDR SWIA202266923Landing · corrodedLEFT WING PLANK HAS SEVERAL AREAS OF CORROSION AROUND FUEL PANEL 540BB OPENING. REPAIRED THE WING PANEL LANDING IAW 601R-57-21-0030 REV-, MAJOR REPAIR TASK CARD 51-900-1003-SKY.SDR SWAA2022111058069Angle · crackedCRACK BODY FAIRING STRUCTURE SUPPORT ANGLE LOCATED BS500D AT LEVEL STR19L AT LOWER FUSELAGE 2022-562006 / [01] REPLACED BODY FAIRING STRUCTURE SUPPORT ANGLE AND STRAP LOCATED BS500D AT LEVEL STR19L AT LOWER FUSELAGE I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-0SDR SIMA20221009005None · crackedLH WING SPAR I IS CRACKED IN THE LOWER OUTBD FLANGE RADIUS (MAJOR REPAIR) -C/A-REMOVED AND REPLACED L/H OUTBD WING SPAR 1 IAW EMB 175 SRM 51-40-08SDR SWAA2022111057785Plate · crackedCRACK INTERNAL CAVITY CORRUGATED PLATE IRSS 224 ON RT MAIN LANDING GEAR 2022-561896 / [01] REPLACED CORRUGATED PLATE LOC. ON IRSS 224 ON RT MAIN LANDING GEAR I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DWG # 115A2001 SHEET 18 REV. -. DUE TO NOT FOUND SDR FDEA202210072513Former · crackedR/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-14) REPLACED PARTS WITH NEW FORMER B67-57-002-04 ALONG WITH ANGLE B67-57-003-04 ON RS FOR FLE OSS 499, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND NSDR FDEA202210072512Former · crackedR/H WING AT STATION OSS.441 L/E FORMER IS CRACKED (P/N: 114T2170-6) REPLACED PARTS WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FOR FLE OSS 441, ATTACHED FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND
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