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 SWAA2023061548548Angle · crackedCRACK ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING 2023-310574<[01] REPLACED ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 ANDSDR IPXA2023052193285Doubler · crackedINSPECTION TYPE:C3*** MAJOR REPAIR *** L/H INNER FIXED LE HAS A CRACKED BEADED DOUBLER AT APPROX. XOS=629.6 - XOS=633.4 RIB BAY.CUT OUT DAMAGED SECTION OF BEADED DOUBLER AND INSTALLED REPAIR DOUBLER AT STA APPROX. XOS=629.6 - XOS=633.4 RIB BAY IAW MD-11 SRM 57SDR SWAA2023061447034Barrier · cracked** PER CUSTOMER REQUEST ** LEFT HAND VAPOR BARRIER CRACKED AND STOP DRILLED O/B AREA<[01] REPAIRED L/H VAPOR BARRIER AT DAMAGED AREA PER B737 SRM 51-70-04-2R-0 PARA 4.L.7. MATERIALS USED RESIN P/O#1800550; CLOTH P/O#1738579. PERFORMED VISUAL AND TAP TEST INSPESDR SWAA2023062646842Angle · corrodedL/W #1 TANK FWD BOOST PUMP UPPER BONDING JUMPER ATTACH POINT IS CORRODED ON FRONT SPAR<[01] SRM 57-20-10-1A-3 IS APPLICABLE TO THIS REPAIR.[05] REMOVED CORROSION ON LEFT WING FRONT SPAR AROUND BOOST BUMP UPPER BONDING JUMPER L= 4.6' W = 2.4' IAW SRM 57-20-10-1SDR SIMA20230508001Rib · crackedRIGHT WING LEADING EDGE RIB #36 IS CRACKED AT UPPER AFT FLANGE. (MAJOR REPAIR)-C/A-REMOVED AND REPLACED RIGHT WING LEADING EDGE RIB #36 IAW EMB 170 SRM 51-40-08.SDR DALA2023050803611Unknown · unknownAIRCRAFT 3570, SEALANT FOUND DETERIORATED AND MISSING UPON INSPECTION PER AMDS #5720-01102-03A STEP #6 AT THE FOLLOWING LOCATION: RB #13, STR #11, LOWER SKIN, INBOARD SIDE ONLY. TO APPLY SEALANT 06ABB1 ON AFFECTED AREAS PER AMDS #5720-01102-03A STEP #20. CORRESDR DALA2023050803609Unknown · unknownAIRCRAFT 3570, SEALANT FOUND DETERIORATED AND MISSING UPON INSPECTION PER AMDS #5720-01102-03A STEP #6 AT THE FOLLOWING LOCATION: RB #11, STR #10, LOWER SKIN, OUTBOARD SIDE ONLY. TO APPLY SEALANT 06ABB1 ON AFFECTED AREAS PER AMDS #5720-01102-03A STEP #20. CORRSDR DALA2023050803608Unknown · unknownAIRCRAFT 3570, SEALANT FOUND DETERIORATED AND MISSING UPON INSPECTION PER AMDS #5720-01102-03A STEP #6 AT THE FOLLOWING LOCATION: RB #11, STR #13, LOWER SKIN, OUTBOARD SIDE ONLY. TO APPLY SEALANT 06ABB1 ON AFFECTED AREAS PER AMDS #5720-01102-03A STEP #20. CORRSDR DALA2023050803607Unknown · unknownAIRCRAFT 3570, SEALANT FOUND DETERIORATED AND MISSING UPON INSPECTION PER AMDS #5720-01102-03A STEP #6 AT THE FOLLOWING LOCATION: RB #2, STR #2, UPPER SKIN, BOTH SIDES AFFECTED. TO APPLY SEALANT 06ABB1 ON AFFECTED AREAS PER AMDS #5720-01102-03A STEP #20. CORRESDR DALA2023050803606Unknown · unknownAIRCRAFT 3570, SEALANT FOUND DETERIORATED AND MISSING UPON INSPECTION PER AMDS #5720-01102-03A STEP #6 AT THE FOLLOWING LOCATION: RB #2, STR #2, UPPER SKIN, BOTH SIDES AFFECTED. TO APPLY SEALANT 06ABB1 ON AFFECTED AREAS PER AMDS #5720-01102-03A STEP #20. CORRESDR SWAA2023061648123Barrier · crackedRH WHEEL WELL FWD ANGLE SUPPORT VAPOR BARRIER HAS ONE CRACK AT STA 663;RBL 55<[01] REMOVED AND REPLACED ANGLE SUPPORT AT R/H VAPOR BARRIER; STA 663; RBL 55 AS PER B737-700 SRM 51-40-02-0G-0; DWG # 111A1000.;[02] VERIFIED STEP 1SDR SWAA2023061647756Barrier · crackedLH WHEEL WELL;FWD ANGLE SUPPORT VAPOR BARRIER HAS TWO CRACKS AT STA 663;LBL 8 AND LBL 55<[01] REMOVED AND REPLACED LH WHEEL WELL; FWD ANGLE SUPPORT VAPOR BARRIER STA 663 REF B737; SRM 51-40-02-0G-0 (REMOVAL) AND SRM 51-40-02-0G-0 AND DWG # 111A1000 (INSTALLATISDR JR2R20230506544Angle · crackedLH WING SPAR 2 LOWER STUB ANGLE CRACKED ON THE FWD SIDE OF THE LH MLG WHEEL WELL FWD BULKHEADSDR SWAA2023061652483Beam · crackedR/W UPPER INBOARD FIXED TRAILING EDGE BEAM AT WBL 201.90 FOUND CRACKED<[01] REMOVED AND REPLACED BEAM AT RT WING UPPER I/B T/E WBL 201.90 REF B737-700 SRM 51-40-02-0G-0 (REMOVAL) AND SRM 51-40-02-0G-0 AND DGW# 115A2512 (INSTALLATION);[02] VERIFIED STEP 1SDR IPXA2023050493119Plate · crackedINSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SIDE PLATE R/H SIDE BETWEEN FR76 AND FR77 CRACKED.REMOVED AND REPLACED PLATE IAW-SRM 51-40-21SDR FDEA202305010784Cap · corrodedRIGHT WING - TRAILING EDGE REAR SPAR UPPER CAP AT XORS 1043 FOUND CORROSION. RIGHT WING TRAILING EDGE REAR SPAR UPPER CAP AT XORS 1043 CORRODED AREA REPAIR CARRIED OUT AS PER EA# 1-5710-T0374279 PART 1, TITLE : WINGS - BASIC WING STRUCTURE - RH WING - CORSDR SWAA2023060543508Barrier · crackedCUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT STA 663 RH SIDE. 2023-299201<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17/OCT/23.;[02] TOOL USED HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 22/JAN/24.;[03] TOOL USED: SCALE P/N: CR520SDR SWAA2023052443079Panel · crackedBREAK ASSEMBLY PANEL CRACKED IB OF #2 SEAT TRACK AT LH STA 537.45. PN 143A5240-35.<[01] INSTALLED PANEL 143A5240-33 PER SRM 51-40-02;[02] CWSDR SWAA2023050541936Web · crackedLH VAPOR BARRIER FWD WEB AT LBL 20 FOUND CRACKED<[01] REMOVED; FABRICATED AND REPLACED CRACKED LH VAPOR BARRIER FWD WEB AT LBL 20 AS PER SRM 51-40-02-0G-0 AND DWG#111A1000.;[02] CARD COMPLETEDSDR FDEA202304270765Cap · corrodedRIGHT HND WING TRAILING EDGE LOWER SPAR CAP FOUND WITH CORROSION AT STATION XORS 1052. RIGHT HAND WING TRAILING EDGE LOWER SPAR CAP CORROSION AT STATION XORS 1052 REPAIRED AS PER EA # 1-5710-T0374193 P1 TITLE: WING - BASIC WING STRUCTURE - RH WING LOWERSDR SWAA2023053142055Winglet · delaminatedRH WINGLET AFT (CARBON FIBER) SPAR ;SIGNS OF DELAMINATION AND LOOSE FIBERS AT MOST UPPER TOOLING HOLES.<[01] DAMAGE FOUND AT RH WINGLET UPPER SKIN INTERNAL AREA OUTSIDE OF AAR MIAMI REPAIR CAPABILITIES; WINGLET TO BE REPLACED. INSTALL ACCOMPLISHED ON ROUTINE CSDR SWAA2023053142056Winglet · delaminatedLH WINGLET AFT (CARBON FIBER) SPAR ;SIGNS OF DELAMINATION AND LOOSE FIBERS AT MOST UPPER TOOLING HOLES.<[01] DAMAGE FOUND AT LH WINGLET UPPER SKIN INTERNAL AREA OUTSIDE OF AAR MIAMI REPAIR CAPABILITIES; WINGLET TO BE REPLACED. INSTALL ACCOMPLISHED ON ROUTINE CSDR SWAA2023050542211Barrier · delaminatedCUSTOMER REQUEST : LEFT VAPOR BARRIER - HAS REPAIR APPEARS TO BE LIFTING AT HE EDGE.<[01] APPLIED A PERMANENT REPAIR ON DAMAGED AREA AT L/H VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-10. MATERIALS USED PO#1800550 AND PO#1690463;[02] VERIFIED 1 PERMANENT REPAIR SDR SWAA2023050541685Angle · crackedCENTER TANK LEFT HAND LOWER ATTACH ANGLE HAVE CRACK IN OPEN HOLE AT STA 663; LBL 31.83 ; W/L 168.54 CENTER TANK LEFT HAND LOWER ATTACH ANGLE HAVE CRACK IN OPEN HOLE AT STA 663 LBL 31.83 W/L 168.54<[01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTSDR FDEA202304260761Tee Fitting · corrodedLT WING: REAR SPAR UPPER CAP - STA. XORS 981-1042(FWD. OF O/B AILERON) - EVIDENCE OF SURFACE CORROSION AROUND SEVERAL FASTENER HOLES (2). REMOVED CORROSION ON LT WING REAR SPAR UPPER CAP @ STA XORS 981-1042 PER SRM 51- 21-01 07. REPAIRED PER E.A 1-5710-T3738SDR SWAA2023053141641Support Beam · wornLEFT WING DEFLECTOR PANEL UPPER SUPPORT BEAM WORN<SDR DALA2023042903350Unknown · unknownAIRCRAFT 3502, INSPECTED RIGHT OUTER WING FUEL TANK GLOW SEALANT ON RIGHT WING. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-01B. (LP 2736250)SDR DALA2023042903349Unknown · unknownAIRCRAFT 3502, INSPECTED LEFT OUTER WING MIDBOX FUEL TANK GLOW SEALANT ON LEFT WING. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-01A. (LP 2736245)SDR DALA2023042903348Unknown · unknownAIRCRAFT 3502, INSPECTED OUTER WING GLOW SEALANT FOR OPTIMISATION IN RIGHTWING FUEL TANK. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-05B. (LP 2736243)SDR DALA2023042903347Unknown · unknownAIRCRAFT 3502, INSPECTED OUTER WING GLOW SEALANT FOR OPTIMISATION IN LH WING FUEL TANK. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-01A. (LP 2736237 )SDR DALA2023042903346Unknown · unknownAIRCRAFT 3502, INSPECTED OUTER WING GLOW SEALANT FOR OPTIMISATION IN RIGHT WING FUEL TANK. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-01A. (LP 2736232)SDR DALA2023042903345Unknown · unknownAIRCRAFT 3502, INSPECTED OUTER WING GLOW SEALANT FOR OPTIMISATION IN LH WING FUEL TANK. CORRECTIVE ACTION: REMOVED NECESSARY SEALANT AND RESTORED WING GLOW SEALANT PER WC 5720-1102-07A. (LP 2736228 )SDR SWAA2023050531147Web · crackedRIGHT HAND 663 VAPOR BARRIER WEB IS CRACKED AT RBL 50<[01] EVALUATED R/H 663 VAPOR BARRIER AND FOUND A CRACK 4.5' AT RBL 50. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A & NOTE. CLEAN AND PREP. IAW B737-700 SRM 51-70-04-2R-10 PAR 4A-C. VERIFY SDR SWAA2023050530386Angle · crackedCENTER TANK RIGHT HAND LOWER ATTACH ANGLE IS CRACKED AT STA 663; RBL 8; W/L 168.54<[01] ANGLE BEEN REPAIRED ON N/R TTG8Q00KKYZ9 I.A.W SRM 57-10-10-2R-5;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR FDEA202304220740Rib · crackedLEFT HAND WING LEADING EDGE #8 SLAT INTERNAL RIB FOUND CRACK DURING BORESCOPE INSPECTION AT STATION XOS 1086.831. CRACKED RIB AT LEFT HAND WING #8 SLAT INTERNAL AT STATION XOS 1086.831 REPAIRED AS PER EA# 1-5750-T0374170 PART 1 TITLE: WINGS -FLIGHT SURFACESDR FDEA202304220739Rib · crackedLEFT HAND WING LEADING EDGE #8 SLAT INTERNAL RIB FOUND CRACK DURING BORESCOPE INSPECTION AT STATION XOS 1092.115. CRACKED RIB AT LEFT HAND WING #8 SLAT INTERNAL AT STATION XOS 1092.115 REPAIRED AS PER EA# 1-5750-T0374170 PART 1 TITLE: WINGS -FLIGHT SURFACESDR FDEA202304220738Rib · crackedLEFT HAND WING LEADING EDGE #8 SLAT INTERNAL RIB FOUND CRACK DURING BORESCOPE INSPECTION AT STATION XOS 1130.033. CRACKED RIB AT LEFT HAND WING #8 SLAT INTERNAL AT STATION XOS 1130.033 REPAIRED AS PER EA# 1-5750-T0374170 PART 1 TITLE: WINGS -FLIGHT SURFACESDR FDEA202304220737Rib · crackedLEFT HAND WING LEADING EDGE #8 SLAT INTERNAL RIB FOUND CRACK DURING BORESCOPE INSPECTION AT STATION XOS 1135.627. CRACKED RIB AT LEFT HAND WING #8 SLAT INTERNAL AT STATION XOS 1135.627 REPAIRED AS PER EA# 1-5750-T0374170 PART 1 TITLE: WINGS -FLIGHT SURFACESDR FDEA202304220736Rib · crackedLEFT HAND WING LEADING EDGE #8 SLAT INTERNAL RIB FOUND CRACK DURING BORESCOPE INSPECTION AT STATION XOS 1141.220. CRACKED RIB AT LEFT HAND WING #8 SLAT INTERNAL AT STATION XOS 1141.220 REPAIRED AS PER EA# 1-5750-T0374170 PART 1 TITLE: WINGS -FLIGHT SURFACESDR SWAA2023050530376Angle · crackedCENTER TANK RIGHT HAND LOWER ATTACH ANGLE IS CRACKED AT STA 663; RBL 48; W/L 168.54<[01] STARTED REMOVEING STA 663 CENTER TANK RIGHT HAND LOWER ATTACH ANGLE IAW SRM 51-40-02-0G-0 SRM 57-10-10-2R-5 FIG 202;[02] VERIFIED ITEM 1 OF STEPS 1 AND 2;[03] COMPLETED RESDR SWAA2023042029470Spar · crackedCOMPLIED WITH REINSPECT; FOUND CRACK EXTENDED PAST STOP DRILL 4 INCHES<[01] PERFORMED INTRIM REPAIR PER SRM 57-10-10-01A-2; DVI EVERY 1200 CYCLES; OK TO CONTINUE ON TLDSDR SWAA2023052429272Support · crackedWING BOX CENTER SECTION - FLOOR SUPPORT HAS A CRACK BS 540 LBL 2<[01] REMOVED CRACKED WING BOX CENTER SECTION - FLOOR SUPPORT BS 540 BL 0 - LBL 25 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW WING BOX CENTER SECTION - FLOOR SUPPORT BS 540 BL 0 - LBL 25 IAW SRSDR FDEA202304190702Bracket · crackedR/H WING INBD L/E AREA HAS 1EA SLAT TORQUE TUBE GUIDE ATTACH BRACKET CRACKED IN MULTIPLE LOCATIONS AT APPROX IFSS 280 REMOVED AND REPLACE TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02 AND BAC DWG 114T1240 SHEET 2 REVISION E.SDR FDEA202304190698Unknown · unknownRIGHT HAND WING LEADING EDGE INTERNAL SUPPORT BEADED DOUBLER FOUND CRACK BETWEEN STATION 659-667. RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT DOUBLER AT BETWEEN XOS 659 - 667 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CSDR FDEA202304190697Unknown · unknownRIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT BEADED DOUBLER FOUND CRACK AT STATION XOS 638. RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT DOUBLER AT STATION XOS 638 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSSDR FDEA202304190675Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT BEADED DOUBLER FOUND CRACK BETWEEN STATION 659 - 667. LEFT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT DOUBLER BETWEEN STATION XOS 659-667 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202304190674Stringer · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT STRINGER FOUND CRACK BETWEEN STATION 659 - 667. LEFT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT STRINGER BETWEEN STATION XOS 659-667 REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAISDR SWAA2023052528800Barrier · crackedRH VAPER BARRIER IS CRACKED AT BS 663; RBL38; WL 159.<[01] IDENTIFIED THE PANEL IAW SRM 57-10-10-0I-2 FIGURE 2 ITEM [4]. DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARAGRAPH 4.D.(1) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-10 PER SRM SDR SWAA2023052228246Panel · corrodedRT WING L/E FUELING STATION AT 621GB DOOR - P-15 PANEL HAS SURFACE CORROSION AROUND I/B AND O/B GAUGES. 124-011<[01] FAULT WAS RESOLVED ON ANOTHER FAULT. FAULT NUMBER TTG8Q00KFP2Q;;[02] VERIFIED TTG8Q00KFP2QSDR COEA2023061513919Slat · chafedWO 246760 NR 600013 HEAVY CHECK COE/MAJOR REPAIR: R/H WING FRONT SPAR LOWER STRIP SLAT, BOTTOM SURFACE IS CHAFED BETWEEN RIBS 4R-5R. CORRECTIVE ACTION: REPAIR PER SRAS ES_00217384_01...20844 ISSUE A, DATED 6/6/2023.
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