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 SWAA2023072775941Panel · damagedPANEL 195BL HAS SEVERAL FASTENERS HOLE ELONGATED<[01] APPLIED REPAIR IN DAMAGED AREA (FASTENERS HOLES ELONGETED) AT PANEL #195BL AS PER B737 SRM 51-70-04-2R-9; MARERIAL USED PO# 1776837;PO#2012656 AND PO#1738579. APPLIED TOPCOAT ON PANEL 195BL REF B737 AMM 51-SDR SWAA2023072778135Panel · damagedPANEL 194CL HAS SEVERAL FASTENERS HOLE ELONGATED.<[01] REPAIRED DAMAGE FASTENERS HOLES AS MARKED WITH A PERMANENT REPAIR AS PER B737SRM 51-70-04-2R-9 .MATERIALS USED PO#2008859 AND PO#1738579;[02] PERFORMED TAP TEST INSPECTION ON REPAIRED AREAS ;FOUND NO DELAMSDR SWAA2023072778684Panel · damagedPANEL 195CL HAS SEVERAL FASTENERS HOLE ELONGATED.<[01] REPAIRED PANEL #195CL AT DAMAGED ELONGATED HOLES PER B737 SRM 51-70-04-2R-9 PARA 4.E. MATERIALS USED RESIN P/O#2012656; CLOTH P/O#1738579;[02] ADD ON STEP 1 PERFORMED TAP TEST INSPECTION ON REPAIRED AREAS SDR SWAA2023072670840Winglet · crackedLEFT WING; WINGLET SPLIT SCIMITAR UPPER END HAS POSSIBLE CRACK 8' BELOW UPPER CAP. (MARKED)<[01] REMOVED DAMAGED STRAKLET FROM A/C INVENTORY AND REPLACED WITH NEW SERVICEABLE STRAKLET. STRAKLET TO BE INSTALLED ON MT# 757-31-01 (INSP - INTERNAL - LEFT WINGSDR SWAA2023072865860Frame · crackedLW INBD FIXED L/E WTB END RIB ASSEMBLY STRAKELET FRAME SHOWS EVIDENCE OF CRACK.<[01] REMOVED AND REPLACED AT L/W INBD FIXED L/E END RIB THE STRAKELET FRAME AS PER B737-700 SRM 51-40-02-0G-0 AND DWG# 116A3110;[02] VERIFIED STEP 1SDR SWAA2023072865861Frame · crackedRW INBD FIXED L/E WTB END RIB ASSEMBLY STRAKELET FRAME FOUND CRACKED.<[01] REMOVED AND REPLACED AT RW INBD FIXED L/E WTB END RIB THE STRAKELET FRAME AS PER B737-700 SRM 51-40-02-0G-0 AND DWG# 116A3110;[02] VERIFIED; STEP # 1SDR R61A2023070800386Bushing · elongatedWHILE ACFT IN HEAVY CHECK AND PERFORMING 170EO-57-10-0017 F52 REINF & RR AILERON TORQUE TUBE SUPPORTS. FOUND 2EA. STUCK FASTENERS FOR REMOVAL THROUGH AILERON TORQUE TUBE SUPPORT FITTINGS. PERFORMED PERMANENT REPAIR BY REAMING HOLE AND FABRICATING AND INSTALLINSDR SWAA2023081460413Support · crackedMAIN CABI CENTER WING BOX FLOOR SUPPORT INNER CHORD CRACKED AT STA 520 LBL 64 WL 208.1<[01] VERIFIED / INSPECTED REPAIR ACCOMPLISHED AT CABIN FLOOR STRUCTURE STA 520 LBL 64 WL 208.1. FABRICATED PARTS REPAIR DOUBLERS. INSTALLED. REF. FABRICATED INNER CHORD CREASDR CALA2023061901919Unknown · corroded(SUPPORT TASK) RH WING INSIDE LEADING EDGE COVE AT APPROXIMATE WING STATION 180 - CORROSION NOTED ON FRONT SPAR LOWER CHARD REPAIR WAS ACCOMPLISHED FROM KRAS 173 TO KRAS 197 AND REQUIRES EC/RA 5720-03341 (LATEST REVISION) ON OR BEFORE 18 MONTHS FROM PERMANENT SDR SWAA2023071759572Panel · pulledR/W L/E PANEL 621PB HAS PULLED FASTENER HOLE (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-41-01-0I-4 FIGURES 1+3; TABLE 3; ITEM [1].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR 4.A (5).<BR>A PERMANENT REPAIR WILL BE SDR SWAA2023071759574Panel · pulledL/W L/E PANEL 621HB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621HB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 4; SHEET1; TABLE 4; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. SDR SWAA2023071759577Panel · pulledR/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621SB MATERIAL IAW SRM 57-41-01-0I-4 TABLE 3 FIGURE 3 ITEM 1. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A(5). DAMAGE IS REPAIRABLSDR SWAA2023071759970Panel · pulledL/W L/E PANEL 521TB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521TB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759974Panel · pulledL/W L/E PANEL 521JB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 4 TABLE 4 ITEM 1.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED SDR SWAA2023071759973Panel · pulledL/W L/E PANEL 521MB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 521MB IAW SRM 57-41-01-0I-4 FIGURE 4 ITEM [1]; DAMAGE TO THE PANEL IS BEYOND THE ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A.(4).(C) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759972Panel · pulledL/W L/E PANEL 521QB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521QB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759971Panel · pulledL/W L/E PANEL 521WB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521WB PANEL IAW SRM 57-41-01-0I-4 FIGURE 2; ITEM 1; TABLE 2<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759976Panel · pulledL/W L/E PANEL 521CB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 3.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED SDR FDEA202306141036Beam · crackedL/H WING T/E SUPPORT STRUCTURE IS CRACKED AT APPROX WS 1030 REMOVED & REPLACED LEFT WING TRAILING EDGE PANEL SUPPORT BEAM IAW BAC DWG 113T1913, REVISION ASDR SWAA2023062858776Angle · crackedCRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE. CRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE.<[01] INSTALLED REPAIR AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 PER REF SRM 57-10-10-2R-5 REPASDR SWAA2023062858775Angle · crackedLOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 7 STA 663.75 MKD DOT LOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 9.25 STA 663.75 MKD DOT<[01] ACCOMPLISHED REPAIR AT RT. VAPOR BARRISDR SWAA2023062857472Barrier · crackedRIGHT VAPOR BARRIER HAS SIGNS OF CRACK.<[01] REPAIRED DAMAGED AREA AT RIGHT VAPOR BARRIER PER B373 SRM 51-70-04-2R-0 PARAGRAPH (4.N.2) MATERIAL USED RESIN EY-3804 PO#1800550 AND FIBER GLASS BMS9-3 PO#1738579; PERFORMED VISUAL INSPECTION AND TAP TEST ON REPAIR SDR SWAA2023070556262Bracket · brokenL. WING T/E BULB SEAL BRACKET IS BROKEN AT ORSS 269.<[01] REMOVED AND REPLACED L. WING T/E BULB SEAL BRACKET AT ORSS 269 PER SRM 51-40-02-0G-0 AND IPC 57-50-00-25;[02] VERIFIED CORRECTIVE ACTION 1SDR ASAA2023060643478Plate · wornWHILE REPLACING OUTBOARD FWD STRIKER PLATE FOR ECS DOOR (192DR) FOUND DAMAGE UNDER STRIKER PLATE IN STRUCTURE MEASURING .093" DEEP, .281" LONG AND .156' WIDE. GROUNDED - YES. REF MIG-5 L/P 300010908 FOR PERMANENT REPAIR PER SRM 57-10-13-2R-3 REPAIR 3. ACC PERMSDR DALA2023060604614Unknown · unknownSHIP 660 MIGRATED BUSHING AT FWD UPPER SPAR OF UPPER LINK ON RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00629.FWD UPPER SPAR FITTINGS, LUGS HOLES AT RH PYLON WERE REPAIRED PER B757-200 SRM 54-51-90-2R REPAIR 3 AND LEAK CHECK WAS PERFORMED PER AMDS AND TEST OKSDR DALA2023060604613Unknown · unknownSHIP 660 MIGRATED BUSHING AT FWD UPPER SPAR OF UPPER LINK ON LH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00634. FWD UPPER SPAR FITTINGS, LUGS HOLES AT LH PYLON WERE REPAIRED WITH INNER DIAMETER WITH FINAL DIAMETER 1.9260" PER B757-200 SRM. (2797287)SDR JGVR20230531003Unknown · unknownMECHANICALLY BLENDED 1 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR WS 21 TO 23 AND MECHANICALLY BLENDED 1 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPAR WS 30 TO 33. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED FINDINGS AND SUBMITSDR SWAA2023061354591Barrier · crackedFOUND BRACKET AT R/H VAPOR BARRIER STA 663 RBL 25 LOWER AREA CRACKED.<[01] REMOVED AND REPLACED BRACKET (STIFFENER)AT R/H VAPOR BARRIER STA 663 RBL 25 LOWER AREA PER REF SRM 51-40-02-0G-0 AND DWG 111A1000;[02] VERIFIED REPLACEMENT OF BRACKET (STIFFENER) AT R/HSDR SWAA2023061453687Web · crackedLEFT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT LBL 35 BETWEEN W/L 150 AND 170<[01] VAPOR BARRIER BEEN FABRICATED ON N/R TTG8Q00LAZ39 STEP 16;[02] JOB COMPLETE; AUDIT C/WSDR FDEA202305241069Shim · damaged#3 PYLON AFT BULKHEAD TO UPPER SPAR CHORD ANGLE T/E SHIM HAS MIGRATED OUT OF POSITION. (MKD) WORK WITH N/R 641 LOOSE BOLTS NOTE: THESE LOOSE BOLTS MAY REQUIRE REMOVAL FOR NDT CHECK FOR CONDITION OF HOLES PRIOR TO REPLACEMENT. 0000098319 : NAVARRO, ENRIQUSDR DALA2023052604196Unknown · unknownSHIP 6710 A.D, A.A.: LOOSE FASTENERS NO. 2 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00172: FASTENER NO.2 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT SDR COEA2023070514919Bonding Plate · chafedWO 246760 NR 600033 HEAVY CHECK COE/MAJOR REPAIR: R/H WING FRONT SPAR UPPER STRIP SLAT BONDING PLATE HAS CHAFE DAMAGE BETWEEN RIBS 4R & 5R.CORRECTIVE ACTION: REPAIRED PER SRAS S571R0076...1614 ISSUE E, DATED 6/16/2023.SDR SWAA2023070563462Bracket · crackedL/W L/E UNDER PANEL #521NB NUT PLATE SUPPORT BRACKET CRACKED.<[01] REMOVED DAMAGE NUT PLATE CHANEL INSTALLED NEW NUT PLATE CHANNEL ON L/W L/E UNDER PANEL # 521NB SUPPORT BRACKET PER SRM 51-40-02 0G-0;[02] VERIFIED STEP 1; NUT PLATE CHANNEL REPLACED.SDR SWAA2023062150669Angle · crackedCRACK ANGLE LOCATED BS663.75 AND RBL 6 AT CENTER SECTION REAR SPAR 2023-330413<[01] REPLACED ANGLE (STIFENER) LOCATED BS663.75 AND RBL 6 TO RBL 34 AT KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 111A1000 SHEET 132 REV. A .SEE INDIVIDUAL SISDR SWAA2023061351534Barrier · crackedL/H MLG WHEEL WELL VAPOR BARRIER HAS A CRACK AT STA 663.75 LBL 34 AND WL150.<[01] APPLIED REPAIRED AT VAPOR BARRIER PER B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7)MATERIAL USED RESIN EY3804 PO#1800550 FIBERGLASS PO#1738579;[02] VERIFIED STEP 1SDR SWAA2023061351998Barrier · crackedR/H MLG WHEEL WELL VAPOR BARRIER HAS A CRACK AT STA 663.75 RBL 34 AND WL150.<[01] APPLIED REPAIRED AT VAPOR BARRIER PER B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7) MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1SDR FDEA202305161075Skin · delaminatedRIGHTHAND WING; TRAILING EDGE XW=899 OB OF OB AILERON 4" MODERATE CORROSION @ WING EDGE. MARKED REPAIRED TRAILING EDGE XW=899 FOUND APPROX 4" BY 2" AREA OF DELAMINATION AS REQ REF 51-43-01-0G PG 6 PAR 10SDR SWAA2023061649216Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 REP. 5;[02] INSTALLED EWIS PROTECTION ON REPAIR AREA BS 663 RBL 6-35 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA OF UPPER ATTACH ANGLE AT BSSDR SWAA2023061649217Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] VERIFIED SRM APPILCABILITY OF SRM 57-10-10-2R-5 REP. 5;[02] INSTALLED EWIS PROTECTION ON REPAIR AREA BS 663 LBL6-35 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA OF UPPER ATTACH ANGLE ATSDR SWAA2023061449379Stiffener · crackedCRACK INDICATION OBTAINED FROM FASTENER HOLE ON VAPOR BARRIER STIFFENER AT LBL 51<[01] REAMED FASTENER HOLE ON VAPOR BARRIER STIFFENER AT LBL 51 TO 2ND OVERSIZE AS PER B737-700 SRM 51-40-02-0G-0 STEP 4 D.;[02] VOID STEP #1;[03] ACCOMPLISHED EA: 23-157-01649/88SDR SWAA2023061449378Angle · crackedCRACK INDICATIONS OBTAINED FROM OPEN FASTENER HOLES AT LH VAPOR BARRIER UPPER ATTACH ANGLE VERTICAL FLANGE AT LBL 7;23;24;29 30;31 & 41. ALSO; CRACK FOUND AT LBL 41. CRACK LENGTH : 0.718' CRACK INDICATIONS OBTAINED FROM OPEN FASTENER HOLES AT LH VAPOR BARRIER SDR AALA202305175735Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305179165Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305176148Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305174844Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305171331Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305177516Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305179724Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305170765Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202305174279Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
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