JASC 5720
Service difficulty reports · 13,633
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 SWAA2024082611503Angle · crackedCRACK ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-421002<[01] REPLACED ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2710; SHEET 8; REV: A. MEASURE OF CRACK IS L:0.462?; TOOL USED SDR SWAA2024080910310Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS219 AT RT WING 2024-415054<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS219 AT RT WING I.A.W B737-800 SRM 51-10-02 AND DWG 115A2713 SHEET 6 REV ?A?;[02] CORRECTED STEP 1 REPLACED CORRUGATED PLATE TRASDR SWAA2024080910151Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS219 AT LT WING 2024-415048<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS219 AT RT WING I.A.W B737-800 SRM 51-10-02 AND DWG 115A2713 SHEET 6 REV ?A?;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATESDR SWAA2024080909008Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 290 AT RT WING 2024-414968<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 290 AT RT WING I.A.W B737-800 SRM 51-10-02;[02] CORRECTED STEP 1: REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 290 ATSDR IPXA2024072453579Doubler · crackedR/H WING. FIXED L/E COMPARTMENT HAS CRACKED BEADED DOUBLER LOCATED APPROX STA XOS 680. (015-11) ATA57.REMOVED 12 EA WIRE CLAMPS FOR ACCESS TO REMOVE BEADED DOUBLER SECTION R/H WING FIXED L/E COMPARTMENT APPROX STA 572 PER REF MD-11 SRM 51-31-01-0G-0.INSTALLED SDR SWAA2024081307803Support Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+5;21 INCH AFT OF REAR SPAR; SUPPORT BRACKET REAR FACE HAS CRACK.<[01] REMOVED AN REPLACED SUPPORT BRACKET AT R/WING TE ORRS 261+5;21 INCH AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081307807Attach Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+11;15 INCH AFT OF REAR SPAR; O/B ATTACH BRACKET HAS CRACK.<[01] REMOVED AND REPLACED BRACKET AT R/WING TE; ORRS 261 + 11.15 INCH AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081308032Support Bracket · crackedLH WING TE: DEFLECTION CONTROL RIB AT ORRS 261; 18 INCHES AFT OF REAR SPAR; SUPPORT BRACKET FRONT FACE HAS CRACK.<[01] TASK COMPLETE: <BR>REMOVED CRACKED BRACKET AND REPLACED WITH NEW (PN: 115A2953-1 LOT: 238381/039685) IAW SRM 51-40-02-0G-0 4.B.;[02] VERIFIEDSDR SWAA2024081308033Support Bracket · crackedLH WING TE: DEFLECTION CONTROL RIB AT ORRS 261+8; 17 INCHES AFT OF REAR SPAR; SUPPORT BRACKET AFT FACE HAS CRACK.<[01] TASK COMPLETE: <BR>REMOVED CRACKED BRACKET AND REPLACED WITH NEW (PN: 115A298291 LOT: 234768/033958) IAW SRM 51-40-02-0G-0 4.B.;[02] VERIFIEDSDR SWAA2024081307802Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+5; 19 INCHES AFT OF REAR SPAR; SUPPORT BRACKET FRONT FACE HAS CRACK.<[01] TASK COMPLETE:<BR>CRACKED SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETESDR SWAA2024081307806Support · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+11;18 INCH AFT OF REAR SPAR; REAR SUPPORT ATTACH POINT HAS CRACK.<[01] REMOVED AND REPLACED SUPPORT AT R/WING TE; ORRS 261 + 11.18 AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024080907747Web · crackedCRACK WEB TRAILING EDGE LOCATED ORSS275 DEFLECTION CONTROL RIB AREA AT LT WING 2024-414820<[01] REPLACED WEB TRAILING EDGE LOCATED ORSS275 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-800 SRM 51-40-02 DRAWING 115A2512 REV- SHEET 16.;[02] REPLACED WEB TRAILISDR SWAA2024071807345Support Beam · elongatedLH WING TRAILING EDGE FIXED UPPER PANEL O/B SUPPORT BEAM RETAINER HAS ATTACHMENT BOLT HOLES ELONGATED. (I/B OF #5 SPOILER)<[01] REMOVED BOLTS FOUND HOLES NOT ELONGATED BOLTS WERE LOOSE REINSTALLED AND TIGHTENED BOLTS PER SRM 57-51-02-2R-1 FIG.203 SHEET 3;[02] SDR SWAA2024072906727Bracket · corrodedRH WING LEADING EDGE FUEL GAUGE BRACKET HAS CORROSION MARKED<[01] REMOVED AND REPLACED WING REFUEL PANEL PER SOPM 20-50-01 AND MM 28-41-61.REFUELING PANELS OPS CHECKED GOOD PER MM 28-41-61;MM 28-21-81 AND MM 28-21-00;[02] C/W INSPECTIONSDR CALA2024070801971Support Angle · crackedR/H WING RIB 15 O/B WEB SUPPORT ANGLE CRACKED PER HAECO LCQ N/R 9298670/26670 GEN BY V926223 REMOVED AND REPLACED SUPPORT ANGLE ON R/H WING RIB 15 O/B WEB IAW SRM A319 51-72-11-911-001 BY MECH V934190 INSP BY V892442SDR FDEA202406280876Angle · damagedNEED TO CREATE ANGLE B67-57-003-01 TO REPLACE 114T2171-4 AT FLE LW OSS 441.569. FABRICATED AND REPLACED FORMER 114T2170-5 & ANGLE 114T2171-4 WITH B67-57-002-01 & B67- 57-003-01SDR SWAA2024080704328Plate · crackedCRACK RAIL NUT PLATE LOCATED OFSS579 INTERNAL CAVITY LEADING EDGE AT LT WING 2024-404905<[01] REPLACED RAIL NUT PLATE LOCATED OFSS579 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9.;[02] REPLACED RAIL NUT PLATE LOCASDR SWAA2024080704478Plate · crackedCRACK ON RAIL NUT PLATE LOCATED OFSS470 INTERNAL CAVITY LEADING EDGE AT RT WING 2024-404914<[01] REPLACED RAIL NUT PLATE AND FASTENERS LOCATED OFSS470 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9.;[02] CORRECTED SSDR SWAA2024071804426Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 265 AT LT WING 2024-393422<[01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 265 AT LT WING I.A.W. B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 ;SRM 51-40-02-0G-0 AND TOOK MEASURE OF CRACK IS L: 0.639 INCH TOOLSDR SWAA2024071804425Support Angle · crackedCRACK SUPPORT ANGLE LOWER SURFACE REAR SPAR AT IRSS 139 LEVEL LT WING 2024-393421<[01] REPLACED SUPPORT ANGLE LOWER SURFACE REAR SPAR AT IRSS 139 LEVEL LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9.;[02] CORRECTED ACTION 1 <BR>REPLACED SUPPORT ANGLE LOSDR SWAA2024080504186Angle · crackedCRACK ANGLE LOCATED TRAILING EDGE ORSS 291 AT RT WING 2024-401769<[01] CALIPER P/N: 500-196-30; S/N: A23329368; DUE DATE: 06/MAR/25.;[02] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE ORSS 291 AT RT WING IAW B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9;AND DSDR SWAA2024071803992Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 261 INTERNAL AREA AT RT WING 2024-393413<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 261 INTERNAL AREA AT RT WING I.A.W. B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 ;SRM 51-40-02-0G-0 AND TOOK MEASURE OF CRACK IS L: 0.1.030SDR J6BA2024081400618Pad · damagedR/H WING DAMAGED NEAR JACK PAD; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REPAIRED R/H WING OUTER SKIN NEAR JACK PAD IAW MHIRJ REO # 601R-57-51-1048 REV -- DATED 7/25/2024SDR SWAA2024072402944Web · crackedRIGHT WING; TRANSVERSE WEB IS CRACKED ON O/B UPPER LEG AT O/B RIVET<[01] REMOVED AND REPLACED RIGHT WING TRANSVERSE WEB ON O/B UPPER LEG IAW SRM 51-40-02 AND DWG# 115A6200 REV B.SDR SWAA2024072403069Plate · crackedRIGHT WING; T/E WAFFLE PLATE IS CRACKED AT I/B ATTACH RIVET 10-INCH I/B OF #6 FLAP TRACK<[01] REMOVED AND REPLACED RIGHT WING T/E WAFFLE LOCATED 10' I/B OF #6 FLAP TRACK IAW SRM 51-40-02 AND AIPC 57-50-00-22A.;[02] VERIFIED CORRECTION ACTION ITEM 1; MEASUREMENSDR VNAA20240723014Skin · gouged1211.83FH PERM REPAIR - TEMPORARY FOR LH SLAT NO.3 TE SKIN GOUGE WITHIN 1211.83 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH SLAT TE SKIN WAS REPAIRED PER REO 690-57SDR SWAA2024071802245Angle · crackedCRACK ANGLE ACCESS PANEL 343AT AT RT WING 2024-376742<[01] REPLACED ANGLE ON ACCESS PANEL 343AT AT RT WING IAW B737-700 #DWG: 186A3005 SHEET:1 REV:B SRM 51-40-02 AND SRM 51-10-01 ITEM 9.;[02] REPLACED ANGLE ON ACCESS PANEL 343AT AT RT WING IAW B737-700 #DWG: 1SDR SWAA2024071102047Angle · crackedCRACK TRAILING EDGE ANGLE LOCATED AT DEFLECTION CONTROL RIB AREA AND AT LEVEL ORSS 272 AT LT WING 2024-384347<[01] REPLACED ANGLE LOCATED AT DEFLECTION CONTROL RIB AREA AND AT LEVEL ORSS 272 AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A6200 REV A SHEESDR CALA2024071902066Strap · damagedL/H WING L/E PANEL 521FB ATTACH LOWER WING STRAP ASSEMBLY WAS REPAIRED DUE TO CORROSION. REF BAM N/R 001997213 FOR COMPLETION OF REPAIR. REF SRM 57-20-01-2R-3 REPAIR 3. A SIGNIFICANT FINDINGS REPORT IS REQUIRED TO BE ISSUED FOR THIS REPAIR.SDR UIEA2024052700452Support Bracket · corrodedLHW - L/E CAVITY AT WS 1260 SUPPORT BRACKET FOUND SURFACE CORROSION AS MARKED(<P>LHW - L/E CAVITY AT WS 1260 SUPPORT BRACKET REPLACED AS PER AMM 20-51-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052700453Support Bracket · corrodedRHW - L/E FRONT SPAR CAVITY LOWER FIXED FAIRING FWD VERT SUPPORT BRACKET FOUND CORROSION NEAR OLES 1564 (#26E L/E SLAT AREA)(<P>RHW - L/E FRONT SPAR CAVITY LOWER FIXED FAIRING FWD VERT SUPPORT BRACKET REPLACED AS PER AMM 20-51-01. NO FURTHER DEFECTS NOTED.</P>SDR UIEA2024060700502Support Bracket · brokenR/H WLG WING REAR SPAR - WS 380 STIFFENER ATTACHED SUPPORT BRACKET FOUND BROKEN(<P>SUPPORT BRACKET P/N: 65B12757-4 FABRICATED AS PER DRAWING AND RI NO.RI-57-00-16908 REV.A AND INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED. </P>)SDR SWAA2024070100302Web · crackedLEFT WING; TRANSVERSE WEB IS CRACKED ON UPPER LEG O/B END; ABOVE #1 PYLON AFT TIP. REMOVED AND REPLACED LEFT WING TRANSVERSE WEB; P/N 115A2156-7 IAW SRM 51-40-02-0G-0 AND DWG. 115A2512; REV. -.SDR 2024F00148Fairing · wornTHE FIBERGLAS FAIRING ON THE FRONT OF THE OB FLAP, IB HINGE ON THE RH WING CAME LOOSE AND CHAFED INTO THE BOTTOM WING SKIN JUST FORWARD OF THE FLAP HINGE. AIRBUS ENGINEERING WAS CONTACTED WITH THE DAMAGE SPECIFICATIONS AND THEY ISSUED REPAIR INSTRUCTIONS UNDESDR SWIA20240809605Skin · chafedLH WING LOWER SKIN WS128.00 AT THE NOSE OF FLAP FAIRING 586AB THE SKIN IS CHAFFED (C-CHECK RO 8/7/2024) PERFORMED BLENDED OUT AND EVALUATED DAMAGE ON LH WING LOWER SKIN WS128.00 AT THE NOSE OF FLAP FAIRING 586AB THE SKIN, MESUAREMENTS ARE: ORIGINAL THICSDR VNAA202407110022Bracket · crackedDURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. PER REO 670-57-42-577. REV.--SDR VNAA202407110021Bracket · crackedDURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577. REV.--SDR SWAA2024071198000Angle · crackedRIGHT WING; I/B UPPER T/E PANEL JUST AFT OF REAR SPAR; UPPER U SUPPORT CHANEL FWD ATTACH ANGLE IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] RIGHT WING; I/B; UPPER SDR SWAA2024070997678Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2024-361560<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9.<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[02] CORRECTED STSDR SWAA2024070997671Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2024-361555<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.;[02] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.WSDR SWAA2024070906492Support Beam · wornWEAR ON DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING 2024-361557. POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 16-SEP-25. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1SDR SWAA2024070997589Support Fitting · damagedL/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B AFT SUPPORT ROD UPPER SUPPORT FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR SPAR FIXED T/E LOWER PANEL 551GB SUPPORT ROD UPPER SUPPORT FITTING; REF SRM 51-40-02-0G-0;[02] VERIFIED REMOVED ANSDR SWAA2024071691377Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2024-345719<[01] REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G-2 ;SRM 51-10-02-0G-0 PARAGRAPH 9 CHECK CLARENCE BETWEEN SKIN FSDR SWAA2024061901021Angle · crackedRIGHT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] REMOVED AND REPLACED RIGHT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE PER REF SRM 51-40-02-0G-0;[02] FINAL INSPECTION; VERIFIED STEP SDR IPXA2024062685023Support Beam · corrodedLEFT WING T/E PANEL SUPPORT BEAM HAS CORROSION JUST FWD OF I/B AILERON. INSTALLED FALSE SUPPORT TEE CAP, GUSSET, 3 ANGLES AND 1 FILLER AT LT WING T/E PANEL SUPPORT BEAM IAW SRM 57-50-02-2R-9 REPAIR 9. ACCOMPLISHED SRM 57-50-02-2R-9, REPAIR 9 (REVISION 70).SDR SWAA2024071690377Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2024-345585<[01] REPLACED SUPPORT ANGLE (FITTING) LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING (1 E/A) IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 DWSDR SWAA2024071690458Angle · crackedCRACK ON ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT 2024-345592<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02.;[02] COMPLETED TASK CERTIFIEDSDR SWAA2024070290504Former · crackedLEFT WING FAIRING FORMER CRACKED; BS500D; BETWEEN STR 18/19 6-INCH O/B OF FUSELAGE SKIN; I/B UPPER CORNER OF FIXED L/E SKIN (MARKED)<[01] REMOVED CRACKED FAIRING FORMER (FRAME) PER SRM 51-40-02;[02] REMOVED AND REPLACED LEFT WING FAIRING FORMER P/N:116A318- ATSDR SWAA2024062890374Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 217 AT RT WING 2024-341179<[01] REPLACED CORRUGATED PLATE LOCATED INBOARD TRAILING EDGE IRSS 217 AT RT WING IAW SRM B737-700 51-10-02 ITEM 9. LENGTH OF CRACK IS 0.375? TOOL USED CALIPER P/N:500-193-30 S/N:00376SDR SWAA2024062890375Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 241 AT LT WING 2024-341180<[01] REPLACED INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 241 AT LT WING IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9.<BR>MEASURE CRACK IS: 0.375? TOOL USED CALIPER P/N:700-113-1
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