JASC 5720

Service difficulty reports · 13,629

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.

SDR SWAA2025121647512Angle · elongatedELONGATED HOLE ON TEE ANGLE TRAILING EDGE LOCATED AT ORSS250 APPROX, RT WING. REPLACED THE TEE ANGLE LOCATED TRAILING EDGE IAW SRM 51-10-02, ITEM 9, AND SRM 51-20-01.Nov 26, 2025 · N452WN · Boeing 7377H4SDR CALA2025120111611Angle · crackedLEFT WING WEB ALONG DEFLECTION CONTROL RIB POSSIBLE CRACK. REMOVED AND REPLACED AT LEFT WING ANGLE WEB ALONG DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-20-01-0G-0, AMM 51-21--41-370-802, AND IPC 57-50-00-36A.Nov 26, 2025 · N38479 · Boeing 737924ERSDR SWAA2025121739670Support Beam · crackedCRACK ON SUPPORT BEAM LOCATED TRAILING EDGE ORSS 280 ON THE RT WING. REPLACED THE SUPPORT BEAM IAW SRM 51-40-02-0G-0, AND DWG 115A3712, SHEET 6, REV B.Nov 25, 2025 · N452WN · Boeing 7377H4SDR SWAA2025121739895Support Angle · elongatedELONGATED HOLE TRAILING EDGE SUPPORT ANGLE LOC AT LEVEL ORSS 250 ON THE LT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND SRM 51-20-01.Nov 25, 2025 · N452WN · Boeing 7377H4SDR SWIA2025112476510Beam · damagedRIGHT INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE) HAS WEAR DAMAGE AT FLAP STATION 24.0. REPAIRED RIGHT WING INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE) AT FLAP STATION 24.0 IAW REO 670-57-52-257 REV -B. COMPILED WITH ALL STEPS OF REO 670-57-52-257 REV -B. Nov 24, 2025 · N813SK · Cndair CL6002D24SDR SWAA2025121639499Support Angle · crackedCRACKED DEFLECTION CONTROL RIB, TRAILING EDGE SUPPORT ANGLE LOCATED AT ORSS 270, LT WING. REPLACED THE DEFLECTION CONTROL RIB TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 270 LT WING IAW SRM 51-40-02-0G, AND SRM 51-10-02-0G, ITEM 9. CRACK MEASUREMENT: L=0.550 INNov 24, 2025 · N452WN · Boeing 7377H4SDR CALA2025112511461Angle · crackedCRACK - ANGLE SUPPORT, BOOST PUMP COVER, INBD FIXED L.E. (P/N 1 CORRECT DISCREPANCY CRACK ANGLE SUPPORT , BOOST PUMP COVER INBR FIXED L.E.(P/N116A3939-2)AT IFSS 120.00 REF AAR N/R 99974380 REMOVED AND REPLACED UPPER SUPPORT ANGLE P/N116A3939-2 AT RH WING I/BNov 24, 2025 · N37277 · Boeing 737824SDR SWAA2025122939106Support Bracket · crackedCRACK INBD TRAILING EDGE SUPPORT BRACKET IRSS 212, RT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, ITEM 9, AND DWG 115A2001, SHEET 50, REV -.Nov 23, 2025 · N8624J · Boeing 7378H4SDR SWAA2025122939104Web · crackedCRACK WEB TRAILING EDGE FIXED PANEL ORSS 271 ON RT WING. REMOVED AND REPLACED THE WEB T/E FIXED PANEL IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DWG 115A2512, SHEET 16, REV -.Nov 23, 2025 · N8624J · Boeing 7378H4SDR VNAA202511210029Bracket · wornSLAT PANEL NR 3, WEAR ON BRACKET ASSY OF SLAT TRACK NR 1 AT RT WING. SLAT PANEL NR 3, WEAR ON BRACKET ASSY OF SLAT TRACK NR 1 AT RT WING WAS REPAIRED PER REO 690-27-81-013 REV -.Nov 21, 2025 · N647NN · Cndair CL6002D24SDR VNAA202511210008Support Bracket · corrodedCORROSION ON HYDRAULIC LINES SUPPORTS BRACKETS BTW WS 29.00 AND WS 68.00 ON REAR SPAR AT LEFT MLG WHEEL WELL. WAS EVALUATED,DUE EXCESSIVE CORROSION ON HYDRAULIC LINES SUPPORTS BRACKETS BTW WS 29.00 AND WS 68.00 ON REAR SPAR AT LEFT MLG IAW SRM 53-00-00-101-00Nov 21, 2025 · N647NN · Cndair CL6002D24SDR VNAA202511210007Channel · corrodedCORROSION ON ACCESS PANEL SUPPORTS BTW WS 68.00 AND LBL 45, ON REAR SPAR AT LT WING, ALSO NUT CHANNEL BTW FS 797.00 AND FS 830.40, ON LBL 45 AT LEFT MLG WHEEL WELL. CORROSION ON ACCESS PANEL SUPPORTS BTW WS 68.00 AND LBL 45, ON REAR SPAR AT LEFT WING WAS REMNov 21, 2025 · N647NN · Cndair CL6002D24SDR UIEA2025111801307Strap · corrodedCORROSION ON STRAP NEAR UPPER FACE OF LT WING L/E UPPER FIXED PANEL, OLES 1487. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 62. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV 62 & DWG 65B10636, SHEET 3, REV A, DWG 112U3003, SHEET 1, REV A, DWG 65B10637, Nov 20, 2025 · N249BA · Boeing 747409SDR CALA2025112011363Angle · crackedRIGHT WING TRAILING EDGE, 1 EACH ANGLE CRACKED APPROX. AT WS 270 (APPROX. 8 INCHES I/B OF THE FITTING) REMOVED AND REPLACED ANGLE FITTING PART NO. AAR PO: 1124531.1 IAW BAC DWG 1152930 REV:-, IPC 57-50-00-25. B737-800 SRM 51-40-02-0G-0 AND 51-40-04-0G-0 AT R/Nov 18, 2025 · N14237 · Boeing 737824SDR IXXA20251119001Support Channel · corrodedLEFT WING LOWER PANEL CHANNEL SUPPORT CORRODED AROUND MULTIPLE NUTPLATES AT WBL 97.5 STA 955 TO STA 999 (REFERENCE STREAMER TAG (22582) (SWISHER)Nov 15, 2025 · N431AZ · Boeing 767381SDR VNAA202601170009Angle · corrodedCORROSION ON SETTLEMENT ANGLE OF ACCESS PANEL642AZ AT RH WING. SETTLEMENT ANGLE OF ACCESS PANEL 642AZ AT RH WING WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER SRM 51-42-21-001-001-A01Nov 13, 2025 · N645NN · Cndair CL6002D24SDR SWAA2025121534443Angle · crackedCRACKED ANGLE, TRAILING EDGE ACCESS PANEL 551FB ON LT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, AND DWG 115A2710, SHEET 9, REV A.Nov 12, 2025 · N917WN · Boeing 7377H4SDR SWAA2025120834506Bracket · crackedRIGHT WING T/E PANEL 651FB FWD EDGE 3RD BRACKET FROM OTBD END CRACKED. REMOVED BROKEN BRACKET & PREP TO INSTALL A NEW BRACKET PER SRM 51-40-02-0G -0. REMOVED AND REPLACED THE RT T/E PANEL 651FB FWD EDGE 3RD BRACKET FROM OTBD END IAW SRM 51-40-02-0G-0. STEPNov 12, 2025 · N7888A · Boeing 737752SDR SWAA2025120234457Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02, AND DWG 115A2713, SHEET 3, REV A. MEASUREMENT OF CRACK IS 0.867.Nov 12, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234459Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A2930, SHEET 7, REV -.Nov 12, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234036Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS232 AT RT WING. REPLACED CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV - . CRACK LENGTH: 1.007.Nov 11, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234037Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT RT WING. REPLACED SUPPORT BRACKET IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02, AND DWG 115A2930, SHEET 7, REV -. MEASUREMENT OF CRACK: 0.772.Nov 11, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234038Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. REPLACED CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2714, SHEET 13, REV A. CRACK LENGTH: 0.930.Nov 11, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234039Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV - . CRACK LENGTH IS: 0.890.Nov 11, 2025 · N462WN · Boeing 7377H4SDR SWAA2025120234040Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 EXTERNAL AREA AT RT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 EXTERNAL AREA AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.Nov 11, 2025 · N462WN · Boeing 7377H4SDR VNAA202601170014Angle · corrodedCORROSION ON RH/LH MLG BIN SUPPORTS (6EA) BTW STA FS 693 TO STA FS847 AND CORROSION ON GUSSET (4EA) BTW STA FS 693 TO STA FS847,AND CORROSION ON FAIRING SUPPORT (4EAS) BTW STA FS 732 TO STA FS 752. CORROSION ON RH/LH MLG BIN SUPPORTS (3EA) BTW STA FS 693 TO SNov 10, 2025 · N645NN · Cndair CL6002D24SDR VNAA202601170013Angle · corrodedCORROSION ON FAIRING SUPPORTS (SETTLEMENTS AREA, LOWER/UPPER) BTW STA FS847.00 TO STA FS881 BTW STR 18RH TO STR 18LH AND CORROSION ON FAIRING SUPPORT MEMBRANES BTW STA FS 847.00 TO STA FS881 AND BTW STR 25RH TO STR25LH . DUE TO EXCESSIVE DAMAGE ON ANGLE SUPPONov 10, 2025 · N645NN · Cndair CL6002D24SDR SWAA2025121033223Bracket · crackedCRACK ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING. REPLACED BRACKET ON ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING IAW SRM 51-40-02 AND SRM 51-10-02. MEASUREMENT OF CRACK: L=0.895".Nov 9, 2025 · N914WN · Boeing 7377H4SDR SWAA2025121033220Bracket · crackedCRACK ACCESS PANEL 551FB TRAILING EDGE BRACKET LT WING. REPLACED BRACKET ON ACCESS PANEL 551FB TRAILING EDGE LT WING IAW SRM 51-40-02, SRM 51-20-01, AND DWG 115A2710, SHEET 9, REV A.Nov 9, 2025 · N914WN · Boeing 7377H4SDR SWAA2025121033222Support Angle · crackedCRACK ACCESS PANEL 551GB TRAILING EDGE SUPPORT ANGLE LT WING. REPLACED SUPPORT ANGLE ON ACCESS PANEL 551GB TRAILING EDGE IAW SRM 51-40-02; SRM 51-10-02, AND DWG 115A2714 SHEET:10 REV-.Nov 9, 2025 · N914WN · Boeing 7377H4SDR VNAA202601170007Diaphragm · corrodedCORROSION ON DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL. DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL WERE EVALUATE FOUND TO EXCESSIVE DAMAGE PER CRJ900 SRM 51-10-06-001-001-A01 AND REPLACED PER CNov 8, 2025 · N645NN · Cndair CL6002D24SDR SWAA2025121033219Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED TRAILING EDGE IRSS139 RT WING. MEASURE OF CRACK SUPPORT BRACKET IS L:1.664 INCHES, AND NOT FOUND ALLOWABLE DAMAGE, SRM 57-51-02-1A-1. SUPPORT BRACKET MUST BE REPLACED. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 139 RT WNov 8, 2025 · N914WN · Boeing 7377H4SDR SWAA2025121532845Support Beam · crackedCRACKED SUPPORT BEAM, TRAILING EDGE ORSS 280 ON LT WING. REPLACED THE SUPPORT BEAM IAW SRM 51-10-02-0G-0, 51-40-02, & DWG 115A3712, SHEET 5, REV -.Nov 7, 2025 · N917WN · Boeing 7377H4SDR SWAA2025111830618Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 276 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS 276 AT RT WING IAW SRM 51-40-02. MEASURE CRACK IS:0.996.Oct 31, 2025 · N455WN · Boeing 7377H4SDR SWAA2025111830620Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 271 LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED ORSS 271 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7, REV -.Oct 31, 2025 · N455WN · Boeing 7377H4SDR SWAA2025120429810Strap · corrodedCORROSION OTBD FRONT SPAR LOWER STRAP OF SS 345, RT WING. REPAIRED OUTBOARD FRONT SPAR LOWER STRAP OFSS 345 AT RT WING IAW EA 25-157-03068-WIP1; EA EA 25-157-03068-WIP2 AND EA 25-157-03068.Oct 29, 2025 · N231WN · Boeing 7377H4SDR CALA2025120311707Web · crackedLT WING REAR SPAR UNDERNEATH FIXED PNL BTW SPOILER 5 & 6 FWD SIDE OF AFT PLATE SHOWS A POSSIBLE CRACK. REMOVED AND REPLACED WEB ASSY AT LT WING REAR SPAR UNDERNEATH FIXED PNL BTW SPOILER 5 & 6 FWD SIDE OF AFT IAW B737-800 SRM 51-40-02-0G-0 AND AIPC 57-50-00-Oct 27, 2025 · N76288 · Boeing 737824SDR SWAA2025112828448Bracket · crackedCRACK ON BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING. REPLACED THE BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING IAW SRM 51-10-02-0G; SRM 51-40-02-0G-0 AND DWG 115A6200 SHEET 17 REV A TOOK MEASURE OF CRACK IS: 1.754 INCHES.Oct 25, 2025 · N8623F · Boeing 7378H4SDR JJBA20251120103Angle · crackedRH OVERWING PANEL #194ER, #2 LOWER ANGLE CRACKED AT YA-1085 (RIB 1A). RH OVERWING PANEL #194ER, #2 LOWER ANGLE REMOVED AND REPLACED.Oct 24, 2025 · N14158 · Emb EMB145XRSDR IPXA2025110339883Intercostal · brokenRIGHT WING TRAILIN EDGE STA 1196 RIB17 INTERCOSTAL IS BROKEN . INSTALLED INTERCOSTALL AND FITTING AT R/H WING T/E STA 1196 RIB 17. IAW SRM 51-40-21-001.Oct 24, 2025 · N126UP · Airbus A300F4622RSDR IPXA2025112822937Drag Fitting · damagedLEFT WING UPPER SKIN HOLES, UPPON VISUAL INSPECTION, IT WAS FOUND NR 1 HOLE CSK WITH CHATTERING, NR 8 HOLE CSK WITH CORROSION, NR 3 & 5 HOLES HAVE VISUAL DEFECTS NOTED AND VERIFIED HOLES BY MEASURES. ACCOMPLISHED REPAIR PER EO-95917-REQ1 AND VT-SAA EA 757-570Oct 23, 2025 · N409UP · Boeing 75724APFSDR JJBA20251107008Angle · crackedR/H OVERWING PANEL #194ER, #3 LOWER ANGLE CRACKED AT YA-1085 (RIB 1A). RT OVERWING PANEL 104ER, #3 LOWER ANGLE REMOVED AND REPLACED.Oct 21, 2025 · N14158 · Emb EMB145XRSDR 2025F00246Fitting · corrodedWHILE PERFORMING TASK 57-10-00-222 FOUND THAT LH EMERGENCY BRAKE CARRY THROUGH CORRODED AROUND FITTING. DISCONNECTED EXISTING LT MLG EMERGENCY BRAKE PNEUMATIC LINE AND REMOVED EXISTING CARRY-THROUGH FITTING ON RIB LOCATED AT W.S. 37.00 FOR ACCESS. BLENDED 1 EAOct 21, 2025 · N506QS · Cessna 680ASDR SWAA2025111025803Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 AT RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV -.Oct 20, 2025 · N451WN · Boeing 7377H4SDR SWAA2025111025799Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 281 AT RT WING. REPLACED ANGLE TRAILING EDGE ORSS 281 AT RT WING IAW SRM 51-40-02 ; SRM 51-10-02 PARAGRAPH 9 AND DWG 115A6200 SHEET:10 REV -.Oct 20, 2025 · N451WN · Boeing 7377H4SDR SWAA2025110725806Support Angle · corrodedCORROSION ON SUPPORT ANGLE OF UPPER BONDING JUMPER, AFT BOOST PUMP, TANK 2, RT WING T/E. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9.Oct 20, 2025 · N451WN · Boeing 7377H4SDR SWAA2025110725802Support Bracket · crackedCRACK SUPPORT BRACKET T/E ORSS 271, RT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. CRACK LENGTH 0.235 INCH.Oct 20, 2025 · N451WN · Boeing 7377H4SDR IPXA2025111246321Support Beam · inoperativeLEFT WING OTBD FLAP INBD HINGE STRUCTURE FAIRING 535 DL AREA UPPER SUPPORT BEAM HAS EVIDENCE OF CORROSION, ACCOMPLISHED REPAIR IAW VT-SAA EA 011-5700-01-B0623, REV IR.Oct 19, 2025 · N294UP · Doug MD11FSDR SWAA2025111025490Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 271 LT WING. REPLACED ANGLE AND FASTENERS ON TRAILING EDGE LOCATED ORSS 271 LT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV - .Oct 18, 2025 · N451WN · Boeing 7377H4SDR SWAA2025111925352Angle · crackedCRACK ANGLE ON ACCESS PANEL 551FB TRAILING EDGE AT LT WING. MEASUREMENT OF CRACK IS L: 0.300 INCHES. REPLACED THE ANGLE ON ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW SRM 51-40-02-0G SRM 51-10-02-0G ITEM 9 AND DWG: 115A2710, SHEET 9, REV A.Oct 17, 2025 · N910WN · Boeing 7377H4
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