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.
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 SWAA2025111925353Angle · crackedCRACK ANGLE ON ACCESS PANEL 651GB TRAILING EDGE AT RT WING. MEASUREMENT OF CRACK IS L:0.300 INCHES. REPLACED ANGLE ON ACCESS PANEL 651GB TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G ITEM 9, AND DWG 115A2714 SHEET 10 REV -.SDR SWAA2025111925354Support Bracket · crackedCRACK SUPPORT BRACKET ON ACCESS PANEL 651FB AT RT WING. MEASUREMENT OF CRACK IS L: 0.500 INCHES. REPLACED SUPPORT BRACKET ON ACCESS PANEL 651FB AT RT WING IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A2710 SHEET:9 REV:A.SDR CALA2025102110330Bracket · crackedLH WING LOWER SKIN, BETWEEN RIB 7-8 AND S 8-9 HYDRAULIC LINES BRACKET BROKEN. REPLACED CRACKED BRACKET AT LEFT WING LOWER SKIN BETWEEN RIB 7&8 REFERENCE SRM 51-40-02-0G-0, DWG 272A9125-1.SDR CALA2025102110329Bracket · brokenRH WING LOWER SKIN, BETWEEN RIB 7-8 AND S 8-9 HYDRAULIC LINES BRACKET BROKEN. REPLACED CRACKED HYDRAULIC LINES BRACKET P/N 2729125-13 ON THE RIGHT-WING LOWER SKIN BETWEEN RIB 7&8 REFERENCE DWG 2729125-1, SRM 51-40-02-0G-0. ESFR NO. 2175; (WORK ACCOMPLISHED BYSDR SWAA2025111931677Support Bracket · corrodedCORROSION REAR SPAR FUEL BOOST PUMP UPPER BONDING JUMPER SUPPORT BRACKET AT LT WING. R & R THE UPPER BONDING JUMPER AND UPPER BONDING CLIP OF THE AFT FUEL BOOST PUMP TANK 1 IAW AMM 28-22-41-000-801 STEP 2.H.(8), AND AMM 28-22-41-400-801 STEP 3.H.(22) TO 3.H.SDR IPXA2025120161060Angle · crackedRIGHT WING. FIXED L/E RIB LOCATED APPROX STA XOS 1113.252 HAS CRACK. REMOVED EWIS PROTECTION AND INSTALLED RIB SUPPORT AT R/H WING. FIXED L/E LOCATED APPROX STA XOS 1113.252 IAW MD11 SRM 51-00-12 & MD-11 SRM 51-33-01. QC AUDIT C/WSDR IPXA2025103054985Support · crackedLH WING FIXED LEADING EDGE SUPPORT CRACKED AT LWR CORNER INSIDE ACCESS PANEL 524GB, INSTALLED PLATE P\N: R5724018520000 BATCH: 0004437520, LH WING FIXED LEADING EDGE SUPPORT IAW A300-600 SRM 57-41-11 PAGE 211 FIGURE 202 (SHEET 2) AND SRM 51-40-21.SDR IPXA2025110362365Web · gougedLEFT WING T/E REAR SPAR UNDER #5 SPOILER O/B SUPPORT WEB GOUGED, REMOVED CRACKED SUPPORT WEB IAW A300-600 SRM 51-40-21. INSTALLED NEW SUPPORT WEB IAW A300-600 SRM 51-40-21.SDR CALA2025101710221Bracket · crackedINSIDE LEFT WING PANEL 551DB, INBD AFT AREA, FOUND ONE BRACKET BENT AND PULLED THROUGH RIVET CAUSING DAMAGE. REMOVED AND INSTALLED FABRICATED BRACKET UNDER LT WING PANEL 551DB, AT INBD AFT AREA IAW SRM 51-40-02-0G-0, DWG 287A9152 REV AA, SRM 51-20-01-0G-0, ASDR CALA2025101410072Channel · delaminatedL/H AILERON HAS COMPOSITE DAMAGE ON TOP T/E. REPAIRED DAMAGED COMPOSITE IAW A319 SRM 51-77-12-911-002 RMVD AND RPLD AILERON TRAILING EDGE CHANNEL IAW A319 SRM 51-42-11 CMM 57-61-21 SRM 51-72-11 CAT A.SDR SWAA2025102723921Bracket · cracked90 DEGREE WIRING HARNESS STAND OFF ON L/E OF PANEL 651FB IS CRACKED. R&R BRACKET REF SRM 51-40-02. INSPECTED WORK ACCOMPLISHED R&R BRACKET REF SRM 51-40-02.SDR CALA2025102310429Fairing · crackedNUMBER 1 PYLON AFTER FAIRING CRACKED IN AFT AREA. REMOVED AND REPLACED NR 1 PYLON AFTER FAIRING ASSY END, LOCATED DRILLED AND COUNTERSUNK, APPLIED ALODINE, PRIMER, TOPCOAT PAINT IAW SRM 51-40-05-0G-0, SRM 51-40-05-0G-0, 51-40-02-0 G-0, SRM 51-40-08-0G-0, SRMSDR SWAA2025111223761Angle · crackedCRACK ACCESS PANEL 551FB TRAILING EDGE ANGLE AT LT WING. REPLACED ANGLE ON ACCESS PANEL 551FB TRAILING EDGE ANGLE AT LT WING AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2710 SHEET 9 REV A<BR>MEASURE OF CRACK IS L=0.611.SDR SWAA2025102723743Stand Off · crackedLEFT WING PANEL 551FB 90 DEGREE WIRING STAND OFF BRACKET IS CRACKED.<[01] R&R BRACKET REF SRM 51-40-02.;[02] INSPECTED WORK ACCOMPLISHED R&R BRACKET REF SRM 51-40-02.SDR SWAA2025111223438Angle · crackedCRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 1 LH WING . REPLACED ANGLE LOCATED AUXILIARY TRACK SLAT 1 LH WING IAW B737-700 SRM 51-40-02 AND DWG# 114A5010 SHEET: 14 REV: C.SDR SWAA2025111223532Angle · crackedCRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 7 RH WING. REPLACED ANGLE LOCATED AUXILIARY TRACK SLAT 7 RH WING IAW B737-700 SRM 51-40-02 AND DWG# 114A5020 SHEET: 40 REV: A .SDR JR2R20251009222Fitting · crackedRH WING TRAILING EDGE AFT SIDE OF WING SPAR2 AILERON QUADRANT LOWER BRACKET IS CRACKED IN THE RH MLG WHEEL WELL. REPLACED BRACKETSDR CALA2025101009902Attach Angle · crackedRIGHT WING FIXED L/E RIB 15 HAS CRACKED SMALL ANGLE AT INNER BOT TOM CORNER. REMOVED AND REPLACED RH WING FIXED L/E RIB 15 ATTACHED ANGLE IAW A319 SRM 51-42-11-001.SDR SWAA2025102822298Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30; REV A.SDR SWAA2025102822294Support Bracket · crackedCRACKED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-O2, & SRM 51-10-02, ITEM 9. MEASUREMENT OF CRACK IS 0.200".SDR SWAA2025102822276Plate · crackedLEFT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 551DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE IAW SRM 51-40-02-0G-0. INSTALLED NEW WAFFLE PLATE IAW SRM 51-40-02-0G-0, PART 115A2781-3.SDR SWAA2025102822277Plate · crackedRIGHT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 651DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE AT RT WING OTBD OF 651BB IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED ALL FASTENER HOLES INTO NEW RT WAFFLE PLATE IAW SRM51-40-02-0G-SDR SWAA2025102222524Plate · crackedRIGHT WING T/E WIGGLE PLATE JUST I/B OF THE #8 FLAP TRACK CRACKED. UPON FURTHER INVESTIGATION; SUSPECTED CRACK ON RIGHT WING T/E WIGGLE PLATE OF # 8 FLAP TRACK WAS LIMITED TO SURFACE FINISH (PRIMER) ONLY. REPRIMED AREA IAW AMM 51-21-99-300-801.SDR SWAA2025102222525Plate · crackedLEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IAW SRM 51-40-02 AIPC 57-50-00-22A.SDR SWAA2025102721832Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV. -.SDR SWAA2025102721833Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A.SDR SWAA2025102721831Support Angle · crackedCRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 24, REV A. MEASUREMENT OF CRACK IS L= 0.813".SDR SWAA2025102821533Bracket · corrodedCORROSION ON BRACKET FUEL BOOST PUMP REA LOCATED IRSS147 AT RT WING (2 E/A). REPLACED BRACKET FUEL BOOST PUMP AREA LOCATED IRSS147 AT RT WING IAW AMM 28-22-41-000-801 AND AMM 28-22-41-400-801.SDR SWIA20251222002Drain Valve · corrodedLH WING WATER DRAIN VALVE COVER FOOTPRINT ADJACENT TO STANDBY BOOST PUMP HAS CORROSION ON WING PLANK. (C-CHECK RO 12/19/2025)PERFORMED REPAIR FOR CORROSION DAMAGE TO LHS LOWER WING PLANK AROUND ELECTRIC BOOST PUMP WATER DRAIN CUTOUT AT BL5.00 BTWN STR 5 - STRSDR SWAA2025102720580Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A6200, SHEET 10, REV-. MEASURESDR SWAA2025102720581Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 RESDR SWAA2025102720642Support Angle · crackedRIGHT WING INBD FIXED T/E PANEL OTBD OF NR 7 SPOILER, AFT SUPPORT ANGLE CRACKED. REMOVED AND REPLACED AFT SUPPORT ANGLE IAW SRM 51-40-02 AND AIPC 57-50-00-25.SDR SWAA2025102720644Plate · crackedRIGHT WING T/E WIGGLE PLATE JUST INBD OF NR 7 AFT CANOE FAIRING CRACKED, ORSS 318. REMOVED AND REPLACED RT WING T/E WIGGLE PLATE INBD OF NR 7 AFT CANOE FAIRING IAW SRM 51-40-02-0G-O.SDR SWAA2025102720645Plate · crackedRIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651GB ON THE INBD SIDE IS CRACKED. REMOVED AND REPLACED RT WING T/E WIGGLE PLATE COMMON TO PANEL 651GB ON THE INBD SIDE IAW SRM 51-40-02-0G-0.SDR SWAA2025102720646Plate · crackedRIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INBD SIDE IS CRACKED. REMOVED AND REPLACED RIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INBD SIDE IAW SRM 51-40-02-0G-0.SDR SWAA2025102720648Support Angle · crackedLEFT WING INBD FIXED T/E PANEL JUST OTBD OF NR 6 SPOILER AFT SUPPORT ANGLE CRACKED. REMOVED AND REPLACED LEFT WING I/B FIXED T/E PANEL AFT SUPPORT ANGLE JUST O/B OF NR 6 SPOILER IAW SRM 51-40-02; AIPC 57-50-00-25 AND AMM 20-50-11-910-801.SDR SWAA2025103020341Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 115A3712 SHEET 7REV A AND DWG 115A3700 SHEET 41 REV - .SDR SWAA2025103019747Nut Plate · crackedCRACK ON RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SDR SWAA2025110318984Angle · crackedCRACKED ANGLE AUXILIARY TRACK SLAT 6, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, AND SRM 51-40-02. DUE TO EVALUATED CRACK ON ANGLE AND NOT FOUND ALLOWABLE DAMAGE IAW SRM-57-42-02-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS L= 2.057.SDR SWAA2025103019097Nut Plate · crackedCRACK ON RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG: 112A4402 SHEET: 14 REV: -.SDR SWAA2025103019094Nut Plate · crackedCRACK ON RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 13, AND SHEET 14 REV-. MEASURE OSDR REXA2026052800822Support Angle · crackedCRACKED SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ. SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01SDR SWAA2025103018639Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 355 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 355 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND 51-10-02 ITEM 9.SDR SWAA2025102218311Angle · crackedLEFT WING VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB IS CRACKED. REMOVED VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT. INSTALLED A NEW ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB PER SRM 51-40-02.. REFINISHSDR SWAA2025092918411Support Angle · crackedRIGHT WING OTBD SUPPORT ANGLE, IMMEDIATELY INBD OF THE DEFLECTION CONTROL RIB FOUND CRACKED ON UPPER OTBD FLANGE. R & R THE RT WING OTBD SUPPORT ANGLE IAW SRM 51-40-02.SDR CALA2025092909381Support Angle · crackedRIGHT WING FIXED LEADING EDGE FOUND SUPPORT ANGLE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING FIXED LEADING EDGE IAW SRM 51-40-02-0G-0 AND DWG 116A4008.SDR SWAA2025102218303Bracket · crackedRIGHT WING; DEFLECTION CONTROL RIB; INBOARD FIXED TRAILING EDGE UPPER PANEL BRACKET CRACKED. (M)<[01] REMOVED CRACKED WEB ANGLE BRACKET PER SRM 51-40-02.;[02] LOCATED; DRILLED AND DEBURRED REPLACEMENT WEB ANGLE BRACKET PER SRM 51-40-05.;[03] INSPECTED WORK IN SDR REXA2026052600623Plate · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING). WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERESDR DALA2025092306961Strap · damagedCOMPLY WITH ER/A 626909-14AD SECTION IV LT WING REAR SPAR LOWER STRAP REPAIR. COMPLIED WITH ER/A 626909-14AD REV. E SECTION IV AND PRI 626909- 14AD REV. E REV 0 - 4. LH WING REAR SPAR LOWER STRAP REPAIR. (1212786)SDR DALA2025092306960Doubler · damagedFUEL LEAK FOUND DURING INSPECTION OF THE L/H WING AFT LOWER SKIN DOUBLER IN THE BRACE FITTING AREA AT XRS = 164, REF: EM 5720- 01103-01A. COMPLIED WITH ER/A 628888-14AD REV. ORIG. PRI REV. (1209016)
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