JASC 5720
Service difficulty reports · 13,631
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 SWAA2025070780044Support Angle · pulledFASTENER HEADS FOR I/B SUPPORT ANGLE PULLED THROUGH ON L/W PANEL 551GB. REPAIRED PER SRM 51-70-04-2R-9-A00753, REPAIR 9 - REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER.SDR FDEA202506091078Support · crackedLH WING TE CAVITY LOWER FACE OF UPPER FIXED PNL FOUND SUPPORT WEB CRACK NEAR L5 SPLR INBD. TRIMMED OUT AND INSTALLED REPAIR BRACKET REPAIR AT LH WING SKIN SUPPORT ABX144.2 I.A.W FEDEX EA NO : T6-5740-T0383807 P1, SEQ NO : 1013, TITLE : WING-ATTACH FITTINGSSDR SCNA20250626233Fitting · wornL/H WING FOUND WEAR MARKING I/B SIDES OF FACE ON O/B FITTING I/B FLAP .SDR SWAA2025071579387Support Angle · crackedCRACK INBOARD SUPPORT ANGLE OF OUTBOARD AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON OUTBOARD AUXILIARY TRACK SLAT 8 AT RT WING. IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG# 114A5010. SHEET 16. REV. A.SDR SWAA2025071579392Angle · crackedCRACK INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 7 AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON INBOARD AUXILIARY TRACK SLAT 7 AT RT WING. IAW SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG# 114A5020 SHEET 16. REV -.SDR SWAA2025071579394Support Angle · crackedCRACK INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW SRM 51-10-01-0G ITEM 9; SRM 51-40-02-0G-0 AND DWG 144A5010 SHEET: 16 REV: A. MEASURE CRACK IS 2.045 INCHSDR VNAA20250716003Canister · crackedDURING INSPECTION OF TASK CARD 57-20-202_R/H-JIC IT WAS DETECTED CRACK ON SLAT TRACK CANISTER BRACKET (TRACK 1-3) AT RH MAIN FUEL TANK. CRACK ON SLAT TRACK CANISTER BRACKET (TRACK 1-3) AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV. --SDR SWAA2025061777886Support Angle · crackedCRACK ACCESS PANEL 651FB TRAILING EDGE SUPPORT ANGLE RT WING. REPLACED SUPPORT ANGLE LOCATED ACCESS PANEL 651FB TRAILING EDGE RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-01-1A-1 MEASURE ARSDR SWAA2025061777512Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 216 AT LT WING. MEASURE CRACK IS: 0.4015 INCHES. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 216 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2001 SHEET: 30 REV A.SDR SWAA2025061776943Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 AT RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-01-1A-1 MEASURE ARE L: 0.700.SDR SWAA2025061776942Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 LT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-01-1A-1 MEASURE ARE L: 0.830.SDR SWAA2025061776939Support Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 RT WING. REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A6200 SHEET 10 REV-.SDR SWAA2025061776940Web · crackedCRACK WEB TRAILING EDGE FIXED ACCESS PANEL ORSS 271 AT RT WING. INSTALLED NEW WEB TRAILING EDGE FIXED ACCESS PANEL ORSS 271 AT RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 5 REV B.<BR>SEE INDIVIDUAL SIGN OFF BELOWSDR IXXA202505310007Support · corrodedLEFT WING FIXED TRAILING EDGE PANEL SUPPORT IS CORRODEDSDR SWAA2025060275765Vapor Barrier · crackedRIGHT WHEEL WELL FIBERGLASS VAPOR BARRIER HAS APPROXIMATELY 17' CRACK BETWEEN RBL 28 AND RBL 36 <[01]. C/W EA ON ATTACHED FAULT; [02] C/W EA 25-157-01402 ON ATTACHED FAULT.SDR SWAA2025060275749Vapor Barrier · crackedA/C HAS FIBER VAPOR BARRIER CRACK BETWEEN RBL 31.83 & RBL 40 APPRX 11.5 IN LENGTH AND 11 FROM BOTTOM OF VAPOR BARRIER. ZONE 1 <[01]. PERFORMED STOP DRILL OF CRACKED AREA AND APPLIED SPEED TAPE. REF SRM. 57-10-10-1A-2 STEP 2(C)(4). DO A VISUAL INSPECTION OF THSDR VNAA202508030004Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --SDR VNAA202508030001Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --SDR NACA2025052500006Bracket · crackedRH FIXED TRAILING EDGE UPPER INBOARD PANEL ANGLE BRACKET CRACKED. STOP DRILLED CRACK. FAB DBLR 15-5 .050 HEAT TREATED ROCKWELL @33. PRIMED INSTALLED ANGLES REF B737 SRM 57-51-90 AND EO 737-53-00003SDR NACA2025052500005Bracket · crackedLH FIXED TRAILING EDGE UPPER INBD PANEL ANGLE BRACKET CRACKED. STOP DRILLED END OF CRACK. FABRICATED CBER 15-5 050 FOR HEAT TREAT - ROCKWELL TEST @33. PRIMED AND INSTALLED REF B737-400 SRM 51-51-90 AND EO 737-00003SDR CALA2025052704959Angle · crackedLEFT WING FIXED L/E FR15 HAS CRACKED SMALL ANGLE AT INNER BAY R & R ANGLE AT LH WING FR15 INNER BAY IAW A320 SRM 51-72-11 -911-001.SDR SWAA2025063073727Rail · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS449 AT RT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 449 AT RT WING IAW-B737-700-SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG# 112A4402 SHEET 13 REV - .SDR SWAA2025063072654Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 AT LT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A6200 SHEET:11 REV:B<BR>CRACK LENGH IS 1.700 INCH.SDR SWAA2025063072396Support Angle · crackedCRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING IAW B737-700 SRM 51-40-02-0G AND SRM 51-10-02-0G ITEM 9.<BR>MEASURE OF CRACK IS: L= 1.870.SDR SWAA2025060670761Winglet · corroded(147-22) R/H WINGLET LOWER STRAKELET HAS CORROSION AT LOWER I/B SURFACE 14.5' FROM LOWER EDGE <[01]. REMOVED AND REPLACED R/H WINGLET LOWER STRAKELET TIP CAP ON FAULT TTG8Q010E2KN; [02] VERIFIED ITEM 1. AUDIT C/W.SDR SWAA2025060670759Winglet · corroded(147-23) R/H WINGLET LOWER STRAKELET HAS CORROSION AT LOWER I/B SURFACE 21.5' FROM LOWER EDGE <[01]. REMOVED DAMAGE AND VERIFIED WITH A 10X MAGNIFYING GLASS I.A.W SRM 51-10-02-0G-0 AND SRM 57-31-01 (AP37. 1-0632). DAMAGE FOUND TO BE OUT OF LIMITS DUE TO 100%SDR SWAA2025051970280Angle · crackedOUTER ATTACHMENT CLIP FOR SUPPORT RIB UNDER LEFT WING PANEL 551GB CRACKED<[01] REMOVED + REPLACED OUTER ATTACHMENT CLIP FOR SUPPORT RIB UNDER LEFT WING PANEL 551GB IAW SRM 51-40-02.SDR SWAA2025060270078Web · crackedLEFT WING INBOARD FIXED TRAILING EDGE WEB; BRACKET WITH CURVED SEAL CRACKED. STREAMER STUFFED INTO CURVED SEAL TO AID IN LOCATION.<[01] REMOVED WEB; BRACKET & SEAL RETAINER IAW B737-700 SRM 51-40-02. RECEIVED NEW BRACKET PN: 115A2953-1 PO# 1098329.1 IAW B737-7SDR SWAA2025060277299Bracket · crackedLEFT WING INBOARD FIXED TRAILING EDGE WEB; BRACKET WITH CURVED SEAL CRACKED. STREAMER STUFFED INTO CURVED SEAL TO AID IN LOCATION.<[01] REMOVED WEB; BRACKET & SEAL RETAINER IAW B737-700 SRM 51-40-02. RECEIVED NEW BRACKET PN: 115A2953-1 PO# 1098329.1 IAW B737-7SDR CALA2025050504456Plate · crackedRIGHT WING TRAILING EDGE WIGGLE PLATES HAVE CRACKS. REMOVED AND REPLACED WIGGLE PLATE PER ECRA NO. 5720-03526 CREATED ESFR REMOVED AND REPLACED WIGGLE PLATE PER ECRA #5720-03526.SDR SWAA2025060666780Support Bracket · elongatedELONGATED HOLE ON SUPPORT BRACKET LOCATED INTERNAL CAVITY LEADING EDGE IFSS152 AT LT WING 2025-291146 <[01]. REPLACED SUPPORT BRACKET LOCATED INTERNAL CAVITY LEADING EDGE IFSS152 AT LT WING IAW SRM B737-700 51-40-02-0G-0; [02] REPLACED SUPPORT BRACKET LOCATEDSDR IPXA2025052517581Rub Strip · cracked**SDR FILED OPEN** 1EA FWD RUBBING STRIP WITH A CRACK AT L/H WING CENTER FLAP UPPER SURFACE. DOT 21-57 APPROVED.SDR SWAA2025052765680Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2025-295979<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT BRSDR SWAA2025052765679Support Bracket · crackedCRACK SUPPORT BRACKET INBOARD TRAILING EDGE ORSS 271 AT LT WING 2025-295977<[01] REPLACED SUPPORT BRACKET INBOARD TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[0SDR SWAA2025052765678Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2025-295976<[01] REPLACED ANGLE AND FASTENERS LOC. TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET: 7 REV:-.SDR SWAA2025060265017Angle · crackedCRACK ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING 2025-274552<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND MEASURES OF CRACK IS: 1.369? <BR>TOOL USED:<BR>CALIPER P/N: 500-197-30; S/N: A18135SDR IPXA2025052379147Web · cracked**SDR FILED OPEN** FAULT: STR-Z600 RH WING REAR SPAR ABOVE FLAP TRACK #4 HAS SUPPORT CRACKED. DOT 11-026 REVIEWEDSDR SWAA2025043064406Bracket · crackedLEFT WING UPR I/B FWD PANEL SUPPORT FWD ATTACH BRACKET IS CRACKED. (Z BRACKET)<[01] R+R LEFT HAND Z BRACKET IAW SRM 51-40-02SDR SWAA2025043064407Bracket · crackedRIGHT WING UPR I/B FWD PANEL SUPPORT FWD ATTACH BRACKET IS CRACKED. (Z BRACKET)<[01] REPLACED BRACKET IAW SRM 51-40-02.SDR CALA2025042904311Support Bracket · cracked(SDR)B757-57-3-0369-RH WING UPPER WTB FAIRING 196AR, AFT BRACKET SUPPORT IS CRACKED SFR REPORTING ONLY REMOVED T-CHORD OUTER CRACKED I.A.W B757-200 SRM 51-40-02-0G-0 A ND RECEIVED T-CHORD OUTER NEW P/N UASRM 53-40-71-01-1-13 TRAVEL ER # T25/1808169 AND INSTALSDR VNAA20250529030Canister · crackedCRACK ON CANISTER WELDED NO. 3 IN WS 148.01 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO. 3 IN WS 148.01 AT INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -SDR VNAA20250529029Canister · crackedCRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -SDR SWAA2025051251405Support Angle · crackedR/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PERSDR SWAA2025050526851Angle · crackedR/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PERSDR SWAA2025050535622Support Angle · crackedR/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PERSDR N6WA2025042201Support Angle · corrodedTIRE BURST SUPPORT ANGLE LH MLG ON AFT SIDE OF AFT WING SPAR CORRODED. REMOVED AND REPLACED LH MLG TIRE BURST SUPPORT ANGLE ON AFT SIDE OF WING SPAR IAW CRJ SRM 51-42-21.SDR SWAA2025050526424Bracket · crackedRIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WSDR SWAA2025050535614Bracket · crackedRIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WSDR DALA2025042103074Stiffener · corrodedLH AUX SPAR WEB STIFFENER 9919401-5 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/209 01577: REPLACED PER B717 DWG 9919401. (LP #0921228)SDR VNAA20250529008Bracket · cracked2900 FH PERM REPAIR - TEMPORARY DISPOSITION FOR DENT DAMAGE TO INBD LOWER WING T/E SKIN BETWEEN WSTA14.500 AND WSTA50.000, RHS SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 2900 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. WITHIN 2900 FLIGHT HO
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