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 UIEA2025032800414Web · cracked1EA CRACK WAS FOUND ON WEB AROUND 2EA FASTENERS ON LHW MID SPAR WEB UPPER FROM WS 382 TO WS 441(<P>M/D SPAR WEB REPAIRED AS PER RI-57-20-17528 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800415Web · cracked5EA CRACK WERE FOUND ON WEB AROUND 2EA FASTENERS ON RHW MID SPAR WEB UPPER FROM WS 382 TO WS 411(<P>MID SPAR WEB REPAIRED AS PER RI-57-20-17527 REV A. NO FURTHER DEFECTS NOTED</P>)SDR CALA2025041803986Angle · crackedLEFT WING FIXED L/E INNER BOTTOM ANGLE HAS CRACK AT FR 15. RMVD AND RPLD L/W FIXED L/E INNER BOTTOM ANGLE AT FR15 IAW A320 SRM 51-72-11-911-002.SDR SWAA2025042124868Bracket · crackedL/H WING TRAILING EDGE UPPER BULB SEAL BRACKET; INBOARD OF FLAP DEFLECTION RIB; IS CRACKED. SEE ATTACHED PICTURE.<[01] REMOVED AND REPLACED L/H WING TRAILING EDGE UPPER BULB SEAL BRACKET; INBOARD OF FLAP DEFLECTION RIB REF AMM 20-50-11SDR SWAA2025052057358Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 140 AT LT WING 2025-250435<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 AT LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2000 SHEET 21 REV ?-? <BR><BR>MEASURE OF CRACK IS L: 0.500 IN. TOOL USED DIGITSDR SWAA2025051251332Support Bracket · corrodedR/H WING L/E FUELING GAUGES SUPPORT BRACKET HAS SEVERAL AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING L/E REFUELING GAUGES SUPPORT BRACKET (P15 PANEL) PER AMM 28-21-00.;[02] INSPECTION C/W C/A #1;[03] REQUIRES INSTALLATION TEST PER AMM 28SDR SWAA2025051956289Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON TRAILING EDGE ORSS 271 RT WING 2025-242547<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDITIONAL DAMAGES AND INSTALLED NEW SUPPORT ANGLE (WEB ASSY) LOCATED ON TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-1SDR SWAA2025051923880Support Bracket · crackedCRACK ON SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING. 2025-242544<[01] REPLACED SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING IAW-B737-700-SRM 51-10-02-0G-0 ITEM 9 AND 51-40-02-0G-0 TOOK MEASURE OF CRACK IS: 0.121 INCHES TOOL USED ELECTRONISDR SWAA2025051956291Angle · crackedCRACK ON ANGLE LOCATED ON TRAILING ORSS 281 RT WING 2025-242548<[01] REPLACED ANGLE (CLIP) LOCATED ON TRAILING ORSS 281 RT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0 AND DWG: 115A6200 SHEET: 11 REV B MEASURES OF CRACK L: 0.4080' TOOL USED DIGSDR SWAA2025051956297Angle · crackedCRACK ACCESS PANEL 551FB ON ANGLE AT LT WING 2025-242556<[01] REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02-0G 51-10-02-0G-0 STEP 9 AND DWG 115A2710 SHEET 9 REV- A. AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE ON SRM. MEASURE SDR SWAA2025051923776Gland Nut · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP IB EDGE AT LT WING 2025-250385<[01] TOOL USED: CALIPER PN: 500-196-30; SN: B23373747; DUE DATE: 26-JAN-26.;[02] TOOL USED STEP 3: ULTRASONIC EQUIPMENT; P/N: BONDMA600D; S/N: 230106912; DUE DATE: 05 FEB 26.;SDR SWAA2025051956277Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT LT WING 2025-242530<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDITIONAL DAMAGES AND INSTALLED NEW SUPPORT ANGLE (WEB ASSY) LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROSDR IPXA2025052521090Web · crackedRT WING INBD LEADING EDGE WEB CRACKED NEAR RIB 2.SDR IXXA20250410002Bracket · cracked5 SLAT O/B L/E PANEL NOSE FORMER BRACKET CRACKED AND FASTENER PULLING THROUGHSDR SWAA2025051957261Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2025-250130<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND SRM B737-700 51-40-02 AND DRAWING # 115A2930 SHEET 6 REV: -.;[02] TASK COMPLETEDSDR SWAA2025051957260Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING 2025-250129<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND SRM B737-700 51-40-02 AND DRAWING # 115A2930 SHEET 6 REV: -.;[02] TASK COMPLETEDSDR UIEA2025040400437Seal · brokenLH WING ACCESS PANEL 561BB WITH BOTH BULB SEAL BROKEN.(<P>BROKEN SEAL REPLACED AND CORRECTLY INSTALLED PER SRM 51-10-02-0G-0 PARA 9 REV 51. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040400439Pad · brokenLEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD BROKEN.(<P>LEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD WAS REPLACED IAW AMM 57-54-06-914-002 REV 144 DATE 22DEC24. NO FURTHER DEFECT NOTED.</P>)SDR KCSA202504051074Angle · crackedCRACKED ANGLE ON RW AFT OF REAR APPROX WBL 412SDR SWAA2025043021682Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INCSDR SWAA2025043021684Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.780 SDR SWAA2025043021685Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -SDR SWAA2025043055843Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INCSDR SWAA2025043055846Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -SDR KCSA202504041065Stiffener · crackedCRACKED STIFFENER ON L/H WING T/E AUX SPAR AT WBL 429.5SDR SWAA2025043055842Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING 2025-238292<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.932 INSDR IXXA20250403008Support Angle · corrodedINBD UPPER T/E PANEL, INBD FWD TO AFT SUPPORT ANGLE IS CORRODED AT THE FWD AND AFT ATTACHING HARDWARE.SDR IXXA20250403001Support Bracket · corrodedSUPPORT ANGLES, AND HARDWARE FOR EWIS CLAMPS AND HYDRAULIC BLOCK CLAMPS ARE CORRODED AT LEFT WING FUEL TANK REAR SPAR JUST ABOVE FORWARD TRUNNIONSDR VNAA202504020032Canister · 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 VNAA202504020031Canister · crackedCRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -.SDR SWI2025F00977Angle · corrodedANGLE FOR RH TIRE BURST PANEL 642AZ IS CORRODED. REPLACED ANGLE FOR RH TIRE BURST PANEL 642AZ REF CRJ900 SRM 51-42-21-001-001-A01, DWG CC670-10320 REV. -F. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY AND 28-900-1000-SKY. SEE CONTINUATION FOR DETAILS. COMPLSDR SWAA2025050554031Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 AT RT WING 2025-232325<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WIN IAW B737-700 SRM 51-40-02-0G AND DWG 115A2930 SHEET 8 REV -;[02] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WIN IAW B737-700 SRM 51-40-02-0G AND DWGSDR SWAA2025050554032Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 280 RT WING 2025-232326<[01] REPLACED ANGLE LOC TRAILING EDGE ORSS 280 RT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A6200 SHEET 11 REV B;[02] CORRECTED STEP 1 REPLACED ANGLE LOC TRAILING EDGE ORSS 280 RT WING IAW B737-700 SRM SDR SWAA2025050554030Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2025-232328<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 LT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9 AND DWG: 115A2930 SHEET: 7 REV - MEASURES OF CRACK L: 0.3950? TOOL USED DIGITAL CALIPER P/N: 500-197-SDR SWAA2025050554033Web · crackedCRACK WEB TRAILING EDGE ORSS 270 FIXED PANEL DEFLECTION CONTROL RIB BEAM AT RT WING 2025-232327<[01] REPLACED WEB TRAILING EDGE ORSS 270 FIXED PANEL DEFLECTION CONTROL RIB BEAM AT RT WING IAW B737 SRM 51-10-02 AND SRM 51-40-02 DWG 115A2512 SHEET 14 REV-A;[02] SDR 9WGA2025042854615Mount · corrodedDURING HEAVY MAINTENACE PNL 513AT MOUNT FLANGE HAS SURFACE CORROSION. REMOVED SURFACE CORROSION BY HAND AT LEFT WING ACCESS PNL 531AT ATTACHING FLANGE IAW MD-11 SRM 51-21-01 PAR. 36 NO MATERIAL LOSS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA2025042220075Plate · crackedDOT#02 A-043 LH WING T/E WAFFLE PLATE CRACKED AT INBD FASTENER WS 302.50<[01] REMOVED AND REPLACED WAFFLE PLATE ON LH WING WS 302.50 I.A.W. SRM 51-40-02-0G-0 AND DWG 115A3712 REV:-;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025050154415Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK INBOARD POSITION OF SLAT 8 AT RT WING 2025-224502<[01] REPLACED SKIN TAB SUPPORT ANGLE LOCATED ON AUXILIARY TRACK INBOARD POSITION OF SLAT 8 AT RT WING I.A.W. B737-700 CMM 57-43-01.<BR>SEE INDIVIDUAL SIGN OFF BELOSDR SWAA2025042219649Bracket · crackedLEFT WING TRAILING EDGE; INBOARD OF DEFLECTION CONTROL RIB; WEB BULB SEAL RETAINER BRACKET CRACKED AT UPPER 2 EA. BOLTS.<[01] 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] 01 - REMOVED ANSDR SWAA2025042219655Angle · cracked(A204 DOT 3) RH WING TRAILING EDGE CAVITY. 1 INCH INBOARD OF DEFLECTION CONTROL RIB. AND 24 INCHES FWD OF PANEL TRAILING EDGE. LATTERAL SUPPORT ANGLE IS CRACKED OUTBOARD FASTNER HOLE COMMON TO SKIN.<[01] REMOVED AND REPLACED LATTERAL SUPPORT ANGLE ON RH WING TSDR SWAA2025050554008Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 272 CONTROL RIB AREA AT LT WING 2025-232249<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9 AND DWG: 115A2930 SHEET: 6 REV - MEASURES OF SDR CALA2025032703249Web · corrodedRIGHT WING REAR SPAR HAS CORROSION AT IB BOOST PUMP LWR GROUND ATTACH POINT. REPAIRED RIGHT WING REAR SPAR IB BOOST PUMP LWR GROUND ATTACH POINT SERVICE PER AAR MIA ESR-WI #23-11683 AND UNITED EC/RA #5720-03507.SDR WRXR20250324001Angle · corrodedCORROSION ABOVE PANEL 691JB, ON WING, AT RH WS222.46 - WS260.04. REMOVED CORROSION TO AREA ABOVE PANEL 691JB AT RH WS222.46 - WS260.04 AND CREATED GRID FOR NDT TO DETERMINE MATERIAL THICKNESS IAW CRJ 900 SRM 51-21-06-001-001-A01. ALODINED, PRIMED, AND PAINTED,SDR AALA202504049776Support · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING AFT LOWER PANEL SUPPORT RAIL FROM FLAP TRACK 7 TO FLAPTRACK 8 HAS AREAS OF CORROSION. REMOVED CORROSION AT RIGHT HAND WING AFT LOWER PANEL SUPPORT RAIL FROM FLAP TRACK 7 TO FLAP TRACK 8. PER B737NG SRM 51-10-02-OG,SDR COEA2025050102803Shield · corrodedWO 265739 NR 600006 BRIDGING COE/MINOR DISCREPANCY: R/H SPOILER THUNDER SHIELD BLADE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: SPOILER REPAIRED PER ATR72 SRM 5771-10-300-823-A01.SDR SWAA2025050615901Plate · crackedWIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4. VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2025042205782Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 11SDR SWAA2025042105784Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202806<[01] INSTALL NEW ANGLE AND PLATE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REVSDR SWAA2025042114956Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 11SDR NACA2025031400002Bracket · crackedCRACKED BRACKET, R/H WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET.
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