JASC 5710

Service difficulty reports · 4,456

Reports filed under 5710 · Wing Main, Frame 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 = '5710'
  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 IPXA2026061035797Former · crackedCRACK-FORMER , FWD SIDE OF LT WING OUTBD L/E NOSE BEAM , OSS 441.6. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO: 114T2241 SH 4 REV. - AND UPS EO NO: SREO-54290-REQ1 REV3.Jun 6, 2026 · N397UP · Boeing 767300SDR SWAA2026062409094Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED FASTENERS AND CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DWG 115A2713 SHEET 3, REV A.Jun 3, 2026 · N7876A · Boeing 7377Q8SDR SWAA2026062409092Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS 272 AT RT WING IAW SRM 51-40-02.Jun 3, 2026 · N7876A · Boeing 7377Q8SDR SWAA2026062409093Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2001; SHEET: 1; REV B.Jun 3, 2026 · N7876A · Boeing 7377Q8SDR SWAA2026062408976Fitting · damagedELONGATED HOLE ON FITTING TRAILING EDGE LOCATED ORSS256 AT LT WING. REPLACED FITTING LOCATED ON TRAILING EDGE ORSS 256 AT LT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02 ITEM 9, DWG 115A5300 SHEET 17, REV- .Jun 3, 2026 · N7876A · Boeing 7377Q8SDR SWAA2026062409091Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT LT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS272 AT LT WING IAW SRM 51-40-02 AND DWG 115A2714; SHEET 6; REV: -. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1Jun 3, 2026 · N7876A · Boeing 7377Q8SDR SWAA2026062309065Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219 AT LT WING. REPLACED CORRUGATED PLATE LOC. ON TRAILING EDGE IRSS 219 AT LT WING IAW SRM 51-40-02-0G-0 AND 51-10-02-0G-0, ITEM 9.Jun 3, 2026 · N476WN · Boeing 7377H4SDR SWAA2026062309073Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04-0G-0 ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (2/EA) REMOVED AND INSTALLED FASJun 3, 2026 · N476WN · Boeing 7377H4SDR SWAA2026062308954Fastener · brokenCRACKED CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04 ON CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (1 E/A). REMOVED AND INSTALLED FASTENER IAW SRM 51-40-02, Jun 3, 2026 · N476WN · Boeing 7377H4SDR IPXA2026061583676Duct · damagedENLARGE - HOLE , RT WING T/E OUTBD FUEL TANK VENT SCOOP AND DUCT ASSY. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-17-0G-0 REV.106. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VJun 3, 2026 · N577UP · Boeing 74744AFSDR KCSA202606021040Tee Angle · crackedVERTICAL TEE CRACKED, O/B END OF FIXED T/E BEAM AT WBL429Jun 2, 2026 · N712CK · Boeing 7474B5FSDR SWIA2026053177168Landing · damagedFAILED NDT, FOUND FULL SCREEN INDICATIONS ON THE LANDING OF RT WING LOWER PLANK ACCESS HOLE, PANEL 640CB. REPAIRED LANDING IAW REO 601R-57-21--030, REV L, & REO 601R-57-21-4120, REV -.May 31, 2026 · N455SW · Cndair CL6002B19SDR VNAA202608010018Retainer · corrodedCORROSION ON INNER SEAL RETAINER 2 EAS AT ACCESS PANEL 583BB. INNER SEAL RETAINER 2 EAS AT ACCESS PANEL 583BB WERE REPLACED PER SRM 51-42-10-001-001-A01May 31, 2026 · N644NN · Cndair CL6002D24SDR SWAA2026061707972Plate · crackedCRACKED OTBD TRAILING EDGE CORRUGATED PLATE ON ORSS 314, RT WING. REPLACED CORRUGATED PLATE LOCATED OTBD TRAILING EDGE ON ORSS 314 AT RT WING. IAW SRM 51-40-02-0G-0 AND DWG 115A3700, SHEET 32 REV-.May 30, 2026 · N482WN · Boeing 7377H4SDR SWAA2026061707886Plate · crackedCRACKED INBD TRAILING EDGE CORRUGATED PLATE LOCATED ON IRSS 242 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON INBD TRAILING EDGE IRSS 242 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001, SHEET 30, REV A.May 30, 2026 · N482WN · Boeing 7377H4SDR IPXA2026061525611Retainer · crackedLEFT WING GEAR W/W OUTBOARD DOOR AFT SEAL RETAINER CRACKED. I.A.W SRM 51-40-02-0G REV. 106 AND DWG:65B10907 SHEET 11 REV.- INSTALL NEW RETAINER.May 30, 2026 · N577UP · Boeing 74744AFSDR IPXA2026061525657Retainer · crackedLEFT WING GEAR W/W OUTBOARD DOOR FWD SEAL RETAINER CRACK (REPLACE)  I.A.W SRM 51-40-02-0G REV. 106 AND BOEING DWG:65B10907 SHEET 11 REV.- INSTALL NEW RETAINER.May 30, 2026 · N577UP · Boeing 74744AFSDR CALA2026060316762Longeron · crackedRIGHT SIDE UNDERWING LONGERON REQUIRES REPLACEMENT OPS 550032484 AND EA 5710-02896 OPS 008. RT SIDE UNDERWING LONGERON REPLACEMENT OP 008 OVERVIEW WAS ACCOMMPLISHED SATISFACTORILY IAW EA 5710-028 96 REV B OP 008May 30, 2026 · N664UA · Boeing 767322SDR AALA202607147542Support Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FALSE REAR SPAR FALSE SUPPORT FITTING BETWEEN RIB 7 AND RIB 8. REPLACED SUPPORT FITTING PER SRM 51-42-11.May 29, 2026 · N9015D · Airbus A319115SDR IPXA2026060288483Erosion Shield · damagedL/H WING L/E NO.3 V.C FLAP EXTERNAL INBD SIDE AND UPPER CORNER AREA. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70°FMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060287525Erosion Shield · damagedL/H WING L/E NO.5 V.C FLAP EXTERNAL INBD SIDE AND UPPER CORNER AREA. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060287486Erosion Shield · damagedL/H WING L/E NO.5 V.C FLAP EXTERNAL OUTBD SIDE AND UPPER CORNER AREA. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CUREMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288202Erosion Shield · damagedL/H WING L/E NO.1E V.C FLAP EXTERNAL OUTBD SIDE. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70F FOR 48 HOURS. May 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288423Erosion Shield · damagedL/H WING L/E NO.1 V.C FLAP EXTERNAL OUTBD SIDE. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOURS.May 28, 2026 · N577UP · Boeing 74744AFSDR SWAA2026061707340Support Angle · elongatedELONGATED HOLE ON SUPPORT ANGLE FOR ACCESS PANEL 551FB TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE AND RE-INSTALLED BRACKET(2E/A) ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW SRM 51-10-02-OG-0, ITEM 9, SRM 51-40-02-OG-0, SRM 51-20-01-0G-0, AND DWG 11May 27, 2026 · N482WN · Boeing 7377H4SDR SWAA2026061707341Support Angle · crackedCRACKED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.May 27, 2026 · N482WN · Boeing 7377H4SDR IPXA2026060257012Former · crackedRIGHT WING OTBD L/E, NOSE FORMER CRACK, OSS 499.60. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 4 REV.- AND SREO-50900-REQ001 REV.May 26, 2026 · N341UP · Boeing 76734AFSDR SWAA2026061506377Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 26 REV-.May 25, 2026 · N483WN · Boeing 7377H4SDR DALA2026052603171Sealant · damagedOUTER WING GLOW SEALANT OPTIMISATION RH WING A350. CORRECTIVE ACTION: ACCOMPLISHED SEALANT APPLICATION AND INSPECTION PER W/C 5720-01102-05B. LOG PAGE GENERATED AND SDR REPORTABLE CHECKBOX MARKED AS PER STEP 23 W/C 5720-001102-05B AND TOPP 20-50-20. (1611373) May 25, 2026 · N514DN · Airbus A350941SDR DALA2026052603170Sealant · damagedOUTER WING GLOW SEALANT OPTIMISATION LH WING A350. ACCOMPLISHED SEALANT APPLICATION AND INSPECTION PER W/C 5720- 01102-05A. AS PER STEP 23 W/C 5720-001102-05A AND TOPP 20-50-20. (1611275) AIRCRAFT WAS GROUNDED.May 25, 2026 · N514DN · Airbus A350941SDR CALA2026060116680Support Beam · crackedRIGHT WING PANEL 671DB HAS A CRACK. INSTALLED PANEL 671 DB IAW B737-800 SRM 51-40-02-0G-0. REMOVED PANEL 671DB & BEAM SPRT RH WING, EVAUATED FOUND TO BE OUT OF LIMITS, VERIFIED MATERIAL, FABRICATED NEW SUPPORT, LOCATED AND DRILL NEW SUPPORT,APPLIED ALODINEMay 23, 2026 · N14249 · Boeing 737824SDR UIEA2026040800152Structure · corrodedRH WING W/W STA 1241 AREA CENTER TANK RH JETTISON TRANSFER VALVE ( V52 ) CUTOUT FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED, ORIGINAL 0.496", L:4" X W:4" X D: 0.006", WITHIN SRM 57-10-May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800153Structure · corrodedL/H WLG W/W STA 1241 AREA CENTER TANK L/H JETTISON TRANSFER VLV (V1) CUTOUT FOUND CORROSION.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL: 0.496" L : 4" X W : 4" X D: 0.012", WITHIN SRM 57-10-May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800154Structure · corrodedL/H WLG W/W STA1241 AREA. CENTER TANK LEFT O/J PUMP (M224) CUTOUT FOUND CORROSION.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL: 0.810", L: 4" X W : 1.8" X D : 0.065" WITHIN SRM 57-10-10-1A-2 ALLOWMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041600201Support Fitting · crackedRHW T/E I/B CAVITY #7 SPOILER ACTUATOR SUPPORT FITTING O/B LOWER EDGE FOUND CRACKED.(<P>SUPPORT FITTING O/B LOWER EDGE CRACK AREA REPAIRED AS PER RI-57-51-18166 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041800217Structure · corrodedRH WLG W/W STA 1241 AREA CENTER TANK RIGHT O/J PUMP ( M225 ) CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18226 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041900220Beam · crackedLHW L/E NEAR #2 PYLON O/B D-BEAM WEB FOUND CRACK ( ILES 693 )(<P>WEB CRACK AREA REPAIRED AS PER RI-57-41-18207 REV B. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026042200232Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM WEB CRACK ( ILES 1116 )(<P>CRACK WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED.</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100279Beam · crackedRHW L/E #17 VC FLAP CAVITY I/B D-BEAM O/B WEB FOUND CRACK ( #3 PYLON O/B )(<P>WEB REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100280Beam · crackedRHW L/E #17 V/C FLAP CAVITY I/B D-BEAM O/B UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100285Beam · crackedRHW L/E D-BEAM ILES 693 LOWER CHORD FOUND CRACK(<P>LWR CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050400292Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050400293Beam · crackedRHW L/E D-BEAM ILES 691 WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-57-41-18266 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051000308Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMMay 23, 2026 · N477MC · Boeing 74747UFSDR CALA2026060116678Support Beam · corrodedRIGHT WING OUTBOARD TE UPPER PANEL SUPPORT SHIM ATTACHMENT HAS DISBONDED UPPER ALL AILERON BALANCE PANEL AFT ATTACHMENT AREA. INSTALLED NEW SUPPORT BEAM ON R/H WING PANEL 671 BT IAW SRM 51-40-02-0G-0. REMOVED BEAM SPRT RH WING, EVAUATED FOUND TO BE OUT OF May 22, 2026 · N14249 · Boeing 737824SDR SCNA20260630272Pressure Deck · crackedTHREE CRACKS WERE FOUND ON THE RT WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB, BS 663.75, RBL 25 TO RBL45: BETWEEN RBL31.83 AND RBL 40.00 CRACK 1=1.1125IN LENGH, CRACK 2=1.060IN LENGTH, BETWEEN RBL 40.00 AND RBL 45.64 CRACK 3=3.0IN LENGTH, IN REFEMay 19, 2026 · N827SY · Boeing 7378F2SDR SWAA2026060104617Cartridge · crackedCRACK FOUND ON LT OUTBOARD AFT FLAP INBOARD CARTRIDGE INNER SURFACE. LEFT WING OUTBOARD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW B737 CMM 57-53-08. ASSEMBLY 2.C.(2);May 19, 2026 · N8670A · Boeing 7378H4SDR CALA2026061116999Pressure Web · crackedCRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64, BETWEEN WL 192.0 AND WL 200.6. CRACK LENGTH : 1". ACCOMPLISHED VERTICAL PRESSURE WEB REPAIR AT STA 663.75 BETWEEN RBL 32 TO RBL 45 IAW SRM 57-10-10-2R-3 PARAGRAPH 5. FIGURE 204. IMay 18, 2026 · N73256 · Boeing 737824SDR REXA2026060400918Hinge · crackedCRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IRMay 18, 2026 · N909XJ · Cndair CL6002D24SDR REXA2026060400912Hinge · crackedCRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IRMay 18, 2026 · N909XJ · Cndair CL6002D24
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