JASC 5753

Service difficulty reports · 31,493

Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753'
  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 SWAA2026060208084Fairing · delaminatedNR 3 FLAP AFT CANOE FAIRING IS DELAMINATED. R & R NR 3 FLAP AFT CANOE FAIRING IAW AMM 27-51-28.Jun 1, 2026 · N8325D · Boeing 7378H4SDR CALA2026060216750Skin · crackedSUPPORT TASK: RH O/B AFT FLAP LOWER SKIN AT I/B TRACK HAS CRACK AT DRAIN HOLE.TRANSCRIBED FROM AAR GSO NRC 9282672. RECEIVED NEW RIGHT WING OTBD AFT FLAP ASSY PN#113A3700-24UAL FLAP ASSY REMOVED AND REPLACED ON AAR GSO NRC 9282690. AAR GSO MECH V896730 ALL MAJun 1, 2026 · N45440 · Boeing 737924ERSDR IPXA2026060435092Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.10 V.C FLAP EXTERNAL OUTBD SIDE. (REPAIR) 1. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70May 31, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060435041Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.10 V.C FLAP EXTERNAL INBD SIDE. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURMay 31, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060435068Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.9 V.C FLAP EXTERNAL INBD SIDE. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.May 31, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060435120Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.8 V.C FLAP EXTERNAL INBD SIDE AREA. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIRMay 31, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060435070Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.7 V.C FLAP EXTERNAL INBD SIDE. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.May 31, 2026 · N577UP · Boeing 74744AFSDR SWIA2026053077186Spar · gougedTHE FWD FACE OF THE LT, INBD FLAP FWD SPAR HAD TWO GOUGES BETWEEN WS 805 AND 977. PERFORMED A MAJOR REPAIR TO THE LT, INBD FLAP FWD SPAR BY BLENDING GOUGES AND APPLYING SURFACE FINISH IAW REO 601R-57-52-2561, REV--, AND TASK CARD 51-900-1003-SKY. MAJOR REPAMay 30, 2026 · N455SW · Cndair CL6002B19SDR SWAA2026061707883Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 26 REV-.May 30, 2026 · N482WN · Boeing 7377H4SDR IPXA2026061713896Skin · crackedTASK T3F18E008M5G0 MISSING REFERENCE TO EO-97438 ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.May 29, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026060288681Skin · debondedDISBOND SKIN, R/H WING T/E OTBD MID FLAP WEDGE UPPER SKIN. PERFORMED NDT/UT FOR REWORKED AREA AND PLUS 6" AROUND HEATED AREA, IAW NDT MANUAL PART 1 51-01-01 REV.182. NO DEFECT FOUND.May 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288239Erosion Shield · damagedEROSION - MOLDING SEAL, R/H WING NO.17 V.C FLAP. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOUMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288457Erosion Shield · damagedEROSION - MOLDING SEAL, RH WING NO.20 V.C FLAP. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOURS. CONDITION CHECK IMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060287450Erosion Shield · damagedEROSION - MOLDING SEAL, RH WING NO.19 V.C FLAP. (REPAIR) 1. IAW 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOURS. CONDITION CHECK IS SMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288228Erosion Shield · damagedERODED MOLDING SEAL, R/H WING L/E NO.18 V.C FLAP. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOURS. CONDITION CHECK IS SATISFACTORYMay 28, 2026 · N577UP · Boeing 74744AFSDR IPXA2026060288222Seal · erodedEROSION ON MOLDING SEAL, R/H WING NO.18 V.C FLAP. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOURS. CONDITION CHECK IS SATISMay 28, 2026 · N577UP · Boeing 74744AFSDR FDEA202605280664Skin · crackedRH WING INNER FLAP TOP SKIN FOUND CARCKED BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2. REPAIRED THE CRACKED SKIN AT RH WING INNER FLAP BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2 PER SRM57-50-00-201 PARA.4E FIG.205. RSC TRACKING EA 6-5750-T0387591 WAS RAISEMay 28, 2026 · N660FE · Airbus A300F4605RSDR SWAA2026060806756Skin · delaminatedRIGHT OTBD AFT FLAP HAS AREA OF DELAMINATION, INBOARD AFT EDGE. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB.May 26, 2026 · N8574Z · Boeing 7378H4SDR IPXA2026060158500Skin · crackedRIGHT WING OUTBOARD FLAP, INBOARD T/E END CAP SKIN, UPPER AND LOWER FOUND SKIN DAMAGE. I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR .May 26, 2026 · N341UP · Boeing 76734AFSDR DALA2026052703184Flap Track · excess playLEVEL 2 CORROSION, LH WING I/B FLAP TRACK NR 2 SUPPORT ECCENTRICAL BEARING WITH PLAY. REPAIRED LT WING I/B FLAP TRACK NR 2 SUPPORT I/B AND OTBD FITTING FACES AND AL BORE HOLES IAW DELTA ERA 633957-14 REV ORIGINAL APPROVED DATE 19/MAY/26. THIS REPAIR APPROVAL May 25, 2026 · N368NB · Airbus A319114SDR SWAA2026052705761Rib · crackedRT WING OUTBOARD AFT FLAP HAS A CRACK INDICATION ON THE INBOARD CLOSURE RIB. TOP OF. CLOSURE RIB BOTTOM PORTION. HFEC VERIFIED. REMOVED AND INSTALLED OUTBOARD TRAILING EDGE FLAP IAW AMM 27-51-21.May 23, 2026 · N7729A · Boeing 73776NSDR UIEA2026033100116Panel · corrodedRH I/B T/E AFT FLAP O/B UPR PANEL LWR SURFACE SEVERAL AREA CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURE ORIGINAL THICKNESS 0.106" L:25" X W 1" X D : 0.009", WITHIN SRM 57-53-01-1A-0 FIG 101 LIMITS.May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800156Panel · corrodedLHW O/B T/E FOREFLAP I/B UPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORRODED.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL: 0.105", L:15" X W:1" X D:0.003", WITHIN SRM 57-53-01-1A-0 May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800157Panel · corrodedLHW OB T/E FOREFLAP O/B UPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORROSION(<P>CORROSION AREA REWORKED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL 0.105" L:14" X W:1" X D:0.002", WITHIN SRM 57-53-01-1A-0 ALMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800158Panel · corrodedLHW I/B T/E AFT FLAP I/B UPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL 0.105" L:22" X W:1" X D:0.002", WITHIN SRM 57-53-01-1A-0 ALMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800159Panel · corrodedLHW I/B T/E AFT FLAP MID UPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. REWORK AREA MEASURED ORIGINAL 0.105" L:23" X W:1" X D:0.003", WITHIN SRM 57-53-01-1A-0 ALLOWABMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040800160Panel · corrodedLHW I/B T/E AFT FLAP O/B UPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORRODED(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORIGINAL 0.105", L:20" X W:1" X D:0.003", WITHIN SRM 57-53-01-1A-0 ALLOWABMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041500199Skin · corrodedRHW I/B T/E FORE FLAP O/B UPPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.105", L: 13" X W: 1" X D: 0.002", WITHIN SRM 57-53-01-1A-0 ALLOWMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041800211Panel · corrodedRHW I/B T/E AFT FLAP MID UPPR PNL FWD LWR SURFACE SEVERAL AREA CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-53-18206 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100287Flap Track · corrodedLHW #4 FLAP TRACK FOUND SURFACE CORROSION AT BEARING PLATE CONTACT AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18196 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100288Flap Track · corrodedRHW #5 FLAP TRACK UPPER SURFACE CORROSION AT BEARING PLATE CONTACK AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18221 REV B. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050500296Stop Fitting · missingRHW L/E TO FRONT SPAR CAVITY ILES 756-766.45 UP STOP FITTING MISSING(<P>STOP FITTING FABRICATED AS PER RI-57-21-18259 REV A, AND NEW FITTING HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW FITTING INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700323Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700324Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700325Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700326Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700327Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700328Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700329Skin · delaminatedLHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700330Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700331Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700332Skin · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700333Skin · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700334Fairing · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700335Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700336Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700337Fairing · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700338Fairing · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026051700339Skin · crackedLHW I/B FORE FLAP O/B UPPER PNL INNER FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER SRM 51-70-10 REPAIR 4 FIG 202. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR SWAA2026060205759Rib · crackedCRACK FOUND ON RH O/B AFT FLAP INBOARD CLOSURE RIB CARTRIDGE INNER SURFACE. LOCATED AND DRILLED FASTENER HOLES, AND INSTALLED NEW NUT PLATES IAW SRM 51-40-02-0G-0 AND DWG 113A3700 REV. D. INSTALLED PROGRAM ROLLER ON NEW CLOSURE RIB IAW AMM 27-51-22-400-801 3.May 22, 2026 · N8564Z · Boeing 7378H4
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