JASC 5753

Service difficulty reports · 31,496

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 AALA202505029752Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT AFT ATTACH FITTING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-72-11.Apr 27, 2025 · N176UW · Airbus A321211SDR SWIA20250715426Panel · mechanic errorMIS-DRILLED FASTENER ON PANEL 584 CB MARKED WITH RED TAPE REQS REMOVAL. (C-CHECK RO 07/15/2025)REMOVED DAMAGE FROM LH WING IB FLAP LOWER SKIN DOUBLER AND RIB AT ST 135.512 IAW REO 6015-57-52-2518 REV -- DATED 2025-06-15. COMPLETED TASK CARD 51-900-1003-SKY ANApr 26, 2025 · N929SW · Cndair CL6002B19SDR SWAA2025052864261Skin · delaminatedR/H O/B AFT FLAP LOWER INBD CORNER HAS PREVIOUS REPAIR THAT HAS DELAMED. REMOVED PREVIOUS REPAIR;,NO ADDITIONAL DAMAGE NOTED PER SRM 57-53-01-2R-14, ACCOMPLISHED TAP TEST PER NDT MANUAL PART 1 51-05-01. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER & BONDEApr 25, 2025 · N8687A · Boeing 7378H4SDR DALA2025043003312Hinge Fitting · wornLH WING OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. MACHINED IB AND OB LUGS TO REMOVE DAMAGE. OB LUG BORE FINAL SIZE IS .533. IB LUG FINAL SIZE IS .594. INNER FACE OF IB LUG SPOTFACED .880 DIAMETER WITH .060 RADIUS TO A DEPTH OF .076. REMAINING LUG THIApr 25, 2025 · N927AT · Boeing 717200SDR SWAA2025042958016Skin · delaminatedL/H WING INBOARD TRAILING EDGE MAIN FLAP LOWER SKIN IS DELAMINATED 6.90 WIDE AND 3.70 LONG. DELAMINATED AREA STARTS 2.45 IN FROM OUTBOARD EDGE AND GOES THROUGH TRAILING EDGE (SEPARATION). SEE PIC. R/H WING INBOARD TRAILING EDGE MAIN FLAP LOWER SKIN IS DELAMINAApr 25, 2025 · N474WN · Boeing 7377H4SDR DALA2025042503256Skin · damagedSHIP 676 LT #3 FLAP DAMAGE. CORRECTIVE ACTION: TEMPORARY REPAIR APPLIED PER B757 SRM 57-53. (7173721)Apr 25, 2025 · N676DL · Boeing 757232SDR DALA2025100807320Hinge Fitting · corrodedCORROSION ON FLAP FWD HINGE FITTING XRS=267 OF REAR SPAR AREA AT LH WING. REPLACED PER SERVICEABLE LT CENTER WING FLAP HINGE FITTING (0931308)Apr 24, 2025 · N921AT · Boeing 717200SDR SWAA2025052753374Skin · delaminatedLEFT OUTBOARD AFT FLAP HAS A HUGE DELAMINATION ON THE UPPER INBOARD SURFACE. (MARKED)<[01] OK TO INSTALL AFT FLAP;[02] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP PER. AMM 27-51-22PERFORMED LEFT WING OUTBOARD AFT FLAP ADJUSTMENT IAW AMM 27-51-22-400-801.;[03] Apr 24, 2025 · N8687A · Boeing 7378H4SDR UIEA2025042200561Skin · damaged#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2025 · N862GT · Boeing 7478FSDR UIEA2025042200562Skin · damaged#20 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2025 · N862GT · Boeing 7478FSDR FDEA202504240636Skin · dentedFOUND LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM IB SIDE CROSS 15 INCH FROM AFT SIDE. REPAIRED LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM IB SIDE CROSS 15 INCH FROM AFT SIDE AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5Apr 24, 2025 · N850FD · Boeing 777FSDR FDEA202504230763Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.6 AND STGR2.7 REPAIRED THE LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB17 BETWEEN STGR2.6 AND STGR2.7 PER A300-600F SRM57-50-00-201 FIG.201 AND COMPLIED WITH EA 6-5750-T0340067 A P2.Apr 23, 2025 · N656FE · Airbus A300F4605RSDR SWAA2025042864023Wedge · debondedLH IB MAIN FLAP TE WEDGE ASSY ADDITIONAL DISBOND UPPER AND LOWER SKINS WHILE PERFORMING TAP TEST FOUND ADDITIONAL AREAS OF DISBOND TO UPPER AND LOWER SKINS OF TE WEDGE. FOUND LOWER SKIN DISBOND 30 IN. L X 12 IN. W. FOUND UPPER SKIN DISBOND OF 27.5 IN. L X 6 INApr 23, 2025 · N224WN · Boeing 7377H4SDR FDEA202504230656Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA:6-5750-T0383190 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BETApr 23, 2025 · N656FE · Airbus A300F4605RSDR SWAA2025052956938Access Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES AT RT WING 2025-274301<[01]. TOOL USED: HOT BONDER PN:HCS9200B SN:16122983 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 12 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25; [03]Apr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956939Access Panel · crackedCRACK ACCESS PANEL 661AB AROUND HOLES TRAILING EDGE AT RT WING 2025-274296 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [0Apr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956940Access Panel · crackedCRACK ACCESS PANEL 661CB TRAILING EDGE AROUND HOLES RT WING 2025-274298 <[01] .TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03] Apr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956948Access Panel · crackedCRACK ACCESS PANEL 561AB TRAILING EDGE AROND HOLES LT WING 2025-274302 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03] TApr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956949Access Panel · crackedCRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2025-274303 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03] Apr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052927467Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING SRM 51-10-02 ITEM 9Apr 22, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956943Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 281 DEFFLECTION CONTROL RIB SUPPORT BEAM RT WING. REPLACED ANGLE ON TRAILING EDGE ORSS 281 DEFFLECTION CONTROL RIB SUPPORT BEAM AT RT WING IAW SRM 51-10-02 AND SRM 51-40-02. MEASURE OF CRACK IS L=1.182 IN.Apr 22, 2025 · N291WN · Boeing 7377H4SDR DALA2025042303179Strut · corrodedSHIP 3084 CORROSION ON REAR NUT INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED REAR NUT INTERCONNECTING STRUT IB FLAP ON LH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 27-51-44-400-001-A ANDPERFORMED GENERAL VISUAL INSPECTION ON Apr 22, 2025 · N384DN · Airbus A321211SDR SWAA2025052956926Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING. REPLACED ANGLE LOCATED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV -.Apr 21, 2025 · N291WN · Boeing 7377H4SDR SWAA2025052956924Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 281 AT LEVEL DEFLECTION CONTROL RIB SUPPORT BEAM LT WING. REPLACED ANGLE ON TRAILING EDGE ORSS 281 AT LEVEL DEFLECTION CONTROL RIB SUPPORT BEAM AT LT WING IAW SRM 51-10-02 AND SRM 51-40-02. MEASURE OF CRACK IS L=1.687 IN.Apr 21, 2025 · N291WN · Boeing 7377H4SDR WRXR20250421001Support · corrodedCORROSION FOUND AROUND 3 FASTENER HOLES OF STRUCTURE UNDER PANEL 681AB. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06-001-001-A01. EVALUATED NDT REPORT, FOUND TO BE OUT OF LIMITS. COMPLIED WITH REO 690-57-00-126 REV -- DATED: 2025-04-17.Apr 21, 2025 · N638NN · Cndair CL6002D24SDR VNAA20250529001Support · wornWEAR ON FLAP FITTING AND PLATE SUPPORT OF "FLAP STUB FAIRING" 171DL AND 172DR AT RH/LH WING TRAILING EDGE ROOT WING. DUE EXCESSIVE DAMAGE ON FLAP FITTING AND PLATE SUPPORT OF "FLAP STUB FAIRING" 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERE FOApr 20, 2025 · N553NN · Bombdr CL6002D15SDR SWI2025F01113Skin · dentedRIGHT INBOARD FLAP, SECOND FROM OUTBOARD VANE ACTUATOR SHAFT HAS DENT. REMOVED INDENTATION ON RH INBOARD FLAP, SECOND FROM OUTBOARD VANE ACTUATOR SHAFT. FOUND TO BE STRUCTURALLY ACCEPTABLE PER REO 670-57-52-257 REV -A DATED 2024-08-20. SEE CONTINUATION CARDApr 19, 2025 · N804SK · Cndair CL6002D24SDR VNAA20250528002Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01, WAS EVALUATED, AREA ON LOWER SKIApr 18, 2025 · N553NN · Bombdr CL6002D15SDR REXA2025042800513Skin · chafed"WHILE SANDING RH I/B FLAP FOR PAINT FOUND SKIN TO BE CHAFED AT I/B HINGE ARM FROM CONTACT WITH CANOE FAIRING WHILE SANDING RH I/B FLAP FOR PAINT FOUND SKIN TO BE CHAFED AT I/B HINGE ARM FROM CONTACT WITH CANOE FAIRING CHAFING WAS REMOVED IAW CRJ700 SRM TASK Apr 18, 2025 · N379CA · Cndair CL6002C10SDR CALA2025042104048Skin · gougedRIGHT WING O/B GLAP I/B L/E OF THE MAIN FL AP HAS A DEEP GOUGE. ECRA 5753-02305 ACCOMPLISHED ECRA 5753-02305 ON ST ENGINEERING NR 124688 SENT TO AVN FOR REPAIR ENTRY'SApr 18, 2025 · N57111 · Boeing 757224SDR UIEA2025032700394Skin · debondedLHW O/B FORE FLAP LOWER T/E O/B AREA FOUND DEBOND(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800395Skin · damagedRHW I/B MID FLAP O/B T/E SCREW HOLE FOUND ELONGATED(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. K. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800398Skin · puncturedLHW O/B FORE FLAP LOWER T/E MID AREA FOUND PUNCH(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800399Skin · delaminatedLHW O/B MID FLAP MOST O/B L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800401Skin · bulgedLHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800402Skin · bulgedLHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800403Skin · bulgedRHW I/B FORE FLAP LOWER SURFACE I/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800404Skin · bulgedRHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED.</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800405Skin · chafedRHW I/B AFT FLAP UPPER SURFACE MOST I/B PANEL FOUND CHAFING(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-53-17513 REV. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800406Skin · chafedRHW I/B AFT FLAP UPPER SURFACE MOST O/B PANEL FOUND CHAFING(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-53-17526 REV. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800407Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE I/B PANEL FOUND PUNCH(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.201. NO FURTHER DEFECTS NOTED</P> / <P> </P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800408Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE O/B PANEL FOUND SCRATCH(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800409Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE MID PANEL FOUND SCRATCH(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR SWAA2025051956575Skin · delaminatedLEFT WING O/B AFT FLAP HAS DELAMINATION ON I/B UPPER SIDE<[01] REPAIRED DELAMINATION DAMAGE ON I/B UPPER SIDE OF LEFT WING O/B AFT FLAP IAW SRM 51-70-10-2R-4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Apr 17, 2025 · N7858A · Boeing 73779PSDR VNAA202504170083Trunnion · corrodedRH OUTBD FLAP W.S. 140.4 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 140.0 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21Apr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170082Trunnion · corroded"RH OUTBD FLAP W.S. 102.9 AFT TRUNNION HAS CORROSION DAMAGE REQUIRES REPAIR CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 120.9 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21"Apr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170081Cradle · corroded"R/H INBD FLAP W.S. 65.5 CRADLE ASSY HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: RECEIVED SERVICEABLE RH WS 65.5 CRADLE ASSEMBLY PN CC670-14301-9. REFERENCE BARCODE HR483812 FOR INSTALL. CC670-14301-9"Apr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170080Trunnion · corrodedRH INBD FLAP W.S. 65.5 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 65.5 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21Apr 17, 2025 · N508AE · Cndair CL6002C10SDR FDEA202504170606Skin · no discrepancyEXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB16-RIB17 BETWEEN FRONT SPAR AND S2.3 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB16-RIB17 BETWEEN FRONT SPAR AND S2.3 WAS EVALUATED AND FOUND NOT IN CONFORMITApr 17, 2025 · N676FE · Airbus A300F4605RSDR FDEA202504170605Skin · damagedEXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB15-RIB18 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB15-RIB18 BETWEEN S2.2 AND REAR SPAR WAS EVALUATED AND FOUND NOT IN CONFORApr 17, 2025 · N676FE · Airbus A300F4605R
Back to JASC 5753