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"

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SDR SWIA2026031175630Flap Track · out of limitsRIGHT, INBD AFT FLAP TRACK NR 6 HAS THICKNESS REDUCTION OF .028". THIS IS OUT OF LIMITS OF SRM 57-53-03/AD01. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED RT, INBD AFT FLAP TRACK NR 6. IAW AMM 27-51-08. OPS CHECKED.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR SWIA2026031175629Flap Track · out of limitsRIGHT, INBD AFT FLAP TRACK NR 5 HAS THICKNESS REDUCTION OF .029". THIS IS OUT OF ALLOWABLE LIMITS OF SRM 57-53-03/AD01. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED RT, INBD AFT FLAP TRACK NR 5. IN REFERENCE TO AMM 27-51-08. OPS CHECKED.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR SWIA2026031175628Flap Track · out of limitsRIGHT, INBD FLAP TRACK 1A HAS THICKNESS REDUCTION OF .028. THIS IS OUT OF ALLOWABLE LIMITS OF SRM 57-52-03/AD01. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED RT, INBD FLAP TRACK 1A. REF: AMM 57-54-25.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR SWIA2026031175627Flap Track · out of limitsLEFT, INBD FLAP TRACK 1A HAS THICKNESS REDUCTION OF .042. THIS IS OUT OF ALLOWABLE LIMITS OF SRM 57-52-03/AD01. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED LT, INBD FLAP TRACK 1A IAW AMM 57-54-25HG2-695, 1-7-27.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR SWIA2026031175626Flap Track · out of limitsLEFT WING INBD AFT FLAP TRACK NR 6 HAS THICKNESS REDUCTION OF .030. THIS IS OUT OF ALLOWABLE LIMITS OF SRM 57-53-03/AD01 TABLE 101. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED LT WING INBD AFT FLAP TRACK NR 6 IAW AMM 27-51-08.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR SWIA2026040275625Flap Track · out of limitsLEFT WING INBD AFT FLAP TRACK NR 5 HAS THICKNESS REDUCTION OF .040". THIS IS OUT OF ALLOWABLE LIMITS OF SRM 57-53-03/AD01 TABLE 101. ASSET TC2-7153 DUE 9-17-26. REMOVED AND REPLACED LT WING INBD AFT FLAP TRACK NR 5 IAW AMM 27-51-08. OPS CHECKED.Mar 11, 2026 · N139SY · Emb ERJ170200LRSDR FDEA202603110351Rib · crackedRH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386775 P1 TO REPAIR RT CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIMar 11, 2026 · N688FE · Airbus A300F4605RSDR FDEA202603110350Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386774 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIBMar 11, 2026 · N688FE · Airbus A300F4605RSDR SWAA2026040777999Attach Angle · crackedLEFT WING DEFLECTION RIB INTERCOSTAL OTBD ATTACH ANGLE CRACKED.<[01] REMOVED ATTACH ANGLE PER SRM 51-40-02;[02] DRILLED NEW ATTACH ANGLE PER SRM 51-40-05 AND INSTALLED NEW RIB PER SRM 41-40-02;[03] DRILLED NEW ATTACH ANGLE PER SRM 51-40-05 AND INSTALLED NEW ANMar 10, 2026 · N8530W · Boeing 7378H4SDR IPXA2026031675369Skin · crackedCRACK - SKIN , LOWER FACE OF L/H WING T/E INBD MID FLAP T/E UPPER FIXED PNL , WBL 438. (REPAIR) I.A.W AMM 27-51-03-404-008 REV.115 INSTALL THE PIN BETWEEN NO.5 SWING ARM AND SPINDLE.Mar 8, 2026 · N574UP · Boeing 74744AFSDR IPXA2026031675363Skin · crackedRIGHT WING INBOARD MID FLAP , T/E LOWER SURFACE CRACK. (REPAIR) 3 BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.Mar 8, 2026 · N574UP · Boeing 74744AFSDR CALA2026030914447Screw · missingFLAP TRACK FAIRING LEFT WING MISSING SCREW INSTALLED NEW SCREW ON LEFT WING NO 3 INBD FLAP FAIRING REF IPC 27-51-18-01.Mar 8, 2026 · N38479 · Boeing 737924ERSDR IPXA2026040554363Fairing · puncturedPUNCTURE IN FWD OTBD AREA OF #1 MOVEABLE FLAP TRACK FAIRING. I.A.W. 747-400F SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV.106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE PUNCTURE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA (DIA:1", 2.5" FROM THE PAMar 6, 2026 · N575UP · Boeing 74744AFSDR FDEA202603060324Skin · dentedDENT ON LOWER SURFACE OF LT OTBD FLAP, LOCATED AT 39.5" FROM INBOARD EDGE AND 2.5" FROM AFT EDGE. LT OTBD FLAP LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, FIG 201, SHEET 6, & SRM 51-70-17-0G, PAR 4A, FIG 10, SHEET 1, REV 94.Mar 6, 2026 · N130FE · Boeing 7673S2FSDR FDEA202603060318Skin · puncturedLH WING INBD T/E AFT FLAP LOWER SKIN FOUND 1EA PUNCTURE BTW IFS179.75 & IFS257.75. REPAIRED LH WING INBD TRAILING EDGE AFT FLAP LOWER SKIN 1EA PUNCTURE BTW IFS179.75 AND IFS257.75 PER SRM 57-53-01-2R REPAIR 1 & B767 SRM 51-70-10-2R REPAIR 2 & EA H-5750-T038Mar 6, 2026 · N102FE · Boeing 7673S2FSDR AALA202603126437Rib · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP OUTBOARD DEFLECTION CONTROL RIB WORN. REPLACED RIB PER AARD 51-00-05 AND EA 372815.Mar 4, 2026 · N983AN · Boeing 737823SDR SWIA2026030376885Skin · dentedLOWER SKIN OF RT INBD FLAP HAS MULTIPLE SMALL DENTS & ROCK DAMAGE. REPAIRED THE SKIN OF THE RT INBD FLAP IAW REO 601R-57-52-2555 REV--. APPLIED SURFACE FINISH IAW SRM 51-25-01, & SRM 51-26-00.Mar 3, 2026 · N207PS · Cndair CL6002B19SDR DALA2026030501526Hinge Fitting · corrodedCORROSION ON LOWER OTBD ATTACH POINT STUD AND MIDDLE FLAP HINGE FITTING STA Y XRS 267 APPROX AT RT WING. REPLACED PER SERVICEABLE CENTER WING FLAP HINGE FITTING RH PER B717-200 AMM 57-55-25. (1476470)Mar 3, 2026 · N964AT · Boeing 717200SDR SWIA2026030277336Skin · damagedREPAIR RT INBOARD FLAP LOWER SKIN DUE TO MULTIPLE DISCREPANCIES. C-CHECK RO 9302026RH IB FLAP LOWER SKIN HAS BEEN REPAIRED REF SRM 57-52-01-201-005-A01 REFER TO CONTINUATION SHEET FOR DETAILS COMPLIED WITH TASK CARD 51-900-1002-SKYMar 2, 2026 · N611SK · Cndair CL6002C10SDR DALA2026031901901Strut · corrodedCORROSION ON INTERCONNECTING STRUTS LH. REMOVED INTERCONNECTING STRUTS L/H P/N:D5757032201100, S/N: 02370 ON UNSERVICEABLE CONDITION AS PER FAM AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). JOB IN PROGRESS. REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320Mar 2, 2026 · N365NB · Airbus A319114SDR FDEA202603010299Rib · crackedRIGHT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB25 AND 26 BETWEEN STGR2Mar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010298Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB18 BETWEEN STGR2.7 AND REAR SPAR, RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB18 AND 19 BETWEEN STGR2.7 Mar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010297Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN S2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 & REAR SPAR, RIB13 BETWEEN S2.6 AND S2.8 COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 7EA CRACKS OF RIB11Mar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010296Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND FRONT SPAR COMPLIED WITH EA 6-5750-T0386614 INSPECTED THE LH WING CENTER FLAP RIB UPR FLANGE OF RIB15 BETWEEN STGR2.5 AND FRONT SPAR AND REPAIRED THE BOTTOM SKIN POCKET CUT OUTMar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010295Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 6EA CRACKS AT RIB16 BETWEEN STGR2.7 AND STGR2.8, RIB17 BETWEEN STGR2.8 AND REAR SPAR, RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6Mar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010294Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 5EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.7 AND REAR SPAR, RIB27 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGES 5EA CRMar 1, 2026 · N746FD · Airbus A300B4622RSDR FDEA202603010293Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK OF RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH Mar 1, 2026 · N746FD · Airbus A300B4622RSDR DALA2026030201432Carriage · crackedLH WING #2 FLAP TRACK CARRIAGE I/B BRIDGE CRACK. REMOVED AND REPLACED PER A330 AMM 27-54-78. (1472360)Feb 28, 2026 · N816NW · Airbus A330323SDR DALA2026030201431Carriage · crackedSHIP 3316 LH WING #4 FLAP TRACK CARRIAGE ASSY O/B BRIDGE CRACK. CORRECTIVE ACTION: REMOVED AND REPLACED LH WING #4 FLAP TRACK CARRIAGE ASSY O/B BRIDGE AS PER A330 AMM 27-54-78. (1472356)Feb 28, 2026 · N816NW · Airbus A330323SDR DALA2026030201420Hinge Fitting · corrodedCORROSION WAS FOUND ON INB AND OUT HOLES (4EAS) UPPER AND LOWER HINGE FLAP ALSO ON SETTLEMENT AREA. REPAIRED PRI 631842-14 REV 2 AND ER/A 631842-14. (1469307)Feb 26, 2026 · N952AT · Boeing 717200SDR SWAA2026022674574Wedge · delaminatedLEFT WING INBOARD FLAP WEDGE APPEARS TO BE DELAMINATED. VERIFIED NEW REPLACEMENT WEDGE FIT CHECK GOOD IAW SRM 51-40-05. VERIFIED NEW REPLACEMENT WEDGE FIT. INSTALLED NEW FLAP WEDGE IAW AMM 27-51-12.Feb 26, 2026 · N273WN · Boeing 7377H4SDR FDEA202602260282Skin · dentedHAIL STRIKE (12 EA'S) ON OUTBOARD FLAP TOP SKIN BETWEEN OTEF STA 25 & OTEF STA 222.5, LH WING. OUTBOARD FLAP TOP SKIN BETWEEN OTEF 25 & OTEF STA 222.5 LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 51-70-10-2R REPAIR 4 FIG 201 SHEET 1 REV 94 DEC15-2Feb 26, 2026 · N135FE · Boeing 7673S2FSDR FDEA202602250278Skin · chafedRH WING INNER FLAP UPR SKIN FOUND CHAFE MARKS BETWEEN RIB16 AND RIB17. REPAIRED THE DAMAGED UPR SKIN IN RH WING INNER FLAP BETWEEN RIB16 AND RIB17 PER SRM57-50-00-201 PARA.4E. TRACKING EA 6-5750-T0386734 RAISED AND ACCOMPLISHED. REPAIR. MAJOR REPAIR IAW GMMFeb 25, 2026 · N746FD · Airbus A300B4605RSDR SWAA2026022673942Skin · delaminatedLEFT WING INBOARD FLAP APPEARS TO BE DELAMINATED. C/W EA 26-157-00528Feb 24, 2026 · N273WN · Boeing 7377H4SDR FDEA202602240273Skin · delaminatedDELAMINATION IN LEADING EDGE AT 69" INNER END ON OUTBOARD FLAP, RH WING LEADING EDGE AT 69 " INNER END ON OUTBOARD FLAP, RH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-0G PAR 4 A FIGURE 10 SHEET 1, REV 93.Feb 24, 2026 · N135FE · Boeing 7673S2FSDR FDEA202602240272Skin · delaminatedDELAMINATION IN LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FLAP, RH WING LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FLAP RH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-Feb 24, 2026 · N135FE · Boeing 7673S2FSDR FDEA202602240271Skin · delaminatedDELAMINATION ON LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE, LEFT WING LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE LEFT WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-06 PAR 4 A FIGURFeb 24, 2026 · N135FE · Boeing 7673S2FSDR AALA202602279204Trunnion · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND INBOARD FLAP TRUNNION SHOWS SIGNS OF WEAR ON THE LOWER AFT SIDE AND UPPER FRONT SIDE. REPLACED TRUNNION PER CMM 57-52-23.Feb 23, 2026 · N182UW · Airbus A321211SDR CALA2026022314025Panel · crackedFLAP FAIRING PANEL 571FB, HAS A CRACK ON THE FWD EDGE BAND, INBD LOWER SIDE. CRACK MEASURES 1"1/4 FRO, THE LEADING EDGE OF THE FAIRING TRAVEL AFT. CRACK IS OUTSIDE OF SRM 57-53-70/1A01 LIMITS. TRM ECRA 5753-02392 APPLIED TO DAMAGE. PART 1 OF ECRA CARRIED OUT Feb 22, 2026 · N668UA · Boeing 767322SDR SWIA2026022175743Skin · gougedLEFT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLER HAS GAUGES. REPAIRED LT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLE IAW REO 601R-57-52-2545, REV-. CHECKS GOOD.Feb 21, 2026 · N952SW · Cndair CL6002B19SDR IPXA2026040136279Skin · crackedL/H WING-I/B FLAP I/B TOP SKIN APPROX 6"FROM I/B END AND 3' FROM T/E HAS DENT IN SKIN AND RUB STRIP (RUB STRIP CRACKED AT DENT) NOT IN MAPPING-109-210-VWV VERIFIED L/H I/B FLAP WAS REPLACED ON T/C T3F18E008AETA. NO FURTHER ACTION REQ.Feb 21, 2026 · N135UP · Airbus A300F4622RSDR SWIA2026022076064Guide · chafedLH WING TE AT FSL168.63, THE ROLLER GUIDE FITTING FOR LH FLAP ROLLER CAM FITTING IS CHAFED (WEAR SIGN) REMOVE AND REPLACED WITH NEW ROLLER GUIDE FITTING. REF: CRJ-900-SRM-51-42-06-001-001-A01. COMPLIED WITH ALL STEPS ON TASK CARD 51-900-1002-SKY. SEE CONTINUFeb 20, 2026 · N899SK · Cndair CL6002D24SDR FDEA202602200247Skin · dentedLH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER B777 SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 51.0 AND EAFeb 20, 2026 · N889FD · Boeing 777FS2SDR SWIA2026021977445Skin · dentedLEFT INBD FLAP HAS DENT ON LOWER EXTERNAL SKIN AT APPROX WS 70. REPAIRED LT INBD FLAP ON LOWER EXTERNAL SKIN AT APPROX WS70, IAW SRM 57-52-01-201-005-A01, 57-52-01-995-803.Feb 19, 2026 · N611SK · Cndair CL6002C10SDR DALA2026022301273Skin · delaminatedSHIP 180 RH WING I/B T/E AFT FLAP O/B CORNER FOUND DELAMINATION. CORRECTIVE ACTION: REPAIRED RH WING I/B T/E AFT FLAP O/B CORNER DELAMINATION AS PER B767-300 SRM 57-53-01-1A-1, SRM 57-53-01-2R-1 AND SRM 51-70-10 (1457697)Feb 19, 2026 · N180DN · Boeing 767332SDR SWAA2026022072236Skin · debondedLEFT OTBD AFT FLAP HAS AREA OF TRAILING EDGE DISBOND. INBD END. 3 IN. IN LENGTH. REMOVED AND REPLACED L/H O/B AFT FLAP REF AMM 27-51-22. UP TO BUT NOT INCLUDING STEP G. (FLAP RIGGING AND ADJUSTMENT). INSPECTED IAW AMM 27-51-22-401-NG.Feb 19, 2026 · N7835A · Boeing 737752SDR SWAA2026022072016Skin · debondedLEFT WING OTBD TRAILING EDGE FLAP HAS DISBONDING ON UPPER SKIN INBD CORNER 12 AT LONGEST AND 8 AT WIDEST HAVING DISBONDING FROM ZONE 1 TO 5. MORE THAN 2 DIAMETER IN ZONE. SPLIT T/E 1 1/2<. REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22.Feb 19, 2026 · N8302F · Boeing 7378H4SDR VNAA20260508014Rib · damagedRIGHT WING I/B FLAP L/E RIB (P/N CC670-14102-2) HAS 1EA ELONGATED NUTPLATE HOLE ON THE O/B SIDE. REPAIRED IAW REO 670-57-52-644 REV-A DATED 2026-02-16Feb 18, 2026 · N512AE · Cndair CL6002C10SDR IPXA2026022561984Skin · crackedMAJOR REPAIR. LEFT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 26. VERIFIED MAJOR REPAIR WORK HAS BEEN ACCOMPLISHED IAW A300-600 SRM 51-40-21. RII REQUIREMENTS COMPLETED IAW UPS GMM 04-02 STEP 1 MAJOR REPAIRSFeb 17, 2026 · N135UP · Airbus A300F4622RSDR IPXA2026032262044Rib · crackedMAJOR REPAIR. RIGHT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 12. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96704-REQ1 AND VT-MAE EA 300-5753-27-A4370, REV. -.Feb 17, 2026 · N135UP · Airbus A300F4622R
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