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 IPXA2026042329452Bolt · wornRIGHT WING OUTBOARD MID FLAP, T/E UPPER SKIN, BOLT WORN 1 EA. REMOVE THE WORN MATERIALS AND CLEAN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. AND PSDL 65B08533 SHEET DL, REV.A. INSTALL THE RH WING OUTBD MID FLAP SUPPORT STRUT.Apr 16, 2026 · N575UP · Boeing 74744AFSDR LR7A2026041603817Flap Track · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LH OUTBOARD WING FLAP TRACK FITTING CRACKED AT OWFS241. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001371812.Apr 16, 2026 · N405LC · Lkheed 382GSDR LR7A2026041603816Skin · wornDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LH OUTER WING FLAP UPPER TRAILING EDGE SKIN WITH WORN COUNTERSINK RIVET HOLES / REPAIRED IAW SMP583 SRM, FIGURE 51-140-12. NR# 1001371794Apr 16, 2026 · N405LC · Lkheed 382GSDR IPXA2026041828803Skin · damagedL/H WING T/E OUTBD FLAP INBD SIDE AFT CAP , WBL 355. .I.A.W AMM 20-11-00-910-802 REV147 INSTALL L/H OUTBD FLAP INBD SIDE P-SEAL & RETAINER UPPER AND LOWER.Apr 16, 2026 · N332UP · Boeing 76734AFSDR SWAA2026041789932Fairing · crackedFOUND #6 FLAP TRACK MID-CANOE FAIRING CRACKED AT 6OCLOCK POSITION AFT SIDE<[01] C/W EA 26-157-01040Apr 16, 2026 · N448WN · Boeing 7377H4SDR DALA2026041602421Fitting · damagedNICK AND CHAFING ON LOWER SURFACE OF THE NEWLY REPLACED LTW RIB 6 FITTING ASSY. REPAIRED PER ERA 633297-14 AD REV ORIGINAL. (1547054) AIRCRAFT WAS GROUNDED.Apr 16, 2026 · N816NW · Airbus A330323SDR DALA2026041602419Bushing · damagedNOTCH AND KNIFE EDGE DAMAGE ON BUSHING OF THE NEWLY REPLACED LHW RIB 6 FITTING ASSY. REPAIRED PER ERA 633297-14 AD REV ORIGINAL. (1546950) AIRCRAFT WAS GROUNDED.Apr 16, 2026 · N816NW · Airbus A330323SDR FDEA202604160448Skin · delaminatedDELAMINATION IN LEADING EDGE AT 9" OF INBOARD END ON OUTBOARD FLAP LH WING LH WING, OUTBOARD FLAP AT LEADING EDGE ON 9" OF INB. EDGE WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R TABLE I, 51-70-17-0G PARAGRAPH 4A FIGURE 10 AND AMM 51-21-10-7 REV. 94 DEC 15,2025Apr 16, 2026 · N281FE · Boeing 767300SDR 2026FA0000358Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N988BE · Cessna 172SSDR 2026FA0000355Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N437SP · Cessna 172SSDR 2026FA0000352Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD RH INBOARD FLAP TRACKApr 14, 2026 · N211AV · Cessna 172NSDR FDEA202604140571Skin · crackedLH WING CENTER FLAP UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WINGS - FLIGHT SURFACEApr 14, 2026 · N669FE · Airbus A300F4605RSDR 2026FA0000339Stiffener · shearedFLAP TRACK SRIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD RH INBOARD FLAP TRACKApr 14, 2026 · N211AV · Cessna 172NSDR FDEA202604140438Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB27 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 REPAIRED THE LH WING CENTER FLAP RIB27 UPPER CRACKED FLANGE BETWEEN REAR SPAR AND STGR2.8. CAT A REPAIR. MAJOR REPAIR IAW GMM 6Apr 14, 2026 · N669FE · Airbus A300F4605RSDR SWIA2026041475910Roller · damagedL/H FLAP GUIDE ROLLERS ARE DAMAGED OR SEIZED AT I/B TO O/B FLAPS. REMOVED AND REPLACED LH GUIDE ROLLER I/B PER ERJ175 AMM 27-51-11Apr 14, 2026 · N85363 · Emb ERJ170200LLSDR SWIA2026041475909Roller · damagedR/H FLAP GUIDE ROLLERS ARE DAMAGED OR SEIZED AT I/B TO O/B SPLIT. MARKED (C-CHECK RO 04/26/2026)REMOVED AND REPLACED RH FLAP GUIDE ROLLER I/B PER ERJ175 AMM 27-51-11Apr 14, 2026 · N85363 · Emb ERJ170200LLSDR IPXA2026042187945Fairing · damagedENLARGED HOLE NR 4 AFT FAIRING HOLE .IAW AMM 51-24-11-477-083 REV.116, REPAINT PEEL OFF AREA. CHECK NORMAL.Apr 14, 2026 · N575UP · Boeing 74744AFSDR FDEA202604140445Skin · delaminatedDELAMINATION ON L EDGE INB MAIN FLAP AT 20" FROM OUTB EDGE. RH WING L/E INBD MAIN FLAP AT 20" FROM OUTBD EDGE RH WING WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 SHEET 5 TABLE 1 AND SRM 51-70-03-0G PAR 5A FIG 5 REV 94 DEC 15/2025Apr 14, 2026 · N281FE · Boeing 767300SDR FDEA202604140444Skin · dentedDENT IN LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FAIRING FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP. LH WING WAS REPAIRED IAW B767 SRM 57-53-01Apr 14, 2026 · N281FE · Boeing 767300SDR FDEA202604140443Skin · dentedDENT IN LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING WAS REPAIRED IAW B767 SRM 57-53-01Apr 14, 2026 · N281FE · Boeing 767300SDR FDEA202604140442Skin · dentedDENT IN LOWER SURFACE ON MAIN FLAP AT 35'' OF OUTBOARD FAIRING FLAP AND 14.25" OF TRAILING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON MAIN FLAP AT 35" ON OUTBOARD FAIRING FLAP AND 14.2" OF TRAILING EDGE ON INBOARD FLAP LH WING WAS REPAIRED IAW SRM 57-5Apr 14, 2026 · N281FE · Boeing 767300SDR 2026FA0000268Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD TRACK OF THE RH FLAPApr 14, 2026 · N211AV · Cessna 172PSDR IPXA2026050481474Skin · gougedRH WING INNER FLAP UPPER SURFACE I/B AFT AREA GOUGED. REMOVED GAUGED ON RT WING INNER FLAP UPPER SURFACE I/B AFT AREA IAW SRM 51-73-10.CK LIMITS. ORIG. MAT 0.031". MAT.LOSS 0.001".MAT.REMAINING.0.030".FOUND TO BE IN LIMITS IAW SRM 57-50-00.TR99333.OK TO RESTOApr 13, 2026 · N141UP · Airbus A300F4622RSDR SWAA2026051288539Tail Cone · crackedNUMBER 3 FLAP TRACK FAIRING TAILCONE 542EB TIP IS CRACKED. DUE TO THE EXTENT OF DAMAGE; REPLACED #3 FLAP TRACK FAIRING TAILCONE 542EB IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 27-51-18-01 ITEM 430.Apr 12, 2026 · N8639B · Boeing 7378H4SDR FDEA202604120440Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-575Apr 12, 2026 · N669FE · Airbus A300F4605RSDR FDEA202604120439Rib · crackedRH WING CENTER FLAP RIBS UPPER FLANGE FOUND 3EA CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-5750Apr 12, 2026 · N669FE · Airbus A300F4605RSDR SWAA2026041388296Wedge · delaminatedRIGHT WING TRAILING EDGE FLAP DELAMINATION<[01] REMOVED DAMAGED WEDGE PER SRM 51-40-02; LOCATED AND DRILLED NEW WEDGE PER SRM 51-40-06;[02] INSTALLED NEW WEDGE PER SRM 51-40-02;[03] ALL TASKS C/WApr 11, 2026 · N278WN · Boeing 7377H4SDR DALA2026042002464Lug · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF LUG B ORE AT RH WING OUTBOARD FLAP PER ER/A 633290-14. SECTION I LIMITED TO 6 MONTHS FROM 09APR26 ON FTN 1X6843. ER/A T O BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE COMPONENT FROM SERV ICE. ASSOCIATEDApr 10, 2026 · N325NB · Airbus A319114SDR IPXA2026041815210Fairing · dentedDENTED SKIN, LT WING T/E FLAP NR 4 AFT FAIRING EXTERNAL SURFACE LOWER SIDE ADJACENT AFT CONE. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CApr 9, 2026 · N575UP · Boeing 74744AFSDR SWIA2026062676341Hinge Arm · gougedLEFT INBOARD FLAP HINGE ARM WS 80.50 ATTACH LUG GOUGED. REPAIRED GOUGED DAMAGE ON LT INBD FLAP HINGE ARM WS 80.50 ATTACH LUG IAW REO 601R-57-54-392 REV -. COMPLIED WITH SKYCARD 51-900-1003-SKY. MAJOR REPAIR.Apr 8, 2026 · N951SW · Cndair CL6002B19SDR IPXA2026053004969Skin · dentedL/H I/B FLAP, LEADING EDGE, AT 3" LEFT OF RIB 19 WITH 1 DENT. ACCOMPLISHED STEP # 1 OF E.A 300-5752-27-A4487 PRELIMINARY 1. (REMOVED PAINT IAW A300-600 SRM 51-75-20-201). SKIN INSERT (1EA) AND BUTTSTRAP (2EA) WAS INSTALLED IAW A300/600 SRM 51-40-21-001 AND SApr 8, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026053004824Skin · gougedL/H I/B FLAP, LEADING EDGE, AT RIB 16, 2 GOUGES WITH SEPARATION OF 1.5 INCH EACH OTHER. ACCOMPLISHED STEP # 1 OF E.A. 300-5752-27-A4487 PRELIMINARY 1. (BLEND GOUGE DAMAGE MINIMALLY TO REMOVE DAMAGE IAW A300-600 SRM 57-50-00-101 AND SRM 51-73-10. SKIN INSERT ANApr 8, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026051304111Bracket · crackedRIGHT WING CENTER FLAP O/B SIDE BRACKET BROKEN. REMOVED AND REPLACED BRACKET IN RT WING CENTER FLAP O/B SIDE PER SRM 51-40-21 PAR 6.Apr 8, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026040994656Skin · debondedDEBONDED SKIN, INBD AFT EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 289.45. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES HEATED AREA , IAW NDT MANUAL PART, 1 51-01-01 REV:143Apr 8, 2026 · N352UP · Boeing 76734AFSDR IPXA2026041394644Support · crackedRT WING NR 6 FLAP TRACK SUPPORT FAIRING INBD AFT SIDE CRACKED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES, AROUND HEATED AREA IAW NDT MANUAL PART 1 51-01-01, REV 143, NO DEFECT FOUND IAW AMM 20-11-00-910-802, REV.147. INSTALLED THE SEAL & RETAApr 8, 2026 · N352UP · Boeing 76734AFSDR UATA20264105702Skin · corrodedRH INNER FLAP, OUTBOARD PYLON, OUTBOARD SKIN CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WING STATION 2900. REMOVED DAMAGED FITTINGS AND SKIN. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE TO NEW FITTINGApr 8, 2026 · N352CA · Casa C212CCSDR UATA1900410265701Hinge · corrodedRH INBOARD FLAP, OUTBOARD PYLON BOTH FLAP HINGE PLATES CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WING STATION 2900. REMOVED DAMAGED FITTINGS AND SKIN. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE TO NApr 8, 2026 · N352CA · Casa C212CCSDR IPXA2026042978769Skin · crackedMAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV.Apr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026042978737Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 EA CRACK INDICATION NOTED AT RIB 26. PERFORM 4X BOTTOM SKIN POCKET CUT OUTS IN AREA ENCLOSED BY RIB 25- RIB 27, STRINGER 2.2 AND REAR SPAR IN ACCORDANCE WITH A300-600 SRM 57-50-00 PARAGRAPH 4E (FIGURE 205) PRINCIPLApr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026042978763Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 12. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026042978760Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 18. CIRCLED IN RED. ACCOMPLISH THE REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026042978755Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026042978551Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 EA CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. PERFORM 4X BOTTOM SKIN POCKET CUT OUTS IN AREA ENCLOSED BY RIB 25- RIB 27, STRINGER 2.2 AND REAR SPAR IN ACCORDANCE WITH A300-600 SRM 57-50-00 PARAGRAPH 4E (FIGURApr 7, 2026 · N141UP · Airbus A300F4622RSDR IPXA2026041172897Skin · bulgedSKIN, R/H WING T/E OUTBD FLAP INBD LWR. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA IAW NDT MANUAL PART 1 51-01-01 REV 143.Apr 7, 2026 · N313UP · Boeing 76734AFSDR IPXA2026041570432Fairing · brokenNUMBER 5 FLAP TRACK AFT FAIRING, FWD LOWER SKIN BROKEN. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 REMOVE THE BROKEN MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 240 MINUTES WITH MINIMApr 7, 2026 · N610UP · Boeing 7478FSDR DALA2026041402348Hinge Fitting · corrodedCORROSION ON CENTER FLAP HINGE FITTING (OUTB/ LOWER HOLE AND STUD) STA XRS 260.000 APROX AT LH WING. CORRECTIVE ACTION: FITTING WAS REMOVED PER B717-200 AMM 57-55-25 (1532955) (AIRCRAFT GROUNDED)Apr 7, 2026 · N928AT · Boeing 717200SDR N6WA2026040802Skin · dentedRIGHT INBD FLAP LOWER INBD SKIN HAD SEVERAL DENTS. PERFORMED REPAIR OF THE RT INBD FLAP LOWER SKIN IAW EO-C550/700-57MR-006.Apr 6, 2026 · N520GJ · Cndair CL6002C11SDR DALA2026040902271Cover · missingCREW REPORTS FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. FWD TO CDL 27-00-16 "M" PROCEDURE C/W. WILL RQ ONCE EACH FLIGHT DAY REP CHK. DISP APPROVED. PLACARD INSTALLED. OK FOR SVC. "M" PROCEDURES REVERSED. INSATLLED FAIRING PIVOT COVER ON LEFT INBOARD MOVApr 5, 2026 · N348NB · Airbus A319114SDR REXA2026050500480Skin · chafedCHAFING ON UPPER SKIN ON FLAP-VANE BTW WS 95 TO WS 98 AT LH WING. CHAFING ON UPPER SKIN ON FLAP-VANE BTW WS 95 TO WS 98 AT LH WING WAS REPAIRED PER EA NO: CRJ957-22003 REV IRApr 3, 2026 · N279PQ · Cndair CL6002D24SDR DALA2026040802226Vane · cracked7.0IN FROM T.E AND 20IN FROM O.B OF 1.5IN LENGTH X2.0IN WIDTH OF THE AFT MOVABLE FLAP VANE. AFT MOVABLE FLAP VANE IT IS OUT OF BOUNDS BECAUSE IT DOES NOT COMPLY WITH THE DISTANCE BETWEEN DAMAGE PER B717-200 SRM 57-53-01 (1527254) (AIRCRAFT GROUNDED)Apr 3, 2026 · N939AT · Boeing 717200
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