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 IPXA2025120741156Skin · puncturedMAJOR REPAIR, DURING CLEAN UP , PUNCTURED INNER FLAP LOWER SKIN INFO SENT TO ENGINEERING ALL STEPS OF EO-95467-REQ4 COMPLETED. THIS IS A PERMANENT REPAIR. THIS DEFERRAL IS NOW CLOSED.Oct 18, 2025 · N138UP · Airbus A300F4622RSDR DALA2026041602431Skin · damagedCOMPOSITE PANEL ON RIGHT CORNER OF OUTBOARD FLAP ON LEFT WING FLEW OFF ON TAKEOFF. R/R LH OTBD FLAP AFT PER B737 AMM 27-51. OPS CHK GOOD. (LOG 7883440 - AIRCRAFT WAS GROUNDED).Oct 17, 2025 · N958DZ · Boeing 7379GPERSDR CALA2025102710552Skin · delaminatedLEFT WING OTBD AFT FLAP DISBOND AREA L=9INCH, W=7INCH AT LOWER SKIN TRAILING EDGE OF THE O/B AFT FLAP WEDGE. CLEANED, PREPPED, PERFORMED THE PERMANENT REPAIR AND RESTORED PAINT ON LT WING OTBD AFT FLAP OWER SKIN. ALL WORK DONE IAW SRM 57-53-01-1A-4, SRM 57-5Oct 17, 2025 · N38479 · Boeing 737924ERSDR VNAA20251015079Beam · chafedLEFT IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING Oct 17, 2025 · N501BG · Cndair CL6002C10SDR VNAA20251015067Slat Track · chafedRIGHT SLAT TRACK 3-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1961 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10SDR FDEA202510162035Skin · damagedBULGE ON PREVIOUS REPAIR, LOWER SURFACE OF OUTBOARD FLAP, AT 20" TO OUTBOARD EDGE AND 4" TO LEADING EDGE. RH WING LOWER SURFACE OF OUTBOARD FLAP AT 20" TO OUTBOARD EDGE AND 4" TO LEADING EDGE WAS REPAIRED I.A.W. SRM 57-53-01-2R FIGURE 201 SHEET 6 TABLE II Oct 16, 2025 · N183FE · Boeing 7673S2FSDR FDEA202510162033Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 99.5 INCHES TO IB EDGE AND 11.5 INCHES TO AFT EDGE. REPAIRED RT WING OTBD FLAP LWR SURFACE DENT AT OTEF STA 99.5 IAW SRM 57-53-01-2R-2, & SRM 51-70-04-2R-1, REV 51.0 AND EA:G-5750-T0385311 P1. MAJOR REPAIR PER GMM 6Oct 16, 2025 · N882FD · Boeing 777F28SDR VNAA20251015059Vane · gougedRIGHT OUTBOARD FLAP VANE LEADING EDGE HAS AN APPROXIMATELY 4" LONG GOUGE FROM CONTACT WITH BUCKTAIL ON TRAILING EDGE OF WING AT WS 231.23. COMPLIED WITH REO 670-57-53-395 REV --.Oct 16, 2025 · N501BG · Cndair CL6002C10SDR VNAA20251015053Slat Track · chafedLEFT SLAT TRACK 1-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 1-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1938 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10SDR VNAA20251015044Beam · chafedRH IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING TROct 16, 2025 · N501BG · Cndair CL6002C10SDR SWIA2026022575332Skin · dentedRH INBOARD FLAP LOWER SKIN HAS 4 DENTS LOCATED 14" FROM INBD EDGE AND 4" FROM TRAILING EDGE, 32" FROM INBD EDGE AND 2" FROM TRAILING EDGE, 20.5" FROM INBD EDGE AND 24" FROM TRAILING EDGE, 26" FROM INBD EDGE AND 24" FROM TRAILING EDGE. (C-CHECK RO 02/22/2026)Oct 15, 2025 · N613SK · Cndair CL6002C10SDR SWIA2026022575322Skin · dentedLH INBOARD FLAP LOWER SKIN HAS 5 DENTS LOCATED 19" FROM INBD EDGE AND 2.5" FROM TRAILING EDGE, 16" FROM INBD EDGE AND 13" FROM TRAILING EDGE, 18" FROM INBD AND 15" FROM TRAILING EDGE, 17.5" FROM INBD EDGE AND 16.5" FROM TRAILING EDGE, 19" FROM INBD EDGE AND 24Oct 15, 2025 · N613SK · Cndair CL6002C10SDR CALA2025101710225Panel · dentedRIGHT WING INBOARD FLAP PANEL 653BB DENTED. REMOVED AND INSTALLED RT INBD FLAP PANEL 653BB IAW SRM 51-40-02-0G-0, DWG 654A0004-832 REV A.Oct 15, 2025 · N68805 · Boeing 737924ERSDR DALA2025101507527Roller · bindingRIGHT WING OTBD FLAP INBD GUIDE ROLLER BINDING WHEN ROLLING WITH PRESSURE ON IT. REPLACED OTBD FLAP CRUISE ROLLER IAW CMM 57-53-21 AND ADJUSTED CRUISE ROLLER IAW AMM SUBTASK 27-54- 62-820-052-C. (1252270)Oct 14, 2025 · N324NB · Airbus A319114SDR DALA2025101507526Roller · bindingLEFT WING OTBD FLAP INBD GUIDE ROLLER BINDING WHEN PRESSURE APPLIED AND TRYING TO ROLL. REPLACED OTBD FLAP CRUISE ROLLER IAW CMM 57-53-21 AND ADJUSTED CRUISE ROLLER IAW AMM SUBTASK 27-54- 62-820-052-C. (1250793)Oct 14, 2025 · N324NB · Airbus A319114SDR VNAA20251014015Vane · chafedDISCREPANCY: LH I/B FLAP VANE LEADING EDGE IS CHAFED AT WS 88, APPROXIMATELY 1" LONG AND .008" DEEP. CORRECTIVE ACTION: LOCATED, DRILLED, DEBURRED AND INSTALLED INBD FLAP VANE CAP PN: CC670-14022-1 IAW CRJ700 SRM 51-40-11-001-001-A01.Oct 14, 2025 · N501BG · Cndair CL6002C10SDR SWI2026F00026Vane · chafedCHAFING ON RT INBD FLAP OTBD FLAP VANE ACTUATOR BODY. REPAIRED RH INBD FLAP OTBD FLAP VANE ACTUATOR BODY IAW REO 601R-57-52-2533 REV.-.Oct 13, 2025 · N454SW · Cndair CL6002B19SDR SWIA20260105013Vane · chafedLEFT INBD FLAP VANE LEADING EDGE IS CHAFED IN MULTIPLE LOCATIONS. LT INBOARD FLAP VANE LEADING EDGE 2 EA. AREAS BLENDED AND REPAIRED TO BE WITHIN LIMITS. REF REO 601R-57-52-004, REV -D, 2012-12-19. 1 EA. BLEND ON SKIN PANEL 601R14303-51 FOUND TO BE OUT OF LIMIOct 13, 2025 · N454SW · Cndair CL6002B19SDR SWAA2025102124073Skin · delaminatedRT OB AFT FLAP IB END UPPER SURFACE HAS SPOT DELAMINATED. REMOVED AND REPLACED R/H OUTBD AFT FLAP IAW AMM 27-51-22-400-801 - AMM 27-51-22-400-801 -ADJUSTMENT AND OPS CK GOOD.Oct 13, 2025 · N8617E · Boeing 7378H4SDR AALA202510217746Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: PREVIOUS REPAIR COMPLETED (FINGER DOUBLER AND FILLER PLATE) ON OUTBOARD FLAP ACCESS DOOR CUTOUT AT TRACK NO 4 AT LEVEL RIB 15 RH WING, L=5.745IN X W=3.800. MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION PRIOR TO FLIGHT AT O/B FLAOct 12, 2025 · N767UW · Airbus A319112SDR IPXA2025111394837Rib · crackedMAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 15. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95517-REQ1 AND VT-MAE EA 300-5750-27-A4185, REV -.Oct 10, 2025 · N129UP · Airbus A300F4622RSDR IPXA2025103193086Skin · dentedRIGHT WING INBD FLAP HAS A DENT ON OTBD TOP SKIN. ACCOMPLISHED IAW EO-95578-REQ1 REV. 2 AND VT-MAE EA 300-5751-27-A4197, REV -.Oct 10, 2025 · N129UP · Airbus A300F4622RSDR CALA2025102110324Skin · delaminatedRH WING O/B AFT FLAP UPPER SKIN WITH TWO DISBOND SIGNAL NOTED, AREA 1 L=1 INCH W=0.750 INCH, AREA 2 L=1.300 INCH W=1 INCH AT FW D EDGE OF I/B END AFT FLAP WEDGE (REF AAR NR 1000056354) FOR SFR ENTRY ONLY. CLEANED,PREPPED AND REPLACED PREVIOUS REPAIR ON RH WIOct 9, 2025 · N68805 · Boeing 737924ERSDR FDEA202510091929Rib · crackedNDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB25/STGR2.8 - REAR SPAR,RIB26/STGR2.6-2.7,RIB26/STGR2.7-2.8,RIB27/STGR2.7-2.8,RIB27/STGR2.8-REAR SPAR TOTAL OF 5 CRACKS FOUND. REPAIRED THE CRACKED RIB UPR FLANGE AT LH WING CENTER FLAP RIB25/STGR2.8 - REAOct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091928Rib · crackedNDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB18/STGR2.8 - REAR SPAR 1EA CRACK WAS FOUND. COMPLIED WITH EA: 6-5750-T0319244 P2, TITLE: WINGS - FLIGHT SURFACES - LHS CENTER FLAP RIB 18 CRACKED AT UPPER FLANGE BETWEEN STGR2.8 AND REAR SPAR. REPAIRED THEOct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091927Rib · crackedNDT INSP - LT WING CENTER FLAP INNER STRUCTURE 1EA CRACK WAS FOUND RIB11/STGR2.7 - 2.8 COMPLIED WITH EA: 6-5750-T0337526 P2. TITLE: WINGS - FLIGHT SURFACES - LHW, CENTER FLAP, SKIN AND RIB REPAIRS PER SRM - RSC TRACKING. REPAIRED THE LH WING CENTER FLAP INNEROct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091926Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB17 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB17 BETWEEN STGR2.8 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-Oct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091925Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB11 & RIB12 & RIB13 & RIB15 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB11 & RIB12 & RIB15 BETWEEN STGR2.8 AND REAR SPAR,RIB13 BETWEEN STGR2Oct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091924Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 4EA CRACK AT RIB19 BETWEENSTGR2.6 AND REAR SPAR,RIB20 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RT WING CENTER FLAP RIB19 BETWEEN STGR2.6 AND REAR SPAR,RIB20 BETWEEN STGR2.8 AND Oct 9, 2025 · N728FD · Airbus A300B4622RSDR FDEA202510091923Rib · crackedNDT INSP - RT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACK AT RIB26 BETWEEN STGR2.6 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB26 BETWEEN STGR2.6 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Oct 9, 2025 · N728FD · Airbus A300B4622RSDR IPXA2025102434573Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. ONE CRACK NOTED AT RIB 17. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.Oct 7, 2025 · N133UP · Airbus A300F4622RSDR IPXA2025102434841Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. TWO CRACKS NOTED AT RIB 27. ACCOMPLISH PERMANENT REPAIR IAW EA 300-5750-27-A4183, REV. -.Oct 7, 2025 · N133UP · Airbus A300F4622RSDR IPXA2025102434554Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 11. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.Oct 7, 2025 · N133UP · Airbus A300F4622RSDR IPXA2025102434561Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 18. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.Oct 7, 2025 · N133UP · Airbus A300F4622RSDR IPXA2025102434775Rib · crackedFAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 26. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWEDOct 7, 2025 · N133UP · Airbus A300F4622RSDR IPXA2025102434779Rib · crackedFAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 25. CIRCLED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWEDOct 7, 2025 · N133UP · Airbus A300F4622RSDR DALA2025101407521Vane · dentedDISBOND OF 2.300IN X 3.100IN. ON DENT LOCATED AT LH AFT MOVABLE FLAP VANE, LOWER SURFACE. REPAIRED PER B717-200 SRM 57-53-01-2R (1239681)Oct 7, 2025 · N946AT · Boeing 717200SDR DALA2025100807338Strut · out of toleranceRIGHT FLAP INTERCONNECT STRUT FAILED RADIAL PLAY DIMENSION CHECK. REPLACED AND ADJUSTED INTERCONNECT STRUT REF A319 AMM 27-51-44. (1239789)Oct 7, 2025 · N324NB · Airbus A319114SDR DALA2025100807356Strut · out of toleranceLT WING FLAP INTERCONNECT STRUT FAILS RADIAL PLAY CHECK. REPLACED AND ADJUSTED INTERCONNECT STRUT REF A319 AMM 27-51-44. (1239803)Oct 7, 2025 · N324NB · Airbus A319114SDR FDEA202510061965Rib · crackedRH WING CENTER FLAP INTERNAL STRUCTURE CRACK AT UPR RIB26 STGR-2.7 TO STGR-2.8. ACCOMPLISHED RIB FLANGE REPAIR AT RIB26, S-2.7~S-2.8 AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, SEQ NO:XXXX, TITLE:WINGS- FLOct 6, 2025 · N690FE · Airbus A300F4605RSDR FDEA202510061964Rib · crackedRH WING CENTER FLAP INTERNAL STUCTURE CRACK AT UPPER RIB26 STGR-2.8 TO REAR SPAR. ACCOMPLISHED RIB FLANGE REPAIR AT RIB26, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, REPAIR CLASSIFIED AS CATOct 6, 2025 · N690FE · Airbus A300F4605RSDR FDEA202510041893Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 2EA CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPAR,AND RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS Oct 4, 2025 · N667FE · Airbus A300F4605RSDR FDEA202510041892Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 4EA CRACKS AT RIB26 BETWEEN STGR2.7 AND REAR SPAR, AND RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 16Oct 4, 2025 · N667FE · Airbus A300F4605RSDR FDEA202510041891Rib · crackedLEFT WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB16 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 16, 17, 19, 26 AND 27 AT STR. 2.7/2.8. REPAIROct 4, 2025 · N667FE · Airbus A300F4605RSDR FDEA202510041890Rib · crackedLEFT WING CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 11 BETWEEN S2.7 AND S2.8 COMPLIED WITH EA 6-5750-T0385199 P1. REPAIRED THE LT WING CENTER FLAP RIB UPPER FLANGE CRACK THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 57506818Oct 4, 2025 · N667FE · Airbus A300F4605RSDR FDEA202510041889Rib · crackedRH WING CENTER FLAP RIBS UPR FLANGE FOUND 8EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, AND RIB26 BETWEEN STGR2.6 AND REAR SPAR, AND RIB27 BETWEEN STGR2.6 AND REAR SPAR. REPAIRED THE RT WING CENTER FLAP RIBS UPR FLANGE 8EA CRACKS AT RIB25 BETWEEN STGR2Oct 4, 2025 · N667FE · Airbus A300F4605RSDR FDEA202510041888Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB12 BETWEEN STGR2.7 AND STGR2.8 REPAIRED THE RT WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB12 BETWEEN STGR2.7 AND STGR2.8. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 5750681Oct 4, 2025 · N667FE · Airbus A300F4605RSDR SWAA2025102721042Fairing · crackedNR 3 FLAP TRACK FAIRING HAS IMPACT DAMAGE; A CRACK AND IS DELAMINATED ON THE INSIDE WHERE THE ATTACHMENT BEAM MAKES CONTACT. REMOVED ATTACH BEAM AND ADJUSTMENT LINK ASSEMBLY FROM DAMAGED #3 FLAP TRACK FAIRING AND INSTALLED ON REPLACEMENT NR 3 FLAP TRACK FAIRIOct 3, 2025 · N8504G · Boeing 7378H4SDR IPXA2025100965035Skin · gougedGOUGE - SKIN, RT WING OUTBOARD AFT FLAP AT WS900 - WS920. REPAIRED GOUGE DAMAGE RT WING OUTBD T/E FLAP AFT FLAP UPPER PANEL BETWEEN WBL 747.7 AND WBL 822.0 IAW EI F 2025A57M-2243, REV 2 AND EO-95508-REQ1 REV 1.Oct 3, 2025 · N573UP · Boeing 74744AFSDR SWAA2025102221083Wedge · delaminatedLEFT INBD AFT FLAP WEDGE IS DELAMINATED. INSTALLED NEW NEW WEDGE ASSY INBD MAIND FLAP IAW 51-40-02-0G AND DWG 113A2100 REV A.Oct 3, 2025 · N8615E · Boeing 7378H4
Back to JASC 5753