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 SWAA2026022465349Retainer · crackedRIGHT WING AFT BULB SEAL RETAINER IS CRACKED AT THE TRANSVERSE WEB. REMOVED AND REPLACED THE AFT BULB SEAL RETAINER IAW SRM 51-40-02-OG-O.Jan 28, 2026 · N922WN · Boeing 7377H4SDR JR2R20260128175Rib · corrodedR/H WING I/B MAIN FLAP TORQUE TUBE SUPPORT STRUCTURE RIB 1 IS CORRODED IN MULTIPLE SPOTS. PERFORMED TEMPORARY REPAIR IAW ETD2026-170-000513.Jan 28, 2026 · N87339 · Emb ERJ170200LRSDR DALA2026020200756Hinge Fitting · wornTHE LEFT WING FLAP IDLER HINGE FITTING INBD AND OTBD LUG INNER FACES WERE FOUND WORN AND ELONGATED BEYOND THE LIMITS OF CMM 27- 50-5. REPAIRED IAW ER/A 14-629961. (1422873)Jan 27, 2026 · N986AT · Boeing 717200SDR DALA2026020100735Flap Track · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) STAGE III APPROVAL REQUIRED FOR REPAIR ON THE LT OUTBOARD FLAP, TRACK 3, RIB 5 BORE PER ER/A 627489-14 REV A. SECTION I IS LIMITED TO 72000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SERJan 27, 2026 · N346NB · Airbus A319114SDR UATA2420127265701Hinge Bracket · corrodedRT INBD. FLAP, THE OUTBD. PYLON AIRFRAME SIDE, BOTH OF THE HINGE PLATES HAVE PITTING CORROSION THAT IS BEYOND LIMITS. DRILLED BOTH HINGE PLATES AND THE INBD. AND OUTBD. PYLON SIDE SKINS OFF. FITTED AND INSTALLED NEW SIDE SKINS P/N 212-13202-05-1 (INBD.) AND P/Jan 27, 2026 · N424CA · Casa C212200SDR DALA2026042002476Spar Web · crackedSPAR WEB CRACKED. PERFORMED CSVE INSPECTION, SPAR WEB DAMAGE REPAIRED, REF. ERA 632073-14 REV. ORG (OUTBOARD FLAP WAS FOUND WITH CRACK DAMAGE TO THE FORWARD SPAR WEB AND FOUR (4) ELONGATED FASTENER HOLES IN THE CARRIAGE FITTING, FORWARD SPAR, WEB, AND RIB ATJan 26, 2026 · Boeing 757*SDR VNAA20260511025Attach Bracket · corrodedRIGHT O/B FLAP HINGE ARM AFT FAIRING BRACKET IS CORRODED AT WS 178. REMOVED AND REPLACED BRACKET P/N 601R14629-82 I.A.W. CRJ-700 S.R.M. 51-42-06-001-001-A01Jan 24, 2026 · N512AE · Cndair CL6002C10SDR SWAA2026012663947Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. R & R RT WING OTBD TRAILING EDGE FLAP IAW AMM 27-51-21.Jan 23, 2026 · N219WN · Boeing 7377H4SDR CALA2026021813852Flap Track · wornFLAP TRACK NR 7 HAS WEAR ON THE UPPER RAIL. REPAIRED THE FLAP TRACK UPPER RAIL IAW SRM 57-53-02-2R-10, REP 10, (REPAIR IS A CATEGORY B) INSPECTION REQUIREMENTS IAW STEP 5 TABLE 202 . ALL WORK CAPTURED ON AAR N/R 1000065135. REPLACED THE NR 7 FLAP TRACK ASJan 22, 2026 · N33289 · Boeing 737824SDR FDEA202601220080Skin · dentedFOUND RT WWING T/E OTBD FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHS. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 203 AND SRM 51-70-04-2R-1 REV 51.0 AND Jan 22, 2026 · N857FD · Boeing 777FS2SDR AALA202602062372Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING OUTBOARD FLAP AFT SECTION UPPER SKIN DELAMINATED AT INBOARD END. REMOVED AND AND REPLACED SKIN. ADJUSTED AND OPS CHECK GOOD. PER NON-ROUTINE 08-9505-8-2227.Jan 21, 2026 · N982AN · Boeing 737823SDR AALA202602025870Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-42-11.Jan 20, 2026 · N580UW · Airbus A321231SDR AALA202602020619Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-42-11.Jan 20, 2026 · N580UW · Airbus A321231SDR CALA2026012213152Rib · wornLEFT OTBD FLAPS NR 1, 2, 3, & 4 AFT FLAP TRACK RIB SUPPORTS HAVE WEAR ON LOWER SURFACES. REMOVED DAMAGE, HFEC AREA, NO DEFECTS NOTED, ROTO PEENED AREA, ALODINED AND PRIMED IAW UAL ECRA 5754-01273, AND ENGINEERING DOC REO-G25762.Jan 20, 2026 · N54241 · Boeing 737824SDR VNAA20260508013Fitting · crackedLEFT FLAP HINGE BOX AFT MOUNTING FITTING AT WS 54.55 (WING SIDE) HAS GOUGES ON THE I/B LUG. REPAIRED INBD FLAP HINGE BOX ATTACHMENT, AFT HINGE FITTING AT WS54.55 LHS IAW MHIRJ REO 670-57-21-1101 REV -- DATED 2026-01-07.Jan 17, 2026 · N512AE · Cndair CL6002C10SDR 2026FA0000030Fairing · damagedRH INBOARD FLAP FAIRING IMPACT DAMAGEJan 17, 2026 · N816QS · Textrn TEXTRON700SDR VNAA20260511024Skin · damagedPANEL 584FB HAS DAMAGED SCREW HOLE FROM WHAT APPEARS TO BE SOMEONE DRILLING OUT A SCREW. REPAIRED LH I/B FLAP FWD SPAR LOWER FLANGE IAW MHIRJ REO 670-57-52-642 REV-- DATED 2026-01-16.Jan 16, 2026 · N512AE · Cndair CL6002C10SDR IPXA2026021042167Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACK INDICATIONS NOTED AT RIB 19. ACCOMPLISH PERMANENT REPAIR IAW EO-96389-REQ1 AND VT-MAE EA 300-5753-27-A4304, REV. -.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021042834Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 18. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-96389-REQ1 AND VT-MAE EA 300-5753-27-A4304, REV. -.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021042071Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, THREE CRACK INDICATIONS NOTED AT RIB 26. REQUIRES FINAL REPAIR STATEMENT AND INSP.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021042836Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 17. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-96389-REQ1 AND VT-MAE EA 300-5753-27-A4304, REV. -.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021042144Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 25. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-96389-REQ1 AND VT-MAE EA 300-5753-27-A4304, REV-.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021041989Rib · crackedMAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 27. OUT OF SEQUENCE, VERIFIED FROM STEP 17. FABRICATED REPAIR DOUBLER IAW SRM 57-50-00, PARA 4.E, FIG. 205.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026021042028Skin · crackedMAJOR REPAIR, LT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 26.Jan 16, 2026 · N145UP · Airbus A300F4622RSDR HNAA2026021600122Pin · corrodedCORROSION ON RH WING OTBD LOWER FLAP SHROUD CENTER SPRING ATTACHMENT PIN. REMOVED AND REPLACED RH WING OTBD LOWER FLAP SHROUD CENTER SPRING ATTACHMENT PIN IAW EMB 145 AMM 57-56-01Jan 16, 2026 · N647AE · Emb EMB145LRSDR FDEA202601160062Skin · dentedDENT ON LOWER SURFACE OF OUTBOARD FLAP RH WING AT 44" TO INB FRAME AND 17" TO LEADING EDGE LOWER SURFACE OF OUTBOARD FLAP RH WING AT 44" TO INB FRAME AND 17" TO LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIGURE 201 TABLE II AND SRM 51-70-1Jan 16, 2026 · N299FE · Boeing 7673S2FSDR 454A2601195121700Flap Track · crackedTHE AIRCRAFT WAS OPENED UP FOR PHASE INSPECTION ON 1/15/2026. UPON INSPECTION, THE RIGHT WING AND LEFT WING INBOARD FLAP, OUTBOARD FLAP TRACKS WERE CRACKED AND SEPARATED BY APPROXIMATELY 1/2". TRACKS BRACKET- OUTBOARD FLAP TRACK. BEECHCRAFT/TEXTRON HAS BEEN NOJan 15, 2026 · N48AP · Beech C90ASDR JR2R20260115368Retainer · corrodedL/H I/B MAIN FLAP TORQ TUBE RETAINER ASSY IS CORRODED. REPAIRED PER ETD.Jan 15, 2026 · N87339 · Emb ERJ170200LRSDR JR2R20260115370Retainer · corrodedR/H I/B MAIN FLAP TORQ TUBE RETAINER ASSY IS CORRODED. REPAIRED PER ETD.Jan 15, 2026 · N87339 · Emb ERJ170200LRSDR SWIA2026011475864Skin · chafedLEFT INBD FLAP VANE LEADING EDGE CHAFED IN MULTIPLE SPOTS. REPAIRED LT INBD FLAP VANE LEADING EDGE INBD PANEL AT BLENDED AREA 1 THAT WAS FOUND TO BE IN LIMITS REF REO 601R-57-52-004 REV.D DATE:2012-12-19. STEPS 1 TO 3. BLENDED AREAS #2 AND #3 ON (MID PANEL & Jan 14, 2026 · N959SW · Cndair CL6002B19SDR SWAA2026012261346Wedge · delaminatedLEFT INBD FLAP TRAILING EDGE WEDGE FOUND DELAMINATED AT TRAILING EDGE. REPAIRED THE LT INBD FLAP TRAILING EDGE WEDGE IAW SRM 57-53-01-2R-7, AND 51-70-10-2R-4.Jan 14, 2026 · N8664J · Boeing 7378H4SDR DALA2026012100447Skin · dentedRIGHT WING INBD T/E LOWER FLAP LOWER SURFACE FOUND DENTED AT WS 255.4. DAMAGED AREA REPAIRED IAW SRM 57-53-01-2R-1, SRM 51-70-10-2R-3, SRM 51-70-10-2R-4, AND SRM 51-70-10. (1400937)Jan 14, 2026 · N177DZ · Boeing 767332SDR SWAA2026011961092Fairing · crackedLEFT WING FWD FLAP TRACK SUPPORT FAIRING #2 IS CRACKED PANEL #543AB<[01] REPLACED FWD FAIRING PER AMM 27-51-28Jan 14, 2026 · N485WN · Boeing 7377H4SDR SWIA2026011375607Vane · chafedLT INBD FLAP VANE, LEADING EDGE CHAFED AT MULTIPLE SPOTS. R & R LT INBD FLAP VANE LEADING EDGE WITH NEW IAW SRM 51-42-10-001-001-A01, & DWG CC670-14010 REV -F.Jan 13, 2026 · N726SK · Cndair CL6002C10SDR REXA2026030900212Fitting · wornWEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING (2EAS) OF FLAP STUB FAIRING 171DL AND 172DR AT RT & LT WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, CRJ900 SRM 51-42-Jan 13, 2026 · N272PQ · Cndair CL6002D24SDR JJBA20260113023Angle · corrodedDURING INSPECTION FOUND CORROSION ON RH IB FLAP IB SIDE L ANGLE. REMOVED AND REPLACED WITH NEW FROM STOCK RH IB FLAP IB SIDE L ANGLEJan 13, 2026 · N12175 · Emb EMB145XRSDR CALA2026011312922Seal · missingFOUND LOWER INBD FLAP BULB SEAL MISSING. REPLACED THE BULB SEAL WITH NEW IAW IPC 27-51-11-01.Jan 12, 2026 · N18243 · Boeing 737824SDR LR7A2026011103800Skin · crackedDURING SCHEDULED INSPECTION, FOUND CRACK ON THE RT OTBD FLAP LOWER SKIN. REPAIRED IAW SMP 583 51-140-12, & MEA 382-57-26-002. LP#59025Jan 11, 2026 · N407LC · Lkheed 382GSDR CALA2026011212885Skin · dentedFOUND PREVIOUS DAMAGE ON RT OTBD FLAP TRAILING EDGE. REMOVED OLD BONDING MATERIAL. MAPPED DAMAGE DENT IS LOCATED BETWEEN RIBS 7 & 8 LOWER SURFACE APPROX. 3" AFT OF TE SPAR FASTENERS. DENT NOT IN ALLOWABLE LIMITS IAW SRM 57-53-00-283-092, FIG 1, SHEET 1. REFJan 10, 2026 · N828UA · Airbus A319131SDR VNAA202501090010Fitting · gougedRIGHT FLAP FITTING (AFT) AT WS 264.00 HAS GOUGED ON LUG EAR.Jan 9, 2026 · N511AE · Cndair CL6002C10SDR SWIA2026010875793Hinge Arm · gougedLEFT INBD FLAP HINGE ARM ASSY AT WS80.50 HAS GOUGE ON FWD HINGE FITTING. REPAIRED FWD HINGE FITTING FOR LT INBD FLAP HINGE ARM ASSY AT WS80.50 PER REO 601R-57-54-388, REV--, COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.Jan 8, 2026 · N941SW · Cndair CL6002B19SDR FDEA202601080041Rib · crackedRIGHT CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB 26 BETWEEN STGR2.6 AND REAR SPAR, RIB 27 BETWEEN STGR 2.7 AND REAR SPAR. RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA:6-5750-T0386104 P1 TO REPAIR RH CENTER FLAP RIB UPPER FLANGE 5EA CRACKS ATJan 8, 2026 · N658FE · Airbus A300F4605RSDR FDEA202601080040Rib · crackedRIGHT CENTER FLAP RIB UPPER FLANGE FOUND CRACK AT RIB 11 BETWEEN S 2.7 AND S 2.8. COMPLIED WITH EA:6-5750-T0386104 P1 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WING - FLIGHT SURFACES - RT CENTER FLAP CJan 8, 2026 · N658FE · Airbus A300F4605RSDR SWAA2026011259281Skin · delaminatedLEFT WING OTBD AFT FLAP HAS 3' X 8' AREA DELAMINATION AT AFT INBOARD CORNER. REMOVED FLAP IAW MM 27-51-22, C/W RII REQUIREMENT FOR REMOVED FLAP IAW MM 27-51-22. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22. OPS AND RIG CHECKED GOOD.Jan 8, 2026 · N7827A · Boeing 73779PSDR FDEA202601080014Skin · dentedRIGHT INBD TE FLAP AFT FLAP IS DAMAGED ON THE UPPER SURFACE. REPAIRED RT INBD TE FLAP AFT FLAP TOP UPPER SURFACE AT WS STA. 287.4 IAW SRM 57-53-01-2R, FIG 201, SHEET 4, REPAIR 1, & SRM 51-70- 10-2R. MAJOR REPAIR. SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.Jan 8, 2026 · N161FE · Boeing 7673S2FSDR IPXA2026011389555Skin · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE; 3 CRACKS NOTED AT RIB27. CIRCLED IN RED. REAMED DAMAGED SHEARED FASTENER HOLE FROM 0.156" TO 0.187" IAW A300 SRM 51-40-44. OK TO INSTALL REPAIR PARTS GIVEN. COMPLIED WITH STEP 4 E OF E.A.#: 300-5753-27-A4260 PREJan 7, 2026 · N150UP · Airbus A300F4622RSDR IPXA2026011389650Skin · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE; 3 CRACKS NOTED AT RIB26. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96213-REQ1 AND VT-MAE EA 300-5753-27-A4260, REV. -.Jan 7, 2026 · N150UP · Airbus A300F4622RSDR DALA2026010800168Bridge · crackedLEFT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE CRACKED. REMOVED AND REPLACED THE LT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE IAW AMM 27-54-78. OK FOR SERVICE. (1390089)Jan 7, 2026 · N818NW · Airbus A330323SDR DALA2026010800167Bridge · crackedFOUND LT WING NR 4 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE CRACKED. REMOVED AND REPLACED LT WING NR 4 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE IAW AMM 27-54-78. OK FOR SERVICE. (1390070)Jan 7, 2026 · N818NW · Airbus A330323SDR DALA2026010800166Bridge · crackedLEFT WING NR 2 FLAP TRACK CARRIAGE ASSY INBD BRIDGE CRACKED. REMOVED AND REPLACED THE LT WING NR 2 FLAP TRACK CARRIAGE ASSY INBD BRIDGE IAW AMM 27-54-78. OK FOR SERVICE. (1390055)Jan 7, 2026 · N818NW · Airbus A330323
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