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 IPXA2025101564861Skin · gougedGOUGE - SKIN - RT WING OUTBOARD FLAP AFT FLAP AT WS 880 - 890. REFER TO 747 NDT MANUAL, PART 6,51-00-00, FIGURE 1,11OR 16 FOR HFEC PROCEDURE. IAW EGAT EI F 2025A57M-2243 SEQUENCE A STEP 3. REQUEST RII VERIFY VALIDATE SPECIALIZED PROCESS IN REPAIR INSTRUCTIONS Oct 3, 2025 · N573UP · Boeing 74744AFSDR DALA2025100607272Support Fitting · corrodedLEFT WING INBD FLAP OUTBOARD MAIN SUPPORT FITTING BEARING CORROSION. REPAIRED PER ER/A 628976-14. (1232420)Oct 3, 2025 · N351NB · Airbus A319114SDR DALA2025100607271Flap Track · corrodedRIGHT WING OB FLAP TRACK #3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING AREA CORROSION. REPAIRED PER ER/A 14-629082. (1232738)Oct 3, 2025 · N351NB · Airbus A319114SDR SWAA2025102720650Skin · debondedLEFT WING O/B AFT FLAP DISBONDED AT I/B LOWER CORNER. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.Oct 2, 2025 · N456WN · Boeing 7377H4SDR CALA2025100609666Seal · missingLEFT WING I/B FLAP LOWER O/B SEAL MISSING. UPATED PICTURE. INSTALLED LEFT WING I/B FLAP LOWER O/B SEAL IAW AMM 27-51-11.Oct 2, 2025 · N37466 · Boeing 737924ERSDR VNAA20251111002Skin · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. NICKS ON LOWER SKIN OF LT INBOARD FLAP FLS 48.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN OF LIMITS PER SRM 57-52-01-101-001-A01 AOct 1, 2025 · N631NN · Bombdr CL6002D15SDR FDEA202509301962Rib · cracked2EA CRACKS (5MM & 20MM) INDICATION WERE FOUND AT RH WING CENTER FLAP RIB27 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB27, S-2.7~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385Sep 30, 2025 · N690FE · Airbus A300F4605RSDR FDEA202509301946Skin · cracked1 EA CRACK (40MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB17 AFTER RIB FLANGE AREA OF TOP SURFACE ACCOMPLISHED RIB FLANGE REPAIR AT RIB17, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16 ~18, REAR SPAR ~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072P1, Sep 30, 2025 · N690FE · Airbus A300F4605RSDR FDEA202509301944Skin · cracked1 EA CRACK (30MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB18 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB18, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16 ~18, REAR SPAR ~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072PSep 30, 2025 · N690FE · Airbus A300F4605RSDR FDEA202509301940Skin · cracked1 EA CRACK (20MM) WAS FOUND AT LH WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 27, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 26~27, REAR SPAR~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385172 P1, SEQ NO: TSep 30, 2025 · N690FE · Airbus A300F4605RSDR SWAA2025102019291Skin · delaminatedRT WING OTBD AFT FLAP HAS DELAMINATION ON THE UPPER SURFACE 4' FROM THE INBOARD END NEAR THE TRAILING EDGE. RT OTBD AFT FLAP WAS REMOVED ALONG WITH FLAP ASSY AND SERVICABLE RT OTBD AFT FLAP WITH FLAP ASSY WAS INSTALLED ON FAULT TTG8Q015LVFW.Sep 29, 2025 · N8513F · Boeing 7378H4SDR FDEA202509271840Skin · dentedDENT ON INBD AFT FLAP WS 420 EXTERNAL SURFACE AT LH WING ON INBD AFT FLAP WS420 EXTERNAL SURFACE AT LH WING WAS EVALUATED AND REQUIRED REPAIR I.A.W SRM B767 57-53-01-2R FIG.201 SHEET 4 REV. 92 APR 15,2025 AND REPAIR I.A.W SRM B767 51-70-10-2R FIG 201 SHEETSep 27, 2025 · N199FE · Boeing 767300SDR EE4Y2025092723174Skin · delaminatedCUSTOMER REPORTS DELAMINATION DAMAGE AFFECTING THE LH INBOARD AFT FLAP LOWER SKIN. THE DAMAGE IS LOCATED AT SPAR 2 AND RIB 5A +50MM. THE DAMAGE AREA WAS EVALUATED AS PER SRM 57-52-00 AD51, HOWEVER, THE DELAMINATION IS LOCATED AT THE ZONE 1 AREA AND TABLE 101. Sep 27, 2025 · N247JB · Emb ERJ190100IGWSDR CALA2025092909366Skin · delaminatedUPON EXTERNAL WALKAROUND FOUND OUTBD RIGHT TRAILING EDGE FLAP DELAMINATED. INSPECTED FLAP TRACKS AND HDWR, STARTED INSTALLATION OF R/H OUTBOARD AFT FLAP REF AMM 27-51-22-400-801 STEPS 3G THRU 3H (4)-(F) VERIFIED R/H OUTBD AFT FLAP INSTALLATION STEPS 3G-3H(4Sep 25, 2025 · N68817 · Boeing 737924ERSDR LR7A2025092503781Rivet · looseDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LEFT OUTBOARD FLAP LOWER TRAILING EDGE SKIN WITH LOOSE RIVETS AT OWFS87L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001308670.Sep 25, 2025 · N407LC · Lkheed 382GSDR CALA2025092609312Repair · missingDURING EXTERNAL WALKAROUND, FOUND AREA ON RT OTBD FLAP, INBD TRAILING EDGE HAD A PREVIOUS REAPAIR OF APPROXIMATELY 69.56 SQ/IN WITH REPAIR DOUBLER MISSING AND AN AREA OF APPROXIMATELY 28 SQ/IN DELAMINATED. WORK WILL BE ACCOMPLISHED ON ORIGINAL LOG 6397083.Sep 25, 2025 · N68817 · Boeing 737924ERSDR FDEA202509251827Hinge · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHSep 25, 2025 · N590FE · Doug MD11FSDR AALA202510140953Rod · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE SEVERAL LINKAGES BETWEEN AFT PYLON AND NUMBER 6 FLAP TRACK HAVE EXCESSIVE PLAY. REMOVED AND REPLACED SEVERAL SUPPORT BEAM BEARINGS (AALA202510142989),. ATTACHMENT HARDWARE (AALA202510141608) AND RODS (AALASep 24, 2025 · N862NN · Boeing 737823SDR AALA202510141608Linkage · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE SEVERAL LINKAGES BETWEEN AFT PYLON AND NUMBER 6 FLAP TRACK HAVE EXCESSIVE PLAY. REMOVED AND REPLACED SEVERAL SUPPORT BEAM BEARINGS (AALA202510142989),. ATTACHMENT HARDWARE (AALA202510141608) AND RODS (AALASep 24, 2025 · N862NN · Boeing 737823SDR AALA202510142989Bearing · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE SEVERAL LINKAGES BETWEEN AFT PYLON AND NUMBER 6 FLAP TRACK HAVE EXCESSIVE PLAY. REMOVED AND REPLACED SEVERAL SUPPORT BEAM BEARINGS (AALA202510142989),. ATTACHMENT HARDWARE (AALA202510141608) AND RODS (AALASep 24, 2025 · N862NN · Boeing 737823SDR DALA2025092506993Rib · damagedDAMAGE FOUND TO LH OUTBOARD FLAP, RIB 1 SKIN, ADJACENT TO FLAP INTERCONNECT STRUT. REPAIRED PER ER/A 629324-14. (1215919)Sep 24, 2025 · N320NB · Airbus A319114SDR DALA2025092506992Rib · damagedDAMAGE FOUND TO RT OUTBOARD FLAP, RIB 1 SKIN, ADJACENT TO FLAP INTERCONNECT STRUT. REPAIRED PER 629325-14. (1215916)Sep 24, 2025 · N320NB · Airbus A319114SDR DALA2025092506986Bonding Plate · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING (533CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1216019).Sep 24, 2025 · N352NB · Airbus A319114SDR DALA2025092506985Bonding Plate · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING 633CB ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1216002).Sep 24, 2025 · N352NB · Airbus A319114SDR SWIA2025092375386Hinge Arm · gougedLEFT OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) HAS GOUGES ON EDGE OF HOUSING FOR SPHERICAL BEARING. REPAIRED DAMAGE ON LH OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) IN COMPLIANCE WITH REO 670-57-53-428 REV-- DATED 2025-09-26. PERFORMED EDDY CURRENT INSPECTISep 23, 2025 · N609SK · Cndair CL6002C10SDR IPXA2025101392852Rib · crackedMAJOR REPAIR - RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, TWO CRACKS INDICATION NOTED AT RIB 11. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 & VT-MAE EA 300-5750-27-A4159, REV -.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101391733Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, THREE CRACK INDICATIONS NOTED AT RIB 27. ACCOMPLISH PERMANENT REPAIR IAW EO-95120-REQ1 AND VT-MAE EA 300-5750-27-A4111.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025100691954Rib · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE. ONE CRACK NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-95368-REQ1 AND VT-MAE EA 300-5750-27-A4158.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025100691980Rib · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE. TWO CRACKS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-95368-REQ1 AND VT-MAE EA 300-5750-27-A4158.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392168Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, THREE CRACK INDICATION NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392393Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 25. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392498Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 19. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392588Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 18. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392543Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 17. PERFORMED 2X CUTOUTS AT RIB 17 TO RIB 19 FROM REAR SAPR TO STR 2.1 IAW SRM-57-50-00 PARA 4E FIG 205 AND EA 300-5750-27-A4159, STEP 15. .ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-RSep 23, 2025 · N173UP · Airbus A300F4622RSDR IPXA2025101392772Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 12. CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.Sep 23, 2025 · N173UP · Airbus A300F4622RSDR FDEA202509231766Skin · dentedLH WING, OUTBD TRAILING EDGE FLAP, DENT ON LEADING EDGE APPROX 9" TO 10" FROM INBD END. MK11 REPAIRED LH WING, OB TE FLAP, DENTED ON LE AREA; MPN;113T3110-4016, PANEL# 566AT, AT WING STATION:538.2-544 IN REF TO B767 SRM 57-53-01-2R FIG 201 SHEET 5 REPAIR 1Sep 23, 2025 · N263FE · Boeing 7673S2FSDR SWIA202602275358Skin · chafedRH INBOARD FLAP LOWER SKIN HAS CHAFE DAMAGE AT INBOARD INTERFACE OF FAIRING. (C-CHECK RO 02/25/2026)REPAIRED RH INBOARD FLAP LOWER SKIN WITH REFERENCE TO SRM 57-52-01 AND REO 670-57-52-628 REV "--" DATED 2025-10-15. REPLACED RH INBOARD FLAP LOWER SKIN WITH Sep 22, 2025 · N609SK · Cndair CL6002C10SDR FDEA202509201941Skin · crackedRH CTR FLAP INTERNAL STRUCTURE CRACK AT UPPER RIB 18, STGR-2.8 TO REAR SPAR. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 18, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16~18, REAR SPAR~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, SEQ NO: 1031, REPAIR CLASSep 20, 2025 · N690FE · Airbus A300F4605RSDR SWAA2025102716473Skin · delaminatedLEFT HAND OUTBOARD AFT FLAP IS DELAMINATED AT AFT INBOARD CORNER. REMOVED AND REPLACED LT OTBD AFT FLAP PER AMM 27-51-22. RII INSPECTED LT OUTBOARD AFT FLAP PER AMM 27-51-22.Sep 19, 2025 · N8504G · Boeing 7378H4SDR SWIA2025091876515Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA47106-690-57-52-320 N813SK CP18197005-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 47106COMPLIED WITH TERMP REPAIR TO L/H INBD FLAP REF REO 690-57-52-320 REV-. . PERFORM PERM REPAIR AT OR BEFORE 8000 FT FROM INCORPORATISep 18, 2025 · N813SK · Cndair CL6002D24SDR FDEA202509171833Flap · no discrepancyEXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB17-18, STGR2.7 - 2.8 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 TP1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, EXISTISep 17, 2025 · N690FE · Airbus A300F4605RSDR UIEA2025090501163Flap · damagedNUMBER 21 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR UIEA2025090501164Flap · damagedNUMBER 18 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR UIEA2025090501165Flap · damagedNUMBER 9 V/C FLAP DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR UIEA2025090501166Flap · damagedNUMBER 8 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR UIEA2025090501167Flap · damagedNUMBER 6 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR UIEA2025091101184Skin · chafedNUMBER 4 V/C FLAP BULLNOSE EDGE CHAFED. PERFORMED REPAIR AT CHAFED AREA IAW SRM 51-70-04, REPAIR 7. NO FURTHER DEFECTS NOTED.Sep 17, 2025 · N859GT · Boeing 74787UFSDR FDEA202509171738Skin · dentedLEFT WING, OUTBOARD FLAP, UNDER SIDE, HAS A LARGE SMOOTH DENT, 144" FROM INBOARD EDGE AND 22.5" UP FROM TRAILING EDGE OF FLAP AS MARKED. REPAIRED L/H WING OUTER SKIN 7.75" X 6" AREA ON LOWER SURFACE OF OUTBOARD TRAILING EDGE FLAP ALUMINUM HONEYCOMB SKIN PASep 17, 2025 · N154FE · Boeing 7673S2FSDR IPXA2025092335886Skin · crackedRIGHT WING CENTER FLAP,TOP SKIN RIB FLANGE, ONE CRACK NOTED AT RIB 13. INSTALLATION IN STEP 17, PRIMER AND TOPCOAT APPLIED. INSTALLED DOUBLER IAW-A300-SRM-51-40-21.Sep 16, 2025 · N124UP · Airbus A300F4622RSDR SWAA2025092215229Wedge · delaminatedLEFT INBD MAIN FLAP OTBD OF NR 3 CANOE ON TRAILING EDGE OF FLAP LOWER SIDE IS DELAMINATED TSR-2025008016. REMOVED DAMAGED TRAILING EDGE WEDGE, LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-06; INSTALLED NEW WEDGE PER SOPM 20-50-01.Sep 16, 2025 · N912WN · Boeing 7377H4
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