JASC 5753

Service difficulty reports · 31,515

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 SWAA083469Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jun 23, 2008 · N646SW · Boeing 7373H4SDR USAA920081262Flap · delaminatedCLT - C-22 - MAJOR REPAIR - FOUND DELAMINATION ON LEFT OUTBOARD AFT FLAP MEASURES 4"X4.5", 5.5" FORWARD OF TRAILING EDGE. REPAIRED DELAMINATION ON LEFT OUTBOARD AFT FLAP 4"X4.5" AREA., 5.5" FORWARD OF TRAILING EDGE IAW B757 SRM 57-53-01. (S)Jun 21, 2008 · N939UW · Boeing 7572B7SDR 08FDEA02368Skin · gougedRIGHT WING INBD FLAP L/E IS GOUGED AT TWO PLACES. REPAIRED RIGHT WING INBD FLAP L/E SECTION IAW A300-600F SRM 57-50-00; FIG 208.Jun 20, 2008 · N675FE · Airbus A300F4605RSDR 08FDEA02351Vane · delaminatedLEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 156 TO XIFH 206. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-22-5.Jun 20, 2008 · N586FE · Doug MD11FSDR 08FDEA02357Skin · damagedLEFT INBOARD FLAP LOWER SKIN HAS REPAIR MISSING, BETWEEN FLAP RIB 2 AND FLAP RIB 4 REMOVED DAMAGED SKIN AND CORE, FABRICATED AND INSTALLED FLAP REPAIR DOUBLER AT LT INBD LOWER SKIN BETWEEN FLAP RIB 2 AND FLAP RIB 4 IAW FEDEX EA 6-5750-121281, RELEASE DATE 29 MJun 20, 2008 · N443FE · Airbus A310203SDR UPS08152598Skin · chafedINSPECTION TYPE:5YR 2EA CHAFE MARKS ON UPPER SURFACE OF RT INBOARD FLAP AT RIB 12 & 14 STR 2.2 & 2.3. 2EA AREAS FOUND OUT OF LIMITS ON NRC 196779. CUT OUT 2EA DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 FIG 205.Jun 19, 2008 · N152UP · Airbus A300F4622RSDR UPS08152597Skin · chafedINSPECTION TYPE:5YR 2EA CHAFE MARKS ON UPPER SURFACE OF RT INBOARD FLAP AT RIB 18 & 19 STRINGER 2.2. 2EA AREAS FOUND OUT OF LIMITS ON NRC 196779. CUT OUT 2EA DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 FIG 205.Jun 19, 2008 · N152UP · Airbus A300F4622RSDR 08FDEA02349Skin · dentedTHE RIGHT INBD FLAP LOWER SURFACE HAS DENTS. LIMITS CHECKED AND THE DENTS WERE FOUND TO BE WITHIN LIMITS AT DOTS C528, 0.029 AND P745, 0.029 IAW A300-600 SRM 57-50-00 PGS 104; 105 AND 106; FIGURE D USING DEPTH GAUGE T8410B. DOT NR C527 WAS FOUND TO BE OUT OF Jun 19, 2008 · N665FE · Airbus A300F4605RSDR 08FDEA02321Skin · chafedFOUND 2 CHAFING MARKS AT LT OUTER FLAP TOP SKIN, RIB 3A-4 AND 14A-15A REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION AND INSTALLING NEW CHAFING PLATES IAW RAS/FOK/131/2008 ISS A, APPROVED BY EA 6-5754-120125.Jun 19, 2008 · N742FD · Airbus A300B4622RSDR UIE2008F00008Skin · delaminatedFOUND DURING A-CHECK. REPAIR THE DAMAGE FOUND ON L/E OF LEFT OB FOREFLAP MEASURING 12 INCHES LONG BY 2 INCHES WIDE IAW SRM 51-70-07. REPAIR CARRIED OUT IAW EO 4457A145. (K)Jun 18, 2008 · N408MC · Boeing 74747UFSDR 08FDEA02318Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FLAP TRACK NR 3 AND 5.7 INCH FWD OF REAR SPAR MEASURING 11.3 INCH BY 3.9 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTJun 18, 2008 · N443FE · Airbus A310203SDR SWAA083346Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.Jun 18, 2008 · N799SW · Boeing 7377Q8SDR CA080619007Flap Track · cracked(CAN) DURING A WALKAROUND THE PILOTS NOTICED EXCESSIVE PLAY ON THE RT OTBD FLAP AT THE INBD HINGE. THE FLAP WAS REMOVED FOR FURTHER INVESTIGATION AND THE INBD FLAP TRACK WAS FOUND TO BE CRACKED AT THE AFT END OF THE TRACK, THE CRACK WEAKEN THE TRACK ALLOWING IJun 17, 2008 · Beech A100ASDR F3LA200800357Arm · chafedDURING C-CHECK INSP NOTED RT NR TWO FLAP TRACK DRIVE LEVER EXTENSION ARM THAT ATTACHES TO FLAP AT AFT ATTACH POINT IS CHAFING INTO FITTING ON OB EAR BOTTOM END AND IB EAR TOP END. MAINT REPAIRED AREA IAW EA A9-57R-30378, SRM 51-73-00 AND SRM 51-21-11. UPON COJun 17, 2008 · N926FR · Airbus A319111SDR 08FDEA02979Fitting · corrodedLT WING NR 3 TRACK FRONT CARRIAGE INTERIOR FITTING WITH CORROSION, DETECTED WHILE PERFORMING N0800. THE NR 3 TRACK FRONT CARRIAGE WAS REPLACED BY ONE FABRICATED AS PER FEDEX EA 6-5740-120510.Jun 16, 2008 · N721FD · Airbus A300B4622RSDR UPS08M52640Fitting · crackedINSPECTION TYPE-C, LT WING OB FLAP STOP BOLT FITTING (SECOND RIB FROM IB) SUSPECT CRACK AS MARKED. HFEC INSP CARRIED OUT IAW NDT SPM R.13 PART 06.10.01.001 ON STOP BOLT FOUND CRACKED AS MARKED. CRACKED STOP BOLT FITTING & ATTACHED PARTS REMOVED IAW SRM 51-31-Jun 16, 2008 · N271UP · Doug MD11FSDR IXX2008F00084Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTAJun 14, 2008 · N721CX · Doug DC872FSDR IXX2008F00051Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTAJun 14, 2008 · N721CX · Doug DC872FSDR IXX2008F00070Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 3000 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER.Jun 13, 2008 · N721CX · Doug DC872FSDR IXX2008F00060Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIRJun 13, 2008 · N721CX · Doug DC872FSDR IXX2008F00055Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIRJun 13, 2008 · N721CX · Doug DC872FSDR IXX2008F00048Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 3000 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER.Jun 13, 2008 · N721CX · Doug DC872FSDR USAA920081217Skin · delaminatedCLT - C3 - MAJOR REPAIR - NR 04-9557-8-0055/001 - LEFT WING OB AFT FLAP DELAMINATED ON TOP SIDE. REPLACED LEFT WING OB AFT FLAP IAW B737, AMM 27-51-39. (K)Jun 13, 2008 · N434US · Boeing 7374B7SDR 08FDEA02254Skin · misrepairedPREVIOUS EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RIGHT WING I/B FLAP TRAILING EDGE LOWER SKIN BETWEEN TRACK 1 TO RIB 10 AND AT THE AFT EDGE MEASURING 59 INCH BY 11.6 INCH. REPAIR NOT IAW EA6-5750-62865. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIRJun 13, 2008 · N443FE · Airbus A310203SDR 08FDEA02245Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING O/B FLAP UPPER MAIN SKIN UNDER RUBSTRIP BETWEEN FLAP TRACK NR 4 TO RIB 7 AND 10 INCH FWD OF REAR SPAR MEASURING 4.7 INCH BY 5.9 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CJun 12, 2008 · N443FE · Airbus A310203SDR CA080612001Vane · cracked(CAN) DURING A DAILY INSPECTION, THE LT INBD FLAP VANE WAS FOUND CRACKED ON THE UPPER SURFACE. THE CRACK IS APPROXIMATELY 2 INCHES LONG. FLAP TO BE REMOVED AND SENT OUT FOR FLAP VANE REPLACEMENT. LOANER FLAP TO BE INSTALLED.Jun 11, 2008 · Cndair CL600*SDR 2008UALA03325Wedge · delaminatedMID FLAP T/E WEDGE IS DELAMINATED 47.5 INCHES OUTBOARD FROM INBOARD EDGE AND IS DENTED ON LOWER SURFACE DUE TO BIRD STRIKE. FOUND DAMAGE TO BE OUT OF LIMITS. REPLACED LT I-B MID FLAP WEDGE REF MM 27-51-11 PG 406, ALL GAPS CHECKED GOOD. AC OK FOR SERVICE.Jun 11, 2008 · N329UA · Boeing 737322SDR 2008UALA03324Skin · damagedLEFT INBOARD AFT FLAP CREASED FROM BIRD STRIKE. FOUND DAMAGE OUT OF LIMITS. REPLACED LEFT IB AFT FLAP REF MM 27-51-11 PG 401, ALL GAPS CHECKED WITHIN LIMITS, OPS CHECKED GOOD. AC OK FOR SERVICE.Jun 11, 2008 · N329UA · Boeing 737322SDR 2008UALA03322Carriage · corrodedLEFT OUTBOARD FLAP SPINDLE DUE TO CORROSION IN THE EXPOSED PORTION OF SPINDLE. REMOVED LT OTBD FLAP OUTBD SPINDLE. REPLACED LT OTBD MIDFLAP CARRIAGE 355 LT.Jun 11, 2008 · N914UA · Boeing 737522SDR 08FDEA02212Skin · delaminatedLEFT WING INBD FLAP T/E AREA IS DENTED AND DELAMINATED APPROX 18 INCHES FROM THE OUTBD EDGE. REPAIRED THE LEFT INBD FLAP BY REMOVING THE DAMAGED AREA ; FABRICATING; AND BONDING A NEW CORE AND DOUBLERS IAW A310 SRM 57-52-12 AND FEDEX EA 6-5750-118501 TITLED "Jun 10, 2008 · N815FD · Airbus A310324SDR UPS08152445Flap · dentedINSPECTION TYPE:N/A LT INBOARD T/E FLAP DENT OUT OF LIMITS. Jun 10, 2008 · N159UP · Airbus A300F4622RSDR QXEA200800656Skin · chafedPDX C4 CHECK LT WING OTBD FLAP IS CHAFFED ON THE UPPER SURFACE BETWEEN STATION YW 209.019 AND 227.019. BLENDED AREA TO SMOOTH CONTOUR TO REMOVE DAMAGE. HFEC IAW -8 400 NDTM PART 6 51-00-01 NO CRACKS NOTED. UT THICKNESS IAW -8 400 NDTM PART 1 51-00-04 MAPPEDJun 9, 2008 · N424QX · Bombdr DHC8402SDR QXEA200800637Skin · chafedPDX C4 CHECK LT WING OTBD FLAP IS CHAFFED ON THE UPPER SURFACE APPROX AT STA YW 250. AND YW 265. BLENDED AREA TO SMOOTH CONTOUR TO REMOVE DAMAGE. HFEC IAW -8 400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51-00-04. BLENDJun 9, 2008 · N424QX · Bombdr DHC8402SDR IXX2008F00087Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00078Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEWJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00073Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. Jun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00045Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00041Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. Jun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00034Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WING OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00033Skin · wornDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00032Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEJun 9, 2008 · N721CX · Doug DC872FSDR 08FDEA02208Skin · delaminatedLT OB FORE FLAP WBL 478 ON T/E IS DELAMINATED CUT OUT DELAMINATED AREA 4 1/2 BY 9 INCH ON LT O/B FOREFLAP WBL 478. FABRICATED FILLER 4 1/2 BY 9 INCH AND DOUBLER 6 INCH BY 12 INCH FROM 0.016" 2024-T3 PO NR 9004174 IAW B727 SRM 57-50-2. BONDED FILLER AND DOUBLJun 9, 2008 · N490FE · Boeing 727227SDR UPS08652440Cap · crackedINSPECTION TYPE:N/A RIGHT WING O/B FLAP LEADING EDGE CAP CRACKED.Jun 9, 2008 · N305UP · Boeing 76734AFSDR 08FDEA02187Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP LOWER SKIN AFT OF FWD SPAR BETWEEN RIB NR 3 AND RIB NR 4, MEASURING 6.9 IN BY 8.6 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED OUTER SKIN REPAIR ON RT WING OUTBD FLAP Jun 6, 2008 · N443FE · Airbus A310203SDR 08FDEA02185Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 6 AND RIB NR 7 AND 2.6 IN FWD OF REAR SPAR MEASURING 4.0 IN BY 4.0 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED OUTER SKINJun 6, 2008 · N443FE · Airbus A310203SDR SWAA083070Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM.Jun 6, 2008 · N332SW · Boeing 7373H4SDR UPS08M52969Hinge · corrodedINSPECTION TYPE:C, RT WING OB FLAP OB FWD HINGE ACTUATOR MOUNTED IB BORE FOUND CORRODED. RT OB FLAP OB HINGE ACTUATOR MOUNTED IB BORE CORROSION REMOVED AND FOUND EXCEED LIMIT IAW CMM57-44-09 PG 602-607 R61.FPI C/O IAW DAC NDT SP R13 PT 08 ON REWORK AREA, FOUJun 5, 2008 · N296UP · Doug MD11FSDR CA080609009Attach Fitting · cracked(CAN) WHILE CARRYING OUT A 7 DAY SERVICE CHECK, TECH FOUND 3 FLAP TO SLAT ATTACHEMENT CLEATS, P/N`S 137201B88, 137202B62 AND 137203B57 WERE FOUND TO BE CRACKED. THE FLAP SECTION WAS REMOVED AND A SERVICEABLE UNIT INSTALLED. FUNCTION CHECKS CARRIED OUT WITH NOJun 4, 2008 · Bag JETSTM3212SDR MAL2008F00004Skin · puncturedPUNCTURE IN UPPER SKIN OF LT FLAP BELOW EXHAUST SHROUD 454AT. DID WET LAYUP COMPOSITE REPAIR ON LT FLAP BELOW EXHAUST SHROUD 454AT IAW EO S51031. (S)Jun 4, 2008 · N449XJ · Saab 340BSDR 08FDEA02152Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 10 AND RIB 11 AND 1.1 IN FWD OF REAR SPAR MEASURING 4.8 INCH BY 10.5 INCH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECTJun 4, 2008 · N443FE · Airbus A310203
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