JASC 5753

Service difficulty reports · 31,515

Reports filed under 5753 · Trailing Edge Flaps, newest first.

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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 AWXA200601506Wedge · debondedDEBONDED NR 5 SLAT WEDGE UPPER SURFACE, INBD END. REPAIRED DEBONDED AREA ON NR 5 SLAT WEDGE UPPER SURFACE I/B END, IAW B737-300, SRM 51-70-10-2R, REPAIR NR 4, FIG 201.Aug 12, 2006 · N335AW · Boeing 7373U3SDR 06FDEA2966Structure · corrodedRIGHT WING TRAILING EDGE O/B FLAP AFT O/B CORNER UNDER STATIC WICK BASE IS CORRODED. COMPLIED WITH EA 6-5750-102894 & N00182 WITH JPF ATTACHED.Aug 12, 2006 · N676FE · Airbus A300F4605RSDR UPS06247831Skin · crackedINSPECTION TYPE-C CRACK ON RT OB FORE FLAP LE AT CUTOUT OB OF IB SEQUENCE CARRIAGE ATTACH BRACKET DAMAGE OUTSIDE LIMITS IAW SRM 57-50-1. CRACK STOP DRILLED IAW SRM 57-5 0-4. HFEC CARRIED OUT IAW NDTM 51-00-00 PT 6 FIG 4 CRACK CONTAINE D. REPAIR CARRIED OUT IAug 11, 2006 · N942UP · Boeing 72722CSDR 06FDEA2962Bushing · galledN01113, NR 2 FLAP TRACK, BUSHING GALLED IN IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR. REPAIRED BUSHING NR2 FLAP TRACK IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR IAW EA 7-5710-100565.Aug 11, 2006 · N201FE · Boeing 727200SDR SWAA062974Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Aug 11, 2006 · N385SW · Boeing 7373H4SDR 06FDEA2949Skin · damagedSNRM N00695: EXISTING REPAIR FOUND AT LT IB TRAILING EDGE FLAP UPPER SKIN.Aug 11, 2006 · N522FE · Doug MD11SDR DHL2006784DHSkin · delaminatedUPON VISUAL INSPECTION OF WING SURFACES ON WALKAROUND FOUND LEFT WING OUTBOARD T/E FORE FLAP WITH DELAMINATION AT T/E APPROX 6 INCHES LONG AND 1 INCH INTO SKIN WITH AREA SOFT. FORE FLAP WAS REPLACED.Aug 10, 2006 · N784DH · Boeing 727227SDR ASAA0680861Skin · gougedFOUND RIGHT WING OUTBOARD FLAP INBOARD VANE IS GOUGED. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER SRM 51 70 2.Aug 10, 2006 · N977AS · Doug DC983SDR ASAA0680860Skin · gougedFOUND LEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT DOUBLER AND FILLER PER SRM 51 70 2.Aug 10, 2006 · N977AS · Doug DC983SDR ASAA0680859Skin · dentedFOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE DENTED. REMOVED DAMAGED VANE SKIN. INSTALLED SKIN FILLER AND EXTERNAL REPAIR DOUBLER PER SRM 57 03 AND 51 70 2.Aug 10, 2006 · N977AS · Doug DC983SDR SWAA062965Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.Aug 10, 2006 · N695SW · Boeing 7373Q8SDR SWAA062964Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.Aug 10, 2006 · N695SW · Boeing 7373Q8SDR SWAA062956Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER INBOARD SIDE. REMOVED AND REPLACED RT AFT FLAP PER MM.Aug 10, 2006 · N335SW · Boeing 7373H4SDR DHL2006745508Structure · crackedRIGHT INBD MIDFLAP AFT LWR CHORD, WBL 100, 2 CRACK INDICATIONS. REMOVED DAMAGED LWR CHORD AT WBL 100 IAW B727 SRM 51-30-2. FAB NEW LWR CHORD SECTION FROM P/N BAC1517-1507 APPROX DIM 4 BY 1 BY 7/8 INCHES IAW B727 SRM 57-50-2 FIGURE 5 AND SRM 51-20-1 FIGURE 2.Aug 9, 2006 · N745DH · Boeing 727224SDR DHL2006745507Flap · delaminatedDELAMINATION OF LEFT INBD MID-FLAP, WBL 140 THRU WBL 243, TE. CLEANED AND PREPPED 8 DISBONDED AREAS ON LT I/B MIDFLAP T/E, APPLIED ADHESIVE AND CURED IAW B727 SRM 51-40-21. CUT OUT DELAMINATED AREAS APPROX 4.2 INCHES BY 5.4 INCHES, FABRICATED FILLER APPROX 4.Aug 9, 2006 · N745DH · Boeing 727224SDR DHL2006745516Flap · delaminatedRT INBOARD MID FLAP SHOW DELAM ARE FROM T/E WBL 130. CUT OUT DELAMINATED AREA ON RT I/B MID FLAP APPROX 4.2" BY 6.2". FABRICATED FILLER APPROX 4.2" BY 6.2" AND DOUBLERS (2 EA) APPROX 3' BY 4.2" FROM 7075-T6 .016, PO 9003142. CLEANED, PREPPED, BONDED, CLEANEAug 9, 2006 · N745DH · Boeing 727224SDR DHL2006745503Angle · crackedLT INBD MID-FLAP AFT LOWER CHORD SHOW 3 CRACK INDICATION WBL 100-120. REMOVED DAMAGED LWR CHORD ANGLE AT LT I/B MIDFLAP AFT LWR AREA WBL100-120 AS PER B727 SRM 51-30-2. FABRICATED NEW CHORD ANGLE BAC1503-100046 14'9"X 2" PO NR 900385 AS PER B727 57-50-2 FIG Aug 9, 2006 · N745DH · Boeing 727224SDR SWAA062931Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.Aug 9, 2006 · N616SW · Boeing 7373H4SDR UIEA200600202Structure · delaminatedDELAM & PUNCTURE DAMAGE TO RT I/B FORE FLAP 60 INCHES FROM I/B EDGE & 12 INCHES FROM TE.Aug 7, 2006 · N409 · Boeing 74747UFSDR UIEA200600201Skin · gouged2 AREAS OF DAMAGE TO UPPER SURFACE LEADING EDGE LT O/B TE AFT FLAP CAUSED BY MID FLAP COVE PANEL SUPPORT BRACKETS, 0.050 DEPTH X .5 DIA. 15 IN FROM O/B EDGE AND 0.040 DEPTH X .5 DIA. 35 IN FROM O/B EDGE, PANEL THICKNESS .120Aug 7, 2006 · N409 · Boeing 74747UFSDR SWAA062895Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.Aug 7, 2006 · N636WN · Boeing 7373H4SDR SWAA062894Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.Aug 7, 2006 · N636WN · Boeing 7373H4SDR SWAA062893Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.Aug 7, 2006 · N636WN · Boeing 7373H4SDR UIEA200600197Skin · delaminatedRT AFT IB FLAP UPPER AND LOWER SIDES OF SKIN HAVE AN AREA OF DELAMINATION. UPPER SIDE IS AT WBL 278.750 AND DAMAGE AREA IS 1.5 INCHES. LOWER SIDE IS AT WBL 272.00 AND DAMAGE IS 2.0 INCHES. ACCOMPLISHED PREPREG 250 DEGREES F. PERMANENT REPAIR OF BOTH AREAS IAWAug 4, 2006 · N809MC · Boeing 747228FSDR SWIA200617031Stringer · crackedLT NACELLE FLAP LOWER SURFACE INTERNAL STRINGER CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT NACELLE FLAP, PN: 120-40327-001.Aug 3, 2006 · N294SW · Emb EMB120ERSDR QXEA200602056Skin · chafedPDX - C4 CHAFE DAMAGE ON LEFT INSIDE FLAP TOP SURFACE. REPAIRED IAW RD 8-51-1022.Aug 3, 2006 · N351PH · Dhav DHC8202SDR SWAA062843Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.Aug 3, 2006 · N656SW · Boeing 7373H4SDR SWAA062833Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FORE FLAP PER MM.Aug 3, 2006 · N636WN · Boeing 7373H4SDR 06FDEA02792Strap · corrodedLHW INBD FLAP OUTBD HINGE (FLAP MOUNTED) OUTBD STRAP FOUND WITH SURFACE CORROSION. SNRM N02107: CORROSION AT LHW INBD FLAP OUTBD HINGE (FLAP MOUNT) OUTBD STRAP REMOVED. FOUND EXCEEDED LIMIT PER CMM 57-52-03 PG 442-444. ORIGINAL THK: 0.260", MATERIAL REMOVEDAug 2, 2006 · N523FE · Doug MD11SDR 06FDEA02778Strap · corrodedRHW INBD FLAP OUTBD HINGE (FLAP MOUNTED) PIVOT OUTBD STRAP FOUND WITH SURFACE CORROSION. SNRM N02122: RT AFT I/B FLAP O/B HINGE PIVOT O/B STRAP SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK: 0.262", REMAINING THAug 2, 2006 · N523FE · Doug MD11SDR SWAA062800Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD CORNER. REMOVED AND REPLACED FLAP ASSY PER MM.Aug 2, 2006 · N320SW · Boeing 7373H4SDR 06FDEA2792Strap · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) OUTBOARD STRAP FOUND WITH SURFACE CORROSION.Aug 2, 2006 · N523FE · Doug MD11SDR 06FDEA2778Strap · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT OUTBOARD STRAP FOUND WITH SURFACE CORROSION.Aug 2, 2006 · N523FE · Doug MD11SDR SWAA062779Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER OUTBOARD SURFACE DISBONDED. REPAIRED FORE FLAP UPPER SURFACE PER SRM.Aug 1, 2006 · N637SW · Boeing 7373H4SDR SWAA062752Bolt · looseAIRFRAME VIBRATION WHEN FLAPS EXTEND FROM 2 TO 5. REMOVED AND REPLACED LT WING INBOARD TRACK FITTING FORE FLAP BOLTS PER MM.Aug 1, 2006 · N525SW · Boeing 7375H4SDR DALA1134569221Skin · dentedDENT ON LOWER SKIN OF RT INBOARD FLAP SRM 57-53-01 VOL I FIG 1.Jul 31, 2006 · N921DN · Doug MD9030SDR UPS06M48259Skin · dentedINSPECTION TYPE:C RT I/B FLAP I/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS RT I/B FLAP I/B SEGMENT LWR SURFACE SKIN DAMAGED REMOVED PER SRM51-31- 01 V.II R.38. RT I/B FLAP I/B SEGMENT LWR SKIN FAB USING 2024-T3 0.040" IAW DWG ARC 2736. NEW FAB SKIN ALODINEJul 31, 2006 · N285UP · Doug MD11FSDR UPS06M48028Skin · dentedINSPECTION TYPE-C RT IB FLAP OB SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. RT IB FLAP OB SEGMENT RMVD IAW CMM57-57-03 REV54. SEGMENT LWR SURFACE DMG SKIN REMOVED IAW SRM51-31-01 VOLII REV38.SEGMENT LWR SKIN FAB USING 2024-T3 0.040 INCH IAW DWG ARC2444. NEWJul 31, 2006 · N285UP · Doug MD11FSDR UPS06M48260Skin · dentedINSPECTION TYPE:C LT I/B FLAP I/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS LT I/B FLAP I/B SEGMENT LWR SURFACE DAMAGED SKIN REMOVED PER SRM 51-31- 01 V.II R.38. LT I/B FLAP I/B SEGMENT LWR SKIN FAB PER DWG ARC 2736 USING 2024T3-0.040". NEW FAB SKIN ALODINEJul 30, 2006 · N285UP · Doug MD11FSDR UPS06M48040Skin · dentedLT I/B FLAP O/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT IB FLAP OB SEGMENT REMOVED PER CMM57-52-03 REV54. LT I/B FLAP O/B SEGMENT LWR SURFACE SKIN DAMAGED REMOVED PER SRM 51-51-01 VOL II REV 38. SEGMENT LWR SKIN FAB USING 2024-T3 0.040" IAW DWG ARC24Jul 30, 2006 · N285UP · Doug MD11FSDR UPS06M48025Skin · wornINSPECTION TYPE-C LT IB FLAP OB SEGMENT LOWER SURFACE OB SIDE EDGE WORN. LT IB FLAP OB SEGMENT LWR OB SIDE SKIN REMOVED IAW SRM51-35-01 VOLII REV38. NEW SKIN FAB USING 2024-T3 0.040 INCH IAW DWG ARC3098. NEW SKIN ALODINE AND PRIME IAW SRM51-21-01 VOLII REJul 30, 2006 · N285UP · Doug MD11FSDR 2006UALA01489Structure · delaminatedRETURNED TO ORD AND CANCELLED DUE TO FLAP DELAMINATION. MAJOR REPAIR ACCOMPLISHED. DETECTED FAILURE OF NR 6 LE SLAT. TE WEDGE REMOVED FOR INSPECTION. INSPECTED LH HORIZ STAB L.E. AND WING UPPER SURFACE AFT OF SLAT TO VERIFY NO DAMAGE TO THE LE HORIZONTAL STJul 29, 2006 · N552UA · Boeing 757222SDR 06FDEA2744Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE BRACKET (WING MOUNTED) FWD ACTUATOR OUTBOARD BORE FOUND WITH CORROSION.Jul 29, 2006 · N523FE · Doug MD11SDR 06FDEA2743Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE BRACKET (WING MOUNTED) LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION.Jul 29, 2006 · N523FE · Doug MD11SDR 06FDEA2742Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE BRACKET (WING MOUNTED) LOWER MOUNT INBOARD BORE FOUND WITH CORROSION.Jul 29, 2006 · N523FE · Doug MD11SDR 06FDEA2741Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE BRACKET (WING MOUNTED) LOWER MOUNT SPOTFACE FOUND WITH SURFACE CORROSION.Jul 29, 2006 · N523FE · Doug MD11SDR SWAA062715Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.Jul 29, 2006 · N684WN · Boeing 7373T0SDR IXXA06SMN254SSkin · nickedDURING ROUTINE C CHECK INSPECTION FOUND LT WING IB FLAP UPPER SKIN REPAIR NICKED AT STATION XW104.000. REMOVED DAMAGED SKIN IAW SRM 51-1-0 PAGE 1, SRM 51-1-21. FABRICATED NEW SKIN (AL 2024 T3 0.040”) CLEANED, TREATED AND PRIMED AREA AND SKIN INTERNAL SURFACEJul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN248SSkin · nickedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING OUTBOARD FLAP LOWER SKIN NICKED FROM STATION XF 415.000 TO STATION XF 425.000. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NEW SKIN (AL 2024 T3 0.032”) AND DOUBLER (AL 2Jul 28, 2006 · N605AL · Doug DC873FSDR UIEA200600191Panel · crackedR/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 4" CRACK AT 3RD SUPPORT ARM I/B OF NR 8 CANOE.Jul 28, 2006 · N506MC · Boeing 7472D3B
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