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 IXXA06SMN042SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT IB FLAP UPPER SKIN HAS INTERN REPAIR XW 105.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 PAGE 1. REMOVED DAMAGED PLATING SEGMENT IAW SRM 57-1-0 PAGE 1, SRM 51-1-21. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.040”) IAW SRM 5Jan 16, 2006 · N606AL · Doug DC873FSDR IXXA06SMN041SSkin · damagedDURING ROUTINE C-CHECK INSPECTION, RIGHT OUTBOARD FLAP UPPER SKIN HAS INTERN REPAIR XF 210.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL2024T3 0.0Jan 16, 2006 · N606AL · Doug DC873FSDR IXXA06SMN039SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, RT OUTBOARD FLAP SKIN LWR PART DENTED AT SEVERAL SPOTS XF 345.000 - XF 404.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICJan 16, 2006 · N606AL · Doug DC873FSDR IXXA06SMN034SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, DENT ON LWR SURFACE RT OUTBOARD FLAP STA XW 404.000 - 406.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2), TR 57-91 DATED 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REJan 16, 2006 · N606AL · Doug DC873FSDR 06FDEA0198Fitting · crackedRIGHT HAND WING - OUTBOARD FLAP SECONDARY UP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP SECONDARY UP STOP CRACKED FITTING. REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 5-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR, AS PER GMM 6-2-100.Jan 16, 2006 · N524FE · Doug MD11SDR SWAA060205Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Jan 16, 2006 · N631SW · Boeing 7373H4SDR ASAA0640033Skin · dentedOKC - FOUND LEFT INBOARD AFT FLAP L/E DENTED AT INBOARD END. REMOVED AND REPLACED SKIN SECTION IAW B737-400 SRM 51-40-02. (M)Jan 15, 2006 · N703AS · Boeing 737490SDR ASAA0640032Skin · delaminatedOKC - RIGHT OUTBOARD AFT FLAP TRAILING EDGE DELAMINATED AT INBOARD SIDE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 4. (M)Jan 15, 2006 · N703AS · Boeing 737490SDR ASAA0640031Skin · delaminatedOKC - FOUND LEFT INBOARD AFT FLAP OUTBOARD T/E WEDGE IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 4. (M)Jan 15, 2006 · N703AS · Boeing 737490SDR ASAA0640030Skin · dentedOKC - FOUND RIGHT INBOARD AFT FLAP HAS SHARP DENT ON THE LOWER SIDE OF FLAP 6 INCHES L/E, 10 INCHES FROM INBOARD END. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER MATERIAL IAW B737-400 SRM 51-70-10 REPAIR 2. (M)Jan 15, 2006 · N703AS · Boeing 737490SDR ASAA0680022Skin · nickedC-CHECK, RT WING OB FORE FLAP CENTER DENTED ON LE PREVIOUS REPAIR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983SDR ASAA0680021Skin · debondedC-CHECK, LT WING OB FLAP CENTER PREVIOUS SKIN REPAIR IS DEBONDED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983SDR ASAA0680020Skin · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED OF LEADING EDGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983SDR 06FDEA0191Hinge Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC1984) AFT MOUNT NR 2 BOLT HOLE FOUND CORROSION. REMOVED AND REPAIR CARRIED OUT PER FEDEX E.A. #1-5750-90720, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAP - RIGHT HAND INBOARD SUPPORT STRUT - CORROSIOJan 15, 2006 · N607FE · Doug MD11SDR 06FDEA0190Hinge Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC1984) AFT MOUNT NR 1 BOLT HOLE FOUND CORROSION. REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-90720.Jan 15, 2006 · N607FE · Doug MD11SDR 06FDEA0188Support Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 2 BOLT HOLE. RT OUTBOARD FLAP ASSEMBLY REPLACED.Jan 15, 2006 · N607FE · Doug MD11SDR 06FDEA0187Hinge Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC1984) OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-90721.Jan 15, 2006 · N607FE · Doug MD11SDR AWXA200600399Skin · delaminatedMCN - DURING C19 CHECK DISCOVERED THE LT OUTBOARD AFT FLAP; INBOARD AFT CORNER HAD SIGNS OF DELAMINATION. MAINTENANCE CUT OUT AND REMOVED THE DAMAGED AREA FROM THE LT OUTBOARD AFT FLAP INBOARD AFT CORNER IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLEJan 13, 2006 · N166AW · Boeing 73733ASDR AALA20060104Spar Cap · corrodedAFW - LEFT HAND INBOARD MAIN FLAP LOWER AFT SPAR LOWER SURFACE AT IFS 19 HAD CORROSION. AREA WAS FOUR INCHES BY 1.7 INCHES WITH A DEPTH OF .027 INCH. VERIFY THE CORROSION WAS COMPLETELY REMOVED. ACCOMPLISH EDDY CURRENT INSPECTION ON BLENDED AREA FOR CRACKS. Jan 13, 2006 · N351AA · Boeing 767323SDR 06FDEA0185Support · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE. REMOVED AND REPLACED AS PER AMM 27- 50-30-4. ADJUSTMENT AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00-5.Jan 13, 2006 · N607FE · Doug MD11SDR A6WA200640042Fitting · wornRT OB FLAP, OB ROLLER GUIDE ON FIXED VANE IS WORN TO MINIMUM LIMITS. MAINTENANCE REMOVED AND REPLACED FLAP FITTING IAW REO. (K)Jan 12, 2006 · N428AW · Cndair CL6002B19SDR IXXA06SMN033SSkin · corrodedDURING C CHECK INSPECT, RT WING INBD FLAP UPPER SKIN CORRODED AT STA XW 1.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED PANEL PLATING IAW DJan 12, 2006 · N722CX · Doug DC872SDR IXXA06SMN030SSkin · corrodedDURING C CHECK INSPECTION, LT OTBD FLAP, T/E INTERNAL PART LWR SKIN CORRODED XF 415.000 XF 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR NR 57-94 DATE 10-01-02. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57Jan 12, 2006 · N722CX · Doug DC872SDR ABXA060025Bolt · brokenINFLIGHT WITH AIRLOAD WHEN FLAPS 12 DEGREES SELECTED, THERE WAS AN AUDIBLE NOISE AND A NOTICEABLE SHUDDER. FOUND ROUND ROLLER HANGER BOLTS BROKEN ON THE RIGHT INBOARD AND RIGHT CENTER AND LEFT INBOARD FLAP ACTUATOR CANOE FITTINGS. REMOVED AND REPLACED BOLTS Jan 12, 2006 · N817AX · Doug DC863SDR AWXA200600311Skin · debondedMCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE RT OUTBOARD AFT FLAP TRAILING EDGE, SEPERATING 8" AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE RT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND COREJan 10, 2006 · N328AW · Boeing 7373B7SDR AWXA200600309Skin · debondedMCN - DURING C24 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD AFT CORNER OF THE RT INBOARD AFT FLAP, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE RT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND COJan 10, 2006 · N328AW · Boeing 7373B7SDR UPS06246088Carriage · corrodedINSPECTION TYPE:C&SI NR 7 FLAP CARRIAGE HAS CORROSION ON I/B FACE AT OB AFT LARGE BEARING HOLE, AND WEAR IN I/B AND OB FWD AND AFT SIDE BEARING BRACKETS ATTACH HOLE. REPLACE CARRIAGE ASSY NR 7 FLAP CARRIAGE ASSY ON I/B SIDE OF RT FLAP REPLACED IAW 27-51-13.Jan 10, 2006 · N938UP · Boeing 727173CSDR UPS06246012Carriage · corrodedC-CHECK AND SI NR 8 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. NR 8 FLAP CARRIAGE REPLACED IAW MM 27-51-13.Jan 10, 2006 · N938UP · Boeing 727173CSDR UPS06246011Carriage · corrodedINSPECTION C-CHECK AND SI SEVERAL AREAS OF CORROSION ON NR 3 FLAP CARRIAGE. NR3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.Jan 10, 2006 · N938UP · Boeing 727173CSDR 06FDEA0136Skin · gougedLEFT WING O/B MIDFLAP UPPER SURFACE GOUGED AT I/B EDGE, APPROX 12 INCHES AFT OF THE LEADING EDGE OF FLAP. *S/D* REPAIRED FLAP PER FED EX EA 7-5710-96547.Jan 10, 2006 · N490FE · Boeing 727200SDR USAA060018Skin · damagedFOUND RT O/B TRAILING EDGE FLAP DAMAGED, O/B TRAILING EDGE FLAP RT SIDE. A 3.5 BY 2.5 DOUBLER INSTALLED IAW SRM 51-70-10. DEFECT SIZE: 1.5" BY .5" DAMAGE ON O/B TRAILING EDGE FLAP RT SIDE.Jan 10, 2006 · N577US · Boeing 737301SDR USAA0618Skin · damagedOUTBOARD TRAILING EDGE FLAP RIGHT SIDE DAMAGED. A 3.5 X 2.5 DOUBLER INSTALLED IAW SRM 51-70-10, DEFECT SIZE: 1.5 X .5 INCH DAMAGE ON O/B TRAILING EDGE FLAP RIGHT SIDE.Jan 10, 2006 · N577US · Boeing 737301SDR USAA0518Structure · damagedRIGHT O/B TRAILING EDGE FLAP - O/B TRAILING EDGE FLAP RT SIDE DAMAGED. A 3.5 X 2.5 DOUBLER INSTALLED IAW SRM 51-70-10, DEFECT SIZE: 1.5 X .5 DAMAGE ON O/B TRAILING EDGE FLAP RT SIDE.Jan 10, 2006 · N577US · Boeing 737301SDR ASAA0640014Flap · chafedLT OB FORE FLAP CHAFED ON L/E 1 INCH FROM IB SIDE. REMOVED AND REPLACED CHAFED SECTION OF L/E IAW SRM. (K)Jan 9, 2006 · N703AS · Boeing 737490SDR ASAA0640013Flap · chafedLT OB MID FLAP CHAFED ON L/E IB SIDE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. (K)Jan 9, 2006 · N703AS · Boeing 737490SDR 06FDEA0099Skin · crackedRT WING OUTBOARD FLAP FOUND 6 CRACKS ON UPPER SKIN FROM STA XOF 543 TO STA XOF 575. BURNICHED AND BLENDED INTERESTED AREAS IAW SRM 57-00-01 FIG 1A SHT 3 VOL 1, CONFIRMED 4 CRACKS STA 549 1 CRACK LONG .300" AT STA 564 FOUND 3EA CRACKS FOR TOTAL LONGEST 1" WOJan 9, 2006 · N302FE · Doug DC1030FSDR SWAA060074Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBD MIDFLAP OUTBD T/E WEDGE DELAMINATED. REMOVED AND REPLACED MIDFLAP PER MM.Jan 7, 2006 · N334SW · Boeing 7373H4SDR SWAA060073Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jan 7, 2006 · N334SW · Boeing 7373H4SDR AWXA200600310Wedge · debondedMCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE LT INBOARD AFT FLAP AT THE OUTBOARD CORNER, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE LT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND CORE IJan 6, 2006 · N328AW · Boeing 7373B7SDR 0601049Skin · damagedREPAIRED RIGHT WING OUTBOARD MID FLAP TRAILING EDGE LOWER SKIN DUE TO SHARP EDGE.Jan 6, 2006 · N767TW · Boeing 737230CSDR IXXA06SMN001SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT OUTBD FLAP T/E UPPER SURFACE HAS NO STANDARD REPAIR, STA XF 403.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94 DATE 10-01-02. REMOVED PANEL PLATING WITH NON STANDARD REPAIR IAW DC8 SRM 57-1-0, DC8 SRM 51-Jan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN025SVane · damagedDURING C-CK, LT WING OTBD FLAP VANE HOLES ELONGATED , XOLDI 6.224. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05587 DATED 12-29-05 SEMAN DWG NR ED-4122 DATED 12-28-05, ED SEMAN NR 2005 1453. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-Jan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN023SSkin · dentedDURING ROUTINE C CHECK INSPECTION, ON RIGHT OUTBOARD FLAP, A SMALL DENT WAS FOUND ON UPPER SKIN AT STA XF 217, DUE TIME CHANGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR 57-94, EO SEMAN 20051460 DATED 12-16-05. REMOVED DAMAGED PLATING IAW DC8 SRM Jan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN005SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP PANEL UPPER SKIN CRACKED 1", AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-5 FIG 1 (SHEET 1-2). REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-5 FIG 1. FAB`D NJan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN004SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT OUTBD FLAP PANEL LWR SKIN DENTED, AT STA XF 420.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-1 FIG 2Q. FABRICATED EXTERNAL REJan 5, 2006 · N722CX · Doug DC872SDR QXEA200600044Skin · chafedPDX - RIGHT OUTBOARD FLAP TOP SKIN CHAFED 2" FROM INBOARD END. REPAIRED IAW RD 8-57-1734, DHC-8-200 SRM 51-20-26.Jan 5, 2006 · N379PH · Dhav DHC8202SDR SWAA060061Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jan 5, 2006 · N383SW · Boeing 7373H4SDR DL76S100647Fitting · unknownWING TRAILING EDGE I/B FLAP, MAIN FLAP COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13. C/W EO 01-073591-12 ME12 AND ME13.Jan 4, 2006 · N139DL · Boeing 767332SDR QXEA200600047Repair · chafedPDX - LEFT OUTBOARD FLAP IS CHAFED ON PREVIOUS REPAIR ON THE TOP SKIN INBOARD END. REPAIRED IAW HORIZON AIR EA 2-52-133, AND DHC-8-200 SRM 51-20-16, 51-40-00 AND SRM 51-20-51.Jan 4, 2006 · N379PH · Dhav DHC8202SDR SWAA060034Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jan 4, 2006 · N352SW · Boeing 7373H4
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