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 05FDEA04084Hinge Bracket · crackedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT UPPER LINK FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-90703 (TITLE: WINGS LEFT HAND WING TRAILING EDGE FLAP, INBOARD HINGE, TENSION STRAP - COMPLIANCE WITH BOEING S/B 57- 10). REPAIR CLASSIFIED Dec 2, 2005 · N578FE · Doug MD11SDR 05FDEA04079Repair · unknownFOUND RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH294 DIMENSION 4.5" BY 8". PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 RESTORED PAINT ON STRIPPED AREDec 2, 2005 · N302FE · Doug DC1030SDR 05FDEA04078Repair · unknownRT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 210 DIMENSION 5 INCH BY 3 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 2P RESTORED PAINT ON STRIPPED AREA Dec 2, 2005 · N302FE · Doug DC1030SDR ASAA0540700Structure · brokenOKC - FOUND LEFT OUTBOARD AFT FLAP OUTBOARD CORNER BENT UP AND BROKEN. REPAIRED DAMAGED AREA, IAW B737-400 SRM 51-70-10 PAGES 213, 221, 238, AND 249. (M)Dec 1, 2005 · N796AS · Boeing 737490SDR SWAA053857Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Nov 30, 2005 · N637SW · Boeing 7373H4SDR SWAA053820Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING OTBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Nov 30, 2005 · N310SW · Boeing 7373H4SDR LR7A05197Fitting · crackedDURING B-2 CHECK PER HB2703, FOUND FLAP TRACK FITTING CRACKED AT FLAP STA 241, LT OWS231. REPLACED FITTING IAW SMP583 CH 51-60 AND 51-70. NR 2031.Nov 29, 2005 · N406LC · Lkheed 382GSDR SWAA053814Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Nov 29, 2005 · N649SW · Boeing 7373H4SDR 05FDEA04026Support Angle · chafedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE CENTER SUPPORT ANGLE STRUCTURE FOUND CHAFED. REMOVED AS PER CMM 20-11-02 AND FOUND WITHIN DRAWING ARC2126 DESIGN LIMIT. ORIGINAL THICKNESS = 0.180", REMAINING THICKNESS = 0.175", MATERIAL REMOVED = 0.005". RNov 29, 2005 · N524FE · Doug MD11SDR 05FDEA04023Flap Track · corrodedRIGHT WING INB FLAP OUTB TRACK FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED PITTING , FABRICATED AND INSTALLED REPAIR BUSHING AND FINAL REAM ID IAW BAC OHM57-40-01.Nov 29, 2005 · N220FE · Boeing 727200SDR 05FDEA04022Flap Track · corrodedLEFT WING OUTBOARD FLAP OUTBOARD TRACK, FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED ALL PITTING FROM BORE "D ", FABRICATED AND INSTALL REPAIR BUSHING AND FINAL REAM ID, IAW BOEING OHM 57-40-01 SIGNED BY TIMCO MECH NR 4951 AND QC 280, CARD N0084Nov 29, 2005 · N220FE · Boeing 727233SDR 05FDEA04008Flap Track · corrodedLEFT WING INBOARD FLAP OUTBOARD TRACK AFT MOUNT BOLT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING FROM BORES G AND F WITH FINAL DIAMETER OF .3765 INCH FOR HOLE F AND .3765 INCH FOR HOLE G. FABRICATED REPAIR BUSHINGS FROM 15-5 PH STEEL PO 453539Nov 29, 2005 · N486FE · Boeing 727227SDR 05FDEA04004Skin · damagedDURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPECTION, NO CRACK FOUND. PERFORMED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.Nov 29, 2005 · N571FE · Doug MD1010FSDR 05FDEA04003Skin · damagedLT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECTION, NO CRACK FOUND. PERFORM DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.Nov 29, 2005 · N571FE · Doug MD1010FSDR QXEA200501757Flap Track · damagedPDX - RIGHTHAND WING NR 2 FLAP TRACK UPPER SURFACE OF LOWER TRACK HAS DIVOT, 8 INCHES FROM FORWARD END. REPAIRED IAW RD 8-57-986.Nov 28, 2005 · N374PH · Dhav DHC8202SDR 05FDEA03970Repair · misinstalledRIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 147 TO 153, YIFH 60 TO 63 FOUND WITH EXISTING DENT REPAIR. EVALUATED AND FOUND REPAIR NOT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RIGNov 28, 2005 · N524FE · Doug MD11SDR 05FDEA03969Repair · misinstalledRIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 EVNov 28, 2005 · N524FE · Doug MD11SDR 05FDEA03968Repair · misinstalledRIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 219 TO 225, YIFH 46 TO 52 FOUND WITH EXISTING REPAIR. EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RINov 28, 2005 · N524FE · Doug MD11SDR 05FDEA03976Repair · properLT WING OUTBOARD FLAP LOWER SKIN FOUND DOUBLER 35.50 X 4.50 INCHES XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.Nov 28, 2005 · N302FE · Doug DC1030SDR 05FDEA03977Repair · properLT WING OUTBOARD FLAP UPPER SKIN FOUND A DOUBLER 35 X 4.25 INCHES AT STA XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.Nov 28, 2005 · N302FE · Doug DC1030SDR SWAA053795Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT EDGE. REPAIRED AFT FLAP PER SRM.Nov 27, 2005 · N354SW · Boeing 7373H4SDR QXEA200501763Fastener · damagedPDX - LEFTHAND WING NR 4 FLAP TRACK INBOARD SIDE OF FLAP TRACK HAS EIGHT FASTENER COLLARS THAT HAVE BEEN BLENDED ON. REPLACED IAW DHC-8-202 SRM 51-40-00 AND RD 8-51-102.Nov 26, 2005 · N374PH · Dhav DHC8202SDR QXEA200501759Flap Track · corrodedPDX - LEFT HAND NR 4 FLAP TRACK HAS PITTING CORROSION ON INBOARD CENTER OF TRACK. REPAIRED IAW RD 8-57-988.Nov 26, 2005 · N374PH · Dhav DHC8202SDR SWIA200515879Flap · icedFLAPS FAIL CAUTION MSG AFTER LANDING DURING FLAP RETRACTION. REMOVED SNOW AND ICE AS REQUIRED. CYCLE FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD.Nov 26, 2005 · N457SW · Cndair CL6002B19SDR QXEA200501760Skin · gougedPDX - LEFTHAND OUTBOARD FLAP UPPER INBOARD SKIN IS GOUGED YW173.00. REPAIRED IAW RD 8-57-1022.Nov 25, 2005 · N374PH · Dhav DHC8202SDR QXEA200501758Flap Track · corrodedPDX - LEFT HAND NR 5 FLAP TRACK HAS PITTING CORROSION ON OUTBOARD CENTER OF TRACK. REPAIRED IAW RD 8-57-989.Nov 25, 2005 · N374PH · Dhav DHC8202SDR 05FDEA03951Flap · corrodedSNRM N0963: LH OUTBD FLAP AFT INBD HINGE BRACKET ATTACH FITTING INBD CENTER BORE FOUND CORRODED. CORRECTIVE ACTION: SNRM N0963: LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT Nov 23, 2005 · N606FE · Doug MD11SDR 05FDEA03950Support Fitting · corrodedCRACK FOUND AT LT WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE MOST OUTBD HOLE DURING HFEC INSPECTION. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIENov 23, 2005 · N606FE · Doug MD11SDR 05FDEA03949Hinge Bracket · corrodedLT WING OUTBD FLAP INBOARD HINGE BRACKET OUTBD CENTER ATTACH HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.Nov 23, 2005 · N606FE · Doug MD11SDR 05FDEA03948Skin · corrodedSNRM N1008: CRACK FOUND AT RH WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE #2 HOLE FROM INBD DURING HFEC INSPECTION. CORRECTIVE ACTION: SNRM N1008: RIGH HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMNov 23, 2005 · N606FE · Doug MD11SDR 05FDEA03947Skin · corrodedSNRM N0596: RH WING OUTBD FLAP AFT INBD HINGE BRACKET FWD OUTBD AFT ATTACH HOLE FOUND WITH CORROSION. CORRECTIVE ACTION: SNRM N0596: RIGHT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED ONov 23, 2005 · N606FE · Doug MD11SDR SWAA053759Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Nov 22, 2005 · N392SW · Boeing 7373H4SDR 05FDEA03937Flap Track · corrodedRIGHT WING O/B FLAR I/B TRACK AFT MOUNT CENTER BOLT HOLE HAS CORROSION. REPAIRED HOLE IAW BOEING OHM 57-40-01. REMOVED CORROSION FROM BORE IAW BOEING OHM 57-40-01. MAG PARTICLE INSPECTION OF BORE IAW BOEING OHM57-40-01. FABRICATED AND INSTALLED BUSHING INov 22, 2005 · N486FE · Boeing 727227SDR 05FDEA03936Flap Track · corrodedRIGHT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNTING BOLT HOLES, BORES HAVE CORROSION. REAMED HOLES 2 EACH TO REMOVE CORROSION WITHIN LIMITS IAW. BAC OHM 57-40-01 NO CORROSION NOTED. FABRICATED AND CAD PLATED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW OHM Nov 22, 2005 · N486FE · Boeing 727227SDR 05FDEA03935Flap Track · corrodedLEFT WING INBOARD FLAP TRACK FORWARD AND AFT MOUNTING FLANGES HAVE CORROSION. MACHINED FWD MOUNT PAD TO .250 REMOVING .020 TO REMOVE CORROSION. AFT PAD TO .260 REMOVING .015 TO REMOVE CORROSION IAW BAC OHM 57-40-01 PAGE 411 FIGURE 402. PERFORMED MAG PARTNov 22, 2005 · N486FE · Boeing 727227SDR CA051124008Rib · cracked(CAN) DURING MAINTENANCE CHECK THE RIB WAS FOUND TO BE CRACKED IAW ATTACHMENT. RIB WAS REPLACED.Nov 21, 2005 · Dhav DHC6SDR ERA2005F00007Skin · delaminatedFOUND WHILE AIRCRAFT WAS UNDERGOING C1-CHECK. DELAMINATION OF COMPOSITE MATERIAL IN THE LT OB FLAP LOWER SURFACE BETWEEN YW327.40 AND YW404.10. REPAIRED IAW RD. (K)Nov 18, 2005 · N882EA · Dhav DHC8103SDR DHL2005765525Skin · chafedFOUND RT WING O/B T/E FORE FLAP, I/B END AT TOP SKIN HAS 2 CHAFE MARKS. FABRICATED AND INSTALLED REPAIR DOUBLER 7.5" BY 4" FROM 2024-T3 .063 IAW B727 SRM 51-10-2 AND B727 MM 51-20-11 AND SRM 51-30-2.Nov 18, 2005 · N765AT · Boeing 727264SDR 05FDEA03897Skin · misdrilledLT IB TE MIDFLAP LWR AFT SKIN HAS NUMEROUS FASTENER HOLES DOUBLE DRILLED OR EXCESSIVELY COUNTERSUNK, O/B OF O/B FLAP TRACK. REPAIRED LT IB MIDFLAP LOWER AFT SKIN PER SRM 51-40-2.Nov 18, 2005 · N466FE · Boeing 727200SDR 05FDEA03893Repair · properLT WING INBOARD FLAP FOUND A DOUBLER 6" BY 5" ON UPPER SKIN AT STA XIFH 288. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VONov 18, 2005 · N302FE · Doug DC1030SDR 05FDEA03885Repair · properFOUND LT WING OUTBOARD FLAP LWR SKIN FOUND A DOUBLER 6" BY 4" AT XOF 467. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3.Nov 18, 2005 · N302FE · Doug DC1030SDR 05FDEA03883Repair · properRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENS.8.5 X 5 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3, RESTORED PAINT ON STRIPPED AREA INov 18, 2005 · N302FE · Doug DC1030SDR 05FDEA03864Repair · unknownLT WING OUTBOARD FLAP UPPER SKIN FOUND A FLUSH DOUBLER 39.25 X 36.50 INCHES WITH INSIDE SPLICES BETWEEN XOF 593 AND XOF 557. REMOVED T/E SECTION OF O/B FLAP IN ORDER TO ACCOMPLISH REPAIR IAW DRAW ARC 453. INSTALLED REPAIR IAW FED EX EA 8-5750-88900 AND SRM 5Nov 18, 2005 · N302FE · Doug DC1030SDR DHL2005803514Panel · wornLT INBOARD FLAP UPPER PANEL PLATING WORN 2 INCHES APPROX, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.025) AND BONDED FINGER DOUBLNov 17, 2005 · N803DH · Doug DC873SDR SWAA053696Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING T/E INBD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Nov 17, 2005 · N648SW · Boeing 7373H4SDR 05FDEA03848Repair · unknownRIGHT WING OUTBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN FROM STA XOF 560 TO STA XOF 599 DIMENSIONS 36.5 X 39 INCHES. REPAIR ACCOMPLISHED WITH EA FEDEX.Nov 17, 2005 · N302FE · Doug DC1030SDR DHL2005803507Skin · wornITEM REF NR 038897: LT WING INBD FLAP PLATING UPPER PART WORN 1" XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-7-1 FIG. 1 ITEM D. CLEANED, TNov 16, 2005 · N803DH · Doug DC873SDR DHL2005803505Skin · wornITEM REF NR 032704: RT OUTBD FLAP UPPER SURFACE WORN (STA XF 203.000-210.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 4, TR 57-94. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG. 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-Nov 16, 2005 · N803DH · Doug DC873SDR AWXA200501543Skin · debondedMCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT INBOARD FORE FLAP 13 INCHES FROM THE INBOARD END FROM WBL 83.74R TO WBL 84.74R. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE, REPAIRNov 14, 2005 · N164AW · Boeing 73733ASDR AWXA200501542Skin · debondedMCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE RT OUTBOARD FORE FLAP 13 INCHES FROM THE INBOARD END FROM WS 301R TO WS 307.5R. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE, REPAIR SENov 14, 2005 · N164AW · Boeing 73733A
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