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 IPXA09657513Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AFSDR IPXA09657512Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AFSDR IPXA09657505Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AFSDR IPXA09657504Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AFSDR IPXA09657476Hinge Fitting · crackedINSPECTION TYPE:N/A RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.875 INCH. RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02 -2R1 FIG 201 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AFSDR FDEA200909223349Skin · chafedLT WING UPPER SKIN ON CTR FLAP HAS 3 EA CHAFE MARKS ON RIVET HEADS. REMOVED DAMAGE AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57- 50-00 FIG. 205Sep 22, 2009 · N670FE · Airbus A300F4605RSDR IPXA09M57517Skin · delaminatedINSPECTION TYPE:4C DENT WITH DELAM ON RIGHT I/B FLAP VANE LOWER SKIN NEAR MID TRACK. REMOVED DAMAGE, APPLIED AND CURED REPAIR PLIES IAW MD-11 SRM 57-50-80 REPAIR 2, FIGURE 201.Sep 21, 2009 · N278UP · Doug MD11FSDR IPXA09657515Doubler · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP L/E AREA THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.Sep 21, 2009 · N312UP · Boeing 76734AFSDR IPXA09657503Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 21, 2009 · N312UP · Boeing 76734AFSDR IPXA09657502Fairing · delaminatedINSPECTION TYPE:C LEFT WING O/B TRAILING EDGE FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 21, 2009 · N312UP · Boeing 76734AFSDR IPXA09657477Support Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG FLANGE FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.625 INCH. LEFT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 RSep 21, 2009 · N312UP · Boeing 76734AFSDR SWIA200922665Paint · roughAIRCRAFT ROLLED TO RIGHT UNCOMMANDED WHEN FLAPS EXTENDED. (FLT 6140) SMOOTHED NEW PAINT RIDGES ON FLAP.Sep 21, 2009 · N471CA · Cndair CL6002B19SDR IPXA09557433Flap · damagedINSPECTION TYPE:C2 RT OUTBOARD AFT FLAP TRAILING EDGE TIP HAS FIBER DAMAGE AT OUTBOARD FLAP TRACK FAIRING. REMOVED DAMAGE & REPAIRED PER SRM 57-53-01-0I-1 FIG 2 SHEETS 1-10&13 & DETAIL VII ITEM.Sep 21, 2009 · N469UP · Boeing 75724APFSDR SWAA096009Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING I/B TRAILING EDGE MID FLAP O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.Sep 21, 2009 · N609SW · Boeing 7373H4SDR SWAA096007Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MT.Sep 21, 2009 · N505SW · Boeing 7375H4SDR FDEA200909213341Skin · dentedRT WING, INBD FLAP HAS A DENT UPPER SKIN MEASURING .5 DIA. X .06 INCH DEEP. CUT OUT DAMAGE AREA, NDT, NO CRACKS FOUND. FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00, FIG. 205Sep 21, 2009 · N670FE · Airbus A300F4605RSDR FDEA200909213340Skin · chafedRT WING, INBD FLAP UPPER SKIN HAS 2EA CHAFE MARKS .2500 INCH X .1250 INCH AT RIB 8-20 INCHES FROM L/E. CUT OUT DAMAGE AREA, NO CRACKS IAW NDT, FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00, FIG. 205.Sep 21, 2009 · N670FE · Airbus A300F4605RSDR FDEA200909213339Skin · gougedLT WING INBD FLAP TOP SKIN HAS 2 EA GOUGES MEASURING 2 INCHES LONG, PREVIOUSLY COVERED BY PAINT, LOCATION BETWEEN RIBS 7 AND 9, 10 INCHES FROM FRONT SPAR. BLENDED 2EA GOUGES, NDT, NO CRACKS NOTED, CUT OUT DAMAGE FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00Sep 21, 2009 · N670FE · Airbus A300F4605RSDR IPXA09657514Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.Sep 20, 2009 · N312UP · Boeing 76734AFSDR IPXA09M57439Skin · dentedINSPECTION TYPE:4C DENT WITH CRACK ON LOWER SURFACE OF LEFT I/B FLAP VANE, MID SPAN. REMOVED DAMAGE AND APPLIED REPAIR PLIES IAW MD-11 SRM 57-50-80 REPAIR 2 FIG 201 SHEET 1 AND 4.Sep 20, 2009 · N278UP · Doug MD11FSDR SWAA095939Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Sep 20, 2009 · N315SW · Boeing 7373H4SDR ASAA0946716Skin · delaminatedLEFT INBOARD AFT FLAP UPPER SURFACE OUTBOARD END IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.Sep 19, 2009 · N703AS · Boeing 737490SDR IPXA09557434Skin Panel · crackedINSPECTION TYPE:C2 LEFT O/B MAIN FLAP LOWER SURFACE HAS POSSIBLE CRACK 11 INCHES FROM AFT AND 2 INCHES FROM O/B END. REPAIRED MAIN FLAP PER 757-200 PR SRM 57-53-01-2R-4.Sep 19, 2009 · N469UP · Boeing 75724APFSDR IPXA09557550Skin · crackedINSPECTION TYPE:C REF SURVEY SEQUENCE 449-W3-02 EXISTING REPAIR DOES NOT CORRELATE WITH THE VALID REPAIR FOR THIS AREA AS SPECIFIED IN B757 SRM 57-53-01-2R4. REMOVED EXISTING SKIN, HFEC SKIN AND STOP DRILL HOLES IAW NDTM 51-00-19 PT6 AND HOLES IAW NDTM51-00-1Sep 18, 2009 · N449UP · Boeing 75724APFSDR FDEA200909183331Skin · damagedWHILE PERFORMING FLAP OPERATIONAL TEST, BRACKET FOR RT NR 5 SPOILER ACTUATOR CAUSED A PUNCTURE IN UPPER FWD OTBD AREA OF RT CENTER FLAP. DAMAGED AREA 26MM X 24 MM. REMOVED DAMAGED SECTION AT RT CENTER FLAP RIB 27 FWD AND OTBD. FABRICATED REPAIR SKIN, BUTT STSep 18, 2009 · N670FE · Airbus A300F4605RSDR AALA20090924TUL02Wedge · damagedLIGHTNING STRIKE DAMAGE JUST FORWARD OF RIGHT INBOARD FLAP WEDGE AREA. REPAIRED PER SRM 57-01 AND 51-00-014.Sep 17, 2009 · N70401 · Doug DC982SDR FDEA200909173317Angle · crackedLT INBD MID FLAP LWR T/E ON ACT ROD CUTOUT WBL 106 ANGLE IS CRACKED. REMOVED ANGLE CRACKED FROM LT I/B MID FLAP IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 51-40-4 FIG 1 SRM 57-50-2 FIG 5. INSTALLED NEW ANGLE IAW SRM 51-30-2 SRM 57-20-2 INSTALLED LOWER SKISep 17, 2009 · N286FE · Boeing 727233SDR SWAA095902Flap · puncturedDURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.Sep 17, 2009 · N756SA · Boeing 7377H4SDR FDEA200909173318Angle · crackedRT WING INBD MID-FLAP, AFT LWR CHORD ANGLE IS CRACKED IN 2 PLACES AT WBL 100. REMOVED LWR SKIN PANEL IAW SRM 51-30-2. REMOVED LWR CHORD ANGLE ON IB MID FLAP IAW SRM 51-30-2 REV 101. FABRICATED NEW CHORD ANGLE 5 FT X 1.5 INCHES FROM BAC1503-100046 7075 T6, Sep 17, 2009 · N286FE · Boeing 727233SDR USAA2009102292848Flap · delaminatedSAL - Q2 - MAJOR REPAIR - DELAMINATION ON TRAILING EDGE OF LEFT WING INBOARD AFT FLAP. REPAIRED TRAILING EDGE OF LEFT WING INBOARD AFT FLAP IAW B737 SRM 51-70-10.Sep 16, 2009 · N455UW · Boeing 7374B7SDR WRLA20090916200Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF LEFT OUTBOARD T/E FLAP CRACK. ACCOMPLISH EI NR:W2009A57B-1093, REV 00 AND EI NR:W2009A57B-1205.Sep 16, 2009 · N271WA · Doug MD11SDR WRLA20090916199Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF RIGHT OUTBOARD T/E FLAP CRACK. ACCOMPLISH E.I NO:W2009A57B-1092, REV 00 AND E.I NR :W2009A57B-1207 REV 00.Sep 16, 2009 · N271WA · Doug MD11SDR A6WA299040585Vane · dentedDENT ON LT WING, INBD FLAP VANE L/E BTWN WS 75.27 TO WS 97.70 LT WING, INBD FLAP VANE L/E REPAIRED IAW SRM 57-52-00, PAGE 201. DUE TO DENT FOUND OUT OF LIMITSIAW SRM 57-52-00, FIG 101 (PAGE 102) REPAIR NR 01. (K)Sep 16, 2009 · N405AW · Cndair CL6002B19SDR FDEA200909163304Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASep 16, 2009 · N670FE · Airbus A300F4605RSDR FDEA200909163303Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASep 16, 2009 · N670FE · Airbus A300F4605RSDR FDEA200909163302Skin · chafedRT WING INBD FLAP UPPER SKIN HAS CHAFE MARK APPROX 1 SQUARE INCH AT 10 INCHES FROM INBD SIDE AND 20 INCHES FROM L/E. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 57-50-00, FIG 205.Sep 16, 2009 · N670FE · Airbus A300F4605RSDR IPXA09M57429Skin · dentedINSPECTION TYPE:4C SMALL DENT ON UPPER SKIN I/B FLAP LT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-00-01 FIG 201 REPAIR 1 SHEET 1 OF 4.Sep 15, 2009 · N277UP · Doug MD11FSDR SWAA095899Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Sep 14, 2009 · N391SW · Boeing 7373H4SDR SWAA095876Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.Sep 14, 2009 · N368SW · Boeing 7373H4SDR IPXA09557362Wedge · damagedINSPECTION TYPE:N/A LT WING O/B TRAILING EDGE FLAP WEDGE HAS A HOLE. REPAIRED PER EO-B757-5750-34923-A.Sep 13, 2009 · N421UP · Boeing 75724APFSDR A6WA200940611Fitting · wornRT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND WITH ROLLER WEAR DAMAGE. RT WING, OTBD FLAP ALIGNMENT FITTING, REPAIRED IAW REO 601R57-51-149, REV NC. (K)Sep 12, 2009 · N425AW · Cndair CL6002B19SDR FDEA200909123315Spar · crackedRT WING LWR T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED LWR CHORD SECTION IAW DWG 27-57-038 REV C & DOUBLER IAW DWG SR27-57-038 REV C. TRIMMED OUT INBD AREA IAW DWG SR27-57-038, REV C & FABRICATED 2 ANGLES & HEAT TREATED ANGLES TO T6 IAW ER NR 2Sep 12, 2009 · N286FE · Boeing 727233SDR FDEA200909123314Spar · crackedLT WING LOWER T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED DOUBLER, CUT-OUT LOWER CHORD, FABRICATED NEW WEB, 2 EACH ANGLES, NEW LWR CHORD, NEW DOUBLER, STRAPS, 2 FILLERS AND INSTALLED PARTS IAW DWG SR27-57-038 REV C.Sep 12, 2009 · N286FE · Boeing 727233SDR A6WA200940571Lug · corrodedLT WING FLAP HINGE BOX AT WS 80.50 AFT LUG CORRODED UNDER BUSHING INBD LT WING FLAP HINGE BOX AT WS 80.50 AFT LUG INBD REPAIRED IAW REO 601R57-21-1164. (K)Sep 11, 2009 · N467AW · Cndair CL6002B19SDR QXEA2009091400678Skin · chafedRIGHT FUSELAGE SKIN CHAFED FROM AFT WING FLAP STAB FAIRING. REMOVED AFT INBOARD , TOP RIGHT WING PANNEL FOR ACCESS IAW SRM 51-42-21. ORINGIAL MATERIAL .063, BLENDED AREA TO DEPTH .012, WIDE .8 LENGTH 1.2 INCHES. SECONDARY STRUCTURE (APRON) BETWEEN FS 820 ANSep 11, 2009 · N603QX · Cndair CL6002C10SDR QXEA2009091400677Vane · chafedRIGHT INBD FLAP VANE CHAFED ON TOP TRAILING EDGE. BLENDED CHAFE AT RT INBD FLAP VANE AT TOP OF TRAILING EDGE. FLAP VANE TOP T/E IS .050", BLENDED AREA OUT .002", REMAINING THICKNESS IS .048". BLENDED AREA WITHIN LIMITS OF SRM 57-52-02. ALL WORK DONE IAW SSep 11, 2009 · N603QX · Cndair CL6002C10SDR RU3A0915Hinge Fitting · chafedLT OUTBOARD FLAP (INBOARD HINGE FITTING ON OUTBOARD SIDE) HAS SEVERE CHAFING DAMAGE (CAUSED BY AFT ROLLER BEARING) NEARLY TO THE POINT OF FAILURE.Sep 11, 2009 · N77 · Beech 300BEECHSDR RU3A0914Attach Fitting · wornRT OUTBOARD FLAP (INBOARD HINGE FITTING ON OUTBOARD SIDE) HAS BEARING WEAR. FLAP BEARING HAS CHAFED FLAP HINGE FITTING ALMOST THROUGH THE THICKNESS OF THE METAL. FLAP ROLLER BEARING ATTACH FITTING FAILURE WAS IMMINENT.Sep 11, 2009 · N77 · Beech 300BEECHSDR IPXA09B57331Flap · delaminatedINSPECTION TYPE:C LT WING I/B AFT FLAP L/E DENT / DELAM 147.5 INCHES FROM O/B EDGE INT REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5.C FIG 2 REV 53.Sep 11, 2009 · N574UP · Boeing 74744AFSDR IPXA09M57440Skin · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ 284-W4-01 RIGHT WING O/B FLAP LOWER SKIN REPAIR DOES NOT CORRELATE WITH SRM. REPAIRED IAW IPXA EO MD11-5750-35012-B AND SAA EA 011-5754-01-A2028 REF IPXA RCD 343248.Sep 10, 2009 · N284UP · Doug MD11F
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