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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS08M53719Intercostal · crackedINSPECTION TYPE:1C LT I/B FLAP O/B HINGE INTERCOSTAL FOUND CRACKED JUST ABOVE O/B ACTUATOR UPPER ATTACHMENT. REMOVED AND REPLACED INTERCOSTAL IAW, SRM 51-31-01 VOL 2 PG 1, 51-21- 01 VOL 2 PG 20.Oct 7, 2008 · N260UP · Doug MD11FSDR ASAA0843662Skin · gougedLT OUTBOARD FOREFLAP L/E IS GOUGED 6 INCHES FROM INBOARD END. REMOVED DAMAGED SKIN, FABBED, HEAT TREATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.Oct 7, 2008 · N764AS · Boeing 7374Q8SDR UPS08M53633Frame · crackedINSPECTION TYPE:1C LT WING O/B FLAP O/B HINGE UPPER FWD CUTOUT FRAME FOR ACCESS PANEL 536GL IS CRACKED AT EDGE. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR DOUBLER IAW SRM VOL 1 57-00-01 PG 6, VOL 2 51-31-01 PG 1.Oct 7, 2008 · N260UP · Doug MD11FSDR UPS08153471Fairing · damagedLEFT WING NR 3 MOVEABLE FLAP TRACK FAIRING DAMAGED PAST LIMITS. ACCOMPLISHED PERMANENT REPAIR / PART REPLACED WITHIN 30 DAYS. PER EO A300-5720-30771.Oct 7, 2008 · N148UP · Airbus A300F4622RSDR UPS08853676Fastener · deformedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT WING INBOARD FLAP INBOARD EDGE WEB EXT REPAIR DOUBLER HAS 2EA DEFORMED FASTENER. REPLACED FASTENERS IAW DC8 SRM 51-01-21.Oct 6, 2008 · N894UP · Doug DC873FSDR 08FDEA04239Structure · crackedLEFT WING INBD MIDFLAP CRACKED 2 PLACES AT CUTOUTS. REMOVED DAMAGED AREA AND FABRICATED NEW ANGLES AND SPLICE REPAIR IAW SRM 57-50-2 AND 51-40-4. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Oct 6, 2008 · N221FE · Boeing 727233SDR 08FDEA04227Fairing · damagedLEFT WING OUTBD FLAP INBD HINGE LOWER BULLET ASSY LOWER SURFACE IS DENTED. REPAIRED LEFT WING OUTBD FLAP HINGE LOWER BULLET ASSY IAW EA 8-5750-123660.Oct 6, 2008 · N550FE · Doug MD1010FSDR 08FDEA04214Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) INBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. REFER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT.Oct 6, 2008 · N613FE · Doug MD11FSDR 08FDEA04212Support Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD (ARC4008) OUTBOARD MOUNTING BORE HOLE BETWEEN FLAP AND HINGE FOUND WITH CORROSION. REFER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT.Oct 6, 2008 · N613FE · Doug MD11FSDR 08FDEA04205Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT INBOARD FACE FOUND PITTING CORROSION. CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 5, 2008 · N613FE · Doug MD11FSDR 08FDEA04208Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD BORE HOLE INNER SURFACE FOUND PITTING CORROSION. CORROSION ON OUTBOARD BORE INNER SURFACE AT RT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09Oct 5, 2008 · N613FE · Doug MD11FSDR DHLA2008745701Skin · delaminatedLT INBD MID-FLAP T/E WEDGE SECTION DISBONDED/HONEYCOMB CORE DELAMINATED AND CRUSHED. ACCOMPLISHED REPAIR TO HONEYCOMB AND SKINS IAW COOPESA EO COO-CMP-2-57-309-08 DATED 10/21/08. REFERENCE FAA FORM 8110-3 DATED 10/29/08 AND ASTAR EVA B257-00127 FOR REPAIR APOct 4, 2008 · N745DH · Boeing 727224SDR ASAA0843937Skin · dentedLT INBD FOREFLAP HAS 2 DENTS 18 INCHES FROM OTBD EDGE ON UPPER CAMBER. PREPPED DAMAGED AREA FABRICATED DOUBLER AND BONDED THE REPAIR IAW SRM 51-70-10 REP 2.Oct 3, 2008 · N771AS · Boeing 7374Q8SDR UPS08853671Flap · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLAP REPLACED ON NR 188423.Oct 3, 2008 · N894UP · Doug DC873FSDR UPS08853670Flap · misrepairedINSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOVED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21.Oct 3, 2008 · N894UP · Doug DC873FSDR UPS08853605Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.Oct 3, 2008 · N894UP · Doug DC873FSDR UPS08853603Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.Oct 3, 2008 · N894UP · Doug DC873FSDR UPS08853553Skin · misrepairedINSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION REPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED.Oct 3, 2008 · N894UP · Doug DC873FSDR ASAA0843596Skin · delaminatedRT WING AFT I/B FORE FLAP DELAMINTATED ON LOWER SURFACE. PREPARED DAMAGED AREA AND PREPARED 3 EACH REPAIR PLYS AND BONDED IAW B737 400 SRM 51 70 16 PG 17.Oct 3, 2008 · N764AS · Boeing 7374Q8SDR 08FDEA04169Hinge Fitting · scratchedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS. SCRATCH MARKS AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE REMOVED AND FOUND WITHIN LIMITOct 2, 2008 · N613FE · Doug MD11FSDR 08FDEA04157Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE PITTING CORROSION REMOVED AS PER EO 1-5750-5008 PAROct 1, 2008 · N613FE · Doug MD11FSDR DL757081273Flap · gougedRIGHT OUTBOARD MAIN FLAP L/E GOUGED ON I/B END. BLENDED OUT GOUGE IAW 757 SRM 51-10-02; OUT OF LIMITS. INSTALLED REPAIR DOUBLER, FILLER, AND CAP END IAW 757 SRMS 51-46-02 AND 57-53-01.Oct 1, 2008 · N648DL · Boeing 757232SDR 08FDEA04167Support Bracket · crackedLEFT WING NR 1 FLAP TRACK - FLAP TRACK TO LOWER TRAILING EDGE PANEL SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED NEW BRACKET REF DWG 65-2289. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 1, 2008 · N485FE · Boeing 727227SDR SWAA085321Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.Oct 1, 2008 · N659SW · Boeing 737301SDR 08FDEA04162Attach Fitting · corrodedLEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 3 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION REMOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMITS. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04161Attach Fitting · corrodedLEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 4 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION REMOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMIT. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04160Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT FITTING AFT BORE HOLE FOUND WITH PITTING CORROSION. FITTING REPAIRED AS PER E.A. NO. 1-5750-122572. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04159Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 INBOARD MID MOUNTING HOLE FOUND CORROSION. FITTING ARC1984 REPAIRED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04158Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 OUTBOARD AFT MOST MOUNTING HOLE FOUND CORROSION. CORROSION IN AFT MOST MOUNTING HOLE FITTING ARC1984 REPAIRED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04156Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD AFT HINGE AFT FITTING AFT BORE HOLE FOUND PITTING CORROSION. FITTING REPAIRED AS PER E.A. 1-5750-122574. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04155Hinge Bracket · corrodedLT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE OUTBOARD NR 3 FOUND WITH PITTING CORROSION. MOUNTING BORE HOLE OUTBOARD NR 3 BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04154Hinge Bracket · corrodedLT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROSION. INBOARD NR 2 MOUNTING BORE HOLE AT LT WING OUTBOARD FLAP ASSY INBOARD HINGE BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAOct 1, 2008 · N613FE · Doug MD11FSDR 08FDEA04153Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC4009 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROSION. CORROSION REMOVED AS PER E.O. 1-5750-5008 PART 1. FINAL HOLE DIAMETER = 0.660", MAXIMUM HOLE DIAMETER = 0.660". CORROSION STILL EXIST.Oct 1, 2008 · N613FE · Doug MD11FSDR DL757081256Flap Track · corrodedCORROSION ON MOUNT SURFACE OF NR 2 FLAP TRACK. DAMAGE WAS MACHINED AND RE-FINISHED.Sep 30, 2008 · N604DL · Boeing 757232SDR 08FDEA04146Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE INNER SURFACE FOUND WITH PITTING CORROSION. CORROSION AT LT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE REMOVED AND FOUND WITHIN LIMIT AS Sep 30, 2008 · N613FE · Doug MD11FSDR 08FDEA04119Hinge · wornLEFT WING INBD FLAP OUTBD HINGE FWD HALF OUTBD FACE LOWER EDGE HAS WEAR MARKS IN 5 SPOTS JUST INBD OF THE NUTPLATES. REMOVED HINGE FAIRING IAW SRM 51-31-01. BLENDED WORN AREAS, FOUND TO REQUIRE REPAIR IAW SRM 51-44-07. BLEND AREA IS 0.065. FABRICATED REPLASep 29, 2008 · N389FE · Doug MD1010FSDR 08FDEA04102Attach Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT POINT INBOARD SURFACE FOUND PITTING CORROSION.Sep 29, 2008 · N613FE · Doug MD11FSDR 08FDEA04090Attach Fitting · scratchedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER OUTBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS.Sep 29, 2008 · N613FE · Doug MD11SDR 08FDEA04077Flap Track · gougedLEFT WING O/B FLAP TRACK I/B EDGE OF TOP FLANGE GOUGED APPROX 14" AFT OF REAR SPAR. BLENDED GOUGE, MATERIAL REMOVED .015 WITHIN LIMITS. MAGNETIC PARTICLE INSPECTED, FLAP PEENED REWORKED AREA, APPLIED ALODINE & PRIMED REF EA 7-5750-118300 P2 PART 1 CLASSIFIEDSep 28, 2008 · N485FE · Boeing 727227SDR USAA920081785Splice Plate · crackedCLT - MAJOR REPAIR - Q5 CHECK, RT WING OUTBOARD MIDFLAP UPPER SURFACE SPLICE PLATE AT THE AFT TRACK ACCESS OPENING IS CRACKED. REPLACED RT WING OUTBOARD MIDFLAP UPPER SURFACE SPLICE PLATE AT THE AFT TRACK ACCESS OPENING IAW B737 SRM 51-20-01 AND BOEING DWG 65Sep 27, 2008 · N432US · Boeing 7374B7SDR F3LA200800628Flap · damagedLINE MX NOTED DAMAGE FROM A BIRD STRIKE ON THE LEADING EDGE OF THE LT WING OUTBOARD FLAP. MX REPAIRED FLAP IAW THE REQUIREMENTS OF A319 SRM 57-53-00, FIGURE 202. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.Sep 26, 2008 · N902FR · Airbus A319111SDR UPS08653448Hinge Fitting · crackedINSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B SUPPORT FITTING FOUND CRACK. CRACK LENGTH .5 INCH APPROX. HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.Sep 26, 2008 · N330UP · Boeing 76734AFSDR ASAA0843575Skin · dentedLEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS AT MID SECTION. PREPPED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.Sep 25, 2008 · N780AS · Boeing 7374Q8SDR ASAA0843574Skin · dentedLEFT WING I/B FOREFLAP UPPER SURFACE HAS DENT AT O/B CORNER. PREPPED DAMAGED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2 PAGE 201.Sep 25, 2008 · N780AS · Boeing 7374Q8SDR SWAA085194Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT LT AFT INBOARD FLAP. REPAIRED PER SWA EA.Sep 25, 2008 · N705SW · Boeing 7377H4SDR UPS08853661Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED INBOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2.Sep 23, 2008 · N894UP · Doug DC873FSDR UPS08853660Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2.Sep 23, 2008 · N894UP · Doug DC873FSDR UPS08153428Rivet · chafedINSPECTION TYPE:5 YR LT WING CENTER FLAP MID CENTER HAVE RIVET HEADS CHAFED. REPAIRED LT WING CENTER FLAP CENTER AREA REF A300-600 SRM.Sep 22, 2008 · N154UP · Airbus A300F4622RSDR 08FDEA03966Vane · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER OUTBOARD HALF FOUND DELAMINATION, APPROXIMATELY 7 INCH BY 37 INCH. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND 'SATISFACTORY'. REPAIR CLASSIFIED AS MINOR PER GMSep 22, 2008 · N606FE · Doug MD11FSDR 08FDEA03965Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON LT CENTER FLAP TOP SKIN, RIB 13-15 AND 20-21. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/229/2008 ISS A, APPROVED BY EA 6-5753-123084.Sep 22, 2008 · N744FD · Airbus A300B4622R
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