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 QXEA2009071300526Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-82. REMOVED PAINT FROM CHAFE AREA AT YW-82 ON LT INBD FLAP IAW SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01 PARA 1-6B(5). HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PARTJul 10, 2009 · N400QX · Bombdr DHC8402SDR QXEA2009071300525Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-98.6. REMOVED PAINT FROM CHAFE AREA AT YW-98.6 ON LT INBD FLAP IAW SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01 PARA 1-6B(5). HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM Jul 10, 2009 · N400QX · Bombdr DHC8402SDR FDEA200907102581Skin · misrepairedRT WING INBD FLAP AFT OTBD SEGMENT LWR SURFACE FOUND 1EA EXISTING DOUBLER NOT REPAIRED IAW SRM AT XIFH 276. REPAIRED AS PER SRM57-10-00 FIG3 VOL1 REV 40.Jul 10, 2009 · N604FE · Doug MD11FSDR QXEA2009071300524Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-117.5. REMOVED PAINT FROM CHAFE AREA AT YW-117.5 ON LT INBD FLAP IAW SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01. HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PART 6, 51-Jul 10, 2009 · N400QX · Bombdr DHC8402SDR QXEA2009071300523Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-150. REMOVED PAINT FROM CHAFE AREA AT YW-150 ON LT INBD FLAP IAW Q400 SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01. HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PART 6, 5Jul 10, 2009 · N400QX · Bombdr DHC8402SDR FDEA200907102576Skin · damagedFOUND ON RT INNER FLAP SB 57-6098 NOT PROPERLY INSTALLED AND AFTER SKIN REMOVAL FOUND DAMAGED/ELONGATED HOLES AND GAUGES IN THE STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND REPAIR THE DAMAGES IAW RAS/FOK/138/2009 ISS. B, APPROVED BY EA 6-5750-Jul 10, 2009 · N751FD · Airbus A300B4622RSDR FDEA200907102575Rib · damagedFOUND ON LT INNER FLAP DURING ACCOMPLISHMENT OF EO 6-5750-7-5000, DAMAGED HOLES IN FLAP STRUCTURE AFTER RIB 7 WAS REMOVED. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR OF DAMAGES IAW RAS/FOK/135/2009 ISS.D, APPROVED BY EA 6-5750-131241.Jul 10, 2009 · N751FD · Airbus A300B4622RSDR FDEA200907102574Rib · damagedFOUND ON RT INNER FLAP DURING ACCOMPLISHMENT OF EO 6-5750-7-5000 DAMAGED HOLES IN FLAP STRUCTURE AFTER RIB 7 WAS REMOVED. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR OF DAMAGES IAW RAS/FOK/133/2009 ISS.D, APPROVED BY EA 6-5750-129178.Jul 10, 2009 · N751FD · Airbus A300B4622RSDR FDEA200907102573Skin · chafedFOUND ON LT INNER FLAP UPPER AND LOWER SKIN CHAFING MARKS, DENT AND SCRATCHES. RIB 12-19 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK AT RIB 12/FRONT SPAR -STR.2.1 , CUT OUT THE SKIN AT RIB 12 /STR.2.1-2.2 AND PERFORM REPAIR IAW SRM 57-50-00 PARA 4.E, CUTOJul 10, 2009 · N751FD · Airbus A300B4622RSDR FDEA200907102572Structure · damagedFOUND ON LT INNER FLAP SB 57-6098 NOT PROPERLY INSTALLED AND AFTER SKIN REMOVAL FOUND DAMAGED/ELONGATED HOLES AND GOUGES IN THE STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND REPAIR THE DAMAGES IAW RAS/FOK/148/2009 ISS. D, APPROVED BY EA 6-5750-1Jul 10, 2009 · N751FD · Airbus A300B4622RSDR WRLA2009190AVane · debondedDURING C-CHECK AT TPE, MAINTENANCE DISCOVERED TWO DISBOND AREAS ON THE RT INBOARD FLAP VANE LOWER SKIN MEASURING 21 X 15 INCHES BETWEEN XIFH 190.8 AND 205.8 AND 39 X 12 INCHES BETWEEN XIFH 216.8 AND 255.8. REFERENCE EGAT NRC NR U07004. REPAIRED DISBONDED AREJul 9, 2009 · N381WA · Doug MD11FSDR FDEA200907092555Attach Fitting · corrodedRT WING - OTBD T/E FLAP VANE FOUND ATTACHMENT FITTING 'F' (NR 4 FITTING FROM INBD) HOLE CORROSION. REWORKED AS PER E.A. 1-5750-132681, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 9, 2009 · N572FE · Doug MD11SDR FDEA200907092554Support · corrodedLT WING OTBD T/E FLAP AT FLAP VANE FOUND VANE ATTACHMENT FITTING "E" (NR 2 FITTING FROM INBD) CORRODED. REWORKED AS PER E.A. 1-5750-132680. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.Jul 9, 2009 · N572FE · Doug MD11SDR FDEA200907092553Support Fitting · corrodedLT WING OTBD FLAP VANE NR 3 SUPPORT FITTING FWD FASTENER HOLE FOUND CORRODED. REPAIRED AS PER EA1-5750-132677. (MAJOR REPAIR)Jul 9, 2009 · N604FE · Doug MD11FSDR FDEA200907092552Tee Fitting · corrodedLTW OTBD FLAP, FLAP VANE NR 4 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132678. (MAJOR REPAIR)Jul 9, 2009 · N604FE · Doug MD11FSDR FDEA200907092551Tee Fitting · corrodedLTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132676. (MAJOR REPAIR)Jul 9, 2009 · N604FE · Doug MD11FSDR FDEA200907092550Tee Fitting · corrodedRTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132679. (MAJOR REPAIR)Jul 9, 2009 · N604FE · Doug MD11FSDR UIEA200900037Skin Panel · corrodedRT WING INBOARD AFT FLAP UPPER EXTERNAL SURFACE PANEL HAS EVIDENCE OF CORROSION AT WBL 259.30 AND 12 INCHES FROM TRAILING EDGE. CUT OUT AREA OF CORROSION AND PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 57-50-02 FIG 5, SHEET 4 AND 10 AND SRM 51-40-06. AJul 9, 2009 · N540MC · Boeing 747243BSDR FDEA200907082534Rib · corrodedFOUND CORROSION ON RT OTBD FLAP RIB 27 REPAIR PERFORMED BY REPLACEMENT OF RIB 27 IAW RAS/FOK/111/2009 ISS. A, APPROVED BY EA 6-5750-129187.Jul 8, 2009 · N751FD · Airbus A300F4605RSDR DHLA2009873591Skin · dentedLEFT I/B FLAP UPPER EXTERNAL SKIN DENTED AT STA. XW106.000 AND WORN (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 1 PG. 2 AND SRM 57-1-0 PG.1. REMOVED FASTENERS AND DAMAGED SKIN IAW SRM 51-1-21. FABRICATED NEW SKIN IAW SRM 57-7-1 FIG. 1 PG. 2 ITEJul 7, 2009 · N873SJ · Doug DC873FSDR IPXA09656660Fairing · delaminatedINSPECTION TYPE:C RIGHT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jul 7, 2009 · N308UP · Boeing 76734AFSDR SWAA094294Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FLAP PER SRM.Jul 7, 2009 · N734SA · Boeing 7377H4SDR FDEA200907072515Skin · gougedRT OTBD FOREFLAP WBL 442, GOUGE FWD OF ATTACH FITTING BURNISHED AREA IAW SRM 51-10-1 AND FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 23. REMOVED FOREFLAP BRACKET FOR ACCESS IAW SRM 51-30-4, FIG 4. CUT DAMAGED AREA IAW SRM 57-50-4, FIG 4 FABRICATED 2 EA DOUBLERS Jul 7, 2009 · N284FE · Boeing 727233SDR IPXA09656683Fairing · delaminatedINSPECTION TYPE:7C LEFT WING - OUTBOARD T/E FLAP L/E INBOARD FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1), FIG 5, REV 44.Jul 6, 2009 · N308UP · Boeing 76734AFSDR IPXA09656652Fairing · delaminatedINSPECTION TYPE:7C LEFT WING - O/B FLAP L/E MID FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1), FIG 5, REV 44.Jul 6, 2009 · N308UP · Boeing 76734AFSDR QXEA2009070900511Doubler · damagedPDX - C5 - THERE ARE MULTIPLE SPOTS OF CHAFING DAMAGE ALONG THE TOP MIDDLE PORTION OF THE LT OUTBOARD FLAP. FOUND DAMAGE TO BE IN PREVIOUS REPAIR. DRILLED OUT PREVIOUS REPAIR AND FABRICATED NEW REPAIR DOUBLER FROM 2024-T3 .040 INCH ALUMINUM REF PREVIOUSLY ISJul 6, 2009 · N400QX · Bombdr DHC8402SDR FDEA200907062488Vane · delaminatedRIGHT WING INBOARD FLAP VANE LOWER AND UPPER SURFACE FOUND DELAMINATED AT BETWEEN NR 1 AND 2 VANE TRACK AREA. REMOVED AND REPLACED IAW AMM 27-50-22-4, REVISION 64. RT INBD FLAP VANE ADJUSTMENT AND TEST IAW WORK CARD NR E1-5750-7-5003 C3 PART 2.Jul 6, 2009 · N617FE · Doug MD11FSDR IPXA09656564Skin · dentedINSPECTION TYPE:N/A RIGHT O/B FLAP TWO AREAS OF DENTS ON UPPER AND LWR SURFACE. REPAIRED REF EO-B767-5750-32516-B.Jul 6, 2009 · N327UP · Boeing 76734AFSDR IPXA09156649Doubler · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 127-W3-01 REPAIR DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER A300-600 SRM 57-50-00 FIG 205 PARA 4E.Jul 5, 2009 · N127UP · Airbus A300F4622RSDR IPXA09156648Doubler · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 127-W3-02 REPAIR DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER EA 300-5753-0 1-A1902.Jul 5, 2009 · N127UP · Airbus A300F4622RSDR IPXA09156633Doubler · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQ 127-W3-01 REPAIR DOUBLER IS GOUGED. REMOVED, FABBED, AND INSTALLED REPAIR DOUBLER IAW A300-SRM 57-50-00 FIG 205, PARAGRAPH 4E.Jul 5, 2009 · N127UP · Airbus A300F4622RSDR IPXA09M56556Skin · gougedLT WING FLAP LOWER SURFACE DENT AND GOUGE. REPAIR IAW EO-MD11-5750-33810-B.Jul 5, 2009 · N252UP · Doug MD11FSDR IPXA09656563Wedge · damagedINSPECTION TYPE:N/A RIGHT O/B FLAP T/E WEDGE DAMAGED. REPAIR PER EO B767-5750-32516-B.Jul 5, 2009 · N327UP · Boeing 76734AFSDR IPXA09656654Hinge Fitting · crackedINSPECTION TYPE:7C LEFT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FIG FOUND CRACKED. LEFT WING I/B MAIN FLAP I/B AFT FLAP HINGE FIG REPAIRED AS PER SRM 57-53-02- 2R1, FIG 201, REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075TJul 4, 2009 · N308UP · Boeing 76734AFSDR WX0A070345Skin · dentedLT INBOARD FLAP LOWER SURFACE - 2 DENTS. WING STA XF41-48, 6X7 INCH, 0156 DEEP & STA XF55 TO XF59 51/4 X 4, .200 DEEP. CUTOUT DENTED AREA - FABED REPLACEMENT SKIN & REPAIR DOUBLER - TREATED - PRIMED REPAIR PARTS & INSTALLED IAW SRM 51-70-6 & 51-70-3Jul 4, 2009 · Doug MD83SDR ASAA0946217Skin · dentedLT T/E INBD AFT FLAP UPPER SKIN AT WBL 92.8 FWD OF T/E IS DENTED. REMOVED DAMAGED SECTION FABRICATED TREATED PRIMED AND BONDED SKIN AND DOUBLER REPAIR. IAW SRM.Jul 3, 2009 · N796AS · Boeing 737490SDR UALA2009070601913Bullnose · damagedRT WING OUTBOARD T/E MIDFLAP BULLNOSE IS DAMAGED. FABRICATED AN EXTERNAL DOUBLER FROM .032 INCH 2024-T3 EXTENDING FROM THE AFT UPPER ROW OF BULLNOSE ATTACH FASTENERS TO THE AFT LOWER ROW OF ATTACH FASTENERS AND SPANWISE A MIN OF 3 FASTENER ROWS ON EITHER SIDJul 3, 2009 · N116UA · Boeing 747422SDR IPXA09M56762Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE NUMBER 281-W3-04 LT WING INBOARD FLAP UPPER SKIN BETWEEN STA XIFH 213.050 TO XIFH 225.140 REPAIR DOUBLER NOT CORRELATED TO SRM 57-10-00 FIG 38. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED, & INSTALLED DOUBLER IAW MD-Jul 2, 2009 · N281UP · Doug MD11FSDR IPXA09M56719Wedge · misrepairedINSPECTION TYPE :1C REPAIR SURVEY SEQUENCE NR 281-W3-03, LT WING INBD FLAP T/E WEDGE BTWN STA XIFH 133.900 TO XIFH 177.300. DOES NOT CORRELATE TO SRM. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR ZEE ANGLE IAW MD-11 SRM 57-20-00 PARA (4) AND FIG. 3.Jul 2, 2009 · N281UP · Doug MD11FSDR P5CA2009071301603Skin · damagedON POST FLIGHT WALKAROUND FOUND LEFT INBOARD FLAP MISSING PIECE OF SKIN. "DAMAGE FOUND TO BE WITHIN LIMITS AS PER SRM 51-70-02. PERFORMED TIME LIMITED REPAIR IAW SRM 57-53-01/51-70-17. REQUIRED DIVE CYCLES WITH PERMANENT REPAIR NEXT "A" CHECK."Jul 2, 2009 · N451PA · Boeing 74746NFSDR SWAA094282Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jul 2, 2009 · N749SW · Boeing 7377H4SDR UALA2009070201908Skin · delaminatedRIGHT INBOARD FLAP OUTBOARD AFT FAIRING IS DELAMINATED. FLAP REMOVED & SENT TO SHOP 273 FOR REPAIR. REPLACED RT TRAILING EDGE FLAP. CREW COMMENTS: GOOD TEST FLIGHT FOR FLAP REPLACEMENT.Jul 1, 2009 · N570UA · Boeing 757222SDR FDEA200907012438Rib · crackedRT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 25A IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A IAW SRM 51-40-21.Jul 1, 2009 · N682FE · Airbus A300F4605RSDR FDEA200907012437Rib · crackedLT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 24; RIB 25A AND 6EA. WEBS IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A ; OLD RIB 24; THE 6 EA. WEBS AND THE SKIN IAW SRM 51-40-21.Jul 1, 2009 · N682FE · Airbus A300F4605RSDR FDEA200907012432Structure · delaminatedFOUND DELAMINATION AROUND ROLLER BLOCKS ON FLAP DEFLECTOR DOORS, INNER AND OUTER SHROUD BOXES, RT WING. REPAIR PERFOREMD BY BONDING REPAIR IAW SRM 51-77-12 AND REINSTALLATION OF ROLLER BLOCKS IAW RAS/BAE/1009227/2009 ISS. A, APPROVED BY EA 6-5750-120223.Jul 1, 2009 · N746FD · Airbus A300B4622RSDR FDEA200907012431Structure · delaminatedFOUND DELAMINATION AROUND ROLLER BLOCKS ON FLAP DEFLECTOR DOORS, INNER AND OUTER SHROUD BOXES, LT WING. REPAIR PERFORMED BY BONDING REPAIR IAW SRM 51-77-12AND REINSTALLATION OF ROLLER BLOCKS IAW RAS/BAE/1009227/2009 ISS A, APPROVED BY EA 6-5750-120223.Jul 1, 2009 · N746FD · Airbus A300B4622RSDR FDEA200907012430Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP TOP SKIN BETWEEN RIB 13-15. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK IAW RAS/FOK/067/2009 ISS. B, APPROVED BY EA 6-5750-129120.Jul 1, 2009 · N746FD · Airbus A300B4622RSDR FDEA200907012429Skin · chafedFOUND CHAFING MARKS ON LT OUTER FLAP TOP SKIN BETWEEN RIB 15-15A. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK IAW RAS/FOK/074/2009 ISS. C, APPROVED BY EA 6-5750-129184.Jul 1, 2009 · N746FD · Airbus A300B4622RSDR FDEA200907012428Skin · chafedFOUND CHAFING MARKS ON RT OUTER FLAP TOP SKIN BETWEEN RIB 15-15A. REPAIR PERFORMED BY BLENDING OUT THE CHAFING MARK IAW RAS/FOK/075/2009 ISS. C, APPROVED BY EA 6-5750-129183.Jul 1, 2009 · N746FD · Airbus A300B4622RSDR IPXA09556838Skin Panel · gougedINSPECTION TYPE:C RT WING OUTBOARD MAIN FLAP UPPER INBOARD SKIN PANEL HAS 4 EA SMALL GOUGES IN EXISTING REPAIR. LOCATED AT STA 419.5 - 424.5, 2.75 INCHES AFT OF PANEL'S FORWARD EDGE. CONTACT AT ON SITE ENGINEERING AS REQUIRED PER APPENDIX C, STEP E. DAMAGE Jun 30, 2009 · N447UP · Boeing 75724APF
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