JASC 5753

Service difficulty reports · 31,513

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 SWIA201334275Vane · chafedLT INBD FLAP VANE LE CHAFFED IN THE CENTER BEYOND LIMITS. C-CHECK REPLACED PN 601R14303-51 IAW SRM.Aug 3, 2013 · N961SW · Cndair CL6002B19SDR SWIA201334271Skin · chafedLT INBD FLAP VANE LE CHAFED ON THE OTBD SIDE. C-CHECK REPAIRED IAW REO.Aug 3, 2013 · N961SW · Cndair CL6002B19SDR SWIA201334270Skin · chafedLT INBD FLAP VANE LE CHAFED IN THE CENTER. C-CHECK BLENDED IAW REO.Aug 3, 2013 · N961SW · Cndair CL6002B19SDR IPXA13179782Skin · chafedINSPECTION TYPE:3C, LT CENTER FLAP UPPER SKIN IS CHAFED BETWEEN RIB 13 AND 15. ACCOMPLISHED REPAIR ON LT CENTER FLAP UPPER SKIN BETWEEN RIB 13 AND RIB 15 STGR 2, 6 TO STGR 2.8 IAW STASA EA 300-5753-01-A4829 AND EO A300-5750-51792-A, PARA 6A.Aug 3, 2013 · N130UP · Airbus A300F4622RSDR IPXA13B79611Skin · puncturedPUNCTURE IN LOWER SKIN LT INBD FLAP COVE PANEL 2.5" FWD OF AFT END AND 1 2.0" OTBD OF INBD EDGE. REPAIRED IAW EO B747-5750-51098-B.Aug 3, 2013 · N573UP · Boeing 74744AFSDR SWIA201334269Skin · chafedRT INBD FLAP VANE LE SKIN CHAFED AT OTBD END. C-CHECK REPAIRED IAW REO.Aug 2, 2013 · N961SW · Cndair CL6002B19SDR SWIA201334268Skin · chafedRT INBD FLAP VANE LEADING SKIN CHAFED NEAR CENTER. C-CHECK REPAIRED IAW REO.Aug 2, 2013 · N961SW · Cndair CL6002B19SDR SWIA201334267Skin · chafedRT INBD FLAP VANE LE SKIN CHAFED. C-CHECK REPLACED IAW REO.Aug 2, 2013 · N961SW · Cndair CL6002B19SDR QXEA2013082101269Structure · corrodedTHREE RIVETS CORRODED ON THE RT INBD FLAP UPPER L/E. REMOVED CORRDED RIVETS ON RT FLAP IAW SRM 51-42-15, PROCEDURE 5, TIEM G, STEP 1. INSTALLED NEW RIVETS IAW SRM 51-42-15 PROCEDURE 5, ITEM E, STEPS 1-3.Aug 2, 2013 · N412QX · Bombdr DHC8402SDR SWAA2013081919296Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED AFT FLAP IAW MM.Aug 2, 2013 · N411WN · Boeing 7377H4SDR FDEA201308021745Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE FOUND DENTED AT XIFH 250 AND ONE INCH FROM T/E. REPAIRED IAW SRM 57-50-01, REPAIR 1, FIGURE 201, REV 53 AND EA 1-5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 2, 2013 · N619FE · Doug MD11FSDR SWAA2013081319171Stiffener · crackedRT WING NR 6 AFT FLAP TRACK STIFFENER CRACKED. R&R STIFFENER IAW SRM.Aug 2, 2013 · N527SW · Boeing 7375H4SDR SWAA2013080718935Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED AT INBD END LOWER SIDE. R&R AFT FLAP IAW MM.Aug 2, 2013 · N292WN · Boeing 7377H4SDR SWAA2013080618888Flap · delaminatedLT WING INBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.Aug 2, 2013 · N649SW · Boeing 7373H4SDR SWAA2013080618887Flap · delaminatedRT WING OTBD AFT FLAP DELAMINATED ON INBD END. R&R AFT FLAP IAW AMM.Aug 2, 2013 · N649SW · Boeing 7373H4SDR DALA13037480971Vane · corrodedDURING ROUTINE INSPECTION, THE LT WING OTBD T/E FLAP FIXED VANE WAS NOTED TO HAVE EXFOLLIATION CORROSION ON THE LOWER SURFACE. THE FLAP VANE WAS REPLACED IAW AMM 27-51-03-501 AND THE REQUIRED INSPECTIONS WERE COMPLETED.Aug 2, 2013 · N971DL · Doug MD88SDR SWIA201334308Hinge Fitting · chafedRT WS54.55 HINGE BOX AFT FITTING HAS OTBD FITTING LUGS CHAFED. C-CHECK REPAIRED FLAP HINGE BOX WING FITTING IAW STS.Jul 31, 2013 · N802SK · Cndair CL6002D24SDR IPXA13179803Skin · gougedINSPECTION TYPE:3C, RT INBD FLAP UPPER SKIN IS GOUGED BETWEEN RIB 16 AND 17 STGR 2.2 TO STGR 2.4. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 16 AND 17 STR 2.2 TO STGR 2.4 IAW EO A300-5750-51803-A PARA 6A.Jul 31, 2013 · N130UP · Airbus A300F4622RSDR IPXA13179801Skin · chafedINSPECTION TYPE:3C, RT INBD FLAP UPPER SKIN IS CHAFED IN 2 PLACES BETWEEN RIB 11 AND 12 STR 2.1 TO STR 2.4. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 11 AND 12 STR 2.1 TO STR 2.4 IAW EO A300-5750-51802-A, PARA 6A.Jul 31, 2013 · N130UP · Airbus A300F4622RSDR IPXA3579588Skin · puncturedINSPECTION TYPE: C-CK, RT INBD MAIN FLAP HAS A SMALL PUNCTURE ON THE UPPER SURFACE. REPAIRED IAW SRM 51-53-01 2R AND 51-70-07-OG.Jul 31, 2013 · N447UP · Boeing 75724APFSDR A6WA20134M1176Panel · damagedLEFT FLAP PANEL 584AB HAS 1 EA ELONGATED FASTENER HOLE TOP RB CORNER. REMOVED ELONGATED HOLE AND INSTALLED FREEZE PLUG, PN 05-2013-056 IAW SRM 57-52-00-02.Jul 30, 2013 · N408AW · Cndair CL6002B19SDR SWIA201334248Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT INBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT INBD VANE ACTUATOR IAW REO.Jul 30, 2013 · N905SW · Cndair CL6002B19SDR SWIA201334247Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT CENTER VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT CENTER VANE ACTUATOR IAW REO.Jul 30, 2013 · N905SW · Cndair CL6002B19SDR SWIA201334246Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT OTBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT OTBD VANE ACTUATOR IAW REO.Jul 30, 2013 · N905SW · Cndair CL6002B19SDR IPXA13579683Skin · damagedINSPECTION TYPE: C1S3, LT INBD MAIN FLAP UPPER SKIN DAMAGED AT APPROX 44.75 FROM INBD END. REPAIRED IAW RCD 012190.Jul 30, 2013 · N432UP · Boeing 75724APFSDR SWAA2013080118745Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW MM.Jul 30, 2013 · N624SW · Boeing 7373H4SDR SWIA201334249Hinge Fitting · gougedLT WING OTBD FLAP INBD FWD HINGE FITTING AFT SIDE HAS A GOUGE. C-CHECK BLENDED GOUGE ON LT WS178.00 FLAP HINGE BOX OTBD AFT SIDE OF AFT HINGE FITTING IAW STS.Jul 28, 2013 · N905SW · Cndair CL6002B19SDR SWAA2013080718928Stiffener · crackedLT WING NR 3 STIFFENER CRACKED ON INBD SIDE OF FLAP TRACK FAIRING. R&R STIFFENER IAW SRM & DRAWING.Jul 28, 2013 · N527SW · Boeing 7375H4SDR IPXA3579535Panel · puncturedRT INBD MAIN FLAP COVE PANEL LWR SURFACE 3 DAMAGE AREAS 81" OTBD OF INBD EDGE 3.1" FWD OF AFT EDGE. REPAIRED IAW EO B757-5750-51606-A.Jul 28, 2013 · N459UP · Boeing 75724APFSDR CALA2013072990026Fairing · crackedFLAP CANOE FAIRING, 571DB HAS 1 INCH CRACK INBD SIDE. PERFORMED PERMANENT REPAIR IAW SRM 57-53-70, 1 PAGE, 103 NOTE A.Jul 28, 2013 · N652UA · Boeing 767322SDR WRLA20130727601Wedge · debondedDISBOND WAS FOUND ON LT WING OTBD FLAP, NRC6753-503L, WEDGE UPPER SKIN AT STA X OF 614.25 TO 676.5. PERFORM THE LT WING OTBD FLAP WEDGE UPPER SKIN REPAIR IAW EI W2013A57B-2048, REV: 0. CHECK CONDITION SATISFACTORY.Jul 27, 2013 · N382WA · Doug MD11FSDR SWAA2013080918987Angle · crackedRT WING FLAP TRACK NR 6 UPPER SURFACE ANGLE CRACKED AT WBL 183.49. R&R ANGLE IAW & DRAWING.Jul 27, 2013 · N527SW · Boeing 7375H4SDR CALA2013072990036Skin · delaminatedRT INBD T/E FLAP DELAMINATED ALONG THE EDGEBAND. 12 INCHES INBD FROM THE BODY. AREA REMOVED OF MOISTURE, R & R RT AFT T/E FLAP IAW MM. RIG AND OPS CHECKED GOOD.Jul 26, 2013 · N585UA · Boeing 757222SDR DALA13036413138Strut · corrodedCORROSION AT INTERNAL STRUCTURE OF INTERCONNECTING STRUT OF LT FLAP. R & R INTERCONECTING STRUT.Jul 26, 2013 · N338NB · Airbus A319114SDR AALA20130726001Flap · puncturedRT INBD FLAP HAS PUNCTURE ON THE LOWER INBD FLAP HAS PUNTURE ON THE LOWER INBD SIDE APPROXIMATLEY 10 INCHES FROM INBD END. ACCOMPLISHMENTS HOT BOND REPAIR IAW SRM 57-53-01-01-2, 51-70-10-2R-2 & SRM 51-70-10-2R.Jul 26, 2013 · N973AN · Boeing 737823SDR ASOA2013081608876Fitting · damagedOVERSIZED HOLES ON LT & RT FWD FLAP FITTING ASSY. REPAIRED IAW REO 670-57-21-575, REV P1. REPAIR CLASSIFIED AS MAJOR.Jul 25, 2013 · N722EV · Cndair CL6002C10SDR SWAA2013072618605Flap · delaminatedLT WING INBD AFT FLAP DELAMINATED ON OTBD CORNER. R&R FLAP ASSEMBLY IAW MM.Jul 25, 2013 · N379SW · Boeing 7373H4SDR IPXA13B79634Skin · delaminatedINSPECTION TYPE:C, LT WING INBD T/E FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 26.Jul 24, 2013 · N578UP · Boeing 74745ESDR A6WA2013073141117Skin · chafedTE FLAP SKIN PANEL 594PB CHAFED. R & R SKIN IAW SRM 51-40-11 AND 51-42-06.Jul 23, 2013 · N408AW · Cndair CL6002B19SDR IPXA13579682Skin · damagedINSPECTION TYPE: C1S3, LT INBD MAIN FLAP UPPER SURFACE COMPOSITE SKIN DAMAGED FROM CONTACT WITH WING T/E FIXED PANEL. REPAIRED IAW RCD 011892.Jul 22, 2013 · N432UP · Boeing 75724APFSDR IPXA13B79633Skin · delaminatedINSPECTION TYPE:C, RT WING INBD T/E MID FLAP T/E COVE PANEL HAS DELAMINATION. FIBERGLASS PREPREG LAY-UP REPAIR PERFORMED IAW SRM 51-70-07, PAR5A (1), FIG 5, REV 25.Jul 22, 2013 · N578UP · Boeing 74745ESDR FDEA201307221632Tee Fitting · corrodedLT OTBD FLAP VANE TEE FITTING "B" MOUNTING HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02 REPAIR 5 FIG.201 REV 53. REPAIRED IAW EA 1-5750-T0301579 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221631Tee Fitting · corrodedRT OTBD FLAP VANE TEE FITTING "F" MOUNTING HOLE CORRODED. FOUND EXCEEDED LIMIT IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA 1-5750-T0301580, PART 1 STEP 1.B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221630Tee Fitting · corrodedRIGHT OTBD FLAP VANE TEE FITTING "C" MOUNTING HOLE CORROSION. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA1-5750-T0301580, PART 1 STEP 1.A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221629Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD AFT (FLAP) HINGE PIVOT HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-04, REV 76. REPAIRED IAW EA 1-5750-166144. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221628Bushing · wornRIGHT WING FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76 AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED EA 1-5750-102153C, PART 3, STEP 2. REPAIRJul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221627Bushing · wornRIGHT WING: RT INBD FLAP OTBD HINGE (FLAP SIDE) , PIVOT INBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-102153C, PART 3, STEP Jul 22, 2013 · N521FE · Doug MD11FSDR IPXA201307229437Skin · puncturedRIGHT WING INBD FLAP LOWER T/E PUNCTURE DAMAGED. REPAIRED IAW EO B747-5750-51514-A.Jul 21, 2013 · N579UP · Boeing 747400SDR IPXA201307229433Skin · puncturedRT INBD MID FLAP LWR SURFACE PUNCTURE 1.4" FROM INBD EDGE. REPAIRED IAW EO B747-5750-51513-A.Jul 21, 2013 · N579UP · Boeing 747400SDR A6WA2013073141118Vane · chafedCHAFE TO L/T INBD FLAP VANE UPPER SKIN T/E AT WS 55.49. BLENDED IAW REO 601R-57-52-2028.Jul 20, 2013 · N408AW · Cndair CL6002B19
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