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 SWAA2014032026248Skin · delaminatedLT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.Mar 10, 2014 · N371SW · Boeing 7373H4SDR SWIA201436845Skin · chafedLT FLAP INBD PANEL 584GB CHAFED. C-CHECK, REPLACED FLAP PANEL IAW SRM.Mar 9, 2014 · N774SK · Cndair CL6002C10SDR IPXA2014031482243Skin · dentedINSPECTION 4C, LT INBD FLAP UPPER SKIN DENTED STA XIFH216. FABRICATED AND INSTALLED REPAIR IAW SRM 57-00-01, REPAIR 1, FIG 201.Mar 9, 2014 · N278UP · Doug MD11FSDR IPXA2014031982312Skin · dentedINSPECTION 3C, LT CENTER FLAP INBD L/E UPPER SIDE HAS A DENT. REPAIRED IAW SRM 57-50-00, PAR 4H, FIG 208, REV 25 AND SREO-5750-44932-B.Mar 8, 2014 · N124UP · Airbus A300F4622RSDR SWAA2014032626528Skin · delaminatedLEFT WING INBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.Mar 7, 2014 · N383SW · Boeing 7373H4SDR HSYA201403061405Flap Track · corrodedCORROSION FOUND ON INBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Mar 6, 2014 · N903FE · Cessna 208BSDR HSYA201403061404Flap Track · corrodedCORROSION FOUND ONCENTER FLAP TRACK WEB, R.S. FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANNULAR CORROSION.Mar 6, 2014 · N903FE · Cessna 208BSDR HSYA201403061403Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Mar 6, 2014 · N903FE · Cessna 208BSDR HSYA201403061402Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Mar 6, 2014 · N903FE · Cessna 208BSDR HSYA201403061401Flap Track · corrodedCORROSION FOUND ON CTR FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Mar 6, 2014 · N903FE · Cessna 208BSDR SWAA2014030725857Flap · damagedLT WING INBD AFT FLAP DAMAGED AT TE INBD CORNER. R & R AFT FLAP IAW MM.Mar 6, 2014 · N444WN · Boeing 7377H4SDR 7AHR2014030782587Skin · dentedINBD LT FLAP WB 96 HAS DENT IN L/E UPPER SURFACE. INSTALLED REPAIR IAW SRM 57-50-4 & 51-30-2.Mar 6, 2014 · N840AL · Boeing 7372X6CSDR 7AHR2014030782557Skin · damagedRIGHT INBD MIDFLAP HAS AREAS OF CORROSION UPPER SURFACE AND PUNCTURE IN SKIN. REMOVED CORROSION IAW SRM 51-10-06. FABRICATED AND INSTALLED REPAIR TO SKIN IAW SRM 51-30-2.Mar 6, 2014 · N840AL · Boeing 7372X6CSDR DALA14015230674Fairing · crackedDENT IN LEFT INBD MAIN FLAP 18, OTBD OF CANOE FAIRING. REPAIRED IAW ERA 452274-14.Mar 6, 2014 · N674DL · Boeing 757232SDR SWIA201436714Vane · chafedLT FLAP VANE OTBD L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON LT FLAP VANE OTBD L/E IAW REO AND SRM.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436713Vane · chafedLT FLAP VANE MIDDLE L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON LT FLAP VANE MIDDLE L/E IAW SRM AND REO.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436712Vane · chafedLEFT FLAP VANE INBD L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON LT FLAP VANE INBD L/E IAW REO AND SRM.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436711Vane · chafedRT FLAP VANE OTBD L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON RT FLAP VANE OTBD L/E IAW SRM AND REO.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436710Vane · chafedRT FLAP VANE MIDDLE L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON RT FLAP VANE MIDDLE L/E IAW SRM AND REO.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436709Vane · chafedRT FLAP VANE INBD L/E CHAFED. C-CHECK, BLENDED CHAFED AREA ON RT FLAP VANE INBD L/E IAW SRM AND REO.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR SWIA201436708Skin · chafedLT INBD FLAP L/E PANEL 584JB IS CHAFED AROUND FLAP VANE ATTACH HOLE. C-CHECK, REPAIRED CHAFED COMPOSITE AROUND FLAP VANE ATTACH HOLE ON L/E PANEL 548JB IAW SRM.Mar 4, 2014 · N982SW · Cndair CL6002B19SDR DALA14014665648Skin · puncturedRIGHT OTBD AFT FLAP LOWER SURFACE NEAR T/E UNDER NR 2 SUPPORT TRACK HAS A PUNCTURE. REMOVED DAMAGED AREA. 2 INCH CIRCLE SKIN & CORE IAW SRM 51-70-17. FABRICATED REPAIR AND INSTALLED, REF SRM 51-70-17. PRIMED AND PAINTED. C/W REPAIR IAW AMDS T/C 2034-8210-01Mar 4, 2014 · N548US · Boeing 757251SDR SWAA2014032426381Angle · crackedRT WING NR 7 MOVABLE FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.Mar 3, 2014 · N385SW · Boeing 7373H4SDR SWIA201436744Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19SDR SWIA201436743Vane · chafedLEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19SDR SWIA201436742Vane · chafedLEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19SDR SWIA201436741Vane · chafedLEFT INBD FLAP VANE CHAFED AT FLAP. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19SDR SWIA201436586Strip · roughWHEN SELECTING FLAPS 45, AIRCRAFT HAS PROMINENT RIGHT ROLL CHARACTERISTICS THAT NEEDS ALMOST 1/2 OF THE LT AILERON TRIM TO NEUTRALIZE. FLT 4689 SANDED RT OTBD FLAP TEFLON STRIP LE TO A SMOOTH TRANSITION TO THE ADJACENT PAINT SURFACE IAW AMM.Mar 2, 2014 · N452SW · Cndair CL6002B19SDR A6WA201441220Skin · chafedLEFT INBD FLAP VANE IS CHAFFED AT INBD END. REMOVED CHAFFED LE SKIN & INSTALLED NEW SERVICEABLE SKIN IAW REO 601R-57-52-004 & SRM 51-42-13.Mar 1, 2014 · N435AW · Cndair CL6002B19SDR IPXA2014030382118Skin · puncturedRT INBD AFT FLAP T/E WEDGE HAS A PUNCTURE IN INNER SKIN APPROX 10 FT FROM INBD EDGE. REPAIRED IAW EO B747-5750-53442-A.Mar 1, 2014 · N576UP · Boeing 74744AFSDR IPXA2014030382113Skin · dentedLEFT INBD AFT FLAP HAS 2.5 INCH DENT IN LOWER SKIN 11 INCHES FROM OTBD EDGE. REPAIRED IAW EO B747-5750-53443-A.Mar 1, 2014 · N576UP · Boeing 74744AFSDR C77A20140301019Flap Track · wornRIGHT WING FLAP TRACK NR 4 INBD, PN 170-39315-002, WORN OUT OF LIMITS WIDTH REDUCTION W= .004 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-638 IAW ETD 2011-170 01072E & EA E170-57-026 2 REV IR WORK ORDER Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301018Flap Track · wornRIGHT WING FLAP TRACK NR 3 INBD, PN 170-39315-002, WORN OUT OF LIMITS WIDTH REDUCTION W= .003 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-637 IAW ETD 2011-170 01072E & EA E170-57-026 2 REV IR WORK ORDER 1Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301017Flap Track · wornRIGHT WING FLAP TRACK NR 2 OTBD, PN 170-39312-004, WORN OUT OF LIMITS WIDTH REDUCTION W= .013 INCHES SRM 0.000 INCHES & ETD 0.039 INCHES & THICKNESS REDUCTION D=.017 INCHES IAW SRM 57-52-03 TABLE 101 & 102, SRM: 0.013 INCHES & ETD 0.039 INCHES. BLENDED WORN AMar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301016Flap Track · wornRIGHT WING FLAP TRACK NR 2 INBD, PN 170-39313-004, WORN OUT OF LIMITS THICKNESS REDUCTION D=.015 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-633 IAW ETD 2011-170 01072E & EA E170-57-026 2 REV IR WORK ORDMar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301015Flap Track · wornRIGHT5 WING FLAP TRACK NR 1 INBD, PN 170-39310-003, WORN OUT OF LIMITS WIDTH REDUCTION W= .006 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-632 IAW ETD 2011-170 01072E & EA E170-57-026 2 REV IR WORK ORDER Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301014Flap Track · wornLEFT WING FLAP TRACK NR 4 INBD, PN 170-39315-001, WORN OUT OF LIMITS WIDTH REDUCTION W= .003 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-533 IAW ETD 2011-170 01072E & EA E170-57-026 1 REV IR WORK ORDER 14Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301013Flap Track · wornLEFT WING FLAP TRACK NR 3 OTBD, PN 170-39314-001, WORN OUT OF LIMITS WIDTH REDUCTION W= .005 INCHES SRM: 0.000 ETD 0.039 & THICKNESS REDUCTION D=.018 INCHES IAW SRM 57-55-03 TABLE 101 & 102, SRM 0.012 INCHES, ETD 0.039 INCHES. BLENDED WORN AREA IAW SRM PART IMar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301012Flap Track · wornLEFT WING FLAP TRACK NR 3 INBD, PN 170-39315-00, WORN OUT OF LIMITS WIDTH REDUCTION W= .004 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-531 IAW ETD 2011-170/01072E & EA E170-57-026 1 REV IR WORK ORDER 140Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301011Flap Track · wornLEFT WING FLAP TRACK NR 2A INBD, PN 170-39320-003, WORN OUT OF LIMITS THICKNESS REDUCTION D=.011 INCHES IAW 170 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-527 IAW ETD 2011-170 01072E & EA E170-57-026 1 REV IR WORKMar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301010Flap Track · wornLEFT WING FLAP TRACK NR 2 OTBD, PN 170-39312-00, WORN OUT OF LIMITS WIDTH REDUCTION W= .011 SRM: 0.000 ETD 0.039 & THICKNESS REDUCTION D=.029 INCHES IAW SRM 57-52-03 TABLE 101 & 102. SRM 0.013 INCHES ETD 0.039. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WOMar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301009Flap Track · wornLEFT WING FLAP TRACK NR 1 INBD, PN 170-39310-004, WORN OUT OF LIMITS WIDTH REDUCTION W= .004 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 784497-523 IAW ETD 2011-170 01072E & EA E170-57-026 1 REV IR WORK ORDER 1Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301007Access Panel · gougedLEFT WING FLAP ACCESS PANEL 561ET HAS MULTIPLE AREAS WITH GOUGE DAMAGE. BLENDED DAMAGED AREA IAW SRM 51-10-03 ON WORK ORDER 784497-542 IAW ETD 2014-170-015876 & EA E170-57-027 REV IR WORK ORDER 1409444.Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR EE4Y2014032700052Flap · dentedRIGHT WING TE MID FLAP AT WBL 95.5 LE WITH DENTS. THE DENTS WERE REPAIRED IAW COO-AMX-14-0004-02B.Feb 28, 2014 · N855AM · Boeing 737752SDR IPXA2014032182364Skin · chafedRT INBD FLAP UPPER SURFACE BETWEEN RIBS 11-14, S2.1-2.4 PREVIOUS REPAIR DOUBLER CHAFED. REPAIRED RT INBD FLAP UPPER SURFACE IAW EA 300-5750-01-A5142 AND EO A300-5750-53763-A.Feb 28, 2014 · N124UP · Airbus A300F4622RSDR IPXA2014031282234Skin · damagedINSPECTION TYPE:2C, CHAFE DAMAGE ON RT INBD FLAP T/E WEDGE LOWER SKIN. RESKINNED LOWER SURFACE OF RT INBD FLAP BETWEEN XIFH 243 - 288 IAW SRM 57-50-01, REPAIR 1, FIG 201.Feb 28, 2014 · N250UP · Doug MD11FSDR SWAA2014032426475Spindle · delaminatedLEFT WING OTBD FLAP NR 2 CARRIAGE SPINDLE DELAMINATED. R & R SPINDLE IAW MT.Feb 27, 2014 · N371SW · Boeing 7373H4SDR SWAA2014031326023Flap · debondedRT WING INBD FORE FLAP DIS BONDED AT INBD EDGE. REPAIRED FLAP IAW SRM.Feb 27, 2014 · N365SW · Boeing 7373H4SDR SWAA2014031225975Skin · delaminatedRIGHT WING FORE FLAP SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.Feb 27, 2014 · N365SW · Boeing 7373H4SDR 2014FA0000104Spar · crackedFOUND FLAP LOWER SKIN CRACKED JUST ON THE OTBD SIDE OF THE INBD FLAP ATTACHMENT. AFTER REMOVAL OF THE SKIN THE AFT SPAR, AND RIB WHERE ALSO DAMAGED & CRACKED.Feb 27, 2014 · Cessna 208B
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