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 FDEA201406071338Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 67 INCHES FROM INBD END 4 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071337Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 66 INCHES FROM INBD END 10 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM- 51-70-04, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071336Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 18 INCHES FROM INBD END, 8 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071335Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 22 INCHES FROM INBD END, 111/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071334Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 57 INCHES FROM INBD END, 5 1/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071333Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 32 INCHES FROM OTBD END, 5 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-91 & SRM 51-70-04.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071332Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 36 INCHES FROM INBD END, 7 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071331Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 53 INCHES FROM INBD END, 91/2 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & 51-70-04, CAT A MAJOR REPAIR.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071330Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 77 INCHES FROM OTBD END, 2 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-01 & SRM 51-70-04.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071329Skin · damagedLEFT WING OTBD FLAP AFT FLAP UPPER SURFACES HAS SEVERAL AREAS WITH HAIL STRIKES. BONDED & REPAIRED LT WING OTBD FLAP, AFT FLAP, IAW SRM-57-53-01 & SRM-51-70- 04, APPROX .5 INCHES IN DIAMETER. REMOVED 4 INCHES. REPAIRED THREE AREAS, 1ST LOCATED AT 13.5 INCHEJun 7, 2014 · N993FD · Boeing 7572Q8SDR FDEA201406071328Wedge · delaminatedRT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 59 INCHES FROM OTBD END, 71/2 FROM AFT EDGE. REPAIRED RT AFT FLAP WEDGE UPPER SURFACE IAW SRM 757 51-70-04.Jun 7, 2014 · N993FD · Boeing 7572Q8SDR SWIA201438312Vane · chafedLT INBD FLAP VANE, INBD SIDE CHAFED. BLENDED CHAFE AREA IAW REO.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA201438311Vane · chafedLT INBD FLAP VANE CENTER AREA OF L/E CHAFED. C-CHECK RO: 06/22/2014, R & R LT INBD FLAP VANE CENTER L/E, PN 601R14303-51 IAW SRM.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA2014062338288Vane · chafedRT INBD FLAP VANE L/E IS CHAFED IN THE OTBD AREA. BLENDED CHAFE AREA IAW REO.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA2014062338287Vane · chafedRT INBD FLAP VANE INBD L/E CHAFED. R & R RT INBD FLAP VANE L/E SKIN IAW SRM.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA2014062338286Vane · chafedRT INBD FLAP VANE CENTER AREA OF L/E CHAFED IN CENTER AREA. R & R RT INBD FLAP VANE CENTER AREA OF L/E IAW SRM.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA2014062338285Vane · chafedLT FLAP VANE IS CHAFED ON THE OTBD SIDE OF THE L/E. BLENDED CHAFE AREA IAW REO.Jun 5, 2014 · N781CA · Cndair CL6002B19SDR SWIA201438245Vane · chafedLEFT INBD FLAP VANE CENTER L/E CAP CHAFED. C-CHECK, R & R LT INBD FLAP VANE IAW SRM.Jun 5, 2014 · N783CA · Cndair CL6002B19SDR SWIA201438244Vane · chafedRIGHT INBD FLAP VANE CENTER L/E CAP CHAFED. C-CHECK, R & R RT INBD FLAP VANE IAW SRM.Jun 5, 2014 · N783CA · Cndair CL6002B19SDR SWAA2014061629111Flap · delaminatedLEFT WING OTBD TE AFT FLAP INBD CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.Jun 5, 2014 · N798SW · Boeing 7377ADSDR SWAA2014061028906Flap Track · looseLEFT WING INBD AFT FLAP TRACK INBD ATTACH LOOSE. R & R TRACK IAW AMM.Jun 5, 2014 · N253WN · Boeing 7377H4SDR SWAA2014061028905Flap Track · looseLEFT WING OTBD AFT FLAP OTBD ATTACH LOOSE. R & R TRACK IAW AMM.Jun 5, 2014 · N253WN · Boeing 7377H4SDR A6WA201441624Frame · chafedRT INBD FLAP INBD LE FRAME CHAFED. R & R RT INBD LE FRAME IAW SRM 51-42-06.Jun 5, 2014 · N437AW · Cndair CL6002B19SDR DALA2014062503757Structure · corrodedCORROSION ON FLEX JOINT LINK AT RT WING INBD FLAP. CORROSION REMOVED IAW SRM 51-10-3, PAR 26 AND FLEX JUINT LINK WAS MEASURED, THE MAX DIAMETER OF HOLE IS 0.194" AND DIAMETER MEASURED 0.211" THEREFORE IT IS OUT OF LIMITS IAW DWG NR 5935915 AND FLEX JUINT LIJun 4, 2014 · N963DL · Doug MD88SDR SWIA201438251Vane · chafedLEFT INBD FLAP VANE, OTBD CAP CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.Jun 4, 2014 · N783CA · Cndair CL6002B19SDR SWIA201438250Vane · chafedLEFT INBD FLAP VANE, CENTER CAP CHAFED. C-CHECK, R & R LT INBD FLAP VANE IAW REO AND SRM.Jun 4, 2014 · N783CA · Cndair CL6002B19SDR SWIA201438249Vane · chafedLEFT INBD FLAP VANE, INBD CAP CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.Jun 4, 2014 · N783CA · Cndair CL6002B19SDR SWIA201438247Vane · chafedRIGHT INBD FLAP VANE, INBD CAP IS CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.Jun 4, 2014 · N783CA · Cndair CL6002B19SDR SWIA201438246Vane · chafedRIGHT INBD FLAP VANE, OTBD CAP IS CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.Jun 4, 2014 · N783CA · Cndair CL6002B19SDR FDEA201406041306Skin · damagedRT INBD FLAP DAMAGED. REPAIRED IAW EA 1-5750-T0308747 PART 1.Jun 4, 2014 · N595FE · Doug MD11FSDR SWAA2014061028886Skin · delaminatedRIGHT WING INBD AFT FLAP LOWER SKIN DELAMINATED 26 INCHES FROM INBD END, 4 INCHES FROM AFT EDGE. REPAIRED AFT FLAP IAW EA.Jun 4, 2014 · N249WN · Boeing 7377H4SDR SWAA2014060628772Flap · delaminatedLEFT WING OTBD AFT FLAP INBD END UPPER SIDE DELAMINATED. R & R AFT FLAP IAW AMM.Jun 4, 2014 · N788SA · Boeing 7377H4SDR REXA2014060600464Hinge Fitting · gougedRIGHT INBD FLAP INBD HINGE ARM GOUGED ON LOWER FWD & AFT OTBD SIDE. REPAIRED IAW REO 601R-57-54-259.Jun 4, 2014 · N8905F · Cndair CL6002B19SDR SWAA2014060528705Flap · delaminatedRIGHT WING INBD LE FORE FLAP DELAMINATED. R & R FORE FLAP IAW MM.Jun 4, 2014 · N625SW · Boeing 7373H4SDR ABXA20140603186Skin · corrodedLEFT INBD FWD FLAP LOWER SKIN IS BULGED AT APPROX IFS 260 & 287 THRU 289, AT PANEL 555FB EDGE. R & R LT INBD FLAP ASSEMBLY IAW AMM 27-51-06. CORRODED, PN 113T2201-23A, PART NAME FLAP ASSEMBLY LT INBD TE MAIN, SN 000225, STRINGER & WS LOCATION FROM 260 TO 289Jun 3, 2014 · N790AX · Boeing 767281SDR FDEA201406021260Vane · delaminatedRIGHT WING OTBD FLAP VANE UPPER SURFACE FOUND DELAMINATED FROM XOFH 558.820 - 586.820. RIGHT WING OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED IAW AMM 27-50-32- 4 REVISION 79. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-32-5 REVISION 79. FOUND SATISJun 2, 2014 · N578FE · Doug MD11FSDR DALA14033895806Skin · gougedDURING L CHECK, A GOUGE WAS FOUND COMMON TO THE LT WING INBD MAIN FLAP L/E SKIN PANEL AT FLAP STA 74-76. COMPLIED WITH ER/A 506543-14, REV A.Jun 2, 2014 · N586NW · Boeing 757351SDR CHQA20140602183Flap · damagedCREW REPORTED THAT THEY RECEIVED A MSG FROM ATC THAT THE RT INBD TIRE HAD SEPARATED ON TAKEOFF. A FLYBY OF THE TOWER AT THEIR INTENDED DESTINATION CONFIRMED THE TIRE FAILURE. THE CREW DECLARED AN EMER. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURJun 2, 2014 · N273SK · Emb EMB145LRSDR FDEA201406021279Skin · dentedHAIL DAMAGE, LT WING MAIN FLAP UPPER SURFACE INBD SIDE HAS 2 DENTS. ACCOMPLISHED EA F-5750-T0308600 PT1 WINGS, LT WING INBD MAIN FLAP UPPER SKIN REPAIR.Jun 2, 2014 · N992FD · Boeing 757232SDR FDEA201406021278Skin · dentedHAIL DAMAGE LT OTBD FLAP HAS 2 DENTS DELAMINATED. ACCOMPLISHED EA F-5750-T0308601 PT 1, WINGS, LT WING OTBD MAIN FLAP UPPER SKIN REPAIR.Jun 2, 2014 · N992FD · Boeing 757232SDR FDEA201406011253Skin · crackedLEFT WING CTR FLAP UPPER SKIN FOUND CRACK BETWEEN RIB 26 - 27, STRINGERS 2.7 - 2.8. COMPLETED EA 6-5750-T0308432 PT1. MAJOR REPAIR IAW GMM6-2-100.Jun 1, 2014 · N659FE · Airbus A300F4605RSDR DALA14033115807Skin · puncturedDURING FINAL INSPECTION OF RT WING, FOUND A PUNCTURE ON INBD MAIN FLAP T/E PANEL LOWER SURFACE, AT APROXIMATELY FLAP STA 161 AND 8 INCHES FROM AFT EDGE. REPAIRED PUNCTURE ON RT INBD MAIN FLAP LOWER SURFACE IAW SRM 51-70-07 & AMM 51-21-10-377-039.Jun 1, 2014 · N587NW · Boeing 757351SDR SWIA2014061638179Skin · damagedDENT AND GOUGE IN TOP SKIN ON RT INBD FLAP 10 INCHES FROM AFT EDGE. REPAIRED FLAP IAW EA.May 31, 2014 · N862AS · Cndair CL6002B19SDR FDEA201405311236Skin · dentedLEFT INBD AFT FLAP OTBD UPPER SURFACE HAS HAIL DAMAGE. SANDED, CLEANED & PREPPED AREA AT LT INBD AFT FLAP OTBD UPPER SURFACE. APPLIED REPAIR TO FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW MM 51-20-01 IAW EA F-57-50-T0308504.May 31, 2014 · N966FD · Boeing 757204SDR FDEA201405311235Skin · dentedRIGHT OTBD AFT FLAP UPPER TE INBD SIDE HAS HAIL DAMAGE. SANDED, CLEANED & PREPARED AREA IAW SRM 57-53-01 FIG 201, 51-70-17 PARA 4 C. APPLIED REPAIR TO FLAP RT OTBD UPPER TE INBD SIDE OF AFT FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW AMM 51-00-01.May 31, 2014 · N966FD · Boeing 757204SDR SWIA2014061638184Vane · chafedRT INBD FLAP VANE IS CHAFED NEAR INBD SIDE. C-CHECK, REMOVE CHAFE ON THE RT INBD FLAP VANE NEAR THE INBD SIDE IAW REO.May 30, 2014 · N862AS · Cndair CL6002B19SDR SWIA2014061638183Vane · chafedRIGHT INBD FLAP VANE IS CHAFED NEAR CENTER. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR THE CENTER IAW REO.May 30, 2014 · N862AS · Cndair CL6002B19SDR SWIA2014061638182Vane · chafedRT INBD FLAP VANE IS CHAFED NEAR OTBD SIDE. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR OTBD SIDE IAW REO.May 30, 2014 · N862AS · Cndair CL6002B19SDR CALA2014060291188Attach Bolt · wornNUMBER 4 RT WING FLAP TRACK AFT CANOE FAIRING ATTACH BOLT WORN. INSTALLED NEW BOLT IAW AMM 57-55-11-400-001.May 29, 2014 · N425UA · Airbus A320232SDR CALA2014060291187Attach Bolt · wornNUMBER 3 RT WING FLAP AFT CANOE FAIRING ATTACH BOLT WORN. INSTALLED NEW CANOE FAIRING BOLT IAW AMM 57-55-11-400-001.May 29, 2014 · N425UA · Airbus A320232
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