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 SWAA2014060228619Fairing · crackedRIGHT WING NR 3 FLAP FAIRING CRACKED FASTENER HOLE AT AFT TAIL CONE CONNECTION. REPAIRED FAIRING IAW WO.May 2, 2014 · N717SA · Boeing 7377H4SDR IPXA2014052783056Skin · chafedRIGHT INBD FLAP UPPER SURFACE SKIN CHAFED. REPAIRED IAW SRM 57-50-00, PARA 4E, FIG 205.May 2, 2014 · N160UP · Airbus A300F4622RSDR SWIA201437637Rod · chafedRIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684AB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684AB, AND FOUND TO BE WITHIN LIMITS IAW REO.May 2, 2014 · N815SK · Cndair CL6002D24SDR SWIA201437636Rod · chafedRIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684CB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684CB, AND FOUND TO BE WITHIN LIMITS, IAW REO.May 2, 2014 · N815SK · Cndair CL6002D24SDR SWIA201437635Rod · chafedRT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684DB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684DB, AND FOUND TO BE WITHIN LIMITS IAW REO AND AMM.May 2, 2014 · N815SK · Cndair CL6002D24SDR ASOA2014052310573Arm · gougedFOUND GOUGE ON RT OTBD FLAP CENTER HINGE ARM WS 220.00 BOTTOM INBD MOUNTING LUG. BLENDED GOUGE IAW EA:26-2014-048, REV. ORIGINAL. PERFORMED SHOT PEENING ON THE REQUIRED SURFACE RT OTBD FLAP CENTER HINGE LUG IAW EA 26-2014-048, STEP 3.May 1, 2014 · N880AS · Cndair CL6002B19SDR SWAA2014050527651Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.May 1, 2014 · N354SW · Boeing 7373H4SDR IPXA2014052883094Skin · corrodedLEFT WING OTBD FLAP UPPER SKIN IS CORRODED UNDER STATIC WICK NEAR RIB 27A. REPAIRED FLAP UPPER SKIN IAW EA 300-5750-01-A5309.Apr 30, 2014 · N162UP · Airbus A300F4622RSDR IPXA2014050982898Skin · crackedDURING A 1C INSPECTION, LEFT INBD FLAP UPPER SKIN CRACKED NEAR XIFH 165. REPAIRED IAW SRM 57-00-01, REPAIR 1, FIG 201.Apr 30, 2014 · N296UP · Doug MD11FSDR SWAA2014050127574Skin · delaminatedRIGHT INBD AFT FLAP DELAMINATED AT LOWER SURFACE. R & R FLAP ASSEMBLY IAW MM.Apr 30, 2014 · N650SW · Boeing 7373H4SDR IPXA2014052883092Skin · corrodedRT WING OTBD FLAP UPPER SKIN IS CORRODED UNDER STATIC WICK NEAR RIB 27A, REPAIRED FLAP UPPER SKIN IAW EA 300-5750-01-A5310, I/R AND EO A300-5750-54401-A.Apr 29, 2014 · N162UP · Airbus A300F4622RSDR SWAA2014052028169Stiffener · crackedLEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.Apr 29, 2014 · N387SW · Boeing 7373H4SDR ASAA2014042907763Skin · damagedRT WING OTBD AFT FLAP LOWER SKIN HAS A CREASE JUST OTBD OF NR 7 FLAP TRACK. ACFT GROUNDED. REPAIRED RT WING OTBD AFT FLAP LOWER SKIN JUST OTBD OF NR 7 FLAP TRACK IAW SRM 51-70-10-2R-0, REPAIR 4.Apr 29, 2014 · N793AS · Boeing 737490SDR ASOA2014051510500Skin · dentedDENT ON RT INBD FLAP LOWER SKIN, AFT OF FLAP ACCESS PANEL 684BB, MARKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED DAMAGED AREA AND FABBED DOUBLER IAW SRM 57-52-00, NR 3. WET INSTALLED DOUBLER (-1) APPLIED ACRODYNAMIC SEALER & AND REApr 28, 2014 · N852AS · Cndair CL6002B19SDR SWIA201437414Hinge · gougedLEFT OTBD FLAP OTBD HINGE ARM ASSY GOUGED BY FOD AT LOWER HINGE BOLT LUG. C-CHECK, REPAIRED LT OTBD FLAP, OTBD HINGE ARM ASSY AT LOWER HINGE BOLT LUG IAW STS EA.Apr 27, 2014 · N868CA · Cndair CL6002B19SDR DALA14026490964Hinge Fitting · corrodedCORROSION FOUND ON FLAP HINGE FITTING, XRS=267 RT WING T/E. HINGE REPLACED IAW AMM 57-40-01 AND 27-50-02 AND HINGE BRACKET AND ACTUATOR REMOVED AND INSTALLED IAW AMM 27-52-02, LEAK CHECKED ACTUATOR WAS PERFORMED, NO LEAKS FOUND.Apr 27, 2014 · N964DL · Doug MD88SDR ASAA2014042607888Skin · chafedRIGHT INBD MID FLAP CHAFED ON UPPER SURFACE. ACFT GROUNDED. REPAIRED SKIN IAW SRM 57-53-01-2R-3, REPAIR 3.Apr 26, 2014 · N793AS · Boeing 737490SDR SWIA201437510Vane · gougedRIGHT WING INBD FLAP, OUTBD VANE ACT SLIDING BEAM, 684CB, HAS GOUGING ON INNER SKIN OF FLAP. C-CHECK, REPAIRED RT INBD FLAP GOUGE OF INNER SKIN AT OUTBD VANE ACTUATOR SLIDING BEAM IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437509Vane · chafedRIGHT INBD FLAP VANE INBD L/E CHAFED. C-CHECK, REMOVED CHAFED OUT OF LIMITS INBD FLAP VANE INBD SECTION SKIN CAP AND INSTALLED NEW FLAP VANE CAP IAW SRM AND REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437508Vane · chafedRT INBD FLAP VANE CENTER L/E CHAFED. C-CHECK, REPAIRED RT INBD FLAP VANE CENTER L/E CHAFE IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437507Vane · chafedRT INBD FLAP VANE OTBD L/E CHAFED. C-CHECK, REPAIRED RT INBD FLAP VANE OTBD L/E CHAFE IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437506Beam · gougedLEFT INBD FLAP, INBD VANE ACTUATOR SLIDING BEAM, 584AB, HAS GOUGING ON THE INNER SKIN OF THE FLAP. C-CHECK, TREATED DAMAGE TO INNER DOUBLER OF LT INBD FLAP UNDER PANEL 584AB IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437505Vane · chafedLEFT INBD FLAP VANE INBD END OF L/E IS CHAFED. C-CHECK, REPAIRED LT INBD FLAP VANE INBD L/E CHAFE IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437504Vane · chafedLT INBD FLAP VANE CENTER LOCATION OF L/E IS CHAFED. C-CHECK, REPAIRED LT INBD FLAP VANE CENTER L/E CHAFE IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR SWIA201437503Vane · chafedLEFT INBD FLAP VANE OTBD LOCATION OF L/E IS CHAFED. C-CHECK, REPAIRED LT INBD FLAP VANE OTBD L/E CHAFE IAW REO.Apr 26, 2014 · N941SW · Cndair CL6002B19SDR FDEA201404260860Skin · crackedLEFT WING INBD FLAP UPPER SKIN CRACKED. REPAIRED AS PER EA 1-5750-T0307737 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.Apr 26, 2014 · N594FE · Doug MD11FSDR FDEA201404260859Vane · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 55. REPAIRED IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 55 AND EA 1-5750-T0307725 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6Apr 26, 2014 · N594FE · Doug MD11FSDR FDEA201404260858Hinge Bracket · corrodedDURING ACCOMPLISHMENT OF FPI INSPECTION, RT INBD FLAP SIDE HINGE PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REVISION 78. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750-T0307723 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM Apr 26, 2014 · N594FE · Doug MD11FSDR 8EKA20140507Fairing · brokenDURING POST FLIGHT CHECK, PILOT DISCOVERED A PIECE OF BROKEN FAIRING ON LT INBD FLAP OB PYLON. FIBERGLASS FAIRING PN 212-13223.1 CHAFED A HOLE THROUGH LT INBD FLAP LE PLATE OVER TIME. REPAIRS ARE CURRENTLY IN PROCESS, SUPPLEMENTAL INFORMATION WILL BE SUBMITTApr 26, 2014 · N348CA · Casa C212CCSDR IPXA2014042882816Skin · crackedLEFT OTBD AFT FLAP LOWER SKIN HAS .600 LONG CRACK. 7.5" FWD OF T/E, AND 67 " OTBD OF INBD EDGE. REPAIRED IAW EO B757-5750-54214-A.Apr 26, 2014 · N454UP · Boeing 75724APFSDR IPXA2014042882797Angle · corrodedLEFT WING OTBD MAIN FLAP ANGLE CORRODED. REPAIRED IAW EO B757-5750-54168-A.Apr 26, 2014 · N454UP · Boeing 75724APFSDR CA140425003Torque Tube · deteriorated(CAN) DURING HEAVY MAINTENANCE INSPECTION, MAINTENANCE DISCOVERED DAMAGE TO THE RT NR 1 PRIMARY FLAP DRIVE TORQUE TUBE. THE ELASTOMERIC TORSION COUPLING AT 1 END OF THE SHAFT WAS DETERIORATED REQUIRING REPLACEMENT OF THE TORQUE TUBE, PN 734380B, SN 0273.Apr 25, 2014 · Dhav DHC8301SDR SWIA201437586Vane · chafedRT INBD FLAP VANE CHAFED, INBD L/E. C-CHECK, BLENDED RT INBD FLAP VANE CHAFE WITH IN LIMITS AND RESTORED FINISH REF REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437585Vane · chafedRT INBD FLAP VANE CHAFED, CENTER L/E. C-CHECK, BLENDED RT INBD FLAP VANE CENTER L/E REF REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437584Vane · chafedRT INBD FLAP VANE CHAFED, OTBD L/E. C-CHECK, BLENDED RT INBD FLAP VANE OTBD L/E REF REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437583Vane · chafedLT INBD FLAP VANE CHAFED, INBD L/E. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE INBD L/E CAP IAW REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437582Vane · chafedLT INBD FLAP VANE CHAFED, CENTER L/E, C-CHECK, BLENDED LT INBD FLAP VANE CENTER L/E WITH ORIGINAL IAW REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437581Vane · chafedLEFT INBD FLAP VANE CHAFED, OTBD L/E. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE OTBD L/E CAP IAW REO.Apr 25, 2014 · N779CA · Cndair CL6002B19SDR FDEA201404240835Mount · corrodedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307631 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240834Mount · damagedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT OUT OF LIMITS AFTER BUSHING REMOVAL IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307631 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISIApr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240833Mount · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240832Mount · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240829Mount · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240828Mount · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240827Mount · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240826Mount · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. MOUNT REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. NEW BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND E.A. 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAApr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240825Bracket · damagedRIGHT WING OTBD FLAP OTBD FWD HINGE ACTUATOR OTBD HOLE FOUND EXCEED LIMIT DURING BUSHING REMOVAL. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0307629 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.Apr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240831Mount · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVIApr 24, 2014 · N594FE · Doug MD11FSDR FDEA201404240830Mount · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVIApr 24, 2014 · N594FE · Doug MD11FSDR R61A201404240603Torque Tube · corrodedDURING HEAVY CHECK, LT FLAP TORQUE TUBE F6 AT SPLINE IS PITTED. MX R & R LT FLAP TORQUE TUBE F6 IAW AMM 27-51-03, PN 5912949-3, TORQUE TUBE.Apr 24, 2014 · N113HQ · Emb ERJ170200LR
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