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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2014032026259Fairing · crackedRT WING NR 6 FLAP SUPPORT FAIRING CRACKED AT TE LOWER SURFACE. REPAIRED FAIRING IAW SRM & EA.SDR DALA14017405649Skin · wornLEFT WING INBD FLAP WORN. BLENDED OUT DAMAGE IAW SRM 57-53-01. UT INSP TO FLAP L/E AREA IAW NDTM PT.4, 51-00-10 AND FOUND OUT OF LIMITS IAW SRM 57-53-01. CUT OUT DAMAGE AREA OF SKIN, FABRICATED REPAIR IAW SRM 57-53-01, FIG 201. INSTALLED REPAIR IAW SRM 57SDR DALA14017395649Skin · wornLT WING INBD FLAP L/E IS WORN OUT OF LIMITS. BLENDED OUT DAMAGE IAW SRM 57-33-01. UT INSP TO FLAP L/E AREA IAW NDTM PT 4 51-00-10. CUTOUT DAMAGE AREA", FABRICATED REPAIR IAW SRM 57-53-01, FIG 201. INSTALLED REPAIR IAW SRM 57-53-01, FIG 201,SDR DALA2014070906950Shroud · delaminatedDURING INSPECTION, FOUND RT WING AFT T/E, FIXED SHROUD ASSY WITH DELAMINATION ON UPPER SKIN LOCATED JUST FWD OF INBD FLAP. COMPLIED WITH PRI 524331-14AD, REV 1 RECEIVED FINAL ERA 524331-14, REV ORIG FINAL ERA MATCHES PRI 524331-14AD, REV 1.SDR FDEA201403170517Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED IAW CMM 57-44-08 REVISION 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306652 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR SWAA2014032126307Flap · delaminatedRT WING INBD FORE FLAP DELAMINATED AT OTBD END. REPAIRED FLAP IAW SRM.SDR SWIA201436892Vane · chafedRT INBD FLAP LEADING EDGE INBD VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON RT INBD FLAP L/E INBD VANE IAW REO.SDR SWIA201436891Vane · chafedRIGHT INBD FLAP L/E MID VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON RT INBD FLAP L/E MID VANE IAW REO.SDR SWIA201436890Vane · chafedRIGHT INBD FLAP L/E OTBD VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON RT INBD FLAP L/E OTBD VANE, IAW REO.SDR SWIA201436889Vane · chafedLEFT INBD FLAP L/E INBD VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON LT INBD FLAP L/E INBD VANE, IAW REO.SDR SWIA201436888Vane · chafedLEFT INBD FLAP L/E MID VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON LT INBD FLAP L/E MID VANE, IAW REO.SDR SWIA201436887Vane · chafedLEFT INBD FLAP L/E OTBD VANE IS CHAFED. C-CHECK, BLENDED AND CHECKED LIMITS ON LT INBD FLAP L/E OTBD VANE IAW REO.SDR SWIA201436886Vane · chafedRT INBD FLAP VANE UPPER L/E IS CHAFED AND NICKED APPROXIMATELY THREE FEET FROM INBD END OF VANE. C-CHECK, BLENDED AND CHECKED LIMITS ON RT INBD FLAP VANE UPPER L/E, IAW REO.SDR SWIA201436863Vane · chafedRT INBD FLAP VANE MID-SECTION CHAFED. C-CHECK, INSTALLED NEW FLAP VANE IAW SRM.SDR FDEA201403160515Hinge Fitting · corrodedRIGHT WING OTBD FLAP FWD HINGE FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306612 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120SDR R61A201403160405Support · corrodedDURING HEAVY CHECK, RT FLAP BEARING SUPPORT AT TUBES 5,6 CORRODED. MAINTENANCE R & R RT FLAP BEARING SUPPORT AT TUBES 5, 6 IAW AMM 25-51-04, OPS CHECK, PN 1702961, FLAP BEARING SUPPORT.SDR SWAA2014032626525Flap · delaminatedRIGHT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR IPXA2014031982324Skin · dentedINSPECTION C09, DENT FOUND ON LT WING OTBD FLAP T/E WEDGE LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV 58.01 & SRM 51-70-07-0G-0, GENERAL FIG 9, REV 58.01.SDR IPXA2014031982323Skin · dentedINSPECTION C09, DENT ON LT WING OTBD FLAP T/E WEDGE LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV 58.01 & SRM 51-70-07-0G-0, GENERAL FIGURE 10, REV 58.01.SDR FDEA201403140503Support Fitting · corrodedRIGHT WING OTBD FLAP VANE NR 1 SUPPORT FITTING FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02 FIGURE 201 REPAIR 5 REVISION 54. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403140502Support Fitting · corrodedLEFT WING OTBD FLAP VANE NR 1 SUPPORT FITTING FOUND CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 57-50-02 FIGURE 201 REPAIR 5 REVISION 54. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR SWIA201436874Vane · chafedLEFT INBD FLAP VANE L/E CENTER BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW LT INBD FLAP VANE CAP MID SECTON IAW SRM.SDR SWIA201436873Vane · chafedRT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW RT INBD FLAP, OTBD VANE CAP IAW SRM.SDR SWIA201436872Vane · chafedLEFT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, REPLACED LT FLAP VANE L/E SKIN IAW SRM.SDR FDEA201403130497Skin · corrodedLEFT WING OTBD FLAP LOWER SKIN BULGING & RIVETS PULLING THRU SKIN AT WS 530. CUT OUT DAMAGED AREA OF SKIN, FABRICATED REPAIR DOUBLER, FILLER, AND TWO TAPERED FILLERS AND INSTALLED ALL REPAIR PARTS IAW EA F-5740-T0306565 PART 1.SDR C77A20140313026Flap Track · wornRT WING FLAP TRACK NR 4 INBD, PN 170-39315-002, WORN OUT OF LIMITS WIDTH REDUCTION W=.003 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-632 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 1412SDR C77A20140313025Flap Track · wornRT WING FLAP TRACK NR 3 OTBD, PN 170-39314-002, WORN OUT OF LIMITS WIDTH REDUCTION W=.004 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-631 IAW ETD 2011-170 01072E & COMPASS EA E175-57-186 2 REV IR WORK ORSDR C77A20140313024Flap Track · wornRT WING FLAP TRACK NR 3 INBD, PN 170-39315-002, WORN OUT OF LIMITS WIDTH REDUCTION W=.004 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-630 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 1412SDR C77A20140313023Flap Track · wornRT WING FLAP TRACK NR 2A OTBD, PN 170-39321-004, WORN OUT OF LIMITS THICKNESS REDUCTION D=.004 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-629 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDERSDR C77A20140313022Flap Track · wornRT WING FLAP TRACK NR 2A INBD, PN 170-39320-004, WORN OUT OF LIMITS THICKNESS REDUCTION D=.012 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-628 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDERSDR C77A20140313021Flap Track · wornRT WING FLAP TRACK NR 2 OTBD, PN 170-39312-004, WORN OUT OF LIMITS WIDTH REDUCTION W=.007 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-627 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 1412SDR C77A20140313020Flap Track · wornRT WING FLAP TRACK NR 2 INBD, PN 170-39313-004 WORN OUT OF LIMITS WIDTH REDUCTION W=.005 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-626 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 14129SDR C77A20140313019Flap Track · wornRT WING FLAP TRACK NR 1A, PN 170-39060-0023, WORN OUT OF LIMITS THICKNESS REDUCTION D= .020 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-625 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 14SDR C77A20140313018Flap Track · wornRT WING FLAP TRACK NR 1 OTBD, PN 170-39310-004, WORN OUT OF LIMITS WIDTH REDUCTION W=.003 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-624 IAW ETD 2011-170 01072E & EA E175-57-186 2 REV IR WORK ORDER 1412SDR C77A20140313017Flap Track · wornLT WING FLAP TRACK NR 2 OTBD, PN 170-39312-003, WORN OUT OF LIMITS WIDTH REDUCTION W=.009 INCHES & THICKNESS REDUCTION D=.017 INCHES IAW SRM 57-52-03 TABLE 101 & 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-534 IAW ETD 2011-170 01072ESDR C77A20140313016Flap Track · wornLT WING FLAP TRACK NR 2 INBD, PN 170-39313-003, WORN OUT OF LIMITS WIDTH REDUCTION W=.003 INCHES & THICKNESS REDUCTION D=.018 INCHES IAW SRM 57-52-03 TABLE 101 & 102. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 736922-533 IAW ETD 2011-170 01072ESDR C77A20140313015Flap Track · wornLT WING FLAP TRACK NR 1 OTBD, 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 736922-531 IAW ETD 2011-170 01072E & EA E175-57-186.1 REV IR WORK ORDER 14129SDR C77A20140313014Flap Track · wornLT WING FLAP TRACK NR 1 INBD, PN 170-39310-004, WORN OUT OF LIMITS WIDTH REDUCTION W=.009 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 736922-530 IAW ETD 2011-170 01072E & EA E175-57-186.1 REV IR WORK ORDER 14129SDR C77A20140313013Flap Track · wornLT WING FLAP TRACK NR 4 INBD, PN 170-39315-001, WORN OUT OF LIMITS WIDTH REDUCTION WORK ORDER 736922-529 IAW ETD 2011-170 01072E & EA E175-57-186.1 REV IR WORK ORDER 1412983.SDR C77A20140313012Flap Track · wornLT WING FLAP TRACK NR 3 OTBD, PN 170-39314-001, 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 736922-528 IAW ETD 2011-170 01072E & E175-57-186.1 REV IR WORK ORDER 1412983.SDR C77A20140313011Flap Track · wornLT WING FLAP TRACK NR 3 INBD, PN 170-39315-001, WORN OUT OF LIMITS WIDTH REDUCTION W=.005 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 736922-527 IAW ETD 2011-170 01072E & EA E175-57-186 1 REV IR WORK ORDER 1412SDR IPXA2014040782549Vane · delaminatedINSPECTION 2C, LT WING INBD FLAP VANE LOWER SURFACE HAS DELAMINATION. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201, REV 55.SDR FDEA201403110479Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, FWD MOUNT OTBD LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-122591B PART 3. REPAIR CLASSIFIED MAJOSDR FDEA201403110475Hinge Fitting · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-122591B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1SDR FDEA201403110474Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHINGS FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306652 PART 1. REPAIR CLASSIFIED MAJOSDR SWAA2014032626547Skin · delaminatedLEFT WING AFT FLAP INBD TE LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR FDEA201403110484Skin · damagedRIGHT WING INBD FLAP OTBD EDGE RIB SKIN FOUND WITH MISSING MATERIAL ABOUT 4.0 INCHES X 4.5 INCHES. DAMAGED SKIN REMOVED AND REPLACED IAW SRM 51-35-01 REVISION 55. SKIN FABRICATED IAW DWG ARC2305 REVISION C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION SDR FDEA201403110482Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD AFT HINGE PIVOT INBD LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW EA 1-5750-160605A PART 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 120.SDR SWAA2014040326793Channel · crackedRIGHT WING NR 6 FLAP TRACK FAIRING CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.SDR SWAA2014040126722Angle · crackedRIGHT WING NR 6 LOWER POSITION FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
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