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 EPHR20140120004Skin · puncturedRT WING IB MID FLAP LEADING EDGE SKIN UPPER SURFACE PUNCTURED AT WBL 329. REPAIRED IAW SRM 51-70-06.SDR EPHR20140120003Skin · damagedRIGHT WING OTBD AFT FLAP HAS A SMALL AREA OF DAMAGE ON THE T/E OF THE T/E WEDGE AT APPROX WS 950. THE DAMAGE IS REPAIRED IAW SRM 51-70-06. PROJECT 743WA-305, NRI 3281.SDR EPHR20140120002Skin · gougedRIGHT WING OTBD AFT FLAP UPPER SURFACE HAS THREE SMALL AREAS OF DAMAGE, ON THE OTBD FWD EDGE BAND OF THE UPPER SKIN PANEL BETWEEN WBL 770 AND 808 WS 1141 TO 1178. THE DAMAGE AT ALL AREAS IS OUT OF SRM 57-53-01, FIG 101, DETAIL II DUE TO PROXIMITY TO FASTENER HSDR IPXA2014020581777Housing · corrodedINSPECTION C, LT WING INBD FORE FLAP OTBD LEVER HOUSING CORRODED. LEVER HOUSING REPLACED IAW SRM 51-10-02 AND SRM 51-40-02, REV 27.SDR IPXA2014020381754Housing · corrodedINSPECTION C, LEFT WING INBD FORE FLAP OTBD LEVER HOUSING CORRODED. REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02, REV 27.SDR C77A20140121035Flap Track · wornRIGHT WING FLAP TRACK NR 3 OTBD, PN 170-39314-002, 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 737209-626 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDER 90SDR C77A20140121034Flap Track · wornRIGHT WING FLAP TRACK NR 2A OTBD, PN 170-39321-004 WORN OUT OF LIMITS THICKNESS REDUCTION D .020 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-625 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDESDR C77A20140121033Flap Track · wornRIGHT WING FLAP TRACK NR 2A INBD, PN 170-39320-004, WORN OUT OF LIMITS THICKNESS REDUCTION D .010 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-624 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDSDR C77A20140121032Flap Track · wornRIGHT WING FLAP TRACK NR 2 OTBD, PN 170-39312-004, 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 737209-623 IAW ETD 2011-170 01072E & COMPASS EA E175-57-184 2 REV IR WSDR C77A20140121031Flap Track · wornRIGHT WING FLAP TRACK NR 2 OTBD, PN 170-39312-004, WORN OUT OF LIMITS WIDTH REDUCTION W .010 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-623 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDER 90SDR C77A20140121030Flap Track · wornRIGHT WING FLAP TRACK NR 2 INBD, PN 170-39313-004, WORN OUT OF LIMITS THICKNESS REDUCTION D .014 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-622 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDESDR C77A20140121029Flap Track · wornRIGHT WING FLAP TRACK NR 1 OTBD, PN 170-39310-004, WORN OUT OF LIMITS WIDTH REDUCTION W .005 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-621 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDER 90SDR C77A20140121028Flap Track · wornRIGHT WING FLAP TRACK NR 1 INBD, PN 170-39310-003, WORN OUT OF LIMITS WIDTH REDUCTION W .003 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-620 IAW ETD 2011-170 01072E & EA E175-57-184 2 REV IR WORK ORDER 90SDR C77A20140121027Flap Track · wornLEFT WING FLAP TRACK NR 3 OTBD, PN 170-39314-001 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 737209-528 IAW ETD 2011-170 01072E & EA E175-57-184 1 REV IR WORK ORDER 906SDR C77A20140121026Flap Track · wornLEFT WING FLAP TRACK NR 3 INBD, PN 170-39315-001, WORN OUT OF LIMITS WIDTH REDUCTION W .002 INCHES IAW SRM 57-55-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-527 IAW ETD 2011-170 01072E & EA E175-57-184 1 REV IR WORK ORDER 906SDR C77A20140121025Flap Track · wornLEFT WING FLAP TRACK NR 2A OTBD, PN 170-39321-003 WORN OUT OF LIMITS THICKNESS REDUCTION D .016 INCHES IAW SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-526 IAW ETD 2011-170 01072E & EA E175-57-184 1 REV IR WORK ORDERSDR C77A20140121024Flap Track · wornLEFT WING FLAP TRACK NR 2 OTBD, PN 170-39312-003, WORN OUT OF LIMITS WIDTH REDUCTION W .012 INCHES IAW SRM 57-52-03 TABLES 102 & THICKNESS REDUCTION D .020 INCHES IAW SRM 57-52-03 TABLES 101. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 737209-52SDR C77A20140121023Flap Track · wornLEFT WING FLAP TRACK NR 2 INBD, PN 170-39313-003, 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 737209-523 IAW ETD 2011-170 01072E & EA E175-57-184 1 REV IR WORK ORDER 906SDR C77A20140121022Flap Track · wornLT WING FLAP TRACK NR 1 OTBD, PN 170-39310-003, WORN OUT OF LIMITS WIDTH REDUCTION W .003 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03 ON WORK ORDER 737209-521 IAW ETD 2011-170 01072E & EA E175-57-184 1 REV IR WORK ORDER 90630SDR C77A20140121020Flap Track · wornLEFT WING FLAP TRACK NR 1 INBD, WORN OUT OF LIMITS WIDTH REDUCTION W .003 INCHES IAW SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW SRM PART II 51-10-03.SDR FDEA201401180135Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE OTBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3.SDR FDEA201401180134Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE INBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. . BUSHING & WASHER FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2, 2B, 3, 4 & 5.SDR FDEA201401180133Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE OTBD ACTUATOR HOLE. WORN BUSHING ON OTBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED IAW EA 1-5750-87638C PART 2 TITLE, WINGS - TE & TE DEVICESSDR FDEA201401180132Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE INBD ACTUATOR HOLE. WORN BUSHING ON INBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED & INSTALLED IAW 1-5750-87638C PART 2 TITLE, WINGS - TE & TSDR SWIA201436276Support · gougedRT WING INBD FLAP VANE INBD ACTUATOR SUPPORT STRUCTURE IS GOUGED. C-CHECK REPAIRED RT WING INBD FLAP VANE ACTUATOR SUPPORT STRUCTURE GOUGE IAW REO.SDR SWIA201436275Support · gougedRT WING INBD FLAP VANE OTBD ACTUATOR SUPPORT STRUCTURE IS GOUGED. C-CHECK BLENDED RT WING INBD FLAP VANE OTBD ACTUATOR SUPPORT STRUCTURE IAW REO.SDR SWIA201436045Paint · defectiveEXCESSIVE RIGHT ROLL WITH FLAPS 45. REQUIRES APPROXIMATELY 65% LT WING DOWN TRIM. FLT 5591 INSPECTED ALL FLAP PANELS & FOUND NO DEFECTS. VERIFIED FLAP RIGGING GOOD. INSPECTED AILERONS, FOUND NO DEFECTS. ALL SPOILER PANELS STOW COMPLETELY AS REQUIRED. SANSDR IPXA2014021481927Skin · gougedLEFT CENTER FLAP UPPER SKIN REPAIR DOUBLER HAS GOUGES BETWEEN RIB 21 AND RIB 23, STRINGERS 2.6-2.7. ACCOMPLISHED REPAIR ON LT CENTER FLAP UPPER SKIN IAW EO A300-5750-53433-A, PARA 6A.SDR A6WA201401254529Skin Panel · damagedLIGHTNING BURN DAMAGE TO RT OTBD FLAP UPPER SKIN PANEL & TE. PERFORMED CHANNEL SPLICER & DOUBLER REPAIR IAW CRJ 200 SRM 57-53-00 REPAIR NR 3.SDR IPXA2014012081484Skin · dentedINSPECTION C09, DENT ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP AT AT IFS 142.25. REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 FIG 201, REV 58, & SRM 51-70-10-2R-2, REPAIR 2, FIG 203, REV 58.SDR IPXA4681483Skin · dentedINSPECTION C09, THREE DENTS ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV 58.0, SRM 51-70-10-2R-2 REPAIR 2, FIG 203, REV 58.00.SDR IPXA2014012081482Skin · dentedINSPECTION C09, DENT ON THE LT WING OTBD FLAP UPPER PANEL INNER SURFACE AT T/E FLAP STA 78.75. REPAIRED IAW -SRM 57-53-01-2R-1 REPAIR 1, FIG 201, REV.58, SRM 51-70-10-2R-2, REPAIR 4, FIGURE 201, REV 58.SDR IPXA2014012081481Skin · dentedINSPECTION C09, DENT ON THE T/E COVER PANEL UPPER SKIN OF LT WING INBD MAIN FLAP AT IFS 184.7. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1, FIGURE 201, REV 58.0 0. 2. SRM 51-70-05-0G-0-GENERAL, REV. 58.00.SDR YN8R2014011700004Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION FLAP TRACKS. R & R FLAP TRACKS.SDR YN8R2014011700003Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION OF 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.SDR YN8R2014011700002Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION ON 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.SDR YN8R2014011700001Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION ON FLAP TRACKS. R & R FLAP TRACKS.SDR SWAA2014013124734Fitting · crackedRT WING AFT FLAP TRACK FAIRING 643BB FWD INTERNAL FITTING CRACKED ON RT SIDE BELOW BUSHING. R & R FITTING IAW SRM & DRAWING.SDR AALA20140121003Skin · corrodedLT INBD MAIN FLAP UPPER SURFACE CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-57-033281.SDR 8EKA20140120001Flap · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND ON THE RT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR 8EKA20140120002Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR 8EKA20140120003Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR IPXA2014012081454Skin · dentedINSPECTION 2C, LEFT WING INBD FLAP UPPER SURFACE DENTED 12 INCHES FWD OF T/E AT CENTER OF FLAP. INSTALLED REPAIR IAW SRM 57-0 0-01, REPAIR 1, FIG 201. MAJOR REPAIR.SDR 8EKA20140120004Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR DALA14004475801Skin · damagedLEFT WING INBD MAIN FLAP, LOWER SURFACE FSTA 233 AREA DENTED AND DELAMINATED. REPAIRED AREA IAW SRM 51-70-10E AMM 51-21-10-377-039.SDR A6WA201401114531Vane · chafedRIGHT INBD FLAP VANE IS CHAFED TWO SPOTS, INBD & MIDDLE LE SECTIONS, AT FLAP STATIONS 58 & 110. R & R UNSERVICEABLE SECTIONS OF RT INBD FLAP VANE LE WITH NEW SERVICEABLE LE SECTIONS.SDR SWAA2014012724572Flap · corrodedRT WING NR 6 MID FLAP CORRODED. REPAIRED MID FLAP IAW CMM.SDR CA140113012Support · cracked(CAN) DURING A SCHEDULED INSPECTION, THE INBD FLAP HANGAR SUPPORT ON THE LT WING WAS FOUND CRACKED. THE FLAP HANGAR SUPPORT RIBS WERE REPLACED WITH NEW RIBS, PN 0523231-7, 0523231-8 TO RECTIFY THE DEFECTS.SDR FDEA201401100081Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR SCNA20140207021Skin · chafedRIGHT OTBD AFT FLAP LOWER SKIN CHAFED OVER OTBD EDGE OF CANOE. REPAIRED RT OTBD AFT FLAP LWR SKIN OVER OTBD EDGE OF CANOE FAIRING.
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