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 C77A20140328017Flap Track · wornRT FLAP NR 2 OTBD FLAP TRACK, PN 170-39312-004, HAS WIDTH REDUCTION OF .005 INCHES, OUT OF LIMITS IAW E175 SRM 57-52-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-634 IAW ETD 2011-170 01072E & EA E175-57-188 2 REV IR WORK ORDER 1419937.SDR C77A20140328016Flap Track · wornRT FLAP NR 3 INBD FLAP TRACK, PN 170-39315-002 HAS WIDTH REDUCTION OF .002 INCHES OUT OF LIMITS IAW SRM 57-55-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-633 IAW ETD 2011-170 01072E & EA E175-57-188 2 REV IR WORK ORDER 1419937.SDR C77A20140328015Flap Track · wornRT FLAP NR 3 OTBD FLAP TRACK, PN 170-39314-002 HAS WIDTH REDUCTION OF .002 INCHES, OUT OF LIMITS IAW E175 SRM 57-52-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-631 IAW ETD 2011-170 01072E & EA E175-57-188 2 REV IR WORK ORDER 1419937.SDR C77A20140328014Flap Track · wornRT FLAP NR 4 INBD FLAP TRACK, PN 170-39315-002, HAS WIDTH REDUCTION OF .002 INCHES, OUT OF LIMITS IAW SRM E175 57-55-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-630 IAW ETD 2011-170 01072E & EA E175-57-188 2 REV IR WORK ORDER 1419937.SDR C77A20140328013Flap Track · wornLT FLAP NR 1 OTBD FLAP TRACK, PN 170-39310-005 HAS WIDTH REDUCTION WEAR OF .006 INCHES, OUT OF LIMITS IAW E175 SRM 57-52-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-545 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WORK ORDER 1419SDR C77A20140328012Flap Track · wornLT FLAP NR 2A OTBD FLAP TRACK, PN 170-39321-003 HAS WIDTH REDUCTION WEAR OF .024 INCHES, OUT OF LIMITS IAW SRM 57-52-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-540 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WORK ORDER 1419936.SDR C77A20140328011Flap Track · wornLT FLAP NR 2 OTBD FLAP TRACK, PN 170-39312-003 HAS WIDTH REDUCTION WEAR OF .022 INCHES, OUT OF LIMITS IAW E175 57-52-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-539 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WORK ORDER 1419936.SDR C77A20140328010Flap Track · wornLT FLAP NR 3 INBD FLAP TRACK, PN 170-39315-001 HAS FLANGE WIDTH REDUCTION WEAR OF .004 INCHES, OUT OF LIMITS IAW E175 SRM 57-55-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-538 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WORK ORDSDR C77A20140328009Flap Track · wornLT FLAP NR 3 OTBD FLAP TRACK, PN 170-39314-001 HAS FLANGE WIDTH REDUCTION WEAR OF .001 INCHES, OUT OF LIMITS IAW E175 SRM 57-55-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-536 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WORK ORDSDR C77A20140328008Flap Track · wornLT FLAP NR 4 INBD FLAP TRACK, PN 170-39315-001, HAS SIDE FLANGE WIDTH REDUCTION WEAR OF .002 INCHES, OUT OF LIMITS IAW E175 SRM 57-55-03. BLENDED WORN AREAS IAW SRM PART II 51-10-03 ON WORK ORDER 740147-535 IAW ETD 2011-170 01072E & EA E175-57-188 1 REV IR WOSDR C77A20140328006Skin · damagedLT WING INBD MAIN FLAP ACCESS PANEL 561BB CUT OUT HAS TWO DAMAGED FASTENER HOLES, ONE MISSING A FASTENER INSERT. REPAIRED DAMAGE TO COMPOSITE STRUCTURE IAW SRM 51-71-09 ON WORK ORDER 740147-554 IAW ETD 2014-170-024381 & EA E175-57-189 REV IR WORK ORDER 142007SDR C77A20140328005Skin · wornLT WING INBD MAIN FLAP ACCESS PANEL 561BB CUT OUT HAS TWO DAMAGED FASTENER HOLES, ONE MISSING A FASTENER INSERT. REPAIRED DAMAGE TO COMPOSITE STRUCTURE IAW SRM 51-71-09 ON WORK ORDER 740147-554 IAW ETD 2014-170-024381 & EA E175-57-189 REV IR WORK ORDER 142007SDR DALA14019521812Fairing · delaminatedINBD MAIN FLAP L/E OTBD FAIRING FOUND DELAMINATED. LT WING INBD MAIN FLAP L/E OTBD FAIRING COMPOSITE PREPREG HOT BOND. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05, PAR.5A, 1 AND REF PROCESS CARD :KEW514086-01.SDR DALA14019531812Fairing · delaminatedRIGHT WING INBD MAIN FLAP L/E OTBD FAIRING FOUND DELAMINATED. RT WING INBD MAIN FLAP L/E OTBD FAIRING COMPOSITE PREPREG HOT BOND. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05 PAR 5A(1) AND REF PROCESS CARD KEW514094-01.SDR CA140402008Roller · worn(CAN) AFTER FINDING A FAILED ROLLER AND WORN INSIDE FLAP WALL, CHECKED ALL ACFT AND RT OTBD FLAP WAS FOUND OF THIS ACFT WAS ALSO FOUND WORE AND READY TO FAIL. BECAUSE OF HIGH CYCLES AND HOURS ON OUR ACFT EACH YEAR. WE WILL REMOVE ALL FLAPS AND REPLACE ROLLESDR FDEA201403270591Pivot Assy · wornRT WING INBD FLAP AFT, FLAP SIDE OTBD HINGE PIVOT FOUND EXCEED LIMITS AFTER WORN BUSHING REMOVED. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750-87612B PART 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403270590Pivot Assy · wornLT WING INBD FLAP AFT FLAP SIDE OTBD HINGE PIVOT FOUND EXCEED LIMITS AFTER WORN BUSHING REMOVED. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750- 87606C PART 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR ASOA20140327032Structure · damagedFLAP FAILED AT 8 DEGREES DURING TAKEOFF. MAINTENANCE COMPLIED WITH GVI OF FLAPS AND SURROUNDING AREA OF DAMAGE. MAINTENANCE R & R RT INBD FLAP IAW AMM 27-50-00, ZERO RIG AND OPS CHECKED GOOD. APPROVED FOR RETURN TO SERVICE.SDR CA140326023Flap Track · corroded(CAN) ACFT REPORTED CORROSION BETWEEN THE FLAP TRACK NR 3 AND FLAP TRACK SUPPORT BEAM. ON IDENTIFYING THE CORROSION, THE BEAM WAS BLENDED TO DEPTHS UP TO 0.01 AND IN COMBINATION WITH ACFT VIBRATIONS RESULTED IN CRACKING. A TRIAGE WAS CONDUCTED ON THE ISSUE ASDR FDEA201403260592Skin · dentedDENT IN LOWER SURFACE OF LT WING OTBD AFT FLAP. LWS 415, APPROXIMATELY 18 INCHES OTBD OF THE AFT FLAP INBD EDGE. REPAIRED IAW SRM 57-53-01 REP 1 FIG 201 TABLE II & SRM 51-70-17.SDR SWAA2014032726569Angle · crackedLEFT WING FORE FLAP TE SHELF PANEL ANGLE CRACKED. R & R ANGLE IAW SRM.SDR FDEA201403250580Pivot Assy · corrodedRIGHT WING OTBD FLAP, AFT INBD HINGE PIVOT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW CMM 57-52-04 REVISION 78 AND EA 1-5750-T0306920 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403250579Pivot Assy · corrodedLEFT WING OTBD FLAP, AFT OTBD HINGE PIVOT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW CMM 57-52-04 REVISION 78 AND EA 1-5750-T0306919 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403240556Hinge Fitting · corrodedLEFT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM SDR SWAA2014041026996Skin · delaminatedRIGHT WING OTBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR IPXA2014040982571Skin · dentedINSPECTION 3C, RT WING INNER FLAP LOWER SKIN BETWEEN RIBS 14-17, S2.7-2.10 HAS DENT/CHAFE. REPAIRED RT WING FLAP LOWER SKIN IAW EA 300-5750-01-A5223-IR AND EO A300-5750-54019-A.SDR SWAA2014040326803Skin · delaminatedRIGHT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2014033126655Flap · delaminatedRIGHT WING TE OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2014033126654Flap · delaminatedLEFT WING OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR IPXA201404182711Skin · gougedDURING 10 YEAR INSPECTION, LT WING CENTER FLAP UPPER SURFACE REPAIR DOUBLER IS GOUGED BETWEEN RIB 15 AND 16. ACCOMPLISHED REPAIR ON LT WING CENTER FLAP UPPER SKIN BETWEEN RIB 15 AND 16 IAW SRM 57-50-00, FIG 205, REV 25.SDR IPXA201404182699Skin · corrodedLEFT OTBD FLAP T/E UPPER SKIN HAS CORROSION UNDER STATIC DISCHARGE RETAINER BASE ACCOMPLISHED REPAIR ON LT OTBD FLAP T/E UPPER SKIN UNDER STATIC DISCHARGE RETAINER BASE IAW EO A300-5750-53941-A, PARA 6A.SDR SWAA2014032426414Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW MM.SDR SWIA201436931Vane · gougedINBD LT INBD MOST FLAP VANE GOUGED. C-CHECK, BLENDED GOUGED AREA ON INBD LT INBD MOST FLAP VANE IAW SRM AND REO.SDR SWIA201436930Vane · gougedINBD LT MID FLAP VANE GOUGED. C-CHECK, BLENDED GOUGED AREA ON INBD LT MID FLAP VANE IAW SRM AND REO.SDR SWIA201436929Vane · gougedINBD LT OTBD FLAP VANE GOUGED. C-CHECK, BLENDED GOUGED AREA ON INBD LT OTBD FLAP VANE IAW SRM AND REO.SDR SWIA201436928Vane · gougedINBD RT INBD MOST FLAP VANE GOUGED. C-CHECK, BLENDED GOUGED AREA INBD RT INBD MOST FLAP VANE IAW SRM AND REO C.SDR SWIA201436927Vane · gougedINBD RT MID FLAP VANE GOUGED. C-CHECK BLENDED GOUGED AREA ON INBD RT MID FLAP VANE IAW SRM AND REO.SDR SWIA201436926Vane · gougedINBD RT OTBD FLAP VANE GOUGED. C-CHECK, BLENDED GOUGED AREA ON INBD RT OTBD FLAP VANE IAW REO.SDR SWAA2014032426461Flap · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED. R & R FORE FLAP IAW MM.SDR SWAA2014062329294Fairing · delaminatedLEFT WING INBD FLAP OTBD TRACK FAIRING INBD LOWER SURFACE DELAMINATED. REPAIRED FAIRING IAW EA.SDR SWIA201436992Skin · chafedRIGHT INBD FLAP BONDING WIRE CHAFING INTERIOR SKIN AT MID VANE ACTUATOR. C-CHECK, REMOVED CHAFE IAW REO.SDR SWIA201436991Vane · chafedLEFT INBD FLAP VANE CHAFED ON L/E AT INBD END. C-CHECK, R & R FLAP VANE CAP IAW SRM AND REO.SDR SWIA201436990Vane · chafedRIGHT INBD FLAP VANE CHAFED ON L/E AT INBD END. C-CHECK, CHAFE BLENDED IAW REO.SDR SWIA201436989Vane · chafedLEFT INBD FLAP VANE L/E CHAFED AT CENTER. C-CHECK, CHAFE BLENDED IAW REO.SDR SWIA201436988Vane · chafedLEFT INBD FLAP VANE L/E CHAFED AT OTBD END. C-CHECK, CHAFE REMOVED IAW REO AND SRM.SDR SWIA201436987Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED AT CENTER. C-CHECK, CHAFING BLENDED IAW REO.SDR SWIA201436986Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED AT OTBD END. C-CHECK, CHAFING BLENDED IAW REO.SDR DALA14017565804Skin · dentedDENT ON LT WING INBD MAIN FLAP UPPER SURFACE, MF STA 235, 17 INCHES FROM T/E. REPAIRED FLAP IAW SRM 51-70-10.SDR CA140402007Bearing · worn(CAN) THE ACFT WAS COMING IN TO LAND AND WHEN APPROACH FLAPS WERE SELECTED, THE ACFT ROLLED SLIGHTLY. THE PILOT LANDED THE ACFT WITHOUT NO OTHER PROBLEMS. THE PILOT CHECKED THE FLAPS AND FOUND THE RT OTBD INNER ROLLER HAD FAIL AND RUBBED THOUGH THE INSIDE WALSDR SWIA201436994Skin · chafedRIGHT WING INBD FLAP, UPPER SKIN IS CHAFED 45-57" AND 70" FROM INBD END OF FLAP AND 8" AFT OF L/E OF FLAP. C-CHECK, BLENDED CHAFE AND REPAIRED FLAP IAW EA.
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