JASC 5753
Service difficulty reports · 31,521
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 04FDEA02224Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 3 PIVOT INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOASDR 04FDEA02223Fitting · corrodedRT WING INBOARD FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.878. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, TITLE: WINSDR 04FDEA02221Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.187 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD SDR 04FDEA02219Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.497, MATERIAL REMOVED = 0.026, REMAINING THICKNESS = 0.471 AND REPAIRED AS PER FEDEX EA 1-575SDR 04FDEA02217Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 2 ACTUATOR OUTBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OSDR 04FDEA02215Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.411, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5SDR 04FDEA02212Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARSDR 04FDEA02211Hinge · corrodedLT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 1 ACTUATOR INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT SDR 04FDEA02210Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAPSDR 04FDEA02209Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-SDR 04FDEA02198Hinge · crackedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) MIDDLE FITTING FOUND CRACKED. ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50-30-4 AND FLAP STRUCTURAL ADJUSTMENT/TEST CARRIED OUT AS PER MM 27-50-30-5, FOUND SATISFACTORY AND FLAP ADJUSTMENT/TEST CARRIED SDR AWXA200400859Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND SEPARATED AT THE AFT INBOARD CORNER, WATER WAS FOUND LEAKING FROM INSIDE FLAP AT SEPARATED SKIN, WBL 230.68 TO WBL 231.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT OUTBOARD FLAP SKIN AT AFT ISDR AWXA200400864Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT OUTBOARD FORE FLAP 106.5 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DAMAGED ON UPPER SURFACE OF LT OUTBOARD FORE FLAP FROM WBL 307.11 LT TO 413.61 LT; CLEANED AND PREPARSDR DHL2004804531Skin · wornLT WING IB FLAP UPPER SKIN WORN XW 91.000 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW ED EDW 27-4, DWG W27-R04 REV. IR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW ED EDW 27-4, DWG W27-R04. FABRICATED NEW PLATING SEGMESDR SWAA042112Spindle · failedINBOUND CREW REPORTED A HEAVY THUMP WHEN FLAPS 30 SELECTED. UPON INSPECTION, MX REPORTED RT OUTBOARD FLAP SPINDLE FAILURE. REMOVED AND REPLACED RT OUTBOARD FLAP SPINDLES PER MM.SDR CA040922003Pulley Bracket · failed(CAN) AFTER TAKE-OFF, WHEN RAISING FLAPS FROM 100 TO 00, PILOT FELT A RELEASE OF TENSION AND A/C BANKED LT, UNTIL FLAP HANDLE LOCKED IN AT 00 POSITION. PILOT CHECKED FLT CONTROLS & ALL APPEARED NORMAL, PILOT SUSPECTED SOMETHING WRONG WITH FLAPS. A/C FLOWN TO BSDR USAA040393Skin · delaminatedPIT - FOUND SKIN DELAMINATED 12 INCHES BY 3 INCHES WIDE DELAMINATED, LT WING T/E FLAP, TRAILING EDGE DELAMINATED, 15 INCHES FROM INBOARD END. REMOVED SKIN AND CORE, INSTALLED NEW SECTION AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)SDR SWAA042095Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD AFT T/E FLAP PER MM.SDR IXXA060415SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP TRAILING EDGE PANEL FITTING CRACKED AT STATION XW375. REPLACED FITTING PER ALL APPLICABLE DATA.SDR DL767040679Wedge · delaminatedIB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14.SDR 04FDEA02144Fitting · corrodedCOMPLY WITH EA 8-5750-79540; WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79540, WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177 AT MAE.SDR SWAA042075Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM.SDR SWAA042074Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM.SDR AWXA200400867Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP WAS FOUND DELAMINATED AT WBL 262.0, JUST ABOVE NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP AT WBL 262.0; CLEANED AND SDR DHL2004745534Skin · dentedDURING A C-CHECK, RT WING I/B FOREFLAP L/E HAS A DENT WS 335. DAMAGED FOUND TO BE OUT OF LIMIT IAW B727 SRM 57-50-1 FIG 3. CUT OUT DAMAGED AREA & FABBED FILLER FROM 2024 T3 .050 PO 900980 DIM 2.6875 INCH X 2.5 INCH & 2 EA DOUBLERS FROM 2024 T3 .063 PO 90079SDR SWAA042059Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.SDR DL767040671Support Beam · corrodedLEFT AND RIGHT INBOARD FLAP INBOARD AND OUTBOARD SUPPORTS CORRODED. REPAIRED IAW ERA 091244-14.SDR 04FDEA02137Stop Fitting · corrodedLEFT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02136Stop Fitting · crackedRIGHT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02135Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.403, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEXSDR 04FDEA02134Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.394 AND REPAIRED AS PER FEDEX EASDR 04FDEA02133Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TSDR 04FDEA02132Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02131Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.002, REMAINING THICKNESS=0.504, AND REPAIRED AS PER FEDEX EA NR 1-5SDR 04FDEA02130Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.503, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.499 AND REPAIRED AS PER FEDEX EA NSDR 04FDEA02129Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02128Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.095 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TRAILING SDR 04FDEA02127Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINSDR 04FDEA02126Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.405", MATERIAL REMOVED = 0.005, REMAINING THICKNESS=0.400, AND REPAIRED AS SDR 04FDEA02125Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED ASPER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER 1.062, FINAL DIAMETER 1.207, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: SDR 04FDEA02124Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02123Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED.SDR 04FDEA02122Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.505, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EASDR 04FDEA02121Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02120Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.510, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.507, AND REPAIRED AS PER FEDEX EA NR 1-SDR 04FDEA02119Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NO. 1-5750-77941. TITLE: WINGS - SDR 04FDEA02118Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.406, MATERIAL REMOVED=0.008, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEX ESDR 04FDEA02117Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - SDR 04FDEA02116Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.404, MATERIAL REMOVED=0.007, REMAINING THICKNESS=0.397 AND REPAIRED AS PER FEDEX ESDR 04FDEA02115Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.196 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AN
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