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 04FDEA01452Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.506, MATERIAL REMOVED : 0.007, REMAINING THICKNESS OF LUG: 0.506. REPAIR CARRIED OUT AS PER SDR 04FDEA01451Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.094. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGESDR 04FDEA01450Hinge · corrodedRIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.510, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.508. REPAIR CARRIED OUT AS PESDR DL738040464Spar · damagedRT IB MAIN FLAP FRONT SPAR LOWER CHORD FOUND TO BE DAMAGED. DAMAGE WAS LOCATED BETWEEN 26 INCHES AND 34 INCHES FROM THE IB END OF SPAR. DAMAGE WAS REMOVED AND REPAIR INSTRUCTION ISSUED IAW ERA 090294-14.SDR SWAA041492Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.SDR 04FDEA01449Hinge · corrodedRIGHT WING - INBOARD FLAP AFT OUTBOARD HINGE - FOUND INBOARD PIVOT BORE HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 - 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.252. COMPLIED WITH FEDEX EA 1-5750-76714, WINGSSDR DL73S040466Roller · out of positionDURING ROTATION A STRONG RT WING UP FORCE WAS ENCOUNTERED AS THE AIRCRAFT BECAME AIRBORNE. SUBSTANTIAL RT AILERON WAS NECESSARY TO KEEPS WINGS LEVEL. FOUND LT OB FLAP IB TRACK WITH BELLCRANK ROLLER OUT OF CAMTRACK. REPLACED BELLCRANK.SDR AWXA200400655Wedge · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK FOUND A DISBOND AREA ON THE LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END WBL 230.68 TO WBL 235.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END; FABRICATED A CORE FILLER AND REPAIRSDR 04FDEA01430Hinge · corrodedCOMPLY WITH EA 8-5750-77413 WING - RT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-77412.SDR 04FDEA01429Hinge · corrodedCOMPLY WITH EA 8-5750-77414, WING - OUTBOARD FLAP, REWORK OF POSITION INDICATION HOLE IN ARC1991 HINGE. COMPLIED WITH EA 8-5750-77414.SDR ASAA0480451Vane · nickedOKC - DURING HV-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD VANE IS NICKED AT LEADING EDGE. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M)SDR 2004UALA00484Fitting · crackedLEFT INBOARD T/E MAIN FLAP MIDDLE AFT FLAP HINGE FITTING CRACKED ON INBOARD SIDE NEAR FLAP AFT SPAR. INSTALLED ANGLE REPAIR.SDR 2004UALA00483Fitting · crackedRT WING INBOARD FLAP, MIDDLE T/E HINGE FITTING IS CRACKED AT SPAR. INSTALLED ANGLE REPAIR.SDR 04FDEA01413Hinge · corrodedWINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. COMPLIED WITH EA 8-5750-77415, WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE.SDR 04FDEA01410Strap · out of limitsLEFT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD STRAP P/N ARC 2517-1 IS OUT OF LIMITS IAW DC10 CMM 57-52-01. REMOVED OUT OF LIMITS STRAP, LOCATED AND DRILLED HOLES IN NEW STRAP IAW DAC DWG ARC 2512. LOCATED BUSHING HOLE IAW DAC DWG ARC 2512 AND EA 8-5710-77SDR 04FDEA01402Flap Track · wornLEFT HAND INBOARD FLAP TRACK HAS SIGNS OF WEAR (6 PLACES), MARKED. CHECKED LIMITS ON LEFT HAND INBOARD FLAP TRACK NUMBER 2 IAW DC10-10 F/E MM 27-50-03-2, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW DC10-10 MM 27-50-03-2 STEP 4B (2) (A).SDR 04FDEA01358Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX ALSDR 04FDEA01357Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX SDR DL738040485Spar · damagedREPAIR OF RIGHT INBOARD MAIN FLAP FRONT SPAR LOWER CHORD.SDR 04FDEA01353Carriage · corrodedLEFT O/B FLAP BOTH I/B AND O/B ROLLER CARRIAGES HAVE WORN AREAS AND CORROSION. REPLACED CARRIAGES ON W/C E 8- 5750-7-5000 PT 3 AT MAE.SDR 04FDEA01334Fitting · corrodedLEFT I/B FLAP SIDE LOAD ROLLER FITTING HAS CORROSION IN BORES AND IS CHAFED. REPLACED FITTING ON W/C E8-5750-7-5002 PT 1 AT MAE.SDR 04FDEA01333Bracket · chafedRIGHT I/B SIDE LOAD ROLLER BRACKET IS WORN/CHAFED. REPLACED BRACKET ON W/C E8-5750-75002 PT 2 AT MAE.SDR 04FDEA01332Mount · corrodedRIGHT I/B FLAP SIDE LOAD ROLLER FITTING MOUNT IS CORRODED. REPLACED ASSY ON WC E 8-5750-7- 5002 AT MAE.SDR MWEA040079Doubler · delaminatedRIGHT OUTBOARD FLAP CENTER FIXED VANE HAS A 5.2500 INCH SQUARE DELAMINATION 2.7500 INCH FORWARD OF TRAILING EDGE AT OB EDGE LOWER SURFACE. FABRICATED AND INSTALLED REPAIR FITTINGS AND DOUBLER.SDR SWIA200413320Rib · crackedLEFT NACELLE FLAP 3RD UPPER RIB SUPPORT (FROM OUTBOARD) CRACKED. DISCOVERED DURING A-CHECK INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH SERVICEABLE UNIT. REF MM 27-50-03.SDR 04FDEA01327Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01326Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01325Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.403, MATSDR 04FDEA01324Hinge · corrodedRIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.404, MSDR 04FDEA01323Spindle · wornLEFT O/B FLAP I/B ROLLER SPINDLE IS WORN AND IS CORRODED. REMOVED AND REPLACED SPINDLE ON W/C E 8-5750-7-5000 PT 3.SDR 04FDEA01322Stop Fitting · wornLEFT WING O/B FLAP O/B STOP WORN AND MISSING. REMOVED AND REPLACED STOP AT MAE.SDR 04FDEA01321Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.504, MASDR 04FDEA01319Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.477, MASDR 04FDEA01318Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER HOSDR 04FDEA01317Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: SDR 04FDEA01315Hinge · corrodedRIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORROSION REMOVED AS PER CMM 20-SDR 04FDEA01312Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01311Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.21SDR 04FDEA01310Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.402, MATERIAL REMOVED: 0.003, REMAINING THICKNESSSDR 04FDEA01309Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.408, MATERIAL REMOVED: 0.007, REMAINING THICKNESS: SDR 04FDEA01308Hinge · corrodedRIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.093. REPAIRED AS PER EA 1-5750-76672SDR 04FDEA01307Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76672. RSDR 04FDEA01306Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESDR 04FDEA01305Hinge · corrodedRIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.492, MATERIAL REMOVED AT O/B FACE: 0.021, I/SDR 04FDEA01304Hinge · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.092. REPAIRED AS PER EA 1-5750-76671SDR 04FDEA01303Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.094, FINAL DIAMETER: 1.096. REPAIRED AS PER EA 1-5750-76671. SDR 04FDEA01302Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.498, MATERIAL REMOVED: 0.002, REMAINING THICKNESSDR 04FDEA01301Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.496, MATERIAL REMOVED AT O/B FACE: 0.004, I/B FACSDR 04FDEA01300Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. O/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.395, MATERIAL REMOVED: 0.002, REMAINING THICKNESS:SDR 04FDEA01299Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. I/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.392, MATERIAL REMOVED: 0.002, REMAINING THICKNESS:
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