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 SWAA042771Skin · crackedDURING SCHEDULED 5Y CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED LT WING INBOARD AFT FLAP PER SRM.SDR UIEA200400160Fairing · wornDURING SCHEDULED MAINTENANCE, FOUND NR 1 MOVABLE CANOE PRIMARY DOOR FAIRING BEARINGS WORN. HOLE ELONGATION WAS FOUND IN TWO LOCATIONS. OVERSIZED THE HOLES TO A MAXIMUM DIAMETER OF .7827 INCHES. DRY PNETRANT INSPECTED THE AFFECTED AREA TO ENSURE DEFECT FREE SDR 04FDEA02792Stop Fitting · crackedLEFT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING FOUND CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.SDR 04FDEA02791Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINSDR 04FDEA02790Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 SDR 04FDEA02785Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.504 INCH, REMAINING THICKNESDR 04FDEA02789Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02788Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02787Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02786Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02759Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.18SDR 04FDEA02757Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.SDR 04FDEA02755Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.095 INCH AND REPASDR 04FDEA02753Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.079 INCH, FINAL DIAMETER=1.081 INCH AND REPASDR 04FDEA02768Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCHSDR 04FDEA02767Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL TSDR 04FDEA02766Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INSDR 04FDEA02764Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINSDR 04FDEA02763Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NSDR 04FDEA02762Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.503 INCH, REMAINING THICKNESS=0SDR 04FDEA02761Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.089 INCH, FINAL DIAMETER=1.091 INCH AND REPAIRED ASDR 04FDEA02760Hinge Bracket · corrodedRT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.505 INCH, REMAINING THICKNESSSDR 04FDEA02758Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGSDR 04FDEA02756Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. SDR 04FDEA02754Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.501 INCH, REMAINING THICKNESDR 04FDEA02752Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.509 INCH, REMAINING THICKNSDR 04FDEA02784Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02782Hinge · corrodedSNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749.SDR 04FDEA02781Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02780Hinge · corrodedSNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749.SDR 04FDEA02779Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02778Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02777Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02776Hinge · corrodedSNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02775Hinge · corrodedSNRM NR N0484 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, OB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR BJNA040907Skin · damagedFOUND THE LEFT INBOARD FORE FLAP TRAILING EDGE DAMAGED FROM POSSIBLE FOD. REMOVED AND REPLACED THE LEFT INBOARD FORE FLAP IAW THE AMM 27-51-41. (M)SDR 04FDEA02726Stop Fitting · crackedRT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING CRACKED. RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME 1.SDR SWAA042708Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E FLAP PER MM.SDR MALA040722Tab · chafedDURING C1 INSPECTION IN YYC, RIGHT IN BOARD FLAP TAB LEADING EDGE HAS CHAFING. MAINTENANCE REPAIRED IAW EO A57073. AIRCRAFT RETURNED TO SERVICE 9/25/04.SDR 04FDEA02684Block · wornON TAKEOFF AT 200 FT GOT STALL WARNING AND SLAT DISAGREE. CLEANED UP PER CHECK LIST. KEPT GETTING PSEU FAIL LEVEL 1 AND SLAT DISAGREE LEVEL 2. ALERT IN CLEAN CONFIG. DIVERT TO MEM. DUMPED 19K LBS OF FUEL NORTH MEM. FOUND NR 4 SLAT, NR 10 TRACK WITH EXCESSDR P5CA0401208Skin · corrodedLT WING MID FLAP ENTIRE CENTER SECTION PANEL HAS SEVERAL CORROSION SPOTS. REMOVED SURFACE CORROSION , PRIMED AND TREATED.SDR SWAA042661Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM.SDR MALA040718Tab · chafedDURING C1 INSPECTION IN YYC, LEFT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT INBOARD ATTACH POINT. MAINTENANCE REPAIRED IAW EO A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04.SDR IXXA060588SSkin · gougedDURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP TOP SKIN GOUGED AT STATION XF 90. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-21.SDR GAIA04106Skin · dentedDURING C-CHECK INSPECTION FOUND RT OB AFT FLAP TRAILING EDGE DENTED. REF FASI NR, ACCOMPLISHED BONDED DOUBLER REPAIR IAW SRM 57-50-3, FIG 4.SDR GAIA04100Skin · debondedDURING C-CHECK INSPECTION, FOUND RT OB MID FLAP UPPER SKIN DISBONDED. REF FASI NR 86359, ACCOMPLISHED BONDED DOUBLER REPAIR IAW SRM 57-50-2, FIG 3.SDR SWAA042630Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING T/E AFT INBOARD FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR USAA040806Skin · debondedPIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.SDR UPS04243243Skin · delaminatedINSPECTION TYPE:C, DELAM ON RIGHT O/B MIDFLAP T/E WEDGE FWD FACE I/B OF NR 2 AFT FLAP TRACK. DELAM OUT OF LIMITS. MIDFLAP REPLACED IAW MM 27-51-12.SDR AWXA200401047Wedge · delaminatedDURING C-14 CHECK FOUND THE RT WING OB AFT FLAP DELAMINATED ON THE TRAILING EDGE IB CORNER. MAINTENANCE CUTOUT DAMAGE ON RT WING OB AFT FLAP AT TRAILING EDGE IB CORNER; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRM 51-70-10, FIG. 31.
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