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 AALA2020071439015Trunnion · wornAIRCRAFT WAS GROUNDED: WHILE PERFORMING INSPECTION TASK CARD 26T50057066 MAINTENANCE FOUND THE LEFT WING TRAILING EDGE INBOARD FLAP TRUNNION WORN BEYOND LIMITS. REPLACED FLAP ASSEMBLY PER TASK CARD 26L00027003.SDR SWIA2020090952433Skin · corrodedRT INBOARD FLAP VANE LEADING EDGE INBOARD, MID, AND OUTBOARD DOUBLERS ARE CHAFED APPROX 1INL X .5INW X .015IND. C-CHECK RO 9/5/2020. REMOVED DAMAGED RT FLAP VANE LEADING EDGE SKINS, IAW CRJ 200 SRM, AS DOCUMENTED ON ATTACHED CONTINUATION CARD.SDR IPXA2020071057607Plate · crackedRIGHT WING OTBD FLAP R:61 ANGLE PLATE CRACKED, REMOVED & REPLACEDSDR SWIA2020090952432Skin · chafedLT WING INBOARD FLAP VANE LEADING EDGE SKIN HAS CHAFES AT THREE LOCATIONS: FS 6.0 MEASURING L= 1.051"; W= .455"; D= .008". FS 54.5 MEASURING L= 1.136", W= .377", D= .013". FS 91.0 MEASURING L= 1.134", W= .360", D= .005". C-CHECK RO 9/5/2020. REPLACED 3 EACSDR SWIA2020081251798Nut · corrodedRH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.0 HAS A CORRODED NUT ON THE LWR ATTACH BOLT. REMOVED AND REPLACED RH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.00 LWR ATTACH BOLT NUT AND WASHER P/N MS17826-8 AND P/N NAS1149D0863K REF AMM TASKSDR SWIA2020081251797Clamp · corrodedRH OB FLAPS MOST OB SKEW DETECTOR HARNESS HAS CORRODED CLAMP HARDWARE. REMOVED AND REPLACED RH OB FLAPS MOST OB SKEW DETECTOR HARNESS CLAMP HARDWARE (SCREW P/N NAS1801-3-7 AND WASHER P/N NAS1149D0332J ) REF CRJ 700 AMM TASK.SDR SWIA2020081251796Bolt · corrodedTHE FWD 2 MOUNT BOLTS OF THE LH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE 2EA FWD MOUNT BOLTS OF THE LH OB FLAPS OB HINGE BOX. REF CRJ700 AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.SDR SWIA2020081251795Bolt · corrodedTHE FWD 2 MOUNT BOLTS OF THE RH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE FWD 2EA MOUNT BOLTS OF THE RH OB FLAPS HINGE BOX. REF AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.SDR IPXA2020071857918Support Angle · crackedINSPECTION TYPE:2C, RT WING OTBD FLAP INBD FWD HINGE FAIRING AFT UPPER SUPPORT ANGLE WAS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-35-01.SDR 120B2020070800040Bushing · wornFLAP TORQUE TUBE ATTACH BRACKET DIAGONAL LINK HAS UP/DOWN PLAY AT BRACKET ATTACH POINT.SDR SWIA202052655Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA42654-SRM 57-52-01 784SK RT INBOARD FLAP-RI -FOUND DENT ON RT INBOARD FLAP ON UPPER SKIN 4.8" FROM TRAILING EDGE AND 23" FROM INBOARD EDGE OF FLAP. DENT IS WITHIN LIMITS, PER SRM 57-52-01. DENT MEASURES .065" DEEP ANSDR IPXA2020070757475Skin · dentedINSPECTION TYPE:SEGR/WING I/B FLAP LOWER SURFACE HAS SEVERAL DENTSREPAIRED PER EA 300-5750-27-A2474 & SRM 57-52-12-001, FIG 3, LHT3.SDR SWIA2020090252162Skin · dentedRIGHT INBOARD FLAP HAS FOUR SHARP DENTS ON THE LOWER SKIN. FIRST DENT .015" DEEP .250" LONG, 14.625" FROM TRAILING EDGE 5.25" FROM INBOARD RIB. SECOND DENT .008" DEEP .375" LONG, 15.375" FROM TRAILING EDGE 19.5" FROM INBOARD RIB. THIRD DENT .008" DEEP .375"SDR HALA2020070700139Vane · corrodedON OVERNIGHT, FOUND LEFT WING OUTBOARD FIXED FLAP VANE CORRODED AT THE INBOARD EDGE. REMOVED AND REPLACED LEFT OUTBOARD FIXED FLAP VANE IAW AMM 27-50-02. ADJUSTED THE LT OUTBOARD FIXED FLAP VANE IAW AMM 27-50-02. CHECKED GOOD. OKAY FOR SERVICE.SDR FDEA202007061451Skin · debondedRIGHT WING I/B FLAP LEADING EDGE LOWER SURFACE, AREA OF DISBONDING INLINE WITH CENTER TRACK OF AFT FLAP. REPAIRED RIGHT WING I/B FLAP LEADING EDGE LOWER SURFACE ROCK SHIELD IAW SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-06-0G.SDR UIEA2020070751403Skin · delaminatedLEFT WING OTBD FORE FLAP L/E, FOUND THE OTBD AREA DELAMINATED. THE DELAMINATED AREA WAS REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070751404Skin · delaminatedLEFT WING OTBD FORE FLAP L/E INBD AREA, FOUND DELAMINATION. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070751405Skin · delaminatedLEFT WING OTBD AFT FLAP T/E AREA, UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATED AREA WAS REPAIRED IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070761406Skin · delaminatedLEFT WING OTBD MID FLAP T/E AREA UPPER SURFACE WAS FOUND DELAMINATED. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791437Skin · delaminatedRIGHT WING INBD MID FLAP INBD L/E, FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791438Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATED FROM INBD 261". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791439Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E FOUND DELAMINATED FROM O/B 18". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791440Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E WAS FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791441Skin · dentedRIGHT WING, INBD AFT FLAP LOWER SURFACE, CENTER T/E SECTION WAS FOUND DENTED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PAR, 5A REV 88.SDR UIEA2020070762442Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATION FROM INBD 339 INCHES. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791443Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E FROM INBD 46 INCHES HAD DELAMINATION. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020007001444Skin · delaminatedRT WING O/B MID FLAP L/E FOUND DELAM. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506740-01 FOR REPAIR DETAILS.SDR UIEA2020070701445Skin · delaminatedRT WING I/B FORE FLAP FWD L/E FOUND DELAM FROM I/B 30". PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506765-01 FOR REPAIR DETAILS.SDR UIEA2020070701446Skin · delaminatedRT WING O/B FORE FLAP L/E FOUND DELAM FROM I/B 160". PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506732-01 FOR REPAIR DETAILS.SDR ABXA20200721142Flap Track · corroded#2 FLAP TRACK ASSY HOLE REPAIR. AIRCRAFT WAS GROUNDED.SDR U2RA20200902002Skin · dentedRIGHT WING INBOARD MID FLAP LOWER SKIN HAS MULTIPLE DENTS. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER EO 20219.SDR SWIA2020082151945Guide Plate · chafedLEFT WING INBOARD FLAP INBOARD FAIRING GUIDE PLATE ON THE OUTBOARD HINGE ARM IS CHAFED. REMOVED AND INSTALLED A NEW FAIRING GUIDE PLATE ON THE LEFT WING INBOARD FLAP INBOARD FAIRING GUIDE PLATE ON THE OUTBOARD HINGE ARM REF. SRMSDR SWIA2020082151911Vane · chafedLEFT WING INBD FLAP VANE LEADING EDGE CHAFFED ON INBD SIDE MARKED (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED LH WING INBOARD FLAP VANE CAP REF CRJ200 SRM, AND DWG. SEE ATTACHED TASK. SEE CONTINUE CARD FOR DETAILS.SDR P5CA2020070100235Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING (587PT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100236Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING (587QT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100237Fairing · delaminatedRT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100238Fairing · delaminatedRT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR P5CA2020070100239Fairing · delaminatedLT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION (FROM I/B 58"). PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.SDR UIEA2020063021337Attach Fitting · crackedONE CRACK FOUND ON THE LEFT WING INBD FLAP TRACK NR 4 FWD ATTACH SUPPORT FITTING OTBD ANGLE. THE ATTACH FITTING WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.SDR UIEA2020063021338Attach Fitting · crackedONE CRACK FOUND ON THE RIGHT WING INBD FLAP TRACK NR 4 FWD ATTACH SUPPORT FITTING OTBD ANGLE. THE ATTACH FITTING WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.SDR UIEA2020063021339Attach Fitting · crackedONE CRACK FOUND ON THE RIGHT WING INBD FLAP TRACK NR 4, FWD ATTACH SUPPORT FITTING INBD ANGLE. REPLACED AND INSTALLED A NEW ATTACH FITTING IAW SRM 51-10-02 AND SRM 51-40-02.SDR UIEA2020063041350Skin · delaminatedLEFT WING OTBD MID FLAP T/E UPPER SKIN FOUND DELAMINATED 156 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041351Skin · delaminatedLEFT WING OTBD MID FLAP T/E UPPER SKIN FOUND DELAMINATED 112 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041352Skin · delaminatedLEFT WING OTBD FORE FLAP L/E, INBD SURFACE FOUND DELAMINATED 98 INCHES TO I/B. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041353Skin · delaminatedRIGHT WING INBD FORE FLAP UPPER SURFACE T/E FOUND DELAMINATED 166 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041354Skin · delaminatedRHW I/B FORE FLAP FOUND DELAMINATED AT THE INBD L/E SURFACE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041355Skin · delaminatedRIGHT WING INBD FORE FLAP UPPER SURFACE T/E FOUND DELAMINATION, 141 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041356Skin · delaminatedRIGHT WING OTBD AFT FLAP UPPER SKIN T/E CTR SECTION FOUND DELAMINATED 84 INCHES FROM I/B EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041357Skin · delaminatedRIGHT WING OTBD MID FLAP T/E UPPER MID AREA FOUND DELAMINATION. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.SDR UIEA2020063041358Skin · delaminatedRIGHT WING OTBD MID FLAP L/E INBD SECTION FOUND DELAMINATION, 112 INCHES FROM INBD EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.
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