N610FE

Service difficulty reports · 497

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N610FE' AND registry_match = 'registration'
  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.

SDR FDEA201203140933Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP HINGE, CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. REPAIR CARRIED OUT IAW STEP 1, 2, 9, 10, 11 AND 12 OF EA 1-5750-150447, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 14, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203140931Vane · corrodedRT WING OTBD FLAP VANE FITTING, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-150450. PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Mar 14, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203140934Bushing · wornRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIA 1.224" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-04, REV 72 , MAX ALLOWABLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW Mar 14, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203140932Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.223", FINAL HOLE DIA. 1.249" , MAX ALLOWABLA DIA 1.220" REPAIR CARRIED OUT IAW STEP 1,2,9,10,11 AMar 14, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203130912Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING F ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02 FIG 201, REV 48 EXISTING HOLE:0.851"(LENGTH), 0.557"(WIDTH). FINAL HOLE 0.944"(LENGTH), 0.660"(WIDTH). MAXIMUM HOLE 0.940"(LENGTH), 0.670"(WIDTH).REPAIR Mar 13, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203130911Fitting · corrodedLEFT WING OTBD FLAP VANE FITTING B ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48 EXISTING HOLE:0.873"(LENGTH), 0.623"(WIDTH). FINAL REWORK HOLE 0.930"(LENGTH), 0.706"(WIDTH). MAXIMUM REWORK HOLE 0.940"(LENGTH), 0.640"Mar 13, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203120888Hinge · damagedRT WING OTBD FLAP, OTBD HINGE BUSHING ON PIVOT HOLE REMOVED IAW CMM 20-20-07, REV 72 . BORE MEASURED DIA 2.315" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 MAX ALLOWABLE, DIA 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW STEP 10 AND 11 OF EA 1-57Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120894Skin · chafedLT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT FOUND CHAFED. REPAIRED IAW SRM 51-31-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 12, 2012 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201203120893Hinge Fitting · damagedLT WING (FLAP SIDE) INBD FLAP OTBD HINGE INBD PIVOT HOLE FOUND STEP HOLE. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . EXISTING HOLE DIA 1.190", /1.253" , MAXIMUM HOLE DIA 1.220" BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-150446, PART 1 Mar 12, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203120892Bushing · wornLT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 72 EXISTING HOLE DIA 1.283", MAX ALLOWABLE HOLE DIA 1.220" HOLE MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . BUSHING FABRICATED AND INSTALLEDMar 12, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203120890Bushing · wornRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE INBD PIVOT HOLE BUSHING WORN. BUSHING REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA 1.283", MAX HOLE DIA 1.220", NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 AND 5. REPAIR CLMar 12, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203120889Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE FOUND STEP HOLE. REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA.1.282" /1.192", MAX ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 ANMar 12, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203120885Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE PIVOT HOLE FOUND EXCEEDED CMM LIMITS AFTER BUSHING REMOVAL FOR NDT ACCESS. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 2.315" MAX ALLOWABLE DIA 2.3135'. REPAIR CARRIED OUT IAW EA 1-57Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120883Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 0.582', FINAL HOLE DIA 0.598", MAX. ALLOWABLE DIA 0.584' REPAIR CARRIED OUT IAW EA 1-5750-150447, PARMar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120882Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA 0.585", FINAL HOLE DIA. 0.598", MAX ALLOWABLE HOLE DIA.0.584" REPAIR CARRIED OUT IAW STEP 3 OF EA 1-5Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120881Hinge Fitting · corrodedRT WING (WING SIDE) OTB FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-09, REV 72. EXISTING THK UPPER:0.412", LOWER:0.408". REMAINING THK UPPER:0.407", LOWER:0.403'. MATERIAL REMOVED: UPPER: 0.005", LOWER:0.005" IAW STEP Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120880Bushing · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72. BORE MEASURED DIA 1.223", AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAX ALLOWABLE DIA 1.220", WASHER INSTALLED IAW EA 1-5750-160003, PARMar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120879Hinge Fitting · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72 BORE MEASURED DIA 1.222", AND FOUND EXCEEDED LIMIT IAW 1 CMM 57-44-08 REV 72. MAX ALLOWABLE DIA.1.220" .BUSHING FABRICATED AND INSTALLED IAW STEP 5 Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203120878Hinge Fitting · corrodedRIGHT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.355", REMAINING THICKNESS UPPER: 0.365", LOWER: 0.345", MATERIAL REMOVED UPPER: 0.010", LOWER Mar 12, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090844Longeron Splice · crackedDURING X-RAY INSPECTION, FOUND A CRACK ON STA 5-123, LONGERON SPLICE 2 LT. LONGERON REMOVED IAW SRM 51-31-01, REV 48. NEW LONGERON SPLICE FABRICATED IAW DWG A5A7111-501, REV C. NEW FABRICATED LONGERON SPLICE INSTALLED IAW SRM 51-31-01, REV 48. REPAIR CLASMar 9, 2012 · N610FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203090843Bushing · migratedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE PIVOT HOLE REPAIR BUSHING FOUND MIGRATED. REPAIRED IAW EA 1-5750-160002 STEP 3, 7, 8 AND 9 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090842Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, STEP 4 AND 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090841Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2,7,8,9 AND 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090840Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2.Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090839Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE, INBD ACTUATOR, HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 1, 7, 8 AND 9 .Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090838Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. REPAIRED IAW EA1-5750-160002, PART 1 STEP 1, 7, 8 AND 9 .Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090837Bushing · wornLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE INBD ACTUATOR HOLE BUSHING WORN. MEASURED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.254", MAX HOLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW STEP 9 AND 10. WASHER FABRICATED IAW SMar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090836Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA. 0.398", FINAL HOLE 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED PER STEPMar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090835Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA. 0.398", FINAL HOLE DIA. 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED IAW Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090834Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW REV 72 UPPER FACE EXISTING THICKNESS: 0.413", MATERIAL REMOVED :0.003", REMAINING THICKNESS :0.410", LOWER FACE EXISTING THICKNESS: 0.410", MATERIAL REMOVED :0Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090833Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. MAX ALLOWABLE DIA.0.584", EXISTING HOLE DIA 0.538", FINAL HOLE DIA 0.595", BUSHING FABRICATED AND INSTALLED IAW STEP Mar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203090832Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 0.585", FINAL HOLE DIA.0.597", MAX HOLE DIA 0.584". BUSHING FABRICATED AND INSTALLED AS IAW STEMar 9, 2012 · N610FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203070796Attach Fitting · crackedRIGHT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. ATTACH FITTING REMOVED AND REPLACED AS PER EA 1-5750-160011.Mar 7, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203070795Attach Fitting · crackedLEFT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER EA 1-5750-160010. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 114.Mar 7, 2012 · N610FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203060790Skin · crackedRIGHT WING FIXED L/E SKIN FOUND CRACKED AT NR 8 SLAT TRACK CUTOUT INBD SIDE, LOWER CORNER. REPAIR CARRIED OUT AS PER SRM 57-40-02 REPAIR 7 FIG.201 REV 48. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.Mar 6, 2012 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201203050779Roller Tray · corrodedCENTER CARGO COMPARTMENT STA 1701, X=-58 (APPROX) FOUND ROLLER TRAY WITH SURFACE CORROSION. NEW ROLLER TRAY REWORKED AS PER DRAWING AFJ7063 REV. A NEW ROLLER TRAY INSTALLED AS PER AMM 20-50-02 REV 72 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 114.Mar 5, 2012 · N610FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201203050778Beam · crackedL3 DOOR NR 2 STOP BEAM FOUND CRACKED. STOP BEAM REMOVED AND REPLACED AS PER SRM 51-31-01 REV 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 114.Mar 5, 2012 · N610FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201203050777Skin · crackedLT WING NR 5 L/E SLAT OTBD TRACK CUTOUT LOWER OTBD CORNER FOUND CRACKED. REPAIR CARRIED IAW SRM 57-40-02 REPAIR 7 FIG.201 REV 48 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.Mar 5, 2012 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201203050776Access Panel · crackedLT WING L/E LOWER SURFACE ACCESS PANEL 519CB FWD INBD CORNER, FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 REPAIR 7 FIG.201 REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV.114Mar 5, 2012 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012014530Pressure Switch · failedDUE TO ENG NR 3 FUEL FILTER AND MASTER CAUTION LIGHT . SPEED 50 KTS. NO MAX BREAKING RECEIVED. R & R FUEL FILTER PRESSURE SWITCH.Dec 1, 2010 · N610FE · Doug MD11F · Engine Fuel DistributionSDR FDEA201003220955Bushing · damagedLT HORIZ STABILIZER INBD L/E 2 EACH BUSHING FOUND DAMAGED. REPAIRED AS PER EA1-5510-132389.Mar 22, 2010 · N610FE · Doug MD11F · Horizontal Stabilizer StructureSDR FDEA201003200945Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 55 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200944Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 10 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200943Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 8 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION ON (2) LOCATIONS. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200942Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -35 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIRED AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200941Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -37 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200940Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -55 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT (3) LOCATIONS. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200939Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX. 'X' = -60 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT THREE (3) LOCATIONS. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200938Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROXIMATELY 'X' = -90 CENTER TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT ONE (1) LOCATION. REPAIR AS PER EA 1-5710-132380.Mar 20, 2010 · N610FE · Doug MD11F · Fuel StorageSDR FDEA201003200937Fuel Tank · corrodedMAIN DECK CARGO - STA 1229 'X' = -100 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT (2) LOCATIONS. REPAIR AS PER SRM 51-21-01 REV 43 AND SRM 57-10-01 REV 43.Mar 20, 2010 · N610FE · Doug MD11F · Fuel Storage
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