Construcciones Aeronauticas C-212-200

Service difficulty reports · 83

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'C212200'
  ORDER BY difficulty_date DESC"

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SDR JTAA20260821001Engine · making metalNR 2 ENGINE FAILED IN FLIGHT. ON INSPECTION FOUND METAL PARTICLES IN OIL FILTER BOWL.Aug 21, 2026 · N309HG · Casa C212200 · Engine (Turbine/Turboprop)SDR UATA2420714265701Rib · buckledLEFT WING HAS BUCKLED RIB AND WRINKLED SKIN AT WING STATION 6500. CAUSE/TIMEFRAME OF DAMAGE UNKNOWN. WING APPEARS TO HAVE ENDURED IMPACT ON BOTTOM OF WING TIP AREA. SFP APPROVED BY ANC FSDO FOR RELOCATION TO GREYBULL, WY FOR REPAIRS.Jul 8, 2026 · N424CA · Casa C212200 · Wing, Rib/BulkheadSDR UATA2870513265701Stiffener · crackedFOUND A CRACK IN STIFFENER ON THE LH WING FALSE SPAR AT W.S. 4900. THE CRACKED STIFFENER WAS R&R WITH NEW, FABRICATED STIFFENER MADE FROM 2024-T3 ALUMINUM .032" THICK, THE PRE-EXISTING SPACER HAD NO DAMAGE AND WAS REUSED. THE NEW STIFFENER WAS PRIMED WITH SUPEMay 6, 2026 · N439RA · Casa C212200 · Wing Main, Frame StructureSDR UATA2420127265305Floorbeam · collapsed- F15 WEB SAGGING UNDERFLOOR - REMOVED FRAME15 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.084 THICK, 38.5 INCHES LONG. STRAIGHTENED OUT THE WEB ON FRAME 15. FABRICATED A DOUBLER FROM 2024 T3, 0.032" THICK MEASURING 38.5" LONG X 3 1/4Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor BeamSDR UATA2420127265304Floorbeam · corrodedF16 TOP CAP CORRODED AT NUT PLATES. REMOVED FRAME 16 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.100 THICK. ETCHED AND ALODINED THE "T" ANGLE AND PRIMED WITH SUPER KOROPON EPOXY PRIMER. INSTALLED THE "T" ANGLE USING MS20470AD-4 AND MSJan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor BeamSDR UATA2420127265303Floorbeam · buckledF12 BUCKLED UNDER FLOOR. F12 UNDERFLOOR T ANGLE CENTER CAP - REMOVED DAMAGED T ANGLE. FABRICATED NEW T ANGLE FROM 2024T3 .085" X 1 5/8" X 1" TO SAME SIZE, DESIGN, AND HOLE PATTERN AS PREVIOUSLY INSTALLED. FABRICATED REPAIR DOUBLER 4 1/2"X 39 1/2" ALL NEW PARTSJan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor BeamSDR UATA2420127265302Floorbeam · corrodedF11 CAP CORRODED BETWEEN SEAT RAILS. FL 1 UNDERFLOOR T ANGLE CENTER CAP - REMOVED FRAME 11 CAP SPLICE SECTION. FABRICATED NEW CAP SPLICE SECTION FROM 2024T351 0.125" X 1 5/8" X 1" ALUMINUM TO SAME SIZE, DESIGN, AND HOLE PATERN AS PREVIOUSLY INSTALLED. PARTS WEJan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor BeamSDR UATA2026012765301Fitting · corrodedL F11 REAR UNDER FLOOR FITTING CORRODED BEYOND LIMITS, F11 & F6 UNDERFLOOR FITTING HAVE CORROSION AT NUT PLATES. F6 & F11 JUNCTION BAR FITTINGS FOUND CORRODED. JUNCTION BAR FITTINGS. REMOVED ALL JUNCTION BAR FITTINGS FROM F6 & F11. REMOVED CORROSION UNDER & AJan 27, 2026 · N424CA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA2420127265701Hinge Bracket · corrodedRT INBD. FLAP, THE OUTBD. PYLON AIRFRAME SIDE, BOTH OF THE HINGE PLATES HAVE PITTING CORROSION THAT IS BEYOND LIMITS. DRILLED BOTH HINGE PLATES AND THE INBD. AND OUTBD. PYLON SIDE SKINS OFF. FITTED AND INSTALLED NEW SIDE SKINS P/N 212-13202-05-1 (INBD.) AND P/Jan 27, 2026 · N424CA · Casa C212200 · Trailing Edge FlapsSDR UATA2025121100501Skin · crackedRIGHT HORIZONTAL STAB TOP SKIN CRACKED JUST OTBD OF AFT ATTACH FITTING HSS 740. REMOVED TOP REAR SKIN FROM STAB ROOT TO WS 1200. ELEVATOR COVE SKIN WAS DE-RIVITED TO WS 1500 FOR ACCESS. FABRICATED NEW SKIN AND PATTER AS ORIGINAL INSTALLATION. ACID ETCHED, ALNov 29, 2025 · N439RA · Casa C212200 · Horizontal Stabilizer, Plate/SkinSDR UATA2870815255301Frame · buckledLH FWD FRAME OF THE LOWER RAMP OPENING (P/N 212-23201-03-1) IS BUCKLED BETWEEN FRAME 17+18. REPLACED DAMAGED C CHANNEL 212-23201-03-1 WITH NEW. SEE 337 DATED 08/13/2025 FOR FURTHER INFORMATION. IMPACT DAMAGE FOUND IN C CHANNEL 212-23201-03-1 FWD OF F18. REMOVEAug 13, 2025 · N439RA · Casa C212200 · Fuselage Main, StructureSDR UATA2024092400001Frame · buckledFRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILABSep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, FrameSDR UATA2024092402709Attach Fitting · corrodedLH HORIZONTAL STABILIZER FORWARD ATTACH FITTING HAS CORROSION AT THE GUIDE PIN HOLE FOR THE TRIANGLE LEADING EDGE. (LOCATED INSIDE THE STABILIZER). REMOVED THE HORIZONTAL STABILIZER. DRESSED OUT THE CORROSION AND TREATED (ETCHED AND ALODYNED) PER THE CASA CORRSep 10, 2024 · N439RA · Casa C212200 · Horizontal Stabilizer StructureSDR UATA2024092405308Fitting · corrodedTHE EXTRUSION ON THE AFT SIDE OF FRAME 11 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 1 RH AFT FITTING 212-22406-06-2 WITH NEW RA-212-22406-06-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA2024092405307Fitting · corrodedTHE EXTRUSION ON THE AFT SIDE OF FRAME 6 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 RH AFT FITTING 212-22406-07-1 WITH NEW RA-212-22406-07-1 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA2024092405306Fitting · corrodedTHE EXTRUSION ON THE FWD. SIDE OF FRAME 6 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 RH FWD FITTING 212-22406-06-1 WITH NEW RA-212-22406-06-1 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA2024092405305Fitting · corrodedTHE EXTRUSION ON THE FWD. SIDE OF FRAME 6 (LEFT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 LH FWD FITTING 212-22406-06-2 WITH NEW RA-212-22406-06-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA2024092405304Fitting · corrodedTHE EXTRUSION ON THE AFT SIDE OF FRAME 6 (LEFT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 LH AFT FITTING 212-22406-07-2 WITH NEW RA-212-22406-07-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous StructureSDR UATA202409245303Frame · buckledFRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILABLSep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, FrameSDR UATA202409245302Frame · crackedONE PROFILE AT FRAME 10 IS CRACKED AT THE TOP END AND THE FRAME IS BUCKLED (UNDER FLOOR). REPLACED PROFILE, STRAIGHTENED FRAME, AND INSTALLED FRAME DOUBLER. FAA FORM 337 WAS COMPLETED.Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, FrameSDR UATA2024092405701Profile · crackedL/H OUTBOARD WING HAS ONE CRACKED PROFILE ON THE FALSE SPAR AT WING STATION 4900. REPLACED CRACKED PROFILE WITH ONE OF LOCAL MANUFACTURE.Sep 10, 2024 · N439RA · Casa C212200 · Wing Main, Frame StructureSDR 2020F00439Frame Angle · corrodedDURING ROUTINE INSPECTION, ON FRAME 6 UNDER THE FLOORBOARDS AT APPROXIMATELY BL 700(LT), THE FRAME ANGLE WAS FOUND CORRODED WITH A SUBSEQUENT CRACK IN THE SUPPORTING ANGLE UNDERNEATH IT.Nov 4, 2020 · N117BH · Casa C212200 · Fuselage Main, FrameSDR BIGA20200701003Terminal · looseDURING FLIGHT INTO ICING CONDITIONS THE WINDSHIELD HEAT WAS SELECTED ON AND THE POWER TERMINAL OF THE COPILOT’S WINDSHIELD EXHIBITED ARCING. WINDSHIELD HEAT WAS DE-SELECTED AND THE APPROPRIATE CIRCUIT BREAKERS WERE PULLED. DURING GROUND SYSTEM TROUBLESHOOTINJun 29, 2020 · N217BH · Casa C212200 · Windshield/Door Rain/Ice RemovalSDR UATA2421209495701Profile · crackedIN COMPLYING WITH AD98-12-28, FOUND ONE FALSE SPAR PROFILE TO BE CRACKED. REPLACED PROFILE WITH A NEW FABRICATED PROFILE.Dec 4, 2019 · N424CA · Casa C212200 · Wing Miscellaneous StructureSDR BIGA20190821001Line · leakingINITIAL REPORTS WERE OF AN SMOKE IN THE COCKPIT, NOTICED HYDRAULIC FLUID ON THE WINDOWS INTERNALLY AND EXTERNALLY AND HYDRAULIC FLUID FROM THE RADOME TO THE RAMP DOOR DRIPPING OFF THE BELLY. HYDRAULIC FLUID SEEMED TO BE CONCENTRATED ON THE RIGHT (CO-PILOT) Aug 18, 2019 · N107BH · Casa C212200 · Hydraulic System, MainSDR 39LA20190611184Skin · corrodedDURING SCHEDULED INSPECTIONS, A CORROSION WAS FOUND ON THE CENTER WING UPPER SKIN, R/H WS1175 TO WS3500 . ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR.Jun 11, 2019 · Casa C212200 · Wing, Plate/SkinSDR 39LA20190611183Skin · corrodedDURING SCHEDULED INSPECTIONS, A CORROSION WAS FOUND ON THE CENTER WING UPPER SKIN, L/H WS1175 TO WS3500 . ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR.Jun 11, 2019 · Casa C212200 · Wing, Plate/SkinSDR 39LA2019061105182Skin · puncturedDURING SCHEDULED INSPECTIONS, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE TAIL STAND MOUNT. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, OPENJun 5, 2019 · N602AR · Casa C212200 · Fuselage Main, Plate/SkinSDR 39LA2019060311801Floorbeam · corrodedDURING SCHEDULED INSPECTIONS, THE FLOOR BEAM AT LANDING GEAR FRAME 9 WAS FOUND TO HAVE CORROSION AT A FLOORBOARD NUTPLATE. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. OPENMay 31, 2019 · N602AR · Casa C212200 · Fuselage Main, Floor BeamSDR 39LA20181030178Channel · corrodedDURING REPAIR ACTIONS TO THE RT INBD FLAP PIVOT CONTROL POINT, THE CHANNEL ATTACHED TO THE SUPPORT BOX WAS FOUND TO BE CORRODED. REF SRM FIG 2-24 POS 3 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE TOct 30, 2018 · N602AR · Casa C212200 · Trailing Edge FlapsSDR 39LA20181030177Fitting · wornDURING INSPECTION, DANAGE WAS NOTED TO THE RT INBD FLAP PIVOT CONTROL POINT. THE LT AND RT FITTING PLATES WERE FOUND WORN BEYOND LIMITS AT THE BOLT HOLES. REF SRM FIG 2-24 POS 7 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS Oct 30, 2018 · N602AR · Casa C212200 · Trailing Edge FlapsSDR KGBR201809240001Screw · looseDURING PANEL REMOVAL FOR INSPECTION. PANEL HOLDING PRESSURE RELIEF VALVE PN:1604270 DISCOVERED ONE ADJUSTING SCREW LOOSE, SECOND ADJUSTING SCREW MISSING AND LAYING ON BOTTOM OF TANK.Sep 24, 2018 · N349TA · Casa C212200 · Fuel StorageSDR 39LA20151004145Blade · crackedDURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED.Oct 4, 2015 · N602AR · Casa C212200 · Propeller Blade SectionSDR 39LA20150902142Unknown · fumesDURING CRUISE, WHEN HEATER VLV OPENED, THE FLIGHT CREW NOTICED FUMES IN BOTH THE FLIGHT DECK & CABIN. TESTED GEARBOX FOR POSITIVE PRESS & FOUND NORMAL NEGATIVE PRESS. HEATING SYS CHECKED GOOD ON GND IAW AMM 21-40-00.Sep 2, 2015 · N602AR · Casa C212200 · Air Distribution SystemSDR 8EKA20150630001Governor · sticksPROP GOVERNOR STUCK IN FLIGHT. ACFT RETURNED TO BASE. GOVERNOR FOUND TO BE STICKY.Jun 11, 2015 · N502FS · Casa C212200 · Propeller GovernorSDR 39LA20150326110Cap · corrodedRIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300.Mar 26, 2015 · N602AR · Casa C212200 · AileronsSDR 8EKA20150309001Attach Bracket · crackedDURING PERIODIC SCHEDULED INSPECTION FOUND CRACK IN FWD ATTACHMENT BRACKET FOR THE RT HORIZONTAL STABILIZER INBD LE.Mar 6, 2015 · N437CA · Casa C212200 · Horizontal Stabilizer Miscellaneous StructureSDR 39LA20150224109Shaft · shearedDURING THE WALK AROUND INSPECTION PRIOR TO FLIGHT, MX OBSERVED THAT THE LT & RT ELEVATORS WERE DEFLECTED IN OPPOSITE DIRECTIONS. FURTHER INVESTIGATION REVEALED THAT THE LT ELEVATOR INTERCONNECT SHAFT HAD SHEARED. THERE WERE REPORTS OF HIGH WIND CONDITIONS INFeb 24, 2015 · N607AR · Casa C212200 · Elevator Control SystemSDR 39LA20150203106Light · malfunctionedAT CRUISE FLIGHT DURING NIGHT VISION GOGGLE TRAINING THERE WAS AN ORDER OF SMOKE IN THE FLIGHT DECK. THE COPILOTS SIDE OF THE OVERHEAD PANEL WAS HOT TO THE TOUCH IN THE VICINITY OF THE LIGHT SWITCHES & RHEOSTATS. FLIGHT DECK LIGHTING WAS EXTINGUISHED & THE OFeb 3, 2015 · N604AR · Casa C212200 · Flight Compartment LightingSDR 39LA2014060900005Propeller · splitIN CRUISE FLIGHT HEARD A LOUD BANG. SCANNED THE ENG INSTRUMENTS, THE LT TORQUE GAUGE WAS AT 120%, THE LT EGT HAD DROPPED BY APPROXIMATELY 100 DEGREES & THE LT FUEL FLOW HAD DROPPED TO 215 PPH FROM 300PPH. THERE WAS NO OTHER INDICATIONS OF A PROBLEM. PULLEDJun 9, 2014 · N969BW · Casa C212200 · Propeller Blade SectionSDR 3RAA20140520001Gear · failedDURING A JUMP RUN, WHILE IN CRUISE, THE LT ENGINE CHIP LIGHT FLICKERED MOMENTARILY & THEN THE ENGINE SHUT DOWN. RETURNED TO THE DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. SUSPECT CATASTROPHIC FAILURE OF THE LT ENGINE. R & R ENGINE. ACFT RETURNED TO SERVMay 19, 2014 · N467CS · Casa C212200 · Turbine Engine Reduction GearSDR 39LA2013011800003Indication Sys · malfunctionedON CLIMB OUT, RT ENGINE EGT BEGAN TO FLUCTUATE BETWEEN 200- 400 DEGREES. CLIMB POWER WAS SET PRIOR TO FLUCTUATION, EGT READING WAS ERRONEOUS. POWER REDUCED TO PRECLUDE AN INADVERTENT EGT OVER TEMP. SHORTLY AFTER, EGT FLUCTUATIONS BECAME LARGER CAUSING THE EJan 17, 2013 · N969BW · Casa C212200 · Engine Indicating SystemSDR 39LA2013011500013Sensor · dirtyON CLIMB OUT, ABOUT 8 MILES FROM DPRATURE, RT ENGINE STARTED TO SURGE BETWEEN 95 -60 PERCENT TORQUE, AND 650- 250 EGT. RETURNED TO DEPARTURE. AS ACFT LEVELED OFF AND STARTED TO DESCEND THE ENGINE RAN NORMALLY. NO OTHER ABNORMALITIES WERE NOTED AND LANDINGJan 15, 2013 · N605AR · Casa C212200 · Engine (Turbine/Turboprop)SDR P4YA2012091200001Cable · separatedDURING HEAVY CHECK, FOUND NR 1 ENGINE TELEFLEX CABLE DAMAGED/PULLED APART AT THE SWAGE HOUSING.Aug 24, 2012 · N962BW · Casa C212200 · Engine ControlsSDR EHAA20120824007Gearbox · inoperativeDURING CRUISE AT FL 85, THE NR 2 ENGINE RAPIDLY STARTED TO LOSE POWER AND DISPLAYED INDICATIONS OF FAILURE. THE COPILOT AND I NOTICED A CHANGE IN ACFT AND ENGINE PERFORMANCE, VERIFIED BY ENGINE TORQUE, RPM, FUEL FLOW, EGT AND SUBSEQUENT LOSS OF OIL PRESSURE DAug 24, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)SDR EHAA20120731006Engine · power lossDURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER.Jul 31, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)SDR KGBR2012070600001Spar · corrodedLT WING, UPPER FWD SPAR AFT HORIZONTAL LEG, EXFOLIATED AT APPROX WS 3496, ALSO PROBABLE EXFOLIATION AT WS 2130 TO 2450 AND POSSIBLE EXFOLIATION AT WS 2900 TO 3000.Jul 6, 2012 · N602AR · Casa C212200 · Wing SparSDR 3RAA2012212001Mount Bracket · brokenDURING CLIMB AFTER TAKEOFF, THE PILOTS RUDDER PEDALS MOVED ALL THE WAY FORWARD. THE COPILOT TOOK OVER AND SAFELY LANDED THE AIRCRAFT. MAINTENANCE INVESTIGATED AND DISCOVED THE PILOTS RUDDER PEDAL ADJUSTMENT MOUNT BRACKET HAD BROKEN OFF IT'S MOUNT ALLOWING THMar 29, 2012 · N467CS · Casa C212200 · Rudder Control SystemSDR STZA2011F00151Wire Harness · corrodedPRIMARY LT FUEL BOOST PUMP LOST POWER. ACFT SAFELY RETURNED TO ORIGINATING AIRPORT. FOUND THAT THE PUMP WIRE HARNESS (THE INTEGRAL WIRES FROM THE PUMP TO THE CONNECTOR) WAS CORRODED.Jun 23, 2011 · N502FS · Casa C212200 · Fuel Boost PumpSDR BIGASDR1103Plate · crackedAFTER START UP AND ATTEMPTING TO TAXI THE LT AND RT BRAKES WOULD NOT RELEASE PROPERLY AFTER HAVING THE PARKING BRAKE SET. BOTH BRAKE ASSEMBLIES (PN 5006484-3) WERE SENT OUT FOR OVERHAUL. THE BACKING PLATE (PN 5006180) FOR BRAKE ASSY SN APR84-161 WAS FOUND CRMay 2, 2011 · N117BH · Casa C212200 · Landing Gear Brake System
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