Douglas DC-8-62

Service difficulty reports · 2,778

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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 aircraft_model_key = 'DC862'
  ORDER BY difficulty_date DESC"

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SDR CKSA98614Skin · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 376L-0551, FOUND LT HORIZ STAB PANEL UPPER AND LWR SURFACE SHOWS LEVEL 2 CORROSION BETWEEN STA XE 73 AND STA XE 149. REPLACED PANEL IAW SRM 55-2-0 (SEE M-40 NUMER 38156 FOR DETAILS). FOUND DURING D CHECK, ROUTINOct 13, 1998 · N818CK · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR CKSA98613Fitting · crackedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 573R-0551, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED 2 AT STA 395.00 LONGERON 21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PEROct 13, 1998 · N818CK · Doug DC862 · Fuselage Miscellaneous StructureSDR CKSA98612Skin · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD 376L-1-0551, FOUND LT HORIZ STAB T/E PANEL UPPER AND LOWER PART SOWING LEVEL 2 CORROSION BETWEEN STA XE29 TO STA XE73. REPLACED UPPER PANEL AT LT HORIZ STAB, STA XE25 TO STA XE312 DUE TO OTHER ADJACENT AREAS AFFECTED (ROct 13, 1998 · N818CK · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR CKSA98611Fitting · crackedRT MLG W/W LONGERON 24 FITTING CRACKED 3.5 FROM STA 872 THROUGH STA 877. INSPECTED W/EDDY CURRENT METHOD, FOUND CRACK TO BE 5 .5 LONG IAW DP54751 ITEM 4-7 FIG 51, RECORDED ON M-40 38223. REPAIRED LONGERON FITTING IAW SRM 53-2-2. FOUND DURING D CHECK, ROUTINOct 13, 1998 · N818CK · Doug DC862 · Fuselage Miscellaneous StructureSDR CKSA98610Blkhd Doubler · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD 559R-0551, FOUND AFT BAGGAGE COMPARTMENT BULKHEAD DOUBLER CORRODED, FS 1218 BETWEEN LONGERON 24R AND 25R. REMOVED CORROSION IAW SRM 51-1-8, FOUND OUT OF LIMITS IAW SRM 53-2-0. INSTALLED NEW ANGLE IAW SRM 51-3-0, 51-1-Oct 13, 1998 · N818CK · Doug DC862 · Fuselage Main, BulkheadSDR CKSA98609Blkhd Doubler · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 559R-0551, FOUND AFT BAGGAGE COMPT BULKHEAD DOUBLER CORRODED LOCATION STA 1200, LONGERON 23R TO LONGERON 24R, CORROSION FOUND TO BE LOCAL. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2Oct 13, 1998 · N818CK · Doug DC862 · Fuselage Main, BulkheadSDR CKSA98608Seat Track · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 4640-0551, FOUND SEAT TRACK CORRODED AT FLT COMPARTMENT MID AREA. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-0. FOUND DURING D CHECOct 13, 1998 · N818CK · Doug DC862 · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98607Skin · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 107R-0551 FOUND RT WING L/E CORRODED AT ZONE 7R, STA XW 761. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW 57-2-0. REPAIRED AFFECTED AREA IAW SRM 57-2-1. FOUND DURING D CHECK, ROUTINE CPCP TAOct 13, 1998 · N818CK · Doug DC862 · Wing, Plate/SkinSDR CKSA98606Stop · corrodedLT AFT EMERGENCY WINDOW STOP LWR PART EXTERNAL SKIN SHOWS LEVEL 2 CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED STOP IAW SRM 51-3-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUOct 13, 1998 · N818CK · Doug DC862 · Emergency ExitsSDR IXXA9800080Tires · wornAFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW HEARD AND FELT A VIBRATION THROUGH THE COCKPIT FLOOR. THE AIRCRAFT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE NOSE TIRES OUT OF ROUND. Oct 12, 1998 · N728PL · Doug DC862 · TireSDR IXXA9800079Retract Mech · lack of lubeAFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOSE GEAR DOOR HAD FALLEN OPEN CAUSING A LOUD NOISE AND SLIGHT VIBRATION FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR, THE VIBRATION CONDITION WAS STILL PRESENT. THE AIROct 12, 1998 · N728PL · Doug DC862 · Landing Gear Door Retract SectionSDR RRXA99193Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 759 BETWEEN BL 54 LEFT TO BL 64, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 Oct 6, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981003Radio Alt · inoperativeCREW REMOVED AND REPLACED NR 2 RADIO ALT OFF FLAG IN/VIEW. REMOVED AND REPLACED NR 2 RADIO ALT, OPS NORMAL IAW 34-16-00.Oct 2, 1998 · N791AL · Doug DC862 · Ground Proximity SystemSDR ARWA981002Detector Unit · inoperativeRETURNED TO BLOCK, ACCESSED CURRENT DETECTOR UNIT LIGHT ILLUMINATED. REMOVED AND REPLACED CURRENT DETECTOR UNIT, OPS CHECKED NORMAL IAW MM 30-30-00.Sep 30, 1998 · N8968U · Doug DC862 · Pitot/Static Anti-Ice SystemSDR ARWA981001Pitot Heat · inoperativePITOT HEATER INOP, LIGHT ON ZERO INDICATING ON OAI 1 AND OA. RESET CIRCUIT BREAKER ON PITOT HEAT SYSTEM, HEATER INOP. LT OPS CHECKED NORMAL PER MM 30-32, OAT 1 AND OAT 2 IS FUNCTION OF OLEO SWITCH, OPERATION NORMAL.Sep 30, 1998 · N8968U · Doug DC862 · Pitot/Static Anti-Ice SystemSDR RRXA99227Shear Tie · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 902 AND LONGERON 24 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC-8 SRM 51-1-20D. (CORROSIONSep 22, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA99226Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSISep 22, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA980911Fitting · looseTUS - SHUTDOWN NR 4 ENGINE S/N 671443 AT 1345Z DUE TO STEADY OIL PRESS LIGHT AND INDICATED PRESS LESS THAN 35 PSI. WINDMILLING PRESS AT 18 PSI. TIGHTENED LOOS SWIVEL FITTING AT NR 6 BEARING INLET. ENGINE RUN UP. NO LEAKS NOTED. (M)Sep 22, 1998 · N802BN · Doug DC862 · Turbine Engine Oil SystemSDR ARWA980910Spar · crackedRT WING FRONT SPAR LOWER CAP HAS TWO ADJACENT ATTACHMENT HOLES CRACKED BETWEEN STA XFS 515.000 AND XFS 526.760. CUT OUT DAMAGED AREA PER DRA J060232, FABRICATED FILLER, ANGLES AND DOUBLER PER DRG J060232 AND ROD SKETCH 97-02-10-005. LOCATED, DRILLED AND STRSep 19, 1998 · N802BN · Doug DC862 · Wing SparSDR ARWA980909Fan Blades · bentON PREFLIGHT FOUND BENT FAN BLADES NR 4 ENGINE. BLENDED 5 BLADES PER JT3D M/M (P/W) 72-00-00 BORESCOPE C/W, NO DEFECTS NOTED AT THIS TIME IAW M/M 72-00-00.Sep 17, 1998 · N1808E · Doug DC862 · Turbine Engine Compressor SectionSDR RRXA99217Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 1606 AND LONGERON 32 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-2-0 FIGUSep 15, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA980907Actuator · inoperativeCONTROL WHEEL SWITCHES ON CAPT AND FO FOR LONGITUDINAL TRIM INOP. ON PREFLIGHT SWAPPED TRIM ACTUATOR, REINSTALLED LOANER TRIM ACTUATOR, SYS OPS CHECK NORMAL IAW MM 27-43-0.Sep 15, 1998 · N791AL · Doug DC862 · Stabilizer ActuatorSDR ARWA980906Actuator · dirtyNO SPOILER DEPLOYMENT WITH REAR WHEELS SPIN UP. SPOILER HANDLE STIFF TO ACTUATE. FOUND BELL CRANK AND SPOILER HYD. ACTUATOR HAD EXCESSIVE BUILD-UP OF ANTI-CORROSION PAINT. REMOVED BUILD UP AND LUBE CRANK. SPOILER SYSTEM, OPS CHECKED GOOD IAW DC-8 M/M 27-6Sep 11, 1998 · N791AL · Doug DC862 · Drag Control ActuatorSDR ARWA980905Compressor · stalledBLOCK TURNBACK AFTER SPOOLED AND STABLE NR 1 OR NR 2 ENG COMPRESSOR STALL. FOUND PAPER IN INLET OF NR 2 ENGINE. REMOVED FOD (PAPER) FROM INLET, STARTED AND SPOOLED UP NR 2 ENGINE IAW DC-8 MM 80-00-0, NO DEFECTS NOTED AT THIS TIME.Sep 10, 1998 · N791AL · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98056Switch · failedON CLIMBOUT, NR 2 ENGINE LOW OIL PRESSURE LIGHT ON. CHECK LIST COMPLETED AND LIGHT STILL ON. SHUT DOWN NR 2 ENGINE PRECAUTIONARY. CREW DEBRIEF REVEALED NO OIL PRESSURE LOSS AND NO OIL QTY LOSS. DISCOVERED OIL DIFFERENTIAL PRESSURE SWITCH LEAKING. REMOVED Sep 4, 1998 · N181SK · Doug DC862 · Engine Oil PressureSDR ARWA980901Control Cable · brokenWHEEL LONGITUDINAL TRIM WILL NOT TRIM NOSE UP, SUITCASE HANDLE ARE SPLIT LEFT HANDLE FULL AFT. RIGHT HANDLE IN NEUTRAL POSITION. FOUND LONGITUDINAL TRIM CABLE 113A BROKEN. REMOVED AND REPLACED CABLE IAW DC-8 91-10-0 AND 91-10-2. INSTALLED CABLE PER MM 27-4Sep 1, 1998 · N791AL · Doug DC862 · Stabilizer Control SystemSDR IXXA9800068Switch · defectiveEN ROUTE FROM BWI TO WRI, WHEN THE LANDING GEAR WAS RETRACTED, THE LANDING GEAR UNSAFE LIGHT REMAINED ON. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO WRI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THEAug 28, 1998 · N728PL · Doug DC862 · Landing Gear Position and WarningSDR ABXA9800795Door Handle · out of adjustDURING PREFLIGHT, FOUND THAT THE COCKPIT DOOR WOULD NOT OPEN FROM CABIN SIDE. REPAIRED COCKPIT DOOR HANDLE AS REQUIRED, OPS CHECKED GOOD.Aug 26, 1998 · N803AX · Doug DC862 · Fixed Inner DoorsSDR RRXA99223Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 920 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSIAug 25, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9800779Angle · crackedRIGHT WING LEADING EDGE INTERIOR, VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM OUTBOARD END OF INBOARD SLOT BOX STATION XS 250.089. REPLACED ANGLE IAW DWG 9753293 AND DC8 SRM 51-1-20 AND 51-1-21.Aug 21, 1998 · N803AX · Doug DC862 · Wing Miscellaneous StructureSDR RRXA99209Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 32 LEFT AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAAug 17, 1998 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9800744Battery Pack · dischargedDURING PRE-DEPARTURE CHECK, FOUND THAT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY PACK IAW DC8 MM 33-50-01. OPS CHECKED GOOD.Aug 13, 1998 · N804AX · Doug DC862 · Emergency LightingSDR ARWA980810Antenna · failedMIA - FLT 617 - NR 1 AND NR 2 RADAR INOP. REMOVED AND REPLACED ANTENNA AND REPLACED BOTH R/T'S REPLACED BOTHS INDICATORS AND CONTROL HEADS, ACCOMPLISHED OPERATIONAL CHECK IAW MM 34-41-0, OPS CHECK NORMAL DURING 2 HOURS GROUND CHECK. NR 2 RADAR IND CONTROL P/Aug 12, 1998 · N1808E · Doug DC862 · Weather Radar SystemSDR ARWA980809Filter · contaminatedMIA - FLT 617 - HYD OIL TEMP REACHED 80 PERCENT. REMOVED AND REPLACED LEFT WHEEL WELL FILTERS IAW MM 29-10-00. OPS AND LEAK CHECK NORMAL. NO LEAKS NOTED. (M)Aug 12, 1998 · N1808E · Doug DC862 · Hydraulic Filter, AuxiliarySDR ABXA9800790Fitting · crackedLONGERON END FITTING AT FRAME STATION 1520, LONGERON 28 LEFT AT MANUFACTURE SPLICE WAS CRACKED AND CORRODED. REPLACED FITTING IAW DC8 SRM 51-3-0 AND SRM 51-1-20.Aug 12, 1998 · N803AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9800789Angle · crackedRIGHT WING LEADING EDGE AT STATION 778.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K 05056-7003.Aug 12, 1998 · N803AX · Doug DC862 · Wing Miscellaneous StructureSDR ABXA9800788Fitting · corrosionRIGHT UPPER CUSP MEMBRANE FITTING HAS HEAVY CORROSION FS 340 TO 350. REPAIRED IAW DC8 SRM 51-1-20D.Aug 12, 1998 · N803AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9800787Doubler · crackedLONGERON 24R AT STATION 879 HAS A 3.6 INCH LONG CRACK RUNNING FORWARD AND AFT OF FITTING LOCATION. REPAIRED IAW DC8 SRM 53-2-2 AND 51-1-20D.Aug 12, 1998 · N803AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9800786Frame · corrodedFRAME STATION 798 RIGHT BELOW CUSP AREA CORRODED OUT ON FORWARD AND AFT SIDE OF FITTING. REPAIRED IAW DWG 5641008 AND ABX REA D853-22904 MR.Aug 12, 1998 · N803AX · Doug DC862 · Fuselage Main, FrameSDR ABXA9800793Floorbeam · corrodedFLOORBEAM 1540 CORRODED FROM LBL 24 TO RBL 38 LOWER FLANGE. REPAIRED FLOORBEAM IAW ABX REA D853-22918 MR.Aug 11, 1998 · N803AX · Doug DC862 · Fuselage Main, Floor BeamSDR ABXA9800792Vane · corrosionRIGHT INBOARD SLOT VANE OUTBOARD END HAS HEAVY CORROSION UNDER THE SURFACE IN 2 PLACES. REPAIRED SLOT VANE IAW DC8 SRM 57-2-1.Aug 11, 1998 · N803AX · Doug DC862 · Trailing Edge FlapsSDR ABXA9800791Intercostal · crackedCORRODED AND CRACKED INTERCOSTAL AT FUSELAGE STATION 1500 LONGERON 29R AFT ACCESSORY COMPARTMENT. REPAIRED IAW DC8 SRM 53-4-1, 51-1-8 AND 51-1-21.Aug 11, 1998 · N803AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9800772Rib · crackedRIGHT WING LEADING EDGE AT STATION 316.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DRAWING K 05056 AND DC8 SRM 51-1-20D.Aug 11, 1998 · N803AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9800771Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 360.250 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.Aug 11, 1998 · N803AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9800770Skin · corrodedRIGHT WING LEADING EDGE AT STATION XFS 304.0 UPPER LEADING EDGE SKIN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW DC8 SRM 57-2-1.Aug 11, 1998 · N803AX · Doug DC862 · Wing, Plate/SkinSDR RRXA99221Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGEAug 10, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA980808Controller · failedMIA - FLT 617 - NR 1 AND NR 2 RADAR INOP R/I. A/C RETURNED TO MIAMI, REMOVED AND REPLACED PITCH COMPUTER, OPS CHECKED NORMAL IAW MM 22-13-0. NR 2 RADAR R/T, P/N 2067151-0153 S/N 2915. (M)Aug 10, 1998 · N1808E · Doug DC862 · Flight ControllerSDR RRXA99215Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGEAug 9, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA99212Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 31 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGEAug 9, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA99210Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34 LEFT AND FITTING AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (Aug 9, 1998 · N995CF · Doug DC862 · Fuselage Main, Longeron/Stringer
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