Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR IXXA06SMN097SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 430.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DMar 9, 2006 · N602AL · Doug DC873F · Standard Practices/StructuresSDR IXXA06SMN085SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RIGHT WING - CTR L/E LWR EXTERNAL PART NON STANDARD REPAIR XFS 335.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4189 DATE 03-07-06, EO SEMAN 2006154 DATE 03-15-06. REMOVED NON STANDARD Mar 9, 2006 · N602AL · Doug DC873F · Standard Practices/StructuresSDR IXXA06SMN084SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT ELEVATOR UPPER SKIN 1 INCH CRACK AT STA XE 71.169. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1 (SHEET 1, 2). REMOVED DAMAGED PLATING IAW DC8 SRM 55-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NEW PLATING (AL 2024 T3 0.Mar 9, 2006 · N602AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN079SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT HORZ STAB L/E UPPER SURFACE HAS NON - STANDARD REPAIR, STA XFS 47.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4188 DATE 03-08-06, EO SEMAN 2006149 DATE 03-15-06. REMOVED NON STANDARMar 9, 2006 · N602AL · Doug DC873F · Standard Practices/StructuresSDR IXXA06SMN078SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING INBOARD FLAP L/E LWR FWD PART DENTED, XW 40.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPMar 9, 2006 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN076SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING NR 1 STUB WING CRACKED 2.5 INCH, XILD 42 LWR SKIN. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1A FIG 1. REMOVED EXISTING DOUBLERS IAW DC8 SRM 51-1-20D, DC-8 SRM 51-1-21. PERFORMED STOP HOLE ON CRACK END. FABRICATED EMar 9, 2006 · N602AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN070SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LEFT CUSP EXTRUSION UPPER SURFACE FRAME NON STANDARD REPAIR, STA 1560.000 L-20L. PERFORMED MAJOR REPAIR. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED AREA, FABRICATED NEW FRAME SEGMENT P/N 52645791. FABRICATED (02 EA) ANGMar 9, 2006 · N602AL · Doug DC873F · Standard Practices/StructuresSDR UPS06846528Longeron · corrodedL30L AT STA 285 IS CRACKED AND WITH EXFOLIATION CORROSION. REMOVED FITTING, AND LONGERON FROM ST 280-310. FABRICATED REPAIR SECTION OF LONGERON AND INSTALLED FITTING, REPAIR SECTION AND 2 SPLICES IAW SRM 53-02-02 FIG 10 AND 51-01-20D.Mar 4, 2006 · N867UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846527Fitting · crackedR/WING TE STA XW5 FITTING FOR SPOILER ATTACHMENT CRACKED. FABRICATED REPLACEMENT FITTING IAW SAA EA NR 008-5730-01-A0107 AND UPS RA DC8-57-20157.Mar 2, 2006 · N867UP · Doug DC873F · AileronsSDR UPS06846328Smoke Barrier · unsecureSMOKE CURTAIN DIFFICULT TO SECURE ON GROUND. EN ROUTE SMOKE/FIRE CURTAIN DOES NOT REMAIN SECURE AT 6.0 (FL35) D320807 ASSIGNED. *S/D* REPLACED VELCRO PER EO DC8-2550-1873 FINAL REPAIR APP 8.2 COMP.Feb 28, 2006 · N810UP · Doug DC873F · Emergency EquipmentSDR UPS06846307Battery Pack · inoperativeEMERGENCY LIGHTS FAILED TO OPERATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.Feb 28, 2006 · N811UP · Doug DC873F · Emergency LightingSDR UPS06846465Fitting · corrodedC3 IN C-PIT L31L BETWEEN STA 1040-1060 HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW SRM 51-1-20D.Feb 26, 2006 · N867UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846432Shear Tie · crackedFOUND CRACK IN RADIUS OF FRAME TO FUSELAGE BRACKET L36 STA 1280. REMOVED SHEAR TIE AT STA 1280 L36L IAW SRM 53-02-00-0 FIG 2A. FABRICATED AND INSTALLED SHEAR TIE AT STA 1280 L36 IAW SRM 53-02-00 FIG 2A, 53-04-01-0, 51-01-20D.Feb 26, 2006 · N867UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS06846431Longeron · crackedFOUND LONGERON 34R CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED LONGERON 34R AT STA 1260-1288 IAW SRM 51-3-2, 51-1-20D, AND 51-1-21Feb 26, 2006 · N867UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846414Web · crackedINSPECTION TYPE:C3 LT FWD MAIN ENTRY DOOR JAMB STRUCTURE HAS A CRACK AT AFT LWR CORNER STA 70. CUT OUT DAMAGE ON L1 DOOR LWR DOOR JAMB CORNER AT STA 70 IAW SRM 53-2-0, FABRICATED AND INSTALLED WEB AT STA 70 L1 DOOR LWR AFT CORNER IAW DWG 5597646, AND SRM 51-0Feb 26, 2006 · N867UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846326Rib · crackedRT WING CENTER L/E INTERIOR AT APPROX STA XW 280 HAS 1 SUPPORT RIB CRACKED AT END. STOP DRILLED 2 CRACKS, FABRICATED AND INSTALLED 2 ANGLES AND 1 FILLER IAW SRM 57-02-00 FIG 02, 57-03-02 FIG 03, 53-03-02 FIG 05 AND 51-01-20D.Feb 26, 2006 · N867UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06846488Spar Cap · crackedINSPECTION TYPE:C3 LH LWR REAR SPAR HAS A 9" CRACK AT STA 857 LBL 53 TO LBL 60, STOPPED DRILLED CRACK AT STA 857 LBL53 IAW SRO 8570009 NOTE 19 FABRICATED AND INSTALLED -63 ANGLE,-7,-9,-11,-15,-17,-21,-23 -25,-27,-29,-33 STRAP ANGLES,-35,-37,-39,-41 SHIMS, AND Feb 25, 2006 · N867UP · Doug DC873F · Wing SparSDR UPS06846430Rib · crackedINSPECTION TYPE:C3 REF EO DC8-5510-1074-N APPD B PAGE 8, STIFFENING PLANK RIB IS CRACKED BETWEEN BOLTS NR 36 AND NR 37. REMOVED STIFFENING PLANK RIB BETWEEN BOLTS 36 AND 37 IAW SRM 51-01-20D-0, LOCATED, DRILLED UP, AND INSTALLED REPLACEMENT PLANK IAW SRM 51-1Feb 25, 2006 · N867UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS06846413Web · crackedINSPECTION TYPE:C3 ELONGATED FASTENER HOLE AT AFT LWR CORNER OF R1 DOOR FS 190 JUST ABOVE L21R. REMOVED DAMAGED WEB AT STA 190 L21R IAW SRM 51-01-21, FABRICATED AND INSTALLED WEB AT STA 190 L21R IAW DWG 5615700 ITEM 17 AND SRM 51-01-08, SRM 51-1-8 AND SRM 51-Feb 25, 2006 · N867UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846464Doubler · corrodedINSPECTION TYPE:C3 WASTE WATER SERVICE ACCESS DOOR LAND HAS CORROSION AT UPPER 2 LATCHES, ATTACH AREA APPROX 1" BY 1" STA 80 AND L25R. REPAIRED WASTE WATER SERVICE DOOR INTERNAL DOUBLER IAW SAA EA# 008-5320-01-A0095 AND UPS RO DC8-53-20535.Feb 24, 2006 · N867UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846412Web · crackedINSPECTION TYPE:C3 CRACK ON FLOOR WEB APPROX STA LOCATION IS BETWEEN 35 AND 55 RIGHT SIDE LENGTH IS APPROX .75 INCH. STOP DRILLED CRACK ON FLOOR WEB AT STA 35 TO 55 RIGHT SIDE, FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 35-55 RIGHT SIDE IAW SRM 53-02-00, Feb 24, 2006 · N867UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846270Battery Pack · dischargedINSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY EXIT LIGHTS OVER ENTRY DOOR & IN COMPANION WAY OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS OK.Feb 23, 2006 · N805UP · Doug DC873F · Emergency LightingSDR UPS06846246Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY DEAD. FOUND DURING PRE-DEPARTURE CHECK. REPLACED PER MM 33-50-01-2, CHECKS OK.Feb 22, 2006 · N874UP · Doug DC873F · Emergency LightingSDR DHL2006807002Sensor · malfunctionedON TAXI OUT NR 1 N1 APPROACHED 35% THEN N1 ROLLED BACK 13% N2 ROLLED BACK 40% EGT CLIMBED TO 700/C. SHUT ENG DOWN. ATTEMPTED RESTART ENG NR 1 N2 20% N1 ROSE 8% & STALLED EGT. T/S REMOVED & REPLACED CIT SENSOR, NO HELP. REMOVED AND REPLACED MEC, LEAK CHECK Feb 22, 2006 · N807DH · Doug DC873F · Fuel Controlling SystemSDR DHL2006807001Battery · malfunctionedREMOVED EMER EXIT LIGHT BATTERY DUE TO EXTREME COLD PLACED IN WARM ENVIRONMENT REINSTALL BEFORE FLT. RE-INSTALLED EMER EXIT LIGHT BATTERY ASSY REF MM 33-50-1 OPS CHECKED NORMAL.Feb 20, 2006 · N807DH · Doug DC873F · Emergency LightingSDR DHL2006804547Door Frame · damagedEXT FUSELAGE "D" BELLY DOOR JAMB LWR FWD CORNER HAS NOT BEEN REPAIRED PREVIOUSLY IAW SERV REWORK DWG SR08530019. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 02-20-06, AD2005-18-07, SB DC8 53-078, SVC REWORK DWG SR08530019, BOEING MSG NR 1-152801694 (ED-4Feb 17, 2006 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2006804552Fitting · crackedAFT CARGO COMPT FITTING CRACKED 2 INCHES AT STA 1200.000 L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED FFeb 16, 2006 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006804549Doubler · crackedRT WING NR3 MAIN TANK 505F ACCESS DOOR INTERNAL DOUBLER FLANGE CRACKED 0.750 XRS 12.000 S-5 (MAJOR REPAIR). REMOVED FASTENERS. CUT OUT DAMAGED SECTION IAW DWG AA66-57-R09. PERFORMED NDT INSP USING DYE PENETRANT IAW NDT SPM. APPLIED YELLOW COATING TO TANK INTEFeb 16, 2006 · N804DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2006804548Doubler · crackedRT WING NR3 MAIN TANK 506C ACCESS DOOR INTERNAL DOUBLER FLANGE CRACKED 0.250 INCH STA 12.000 S-13 S-14 (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG AA66-57-R08. PERFORMED NDT INSP USING DYE PENETRANT METHOD IAW NDT SPM PAFeb 16, 2006 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2006804551Repair · misinstalledINSPECT PREVIOUS REPAIRS AT STR 36 STA 310 AND 280 TO ENSURE IT COMPLIES WITH SRM. DOCUMENT ON THIS NON ROUTINE (REFERENCE ATTACHED AIR CANADA N/R 907). IF REPAIR IS NOT IN CONFORMANCE WITH THE SRM OR IN POOR CONDITION, REWORK PER SRM OR APPROVED DATA.CORR.: VFeb 16, 2006 · N804DH · Doug DC873F · Aircraft StructuresSDR DHL2006804550Door Frame · cracked"D" CARGO DOOR JAMB LWR AFT CORNER CRACKED 0.650" STA 1440.000 L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 01-13-06, AD2005-18-07 SB DC8 53-078, SVC REWORK DWG SR 08530019, BOEING MSG 1-15655483-2 (ED-4152), MSG 1-151655483-3 DATED 01-13-06. REMOFeb 16, 2006 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2006804545Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 120.000 L-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-15-06 DWG AA66-53-R07 REV IR DATED 01-16-06. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR ANGLE (EXTRUSION 7075T6 511 0.090") FILFeb 16, 2006 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006804546Repair · brokenFUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER WITH 02 BREAKS STA -156.000 TO STA -165.000 (PNEU. GROUND START) MAJOR REPAIR. REMOVED INTERNAL REINFORCEMENT REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-3-0. CUT OUT INTERNAL DOUBLER AND FABRICATED EXT REPAIR DOUBLER (AL Feb 16, 2006 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2006804544Fitting · crackedNR 1 ALT TANK 505B ACCESS DOOR FITTING CRACKED 1" XRS 428.000 - XRS 463.000 S-38. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTINGFeb 15, 2006 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS06846191Battery Pack · inoperativeEMERGENCY LIGHTS DO NOT TEST. REPLACED EMERG LIGHT BATTERY PACK. OPS CK GOOD.Feb 15, 2006 · N818UP · Doug DC873F · Emergency LightingSDR UPS06846305Splice · crackedINSPECTION TYPE:C2 LONGERON SPLICE FITTING IS CRACKED AT STA 1260-1280 L35R. REMOVED AND REPLACED SPLICE FITTING AT STA 1260-1280 L35R IAW SRM 51-03-02-0, AND SRM 51-1-20D.Feb 14, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846304Stringer · crackedINSPECTION TYPE:C2 STR END FITTING CRACKED ON STR 51 NR 3 MAIN TANK BETWEEN XRS 23-XRS 50. REMOVED AND REPLACED END FITTING AT STR 51 NR 3 MAIN TANK STA XRS 23 - XRS 50 IAW SRM 51-3-2 AND SRM 51-01-20D.Feb 14, 2006 · N814UP · Doug DC873F · Wing, Longeron/StringerSDR UPS06846171Light · malfunctionedEMERG EXIT LIGHT ON IN FLT WILL NOT EXTINGUISH IN ARMED POS. THIS DISCREPANCY COULD NOT BE DUPLICATED ON THE GROUND. PERFORMED EMERG LIGHTING CK PER MM 33-50-02-2 WITH ALL NORMAL RESULTS.Feb 14, 2006 · N802UP · Doug DC873F · Emergency LightingSDR UPS06846408Fitting · crackedINSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1150 L35R. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846300Fitting · crackedINSPECTION TYPE:C2 END FITTING CRACKED IN 60 HOLE L10L AT STA 1770. REMOVED END FITTING AT STA 1770 L10L IAW SRM 51-1-21, LOCATED AND DRILLED REPLACEMENT FITTING AND INSTALLED AT STA 1770 L10L IAW SRM 51-3-2, AND SRM 51-1-21.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846299Longeron · crackedINSPECTION TYPE:C2 L35L CRACKED AT STA 1260-1280. REMOVED AND REPLACED LONGERON 35L AT STA 1270 TO 1350 IAW SRM 51-1-21, 51-1-20D.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846297Fitting · crackedINSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1140 BETWEEN L34R AND L33R. REMOVED END FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED END FITTING AT STA 1140 BETWEEN L34R AND L33R IAW DWG 4758514 AND SRM 53-1-0 AND SRM 51-1-20D.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846244Longeron · crackedINSPECTION TYPE:C2 FOUND LONG 35R STA 1287-1295 IS CRACKED. REMOVED AND REPLACED LONGERON AT STA 1270-1350 L35R IAW SRM 51-01-20D-0 AND SRM 51-1-21.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846242Floor Support · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON ATTACH CLIP BETWEEN FLOORBEAM AND FLOOR PNL AFT ACC COMPT CEILING STA 1680 LBL 13. REMOVED CORRODED FLOOR SUPPORT CHANNEL IAW SRM 53-2-0 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL IAW SRM 53-07-01 SRM 51-02-00Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846240Longeron · crackedINSPECTION TYPE:C2 LONG 34R STA 1287-1295 IS CRACKED. REMOVED LONG 34R FROM STA 1270 TO 1350 IAW SRM 51-1-21. INSTALLED REPLACEMENT LONGERON AT STA 1270-1350 IAW SRM 51-01-20-D-0.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846209Longeron · crackedINSPECTION TYPE:C3 L16L CRACKED BEHIND CANTED FRAME, MAIN CABIN STA 1746 REMOVED END FITTING AND SHEARTIE AT STA 1746 L16L IAW SRM 51-03-00-0. FABRICATED AND INSTALLED LONGERON SPLICE FITTING AND SHEARTIE IAW SRM 53-02-02-0, 53-05-01-0 AND SRM 51-01-20D-0Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06846176Fitting · crackedINSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1140 L35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 13, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846175Doubler · corrodedINSPECTION TYPE:C2, CORROSION ON C-PIT LOWER SKIN DOUBLER STA 1181-1184 BETWEEN L32R-33R. REMOVE, FABRICATE AND REPLACE DOUBLER IAW SRM DWG 3754065, SRM 51-1-20D.Feb 12, 2006 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06846301Fitting · crackedINSPECTION TYPE:C2 LONGERON END FITTING AT L30L STA 1690 IS CRACKED. REMOVED AND REPLACED END FITTING AT STA 1690 L30L IAW SRM 51-01-21, AND SRM 51-1-20D.Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846296Fitting · corrodedINSPECTION TYPE:C2 LONGERON END FITTING AT STA 1690 L24L HAS CORROSION INSIDE OF FITTING. REMOVED END FITTING AT STA 1690 L24L CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-02-00-0, LOCATED AND DRILLED REPLACEMENT END FITTING AND INSTALLED IAW SRM 51-1-21, 5Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous Structure
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