Douglas DC-8-71F

Service difficulty reports · 8,938

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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 aircraft_model_key = 'DC871F'
  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 RRXA991649Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 772.5, CRACKED AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991648Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN, INTERNAL DOUBLER AT STA XFS 572.5, CRACKED AT THE DRAIN HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW MFG DWG Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991639Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, RT MLG DOOR ON INNER SKIN AT O/B CORNER OF AFT END CENTER WING TO WING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 52-Aug 15, 1999 · N8087U · Doug DC871F · Landing Gear DoorsSDR RRXA991638Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, UPPER T/E SKIN, UPPER SEVERAL FASTENER HOLES BETWEEN 1 AND 4 AFT OF REAR SPAR AT XR 5162.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED AND REPAIREAug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991468Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK AT LONGERON 31 RIGHT, STATION 1755, EXTERIOR FUSELAGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-1. (CORROSIAug 15, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA991464Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING CENTER, L/E UPPER SKIN AT STA XFS 316.5 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991461Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN AT STA XFS 630. 3 FORWARD OF THE SPAR, AT A RIVET HEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIRAug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991460Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB AT FASTENER END, BETWEEN STA XFS 622.5 AND XFS 628.75 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND RAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991459Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER RIB AT STA XFS 521.168, 6 FWD OF THE SPAR. THE CRACK APPROXIMATELY 25 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB AND REPAIRAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991456Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT OBD L/E UPPER RIB AT FASTENER END AT STA XFS 585. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991454Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT WING LOWER L/E RIB AT FASTENER END AT STA XFS 653.75, FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991453Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 616.25 AT THE LWR FASTENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 5Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991452Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN, INTERNAL DOUBLER AT STA XFS 597.5 AT THE DRAIN HOLE, CRACK RUNS AFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991451Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 735.0 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991450Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 772.5 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991449Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN, INTERNAL DOUBLER, AT STA XFS 572.5 AT THE DRAIN HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG NR 6769Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991443Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT MAIN LANDING GEAR DOOR ON INNER SKIN AT O/B CORNER OF AFT END, CENTER WING TO WING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLAug 15, 1999 · N8087U · Doug DC871F · Landing Gear DoorsSDR RRXA991442Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING, UPPER T/E SKIN, SEVERAL FASTENER HOLES BETWEEN 1 AND 4 AFT OF REAR SPAR AT STA XR5162.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, FABRICATED ANAug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991430Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION AND CRACK, FUSELAGE, AT FSY 1755, LONGERON 31 RIGHT EXTERNAL FUSELAGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-1. (Aug 15, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS99830350Floorbeam · crackedINSPECTION TYPE:C123, CORROSION FLOORBEAM FS 1600 RT. REPAIRED IAW REO-06679, INSTALLED IAW DC8 SRM 51-1-20D.Aug 13, 1999 · N752UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS99830334Floorbeam · crackedINSPECTION TYPE:N/A, FOUND FLOORBEAM CRACKS AT STA 1600 AND 1620. *S/D* REPAIR COMPLETED ON FLOORBEAM.Aug 13, 1999 · N752UP · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA991441Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK AT LONGERON 31 RIGHT, STA 1755. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-1. (CORROSION DAMAGE RECORAug 13, 1999 · N8087U · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA9900020Plating · crackedDURING A SCHEDULED HEAVY MAINTENANCE VISIT, A CRACK WAS DETECTED ON THE RIGHT WING LOWER EXTERNAL PLATING AT WING STATION XRS323, BETWEEN STRINGER 62 AND 63. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL REPAIR FILLAug 13, 1999 · N821BX · Doug DC871F · Wing, Plate/SkinSDR RRXA991429Skin · damagedDURING A MAINTENANCE VISIT, FOUND EXTERIOR RT LIGHTNING STRIKE AT STA 250 RT BETWEEN LONGERONS 21 RIGHT AND LONGERON 22 RIGHT (EO).Aug 10, 1999 · N8079U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS99830311Light · inopEMERGENCY LIGHT DISARM CHECK DOES NOT CHECK. RELAMPED EMERGENCY LIGHT SWITCH IND LIGHT CKS GOOD PER MM 33-50-00.Aug 9, 1999 · N718UP · Doug DC871F · Emergency LightingSDR UPS99830257Battery Pack · dischargedINSPECTION TYPE:W/,E EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. EMERGENCY LTS GROUND OPERATIONAL TEST NORMAL PER MM 33-50-01.Aug 1, 1999 · N718UP · Doug DC871F · Emergency LightingSDR UPS99830254Seal · looseON DEPART, (C/O) NOTICED AFTER GEAR RETRACT, THE GEAR NOT LATCH LIGHT FLICKERED. DID UPLATCH CK AND LIGHT EVENTUALLY CAME ON STEADY. WENT TO GEAR NOT LATCH LIGHT ILLUMINATED. CKLIST AND C/W, THIS INCLUDED CYCLING GEAR AND LOOKING THROUGH PEEPHOLE TO CHECK IJul 31, 1999 · N750UP · Doug DC871F · Landing Gear DoorsSDR UPS99830199Battery Pack · dischargedEMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01 CHKS GOOD.Jul 28, 1999 · N748UP · Doug DC871F · Emergency LightingSDR UPS99830174Overtemp Light · illuminatedMAIN AIR OVERTEMP LIGHT ILLUM WITH MANIFOLD AIR TEMP IN NORMAL RANGE NO WARNING LIGHT. MONITORED LIGHT SUSPECT PRESS TO TEST. SWITCH LIGHT STILL ILLUM AFTER SHUTDOWN. RELAMPED MAN OVERTEMP LIGHT. RAN ALL ENG. NO OVERTEMP NOTED OPS CK OK.Jul 27, 1999 · N744UP · Doug DC871F · Overheat DetectionSDR UPS99830153Skin · crackedMAINTENANCE FOUND LEFT WING LOWER SURFACE, APPROX 16 INCHES INBOARD OF NR 1 PYLON, CRACKED SKIN APPROX 4 INCHES LONG. ROUTED OUT CRACKED AREA IAW REO-06635. FABRICATED FILLER, INTERNAL DOUBLERS AND TRIPLERS, EXTERNAL DOUBLER AND TRIPLER IAW REO-O6635. ALODIJul 23, 1999 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS99830158Skin · crackedINSPECTION TYPE:N/A ON POST FLIGHT, ENGINEER AND MECHANIC VERIFIED A SMALL CRACK ON NR 2 PYLON. ACCOMPLISHED EO DC8-5430-11626-A APPENDIX B INTERIM REPAIR NR 2 PYLON OUTBOARD RAMP AT THE ENGINE FAN EXHAUST OUTLET. TRANSFERRED TO DMI LIST C/N D-175661 ASSIGNEJul 21, 1999 · N752UP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR IXXA9900015Pack · malfunctionedEN ROUTE FROM TOL TO DFW, THE RIGHT AIR CONDITIONING PACK HAD ZERO FLOW, RUNS HOT AND EMITTED A BURNING ODOR WHEN FULL COLD SELECTED. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE RIGHT PACK SYSTEM IN ACCORDANCE WITH THE MAJul 10, 1999 · N822BX · Doug DC871F · Cabin Cooling SystemSDR UPS99830064Wire · shortedEMERGENCY EXIT LIGHTS INOP. T/S AND FOUND WIRE LG19DW22 SHORTED TO GROUND AT COCKPIT DOME LIGHT ASSY. REPAIRED WIRE LIGHT, OP CHECKS GOOD.Jul 7, 1999 · N701UP · Doug DC871F · Light System WiringSDR UPS99830022Frame · corrodedINSPECTION TYPE:C2 FS 60 FRAME AT LBL 40 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 1B.Jul 3, 1999 · N750UP · Doug DC871F · Fuselage Main, FrameSDR RRXA991365Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, INTERCOSTAL TOP CUP BETWEEN LEFT WING NR 2 AND NR 3 SPOILERS AT STA XW 129. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW Jul 3, 1999 · N8091U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991168Fuel Filter · contaminatedON CLIMB-OUT LEAVING BNA OUT OF 9.0 NR 1 ENG FLAMED OUT MADE PRECAUTIONARY SHUT DOWN WAITED 2 MINS PERFORMED RELIGHT PROCEDURE ENG RELIT AND PERFORMED OK IN TO DAY. INSPECTED NR 1 ENG IAW DC-8 MM. NO DEFECTS FOUND, TAXIED ACFT TO RUN UP PAD RAN AT ALL PWR SEJul 1, 1999 · N8079U · Doug DC871F · Engine Fuel DistributionSDR IXXA9900012Acm · defectiveEN ROUTE FROM PDX TO TOL, THE FLIGHT CREW NOTICE SMOKE EMMITTING INTO THE COCKPIT, ACCOMPANIED WITH LEFT PACK TEMPERATURE INCREASING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, SECURED THE LEFT PACK, SMOKE SUBSIDED. THE FLIGHT RETURNED TO PDX FORJun 29, 1999 · N828BX · Doug DC871F · Cabin Cooling SystemSDR UPS99830045Seat Track · corrodedINSPECTION TYPE:C2 FS 1480 TO 1540, RBL 52, THE SEAT TRACK IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SEAT TRACK FS 1470 TO 1580, SPLICED IN A NEW TRACK IAW SRM 53-2-3 FIG 8A.Jun 28, 1999 · N750UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830042Fitting · crackedINSPECTION TYPE:C2 FS 1240 AT LONG 33R, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.Jun 28, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99830056Rib · crackedINSPECTION TYPE:C2 RT WING L/E RIB AT XFS 425.5 IS CRACKED AT THE AFT LWR END. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jun 27, 1999 · N750UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99829973Light · inoperativeINSPECTION TYPE:N/A, FWD ENTRY DOOR EMERG EXIT LIGHT HAS ONE BULB INOP. REMOVED AND REPLACED ASSY PER DC8 MM 33-50-02P201, OPS CK GOOD.Jun 27, 1999 · N708UP · Doug DC871F · Emergency LightingSDR UPS99830060Seat Track · corrodedINSPECTION TYPE:C2 FS 1310, 1320 TO 1420, BL 0, THE CABIN SEAT TRACK IS CORRODED AT THE CLIPNUTS. CUT OUT DAMAGED SEAT TRACK FS 1310 TO 1430, FABRICATED, AND REPLACED TRACK AND INSTALLED IAW SRM 53-2-3.Jun 26, 1999 · N750UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830057Intercostal · corrodedINSPECTION TYPE:C2 FS 1440 TO 1460, LBL 8, THE CEILING INTERCOSTAL IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 1B.Jun 26, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99829974Fairing · cracked10 INCH CRACK; LEFT INBOARD FLAP SURFBOARD FAIRING D/D 174412. REMOVED AND FABRICATED PLATING AND INSTALLED PLATING PER SRM 57-7-1 PAGE 2. THIS CLEARS DEFFERAL 174412.Jun 26, 1999 · N708UP · Doug DC871F · Trailing Edge FlapsSDR UPS99830039Doubler · crackedINSPECTION TYPE:C2 RT WING L/E AT XFS 372, THE LIFT TRANSDUCER DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769589 AND SRM 51-1-21.Jun 25, 1999 · N750UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS99830043Web · corrodedINSPECTION TYPE:C2 FS 512 TO 520, LONG 33R TO 35R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRM 53-2-0 FIG 23.Jun 24, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99830050Angle · corrodedINSPECTION TYPE:C2 MAIN CABIN FS 879 TO 900, LBL 61, THE HORZIZONTAL ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5645332 AND SRM 51-1-21.Jun 22, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991153Pin · failedON GEAR RETRACTION LOUD BANG FROM REAR OF AIRCRAFT DOORS AND LANDING GEAR UNSAFE LIGHTS ON IN FRONT OF COCKPIT, FE LEFT GEAR DOOR LIGHT ON. AIRCRAFT FERRIED TO KMQY FOR REPAIR. INSTALLED NEW BOSS PIN PER S/B 32-102R5-6/12/72, EWW MA AI3210-01:03 AND 8110-3,Jun 22, 1999 · N500MH · Doug DC871F · Landing Gear Retraction/Extension SystemSDR UPS99830061Angle · corrodedINSPECTION TYPE:C2 VERTICAL SUPPORT ANGLE AT FS 1480, LONGERON 27L HAS HEAVY CORROSION. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3773157 AND SRM 51-1-20D.Jun 21, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99830055Fitting · crackedINSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED FS 1200 BETWEEN LONGERON 34R AND 33R. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D.Jun 21, 1999 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
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