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 UPS03841413Longeron · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 LEFT CRACKED BETWEEN FS 1768-1777. REMOVE CRACKED LONGERON IAW UPS DC8 SRM 51-1-20 & 51-1-21. LOCATE NEW LONGERON AND DRILL EXISTING FASTENER HOLES IAW UPS DC8 SRM 51-3-2. INSTALLED NEW LONGERON IAW UPS DC8 SRSep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841412Fitting · crackedINSPECTION TYPE:C3 AFT FUSE INTERIOR L17LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED CRACKED LONGERON END FITTING AND INSTALLED NEW FITTING IAW UPS DC8 SRM, 51-1-20D AND 51-1-21.Sep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841411Fitting · crackedINSPECTION TYPE: C3, AFT FUSE INTERIOR L10LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED L10LT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841410Longeron · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 RIGHT CRACKED BETWEEN FS 1768-1776. REMOVED L-17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 56493 27, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DSep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841409Fitting · crackedINSPECTION TYPE: C3, AFT FUSE INTERIOR L17 RT END FITTING CRACKED BETWEEN FS 1766-FS 1772. REMOVED L17 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841408Attach Fitting · crackedINSPECTION TYPE: C3, NR 4 ALT HAS FWD BOOST PUMP MOUNT FITTING CRACKED AT S-59. REMOVED AND REPLACED FITTING WITH NEW FITTING PO SP0938702 IAW DC8 SRM 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873F · Wing, Attach FittingsSDR UPS03841407Fitting · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L10 RT END FITTING CRACKED BETWEEN FS 1768-1772. REMOVED L10 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841405Frame · corrodedINSPECTION TYPE: C3, FRAME CORRODED AT STA 260 BETWEEN LONGERONS 35L-35R. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE SECTION OF FRAME IAW DC8 SRM 53-2-0. FABBED FRAME, 4 EA RPR ANGLES, & STRAPS IAW DC8 SRM 51-1-1, 53-Sep 9, 2003 · N813UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841404Longeron · corrodedINSPECTION TYPE: C3, LONGERON 36 CORRODED AT STA 220-240 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .027 INCH, REMAINING .053 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE IAW DC8 SRM 53-2-2. RECEIVED LONG SECTION, LOCATED, DRSep 9, 2003 · N813UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841403Skin · misrepairedINSPECTION TYPE: C3, L1 DOOR CORNER UPPER FWD CORNER IS NOT PER SRM. FABBED -15 -17 DOUBLERS, -19 FILLER IAW DC8 SRM 53-2-0 FIG 15 TR 53- 155. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D. RE-INSTALLED FOM PARSep 9, 2003 · N813UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841402Fitting · crackedINSPECTION TYPE: C3, AFT PIT AT STA 1220 STR 34R INSIDE TORQUE BOX AREA FITTING CRACKED. REMOVED FITTING CRACKED IAW DC8 SRM 51-1-20D, REC'D NEW Z-FITTING AND 2 EA PLATES P/N 3755841-1, P/N 3755841-3, P/N 3755841-5. LOCATED, DRILLED, AND TRIMMING IAW DC8 SRSep 9, 2003 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841401Frame · corrodedINSPECTION TYPE: C3, AFT PIT AT STA 1040 STR 34R FRAME HAS CORROSION UNDER NUT PLATE. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .070 INCH, REMAINING .010 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB RPR ANGLE AND 2 FILLERS IAW UPS EO DC8-5310-11Sep 8, 2003 · N813UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841397Skin · crackedINSPECTION TYPE: C3, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT UPPER AFT CUTOUT CRACKED AREA IAW DC8 SRM 53-2-0 FIG 16, TR 53-130 & TR53-156 PERFORMED HFEC IAW MD NDT SPM 06-10-01.001 NO CRACKS NOTED. REMOVED INTERCOSTAL ABOVE R2 DOOR, 2 EA CLIPS, TOP AFT Sep 8, 2003 · N813UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841400Attach Angle · corrodedINSPECTION TYPE: C3, FWD PIT SMOKE BARRIER UPPER ATTACH ANGLE CORRODED NEAR CENTER LINE. REMOVED CORR IAW DC8 SRM 51-1-8, ORIG .063 INCH, REMOVED .014 INCH, REMAINING .049 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 5Sep 7, 2003 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003805600Panel · delaminatedRIGHT CTR WING LOWER PART PANEL NR 721 INTERNAL SKIN DELAMINATED AT STA 730.000. REMOVED AND REPLACED NR 721 PANEL ON RIGHT CTR WING, STA 730.000. FOR REMOVAL SEE JC 8-10-30-003, FOR INSTALLATION SEE JC 8-90-30-003.Sep 5, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805596Clip · crackedNR 4 PYLON 497 ACCESS PANEL INTERNAL PART CLIP CRACKED AT STA 321.000. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-18B. INSTALLED NEW CLIP WITH NEW FASTENERS ON NR 4 PYLON 497 ACCESS PANEL STA 321.000 IAW SRM 51-Sep 5, 2003 · N805DH · Doug DC873F · Nacelle/Pylon Miscellaneous StructureSDR DHL2003805597Clip · crackedNR 2 MAIN TANK CLIP CRACKED 1.000 AT STA XRS 22.750, S-61. REMOVED 505F, 560F ACCESS DOOR (INTERNAL). REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. REINSTALLED 560F, 505F ACCESS DOOR IAW MM 20-16-0 PG 201-202. FOR Sep 4, 2003 · N805DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003805598Bracket · crackedN/R LT MLG MID DOOR LWR BRACKET WITH CRACK IN IT. REMOVED AND REPLACED BRACKET TO LEFT MLG MID DOOR IAW SRM 32-12-1 PG 401. REFER TO JC 8-32-20-007 FOR OPS CHECK.Sep 3, 2003 · N805DH · Doug DC873F · Landing Gear DoorsSDR DHL2003801089Seal · leakingCABIN PRESSURIZATION SYSTEM WILL NOT HOLD CABIN PRESSURE BELOW 10,000 UNLESS BOTH FLOW SWITCHES ARE IN THE MID POSITION OR HIGHER. CABIN ALTITUDE HORN ACTUATED AND THE EMERGENCY PROCEDURES WERE ACCOMPLISHED.INSPECTED AND CLEANED MAIN DOOR SEAL AND INFLATION HOSep 2, 2003 · N801DH · Doug DC873F · Cargo/Baggage DoorsSDR UPS03841212Intercostal · crackedINSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 260-280 IS CRACKED AT LONG. 33R REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG.5750726,AND SRM. 51-1-20D.Aug 31, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003805595Skin · delaminatedLEFT LOWER FUSELAGE PANEL NR 736 INTERNAL SKIN DELAMINATED STA 1040.000 - STA 1060.000. REMOVED AND REPLACED LEFT LOWER FUSELAGE PANEL NR 736 IAW SRM 51-3-0 PG 1.Aug 30, 2003 · N805DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003805531Skin Panel · delaminatedLEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 47.00). REMOVED AND REPLACED LWR WING T/E LWR PANEL (STA XW.5.000 - 47.000) IAW SRM 51-3-0 PG 1.Aug 29, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805599Panel · delaminatedRT LOWER FUSELAGE PANEL NR 736 EXTERNAL SKIN DELAMINATED, STA 1040.000 - STA 1060.000. REMOVED AND INSTALLED RT LOWER PANEL NR 736 (STA 1040.000 - 1060.000) IAW MM 53-50-3.Aug 29, 2003 · N805DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003805601Panel · delaminatedRIGHT AFT ADF SENSE ANTENNA PANEL INTERNAL SKIN DELAMINATED, STA 980.000. REMOVED AND INSTALLED RIGHT AFT ADF SENSE FOR OPS CHECK SEE JC BE1E34026.Aug 29, 2003 · N805DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003805594Skin · delaminatedLEFT WING-FUSELAGE NR 708 UPPER FAIRING INTERNAL SKIN DELAMINATED, STA 1040.000 - STA 1080.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 708 (STA 1040.000 - 1080.000) IAW SRM 51-3-0 PG 1.Aug 29, 2003 · N805DH · Doug DC873F · Aerodynamic FairingsSDR DHL2003805580Skin · damagedRIGHT INNER WING CTR EXTENDED L/E SLOT OUTER PLATING SHOWS ELONGATED HOLES AROUND STA XW.257.000 (MAJOR REPAIR). PERFORMED MAJOR REAPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FAAug 28, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805588Skin · damagedRT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AT STA XS 247.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER EXTERNAL DAug 28, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR UPS03841231Frame · corrodedINSPECTION TYPE: C2, STATION 55 BELTFRAME IS CRACKED AND CORRODED BETWEEN LONG. 35L TO 35R. REMOVED DAMAGED AREA,FABRICATED AND INSTALLED REPAIR J-ANGLES I.A.W. DC8-53A-011,AND SRM 51-1-20DAug 28, 2003 · N809UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841203Fitting · crackedINSPECTION TYPE: C2, STATION 300 LONG. 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3754041,SRM.53-2-0 FIG. 1B, DWG. 9751879.Aug 28, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841164Web · crackedINSPECTION TYPE: C2, WEB IN RUDDER LE AT FORWARD SPAR IS CRACKED AT XR 160 REMOVED WEB SECTION,FABRICATED AND INSTALLED REPLACEMENT WEB SECTION IAW SRM. 55-2-4 FIG. 1Aug 28, 2003 · N809UP · Doug DC873F · Rudder Miscellaneous StructureSDR DHL2003805587Skin · damagedLEFT WING EXTENDED L/E OUTBD VANE FWD PLATING ELONGATED HOLES AROUND STA XOLDO.67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, THE EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREAAug 27, 2003 · N805DH · Doug DC873F · Leading Edge DevicesSDR UPS03841226Frame · corrodedINSPECTION TYPE: C2, STATION 1320 LONGERON 31 RT AND FRAME ARE CORRODED BEYOND LIMITS, REMOVED,FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA. 1230 TO 1320 I.A.W. SRM. 53-4-1 FIG. 43A,AND REMOVED CORRODED AREA ON FRAME,FABRICATED AND INSTALLED FILLER ANDAug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841222Fitting · crackedINSPECTION TYPE: C2, FLOORBEAM FITTING IS CRACKED AT STA. 340 RBL. 58 REMOVED AND REPLACED FITTING IAW DWG. 9754022,AND SRM. 51-1-20DAug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841221Bulkhead · crackedINSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT LBL 26 AND 36, 67 ABOVE CABIN FLOOR CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLERS AND FILLERS I.A.W. DWG. SRO08530007Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS03841218Bulkhead · crackedINSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT STA 1766 AT RBL 26 AND 36. CUTOUT DAMAGED AREAS AT RBL 26 AND 36,NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRO8530007.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS03841217Frame · corrodedINSPECTION TYPE: C2, AFT SIDE STATION 70 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONGERON 29L AND 30L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED ANGLE REPAIR AND DOUBLERS I.A.W. SRM. 53-2-5 FIG. 8C-2.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841215Longeron · corrodedINSPECTION TYPE: C2, LONGERON 28R IS CORRODED BEYOND LIMITS AT SPLICE FITTING AT STA. 450. REMOVED,FABRICATED AND REPLACED LONGERON SECTIONS BETWEEN STA.430 AND 470,AND REPLACED LONGERON SPLICES I.A.W. SRM. 53-2-2 FIG.8.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841213Intercostal · crackedINSPECTION TYPE: C2, COCKPIT SUBFLOOR INTERCOSTAL UPPER FLANGE IS CRACKED AT STA.-21 LBL 12. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 53-2-0 FIG. 1B.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841209Fitting · crackedINSPECTION TYPE: C2, LONG. 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA. 1140 AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841208Fitting · crackedINSPECTION TYPE: C2, LONG. 32L SPLICE FITTING IS CRACKED AT STA. 610. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841206Fitting · crackedINSPECTION TYPE: C2, FLOOR SUPPORT FITTING IS CRACKED AT STA. 120 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 5758571,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841201Frame · crackedINSPECTION TYPE: C2, BELT FRAME IC CRACKED AT STA. 55 LONG. 24L TO 25L CUTOUT DAMAGE, FABRICATED AND INSTALLED FILLER AND ANGLE DOUBLER I.A.W. SRM. 53-2-0 FIG. 2.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841200Longeron · crackedINSPECTION TYPE: C2, STATION 1240 LONG. 30R IS CRACKED REMOVED LONGERON SECTION STATION 1230-1250,FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-4-1 FIG.4,53-2-2 FIG. 10.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841187Angle · crackedINSPECTION TYPE: C1, MIDSHIP ACCESSORY COMPARTMENT RT SIDE AT STA 670 L28R IS CRACKED. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS IAW DC8 SRM 53-2 -0(ORIG-.062 AND REMAINING-.017). FABRICATED REPAIR ANGLE IAW DC8 SRM T R53-122. ALODINED AND PRIAug 27, 2003 · N801UP · Doug DC873F · Fuselage Main, StructureSDR UPS03841166Intercostal · corrodedINSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 80-100 AT LONGERON 28 RT IS CORRODED BEYOND LIMITS REMOVED,FABRICATED AND REPLACED INTERCOSTAL IAW SRM. 53-3-2 FIG. 5 AND 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841162Longeron · crackedINSPECTION TYPE: C2, STA. 1720 AND 1740 LONG. 15R IS CRACKED AT FRAME ATTACH BOLTS. REMOVED DAMAGED LONGERON SECTION STA. 1720-1760, FABRICATED AND INSTALLED SECTION IAW SRM. 53-2-2 FIG. 10.Aug 27, 2003 · N809UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841210Fitting · crackedINSPECTION TYPE: C2, 2 EACH CRACKED SEAT TRACK FITTINGS ,B-PIT CEILING STA. 420,RBL 24. REMOVED DAMAGED SEAT TRACK SECTION BETWEEN STA. 300 TO 490 RBL 24-31 FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM. 53-2-3 FIG. 8A,AND REPLACED FITTINGS IAW SRM. 53Aug 26, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841207Fitting · crackedINSPECTION TYPE: C2, SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 700 LBL. 24. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755222,AND SRM. 51-1-20D.Aug 26, 2003 · N809UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841205Skin · crackedINSPECTION TYPE: C2, RT PRIMARY HEAT EXCHANGER CUTOUT HAS A CRACK ON SKIN AT LOWER AFT CORNER STATION -12 AT LONG. 27R. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-5330-4732-D APPX. A.Aug 26, 2003 · N809UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841199Web · corrodedINSPECTION TYPE: C1, FLIGHT DECK SUBFLOOR FS 133 LBL36 INDICATION OF HIDDEN CORROSION (MISSING AND FITTED REIVET HEADS) REMOVED COVER PANEL TO FOM. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED FILLER DOUBLER AND FINGER DOUBLERS IAW DAC DWG SR08530026. ALODINEAug 26, 2003 · N801UP · Doug DC873F · Fuselage Miscellaneous Structure
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