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 IXXA0400009ODoor · unsecureCREW HAD MASTER WARNING LIGHT/BELLY DOOR LIGHT AT 90 KNOTS. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINTENANCE COMPLIED WITH REJECTED TAKEOFF INSPECTION AND NO DEFECTS WERE NOTED. MAINTENANCE THEN INSPECTED BELLY DOORS AND FOUND THE -B- PIT DOOR AJARFeb 3, 2004 · N603AL · Doug DC873F · Cargo/Baggage DoorsSDR DHL2004806572Skin · corrodedITEM REF. NR. 0738: LT WING CENTER L/E OB. VANE SLOT CORRODED AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-8, DWG U80-R08. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OJan 31, 2004 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2004806583Skin · corrodedLEFT WING CTR L/E CORRODED AT STA XW 257.000 (EXTERNAL SKIN). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW EDJan 31, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806580Skin · corrodedVERTICAL STAB L/E HAS HOLES CORRODED STA ZFS 179.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG 3. TRIMMED OUT AND REMOJan 31, 2004 · N806DH · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2004806571Skin · wornNOSE SECTION EXTERIOR SKIN WORN (STA 8.000 - 25.000, L-15L TO L-17L) HOLD OPEN HOOK COMPT (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 561-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-17, DWG U80-R17. PJan 31, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806578Skin · corrodedLT WING INBOARD OUTER L/E CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IJan 31, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806575Skin · crackedLT ELEVATOR UPPER SKIN SURFACE WITH 3.000 CRACK IN STA XE 39.188 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, TRIMMED OUT CRACKED SKIN, PERFORMED NDT INSPECTION. FABRICATED FILLER AND DOUBLER (2024-T3AL 0.032) CLEANED, TREATED AND PRIMED AREA ANJan 29, 2004 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2004806570Intercostal · crackedRIGHT WING T/E INTERCOSTAL LWR SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED INTERCOSTAL (7075-T6AL 0.090) IAW SRM 57-1-0. HEAT TREATED IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA ANDJan 29, 2004 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2004806569Intercostal · crackedLEFT WING T/E INTERCOSTAL LOWER SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (7075-TO-0.090) IAW SRM 57-1-0 PG 1. HEAT TREATED NEW INTERCOSTAL IAW SRM 51-1-1 PG 11, 13-21. CLEANED, TREAJan 29, 2004 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2004806566Skin · dentedRT ELEVATOR CONTROL TAB T/E WITH 1.500 X 0.500 DENT IN IT. CLEANED DAMAGED AREA IAW SRM 51-1-9 PG.1. FABRICATED DOUBLER (2024-T3AL 0.016) IAW SRM 55-2-2 PG.5, PAR.5 FIG. 3B. BONDED DOUBLER WITH HYSOL IAW SRM 51-1-9 PAR.4. REFER TO NR 2428 FOR REBALANCING.Jan 28, 2004 · N806DH · Doug DC873F · Elevator, Tab StructureSDR DHL2004806565Support Fitting · crackedITEM REF. NR. 0593: FWD CARGO COMPT. SEAT TRACK SUPPORT FITTING CRACKED 1.000 STA 120.000, BL0. CORR.: REMOVED CRACKED SEAT TRACK SUPPORT FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PJan 28, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806562Support · corrodedITEM REF. NR. 2209: AFT CARGO COMPT. LT TUNNEL FLOORBEAM VERTICAL SUPPORT CORRODED, STA 1520.000. CORRODED. REMOVED CORROSION FROM FLOORBEAM VERTICAL SUPPORT STA 1520.000 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. REMOVED CORRODED Jan 28, 2004 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004806568Skin · dentedRIGHT ELEVATOR CONTROL TAB EXTERNAL UPPER SKIN DENTED 1.500. REMOVED DAMAGED AREA IAW SRM 55-2-2 PG 5, PAR 5B. FABRICATED DOUBLER (2024-T3AL 0.016) IAW SRM 52-2-2 PG 5. INSTALLED DOUBLER IAW SRM 51-1-9 PAR 2.Jan 28, 2004 · N806DH · Doug DC873F · Elevator, Tab StructureSDR DHL2004873002Bolt · looseNR 2 START LEVER WILL NOT SHUT OFF, STUCK IN ON POSITION. REINSTALLED BOLT AND NUT ASSEMBLY ON NR2 ENGINE POWER CONTROL MECHANISM IAW M/M 76-11-1. RAN NR 2 ENGINE IAW JET RUN UP 13.1. CHECKED OPERATION OK. NR 2 FIRE HANDLE WILL NOT SHUT DOWN NR 2 ENGINE. AFJan 28, 2004 · N873SJ · Doug DC873F · Mixture ControlSDR DHL2004806574Skin · crackedFWD CARGO COMPT -A- BELLY DOOR LOWER PART EXTERNAL SKIN, STA 290.000 - 300.000, L31-L32R CRACKED 0.70 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-10, DWG U80-R10. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. FABRICATED NEW Jan 27, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806581Skin · corrodedLEFT WING OUTBOARD L/E LOWER PART CORRODED STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DJan 27, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806577Skin · corrodedLEFT WING OTBD L/E UPPER & LOWER PART CORRODED AT STA XW 761.695. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIRS (3EA). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDUJan 27, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806584Skin · damagedINTERIM REPAIR ON UPPER SURFACE OF RIGHT OUTBOARD FLAP, STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-1, DWG U80-R01. REMOVED SKIN SEGMENT WITH INTERIM REPAIR ON IT IAW ED EDU80-1, DWG U80-R01, SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMJan 27, 2004 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004806585Skin · damagedRIGHT OUTBOARD FLAP WITH INTERIM REPAIR ON UPPER FWD PLATING, STA XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-2, DWG U80-R02. REMOVED RIGHT OUTBOARD FLAP PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED SPLICE (2Jan 27, 2004 · N806DH · Doug DC873F · Trailing Edge FlapsSDR UPS04841780Relay · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON WITH SWITCH IN ARM POSITION. C/B RESET, LIGHTS WENT OUT. EN ROUTE EMERGENCY EXIT LIGHTS CAME ON AGAIN. WOULD NOT RESET, DISARM LIGHT TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIJan 27, 2004 · N813UP · Doug DC873F · Light System WiringSDR DHL2004806579Skin · corrodedRIGHT WING UPPER SKIN CORRODED AT STA XRS 202.000 S-12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-12, DWG U80-R12. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENJan 26, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806582Skin · corrodedRIGHT WING TOP PANEL PLATING CORROSION, STA XRS 204.000 S-9 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-11, DWG U80-R11. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. Jan 26, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806576Fitting · crackedRIGHT INBOARD STUB WING FITTING CRACK 4.000 STA XW 223.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM PO201953, DWG 5754705. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM PO201953, DWG 5Jan 25, 2004 · N806DH · Doug DC873F · Wing, Attach FittingsSDR DHL2004806561Skin · crackedITEM REF. NR. 1305: RT IB AILERON L/E WITH 1.500 CRACK AROUND FASTENER HOLE STA XA 502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN (7075-T6AL 0.040) CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SIDE. APPLIEDJan 24, 2004 · N806DH · Doug DC873F · AileronsSDR UPS04841835Beam · corrodedINSPECTION TYPE: C1, FWD PIT C1 DOOR JAMB CORNER TORQUE BOX BEAM IS CORRODED BEHIND T-BOLT LATCHES. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND WITHIN LIMITS IAW DAC DWG 9754007, REO G09673. MAT ID FOR SHIM 4340 STEEL BAR PO 371199.1 IAW REO G0967Jan 24, 2004 · N814UP · Doug DC873F · Fuselage Main, StructureSDR DHL2004806563Skin · corrodedRUDDER RT SKIN INTERNAL PART CORRODED AT STA ZR 140.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MFG MSG NR DHL-CVG04-0012H, DHL-CVG04-0014H, ED3584-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG.12. REMOVED CORRODED Jan 23, 2004 · N806DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2004806564Skin · corrodedITEM REF. NR. 2249: RUDDER LT SKIN INTERNAL PART CORRODED STA ZR. 162.000-ZR 173.000 (MAJOR REPAIR). CORRODED, PERFORMED MAJOR REPAIR IAW MFG MSG NR DHL-CVG 04-0013H, DHL-CVG04-0015H, ED3583-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IJan 23, 2004 · N806DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2004804002Connector · damagedSHORTLY FOLLOWING ENGINE START, NR 4 ENG SHORT CIRCUIT FIRE CAUTION LIGHT BEGAN FLASHING. LOOP-A TESTED OK SWITCHED TO B-LOOP MEL 26-2-3 CONTROL 15484. DEFERRED NR 4 ENGINE A-LOOP IAW MEL 26-2-3 DMI 15484 PLACARD INSTALLED. SHORTLY FOLLOWING ENGINE START NJan 23, 2004 · N804DH · Doug DC873F · Fire DetectionSDR DHL2004804001Fire Loop · out of positionNR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. DEFERRED PER MEL 26-2-3 DMI 15475. NR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. CHECKED NR 4 ENGINE FIRE LOOP FOR SECURITY, FOUND OK. REPOSITION LOOP FOR BETTER CLEARANCE CHECKED AS PJan 22, 2004 · N804DH · Doug DC873F · Fire DetectionSDR DHL2004806558Cargo Track · wornUPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1570.000-1590.000). REMOVED DAMAGED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50.Jan 21, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806552Cargo Track · wornUPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1590.000-1640.000). REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50.Jan 21, 2004 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806551Intercostal · crackedFWD ACCY COMPT BEAM JOINT ANGLE WITH INTERCOSTAL CRACKED 2.000 STA 70.000 LBL 47. REMOVED CRACKED ANGLE IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-1 PG 1, 2.Jan 21, 2004 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004806556Attach Fitting · crackedLEFT WING STUB WING INTERNAL PART FITTING CRACKED 4.000 AT STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM Jan 20, 2004 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2004806557Clip · crackedNR 3 MAIN TANK CLIP CRACK 1.000 BETWEEN REAR SPAR AND S-51, XRS 22.750. REMOVED CRACKED CLIP (NR 3 MAIN TANK XRS 22.750). CLEANED, TREATED AND APPLIED COATING MATERIAL TO CLIP AND AREA IAW SRM 51-1-12 PG 7-21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9.Jan 20, 2004 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS04841773Skin · corrodedINSPECTION TYPE: PFLT, BELLY SKIN BULGED/CRACKED AREA OF PIT 34 DOOR CUTOUT AT LONG 35R & LR 36. ACCCOMPLISH LFEC INSP OF AREA FOUND INDICATION OF 30 PERCENT DEFECT IN 3 AREAS (MARKED) PER ENGINEERING REQUEST ACCOMPLISHED ETLF 6-10-02 TO MAP AREA OF DEFECJan 20, 2004 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806550Door · crackedLEFT INBOARD SLOT UPPER DOOR WITH 0.750 CRACK IN IT. REMOVED AND REPLACED LEFT INBOARD SLOT UPPER DOOR IAW MM 27-80-1 PG 201-204. REFER TO NR 2228 FOR OPS CHECK.Jan 20, 2004 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL200480654Fitting · crackedMAIN CARGO COMPT CUSP EXTRUSION FWD FITTING CRACKED 3.000 AT STA 1180.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. IJan 16, 2004 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004806555Attach Fitting · corrodedAFT CARGO COMPT ANCHOR PLATE SUPPORT FITTING CORRODED, STA 1440.000-1460.000, RBL 10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANCHOR PLATE SUPPORT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATEJan 15, 2004 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004806547Skin · damagedINTERIM REPAIR ON RIGHT INBOARD FLAP UPPER SURFACE STA XW 104.000-122.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-TJan 15, 2004 · N806DH · Doug DC873F · Trailing Edge FlapsSDR UPS04841834Skin · corrodedINSPECTION TYPE: C1, REMOVED BATHTUB FITTING AT STA 879 AND FOUND THE SKIN UNDER FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. MATERIAL ID FOR FILLER IAW REO G09662, FABBED FILLER IAW REO G09 662. ALODINED ANJan 15, 2004 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS04841833Fitting · crackedINSPECTION TYPE: C1, CABIN STA 680 LONGERON 11 RIGHT SIDE FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-3-5. LOCATED NEW FITTING, DRILLED EXISTING FASTENER HOLES, DEBURRED IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-3-0.Jan 14, 2004 · N814UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04841819Intercostal · crackedINSPECTION TYPE: C1, AFT PIT STA 1540 RBL 30 INTERCOSTAL ON AFT BULKHEAD CRACKED AT NUT PLATE. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-21.Jan 14, 2004 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004806540Skin · crackedUPPER FUSELAGE EXTERIOR SKIN WITH 1.000 INCH CRACK IN IT (STA 1742.000-1743.000, L-16L TO L-17L), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-5-3 FIG 1, SRM 53-2-1 FIG 7. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT CRACKED SKIN AREA IAW SRM 53-2-1 FJan 14, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806546Fitting · crackedAFT CARGO COMPT FITTING CRACKED 2.000, L-34R L-35R, STA 1240.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9.Jan 14, 2004 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806543Skin · crackedEXTERNAL FUSELAGE FWD SVC DOOR JAMB FWD UPPER CORNER CRACKED 1.000 AT STA 160.000 L-11R - L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181, DWG SRO8530021, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUTJan 13, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806553Skin · corrodedLEFT WING OTBAORD L/E CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2H. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED EXISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUJan 12, 2004 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004806554Skin · wornLEFT WING INBOARD FLAP UPPER SKIN WORN AT STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED WORN SKIN IAW SRM 51-1-21, SRM 51-3-0 PG 1. FABRICATED NEW SKIN (2024-T3AL 0.040) IAW SRM 57-7-1 FIG 1. CLEANED, Jan 12, 2004 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004806532Fitting · crackedNR 3 RIGHT STUB WING ZEE PAN FITTING WITH 8.000 CRACK, STA XILD 42.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN FITTING IAW SRM 51-1-21 PG 1.Jan 12, 2004 · N806DH · Doug DC873F · Wing, Attach FittingsSDR DHL2004806541Skin · crackedUPPER FUSELAGE EXTERIOR SKIN WITH 1.000 CRACK IN IT (STA 1742.000-1743.000, L-16R TO L-17R), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SRM 53-5-3 FIG 1. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN AREA AND FABRICATED FILLERJan 12, 2004 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004806537Shear Tie · crackedACCESSORY COMPT FORMER ATTACHING FRAME TO FUSELAGE 1.000 CRACK, STA 640.000 L-26R TO L-27R. REMOVED FASTENER IAW SRM 51-1-21 PG 1-2. CUT OUT FORMER DAMAGED AREA AND FABRICATED FORMER REPAIR ANGLE (7075 0.0.071) IAW SRM 53-2-0 PG 11 FIG 2A. HEAT TREATED IAW Jan 12, 2004 · N806DH · Doug DC873F · Fuselage Main, Structure
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