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 DHL2007806522Fitting · crackedRT WING FWD FITTING CRACKED 1" STA XW 74.000 S-51, REF NR 3 MAIN TANK ACCESS DOOR NR 505F) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE YELLOW COATING IApr 4, 2007 · N806DH · Doug DC873F · Wing, Attach FittingsSDR DHL2007806531Doubler · crackedRT WING ACCESS DOOR NR 505F INTERNAL DOUBLER HAS TWO CRACKS OF 0.500" AND 0.250" STA XRS 18.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 36. PERFORMED NApr 4, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806532Doubler · crackedLT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 21.000 S-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 36. PERFORMED NDT INSPECTION IAApr 4, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806518Skin · wornRT INBD FLAP UPPER SKIN WORN STA XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 ITEM D, SRM 51-1-14 PG 1. CLEANED, Apr 4, 2007 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2007806529Frame · brokenFOUND RT WING CTR L/E INTERIOR FORMER BROKEN STA XFS 510.222. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075-0 0.063") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3 FIG 4. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-1Apr 3, 2007 · N806DH · Doug DC873F · Wing SparSDR DHL2007806517Skin · delaminatedNR 1 RT SPOILER PANEL EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED NR 1 RT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 075764 FOR OPS CHECK.Apr 3, 2007 · N806DH · Doug DC873F · SpoilersSDR UPS07849586Release Mech · contaminatedINSPECTION TYPE:N/A DIVERSION - LEFT NOSE GEAR DOOR OPEN IN FLIGHT. FOUND LEFT NOSE GEAR DOOR RELEASE TRIGGER JAMMED WITH DEBRIS. CLEANED TRIGGER IAW MM 32-20-00-01. GEAR DOOR LATCHES NORMALLY, A/C OK FOR SERVICE.Apr 3, 2007 · N819UP · Doug DC873F · Landing Gear DoorsSDR DHL2007806524Fitting · crackedMAIN CARGO COMPT BELOW CABIN FLOOR FITTING CRACKED STA 717.750 RBL 22". REMOVED AND REPLACED CRACKED FITTING IN MAIN CARGO COMPT STA 717.750 RBL 22" IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806520Skin · crackedLT RUDDER EXT SKIN DENTED AT STA ZR 188.781 AND CRACKED 1" AT STA ZR 198.844 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING (PLATING AND BONDED DOUBLEApr 2, 2007 · N806DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2007806513Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED (STA 1140.000 - 1160.000 L-35R). REMOVED AND REPLACED CRACKED FITTING AT AFT CARGO COMPT BILGE (STA 1140.000 - 1160.000 L-35R) IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806512Fitting · crackedMAIN CARGO COMPT BELOW CABIN FLOOR FITTING CRACKED STA 717.750 RBL 22". REMOVED AND REPLACED CRACKED FITTING IN MAIN CARGO COMPT STA 717.750 RBL 22" IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806530Fitting · corrodedNR 1 CARGO DOOR JAMB FITTING CORRODED, STA 280.000 L-31R. REMOVED CORROSION FROM FITTING AT NR 1 CARGO DOOR JAMB IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA Apr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806508Skin · delaminatedFOUND LT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 219.000 - 339.000). REMOVED AND REPLACED LT WING T/E LWR PANEL (STA XF 219.000 - 339.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Apr 2, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806523Door Frame · misrepairedREPAIR ON FWD UPPER JAMB CORNER OF "B" CARGO DOOR IS NOT IN ACCORDANCE WITH DWG SR08530019 (STA 520.000 - 540.000 L-25R TO L-27R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. REMOVED EXISTING NON Apr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2007806519Door Frame · misrepairedREPAIR ON FWD UPPER JAMB CORNER OF "C" CARGO DOOR (STA 1160.000 - 1180.000, L-21R TO L-23R) IS NOT IN ACCORDANCE WITH DWG NR SR08530019 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. REMOVED NON SApr 2, 2007 · N806DH · Doug DC873F · Fuselage Main, StructureSDR UPS07849626Floorbeam · crackedINSPECTION TYPE:C2 MAIN CARGO FLOORBEAM AT STA 280 RBL 24 CRACKED FROM EXFOLIATION CORROSION. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 280 RBL 24 IAW SRM 51-2-1 PG 8 FIG 1. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR 51-130 FIG 1 SHEET 1.Apr 2, 2007 · N805UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07849588Battery Pack · failedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK WILL NOT CHARGE. EMERGENCY EXIT BATTERY PACK REPLACED IAW DC8 AMM 33-50-01-2.Apr 2, 2007 · N814UP · Doug DC873F · Emergency LightingSDR UPS07849587Battery Pack · inoperativeINSPECTION TYPE:N/A FWD PASSAGEWAY AND EMERGENCY LIGHT NEXT TO EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED PASSAGEWAY AND EMERGENCY LIGHT. LIGHT OPS GOOD.Apr 1, 2007 · N851UP · Doug DC873F · Emergency LightingSDR DHL2007806562Fitting · crackedMAIN CARGO COMPT FWD FITTING CRACKED 1" STA 902.125 L-19R. 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, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-0251-001 (WO 470) FOR FIMar 31, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849618Rib · crackedINSPECTION TYPE:C2 12TH RIB FROM BOTTOM OF RUDDER ON L/E IS CRACKED. STOP DRILLED CRACK ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0 FIG 2 SHEET 2.Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/RibSDR UPS07849617Rib · crackedINSPECTION TYPE:C2 18TH RIB FROM BOTTOM OF RUDDER ON L/E CRACKED. STOP DRILLED CRACK ON 18TH RIB FROM BOTTOM OF L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 18TH RIB IAW SRM 55-06-00 FIG 028.Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/RibSDR UPS07849611Attach Angle · crackedINSPECTION TYPE:C2 ATTACH ANGLE FOR VERT FIN L/E TO FUSELAGE BENT AND CRACKED RIGHT SIDE FS 1690. REMOVED ATTACH ANGLE FOR VERT FIN TO FUSELAGE AT STA 1690 IAW SRM 51-3-0. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER AT FS 1690 VERT FIN L/E TO FUSELAGE Mar 31, 2007 · N805UP · Doug DC873F · Vertical Stabilizer, Attach FittingsSDR DHL2007806511Cargo Track · wornFOUND UPPER CARGO COMPT NR 7 TRACK LUG WORN STA 228.000. CUT OUT WORN SECTION OF TRACK NR 7 IAW SRM 53-2-3 PG 17-19. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 53-2-3 PG 17-19, SRM 51-3-0, SRM 51-3-1 (TORQMar 30, 2007 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007806526Panel · delaminatedLT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 507.000 - 566.000). REMOVED DELAMINATED T/E UPPER PANEL (STA XA 507.000 - 566.000) IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T/E PANEL IAW SRM 51-3-0, SRM 51-3-1Mar 30, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS07849639Skin · corrodedINSPECTION TYPE:C2 AFTER REMOVAL OF C-2 (B-PIT) SCUFF PLATE FOUND CORROSION ON FUSELAGE SKIN. REMOVED CORROSION AND FOUND SKIN TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. PROCURED AND INSTALLED REPLACEMENT SKIN FROM STA 450-610 L31L-L31R IAW SRM 51-1-20D, ANDMar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849631Skin · crackedINSPECTION TYPE:C2 HFEC INSP DETECTED A CRACK ON THE C-4 (D-PIT) LWR AFT DOOR JAMB CORNER STARTING AT FASTENER GOING FWD TO EDGE OF DOOR CUTOUT. CUT OUT DAMAGED AREA AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLEDMar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007806506Angle · crackedFOUND RT OUTBD FLAP T/E ANGLE CRACKED (STA XF 125.000 - 169.000). REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL2024 "0" 0.050") IAW SRM 57-7-1 FIG 3. PERFORMED HEAT TREATMENT FROM 2024 "0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREMar 29, 2007 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS07849725Fitting · crackedINSPECTION TYPE:C2 C-PIT, AT UPPER CORNER OF CROSS SLIDE DOOR CUTOUT, FITTING HAS 4.5" CRACK STA 1200 RBL 65. REMOVED CRACK FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAW SRM 51-1-20D. INSTALLED REPLACEMENT FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAMar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849628Longeron · crackedINSPECTION TYPE:C2 AIR CONDITIONING COMPT LONGERON CORRODED AT STA 45 L30R AND 5 INCH LONG CRACK STA 65. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21 AND 51-1-20D.Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849619Bulkhead · corrodedINSPECTION TYPE:C2 A/C COMPT FWD BULKHEAD CORRODED AT STA 8 BL 0. REMOVED CORRODED WEB AND CHANNEL AT STA 8 BL 0 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR WEB, AND CHANNEL AT STA 8 BL 0 IAW SRM 51-09-00 FIG 068A, AND EO DC8-5350-7876.Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, BulkheadSDR DHL2007806507Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED STA 1140.000 - 1120.000 L-35R. REMOVED AND REPLACED CRACKED FITTING IN AFT CARGO COMPT BILGE (STA 1140.000 - 1120.000, L-35R) IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Mar 28, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806515Intercostal · crackedMAIN CARGO COMPT INTERCOSTAL SUPPORT ANGLE CRACKED 1" STA 1580.000 L-11L. REMOVED CRACKED INTERCOSTAL SUPPORT ANGLE IAW SRM 51-1-21. FABRICATED ANGLE (AL 7075T6 0.040") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALMar 28, 2007 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007806509Cargo Track · wornUPPER CARGO COMPT NR 4 TRACK LUG WORN (STA 1675.000 - 1705.000). CUT OUT TRACK DAMAGED SEGMENT AND FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SMar 28, 2007 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007806516Doubler · corrodedFUS AFT ACCY COMPT INTERNAL DOUBLER CORRODED (STA 1560.000 - 1580.000, L-22R). REMOVED CORROSION FROM INTERNAL DOUBLER (STA 1540.000 - 1580.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED INTERNAL DOUBLER IAW SRM 51-1-21, SRMMar 28, 2007 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849585Frame · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS 44 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00-0, 51-1-20D AND DWG 5644310.Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS07849584Frame · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS32 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5 5-02-00-0, 51-1-20D AND DWG 5644310.Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS07849571Packing · leakingAT CRUISE FL 350 HYD PRESS SENT TO ZERO AND HYD QTY WENT TO EMER/AUX POSITION. LOSS OF HYD QTY AND PRESS CHECKLIST ACCOMPLISHED. REPLACED PACKINGS & RETAINER RINGS REF IPC 29-11-24 ITEM 175,180,185 ON WING SLOT CONTROL VALVE IAW MM 27-80-04-2. LEAK AND OPS CMar 28, 2007 · N803UP · Doug DC873F · Hydraulic System, MainSDR DHL2007806510Cargo Track · wornUPPER CARGO COMPT NR 2 TRACK LUG WORN STA 1588.000. REMOVED WORN TRACK SEGMENT AND SPLICES IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SPLICES IAW SRM 53-2-3Mar 27, 2007 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007806504Angle · corrodedFWD ACCY COMPT SUB-FLOORBEAM ANGLE CORRODED STA 50.000 LBL 30". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED SUPPORT ANGLE IAW SRM 51-1-21. FABRICATED NEW SUPPORT ANGLE (AL2024T3 0.050") IAW SRM 53-2Mar 25, 2007 · N806DH · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07849635Door Frame · damagedINSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-2 (B-PIT) DOOR JAMB UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 20. REMOVED STEEL DOUBLER FROM B-PIT DOOR JAMB UPPER FWD CORNER IAW SRM 51-01-21A. FABRICATED AND INSTALLED CORRECT TRIPLER, DOUBLER, AND FIMar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849627Door Frame · damagedINSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-3(C-PIT) DOOR JAMB LWR FWD CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG 22 AND/OR DWG SRO8530019. REPAIRED DOOR CORNER IAW SAA EA 008-5310-01-A0755.Mar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849615Skin · crackedINSPECTION TYPE:C3 EXTERIOR FUSELAGE SKIN CRACKED AT L30L STA 1690. REPAIRED FUSELAGE SKIN AT STA 1690 L30R - L28L IAW SAA EA 008-5330- 01-0750, UPS EO DC8-5330-26567-A, FAA FORM 8100-9, AND AMOC APPROVAL FOR AD 2007-02-02.Mar 22, 2007 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849575Frame Splice · crackedINSPECTION TYPE:C3 L24L END FITTING CRACKED ON AFT SIDE OF STA 1690 FRAME SPLICE. REMOVED END FITTING AT STA 1690 L24L IAW SRM 51-1-21. DRILLED, REAMED AND INSTALLED END FITTING AT STA 1690 L24L IAW SRM 51-3-2 AND SRM 51-1-20D.Mar 22, 2007 · N811UP · Doug DC873F · Fuselage Main, FrameSDR UPS07849542Light · malfunctionedAFTER TAKEOFF, EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH EXCEPT TO DISARM EMERGENCY LIGHTS. FOUND C/B PULLED. RESET C/B AND PERFORMED EMERGENCY LIGHTS. OPS CHECK PER MM 33-50-01-2. EMERGENCY LIGHTS, OPS CHECK GOOD.Mar 22, 2007 · N851UP · Doug DC873F · Emergency LightingSDR UPS07849576Floorbeam · corrodedINSPECTION TYPE:C3 FLOORBEAM STA 1790 LBL 8 HAS DEEP GOUGE AND EXFOLIATED CORROSION. REMOVED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 51-3-0. FABRICATED AND INSTALLED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 53-7-3, AND SRM 51-3-0.Mar 21, 2007 · N811UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07849537Brake Assy · brokenINSPECTION TYPE:N/A BTB 20:10Z REASON FOR BTB IS BLOWN TIRE ON T/O ROLL. PERFORMED REJECTED TAKEOFF. FOUND NR 6 WHEEL ASSY BROKEN (RIM). REPLACED NR 6 BRAKE ASSY AND WHEEL ASSY PER MM 32-42-01-4 AND MM 32-40-01-2. NO OTHER DAMAGE FOUND.Mar 21, 2007 · N894UP · Doug DC873F · Landing Gear Brake SystemSDR DHL2007806501Cargo Track · wornUPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 1670.000 - 1705.000). CUT OUT NR 3 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES (AL7075T6 0.100"/ 0.125"/ 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA IAW SRMMar 20, 2007 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA070015ODownlock Switch · defectiveDURING LANDING INTO KTOL WHEN THE GEAR HANDLE WAS PLACED IN DOWN POSITION LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE, RED LIGHT CYCLE ON AND OFF. THE CREW RECYCLED THE GEAR AND GEAR OPERATED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTMar 17, 2007 · N604BX · Doug DC873F · Landing Gear Position and WarningSDR DHL2007806500Floor Panel · corrodedUPPER CARGO COMPT FLOOR PANEL UPPER SKIN CORRODED (STA 1550.000 - 1560.000) RBL 51" - 54". REMOVED CORROSION FRONT FLOOR PANEL UPPER SKIN (STA 1550.000 - 1560.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT FLOOR PANEL DAMAGEMar 15, 2007 · N806DH · Doug DC873F · Fuselage Floor PanelSDR UPS07849602Floorbeam · corrodedINSPECTION TYPE:C3 FLOORBEAM STA 1723 RBL 30 - RBL 15 HAS POPPED RIVETS AND EXFOLIATION CORROSION. REMOVED CORROSION AND REPAIRED FLOORBEAM AT STA 1723 RBL 30 - RBL 15 IAW SAA EA 008-5320-01-A0762, UPS RAA DC8-53-20617, AND FAA FORM 8100-9.Mar 15, 2007 · N811UP · Doug DC873F · Fuselage Main, Floor Beam
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