Douglas DC-8-63F

Service difficulty reports · 1,883

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC863F'
  ORDER BY difficulty_date DESC"

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SDR ARWA9610006Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON RT SIDE UPPER PLATING OF FUSELAGE STA 834.5 AND 857.125, BETWEEN LONG 11R AND 12R. REPAIRED PLATING IAW DC-8 SRM 53-2-1 FIG 2 SH 5.1. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-20D AND 51-1-17.Oct 25, 1996 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9610005Fitting · crackedDURING C-CHECK, FOUND CRACKED FITTING AT FWD LWR CARGO NR 1 PIT RT TUNNEL STA 340. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUTHORIZATION DATED 09-10-96 FILE C1-P63-ATM/759. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D.Oct 25, 1996 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9610004Skin · corrodedDURING C-CHECK, FOUND LEVEL 1 CORROSION AND MISSING RIVETS AT STA 1660 AND L24L OF FUSELAGE. REPAIRED CORRODED AREA IAW FAA 8110-3 FORM APPROVED DRAWING CF-N661AN-05/96, DATED SEPTEMBER 17, 1996 AND DC-8 SRM 53-2-2 FIG 10 SH 1B4.Oct 25, 1996 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9610003Angle · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION IN ANGLE FROM STA 300 TO 320 AND L29L NR 2 PIT. REPAIRED ANGLE AND OUTER SKIN, IAW DC-8 SRM 53-2-0 FS 1B AND 53-2-1.Oct 25, 1996 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9610001Clamp · looseWHILE CLIMBING THROUGH FL 28.0, PNEUMATIC DUCT RUPTURED IN FLIGHT. CABIN PRESSURIZATION CLIMBED TO 10,000 FT. AIRCRAFT RETURNED TO LIMA WITHOUT INCIDENT. DURING TROUBLESHOOTING, FOUND RT SIDE COLD AIR DUCT CLAMP DISCONNECTED AT BULKHEAD. RECONNECTED CLAMP,Oct 24, 1996 · N661AV · Doug DC863F · Air Distribution SystemSDR ABXA9600648Battery Rack · dischargedEMERGENCY EXIT LIGHTING FAILS TEST ON A-1 CHECK. REPLACED EMERGENCY LIGHTING BATTERY RACK ASSEMBLY, OPS CHECKED GOOD IAW DC-8 MM 33-50-0.Oct 17, 1996 · N815AX · Doug DC863F · Emergency LightingSDR ARWA9610046Generator · miswiredON TAXI OUT NR 2 GENERATOR FIELD RELAY TRIPPED. STRONG BURNING SMELL IN COCKPIT BEHIND ELECTRICAL CONTROL PANEL BULKHEAD. DISCONNECTED NR 2 GENERATOR CSD AND RETURNED TO BLOCK. NO FIRE NOTED. TROUBLESHOOTING REVEALED A WIRING PROBLEM AT NR 2 GENERATOR, CAUOct 8, 1996 · N441J · Doug DC863F · AC Generation SystemSDR ABXA9600639Prox Switch · defectiveAFTER GEAR RETRACTION, GREEN GEAR LIGHTS OUT. THE RED LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED ALONG WITH THE LEFT DOOR NOT LATCHED ON FLIGHT ENGINEER'S PANEL. COMPLIED WITH ALL ABNORMAL PROCEDURES AND LIGHTS REMAINED ILLUMINATED. REPLACED LEFT LANDING GEAOct 6, 1996 · N814AX · Doug DC863F · Landing Gear Position and WarningSDR ARWA9609033Clamp · looseDURING FLIGHT FROM SJU, COULD ONLY PRESSURIZE AIRCRAFT AT TO 5.0PSI DIFFERENTIAL, WITH ALL T.C.'S RUNNING AND OUTFLOW CLOSED. CABIN CONTINUED TO CLIMB TO F.L.16.0 AFTER LEVEL OFF AT F.L. 29.0. AIRCRAFT DIVERTED TO MIA WITHOUT INCIDENT. FOUND CONNECTOR CLAMPSep 28, 1996 · N441J · Doug DC863F · Cabin Compressor SystemSDR IXXA96158Engine · flamed outON CLIMB-OUT FROM BNA TO TOL, THE NR 1 ENGINE FLAMED OUT. THE IGNITORS WERE SELECTED FOR 'BOTH' AND A SUCCESSFUL RESTART WAS ACCOMPLISHED. THE AIRCRAFT CONTINUED TO TOL WITH NO ABNORMAL PROBLEMS. INSPECTION OF THE ENGINE AND FUEL SYSTEM REVEALED NO ABNORMALSep 24, 1996 · N784AL · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA9600629Battery Rack · dischargedEMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHT BATTERY RACK IAW DC-8 MM 33-50-1, OPS CHECKED GOOD.Sep 20, 1996 · N826AX · Doug DC863F · Emergency LightingSDR ARWA9610045Skin · crackedDURING C CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN L/H UPPER SIDE. REPIARED AREA I.A.W. DC8 SRM 52-2-0, FIG. 4, SH. 3. FORMED AND TREATED RE PAIR PARTS I.A.W. DC8 SRM 51-1-4, 52-4-1 AND 51-1-8. INSTALLED REPAIR PARTS I.A.W. DC8 SRM 51-1-17,Sep 12, 1996 · N661AV · Doug DC863F · Cargo/Baggage DoorsSDR ARWA9610044Channel · crackedDURING C CHECK INSPECTION, FOUND 4 IN. CRACK IN R/H MLG I/B DOOR EDGE, AFT LOWER SIDE. REPAIRED CHANNEL I.A.W. DC8 SRM 52-2-0, FIG. 2, SH. 3. FORMED AND TREATED DOUBLER I.A.W. DC8 SRM 51-1-4, 52-0-1, 51-1-8. INSTALLED DOUBLER AT MLG DOOR I.A.W. DC8 SRM 51-1-17Sep 12, 1996 · N661AV · Doug DC863F · Landing Gear DoorsSDR ARWA9610043Skin · crackedDURING C CHECK INSPECTION, FOUND 2 IN. AND 1 IN. CRACK IN LOWER FUSELAGE SKIN STA. 798 AT R/H SIDE OF FRAME, ALSO, CNTR SIDE. REPAIRED WEB I.A.W. DC8 SRM 53-2-0, FIG. 9B, SH. 3. FORMED AND TREATED DOUBLER I.A.W. DC8 SRM 53-8-3, FIG. 1, 51-1-8. INSTALLED DOUBLESep 12, 1996 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9610039Skin · crackedDURING C CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN L/H CNTR SECTION. REPAIRED CARGO DOOR PLATING I.A.W. DC8 SRM 52-2-0, FIG. 4. FORMED AND TREATED REPAIR PARTS I.A.W. DC8 SRM 51-1-4, 51-1-8. INSTALLED AT #3 PIT DOOR I.A.W. DC8 SRM 51-1-17, Sep 11, 1996 · N661AV · Doug DC863F · Cargo/Baggage DoorsSDR ARWA9610038Skin · crackedDURING C-CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN R/H CNTR SECTION. CRACKED AREA WAS REMOVED I.A.W. DC8 SRM 52-2-0, FIG. 4. FORMED AND TREATED DOUBLERS I.A.W. DC8 SRM 52-4-1, FIG. 2, 51-1-8. INSTALLED AT #3 PIT DOOR I.A.W. DC8 SRM 51-1-17,Sep 11, 1996 · N661AV · Doug DC863F · Cargo/Baggage DoorsSDR ARWA9610037Cover · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION IN AFT LOWER CARGO COMPARTMENT, INTERCOASTAL COVER AT L252 STA 1160. CORRODED PLATE SECTION WAS REMOVED, REPAIRED AREA IAW DC8 SRM 53-2-0, FIG 1D SH 3. FORMED AND TREATED DOUBLERS IAW DC8 SRM 53-4-1, FIG 51 Sep 10, 1996 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9610042Skin · crackedDURING C CHECK INSPECTION, FOUND CRACK IN INNER SKIN AFT OF FORWARD CARGO STA. 290 L36. REPAIRED I.A.W. DC8 SRM 53-2-0, FIG. 1D, SH. 3. DAMAGED SKIN WAS REMOVED. FORMED SKIN SECTION AND DOUBLER I.A.W. DC8 SRM 53-4-1, 51-1-4. TREATED AND INSTALLED REPAIR PARTS Sep 9, 1996 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9610040Skin · brokenDURING C CHECK INSPECTION, FOUND BROKEN OUTER SKIN LOWER SIDE AT #1 PIT DOOR. REPAIRED #1 PIT DOOR SKIN I.A.W. DC8 SRM 52-2-0, FIG. 2 SH. 3. INSTALLED DOUBLER I.A.W. DC8 SRM 52-4-1, 51-1-17, 51-1-21. TREATED AREA I.A.W. DC8 SRM 51-1-8. CF W/O 017402 N/R 0460.Sep 7, 1996 · N661AV · Doug DC863F · Cargo/Baggage DoorsSDR ARWA9610041Door · crackedDURING C CHECK INSPECTION, FOUND 2 IN. CRACKS IN OVERWING EMERGENCY EXIT DOOR LOWER AND UPPER CORNERS, R/H FORWARD SIDE AT MAIN CARGO COMPARTMENT. REPAIRED I.A.W. DC8 SRM 52-2-0, FIG. 2, SH. 3. FORMED DOUBLER I.A.W. DC8 DRM 52-7-1, FIG. 2. TREATED AND INSTALLESep 6, 1996 · N661AV · Doug DC863F · Emergency ExitsSDR ARWA9610036Frame · brokenDURING C-CHECK INSPECTION, FOUND BROKEN FRAME AT RT MLG WHEEL WELL INNER SECTION. REPAIRED SECTION AT RT MAIN GEAR IAW DC8 SRM 53-2-1, FIG 1B SH 3. TREATED AND INSTALLED ANGLE DOUBLER IAW DC8 SRM 51-1-8, 51-1-21, CF W/O 017402 N/R 0229.Sep 5, 1996 · N661AV · Doug DC863F · Fuselage Main, FrameSDR ARWA9610035Door · crackedDURING C-CHECK INSPECTION, FOUND 2 INCH CRACK ON RT MLG I/B DOOR SURFACE. REPAIRD AREA IAW DC-8 SRM 52-2-0 FIG 2 SH 3. FORMED AND TREATED DOUBLER IAW DC-8 SRM 52-6-1 PG 2; 51-1-5. INSTALLED AT RT MLG I/B DOOR IAW DC-8 SRM 51-1-17, 51-1-21, CF W/O 017404 N/RSep 5, 1996 · N661AV · Doug DC863F · Landing Gear DoorsSDR IXXA96130Structure · vibrationDURING APPROACH TO CLT, AIRCRAFT EXPERIENCED A SIGNIFICANT VIBRATION WITH FLAP 23 SELECTED. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROL SYSTEMS, LANDING GEAR SYSTEMS, WINGS, AND FUSELAGE WITH NO CAUSE FOUND. A SUBSEQUENT TEST FLIGHT WAS ACCOMPLOSHED WIAug 23, 1996 · N867BX · Doug DC863F · Aircraft StructuresSDR RRXA96084Frame · corrodedDURING C-CHECK, FOUND CORROSION ON FRAME UNDER NUTPLATES, AT Y=1120 AND LONGERON 36. REMOVED NUTPLATES AND CORROSION, FABRICATED FILLER AND DOUBLERS IAW DER APPROVED ENGINEERING SKETCH A98-R15, INSTALLED IAW DC-8 SRM 51-1-20D.Aug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96083Skin · damagedDURING C-CHECK, FOUND TEMPORARY REPAIR ON LT HORIZ STAB LEADING EDGE, O/B SECTION. REMOVED TEMPORARY REPAIR, FABRICATED INTERNAL AND EXTERNAL DOUBLERS AND STRAPS IAW DER APPROVED ENGINEERING SKETCH A98-R14, INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21.Aug 20, 1996 · N957R · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR RRXA96082Skin · corrodedDURING C-CHECK, FOUND LT UPPER HORIZ STAB LEADING EDGE HAD CORROSION IN 2 PLACES AT ATTACHMENT SCREWS, APPROX. XF=143 AND XF=153. REMOVED OLD REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER FROM .063 7075T-6. TREATED, PRIMED AND INSTALLED IAW DER APPRVED ENGINAug 20, 1996 · N957R · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR RRXA96081Longeron · corrodedDURING C-CHECK, FOUND CORROSION ON LONGERON 27R AT GROUND AIR CONDITION CONNECTOR PANEL DOME NUT AT Y=42. REMOVED DOME NUTS, REMOVED CORROSION AND FOUND CORROSION WAS BEYOND LIMITS. REMOVED AND REPLACED LONGERON 27R IAW DC-8 SRM 51-1-20D. INNER DOOR DOUBLEAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA96080Structure · corrodedDURING C-CHECK, FOUND FLOOR TO FRAME FITTING AT Y=920 UPPER WEB, HAD CORROSION INSIDE RT WHEEL WELL. CUT UPPER WEB, REMOVED CORROSION IAW DC-8 SRM 51-1-8, REMOVED Y=920 TRAP FITTING, REPAIRED WEB AND FLOOR BEAM IAW DER APPROVED ENGINEERING SKETCH A98-R07, MODAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, StructureSDR RRXA96079Skin · corrodedDURING C-CHECK, FOUND INTERNAL DOUBLER CORRODED AT Y=220 TO 265 AND LONGERONS 35L TO 35R, ALSO INNER SKIN CORRODED AND BULGED AT Y=224 BETWEEN LONGERONS 33R TO 34R. REMOVED CORRODED SKIN AND INNER DOUBLER, FABRICATED INTERNAL DOUBLER AND EXTERNAL SKIN IAW DERAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA96078Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BULGED AT Y=350, X=-19 AND Z=-59 FWD FUSELAGE. REMOVED FASTENERS ON A-PIT DOOR DOUBLER TO Y=330 AND TO LONGERON 28. CUT SKIN AT Y=389 AND PEELED UP. NO CORROSION FOUND, FABRICATED SKIN SPLICE DOUBLERS AND REPAIRED SKIN IAAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA96077Skin · corrodedDURING C-CHECK, FOUND RT WING LEADING EDGE UPPER ATTACHMENT DAMAGED AT FASTENERS APPROX XFS 20. REMOVED FASTENERS, REMOVED CORROSION, FABRICATED REPAIR DOUBLER FROM .190 7075T-6 MATERAIL IAW DER APPROVED ENGINEERING SKETCH A98R05 AND INSTALLED IAW DC-8 SRM 51Aug 20, 1996 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA96076Frame · corrodedDURING C-CHECK, FOUND CORROSION ON FRAME Y=1060, AT LONGERON 36 UNDER NUTPLATE AND 35 LEFT, Y=1040 AT LONGERON 33 AND 34 RIGHT, UNDER NUTPLATES. REMOVED NUTPLATES, REMOVED CORROSION, TREATED AND PRIMED IAW DC-8 SRM 51-1-8, FABRICATED FILLERS, DOUBLERS AND DRIAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96075Skin · crackedDURING C-CHECK, FOUND UPPER LEADING EDGE GOUGED AND CRACKED AT XRS 289. STOP DRILLED CRACK, FABRICATED DOUBLER FROM .063 7075T-6AL, IAW DER APPROVED ENGINEERING SKETCH A96-R01 AND INSTALLED IAW DC-8 SRM 51-1-20D, 21, 21D.Aug 20, 1996 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA96074Frame · corrosionDURING C-CHECK, FOUND CORROSION UNDER NUTPLATE ON FRAME AND FRAME SPLIT IN AFT LOWER COMPARTMENT, Y=1100 ABOVE LONGERON 34 RT. REMOVED CORROSION, CUT OUT DAMAGED AREA OF FRAME, FABRICATED FILLER DOUBLERS IAW DER APPROVED ENGINEERING SKETCH A98-R02 AND INSTALLAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96073Frame · misdrilledDURING C-CHECK, FOUND HOLE DRILLED IN RADIUS OF FRAME AT CUSP FITTING, RH Y=240. FORMED REPAIR ANGLE FROM 7075-0 MATERIAL AND HEAT TREATED TO T-6 CONDITION IAW DER APPROVED ENGINEERING SKETCH A98-R03. DRILLED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21.Aug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96072Frame · misdrilledDURING C-CHECK, FOUND 4 HOLES DRILLED IN FRAME, LT SIDE AT AFT LOWER CORNER OF CARGO DOOR. REMOVED FASTENERS IN REPAIR AREA, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH A98-R03.Aug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96071Frame · misdrilledDURING C-CHECK, FOUND 6 HOLES DRILLED IN FRAME, LT SIDE OF UPPER CARGO COMPARTMENT ABOVE CUSP, 9 AFT OF CARGO DOOR, Y=280. FABRICATED AND DRILLED REPAIR DOUBLER, HEAT TREATED AND AGED IAW DER APPROVED ENGINEERING SKETCH A98-R03. INSTALLED REPAIR IAW DC-8 SRMAug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96070Frame · misdrilledDURING C-CHECK, FOUND HOLE DRILLED IN FRAME INBD FLANGE, LT SIDE OF UPPER CARGO COMPARTMENT, Y=320, 3 ABOVE FLOOR. REMOVED FASTENERS, FABRICATED REPAIR ANGLE AND HEAT TREATED IAW DER APPROVED ENGINEERING SKETCH A98-R03 AND INSTALLED IAW DC-8 SRM 51-1-21.Aug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA96069Frame · misdrilledDURING C-CHECK, FOUND 2 HOLES DRILLED IN FRAME INBD FLANGE 3 AND 12 ABOVE FLOOR IN UPPER CARGO COMPARTMENT, Y=440, LT SIDE. FABRICATED REPAIR ANGLE IAW DER APPROVED ENGINEERING SKETCH A98-R03. DRILLED, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-20D.Aug 20, 1996 · N957R · Doug DC863F · Fuselage Main, FrameSDR ARWA9608004O-Ring · damagedINFLIGHT AT FL 350, HYDRAULIC QUANTITY SUDDENLY STARTED DESCENDING AND CONTINUED DESCENDING. ISOLATED HYDRAULIC SYSTEM. RETURNED TO MIAMI AND FOUND RUDDER SELECTOR VALVE PLUG LEAKING. REPLACED O-RING, NO LEAKS NOTED IAW DC-8 MM 29-00-00.Aug 14, 1996 · N441J · Doug DC863F · Rudder Control SystemSDR IXXA96123Uplatch · failedEN ROUTE FROM WRI-MDT, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED LIGHT ILLUMINATED. AFTER AN UNEVENTFUL LANDING, MAINTENANCE DETERMINED THE LEFT MAIN GEAR UPLATCH TO BE WORN AND AT FAULT. THE LEFT UPLATCH ASSEMBLY WAS REMOVED, REPLACED, AND OPEAug 6, 1996 · N786AL · Doug DC863F · Landing Gear Retraction/Extension SystemSDR IXXA96115Switch · failedON TAKEOFF OUT OF KRDL, GEAR NOT LATCH LIGHT CAME ON. GEAR CYCLED WITH NO CHANGE. AT TJSJ MAINTENANCE INSPECTED AIRCRAFT AND FOUND RIGHT GEAR UPLATCH TO BE BAD. SWITCH WAS REPLACED AND SYSTEM CHECKS NORMAL. (M)Jul 22, 1996 · N786AL · Doug DC863F · Landing Gear Position and WarningSDR ARWA9607001Switch · inoperativeON CLIMB-OUT FROM ATL, GEAR NOT LATCHED. LIGHT CAME ON, RECYCLED GEAR AND NOW GEAR AND DOOR LIGHT ON. DIVERTED TO MIAMI. TROUBLESHOT, FOUND RT MLG UPLATCH SWITCH BAD. REMOVED AND REPLACED SWITCH I.A.W. 32-30-00. OPS CHECKED NORMAL ON GEAR SWING, RETURN ACJul 21, 1996 · N441J · Doug DC863F · Landing Gear Position and WarningSDR IXXA96106Tire · failedON LANDING TSJU, THE NR 3 AND NR 8 TIRES BLEW, LOCAL TOWER CLOSED RUNWAY UNTIL THE A/C COULD BE REMOVED. THE NR 3 TIRE EXIBITED MULTIPLE FLAT SPOTS AND THE NR 8 TIRE HAD ONE FLAP SPOT. SUBSEQUENT DAMAGE OF THE NR 4 BRAKE LINE OCCURRED. MAINTENANCE REPLACED Jul 10, 1996 · N784AL · Doug DC863F · TireSDR IXXA96121Linkage · brokenEN ROUTE BETWEEN ATL AND TOL, CREW NOTED SPOILER UNLOCK INDICATION LIGHT ILLUMINATED WITH STANDBY SPOILER PUMP OFF. FLIGHT CONTINUED WITH AN UNEVENTFUL LANDING AT TOL. MAINTENANCE FOUND AND REPLACED A BROKEN LEFT INBOARD SPOILER CRANK/LINKAGE IAW THE DOUGLASJun 27, 1996 · N867BX · Doug DC863F · Drag Control SystemSDR IXXA9689Wiring Harness · brokenEN ROUTE MIA TO SJU, CARGO DOOR WARNING LIGHT ILLUMINATED ON DESCENT INTO SJU. FOLLOWING AN UNEVENTFUL LANDING, MX REPAIRED THE WIRING HARNESS OF THE CARGO DOOR WARNING SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. (M)Jun 17, 1996 · N786AL · Doug DC863F · Door Warning SystemSDR CKSA96059Firewire · damagedKMIA - FLT 75848 - SHUTDOWN NR 3 ENGINE AT 1132Z DUE TO FIREWARNING. FIRE WARNING STOPPED WHEN FUEL SHUTOFF. REPAIRED AND REROUTEDDAMAGED WIRE ON RIGHT SIDE LOOP CONNECTOR ON ENGINE. RAN ENGINE AT TAKEOFFPOWER. CHECKS GOOD ON GROUND. NO EVIDENCE OF FIRE FJun 14, 1996 · N811CK · Doug DC863F · Fire DetectionSDR ARWA9606069Plate · corrodedRT WING, INNER WING TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 50.000 THROUGH XRS 74.869. REPAIRED WING TOP PANEL IAW DC-8 SRM 57-2-1, FIG 10, SHEET 2. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-17 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Wing, Plate/SkinSDR ARWA9606068Panel · corrodedRT WING, INNER WING TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 22.750 THROUGH XRS 50.000. REPAIRED WING TOP PANEL IAW DC-8 SRM 57-2-1, FIG 15. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-17 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Wing, Plate/SkinSDR ARWA9606067Plate · corrodedRIGHT WING INNER TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 22.750 TO XRS 50.000. REPAIRED AND TREATED AREA PER DC-8 SRM 57-2-1 AND 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Wing, Plate/Skin
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