N814AX

Part: SPAR — CRACKED (RT WING) · airframe 87,972 hrs · 27,791 cycles

RIGHT WING INTERNAL FUEL TANK AT STA XRS 172 LOWER CENTER SPAR AND WEB HAD CRACK AND CORROSION AT SPAR CAP CRACK. CUT OUT DAMAGED AREA OF CENTER SPAR AND WEB IAW REA D857-49982MR. FABRICATED REPAIR PARTS IAW DAC DWG'S 5613912, 3642213, 3644709 AND SRO8570015. REINSTALLED STRUCTURE IAW DC-8 SRM. REPAIRED IAW REA D857-49982MR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 87,972 hrs · 27,791 cycles

INSPECTION DEVIATION PER ABX REA D853-50097MR, REPAIR TRIPLER, FUSELAGE SKIN, FS 273-280, LONGERON 19 LEFT - 20 LEFT. REPAIRED AREA IAW ABX REA D853-50097MR. COI GENERATED FOR MAINTENANCE TRACKING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 87,972 hrs · 27,791 cycles

AFT CARGO LONGERON 36, BLEEDING CORROSION FROM BOTH SIDES FROM STA 1080 - 1120. REPAIRED AREA IAW REA D853-49986MR.

Part: SKIN — GOUGED (RT WING) · airframe 87,972 hrs · 27,791 cycles

RIGHT WHEEL INBOARD AILERON, 3 RIVETS MISSING HEADS OR PART OF HEAD AND OPEN HOLE AT APPROXIMATELY XA 562, LOWER LEADING EDGE. REMOVED AND REPLACED DAMAGED SKIN SECTION AND DOUBLER IAW REA D857-49983MR.

Part: CRANK ASSY — BROKEN (SPOILERS) · airframe 87,746 hrs · 27,650 cycles

SPOILER EXTEND LIGHT STAYED ON AFTER RETRACTION. NORMAL SPOILER HYDRAULIC PRESSURE INDICATION. MAINTENANCE FOUND RIGHT WING INBOARD TWO SPOILER DRIVE ARMS THAT ATTACH TO SPOILER CABLES BROKEN. REPLACED REAR SPAR ACTUATOR CRANK ASSEMBLIES ON INBOARD SPOILER PANEL FOR THE RIGHT WING IAW DC-8 MM 27-61-01-2. AFTER REPLACEMENT OF RIGHT HAND INBOARD SPOILER CRANKS, SPOILER DEPLOYED SWITCH INSTALLED IN CORRECT POSITION. OPS CHECKED GOOD IAW DC-8 MM CHAPTER 27-63-01-02-0001, PARA 3A.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 87,508 hrs · 27,491 cycles

FLIGHT ENGINEER'S SEAT VERTICAL HOLD WOULD NOT HOLD WHILE SEAT WAS FACING FORWARD. FELL 3 TIMES DURING TAKEOFF AND INITIAL CLIMB. REPLACED SYSTEMS ENGINEER SEAT PER ABX DC8 AMM 25-11-06-2-001. LUBED AND OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,860 hrs · 27,054 cycles

L2 DOOR CUTOUT LOWER FORWARD CORNER HAD REPAIR. UNIT DOES NOT CONFORM TO SRM OR JOB CARD NEA 53100104-002/634. REPAIRED L2 LOWER FORWARD CORNER IAW REA D853-44023MR AND DC-8 SRM 53-2-0.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 86,860 hrs · 27,054 cycles

MAIN CARGO DOOR ACTUATOR ATTACH FITTING WAS SEPARATED AT WELD. REMOVED CORROSION FROM FITTING AND BLENDED FITTING IAW DC-8 SRM 51-1-8, WELDED FITTING IAW AM526856, INSTALLED FITTING IAW DC-8 SRM 51-3-0 AND 51-1-21. REINSTALLED ACTUATOR IAW DC-8 MM 52-36-03. OPS CHECKED GOOD IAW DC-8 MM 52-36-03.

Part: SKIN — CORRODED (RT WING) · airframe 86,860 hrs · 27,054 cycles

RIGHT FORWARD WHEEL WELL HAD CORROSION ON CENTER WING SKIN AFT OF OUTBOARD BLOWOUT PANEL. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER, REPAIR ANGLE AND SPLICE IAW DC-8 SRM 51-1-8 AND REA D857-44039MR.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,860 hrs · 27,054 cycles

AFT LOWER CARGO LONGERON 34 RIGHT HAD CORROSION AT STA 1180 - 1200. REMOVED CORROSION, BEYOND LIMITS. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D. FABRICATED REPAIR STRAP IAW REA D853-44041MR. PRIMED STRAP IAW DC-8 SRM 51-1-8. INSTALLED STRAP IAW DC-8 SRM 51-1-20D AND REA D853-44041MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,860 hrs · 27,054 cycles

L1 DOOR SHOWED CRACK LOWER AFT CORNER. REMOVED DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 51-1-20D, AND REA D853-44030MR.

Part: PRESSURE SWITCH — FAULTY (NR 3 & 4 ENGINE) · airframe 86,850 hrs · 27,044 cycles

NR 4 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK BUT LIGHT STAYED ON. SECURED THE NR 4 ENGINE. ALSO THE NR 3 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK AND LIGHT WENT OUT, BUT ILLUMINATED INTERMITTENTLY. AIRCRAFT DIVERTED TO LOUISVILLE. REPLACED THE NR 4 AND NR 3 ENGINE OIL LOW PRESSURE SWITCHES IAW DC-8 MM 79-32-02-2. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 4) · airframe 86,808 hrs · 27,011 cycles

NR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON ACCOMPANIED BY AN OIL PRESSURE FLUCTUATION AND QUANTITY DECREASING. ENGINE WAS SECURED AND OIL PRESSURE WAS BELOW 5 PSI WITH ENGINE WINDMILLING AT 30 PERCENT N2 FOR REMAINED OF FLIGHT. REPLACED THE NR 4 ENGINE. RUN UP/TRIM CHECK IAW DC-8 A/B.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,794 hrs · 27,003 cycles

EMERGENCY LIGHTS WERE VERY DIM. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC-8 AMM 33-50-01-2.

Part: YOKE — JAMMED (COCKPIT) · airframe 86,051 hrs · 26,556 cycles

ELEVATOR CONTROL YOKE JAMMED ON FINAL APPROACH. YOKE WOULD ONLY GO TO THE NEUTRAL POSITION ON THE ELEVATOR POSITION INDICATOR. VERIFIED ELEVATOR CONTROL COLUMN JAM IN NOSE DOWN POSITION. INSPECTION REVEALED ELEVATOR RIGGING FIXTURE LINK CONTACTED LOWER ELEVATOR CONTROL COLUMN RIGHT SIDE. FOUND RIGGING FIXTURE LINK RETRACT SPRING INSTALLED INCORRECTLY. REMOVED SPRING AND INSTALLED CORRECTLY TO ENSURE TENSION FOR LINK RETRACTION. ELEVATOR OPS CHECKED GOOD IAW DC-8 AMM 27-30-00-0-0006.

Part: FITTING — CRACKED (LT WING) · airframe 85,679 hrs · 26,361 cycles

THE LEFT WING LOWER TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-5-2.

Part: STRUCTURE — LEAKING (RT WING) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

A FASTENER WAS FOUND TO BE LEAKING FUEL AT STA 795. MAINTENANCE REPAIRED THE AREA IAW REA D857-40312MR AND DC-8 SRM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

CORROSION WAS FOUND AT THE FORWARD AIR-CONDITIONING PRESSURE COMPARTMENT AT THE RIGHT CUSP FITTING. CORROSION WAS FOUND UNDER AND AROUND THE NUT PLATES. MAINTENANCE INSTALLED A NEW FITTING IAW DC-8 SRM 51-1-20 AND 51-3-0.

Part: FITTING — CRACKED (RT WING) · airframe 85,679 hrs · 26,361 cycles

THE RIGHT WING LOWER FORWARD TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-2-7.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

CORROSION WAS FOUND ON END FITTING AT FUSELAGE STATION 8-28 LONGERON 27R IN THE FORWARD AIR-CONDITIONING COMPARTMENT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8, 51-2-0 AND DAC DRAWING 4711722.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

CORROSION WAS FOUND ON FITTING AT THE LEFT MLG WHEEL WELL AT FUSELAGE STATION 857. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-40267-MR AND DC-8 SRM 53-2-0.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

CORROSION WAS FOUND AT THE FORWARD LOWER CARGO PIT BETWEEN STA 280 AND 300, LONGERON 28L. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8 AND DAC DRAWING 9754931.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

CORROSION WAS FOUND ON LONGERON 33L BETWEEN FUSELAGE STA 320 - 340 IN LOWER CARGO PIT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,679 hrs · 26,361 cycles

THE FUSELAGE EXTERIOR SKIN AT STATION 1750 LONGERON 15R-16R WAS FOUND TO BE CRACKED BETWEEN FASTENERS. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,679 hrs · 26,361 cycles

THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE CRACKED AT STA 1720 LONGERON 17-18R. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1.

Part: SEAT TRACK — CORRODED (MAIN CARGO BAY) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

THE MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 30, STATION 1723 - 1746 WAS CORRODED. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK IAW DC-8 SRM 51-3-0 AND ZANTOP DRAWING 86302.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,679 hrs · 26,361 cycles

A CRACK 4.5 INCH LONG WAS FOUND ON THE NOSE WHEEL WELL AFT DOOR FORWARD HINGE FRAME. MAINTENANCE REPAIRED THE CRACK IAW REA D853-40280MR.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

THE RIGHT MLG WHEEL WELL HORIZONTAL PRESSURE WEB WAS FOUND TO BE CORRODED. A STIFFENER WAS FOUND TO BE BULGING AT STA 902 RBL 56 THROUGH 65. MAINTENANCE REPAIRED THE AREA IAW REA D853-40284, DAC DRAWING 5645332 AND DC-8 SRM 51-1-8.

Part: STRUCTURE — LEAKING (LT WING) · airframe 85,679 hrs · 26,361 cycles

SPAR CAP LEAKED FUEL JUST INBOARD OF NR 1 PYLON AT S - 64 DOUBLER. REMOVED DOUBLER AND TRIPLER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ABX REA D857-40311MR AND DAC DWG SRO8570013.

Part: STRUCTURE — LEAKING (LT WING) · airframe 85,679 hrs · 26,361 cycles

THE SPAR CAP WAS FOUND TO BE LEAKING FUEL JUST INBOARD OF THE NR 1 PYLON AT WS 444. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D857-40311MR.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 85,679 hrs · 26,361 cycles

THE SEAT TRACK AT FUSELAGE STATION 920 HAD A CORRODED FASTENER HOLE. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK AT STATION 870 - 940 IAW DC-8 SRM 51-3-0 AND 51-1-21.

Part: WATER HEATER — MALFUNCTIONED (GALLEY)

ELECTRICAL BURNING SMELL WAS COMING FROM THE HOT WATER MAKER SHORTLY AFTER IT WAS TURNED ON. WATER WAS FULL, AFTER TURNING IT OFF THE SMELL WENT AWAY. REPLACED THE HOT CUP BRACKET AND HOT CUP IAW DC8 MM. OPS CHECKED GOOD.

Part: UP LATCH SWITCH — OUT OF ADJUST (LANDING GEAR)

IN CRUISE FLIGHT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED LANDING GEAR. LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. SLOW FLEW AIRCRAFT AT 220 KNOTS. ADJUSTED LEFT GEAR DOOR UPLATCH IAW DC8 MM 32-31-4.

Part: DOOR SPRING — OUT OF ADJUST (LT MLG DOOR)

LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING CRUISE FLIGHT WITH LEFT MAIN LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. RECYCLED GEAR, NO CHANGE. ADJUSTED LEFT MAIN LANDING GEAR PROXIMITY SWITCH TARGET STOP. REPLACED LEFT GEAR DOOR SPRING IAW DC8 MM 32-31-5. PERFORMED TEST IAW DC8 MM 32-6, OPS CHECKED GOOD.

Part: ANGLE — CRACKED (BS 930-935)

KEEL BEAM AREA AT APPROXIMATELY STATION 930 TO 935 RIGHT SIDE, THE KEEL ANGLE HAS A 5 INCH CRACK. REPAIRED IAW ABX REA D853-22758 AND DC8 SRM 52-2-0.

Part: SKIN — CRACKED (LT WING)

LEFT WING LEADING EDGE BETWEEN PYLONS INTERNAL UPPER DOUBLER IS CRACKED ABOVE SLOT ACTUATOR. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: DOUBLER — CRACKED (BS 450)

FINGER DOUBLER CRACKED AT STATION 450, LONGERON 31L. CORROSION OUT OF LIMITS. REPAIRED IAW ABX REA D853-22748.

Part: SHEAR TIE — CORRODED (BS 1000)

FORWARD SHEAR TIE AT STATION 1000 HAS HEAVY CORROSION AT LONGERON 33R. REPAIRED IAW DC8 SRM 53-20-0 AND DWG 9755888.

Part: FITTING — CORROSION (BS 920)

CORRODED VERTICAL FITTING RBL 65 STATION 920. REPAIRED IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 25)

LONGERON 31R AT STATION 25 HAS HEAVY CORROSION. REPAIRED IAW DC8 SRM 51-1-20.

Part: SHEAR TIE — CRACKED (BS 1160)

SHEAR TIE CRACKED, STATION 1160 BETWEEN LONGERON 34R TO 35R. REPAIRED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1150)

SHEAR TIE AT STATION 1150 BETWEEN LONGERON 30R AND 33R HAS 6 INCH CRACK. REPAIRED IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 628.75)

RIGHT WING LEADING EDGE RIB AT STA XFS 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 791.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 354)

LEFT WING LEADING EDGE RIB CRACKED AT WS 354 UPPER AFT. REPAIRED IAW DC8 SRM 51-1-20D.

Part: STRINGER — CORRODED (BS 1460)

STRINGERS 34R AND 34L AT STATION 1460 CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-20.

Part: RIB — CRACKED (WS 822.5)

RIGHT WING LEADING EDGE RIB AT STA XFS 822.50 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 747.5)

RIGHT WING LEADING EDGE RIB AT STA XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: SPAR — CRACKED (RT MLG WW)

RIGHT WHEEL WELL AT FWD LOWER OUTBOARD END, REAR SPAR LOWER CHORD HAS NUMEROUS CRACKS. REPAIRED IAW ABX REA D857-22747 MR.

Part: DOUBLER — CORRODED (BS 105)

INTERNAL FINGER DOUBLER CORRODED AND CRACKED AT STATION 105, LONGERON 31R. REPAIRED IAW ABX REA D853-22748 MR.

Part: CUSP — CORRODED (BS 460-560)

MAIN CABIN LOWER CUSP CORRODED BEYOND LIMITS AT STATION 460 TO STATION 560 RIGHT SIDE. REPAIRED IAW DC8 SRM 53-2-5.

Part: SPLICE — CRACKED (BS 440-460)

LONGERON 31L SPLICE FITTING CRACKED BETWEEN STATION 440 TO 460. REPAIRED IAW DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 20-25)

FINGER DOUBLER HAS HEAVY CORROSION AT FS 20 TO 25, STRINGER 31R. REPAIRED IAW DC8 SRM 53-1-0 AND 51-1-20.

Part: FITTING — CRACKED (WS 23)

LEFT WHEEL WELL FITTING CRACKED AT STATION XCW 23 BELOW PRESSURE PANEL. REPAIRED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (BS 1260-1280)

STATION 1260 TO 1280 STRINGER 36 SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D.

Part: BULKHEAD WEB — CRACKED (BS 857)

FUSELAGE STA 857 LBL 16 THE MAIN LANDING GEAR FORWARD BULKHEAD WEB IS CRACKED AT THE ADF ANTENNA LEAD ACCESS PANEL. REPAIRED IAW DC8 SRM 51-3-0.

Part: FITTING — BROKEN (LT WING)

LEADING EDGE OUTBOARD INTERNAL STRUCTURE FITTING BROKEN BETWEEN NR 1 AND NR 2 PYLON. REPAIRED IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (BS 540)

FUSELAGE TO FRAME 540 FORMER BETWEEN LONG 35R-36R IS CRACKED. REPAIRED IAW DC8 SRM 53-2-0.

Part: WEB — CRACKED (WS 510-520)

WEB CRACKED AT STATION 510 - 520 RIGHT, JUST AFT OF SERVICE DOOR AT FLOOR LEVEL. REPLACED WEB IAW DC8 SRM 51-1-20 AND DOUG DWG 9755569.

Part: RIB — CRACKED (WS 728.25)

RIGHT WING LEADING EDGE RIB AT STA XFS 728.25 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACKED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 785)

RIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 778.75)

RIGHT WING LEADING EDGE RIB AT STATION 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.

Part: FITTING — CRACKED (BS 1220)

FLOORBEAM END FITTING IS CRACKED AT STA 1220 AND STR 21R. REPAIRED IAW DWG 3754946 AND DC8 SRM 51-1-20.

Part: FITTING — CRACKED (BS 1040-1060)

STATION 1040 - 1060 STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 635)

RIGHT WING LEADING EDGE RIB AT STA XFS 635.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 816.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 816.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 616.25)

RIGHT WING LEADING EDGE RIB AT STA XFS 616.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-2-0 AND DWG K 05056.

Part: ANGLE — CRACKED (BS 25)

COCKPIT SUB FLOOR AT STATION -25 RBL 8, INTERCOSTAL IS CRACKED AT FWD END (FLOOR SUPPORT ANGLE). REPAIRED IAW DWG 5613327 AND DC8 SRM 51-1-21.

Part: TIE FITTING — CRACKED (BS 680)

FLOORBEAM STA 680 RBL-24 TO WING BOX TIE FITTING CRACKED. REPAIRED IAW DWG 4645517 AND DC8 SRM 51-1-8.

Part: INTERCOSTAL — CRACKED (BS 980)

INTERCOSTAL CRACKED AT RBL 40 BETWEEN STATION 980 AND 1000. REPAIRED IAW DC8 SRM 53-2-0.

Part: INTERCOSTAL — CRACKED (BS 520/540)

INTERCOSTAL ATTACH ANGLE CRACKED AT STATION 520 AND STATION 540, RBL 10. REPAIRED IAW SRM 51-1-21, SRM 53-2-0, AND SRM 51-1-20.

Part: RIB — CRACKED (WS 697)

RIGHT WING LEADING EDGE RIB CRACKED AT STA XFS 697. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506.

Part: TIE FITTING — CRACKED (BS 660)

FORWARD ACCESSORY COMPARTMENT STA 660 LEFT FRAME TO LONGERON 36, TIE FITTING IS CRACKED. REPAIRED IAW DOUGLAS DWG 3750497 AND DC8 SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 250.089)

RIGHT WING LEADING EDGE STA XS 250.089 THE OUTBOARD AFT VERTICAL STIFFENER FOR THE INBOARD SLOT IS CRACKED AT THE LOWER END. REPAIRED IAW DWG 9753293 AND DC8 SRM 51-3-0.

Part: DOUBLER — CRACKED (WS 597-603)

RIGHT WING LEADING EDGE SKIN INTERNAL DOUBLER BETWEEN STA XFS 597 AND XFS 603 IS CRACKED AT THE TAI EXHAUST HOLES. REPAIRED IAW DWG 5769600 AND DC8 SRM 51-1-21.

Part: RIB — CRACKED (WS 220.0)

AT XFS 220.0, NR 2 STUB WING RIB (UPPER) IS CRACKED. REPAIRED IAW DWG K05056.

Part: SUPPORT — CRACKED (NR 2 STUB WING)

NR 2 STUB WING INBOARD SUPPORT LEG CRACKED. REPAIRED IAW DWG 5769859 AND SRM 51-1-29.

Part: RIB — CRACKED (WS 270)

NR 3 STUB WING RIB IS CRACKED AT STA 270 (UPPER RIB). REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 330)

RIGHT WING LEADING EDGE INTERNAL DOUBLER AT STA XFS 330 IS CRACKED. REPAIRED IAW DWG 5769589 AND DC8 SRM 51-1-8.

Part: INTERCOSTAL — CRACKED (BS 520)

STATION 520 RBL 10 ON CEILING INTERCOSTAL ATTACH ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 53-7-7 AND 51-1-21D.

Part: RIB — CRACKED (LT WING)

LEFT WING LEADING EDGE BETWEEN THE NR 1 AND NR 2 PYLONS HAS 3 UPPER RIBS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 245)

NR 2 STUB WING LOWER RIB CRACKED AT XFS 245.0. REPAIRED IAW DWG K05056-7005 AND DC8 SRM 51-1-21D.

Part: INTERCOSTAL — CRACKED (BS 400)

INTERCOSTAL UPPER FLANGE CRACKED AT LONGERON 33R JUST AFT OF FUSE STA 400. REPAIRED IAW DWG 5750726 AND DC8 SRM 51-1-21.

Part: RIB — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB UPPER ARM CRACKED 7TH RIB INBOARD FROM OUTBOARD EDGE OF OUTBOARD SLOT. REPAIRED IAW SRM 57-20 AND DWG K05056.

Part: RIB — CRACKED (WS 647.5)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 647.5. REPAIRED IAW DWG K 05056 AND DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1746)

LONGERON 32L CORRODED BEYOND LIMITS AT STATION 1746 TO 1756. REPAIRED IAW DC8 SRM 53-22.

Part: LONGERON — CRACKED (BS 860)

LONGERON 24L AT STATION 860 HAS CRACK. REPAIRED IAW SRM 53-2-2.

Part: RIB — CRACKED (WS 772.5)

LEFT WING LEADING EDGE RIB AT STATION XFS 7725 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 822.5)

RIGHT WING LEADING EDGE RIB AT STATION XFS 822.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 862.5)

LEFT WING LEADING EDGE RIB AT STATION XFS 826.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 772.5)

RIGHT WING LEADING EDGE RIB AT STATION XFS 772.50 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0, 51-1-8 AND 51-1-21.

Part: RIB — CRACKED (WS 722.5)

RIGHT WING LEADING EDGE RIB AT STATION XFS 722.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 735)

RIGHT WING LEADING EDGE RIB AT STATION XFS 735.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 766.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 766.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 820.25)

LEFT WING LEADING EDGE RIB AT STATION XFS 820.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 828.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 828.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 741.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 272.5)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END AT XFS 272.5. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.

Part: RIB — CRACKED (WS 610)

RIGHT WING LEADING EDGE RIB AT STATION XFS 610.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0, 51-1-8 AND 51-1-21.

Part: LONGERON — CRACKED (BS 960)

LONGERON 24 HAS A CRACK EXTENDING UNDER VERTICAL FITTING ON TORQUE BOX, RIGHT WHEEL WELL AT STATION 960. REPAIRED IAW SRM 53-2-2, 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 728.75)

LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 728.75. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506.

Part: RIB — CRACKED (WS 585)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 585. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 622.25)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 622.25. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 741.25)

LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 741.25. REPAIRED IAW ABX DRAWING K0506 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 660)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 660. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 760)

RIGHT WING LEADING EDGE RIB CRACKED AT STA XFS 760. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K0506.

Part: RIB — CRACKED (WS 814)

LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 814. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506.

Part: RIB — CRACKED (WS 772)

RIGHT WING LEADING EDGE RIB AT XFS 772 CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 201.25)

RIGHT WING LEADING EDGE RIB CRACKED AT STA 201.25. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506.

Part: RIB — CRACKED (WS 410.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 410.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 454.976)

RIGHT WING LEADING EDGE RIB AT STATION XFS 454.976 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-31-1.

Part: LONGERON — CRACKED (BS 946)

LONGERON 24L STATION 946 HAS A CRACK EXTENDING UNDER VERTICAL FITTING. REPAIRED IAW DC8 SRM 53-2-2.

Part: ANGLE — CRACKED (RT WING)

RIGHT WING INBOARD LEADING EDGE AT THE WING ROOT UPPER AFT CORNER, THE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DWG 5613901 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (LT WING)

LEFT WING LEADING EDGE INBOARD END, UPPER CORNER OF THE AFT LEADING EDGE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DWG 5613901 AND DC8 SRM 51-1-8.

Part: FITTING — CORRODED (BS 960-980)

HORIZONTAL FITTING CORRODED AT LBL 48 BETWEEN FUSELAGE STATION 980 AND 960. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-21.

Part: FRAME — CORRODED (BS 902)

BULGING CORROSION AND POPPED RIVETS RBL 64 STATION 902. REPAIRED IAW DWG 5645332 AND DC8 SRM 53-2-0.

Part: RIB — CRACKED (WS 810)

RIGHT WING LEADING EDGE RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 703.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 703.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 691.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 691.25 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG 05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 622.5)

RIGHT WING LEADING EDGE RIB AT STA XFS 622.50 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (LT WING)

LEFT LEADING EDGE SECTION BETWEEN PYLONS, LOWER LEADING EDGE RIB JUST INBOARD OF SLOT ACTUATOR IS CRACKED AT THE AFT END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-11.

Part: RIB — CRACKED (WS 578.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 578.75 CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 828.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 828.75 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 566.25)

RIGHT WING LEADING EDGE RIB AT STATION XFS 566.25 CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 835)

RIGHT WING LEADING EDGE RIB CRACKED AT UPPER END STATION XFS 835.0. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 603.75)

RIGHT WING LEADING EDGE RIB AT STA XFS 603.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.

Part: RIB — CRACKED (WS 697.5)

RIGHT WING LEADING EDGE RIB AT STATION XFS 697.5 CRACKED AT UPPER AFT END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: FITTING — CRACKED (BS 440-460)

STATION 440 TO 460 STRINGER 33R SPLICE FITTING IS CRACKED AT FWD END. REPAIRED IAW DC8 SRM 51-1-21D.

Part: SPLICE — CRACKED (BS 620)

STATION 620 BETWEEN STRINGERS 35R AND 35L FRAME SPLICE HAS 8 INCH CRACK. REPAIRED IAW DC8 SRM 51-1-20.

Part: FITTING — CRACKED (WS 620)

STATION 610 TO 620 STRINGER 31L SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-11 AND 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 340)

INTERCOASTAL JUST AFT OF MAIN DECK FLOORBEAM STATION 340 LBL10 CRACKED. REPAIRED IAW DC8 SRM 53-20 AND 51-1-20D.

Part: FITTING — CRACKED (BS 460-480)

STATION 460 TO 480 STRINGER 35R SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4613574.

Part: SPAR — CORRODED (WS 555)

RIGHT WING REAR SPAR UPPER CHORD AT STATION XRS 555 HAS EXFOLIATION CORROSION. REPAIRED IAW ABX REA D857-22332.

Part: RIB — CRACKED (WS 778.75)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 778.75. REPAIRED IAW ABX DWG K05056 AND DC8 SRM 51-1-20D.

Part: RIB — CRACKED (WS 853.75)

RIGHT WING LEADING EDGE RIB AT STATION 853.75 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: CIRCUIT BREAKER — TRIPPED (NR 2 LORAN SYST)

DURING CRUISE, NR 2 LRN CIRCUIT BREAKER OPENED, ACCOMPANIED BY SMOKE ODOR. OPERATED SYSTEMS, COULD NOT DUPLICATE DISCREPANCY. NO SMOKE ODOR NOTED. OPS CHECKED GOOD IAW DC8 SMM 34-60-00.

Part: RIB — CRACKED (WS 591.25)

RIGHT WING LEADING EDGE AT STATION XFS 591.25 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.

Part: TAB — DELAMINATED (RUDDER)

RUDDER TAB FOUND TO BE DELAMINATED, MID SURFACE, BOTH SIDES 4 BY 6. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: ENGINE — FAILED (NR 4)

NR 4 ENGINE OIL PRESSURE LIGHT ILLUMINATED AT CRUISE, FL 330. QUANTITY WENT TO ZERO, TEMPERATURE WENT OFF SCALE HIGH. PERFORMED ENGINE SECURING. REPLACED NR 4 ENGINE IAW J CARD 7002.

Part: PROX SWITCH — DEFECTIVE (LT MLG)

AFTER 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 GEAR DOOR PROXIMITY SWITCH IAW DC-8 SUPPLEMENTAL MM 32-60-00. VISUAL INSPECTION WAS GOOD.

Part: TQ TUBE BOLT — LOOSE (LT MLG DOOR)

LEFT GEAR DOOR NOT LATCHED IN-FLIGHT AND RED GEAR UNSAFE LIGHT ON. RECYCLED GEAR TWICE. LIGHT FOR LEFT GEAR DOOR WENT OUT THEN BACK ON. PUT GEAR DOWN. FOUND THROUGH-BOLT AT TORQUE TUBE DRUM LOOSE. PERFORMED TEST I/A/W DC-8 M.A.B. 32-6, DATED 03-22-91. LATCH TEST WAS GOOD, RE-ASSEMBLED CABLE AND TESTED. OPS CHECKED GOOD.

Part: BOLT — MISSING (LT MLG)

DURING CLIMB, RETRACTED LANDING GEAR HANDLE AND GEAR UNSAFE LIGHT REMAINED ON. CHECKED LANDING GEAR AND DOOR LATCH POSITION, LEFT GEAR DOOR HAD AN UNLATCHED INDICATION. RECYCLED LANDING GEAR AND THE UNSAFE LIGHT REMAINED ON, LANDING GEAR WAS EXTENDED AND INDICATED DOWN AND LOCKED. INSPECTED LEFT MAIN GEAR AND FOUND THE FORWARD ATTACH BOLT AND NUT FOR THE BOGIE TRIM CYLINDER MISSING. INSTALLED FORWARD ATTACH BOLT AND NUT FOR THE BOGIE TRIM CYLINDER I/A/W DC8 MM CHAPTER 32. COMPLETED LANDING GEAR RETRACTION CHECK AND OPS CHECK WAS GOOD.

Part: BRAKE — LEAKING (NR 8)

NR 8 BRAKE ASSEMBLY HAD MINOR FIRE ON ARRIVAL. EXTINGUISHED FIRE ON NR 8 BRAKE ASSEMBLY. FIRE WAS ATTRIBUTED TO HYDRAULIC FLUID LEAK ON BRAKE ASSEMBLY. REPLACED NR 8 BRAKE ASSEMBLY AND MAIN WHEEL ASSEMBLY.

Part: DUMP VALVE — STUCK OPEN (NR 1 ALT)

AFTER 5,000 FT, 2.5 PSID, MAIN CARGO DOOR WRN LIGHT ILLUMINATED. LOCKS WERE ENGAGED, MORE WIND NOISE THAN NORMAL. WHEN SELECTED, DUMP CHUTE IND WAS MIDWAY BETWEEN DRAIN AND DOWN. MANUALLY CRANKED CHUTE DOWN; DUMPED APPROX 14,100 LBS. FOUND FUEL DUMPING OUT OF LT CHUTE WHICH WAS UP AND LOCKED. CREW HAD TO TRANSFER ALL FUEL FROM LT WING TO STOP FUEL DUMP. INSPECTED DOOR SEAL, LOCKS, HINGES, ACTUATORS, SWITCHES AND WARNING CIRCUIT. GROUND RAN, AND PRESS TO 4 PSI, NO LEAKS NOTED. CYCLED CARGO DOOR SEVERAL TIMES, OPS CHECKED GOOD IAW DC 8 MM. FOUND SEALANT IN NR 1 ALT DUMP FLAPPER VALVE. REMOVED SEALANT, CLEANED AREA, REFUELED, AND LEAK CHECKED.

Part: ENGINE — FAILED (NR 2)

ON CLIMB-OUT OF ILN, NR 2 EPR DROPPED 1.75 TO 1.40. ALL OTHER ENGINE INDICATIONS DROPPED AT THE SAME TIME, ACCOMPANIED BY AN ENGINE VIBRATION. SHUT DOWN NR 2 ENGINE. AIRCRAFT CONTINUED TO ATL AND LANDED WITHOUT ANY FURTHER PROBLEMS. INSPECTED ENGINE ON GROUND AND NOTED TURBINE SECTION DAMAGE. INSPECTED, PREPARED, AND THREE-ENGINE FERRIED AIRCRAFT TO ILN. REMOVED AND REPLACED NR 2 ENGINE IAW DC 8 MM CHAPTER 72.