N842AX

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 55,767 hrs · 26,186 cycles

EMERGENCY EXIT LIGHTS STILL DIM AND EMERGENCY HORIZONTAL GYRO LIGHTS DON'T WORK. GYRO FLAGGED WITH BATTERY POWER ONLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC8 MM. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD. REMOVED AND REPLACED STANDBY HORIZON POWER SUPPLY IAW DC8 MM 34-28-00. OPS CHECKED GOOD, P/N: 501-1228-04, S/N: 3998.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,767 hrs · 26,186 cycles

EMERGENCY EXIT LIGHTS (UNDER GLARESHIELD, OVERHEAD AND CLOSET LIGHTS) VERY DIM. OPS CHECKED ALL LIGHTS, ALL OPS CHECKED GOOD AT THIS TIME IAW DC8 MM.

Part: WINDOW — STICKING (COCKPIT) · airframe 55,144 hrs · 25,591 cycles

FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REPLACED FIRST OFFICER'S SLIDING WINDOW IAW DC8 56-10-0.

Part: SPRING — BROKEN (COCKPIT WINDOW) · airframe 55,115 hrs · 25,568 cycles

DURING MAINTENANCE, FOUND FIRST OFFICER'S WINDOW WAS STUCK. REPLACED SPRING, OPS CHECKED WINDOW. WINDOW DID NOT STICK. PRESSURIZED AIRCRAFT TO 5 PSI DIFF. CHECKED WINDOW AFTER DEPRESSURIZATION. OPENED AND CLOSED NORMALLY.

Part: SPAR CAP — CRACKED (FUSELAGE) · airframe 54,920 hrs · 25,413 cycles

STA 857 LEFT BUTTLINE 24, SPAR CAP CRACKED. REPAIRED SPAR CAP IAW DC-8 SRM 53-2-5, 51-1-8, 51-1-21, AND 51-3-1.

Part: FITTING — CRACKED (LONGERON) · airframe 54,920 hrs · 25,413 cycles

LEFT LONGERON 23 CRACKED AT STA 920. REPAIRED LONGERON IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-20D, 51-3-1, AND 51-3-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,920 hrs · 25,413 cycles

FORWARD LOWER CARGO CORROSION FUSELAGE SKIN AT LONGERON 35 LEFT, FS 620. REPAIR ACCOMPLISHED IAW REA D853-48847MR AND DC-8 SRM 53-2-1, 51-1-20D, AND 51-1-8.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 54,917 hrs · 25,411 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. OPS CHECKED EVERY EXIT LIGHT IAW DC8-1, STEP 7. OPS CHECKED GOOD. OPS CHECKED AGAIN, NO GOOD. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 WDM 33-51-01. OPS CHECKED GOOD IAW DC8-1, STEP 7.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 54,901 hrs · 25,400 cycles

DURING MAINTENANCE INSPECTION, FOUND BATTERIES FOR THE EMERGENCY LIGHT EXPLODED W/O 600187843. REPLACED BATTERY PACK AND OPS CHECKED GOOD IAW DC-8 MM 33-50-02-2.

Part: FAN — DEFECTIVE (CABIN) · airframe 54,460 hrs · 25,032 cycles

LT RECIRCULATION FAN STALLED WITH ODOR OF WIRE BURNING AND ELECTRICAL SURGE ON AIRCRAFT. REMOVED AND REPLACED LT RECIRCULATION FAN IAW DC-8 MM 21-21-01-2. OPS CHECKED GOOD IAW DC-8 MM.

Part: LINK — BROKEN (SPOILER ACT) · airframe 54,367 hrs · 24,960 cycles

RT WING INBOARD SPOILER WOULD NOT DEPLOY. REMOVED AND REPLACED BROKEN ACTUATOR CRANK LINKS IN THE INBOARD AND OUTBOARD POSITIONS FOR THE RT INBOARD SPOILER PANEL IAW MM. OPS CHECKED GOOD.

Part: DOUBLER — CRACKED (RIGHT WING) · airframe 53,983 hrs · 24,667 cycles

RIGHT WING 505F PANEL LAND NUT CHANNEL REMOVED, SEALANT REMOVED, AND HOLES POLISHED TO FACILITATE NDT INSPECTION. REPAIRED AREA IAW DC-8 SRM 51-1-20D AND REA D857-43117MR.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 53,983 hrs · 24,667 cycles

LEFT WING PANEL LAND 505F, UPPER SURFACE, 3 EACH FASTENER HOLES CRACKED. REPAIRED AREA IAW REA D857-43118MR.

Part: FITTING — CRACKED (CABIN) · airframe 53,983 hrs · 24,667 cycles

FUSELAGE STATION 1168, RIGHT SIDE UPPER CUSP LINE CORNER CASTING FROM CUSP EXTRUSION TO STATION 1168 VERTICAL SUPPORT, HAD A CRACK INDICATION FROM BOLT HEAD TO EDGE OF PART, INBOARD SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND 51-1-21D.

Part: ATTACH ANGLE — CRACKED (#1 PYLON) · airframe 53,983 hrs · 24,667 cycles

#1 ENGINE PYLON FOOTSTOOL WAS CRACKED AT THE '6'O-CLOCK POSITION, CENTER BOLT AND NEXT BOLT OUTBOARD. REPAIRED AREA IAW D854-43106MR.

Part: FITTING — CRACKED (FWD LWR CARGO) · airframe 53,983 hrs · 24,667 cycles

FORWARD CARGO AT F.S. 350, BETWEEN LONGERON 36 - 35 LEFT, 'Z' FITTING WAS CRACKED. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-3-2 AND 53-2-0.

Part: SPAR CAP — CORRODED (RT WHEEL WELL) · airframe 53,983 hrs · 24,667 cycles

F.S. 857, BUTT LINE 54 RIGHT, 16" BELOW THE RIGHT MAIN LANDING GEAR WHEEL WELL CEILING, FORWARD BULKHEAD SKIN WAS CORRODED. FABRICATED REPAIR DOUBLER AND SHIM IAW REA D857-43109MR. INSTALLED PARTS AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D857-43109MR.

Part: RIB — CRACKED (RT WHEEL WELL) · airframe 53,983 hrs · 24,667 cycles

F.S. 870, RIGHT WHEEL WELL, LOWER OUTBOARD RIB REPAIR WAS CRACKED. FABBED AND INSTALLED NEW REPAIR, AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D AND ABX DWG 5616306.

Part: FITTING — CORRODED (FWD LWR CARGO) · corrosion level 2 · airframe 53,983 hrs · 24,667 cycles

FORWARD CARGO AT F.S. 330, 'T' BOLT LATCH ATTACH FITTING WAS CORRODED BETWEEN LONGERON 33 RIGHT. REMOVED AND REPLACED BACKUP FITTING IAW DC-8 MM.

Part: FITTING — CRACKED · airframe 53,983 hrs · 24,667 cycles

LEFT WING STATION 340, FLAP SUPPORT FITTING WAS CRACKED. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP SUPPORT FITTING IAW DC-8 MM 20-14-00 AND 20-16-00. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP ACTUATOR CYLINDER AND OPS CHECKED GOOD IAW DC-8 MM 27-51-09.

Part: FITTING — BROKEN (LT I/B AILERON) · airframe 53,983 hrs · 24,467 cycles

LEFT INBOARD AILERON, INBOARD HINGE FITTING WAS BROKEN. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-21A, 51-3-0, 51-1-21, 51-1-24 AND 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,983 hrs · 24,667 cycles

AFT PASSENGER DOOR CUTOUT LOWER FORWARD CORNER SHOWED CRACK INDICATION ON THE FIRST FASTENER COMMON TO THE LOWER DOOR PAN. INSTALLED REPAIR FILLER, DOUBLER, TRIPLER, AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20B AND 51-1-21.

Part: ANGLE — CRACKED · airframe 53,983 hrs · 24,667 cycles

AFT PRESSURE BULKHEAD FORWARD SIDE ANGLE WAS CRACKED AT LONGERON 2 RIGHT, APPROXIMATELY 2 INCHES IN LENGTH. INSTALLED ANGLES AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-11.

Part: FITTING · airframe 53,983 hrs · 24,667 cycles

RIGHT LOWER CUSP AT F.S. 6700, LONGERON 20 RIGHT, HAD POPPED RIVET HEADS FROM CORROSION BULGE. CUTOUT DAMAGED AREA AND INSTALLED NEW DOUBLER AND FILLER, AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 51-1-20D, 53-3-1 AND 51-1-8.

Part: LATCH — INOPERATIVE (FUSELAGE) · airframe 53,366 hrs · 24,178 cycles

AT EWR THE COCKPIT ENTRY DOOR LATCH WAS FOUND TO BE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE COMPLIED WITH ABX REA D852-40152 AND RETURNED THE AIRCRAFT TO SERVICE. AT ILN MAINTENANCE INSPECTED AND REPLACED THE COCKPIT ENTRY DOOR LATCH ASSY.

Part: WINDOW — OUT OF ADJ (COCKPIT) · airframe 53,023 hrs · 23,998 cycles

CAPTAIN''S CLEARVIEW WINDOW (EMERGENCY EXIT) INTERMITTENTLY WOULD NOT OPEN. ADJUSTED CAPTAIN''S CLEARVIEW WINDOW PER DC8 MM 56-10-03.

Part: SCREW — LOOSE (COCKPIT DOOR) · airframe 52,468 hrs · 23,730 cycles

COCKPIT DOOR WOULD NOT OPEN USING KNOB. FOUND LOOSE SCREW. TIGHTENED SCREW. OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 680)

PRESSURE BULKHEAD FS 680, 16 INCHES FROM BOTTOM, TWO CRACKS, ONE RUNS HORIZONTALLY FROM CENTER TO THE RIGHT 18 INCHESLONG, AND SECOND RUNS FROM CENTER HORIZONTALLY TO THE LEFT 4.5 INCHES LONG. REPAIRED IAW DC8 SRM 53-2-5.

Part: PIN — MISSING (SLIDING WINDOW)

FIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND PIN MISSING. REPLACED PIN, OPS CHECKED GOOD.

Part: CONNECTOR — FAILED (COCKPIT)

LOUD AIR NOISE IN FWD COCKPIT AREA. HOT ODOR NOTICED IN COCKPIT. CREW EXPERIENCED BURNING EYES AND HEADACHE. NOISE WAS ELIMINATED BY TURNING OFF NR 3 CTC. REPLACED PNEUMATIC DUCT CONNECTOR, LEAK CHECKED GOOD.

Part: FUSE — FAILED (COCKPIT)

FLIGHT ENGINEER'S PANEL BACKGROUND LIGHTING INOP, SWAPPED FUSES NO HELP. NOTED A SLIGHT SMELL OF BURNING ELECTRICAL WIRE INSULATION UPON ENTERING THE COCKPIT. REPLACED BURNED OUT 5 AMP LIGHT FUSE FOR F/E'S BACKGROUND PANEL LIGHTING. NO OTHER DEFECTS NOTED. OPS CHECKED GOOD IAW DC8 MM.

Part: ACTUATOR — DEFECTIVE (LT MLG)

AFTER PLACING THE GEAR HANDLE IN THE UP POSITION, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND THE DOOR NOT LATCHED LIGHT REMAINED ON. RECYCLED GEAR, WITH NO CHANGE. PERFORMED ALTERNATE UPLATCH CHECK AND GEAR WAS UP AND LOCKED. REPLACED MLG ACTUATOR AND CONTROL VALVE. PERFORMED OPERATIONAL CHECK IAW DC8 MM 32-60-0.

Part: UPLOCK MECH — OUT OF ADJUST (LT MLG)

DURING GEAR UPLATCH CHECK UNSAFE LIGHT CAME ON INDICATING LEFT MAIN GEAR DOOR UNLOCKED. RECYCLED GEAR, PERFORMED ALT UPLATCH CHECK AND LIGHT WENT OUT. READJUSTED LEFT MAIN LANDING GEAR UPLOCK MECHANISM IAW DC8 MM 32-31-0.

Part: BULB — FAILED (LANDING GEAR)

AFTER TAKEOFF WITH GEAR HANDLE UP, THE RED UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK FAILED, WITH LEFT GEAR UNLATCH LIGHT ILLUMINATED. RECYCLED GEAR TWICE. REPLACED TWO BULBS, CLEANED AND LUBRICATED ALL LATCH MECHANISM, OPS CHECKED NORMAL.

Part: SWITCH — DEFECTIVE (LT MLG)

DURING DESCENT, WHEN GEAR WAS LOWERED HAD NO GREEN LIGHTS ON THE LEFT MAIN LANDING GEAR. AIRCRAFT PERFORMED A GO- AROUND, CYCLED GEAR AND INDICATIONS WERE NORMAL. CLEANED CORROSION FROM LEFT GEAR DOWNLOCK SWITCH WIRING TERMINAL STRIP. REPLACED LEFT GEAR DOWNLOCK SWITCH IAW DC-8 MM, OPS CHECKED NORMAL.

Part: SLIDE WINDOW — OUT OF ADJUST (LT COCKPIT)

DURING SERVICE CHECK, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. FOUND UPPER LINKAGE ROD END LOOSE AND OUT OF ADJUSTMENT. ADJUSTED CLEARVIEW WINDOW PER DC-8 MM 56-10-3. CLEANED AND LUBRICATED MECHANISM, WINDOW OPS CHECKED GOOD.

Part: SLIDING WINDOW — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED AND LUBED FIRST OFFICER'S SLIDING WINDOW MECHANISM. OPS CHECK GOOD IAW DC8 MM, CHAPTER 56-10-03.

Part: FIRE LOOP — DEFECTIVE (NR 4 ENGINE)

DURING CLIMB, FIRE WARNING INDICATION OCCURRED ON THE NR 4 ENGINE. DISCHARGED BOTH FIRE EXTINGUISHERS, BUT FIRE WARNING INDICATION REMAINED. COMPLETED INFLIGHT SHUTDOWN OF THE NR 4 ENGINE. REPLACED LOWER FIRE LOOP ASSEMBLY AND UPPER AFT FIRE LOOP ASSEMBLY ON THE NR 4 ENGINE. REPLACED BOTH FIRE EXTINGUISHERS ON THE RIGHT WING. COMPLETED PNEUMATIC LEAK CHECK OF THE NR 4 ENGINE AND NO LEAKS WERE NOTED. NO INDICATIONS OF A FIRE ON THE NR 4 ENGINE WERE NOTED.

Part: SEAT — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S SEAT WOULD NOT REMAIN LATCHED IN POSITIONS SELECTED, FORWARD AFT POSITIONS. LATCH PINS NOT FULLY ENGAGING IN TRACK. LUBED TRACKS, LATCH PINS AND SEAT OPS CHECKED GOOD PER DC8 MM.

Part: FLEX LINE — LEAKING (NR 3 ENG)

HYD SYS PRESS GAUGE READ ZERO WITH BOTH AILERON AND RUDDER REVERSION LIGHTS ON. HYD QTY READ FULL WITH LOW RESERVOIR, LOW PRESS, AND TEMP LIGHTS OUT. REPOWERED AILERONS WITH AUX PUMP; PRESS AND QTY CHECKED OK. AILERON LIGHT EXTINGUISHED, COULD NOT RESTORE NORMAL ENG DRIVEN PUMP PRESS. TESTED HYD SELECTOR LEVER AND COULD READ A 'BUMP' IN PRESS; WHEN CYCLED IT WORKED OK. REPLACED BOTH ENG DRIVEN HYD PUMPS. REPLACED ALL 3 LINES AT LT HYD PUMP. FOUND NR 3 ENG PRESSURE FLEX LINE FROM HYD PUMP TO PYLON CONNECTION TO HAVE A HOLE IN IT; REPLACED LINE. WORK, SYSTEM AND LEAK CHECK DONE IAW DC 8 MM.

Part: TRANSMITTER — DEFECTIVE (NR 1 ENGINE)

ENROUTE TO ILN, NR 1 ENGINE OIL PRESSURE PEGGED TO THE HIGH SIDE. CREW SHUT DOWN ENGINE AS PRECAUTIONARY PROCEDURE. OIL PRESSURE STILL READ PEGGED HIGH. WITH ENGINE SHUT DOWN, OIL PRESSURE READ 100 PSI; SHUT DOWN FOR APPROXIMATELY 20 MINUTES. ALL OTHER INDICATIONS WERE NORMAL. REMOVED AND REPLACED THE NR 1 ENGINE OIL PRESSURE TRANSMITTER AND THE MAIN OIL SYSTEM FILTER. SYSTEM OPS CHECKED GOOD IAW DC 8 MM.

Part: SEAT — WON'T LOCK (LT COCKPIT)

CAPTAIN'S SEAT DOES NOT LOCK IN THE FORE AND AFT POSITION. PIN DOES NOT ENGAGE IN RAIL. REMOVED AND REPLACED CAPTAIN'S SEAT AFTER RETURN FLIGHT TO ILN. SEAT OPS CHECKED GOOD, IAW DC8 MM CHAPTER 25.