N819AX

Part: NONE — NONE · airframe 55,943 hrs · 9,672 cycles

AFT CARGO DOOR EICAS MSG ON ROTATION ~ OPENED AFT CARGO DOOR & CLOSED DOOR. MSG CLEARED. IAW AMM 52-30. OPS CHECK GOOD

Part: PUMP — OIL CONSUMPTION · airframe 55,375 hrs · 9,525 cycles

(L) ENG OIL CONSUMPTION OBSERVED 1 QT/HR. ~ CORRECTIVE ACTION: R&R LH OIL PUMP PER AMM 79-22

Part: NONE — NONE · airframe 55,364 hrs · 9,522 cycles

OBSERVED L ENG OIL CONSUMPTION LOSS RATE OF 1 QT PER 1.2 HRS. ~ CORRECTIVE ACTION: ACCOMPLISHED OIL CONSUMPTION RUN ON #1 ENGINE PER FIM 71-00 TASK 823

Part: FLOW VALVE — FAILED (LT ACM) · airframe 48,815 hrs · 8,128 cycles

PACK L EICAS MSG DURING CLIMB. REMOVED & REPLACED L LOWER FLOW CONTROL AND SHUTOFF VALVE IAW AMM 21-51 OPS CHECK GOOD NO DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 48,370 hrs · 8,033 cycles

AFTER ROTATION - CARGO DOOR AFT EICAS CAME ON, PRESSURE WAS NORMAL. RETURNED FOR PRECAUTIONARY LANDING. MM 52-21950

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,457 hrs · 72,257 cycles

L2 AFT EMERGENCY LIGHT INOP. REPLACE POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD.

Part: SLEEVE — DAMAGED (HEAT EXCHANGER) · airframe 44,089 hrs · 7,168 cycles

BLEED LEAK L FOLLOWED BY BLEED LOSS WING L. REMOVED AND REPLACED THE SLEEVE AT HEAT EXCHANGER PRIMARY CHECK VALVE IAW AMM 21-52. OPS CHECKED GOOD. LT PACK SYSTEM NO DEFECTS NOTED

Part: SKIN — PEELING (RT NACELLE) · airframe 41,763 hrs · 6,724 cycles

AFTER TEST FLIGHT, PANEL 427AL ON RT PYLON INBOARD SIDE PANEL SKIN WAS OBSERVED PEELED OFF.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 87,163 hrs · 28,549 cycles

ON PRE-D CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. SUSPECT EMERGENCY LIGHT SWITCH WAS ON OVERNIGHT WITH NO EXTERNAL POWER. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT RACK ASSEMBLY IAW DC8 AMM 33-50-01-2-0001. OPS CHECKED GOOD.

Part: PANEL — DAMAGED (LT WING) · airframe 86,312 hrs · 27,974 cycles

DURING REMOVAL OF LOWER REAR SPAR FASTENERS SB 57-88, DOUBLER WAS DAMAGED ON EDGE FROM TRAP PANEL ON LEFT WING. REPAIRED AREA IAW REA D857-51393MR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,312 hrs · 27,974 cycles

FORWARD CARGO COMPARTMENT, FORWARD DOOR OPENING LOWER AFT SKIN CUTOUT, PREVIOUS SPEED TAPE REPAIR CAME LOOSE. REPAIRED AREA IAW REA D853-51391MR.

Part: PIN — SHEARED (MLG) · airframe 86,166 hrs · 27,902 cycles

UPON GEAR RETRACTION, "LNDG GEAR UNSAFE' LIGHT REMAINED ILLUMINATED, FAILED UPLATCH CHECK. LEFT GEAR AND LEFT DOOR LATCH LIGHT ILLUMINATED DURING ALT UPLATCH CHECK. MAINTENANCE AT FLL, FOUND LEFT MAIN GEAR RETRACT ACTUATOR ATTACH PIN SHEARED. REPLACED LEFT HAND GEAR RETRACT ACTUATOR ATTACH PIN IAW OVERHAUL MANUAL 32-1-1B. WORK PERFORMED BY AAR LANDING GEAR SERVICES. LANDING GEAR RETRACTION CHECK DEFERRED PER FERRY PERMIT NR 017-04. AIRCRAFT FERRIED TO ILN. AT ILN PERFORMED ADJUSTMENT TEST OF EXTENSION AND RETRACTION SYSTEM IAW DC8 MM 32-30-00-2-0001. AT ILN, REPLACED LEFT HAND MAIN LANDING GEAR RETRACT SWIVEL GLAND LOWER 90 DEGREE FITTING DUE TO LEAKING IAW DC8 MM 20-13-00-2-0001, LEAK CHECKED GOOD.

Part: SEAT — LACK OF LUBE (COCKPIT) · airframe 85,609 hrs · 27,572 cycles

FIRST OFFICER'S SEAT INTERMITTENTLY SLIPPED OUT OF SELECTED FLOOR LATCHED POSITION. CLEANED AND LUBED FIRST OFFICER'S SEAT TRACKS. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 28-11-01-2-0001.

Part: LIGHT — WILL NOT TEST (CABIN) · airframe 85,551 hrs · 27,538 cycles

EMERGENCY EXIT LIGHT, DISARM CHECK, WOULD NOT TEST. RELAMPED, OPS CHECKED NORMAL.

Part: SWITCH — DIRTY (MLG) · airframe 85,385 hrs · 27,415 cycles

DURING DESCENT, LANDING GEAR WAS EXTENDED TO FACILITATE DESCENT. WHEN GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING "NOT LATCHED" LIGHT ILLUMINATED WITH SELECTOR IN LEFT DOOR POSITION. PERFORMED ABNORMAL PROCEDURE. WHEN GEAR LEVER SELECTED TO UPLATCH CHECK POSITION, DOOR LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED FOR REMAINDER OF FLIGHT. CLEANED AND OPS CHECKED LEFT MAIN LANDING GEAR DOOR LATCH SWITCH IAW DC-8 AMM 32. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,245 hrs · 27,324 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY IAW DC8 MM 33-50-01. CHECKED GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 85,234 hrs · 27,315 cycles

CORROSION ON FORWARD EDGE OF ANGLES AT UPPER OUTBOARD CORNER OF RIGHT WHEEL WELL. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND ABX JOB CARD 8078002.

Part: SKIN — CORRODED (CENTER WING) · airframe 85,234 hrs · 27,315 cycles

MAIN CARGO COMPARTMENT CORROSION ON CENTER WING UPPER SKIN AND DOUBLER FROM FS 760 - 855, LEFT BUTTLINE 3 - 23. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND BUSHINGS, ALODINED, PRIMED, INSTALLED AND LEAK CHECKED IAW REA D857-47555MR AND REA D857-47547MR, REV A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 85,234 hrs · 27,315 cycles

L2 DOOR, UPPER AFT CORNER OF DOOR CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21 AND 51-1-11.

Part: PANEL — DAMAGED (NR 3 PYLON) · airframe 85,234 hrs · 27,315 cycles

COI 43055-01, NR 3 PYLON INBOARD STRESS PANEL. REPAIRED AREA IAW REA D854-47544MR, REV A.

Part: PRESSURE SWITCH — DEFECTIVE (NR 3 ENGINE) · airframe 85,167 hrs · 27,272 cycles

AT FL 330, RAT -15, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH 51 PSI AND OIL TEMP. OF 110 DEG. DURING IDLE, TEMP WAS 115 DEGREES, RPESSURE OF 48 PSI. OIL PRESSURE LIGHT FLICKERED AT IDLE. PERFORMED ENGINE SECURING PROCEDURE. NR 3 ENGINE N2 40 PERCENT AND OIL PRESSURE OF 30 PSI WITH ENGINE SECURED. REPLACED NR 3 ENGINE OIL STRAINER. INSPECTED FOR METAL, NONE FOUND. REPLACED LOW OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. RUN UP AND LEAK CHECKED GOOD IAW DC-8 MM 79-20-04-2.

Part: DOWNLOCK SWITCH — MALFUNCTIONED (MLG) · airframe 85,007 hrs · 27,169 cycles

UPON LOWERING LANDING GEAR, LEFT GEAR DOWN LIGHT DID NOT ILLUMINATE AS WELL AS NO RED UNSAFE LIGHT. RAISED GEAR, RED UNSAFE LIGHT ILLUMINATED WITH NO NOT LATCHED LIGHT ILLUMINATED IN ANY POSITION. UPLATCH CHECK NORMAL INDICATION. LOWERED GEAR AGAIN WITH NO ABNORMAL INDICATION. FOUND LEFT MAIN LANDING GEAR DOWN LOCK SWITCH HAD MALFUNCTIONED. REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH IAW DC-8 MM 32-60-00-2-0001. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,920 hrs · 27,114 cycles

EMERGENCY BATTERY CHARGER CIRCUIT BREAKER TRIPPED. REPLACED EMERGENCY LIGHTING BATTERY PACK ASSEMBLY IAW DC-8 MM 33-50-01-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,882 hrs · 27,088 cycles

OVERHEAD EMERGENCY LIGHT FOR FORWARD CREW DOOR WAS INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHTS FOR FORWARD CABIN DOOR. OPS CHECKED GOOD IAW DC-8 MM.

Part: SKIN — CORRODED (F.S. 1700 - 1746) · airframe 84,868 hrs · 27,073 cycles

TEMPORARY REPAIR FUSELAGE SKIN STA. 1700 AND 1746 IAW ABX REA D853-43878. REMOVED TEMPORARY REPAIRS AND REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1. ALODINED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-1.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 84,826 hrs · 27,043 cycles

FIRST OFFICER'S SEAT SLIPPED BACKWARDS TWICE. FORE AND AFT POSITION. PIN DID NOT DROP IN PLACE. MUST ENSURE SEAT IS LOCKED. REPLACED FIRST OFFICER'S SEAT IAW DC-8 AMM 25-11-01-2.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 84,245 hrs · 26,673 cycles

LEFT MAIN WHEEL WELL INSIDE KEEL BEAM, STATION 910, VERTICAL ATTACH ANGLE, LOWER END CRACKED WITH STOP DRILL HOLE. INSTALLED REPAIR ANGLES IAW REA D853-41947.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 84,245 hrs · 26,673 cycles

LEFT FORWARD ENTRY DOOR MADE A BINDING NOISE WHEN MOVED FROM FULL OPEN POSITION. FOUND SNUBBER SUPPORT WEB CRACKED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED NEW SPLICE AT BOTH ENDS IAW REA D853-41451MR.

Part: SKIN — CRACKED (RT WING) · airframe 84,245 hrs · 26,673 cycles

RIGHT WING LEADING EDGE SKIN HAD CRACK WITH STOP HOLES AT XLS 710, OUTBOARD SIDE OF NR 4 ENGINE. INSTALLED DOUBLER REPAIR IAW DC-8 SRM 57-2-1.

Part: SKIN — CRACKED (LT WING) · airframe 84,245 hrs · 26,673 cycles

LEFT WING LEADING EDGE LOWER SKIN, JUST OUTBOARD OF THE NR 1 PYLON HAD 4 EACH CRACKS AT STATION XRS 525. INSTALLED DOUBLER REPAIR AND REPAIRED AREA IAW DC-8 SRM 57-2-1 AND 51-1-8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,245 hrs · 26,673 cycles

LEFT FREON COMPRESSOR EXHAUST CUTOUT HAD 2 SKIN CRACKS AT THE UPPER FORWARD AND AFT CORNERS. INSTALLED EXTERNAL DOUBLER REPAIR AROUND FREON COMPRESSOR EXHAUST IAW DC-8 SRM 53-2-1.

Part: SKIN — CRACKED (LT WING) · airframe 84,245 hrs · 26,673 cycles

LEFT WING TOP SKIN JUST AFT OF FRONT SPAR, SKIN HAD 1 INCH CRACK AT XW 400, INBOARD THE NR 1 PYLON. INSTALLED DOUBLER AND FILLER, REPAIRED AREA IAW REA D857-41949MR AND DC-8 SRM 51-1-20B, 51-1-20D, 51-1-12 AND 51-1-15.

Part: VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 84,098 hrs · 26,584 cycles

AUTO PRESSURIZATION WAS INOPERATIVE AND CABIN PRESSURIZATION COULD NOT BE CONTROLLED MANUALLY WITH ALL BLEEDS ON HIGH AND ALL CTC'S OPERATING. THE CREW DONNED OXYGEN MASKS AND DESCENDED TO FL 10. MAINTENANCE INSPECTED AND REMOVED A PIECE OF INSULATION FROM THE RIGHT SAFETY VALVE. OPERATION CHECKS WERE COMPLETED IAW DC-8 MM, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 84,038 hrs · 26,546 cycles

DURING CRUISE, LOWER CARGO SMOKE DETECTOR YELLOW MAINTENANCE LIGHT ILLUMINATED WITH GREEN LIGHT ILLUMINATED. REPLACED SMOKE DETECTOR UNIT AT AD CNT. DUE TO FALSE ALARM FAULT CODE IAW DC-8 MM 26-15-00-4. SYSTEM OPS CHECKED GOOD.

Part: ACTUATOR — SEIZED (STABILIZER) · airframe 83,670 hrs · 26,355 cycles

THE CREW REPORTED THE STABILIZER HYDRAULIC SYSTEM TO BE INOPERATIVE. THE LEFT SUITCASE HANDLE WAS JAMMED FULL FORWARD. MAINTENANCE INSPECTED AND REPLACED THE LEFT LONGITUDINAL TRIM ACTUATOR IAW DC8 MM.

Part: CONTROL VALVE — LEAKING (LT MLG WW)

ON FINAL APPROACH, WHEN LANDING GEAR LOWERED, HYDRAULIC PRESSURE WAS DECREASING RAPIDLY. PERFORMED LOSS OF HYDRAULICS CHECK LIST. AIRCRAFT WAS TOWED FROM RUNWAY DUE TO LACK OF BRAKE PRESSURE. REPLACED LANDING GEAR CONTROL VALVE IAW DC8 MM 22-32-7. OPS CHECKED GOOD.

Part: WINDOW — LACK OF LUBE (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN ALL THE WAY. CLEANED DEBRIS FROM TRACK AND LUBED CLEARVIEW WINDOW. ROLLERS OPS CHECKED OK IAW DC-8 SMM 56-10-3.

Part: COMPRESSOR — STALLED (NR 4 ENGINE)

NR 4 ENGINE COMPRESSOR STALLED WHEN REDUCING POWER FROM CLIMB TO CRUISE. ENGINE OIL QUANTITY DROPPED RAPIDLY FROM 3.1 TO 1.6 GALLONS. SHUT ENGINE DOWN. REPLACED NR 4 ENGINE IAW ABX JOB CARD J-8090507. OPS AND LEAK CHECKED GOOD.

Part: WARNING — ILLUMINATED (ANTISKID SYST)

DURING APPROACH, ANTISKID LIGHT CAME ON 'LF0 AND LFI' LIGHTS ON SKID CONTROL PANEL WERE ON. AFTER RECYCLING THE GEAR, LIGHTS WENT OUT. TROUBLESHOT ANTISKID SYSTEM IAW DC8 MM. NO DEFECTS WERE FOUND, OPS CHECKED GOOD.

Part: DRIVE LINK — CRACKED (LT TE FLAP)

WHILE COMPLYING WITH AD 88-10-7, FOUND CRACK INDICATION ON LEFT FLAP DRIVE LINK STATION 98 AT POINT J, OUTBOARD LUG. REPLACED LINK IAW DC8 MM 27-51-4.

Part: SKIN — CRACKED (WS 160)

LEFT WING UPPER TRAILING EDGE SKIN STATION XRS 160 AT THE REAR SPAR IS CRACKED IN 2 PLACES. REPAIRED SKIN IAW DC8 SRM 57-2-0.

Part: ANGLE — CRACKED (RT WING)

RIGHT WING INBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (WS 197)

RIGHT WING LEADING EDGE SKIN UPPER SURFACE AT STATION XFS 197 IS CRACKED AT A FASTENER HOLE. REPAIRED LEADING EDGE SKIN IAW DWG 5769859 AND DC8 SRM 57-2-0.

Part: SKIN — CRACKED (WS 251)

LEFT WING LEADING EDGE UPPER SKIN INTERNAL DOUBLER AT STATION XS 251 CRACKED. REPAIRED IAW DACO DWG 5769759 AND DC8 SRM 51-3-0.

Part: BULKHEAD WEB — CRACKED (BS 1890)

1 .5 INCH CRACK AT AFT BULKHEAD STATION 1890, UPPER RIGHT CORNER ABOVE BRACKET WITH MOUNT BOLT FOR RUDDER POWER MECHANISM. REPAIRED IAW DC8 SRM 52-2-0.

Part: BULKHEAD — CRACKED (WS 508.977)

LEFT WING CANTED BULKHEAD LOWER FLANGE CRACKED AT XRS 508.977 BETWEEN STRINGERS 63-64. REPAIRED IAW ABX REA D853-22858MR AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 495)

ATTACH FITTING AT CANTED STATION XRS 495 TO STRINGER 63 (UPPER SKIN) HAS CRACK AT LAST FASTENER HOLE. FABRICATED REPLACEMENT ATTACH FITTING IAW DWG 3648143 AND ABX REA 857-22859.

Part: ANGLE — CRACKED (WS 857)

CRACK IN LEFT WING REAR SPAR LOWER CAP STATION 857 LBL 70 INBOARD APPROXIMATELY 9 LEFT MLG WHEEL WELL, FORWARD, LOWER, OUTBOARD. REPAIRED IAW DWG SR08570009 AND DC8 SRM 51-1-8 AND 51-1-20D.

Part: FRAME — CRACKED (BS 1040)

STATION 1040 FRAME UPPER CHORD, LOWER SURFACE AFT SIDE, AT LONGERON 31R AND 32R HAS HEAVY EXFOLIATION CORROSION AND IS CRACKED. REPAIRED IAW ABX REA D853-22857, SRM 51-1-21, 51-1-20D AND 51-1-11.

Part: SKIN — CRACKED (PAX DOORWAY)

TWO .25 INCH CRACK ON FWD PASSENGER ENTRY DOOR LOWER AFT CORNER SKIN PANEL. REPAIRED IAW DC8 SRM 53-2-0.

Part: FITTING — CRACKED (BS 440-460)

STATION 440 TO 460 LONGERON 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21D AND 51-1-20D.

Part: FITTING — CRACKED (BS 600-620)

STATION 600 TO 620 LONGERON 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.

Part: RIB — CRACKED (WS 641.25)

RIGHT WING LEADING EDGE AT STATION XFS 641.25 IS CRACKED AT UPPER END. REPAIRED IAW DRAWING ABX K05056.

Part: FITTING — CRACKED (BS 1120)

STATION 1120 FRAME TO CUSP FITTING, RIGHT SIDE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-18 AND DWG 9755584.

Part: RIB — CRACKED (WS 550)

LEFT WING LEADING EDGE STUB UPPER RIB CRACKED AT APPROXIMATELY XFS.550. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND ABX DWG K05056.

Part: DOUBLER — CORROSION (WS 372.75-379)

RIGHT WING LEADING EDGE LOWER SKIN DOUBLER FORWARD EDGE BETWEEN STATION XFS 372.75 AND XF 379.0 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW DC8 SRM 51-3-0 AND DWG 5641253.

Part: FITTING — CRACKED (BS 717)

AFT END FITTING ON LONGERON INTERCOSTAL AT STATION 717, LONGERON 14L IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: WEB — CRACKED (BS 150-160)

LOWER TORQUE BOX WEB CRACKED AND CORRODED BEYOND LIMITS, FWD GALLEY DOOR FS 150 TO FS 160, LONGERON 17R TO LONGERON 21R. REPAIRED IAW DC8 SRM 51-1-21, 51-1-20, 51-1-8 AND 51-1-11.

Part: ANGLE — CRACKED (BS 190-200)

TORQUE BOX WEB LOWER SUPPORT ANGLE CRACKED FROM FS 190 TO FS 200, LONGERON 21R. REPAIRED IAW DWG 575700 AND DC8 SRM 51-1-21, 51-1-21D AND 51-1-8.

Part: FITTING — CRACKED (BS 742)

LONGERON END FITTING AT STATION 742 LONGERON 19L CRACKED. REPLACED FITTING PER DC8 SRM 51-1-20D.

Part: SKIN — CORROSION (WS 610)

RIGHT WING LEADING EDGE UPPER SKIN AT STATION XFS 610 HAS HEAVY CORROSION AND IS CRACKED. REPAIRED IAW DC8 SRM 52-2-1 AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE)

STRINGER NR 59 END FITTING CRACKED AT NR 4 ALTERNATE FUEL TANK. INSTALLED REPLACEMENT FITTING PER DWG 5644973, DC8 SRM 51-1-20D AND 51-1-23.

Part: INTERCOSTAL — CRACKED (LT WING)

LEFT WING LEADING EDGE JUST OUTBOARD OF THE LEADING EDGE AUX TANK, THE INTERCOSTAL IS CRACKED AT THE INBOARD END. REPAIRED IAW DC8 SRM 51-01-20 AND DOUG DWG NR 5769859.

Part: RIB — CRACKED (WS 354)

LEFT WING LEADING EDGE RIB AT STATION XFS 354.0 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-20D AND 51-1-8.

Part: RIB — CRACKED (WS 442.185)

RIGHT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT AFT UPPER END. INSTALLED ANGLE REPAIR DOUBLERS IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 227.335)

LEFT WING LEADING EDGE RIB STATION XS 227.335 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 250.089)

LEFT INBOARD STUB WING HAS 2 CRACKS AT STATION XS 250.089. REPAIRED IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-20D.

Part: RIB — CRACKED (WS 250.089)

LEFT INBOARD STUB WING STATION XS 250.089 UPPER LEADING EDGE RIB CRACKED. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND DWG K05056.

Part: RIB — CRACKED (LT WING)

THE LEFT OUTBOARD SLOT OUTBOARD UPPER CLOSURE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 440-460)

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

Part: RIB — CRACKED (RT WING)

RIGHT WING OUTBOARD SLOT, OUTBOARD UPPER CLOSURE RIB IS CRACKED. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-21.

Part: ANGLE — CRACKED (WS 250)

LEFT INBOARD STUB WING AT STATION XS 250 CRACKED AT BOTTOM. INSTALLED REPAIR ANGLE STIFFENER IAW DWG 9753203 AND DC8 SRM 51-1-20.

Part: FITTING — CRACKED (BS 1040-1060)

STATION 1040-1060 STRINGER 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.

Part: STIFFENER — CRACKED (WS 250.089)

LEFT INBOARD STUB WING AT STATION XS 250.089, THE VERTICAL STIFFENER ANGLE (RIB ATTACH ANGLE) IS CRACKED AT THE BOTTOM END. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-8.

Part: BRACKET — CRACKED (WS 603.75-610)

LEFT WING OUTBOARD LEADING EDGE FWD TAI SUPPORT BRACKET BETWEEN STATION XFS 603.75 AND 610 IS CRACKED IN TWO PLACES. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 1440)

INTERCOSTAL CRACKED AT STATION 1440 AND LONGERON 34R. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5616674.

Part: RIB — CRACKED (WS 466.651)

RIGHT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT THE AFT LWR END. REPAIRED IAW ABX DWG K05056 AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 600-620)

STATION 600-620, STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DWG 3750257 AND DC8 SRM 51-3-0.

Part: ANGLE — CRACKED (BS 380)

FORWARD AND AFT SIDES OF STATION 380 FLOORBEAM LBL 11 AND RBL 11. THE INTERCOSTAL ATTACH ANGLES ARE CRACKED. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5610326 AND SRM 51-1-21.

Part: ANGLE — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB AT STATION XS 448.501 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (WS 785)

RIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT LWR END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (WS 585)

LEFT WING LEADING EDGE RIB AT STATION XFS 585.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (WS 803.75)

LEFT WING LEADING EDGE RIB AT STATION XFS 803.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (WS 585)

RIGHT WING LEADING EDGE RIB AT STATION XFS 585.00 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (WS 603.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 603.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 347.75)

LEFT WING LEADING EDGE RIB AT STATION XFS 347.75 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING KO5056.

Part: ANGLE — CRACKED (WS 822.5)

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

Part: RIB — CRACKED (WS 747.5)

LEFT WING LEADING EDGE RIB AT STATION XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.

Part: ANGLE — CRACKED (WS 741.25)

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

Part: ANGLE — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB AT STATION XFS 772.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 442.185)

LEFT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.

Part: ANGLE — CRACKED (WS 672.5)

RIGHT WING LEADING EDGE RIB AT STATION XFS 672.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 448.5)

LEFT WING LEADING EDGE RIB AT STATION XS 448.50 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.

Part: ANGLE — CRACKED (WS 778.75)

RIGHT WING LEADING EDGE RIB AT STATION XFS 778.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG NR K05056 AND DC8 SRM 51-1-8.

Part: MOUNT — SHEARED (NR 3 ENGINE)

DURING C-CHECK, FOUND NR 3 ENGINE REAR INBOARD MOUNT ARM SHEARED AT THREADED PORTION. *S/D* REPLACED NR 3 LEFT AFT ENGINE MOUNT IAW DC8 MM 71-20-02.

Part: BULKHEAD FITTING — CORRODED (BS 70)

STATION 70 BULKHEAD FORWARD SIDE LONGERON 31R INBOARD FITTING HAS HEAVY CORROSION ON LOWER FLANGE BELOW BOLT HEAD. REPLACED FITTING IAW SRM 51-1-21 AND DWG 4614397.

Part: ANGLE — CRACKED (LT WING)

THE LEFT OUTBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM END. REPAIRED IAW DC8 SRM 51-1-21 AND 57-3-3.

Part: RIB — CRACKED (WS 446.651)

LEFT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056.

Part: ANGLE — CRACKED (WS 791.25)

LEFT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.

Part: RIB — CRACKED (WS 716025)

LEFT WING LEADING EDGE AT STATION XFS 716.250. THE UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW ABX DWG K05056.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW EMERG EXIT WOULD NOT OPEN FULLY. ADJUSTED LOWER TRACK IAW DC8 MM.

Part: SWITCH — DEFECTIVE (RT MLG)

ON LANDING, WHEN GEAR HANDLE PLACED IN THE EXTEND POSITION, RIGHT GEAR DOWN LIGHT DID NOT ILLUMINATE. ACCOMPLISHED TOWER FLY-BY TO VERIFY GEAR DOWN. LANDING WAS UNEVENTFUL. REPLACED RIGHT MLG DOWN LOCK SWITCH, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS DISARMED LIGHT CYCLED ON AND OFF WITH EMERGENCY SWITCH OFF. REPLACED EMERGENCY LIGHT BATTERY.

Part: PANEL — CRACKED (HORIZ STAB)

DURING COMPLIANCE WITH AD 90-16-05 AND SB 55-15R3, FOUND HORIZONTAL STABILIZER HAD .75 INCH CRACK, AT LT FORWARD LOWER CONSTANT BOX PANEL. PLACED ON CONTINUING INSPECTION EVERY 900 FLIGHT HOURS OR EVERY 3 MONTHS (WHICH EVER COMES FIRST) IAW DAC SB 55-15.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

DURING CRUISE EXPERIENCED STRONG HYDRAULIC FLUID ODOR IN COCKPIT. FLUID ODOR WAS FOUND TO BE RESIDUAL FLUID FROM PREVIOUS HYDRAULIC LEAK AT CARGO DOOR HYDRAULIC PUMP. CLEANED RESIDUAL FLUID.

Part: AIR DISTR — ODOR (CABIN)

DURING CLIMB, AN ELECTRICAL BURNING SMELL WAS EMITTED FROM THE CTC CONTROL PANEL WHEN THE NR 1 AND NR 4 CTC'S WERE TURNED ON. THE SMELL DISSIPATED AFTER THE CTC'S RAN FOR APPROXIMATELY 30 SECONDS. VISUALLY INSPECTED THE CTC'S AND NO DEFECTS WERE NOTED. VISUALLY INSPECTED BEHIND THE CTC CONTROL PANEL FOR EVIDENCE OF BURNED WIRING OR SWITCHES AND NO DEFECTS WERE NOTED. OPERATED ALL FOUR CTC'S AND OPS CHECK WAS GOOD. NO EVIDENCE OF AN ELECTRICAL BURNING SMELL.

Part: SEAT TRACK — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S SEAT SLID BACK OUT OF LOCKED POSITION DURING TAKEOFF AND AGAIN DURING CRUISE. CLEANED AND LUBED FIRST OFFICER'S SEAT TRACKS AND OPS CHECKED GOOD.

Part: SEAT — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S SEAT WILL NOT STAY IN A LOCKED POSITION. LUBRICATED FIRST OFFICER'S SEAT, OPS CHECK GOOD IN ALL POSITIONS.

Part: SWITCH — FAULTY (THROTTLE ASSY)

LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK OK, WARNING HORN AUDIBLE WITH FLAPS OUT OF ZERO POSITION. RECYCLED GEAR, NO CHANGE NOTED. FOUND THROTTLE SWITCH AT FAULT. CORRECTED PROBLEM, GEAR INDICATION OPS CHECKED GOOD IAW DC-8 SUPPLEMENTAL MM 32-60-00.

Part: UPLATCH — LACK OF LUBE (RT MLG)

RIGHT MAIN LANDING GEAR DOOR FAILED UPLATCH CHECK. RECYCLED GEAR. LIGHT EXTINGUISHED. CLEANED, INSPECTED AND LUBED THE RIGHT MAIN GEAR DOOR UPLATCH. PERFORMED ADJUSTMENT TEST IAW MAB 32-6. OPS CHECKED GOOD.