N822AX

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,401 hrs · 23,387 cycles

EMERGENCY LIGHTS DIM WHEN PERFORMED CHECK FOR (A) CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 71,309 hrs · 23,296 cycles

EMERGENCY EXIT LIGHTS DISARM CHECK WAS INOPERATIVE. FOUND WIRE NR 1 BROKEN AT EMERGENCY LIGHT SWITCH (R7-61). REPAIRED WIRE IAW DC-8 WD 33-51-01. OPS CHECKED GOOD.

Part: CYLINDER — DEFECTIVE (RT MLG) · airframe 70,870 hrs · 22,917 cycles

WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF, THE REG GEAR UNSAFE LIGHT STAYED ON. ALL GREEN LIGHTS WERE OUT. THE RIGHT MAIN LANDING GEAR DOOR NOT LOCKED LIGHT WAS ON. ABNORMALS COMPLETE. REPLACED THE RIGHT BOGIE TRIM CYLINDER DUE TO SWIVEL DETACHED FROM TRIM CYLINDER. NEW CYLINDER INSTALLED BY ALTERNATE METHOD IAW DC-8 MM 32-33-01-2. OPS AND LEAK CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,823 hrs · 22,877 cycles

EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED BATTERY EMERGENCY LIGHT RACK ASSEMBLY. EMERGENCY LIGHT OPS CHECKED GOOD PER AMM 33-50-02.

Part: WINDOW — OBSTRUCTED (COCKPIT) · airframe 70,628 hrs · 22,720 cycles

FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND AFT LOWER LOCK ON FIRST OFFICER'S WINDOW OBSTRUCTED BY SEALANT. REMOVED SEALANT. WINDOW OPERATED NORMAL.

Part: WINDOW — OUT OF ADJ (COCKPIT) · airframe 70,591 hrs · 22,692 cycles

RIGHT CLEAR VIEW WINDOW WOULD NOT OPEN. ADJUSTED RIGHT CLEAR VIEW WINDOW IAW DC-8 MM 56-10-3. REPAIRED EPOCAST. PRESSURIZED AIRCRAFT TO 4 PSID. NO LEAKS NOTED. WINDOW OPENS FREELY.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

FORWARD LOWER CARGO COMPARTMENT (C2) DOOR TORQUE BOX WEB CRACKED/CORRODED AT FASTENER HOLE, STA 560 LONGERON 34 RIGHT. REPAIRED IAW DC8 SRM 51.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO PIT AT FS 1230 BETWEEN LONGERON 33 - 34 RIGHT, Z-FITTING CORRODED. REPLACED Z-FITTING IAW DC8 SRM 53-2-0, AND DC8 SRM 51.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO STA 980 BETWEEN LONGERON 35 RIGHT TO LONGERON 35 LEFT LOWER BULKHEAD HAD CORROSION AT PREVIOUS REPAIR. REPAIRED IAW DC-8 SRM 53-2-0, 51-1-24, 51-1-8, AND REA D853-40335 MR.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1150 BETWEEN LONGERON 35 RIGHT - 36 RIGHT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, AND 53-2-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1340 ABOVE LONGERON 36 FRAME WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51.

Part: FITTING — CORRODED (LT WING) · airframe 70,585 hrs · 22,687 cycles

LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA (P/N 3641117-1). REPAIRED AREA IAW DC-8 SRM 51.

Part: FITTING — DAMAGED (RT WING) · airframe 70,585 hrs · 22,687 cycles

RIGHT WING SKI FITTING AREA HAS 2 DAMAGED FASTENER HOLES AT STA 51 AND AFT SPAR. REPAIRED AREA IAW DC-8 SRM 51-1-12, 51-1-8, 51-1-20D, AND REA D857-40385.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

TAILSKID LEFT UPPER SUPPORT FITTING HAD CORROSION AROUND 3 OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 LEFT BUTT LINE 8. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3-0, AND DAC DWG 5753522.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

TAILSKID RIGHT UPPER SUPPORT FITTING CORRODED AROUND (3) OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 RBL 8. REPLACED RIGHT TAILSKID UPPER SUPPORT FITTING IAW DC8 SRM 51-1-2, AND DWG 5753522.

Part: DOWNLOCK SWITCH — FAILED (RT MLG) · airframe 70,585 hrs · 22,687 cycles

RIGHT MAIN GEAR DOWN GREEN LIGHT DID NOT COME ON, ON GEAR EXTENSION. REPLACED RIGHT MAIN GEAR LOCK SWITCH PER DC-8 MM 32-60-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO STA 1050-1070 LONGERON 35 RIGHT, LONGERON AND SPLICE ASSEMBLY HAD CORROSION BETWEEN LONGERON SPLICE ASSEMBLY AND SKIN, CAUSING BULGE BETWEEN SKIN AND LONGERON. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, 51-20D, 51-1-21, 51-3-0, AND DAC DWG 9758507, AND REA 853-40346.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

UPPER SIDE OF LONGERON NR 24 FITTING CORRODED AT RIGHT MAIN LANDING GEAR WHEEL WELL, AT FORWARD AND AFT SIDE OF FS 920 BATHTUB FITTING, AND FS 920 BATHTUB FITTING CORRODED ON AFT SIDE AT UPPER PRESSURE WEB. REPLACED BATHTUB FITTING IAW DC-8 SRM 51-1-8, 51-1-21, 53-2-0, 51-2-0, 51-1-17, 51-1-20D, 51-3-0, AND DAC DWG 5802677.

Part: FITTING — BROKEN (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1160, BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING ATTACHING FLANGES WERE MISSING. REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-3-0, AND 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO STA 1160 LONGERON 36 - 35 RIGHT, Z-FITTING CORRODED. REPLACED CRACKED FITTING IAW DC8 SRM 53-2-0.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO STA 980 LONGERON 35 LEFT INTERCOSTAL LOWER FLANGE CORRODED AT FASTENERS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED NEW INTERCOSTAL AND INSTALLED IAW DAC DWG 5779929, DC8 SRM 51-1-8, AND 51-1-20.

Part: FITTING — CORRODED (LT WING) · airframe 70,585 hrs · 22,687 cycles

LEFT WING REAR SPAR XRS 0 AFT FACE OF VERTICAL WEB HAD CORROSION OMITTING AROUND FASTENERS. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG'S 4753127, 4652943, 4652944, 5751690, AND REA'S D857-40389, AND D857-40382MR.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1200 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.

Part: SEAL BRACKET — CRACKED (SERVICE DOOR) · airframe 70,585 hrs · 22,687 cycles

RIGHT (TYPE I) FORWARD DOOR, FORWARD LOWER CORNER SEAL DEPRESSION CRACKED. REPAIRED IAW DC8 SRM 52-2-2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

STATION 320 STRINGER 34 RIGHT HAD CORROSION INBOARD SIDE. REPAIRED AREA IAW DC-8 SRM 53-2-0, AND DC-8 SRM 51.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO Z-FITTING, STA 1180 LONGERON 34 - 33 RIGHT CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED ANGLE IAW DC8 SRM 53-2-0.

Part: ANGLE — CRACKED (AILERON) · airframe 70,585 hrs · 22,687 cycles

RIGHT INBOARD AILERON ON OUTBOARD TRAILING EDGE CRACKED. REPAIRED AREA IAW DAC DWG 5705334, DC8 SRM 51-1-8, 51-1-24, AND 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO Z-FITTING, STATION 1220, LONGERON 33 - 34 LEFT CORRODED. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1180 BETWEEN LONGERON 32 - 33 LEFT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3, 51-1-0, 52-2-0, AND 53-2-0.

Part: WINDOW — STUCK (COCKPIT) · airframe 70,585 hrs · 22,687 cycles

FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REMOVED EXCESSIVE SEALANT FROM EPICAST AREA. WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10-3.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1060 - 1080 LONGERON 36 WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG 9758507, AND REA 853-40346MR.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

LONGERON 24 LEFT CRACKED BETWEEN FASTENERS, TOPSIDE STA 980. REPAIRED AREA IAW DC-8 SRM 53-2-2, 51-1-8, AND 51-1-20.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1150 BETWEEN LONGERON 31 LEFT TO 32 LEFT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.

Part: FITTING — CORRODED (LT WING) · airframe 70,585 hrs · 22,687 cycles

LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA. P/N 3641117-2. REPAIRED AREA IAW DC-8 SRM 51.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT LOWER CARGO Z-FITTING, STA 1160 LONGERON 34 - 33 RIGHT, FLANGE CRACKED AT FASTENER HOLE. REPAIRED IAW DC8 SRM 51, AND DC8 SRM 53.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1200, AT LONGERON 35 RIGHT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-3-0, 53-2-0, 51-1-8, AND 51-1-20D.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO PIT AT FS 1260 ABOVE LONGERON 35 RIGHT, FLOOR ATTACH ANGLE CRACKED. REPAIRED AREA IAW DAC DWG 9754949 AND DC8 SRM 51.

Part: FITTING — CORRODED (LT WING) · airframe 70,585 hrs · 22,687 cycles

LEFT WING TRAPEZOID FITTING VERTICAL ATTACH FITTING P/N 5616344-1 WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,585 hrs · 22,687 cycles

AFT CARGO AT FS 1180 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 51-1-20D, 53-2-0, AND 51-1-8.

Part: PANEL — CRACKED (LT WING) · airframe 70,585 hrs · 22,687 cycles

SIX BOLT HOLES REAMED UP AFTER NDT CHECK BEYOND LIMITS OF SRM PANEL 505 F. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-20B, 51-1-21, DAC DWG 5613609, AND REA D857-40362MR.

Part: FITTING — CORRODED (LT MLG) · airframe 70,572 hrs · 22,677 cycles

THE LEFT MAIN LANDING GEAR FORWARD LUG IS CORRODED AND GOUGED INSIDE THE BORE.

Part: TRUNNION — CORRODED (LT MLG) · airframe 70,572 hrs · 22,677 cycles

THE LEFT MAIN LANDING GEAR TRUNNION FORWARD FITTING HAS CORROSION IN BOTH FWD BORES.

Part: SHAFT — SHEARED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

THE HORIZONTAL STABILIZER OPERATING BULKHEAD, LEFT SIDE AFT END, HAD A SHEARED SHAFT.

Part: PANEL — CRACKED (WING) · airframe 70,572 hrs · 22,677 cycles

PANEL 505F BOLT HOLES HAVE CRACK INDICATIONS FOUND DURING NDT INSPECTION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,572 hrs · 22,677 cycles

ALC STATION 1220-1228 LONGERON 30R-31R TORQUE BOX INTERNAL DOUBLER HAD DEEP EXFOLIATION CORROSION. MAINTENANCE REPAIRED THE AREA IAW ABX REA D853-40368.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,572 hrs · 22,677 cycles

FRAME LINK FLANGE CORRODED AT STA 1000 ABOVE LONGERON 36.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

AFT LOWER CARGO AT STATION 1040 - 1060.0 BETWEEN LONGERON 31 LEFT TO LONGERON 31 RIGHT CIRCUMFERENTIAL SPLICE TEAR STRAP AND FINGER DOUBLER HAD CORROSION BETWEEN SKIN TEAR STRAP AND FINGER DOUBLER. REPAIRED AREA AND REPLACED TEAR STRAP, LONGERON SPLICES, INTERCOSTALS, TIE DOWNS, AND PANEL SUPPORTS IAW DC-8 SRM 51-1-20D, 51-1-21, 51-1-8, 53-2-0, AND DAC DWG 5750322.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,572 hrs · 22,677 cycles

Z-FITTING IN AFT CARGO PIT AT FS 1220 LONGERON 34L-35L IS CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,572 hrs · 22,677 cycles

AFT CARGO PIT FRAME AT FS 1120 ABOVE LONGERON 35R-36R WAS CORRODED UNDER AND AROUND NUT PLATES. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 53-2-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

AFT CARGO PIT FRAME AT FS 1480 ABOVE LONGERON 36 FRAME IS CORRODED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,572 hrs · 22,677 cycles

AFT CARGO PIT AT FS 1150 INSIDE FWD TORQUE BOX LONGERON 35R-36R WAS CORRODED. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 53-2-0.

Part: DOUBLER — BULGED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

FINGER DOUBLER FS 80 ON TOP SIDE OF CUSP WEB BULGED AND FASTENERS WERE SHEARED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

LONGERON 24L FS 980 CRACKED BETWEEN FASTENERS ON TOP SIDE. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,572 hrs · 22,677 cycles

FUSELAGE EXTERIOR SKIN CREASED AND GOUGED AT STA 115-120 LONGERON 21R-23R. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 53-2-1.

Part: RELIEF VALVE — FAILED (NR 3 ENGINE) · airframe 69,798 hrs · 22,249 cycles

WITH THROTTLE AT IDLE NR 3 ENG OIL PRESSURE LIGHT CAME ON WITH PRESSURE INDICATING 32 PSI. POWER BROUGHT BACK UP TO 80 PERCENT N2 OIL PRESSURE WENT TO 55 PSI. THEN DROPPED TO 50 PSI WITH NO CHANGE IN THROTTLE SETTING. THROTTLE BROUGHT BACK TO IDLE PRESSURE REMAINED AT 40 PSI AND THEN DROPPED TO BELOW 35 PSI. ENGINE SECURED AT 0530 Z. REMOVED OLD STYLE OIL PRESSURE RELIEF VALVE AND INSTALLED NEW STYLE OIL PRESSURE RELIEF VALVE, (P/N 779606), INSTALLED DIRECT READING GAUGE. RAN ENGINE, BOTH GAUGES READ WITHIN 1/2 PSI OF EACH OTHER. OIL PRESSURE WITHIN LIMITS. NO LEAKS NOTED. OPS CHECKED GOOD IAW P&W 72-61-6.

Part: RELIEF VALVE — MALFUNCTIONED (NR 3 ENGINE) · airframe 69,904 hrs · 22,289 cycles

BELOW 68 PERCENT N2, NR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON. WOULD NOT GO ABOVE 35 PSIUNTIL 68 PERCENT N2. ENGINE WAS SHUT DOWN AT 10,000 FT, HAD POSITIVE OIL PRESSURE THROUGHOUTAPPROACH AND LANDING. REPLACED NR 3 OIL STRAINER AND REBUILT NR 3 OIL PRESSURE RELIEF VALVE. RAN ENGINE, OPS AND LEAK CHECKED GOOD.

Part: LINER — LOOSE (PAX DOOR) · airframe 69,520 hrs · 22,125 cycles

UNABLE TO OPEN FORWARD ENTRY DOOR. SECURED LOOSE TRIM LINER, OPS CHECKED NORMAL.

Part: SEAT — DEFECTIVE (COCKPIT)

FLIGHT ENGINEER'S SEAT VERTICAL HOLD DOESN'T HOLD SEAT. FELL TO BOTTOM POSITION DURING TAKEOFF AND AGAIN IN CLIMB. INSTALLED NEW FLIGHT ENGINEER'S SEAT IAW DC8 MM. OPS CHECKED GOOD.

Part: FITTING — CORRODED (BS 320)

FITTING CORRODED AT STATION 320 BETWEEN LONGERONS 35 AND 36 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: SKIN — CORRODED (RT ELEVATOR)

RIGHT ELEVATOR SKIN CORROSION AFT OF NR 1 HINGE. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-21A.

Part: FORMER — CRACKED (RT WING)

RIGHT WING, LEADING EDGE, STATION XFS 710 FORMER CRACKED. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-8.

Part: INTERCOSTAL — CRACKED (BS 8)

SKIN BULGED AND FITTING CRACKED AT STATION 8 AND LONGERON 30 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4641704.

Part: FITTING — CRACKED (BS 4)

SKIN BULGED AND FITTING CRACKED AT STATION 4 LONGERON 30 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4641704.

Part: SKIN — CORRODED (RIGHT WING)

CORROSION AT RIGHT WING UPPER SKIN AT FORWARD SPAR, STATION XRS 250. INSTALLED REPAIR DOUBLER IAW ABX REA D857-27330MR.

Part: SKIN — CRACKED (WS 710)

RIGHT WING LEADING EDGE STATION XFS 710, TOP SKIN CRACKED. REPAIRED IAW DC8 SRM 57-2-1 AND DWG 5679600.

Part: SKIN — CORRODED (LT TE FLAP)

LEFT INBOARD FLAP, INBOARD AFT UPPER SKIN CORRODED. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5642960.

Part: ANGLE — CORRODED (FUSELAGE)

FITTING AT STATION 320 BETWEEN LONGERON 35 LEFT AND 36 LEFT CORRODED. REPLACED FITTING IAW DC8 SRM 51-1-20D AND 53-2-0.

Part: SKIN — CRACKED (WS 467)

LEFT WING LEADING EDGE ABOVE NR 1 PYLON INTERNAL SKIN WAS CRACKED AT STATION XW 467. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-11.

Part: SKIN — CRACKED (RT WING)

RIGHT WING LEADING EDGE, LOWER SKIN ABOVE THE NR 4 PYLON AT LEADING EDGE OF PYLON CUTOUT HAD A 3 INCH CRACK. REPAIRED IAW DC8 SRM 57-2-1A.

Part: FITTING — CRACKED (BS 1240)

FRAME ATTACH FITTING CRACKED AT STATION 1240 AND LONGERON 35 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

CRACKED FITTING IN TORQUE BOX STATION 1180 AND LONGERON 28 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND 51-1-11.

Part: FITTING — CORRODED (BS 300)

TORQUE BOX BATHTUB FITTING CORRODED AT STATION 300 AND LONGERONS 34 TO 35 RIGHT. REPAIRED IAW DC8 SRM 51-1-0.

Part: PANEL — CORRODED (RT WING)

FOUND CORROSION ON PANEL 520J, RIGHT WING FUEL ACCESS PANEL. FABRICATED REPLACEMENT PANEL IAW DWG 5761041.

Part: RIB — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB AT STATION XFS 847.5 CRACKED AT LOWER AFT END. REPAIRED IAW DC8 SRM 57-3-1, 51-1-20D AND DWG 5769545.

Part: RIB — CRACKED (WS 772.5)

RIGHT WING LEADING EDGE RIB AT STATION FS 772.50 CRACKED AT AFT LOWER END. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056.

Part: RIB — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB CRACKED AT STATION XS 497.491, UPPER, AFT END. REPAIRED IAW DC8 SRM 57-20-0 AND DWG K05056.

Part: RIB — CRACKED (RT WING)

RIGHT WING LEADING EDGE RIB AT STATION XS 484.895 CRACKED AT AFT END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K05056.

Part: FITTING — CRACKED (FS 1180)

FITTING CRACKED AT STATION 1180 AND LONGERONS 34 LEFT TO 35 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND 53-2-0.

Part: RIB — CRACKED (LEFT WING)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 372.750. REPAIRED IAW SRM 51-1-20D AND 57-2-0.

Part: RIB — CRACKED (WS 616.25)

RIGHT OUTBOARD LEADING EDGE RIB CRACKED AT STATION XFS 616.25. REPAIRED IAW DC8 SRM 51-1-21 AND DWG K05056.

Part: RIB — CRACKED (WS 791.25)

RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 791.25. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056.

Part: RIB — CRACKED (WS 622.5)

RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 622.5. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056.

Part: RIB — CRACKED (WS 732.5)

RIGHT WING LEADING EDGE CRACKED AT STATION XFS 732.5. REPAIRED IAW DC8 SRM 51-1-8.

Part: WINDOW — LACK OF LUBE (LT COCKPIT)

CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WAS HARD TO OPEN. FOUND WINDOW TRIM BINDING. RESECURED TRIM, CLEANED AND LUBRICATED LINKAGE.

Part: BULB — FAILED (CABIN)

DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHT FORWARD OF THE CREW ENTRY DOOR INOP. RELAMPED, OPS CHECKED NORMAL.

Part: WINDOW — JAMMED (LT COCKPIT)

DURING PREFLIGHT, FOUND CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) DIFFICULT TO OPEN AND WAS OCCASIONALLY JAMMING. LUBRICATED LINKAGE. WINDOW OPERATES NORMAL.

Part: SKIN — CORROSION (WS 408)

TWO AREAS OF CORROSION WERE FOUND BEYOND LIMITS, LT WING UPPER SKIN INBOARD OF 408 PRODUCTION SPLICE AND BETWEEN CENTER AND AFT SPAR. REPAIRED LT WING UPPER SKIN AT STA 408 BETWEEN CENTER SPAR AND STRINGER 7 IAW SRM 57-2-1, 51-1-8, 51-1-11, 51-1-23 AND 51-1-20D.

Part: SKIN — CRACKED (RT WING)

RT WING I/B SLOT I/B END L/E SKIN HAS A SMALL CRACK AT RIVET. REPAIR L/E SKIN IAW SRM 57-3-3 AND SRM 57-2-1.

Part: SKIN — CORROSION (WS 6-22.75)

LT WING UPPER SKIN AT TANK ACCESS CUTOUT BETWEEN XRS 22.75 AND XRS 6.00 IS BLENDED BEYOND LIMITS ALLOWABLE BY SRM. REPAIRED LT WING SKIN BETWEEN STA XRS 6.00 AND XRS 22.5 IAW ABX REA D857-20865MR.

Part: SKIN — CORROSION (WS 12)

RT WING SKIN ON TOP OF WING AT APPROX STA XRS HAS AN AREA WHICH IS BEYOND ALLOWABLE LIMITS AT STR 14 AFTER CORROSION REMOVAL. REPAIRED RT WING SKIN AT STA XRS 12 IAW ABX REA 857-21427.

Part: SKIN — CORROSION (WS 280)

LT WING UPPER SKIN AT STA XDS 280 BETWEEN STRINGERS 11 AND CTR SPAR HAS CORROSION BLENDOUT WHICH EXCEEDS LIMITS OF SRM 57-2-0. REPAIRED WING SKIN AT STA XRS280 IAW ABX REA 857-20858MR.

Part: SKIN — CORROSION (LT WING)

LT WING INBOARD L/E UPPER SKIN ALONG THE OUTBOARD EDGE HAS INTERGRANULAR CORROSION AT 5 PLACES. REPAIRED IAW ABX REA D857-20862-MR.

Part: SKIN — CORROSION (WS 337-347)

LT WING SKIN UPPER SURFACE BETWEEN XRS 337 TO 347 AND STRINGER 7 IS BEYOND LIMITS AFTER CORROSION REMOVAL. REPAIRED LT WING SKIN BETWEEN XRS 323 TO XRS 358 AND STRINGER 7 IAW ABX REA D857-20866MR.

Part: FITTING — CRACKED (WS 408)

RT WING STR NR 8 END FITTING AT XRS 408 IS CRACKED. REPLACED RT WING UPPER STRINGER NR 8 FITTING IAW DWG 5616894 AND DC8 SRM 51-1-20D.

Part: SKIN — CORROSION (WS 238)

AREA OF LEFT WING TOP PLATING AT APPROX STA XRS238 IS BEYOND ALLOWABLE LIMITS AFTER CORROSION REMOVAL. REPAIRED UPPER WING SKIN AT STA XRS238 IAW SRM 57-2-1, 51-1-8, 51-1-20D AND 51-1-15.

Part: FITTING — CRACKED (FUSELAGE)

NR 1 CARGO COMPARTMENT NEXT TO FORWARD (SECOND AFT) LOWER 'T' BOLT STOP FITTING INSIDE TORQUE BOX IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORROSION (CARGO COMPT)

NR 1 CARGO COMPARTMENT LOWER AFT 'T' BOLT STOP FITTING INSIDE TORQUE BOX IS CORRODED ON BOTH SIDES. REPLACED 'T' BOLT FITTING IAW DC-8 SRM 51-1-20D AND 53-2-0.

Part: LONGERON — CORROSION (BS 1690)

STA 1690 STRINGER 27L IS CORRODED OUT. FABRICATED AND INSTALLED REPLACEMENT LONGERON FROM FS 1510 TO 1690, 27L IAW DC-8 SRM 53-4-1, FIGURE 43A, DWG 5615377 AND SRM 51-1-20D.

Part: SPAR CAP — CRACKED (LT WING)

LEFT L/E AUX TANK IS CRACKED AT OUTBOARD AFT UPPER CORNER ON ANGLE. INSTALLED REPLACEMENT SPAR CAP IAW DC-8 SRM 53-1-0, 51-1-21 AND 51-3D.

Part: FITTING — CORROSION (BS 8.75)

FORWARD SUPPORT BRACE TOP OF LONGERON 24L CORRODED AT STA 8.79. FABRICATED REPLACEMENT FITTING IAW DWG 3641004 AND ABX REA D851-21385-DE AND INSTALLED IAW DC-8 SRM 53-2-0.

Part: FITTING — CRACKED (MAIN CABIN)

VERTICAL WEB LEG CRACKED STA 32.00 LBL 12. REPAIRED FLOORBEAM VERTICAL FITTING IAW ABX REA D853-20863-MR.

Part: SKIN — CORROSION (SERVICE DOORWAY)

RIGHT SERVICE DOOR CUT OUT LOWER SIDE JUST ABOVE LONGERON 21R EXTERIOR SKIN IS CORRODED BEYOND LIMITS. REPLACED FUSELAGE SKIN IAW ABX REA D853-20861-MR.

Part: FITTING — CORROSION (PAX DOOR)

LEFT AFT ENTRY DOOR INTERNAL STRUCTURE TEE EXTRUDED ANGLE AT AFT SECOND FROM TOP STOP HAS BULGING CORROSION. REMOVED CORRODED FITTING, FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D AND DWG 9751065.

Part: FITTING — CRACKED (LT PAX DOOR)

LEFT HAND AFT ENTRY DOOR INTERNAL STRUCTURE FITTING ABOVE UPPER HINGE CRACKED IN RADIUS. FABRICATED AND INSTALLED FITTING IAW DWG 9751065 AND DC-8 SRM 51-1-20D.

Part: SKIN — CORRODED (LT WING)

RIGHT WING L/E OUTBOARD SECTION HAS TWO CRACKS AND HEAVY CORROSION AT INBOARD END ON TOP. REPAIRED LEADING EDGE IAW ABX REA D857-21380-MR AND SRM 57-21-1, FIGURE 38.

Part: RIB — CRACKED (WS 566.25)

RIGHT WING L/E XFS 566.25 UPPER RIB IS CRACKED. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 AND 51-1-21.

Part: FITTING — CORROSION (PAX DOOR)

LEFT AFT ENTRY DOOR INTERNAL STRUCTURE ANGLE ABOVE UPPER HINGE HAS BULGING CORROSION. INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-8 AND 51-3-0.

Part: SKIN — CORROSION (WS 257)

LEFT WING L/E SKIN AT STA XW257 JUST OUTBOARD OF THE NR 2 PYLON HAS INNERGRANULAR CORROSION AROUND THREE FASTENERS. REPAIRED L/E SRM IAW ABX REA D857-21415.

Part: FITTING — CRACKED (BS 660)

STA 660 AT LONGERON 36, THE LEFT HAND FRAME SPLICE FITTING IS CRACKED AT THE OUTBOARD HOLE IN THE UPPER FLANGE. FABRICATED AND INSTALLED FITTING IAW DWG 3750497 AND DC-8 SRM 51-1-20D.

Part: DOUBLER — CORROSION (BS 24-32)

FINGER DOUBLER CORRODED BEYOND LIMITS AT COCKPIT SUBFLOOD PRESSURE PANEL AT FS 24 TO FS 32 LBL 18. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC-8 SRM 53-3-3, FIGURE 6 AND SRM 51-1-21.

Part: SKIN — CORROSION (BS 1660)

AFT ENTRY DOOR CUT OUT, AFT SIDE F/S 1660.00 AND LONGERON 15L HAS INNERGRANULAR CORROSION BETWEEN SKIN LAMINATIONS. REPAIRED AFT ENTRY DOOR JAMB P/N 5615775-127 IAW ABX REA D853-20846-MR.

Part: DOUBLER — CORROSION (BS 1530-1610)

FINGER DOUBLER AT STA 1530 - 1610 LONGERON 31L IS CORRODED. FABRICATED AND INSTALLED FINGER DOUBLER FROM STA 1530 TO 1610 LONGERON 31L IAW SRM 51-1-21, 51-1-8, 51-1-20D AAND DWG 5615374.

Part: SEAT TRACK — CORROSION (BS 580-600)

STA 580 - 600 RBL 44.5, THE SEAT TRACK IS CORRODED ON BOTH ENDS. REPLACED SEAT TRACK FROM FS 550 TO FS 620 RBL 44 IAW DC-8 SRM 53-2-3.

Part: RIB — CRACKED (WS 227.335)

LEFT WING INBOARD L/E RIB AT STA XS 227.335 IS CRACKED AT THE AFT UPPER END. FABRICATED REPAIR ANGLE AND INSTALLED PER DC-8 SRM 57-2-0, FIGURE 2 AND 51-1-21.

Part: SEAT TRACK — CORROSION (BS 980-1000)

STA 980 TO 1000 LBL 44.5 BOTH SEAT TRACK ENDS HAVE HEAVY CORROSION. REPLACED SEAT TRACK FROM STA 970 TO 1030 LBL 44.5 IAW DC-8 53-2-3, FIGURE 14.

Part: FITTING — CRACKED (FUSELAGE)

NR 1 CARGO COMPARTMENT THIRD AFT FROM FORWARD END 'T' BOLT STOP FITTING (INSIDE TORQUE BOX) IS CRACKED ON FORWARD END. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (PAX DOOR)

LEFT ENTRY DOOR INTERNAL STRUCTURE FITTING CRACKED IN RADIUS AT UPPER FORWARD DOOR STOP. FABRICATED AND INSTALLED FITTING IAW DWG 9751065 AND DC-8 SRM 51-1-20D.

Part: THRESHOLD — CRACKED (BS 1660)

LEFT HAND AFT ENTRY DOOR THRESHOLD WEB IS CRACKED AT THE LOWEST AFT DOOR STOP F/S 1660. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC-8 SRM 51-1-20D, 51-1-21, 51-3-0 AND 53-2-0, FIGURE 10.

Part: SKIN — CORROSION (WS 74)

RIGHT WING TOP SKIN HAS AREA'S WHICH ARE BLENDED OUT OF LIMITS DUE TO CORROSION REMOVAL BETWEEN STR 13 AND CENTER SPAR APPROXIMATE STA 74. FABRICATED AND INSTALLED DOUBLER IAW ABX REA D857-20867-MR.

Part: SKIN — CORROSION (WS 400)

STA XRS-400 JUST AFT OF CENTER SPAR, WAS CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA STA 400, INST CONICAL WASHERS, FABRICATED FILLER AND DOUBLERS, INST FILLER AND DOUBLERS IAW SRM 57-21-1, FIGURE 32.

Part: FITTING — CRACKED (BS 834)

INTERCOSTAL END FITTING CRACKED BELOW LONGERON 21R AT FORWARD SIDE OF FRAME, STA 834. FABRICATED REPLACEMENT FITTING AND INSTALLED IAW DC-8 51-12OD, 51-1-8 AND 51-1-11.

Part: SKIN — CORROSION (RT WING)

TWO INCH INBOARD OF STA 736.5 CANTED RIB AND APPROXIMATELY 14 AFT OF LEADING EDGE PANEL, RIGHT HAND WING CORRODED OUT OF LIMITS. BLENDED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D857-21372, SRM 51-1-21 AND SRM 51-1-12.

Part: FITTING — CRACKED (BS 822)

INTERCOSTAL END FITTING CRACKED BELOW LONGERON 21L AT AFT SIDE OF FRAME, STA. 822. FABRICATED REPLACEMENT FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-8 AND 51-1-11.

Part: INTERCOSTAL — CORROSION (BS 420-440)

LOWER FUSELAGE, INTERCOSTAL CORRODED AT STA 420 TO STA 440, ABOVE LONGERON 31R. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED PER DC-8 SRM 53-3-1, 53-4-1, 51-18 AND 51-1-20D.

Part: SKIN — CORRODED (WS 20-40)

LEFT HAND UPPER WING SKIN BETWEEN XRS - 20 AND XRS - 40, FROM CENTER SPAR TO STR 9 IS CORRODED BEYOND LIMITS. REPAIRED IAW ABX REA D857-20859-MR.

Part: INTERCOSTAL — CRACKED (WS 163.75)

RIGHT HAND L/E XW 163.75 HAS A CRACK ON UPPER INTERCOSTAL EXTENDING FROM FASTENER HOLE TO THE END OF PART. REPAIRED IAW DC-8 SRM 57-3-3.

Part: LONGERON — CRACKED (BS 1630)

DURING C-CHECK, FOUND LONGERON 29L CRACKED AT STA 1630. REPAIRED LONGERON 29L AT STA 1600 TO 1630 IAW SRM 53-4-1 FIGURE 43A AND SRM 51-1-20D.

Part: SEAT TRACK — CORROSION (BS 1280)

STA 1280, LBL 44.5 SEAT TRACK CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK AT STA 1280 LBL 44.5 IAW DC-8 SRM 53-2-3, AND 51-1-8.

Part: DOUBLER — CORROSION (BS 24)

COCKPIT SUBFLOOR AT FS 24 LBL 60 FINGER DOUBLER CORRODED BEYOND LIMITS. FABRICATED FINGER DOUBLER AND INSTALLED FINGER DOUBLER IAW DC-8 SRM 53-3-3.

Part: SKIN — CORRODED (WS 408.3)

AREA OF LEFT WING UPPER SKIN AT APPROXIMATE XW + 408.3, CORROSION IS BEYOND ALLOWABLE LIMITS BETWEEN FRONT SPAR AND CENTER SPAR. REMOVED DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, INSTALLED CONICAL WASHERS AND INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1, FIGURE 32 AND SRM 51-1-20D.

Part: STIFFENER — CORROSION (FUSELAGE)

MAIN CABIN PRESSURE WEB STIFFENER CORROSION OUT OF LIMITS. FABRICATED REPLACEMENT STIFFENER AND SHIM IAW DWG 5645332, DC-8 SRM 51-2-0 AND SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 440)

STRINGER 31R STA 440 IS CORRODED IN CENTER OF STRINGER UNDER FRAME. REPAIRED LONGERON 31R STA 350 TO 450 PER SRM 51-1-21.

Part: BULKHEAD — CRACKED (BS 680)

FUSELAGE STA 680 LBL 5 TO LBL 22 JUST BELOW THE CENTER WING LOWER FORWARD SPAR, THE PRESSURE BULKHEAD IS CRACKED IN TWO PLACES. REMOVED CRACKED SECTION OF DOME, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-25, FIGURE 13.

Part: SKIN — CORROSION (WS 74-106)

LEFT WING LOWER SKIN, STA. XRS 74 TO XRS 106, AFT OF THE CENTER SPAR HAS SEVERAL AREAS OF INNERGRANULAR CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER ABX REA D857-20870-MR, DC-8 SRM 51-1-26 AND SRM 51-1-20D.

Part: WEB — CORROSION (FUSELAGE)

NOSE W/W AFT RIGHT HAND PRESSURE WEB HAS EXFOLIATION EXTENDING THROUGH THE WEB. REMOVED EXFOLIATION ON WEB FABRICATED FILLER AND DOUBLER AND INSTALLED IAW ABX REA D853-20857-MR.

Part: DOUBLER — CORROSION (FUSELAGE)

LONGERON 31L UPPER FINGERS OF FINGER DOUBLER HAS HEAVY CORROSION. REPAIRED IAW DC-8 SRM 53-4-1, FIGURE 2 AND SRM 51-1-20D.

Part: CUSP MEMBRANE — CRACKED (BS 220-204)

LEFT HAND LOWER CUSP MEMBRANE CRACKED AND BULGING BETWEEN STA'S 220 - 204, LBL 44 AREA. REMOVED CRACKED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED IAW DC-8 SRM 53-2-0.

Part: RIB — CRACKED (WS 760)

LEFT WING L/E RIB AT STA XFS 760.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC-8 SRM 57-2-0.

Part: CLIP — CRACKED (WS 6.225)

RIGHT HAND WING L/E AT STA XOLDI 6.225, THE UPPER ATTACH CLIP IS CRACKED IN HALF. FABRICATED AND INSTALLED CLIP IAW DWG 5769589 AND DC-8 SRM 51-1-20 AND 51-1-8.

Part: RIB — CRACKED (WS 722.5)

LEFT WING L/E RIB AT STA XFS 722.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC-8 SRM 57-2-0.

Part: FITTING — CRACKED (BS 340)

STA 340 STR 21R FLOORBEAM FITTING IS CRACKED. REPAIRED IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO COMPT)

NR 3 CARGO COMPARTMENT, FOURTH AFT LOWER 'T' BOLT STOP FITTING IS CRACKED ON THE AFT LEG. REPLACED NR 3 CARGO COMPARTMENT FOURTH AFT LOWER 'T' BOLT STOP FITTING IAW DC-8 SRM 53-10, 51-1-20D AND 53-2-0, FIGURE 2D.

Part: SKIN — CORROSION (LT WING)

LEFT WING UPPER L/E SKIN, AT THE OUTBOARD END AND AFT OF THE INBOARD SLOT HAS EXFOLIATION AND INTERGRANNULAR CORROSION. SPLICED SECTION OF LEADING EDGE SKIN PER ABX REA D85721370.

Part: DRIVE LINK — CRACKED (WS 98)

DURING COMPLIANCE WITH AD 88-10-07, FOUND FLAP DRIVE LINK CRACKED AT POINT J. REPLACED FLAP DRIVE LINK IAW DC8 MM 27-51-4.

Part: HOSE — DEFECTIVE (HYD SYST)

HYDRAULIC QUANTITY DECREASED FROM A TO .25 ABOVE STAND PIPE LEVEL ON CLIMBOUT. ACCOMPLISHED EMERGENCY CHECKLIST AND AIRCRAFT CONTINUED TO FLL AND LANDED USING THE EMERGENCY HYDRAULIC CHECKLIST. REPLACED THE PRESSURE HOSE FROM THE STANDBY RUDDER PUMP TO ACCUMULATOR. SERVICED HYDRAULIC SYSTEM AND CYCLED ALL APPLICABLE COMPONENTS, LEAK CHECKED GOOD. ACCOMPLISHED TAXI CHECK AND OPS CHECKED GOOD.

Part: ACTUATOR PIN — BROKEN (RT MLG)

RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH PIN WAS FOUND BROKEN DURING POST FLIGHT INSPECTION. REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH PIN IAW DC8 MM, COMPLETED RETRACTION/EXTENSION CHECKS AND NO DEFECTS WERE NOTED, OPS CHECKED GOOD. BOLT WAS INSPECTED IAW AD 71-25-09, 11,358.2 HOURS PRIOR TO FAILING.

Part: BALLAST — DEFECTIVE (RT GLARESHIELD)

DURING FLIGHT TRAINING, GLARESHIELD FLUORESCENT LIGHT BLINKED, THEN EMITTED LIGHT SMOKE. REPLACED FLUORESCENT BALLAST ASSEMBLY, OPS CHECKED GOOD IAW DC-8 MM 33-0.

Part: EEL WIRE — BROKEN (CABIN)

EMERGENCY EXIT LIGHTS 'DISARM' LIGHT DOES NOT ILLUMINATE, WHEN DISARM SWITCH IS PLACED IN THE DISARM CHECK POSITION. LIGHT COMES ON WHEN SWITCH IS RELEASED TO THE 'DISARM' POSITION. FOUND BROKEN TERMINAL ON EMERGENCY DISARM LIGHT SWITCH. REPAIRED BROKEN WIRE TERMINAL. ALL SYSTEMS OPS CHECKED GOOD IAW DC 8 MM.