N843AX

Part: FASTENER — LOOSE (COCKPIT) · airframe 53,800 hrs · 28,486 cycles

CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD WAS LOOSE AND INTERMITTENTLY INOPERATIVE. TIGHTENED LOOSE MOUNTING HARDWARE FOR CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD REF DC-8 MM 20-00.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,496 hrs · 28,146 cycles

TAIL SKID UPPER ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20 AND 51-1-21. REMOVED AND REPLACED GILLINER IAW DC-8 SRM 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,496 hrs · 28,146 cycles

AFT CARGO STATION 1240, LONGERON 36 FRAME CORRODED. REPAIRED STATION 1240, LONGERON 36 IAW REA D853-46706. INSTALLED INTERCOSTAL, SHEAR TIE, GILLINER ATTACH ANGLE AND GUSSETTS IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,496 hrs · 28,146 cycles

AFT CARGO STATION 1270, STRINGER 36, CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW REA D853-46699MR. REMOVED AND REPLACED DAMAGED 3759222-1 SPLICE FITTING IAW REA D853-46699MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 28,146 cycles

RIGHT AFT SERVICE DOOR UPPER AFT CORNER HAD CRACK INDICATION. CUT OUT CRACK IAW REA D853-46692MR. FABRICATED REPAIR IAW REA D853-46692MR. INSTALLED REPAIR IAW REA D853-46692MR, DC-8 SRM 51-1-21, 51-1-20D, AND 51-1-11.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 53,455 hrs · 28,115 cycles

FORWARD CABIN DOOR BINDED DURING OPENING AND CLOSING. CLEANED AND LUBRICATED FORWARD CABIN ENTRY DOOR. OPERATED DOOR THROUGH SEVERAL CYCLES. NO DISCREPANCIES NOTED.

Part: STRIKER — WORN (RT MLG) · airframe 53,417 hrs · 28,083 cycles

DURING UPLATCH CHECK, THE UNSAFE LIGHT ILLUMINATED WITH THE RIGHT DOOR UNSAFE LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR 3 TIMES WITH NO IMPROVEMENT. RAN THE ALTERNATE UPLATCH CHECK AND A SLIGHT YAW COULD BE FELT. DOOR LIGHT STILL ILLUMINATED. UNTIL FLAPS WERE PLACED TO 25 DEG DOOR CLOSED AND NOT LATCHED/GEAR UNSAFE LIGHT EXTINGUISHED. CONTINUED TO ILN AT NORMAL SPEED AS PER ABNORMAL. FOUND RIGHT MAIN LANDING GEAR DOOR UPLOCK INDICATOR STRIKER WORN. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLOCK INDICATION STRIKER IAW DC-8 MM 32-31-04-4. PERFORMED GEAR EXTENSION AND RETRACTION CYCLE SEVERAL TIMES IAW DC-8 MM 32-30-00-2. NO DISCREPANCIES NOTED, SYSTEM OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,865 hrs · 27,638 cycles

EMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERY AND RELAY ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM 33-50-01-2-0001.

Part: CONTROL BOX — DEFECTIVE (E/E BAY) · airframe 52,647 hrs · 27,472 cycles

DURING LANDING ROLLOUT, ANTI-SKID FELT TO BE CYCLING IN EXCESS. DURING TAXI, WITH ANTI-SKID ARMED AND TAXI SPEEDS APPROXIMATELY 10 KNOTS, BRAKES SEEMED TO LOOSE EFFECTIVENESS AND MAY BE RELEASING INTERMITTENTLY. REPLACED THE ANTI-SKID CONTROL BOX IAW DC-8 MM 32. OPS CHECKED GOOD. CYCLED BRAKES SEVERAL TIMES, CHECKED GOOD.

Part: ANGLE — CORRODED (CABIN) · airframe 52,640 hrs · 27,467 cycles

LEFT SIDE UPPER SURFACE OF CUSP FITTING HAD CORROSION AT STAION 1060. INTALLED NEW CUSP DOUBLER AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-2-5 AND 51-1-20D.

Part: FINGER DOUBLER — CORRODED (COCKPIT) · airframe 52,640 hrs · 27,467 cycles

COCKPIT FLOOR, STATION 10, THE RIGHT SIDE HAD CORROSION AROUND AND UNDER THE FINGER DOUBLER. INSTALLED NEW FINGER DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-20D, DAC DWG. # 56I12298 AND REA D853-40886MR.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 51,780 hrs · 22,999 cycles

DURING PRE-DEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTING VERY DIM. REPLACED EMERGENCY LIGHTING POWER PACK IAW DC8 MM 33-50-01. OPS CHECKED GOOD.

Part: DOOR — MALFUNCTIONED (MLG) · airframe 51,962 hrs · 27,036 cycles

AFTER TAKEOFF, THE GEAR UPLATCH FAILED. THE RIGHT DOOR NOT LATCHED LIGHT ILLUMINATED ON THE FLIGHT ENGINEER''S PANEL. ROLLER CLEARANCES WERE OUT OF TOLERANCE. PERFORMED ADJUSTMENT AND TEST OF THE DOOR UPLATCH MECHANISM IAW DC8 MM 32-31-04. OPS CHECKED GOOD.

Part: TRANSMITTER — FAILED (NR 3 ENGINE)

NR 3 ENGINE OIL PRESSURE READ 36 PSI DURING DESCENT. WHEN PRESSURE DROPPED BELOW 35 PSI, ENGINE WAS SHUT DOWN. OIL PRESSURE WAS 6 PSI WHILE WINDMILLING FOR LAST 10-15 MINUTES OF FLIGHT. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER. OPS CHECKED GOOD.

Part: SPRING — WEAK (LT MLG WW)

DURING CLIMB-OUT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LEFT GEAR DOOR LIGHT INDICATED UNSAFE. RECYCLED GEAR, LIGHT DID NOT GO OUT. LIGHT WENT OUT DURING CRUISE. REPLACED LEFT MAIN LANDING GEAR DOOR UPLATCH TENSION SPRING. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (RT SPOILER)

RIGHT WING SPOILER DELAMINATED, 6 INCH WIDE AREA APPROXIMATELY 75 PERCENT OF LENGTH OF TRAILING EDGE. REPAIRED UNIT COMPLETE IAW DC8 SRM.

Part: SKIN — DELAMINATED (RT WING VANE)

RIGHT WING VANE, LOWER LEADING EDGE SKIN WAS 20 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM.

Part: SKIN — DELAMINATED (LT WING VANE)

LEFT WING VANE, LOWER SURFACE WAS 90 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM.

Part: BATTERY — DISCHARGED (COCKPIT)

DURING PRE-DEPARTURE CHECK, FOUND RIGHT SIDE EMERGENCY LIGHTING UNDER GLARESHIELD VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 MM 33-50.

Part: SWITCH — DEFECTIVE (RT MLG)

DURING APPROACH, RIGHT MAIN LANDING GEAR INDICATOR DID NOT ILLUMINATE. EXECUTED GO-AROUND AND RECYCLED GEAR. INDICATION WAS NORMAL. REPLACED RIGHT MAIN LANDING GEAR DOWN SWITCH. OPS CHECKED GOOD.

Part: TRIM — BINDING (COCKPIT WINDOW)

CO-PILOT'S CLEARVIEW WINDOW (EMERGENCY EXIT ) WOULD NOT OPEN ALL THE WAY. TRIMMED WINDOW TRIM IAW DC8 MM 25-10-00. OPS CHECKED GOOD.

Part: TRANSMITTER — DEFECTIVE (NR 3 ENGINE)

NR 3 OIL PRESSURE FLUCTUATED 35 TO 37 PSI AFTER IDLE POWER SET DURING DESCENT. PRESSURE STEADIED ABOUT 37 PSI ON LEVEL OFF AT LOW ALTITUDE. WHEN PRESSURE DROPPED TO 35 TO 34 PSI, PRECAUTIONARY SHUT DOWN WAS ACCOMPLISHED . REPLACED NR 3 ENGINE OIL FILTER AS A PRECAUTION. NO FAULTS NOTED WITH FILTER IAW DC-8 MM. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER IAW DC-8 MM. OIL PRESSURE CHECKED GOOD ON ENGINE RUN.

Part: WINDOW — STUCK (COCKPIT)

CAPTAIN'S SLIDING WINDOW (EMERG EXIT) DIFFICULT TO OPEN. WO ULD NOT OPEN FULLY. LUBRICATED MECHANISM, OPS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

DURING SERVICE CHECK, FOUND EMERGENCY POWER SUPPLY FAILED CHECK. REMOVED AND REPLACED EMERGENCY POWER SUPPLY PER DC8 MM 24-30.

Part: HYD HOSE — RUPTURED (RT MLG)

ON TAKEOFF FROM ILN, LOST ALL HYDRAULIC PRESSURE. UNABLE TO RAISE FLAPS. RETURNED TO ILN. REPLACED RIGHT BOGIE TRIM HYDRAULIC LINE. LEAK CHECKED GOOD IAW DC8 MM.

Part: REGULATOR — MALFUNCTION (NR 2 ENGINE)

NR 2 ENGINE OIL TEMPERATURE WENT TO 153 DEG DURING CLIMB. REDUCED POWER TO IDLE, BUT TEMPERATURE REMAINED THE SAME. SHUT DOWN NR 2 ENGINE. REPLACED NR 2 ENGINE OIL TEMPERATURE REGULATOR AND NR 2 OIL STRAINER. OPS CHECKED GOOD IAW DC8 MM.

Part: ACTUATORS — LACK OF LUBE (NLG DOORS)

DURING CLIMB, EXPERIENCED SEVERE VIBRATION IN NOSE GEAR AREA AFTER GEAR RETRACTION. RECYCLED GEAR BUT DID NOT HELP. AIR TURN-BACK TO DFW. VIBRATION STOPPED ON APPROACH. OPERATED DOORS, INSPECTED FOR DAMAGE, FOUND NONE. LUBRICATED DOOR ACTUATORS, OPS CHECKED GOOD IAW DC8 MM 32-22-1.

Part: INTERCOSTAL — CRACKED (BS 240-260)

INTERCOSTAL AT LONGERON 33R BETWEEN STA 240 TO STA 260 IS CRACKED AND DENTED. INSTALLED REPLACEMENT INTERCOSTAL AT L33R BETWEEN STA 240 AND STA 260 IAW DWG 5750726 SRM 51-1-20 51-1-8 AND 51-1-20D.

Part: ANGLE — CRACKED (NR 4 PYLON)

NR 4 PYLON UPPER SPAR LATERAL STIFFENER IS CRACKED. INSTALLED REPLACEMENT ATTACH ANGLE IAW DC8 SRM 54-2-1.

Part: FITTING — CRACKED (BS 834-857)

STRINGER NR 1 TIE FITTING CRACKED AT STA 834 TO 857. FABRICATED AND INSTALLED FITTING IAW DWG 3779900 SRM 51-1-20D AND 51-3-0.

Part: SPLICE — CRACKED (BS 1040-1060)

STA 1040 TO 1060 STR 31R SPLICE FITTING CRACKED. REPLACED FITTING IAW SRM 51-1-20D, 51-1-0 AND 51-1-21.

Part: DOUBLER — CORROSION (BS 350-450)

FS 350 TO FS 450 LONG 31L FINGER DOUBLER IS CORRODED. FABRICATED FINGER DOUBLER AND INSTALLED IAW SRM 51-1-21 AND 53-4-1.

Part: DOUBLER — CORROSION (BS 260-360)

FS 260 LONG 28R FUSELAGE SKIN INTERNAL DOUBLER IS CORRODED. REPLACED INTERNAL DOUBLER FROM FS 260 TO FS 360 BETWEEN L28R AND L36 IAW DWG 5755271 AND SRM 51-1-20D AND 51-1-21.

Part: ANGLE — CORROSION (VERT STAB)

LT FUSELAGE TO VERTICAL STAB ATTACH ANGLE IS CORRODED FROM THE REAR SPAR TO THE CENTER SPAR OF VERTICAL STAB. REPAIRED ATTACH ANGLE IAW SRM 53-2-5, 51-1-20D AND 51-1-21.

Part: SKIN — CRACKED (WS 710)

LT WING OUTBOARD L/E SKIN STA XFS 710 AT THE L/E, SKIN IS CRACKED AT SCREW HOLE. INSTALLED REPAIR IAW SRM 57-2-1.

Part: LONGERON — CRACKED (BS 920)

LONGERON 24L CRACKED JUST AFT OF STA 920 ON UPPER END. REPAIRED LONGERON 24L AT STA 920 IAW ABX REA D853-20837MR.

Part: DOUBLER — CORROSION (BS 210)

AREA HAS HEAVY CORROSION AND DOUBLER IS BLOWN-OUT AT STA 210 STA 21R TO 31R AT FINGER DOUBLER AND INTERNAL STRAP. INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 53-4-1, 51-1-8, 51-1-21 AND 51-1-20D FROM STA 205 TO 215 STR 21R TO 31R.

Part: LONGERON — CORROSION (BS 1276-1286)

FS 1276 TO FS 1286 LONG 27R, CORROSION REMOVAL WAS FOUND TO BE BEYOND LIMITS. REPAIRED LONG 27R FROM STA 1276 TO STA 1286 IAW SRM 53-2-2, 51-1-8 AND 51-1-20D.

Part: RIB — CRACKED (WS 766.25)

LT WING L/E RIB AT STA XFS 766.25 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (CARGO DOOR)

C-1 DOOR LOWER NR 4 T-BOLT FITTING IS CORRODED. REPLACED NR 4 T-BOLT FITTING IAW SRM 51-1-21 AND 51-3-0, 51-1-20D.

Part: RIB — CRACKED (WS 828.75)

LT WING L/E RIB AT STA XFS 828.75 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: SEAT TRACK — CRACKED (BS 200)

STA 200 AT STR 33R, SEAT TRACK IS CRACKED ON BOTH SIDES. REPLACED SEAT TRACK FROM STA 170 TO STA 260 AT STR 33R IAW SRM 53-1-0, 53-2-3 AND 51-1-20D.

Part: RIB — CRACKED (WS 791.25)

LT WING L/E RIB AT STA XFS 791.25 CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 778.75)

LT WING L/E RIB AT STA XFS 778.75 IS CRACKED AT THE AFT UPPER END. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 760)

LT WING L/E RIB AT STA XFS 760.0 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 728.75)

LT WING L/E RIB AT STA XFS 728.75 IS CRACKED AT THE AFT UPPER END. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 835)

LT WING L/E RIB AT STA XFS 835.0 IS CRACKED AT THE AFT UPPER END. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CORROSION (BS 340)

TORQUE BOX FRAME FITTING EXFOLIATED AT STA 340 AFT LWR CORNER, LONGERON 31R. REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1221)

FS 1221 BETWEEN LONGERON 35L AND 36 SHEAR TIE FITTING CORRODED AND CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0, 51-1-8 AND 51-1-20D.

Part: FRAME — CORROSION (BS 1140)

STA 1140 AT STRINGER 36 FRAME UPPER CAP HAS HEAVY CORROSION. REPAIRED FRAME UPPER CAP AT STA 1140 STR 36 IAW SRM 53-2-0, 51-1-8 AND 51-1-20D.

Part: FRAME — CORROSION (BS 1060)

STA 1060 FRAME FWD SIDE ABOVE STRINGER 36 HAS HEAVY CORROSION. REPAIRED FRAME AT STA 1060 STR 36 IAW SRM 53-2-0, 51-1-8 AND 51-1-21.

Part: STIFFENER — CRACKED (WS 735.789)

RT WING L/E AT STA XFS 735.789 THE RIB STIFFENER IS CRACKED AT THE INBOARD END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (WS 6225)

RT WING L/E LWR SKIN AT STA XOLOF 6225 HAS CRACKS AT FASTENERS. REPAIRED L/E SKIN AT STA XOLOF 6225 IAW SRM 57-2-1, 51-1-6, 51-1-21 AND 51-1-11.

Part: RIB — CRACKED (WS 728)

RT WING L/E AT STA XFS 728.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: SEAT TRACK — CORROSION (BS 180)

STA 180 AT STR 33R, SEAT TRACK HAS HEAVY CORROSION. FABRICATED AND INSTALLED SECTION OF SEAT TRACK FROM STA 70 TO STA 170 AT STR 33R IAW SRM 53-1-0, 53-2-3 AND 51-1-20D.

Part: FRAME — CORROSION (BS 1060)

FS 1060 AT LONG 32R FRAME UPPER WEB FLANGE, CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS. REPAIRED FS 1060 AT LONG 32R FRAME UPPER WEB FLANGE IAW SRM 53-2-10, 51-1-8 AND 51-1-20D.

Part: FRAME — CORROSION (BS 1160)

STA 1160 FRAME BETWEEN STRINGER 34L AND 36 IS CRACKED AND HAS HEAVY CORROSION. REPAIRED FRAME AT STA 1160 BETWEEN STRINGER 34L TO 36 IAW DWG 5753893 SRM 51-1-8, 51-1-21 AND 51-3-0.

Part: FITTING — CORROSION (CARGO DOOR)

NR 6 T BOLT BACK UP FITTING FOR FWD BAGGAGE COMPARTMENT DOOR IS EXFOLIATED AT LWR DOOR CUT-OUT AREA. REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 720)

CRACK IN FITTING OF FS 720 AT LONGERON 18R AT FWD RT OVERWING EMERGENCY DOOR. FABRICATED AND INSTALLED FITTING IAW SRM 51-1-21 AND 53-4-1.

Part: FITTING — CRACKED (RT AILERON)

INBOARD AILERON INBOARD HINGE FITTING, RT WING IS CRACKED. REPLACED INBD AILERON INBD HINGE FITTING RT WING PER SRM 51-1-21, 51-1-20D AND 51-3-0.

Part: DOUBLER — CRACKED (NR 4 PYLON)

NR 4 PYLON OUTBOARD SIDE 24 FWD OF WING L/E AT TOP, SKIN HAS TWO LARGE CRACKS AROUND ACCESS PANEL LAND. REMOVED CRACKED OTBD DOUBLER, FABRICATED REPLACEMENT DOUBLER IAW DWG 5765901 AND INSTALLED IAW SRM 51-1-21, 51-1-20D, 51-3-8 AND 51-1-11.

Part: FITTING — CRACKED (BS 440-460)

LONGERON 31L SPLINE FITTING CRACKED BETWEEN STATIONS 440 AND 460. REPLACED SPLICE FITTING IAW SRM 51-1-20D.

Part: THRESHOLD — CRACKED (BS 280)

FWD BAGGAGE COMPARTMENT THRESHOLD AT STA 280 RT SIDE-DOOR SILL IS CRACKED. REPAIRED SKIN IAW ABX REA D853-20852MR.

Part: WEB — CRACKED (NR 4 PYLON)

NR 4 PYLON INBOARD LOWER CHORD CRACKED AT STA YOP 234. REPAIRED NR 4 PYLON INBD LOWER CHORD AT STA YOP 234 IAW ABX REA NO D854-20847MR.

Part: FITTING — CORROSION (CARGO DOOR)

NR 5 T BOLT BACK UP FITTING FOR FWD BAGGAGE COMPARTMENT DOOR IS EXFOLIATED AT LOWER CUT-OUT AREA. REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORROSION (BS 300)

SHEAR TIE FITTING HAS CORROSION OUT OF LIMITS AT FS 300 BETWEEN LONGERON 35L AND 34L. REPLACED SHEAR TIE FITTING IAW SRM 53-2-0 AND SRM 51-1-29D.

Part: DOUBLER — CORRODED (BS 450)

FS 450 LONGERON 31R FINGER DOUBLER IS CORRODED. FABRICATED AND INSTALLED FINGER DOUBLER STA 450 LONGERON 31L TO 31R IAW SRM 51-1-21 AND DWG 5755771.

Part: FITTING — CRACKED (CARGO DOOR)

C-1 DOOR LOWER FORWARD LATCH HAS HEAVY CORROSION AND IS CRACKED. REMOVED AND REPLACED C-1 DOOR LOWER FORWARD LATCH IAW SRM 51-1-29D, 51-3-0 AND 51-1-21.

Part: FITTING — CORRODED (CARGO DOOR)

NR 3 T BOLT FITTING FOR FWD BAGGAGE COMPARTMENT DOOR IS EXFOLIATED AT LOWER DOOR CUT-OUT AREA. REPLACED FITTING IAW SRM 51-3-0, 51-1-29D AND 51-1-8.

Part: FITTING — CORRODED (CARGO DOOR)

BOTTOM OF LOWER C-1 DOOR NR 2 LATCH FITTING IS EXFOLIATED. REPLACED LOWER C-1 DOOR NR 2 LATCH FITTING IAW SRM 51-3-0 AND 51-1-29D.

Part: FITTING — CORRODED (CARGO DOOR)

NR 3 T BOLT BACKUP FITTING FOR FWD CARGO COMPARTMENT DOOR IS EXFOLIATED AT LOWER DOOR CUT-OUT AREA. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (CARGO COMPT)

NR 6 T BOLT FITTING FOR FWD CARGO COMPARTMENT DOOR IS EXFOLIATED AT LOWER CUT-OUT AREA. REPLACED FITTING PER SRM 51-2-0 AND 51-1-29D.

Part: FITTING — CORRODED (CARGO DOOR)

NR 5 T BOLT FITTING FOR FWD BAGGAGE COMPARTMENT DOOR HAS CORROSION AT LOWER DOOR CUT-OUT AREA. REPLACED FITTING IAW SRM 51-3-0, AND 51-1-29D.

Part: FITTING — CRACKED (BS 680)

STRINGER 3L END FITTING CRACKED AT STA 680. REPLACED END FITTING STR 3L STA 680 IAW SRM 53-1-0, 51-1-20D AND 53-2-2.

Part: INTERCOSTAL — CORRODED (BS 700-715)

INTERCOSTAL TIE FITTING CRACKED AT STA 700-715 AND STRINGER 19L. REPLACED TIE FITTING STA 700-715, STRINGER IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INTERCOSTAL TIE FITTING CRACKED STA 857 STRINGER 17L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

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

STA 980-1000 LBL44, SEAT TRACK HAS HEAVY CORROSION. REPLACED SEAT TRACK LBL44 STA 960-180 IAW SRM 51-1-21, 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1140-1160)

STA 1140-1160 LBL 44 SEAT TRACK HAS HEAVY CORROSION. REPLACED SEAT TRACK STA 1110 TO 1210 LBL 44 IAW SRM 53-2-3, 51-1-8, 51-3-0 AND 51-1-21.

Part: CLIP — CORRODED (BS 360)

NR 1 LONGERON ATTACH CLIP AT STA 360 HAS HEAVY CORROSION. FABRICATED LONGERON CLIP IAW DWG 2643629, INSTALLED CLIP AT LONGERON 1 STA 360 IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 350)

EXFOLIATION CORROSION ON TORQUE BOX FITTING AT FS 350 BETWEEN LONGERONS 30R TO 33R. REPLACED FITTING AT FS 350 BETWEEN LONGERONS 30R-33R PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1280-1260)

STA 1280-1260 STRINGER 34L SPLICE FITTING CRACKED. REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1260-1280)

STA 1260-1280 STRINGER 34R SPLICE FITTING CRACKED. REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING)

RT WING INTERIOR, INSIDE ACCESS PANEL JUST OUTBOARD OF NR 4 PYLON ON TOP, WING SKIN (STUB-WING SKIN DOUBLER) IS CRACKED. REPAIRED IAW ABX REA D854-20885MR.

Part: SEAT TRACK — CORRODED (BS 360-520)

STA 360-420 AT STRINGER 33R SEAT TRACK HAS HEAVY CORROSION. REPLACED DAMAGED SECTION OF SEAT TRACK STA 360-520 IAW SRM 52-2-3 AND 51-1-20.

Part: FITTING — CORRODED (BAGGAGE COMPT)

FWD BAGGAGE COMPARTMENT T BOLT STOP FITTING (4TH FROM FWD) HAS HEAVY CORROSION (INSIDE TORQUE BOX). REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 280)

TORQUE BOX LOWER FITTING AT STA 280 STR 33R HAS HEAVY CORROSION. REPLACED FITTING IAW SRM 51-1-20D.

Part: REGULATOR — DEFECTIVE (NR 3 ENGINE)

DURING FLIGHT NR 3 ENGINE WAS INTENTIONALLY SHUTDOWN FOR HIGH OIL TEMP. REPLACED NR 3 ENGINE OIL COOLER REGULATOR.

Part: TURBO COMPRESSOR — DEFECTIVE (NR 3)

NR 3 CTC HOWLED AND FLUCTUATED SEVERELY AND PRODUCED A BURNING ODOR. SHUT DOWN CTC AND ODOR DISAPPEARED SHORTLY THEREAFTER. REPLACED NR 3 CTC IAW DC-8 MM 21-10-01. OPS CHECKED GOOD IAW DC-8 MM PROCEDURES 21-10-01.

Part: DRIVE LINK — CRACKED (RT TE FLAP)

WHILE COMPLYING WITH A.D.88-10-07, FOUND RIGHT INBOARD FLAP DRIVE LINK CRACKED AT POINT J. REPLACED LINK IAW DC-8 M.M. 27-51-4.

Part: BATTERY PACK — DEFECTIVE (COCKPIT)

DURING PREDEPARTURE CHECK, FOUND THE EMERGENCY LIGHTING INOPERATIVE. REPLACED THE EMERGENCY LIGHTING BATTERY RACK, EMERGENCY LIGHTING OPS CHECKED GOOD IAW DC-8 MM 33-50-1.

Part: BEAM — CRACKED (CROSS-SLIDE DOOR)

DURING C-CHECK INSPECTION, DISCOVERED FORWARD CROSS-SLIDE DOOR AT NR 1 PIT LOCKING HOOK FITTING, 4TH HOOK FROM FORWARD END, FRAME BEAM IS CRACKED. REPAIRED BEAM AT FORWARD CROSS-SLIDE DOOR IAW ABX REA-D852-13484-MR.

Part: DOUBLER — CORRODED (WS 845)

DURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE HAS CORROSION UNDER RETAINER RING INSIDE PANEL 517B. REPAIRED RIGHT WING OUTBOARD LEADING EDGE INTERNAL DOUBLER ACCESS PANEL 517B, AT XFS 845 IAW ABX REA-D857-13486-MR.

Part: SKIN — CORRODED (FS 1114)

DURING C-CHECK INSPECTION, DISCOVERED FUSELAGE SKIN CORRODED AT FUSELAGE STATION 1114 OUTBOARD OF LONGERON 36, JUST FORWARD OF EXISTING REPAIR. REPAIRED FUSELAGE CORRODED LOWER SKIN AT FUSELAGE STATION 1114, LONGERON 34L TO 34R IAW ABX REA-D853-13488.

Part: PANEL — CORRODED (RT WING LE)

DURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE ALONG FORWARD RIB CORRODED AND SKIN PULLING UP OVER RIVETS AT STATION 329 INSIDE LEADING EDGE PANEL 522B. REPAIRED RIGHT WING LEADING EDGE LOWER ACCESS PANEL 522B IAW ABX REA-D857-13489-MR.

Part: TRAP FITTING — CRACKED (RT MLG)

DURING C-CHECK INSPECTION, DISCOVERED RIGHT HAND TRAP FITTING HAS CRACK EXCEEDING LAST STOP DRILL. REPAIRED RIGHT MAIN LANDING GEAR SUPPORT FITTING IAW ABX REA-D853-13487-MR.

Part: HYD HOSE — FAILED (NR 2 ENGINE)

DURING CRUISE, HYDRAULIC QUANTITY DROPPED TO STANDPIPE LEVEL. FOUND HYDRAULIC PRESSURE LINE BLOWN ON NR 2 ENGINE. REPLACED PRESSURE LINE AND THE NR 2/NR 3 HYDRAULIC PUMPS IAW DC8 MM, CHAPTER 29-10-12. OPS CHECK AND LEAK CHECK WERE GOOD.

Part: LINK — CRACKED (RT TE FLAP)

DURING COMPLIANCE OF A.D. 88-10-07, S.B. 27-246, A.S.B. 27-269 HAD CRACK INDICATION AT POINT J INBOARD SIDE RIGHT HAND FLAP LINK. REPLACED LINK IAW DC8 MM 27-51-4.