N820AX

Part: BRAKE ASSY — BROKEN (MLG) · airframe 70,512 hrs · 23,665 cycles

NR 8 BRAKE COMPENSATING LINK ATTACH POINT BROKE. REMOVED AND REPLACED BRAKE AND TIRE ASSEMBLY IN THE NR 8 POSITION IAW DC-8 MM 32-40-0.

Part: MECHANISM — BROKEN (RT WING TE FLAPS) · airframe 70,323 hrs · 23,504 cycles

WHEN FLAPS WERE EXTENDED TO THE 12 DEG POSITION, THE LEFT FLAP POSITION INDICATED 12 DEG AND THE RIGHT FLAP INDICATED 7 DEG. THE AIRCRAFT ROLLED TO THE LEFT. RETRACTED FLAPS AND RE-EXTENDED, OPS NORMAL. VERIFIED, FOUND RIGHT INBOARD FLAP ACTUATOR MECH ASSEMBLY BROKEN. REPLACED FLAP ACTUATOR ASSEMBLY IAW DC-8 MM 27-51-09-4. LEAK CHECKED GOOD. PERFORMED ADJ/TEST IAW DC-8 MM 27-50-00-5. OPS CHECKED GOOD. REPLACED DAMAGED FLAP STOP ASSEMBLY IAW DC-8 MM 27-51-09. ADJUSTED STOP IAW DC-8 MM 27-50-00. OPS CHECKED GOOD. REPLACED DAMAGED RIGHT WING INBOARD TRAILING EDGE PANEL IAW DC-8 MM 57-10-00. REPLACED RIGHT WING INBOARD FLAP ACTUATOR EXTEND HYDRAULIC LINE IAW DC-8 MM 27-50-00. OPS AND LEAK CHECKED GOOD.

Part: UPLOCK — LACK OF LUBE (MLG) · airframe 70,257 hrs · 23,447 cycles

GEAR UPLATCH FAILED TWICE. RECYCLED AND FOLLOWED ABNORMAL PROCEDURES. SUSPECT CABLE TO NOSE GEAR. TRIED AGAIN ON FINAL APPROACH AND UPLATCH CHECK WAS NORMAL. AIRCRAFT FERRIED TO ILN. INSPECTED UPLATCH ASSEMBLY. GROUND OPS SEVERAL TIMES. LUBRICATED UPLATCH ASSEMBLY. VERIFIED OVERCENTER MEASUREMENTS IAW DC-8 MM 32-31-06. GROUND OPS NORMAL.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

FORWARD CARGO, FS 300, BETWEEN LONGERON 33 RIGHT - LONERON 34 RIGHT, "Z" FITTING WAS CORRODED. REPLACED "Z" FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND DAC DRAWING #3755824.

Part: STRAP — CORRODED (F.S. 485) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

FORWARD CARGO STATION 485, LONGERON 34 RIGHT, DOUBLER ON BACKSIDE OF LONGERON WAS CORRODED. REPLACED STRAP IAW DC-8 SRM 51-1-24 AND 51-1-20D.

Part: LONGERON — CRACKED (F.S. 520) · airframe 69,771 hrs · 23,047 cycles

FORWARD CARGO STATION 520, LONGERON 35 RIGHT, INBOARD FLANGE WAS CRACKED. REPAIRED AREA IAW REA D853-43899-MR.

Part: FITTING — CORRODED (F.S. 70) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

FORWARD CARGO AT STA. 70, STRING 25 LEFT, LONGERON END FITTING WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0.

Part: SHEAR TIE — CORRODED (STA. 1520) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 RIGHT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D.

Part: SHEAR TIE — CORRODED (STA. 1520) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 LEFT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D.

Part: ATTACH ANGLE — CORRODED (F.S. 986) · corrosion level 2 · airframe 69,771 hrs · 23,047 cycles

AFT LOWER CARGO STATION 986, FLOOR ATTACH ANGLE, BETWEEN LONGERON 33 RIGHT AND LONGERON 34 RIGHT, WAS CORRODED. REPAIRED AREA AND INSTALLED NEW FLOOR ATTACH ANGLE IAW DC-8 SRM 51-1-21, 51-1-20D AND REA D853-43896-MR.

Part: SKIN — CRACKED (XFS 515 - 526) · airframe 69,771 hrs · 23,047 cycles

RIGHT WING, INBOARD OF THE #4 PYLON, STATION XFS 515.00 - 526.76, HAD CRACK INDICATION AT HOLES 2 AND 4 GOING OUTBOARD. REPAIRED AREA AND INSTALLED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0, 51-1-20D AND REA D857-43890-MR.

Part: DRIVE LINK — BROKEN (LT SPOILER) · airframe 69,470 hrs · 22,780 cycles

THE LEFT MID FLIGHT SPOILER INBOARD DRIVE LINK FOUND BROKEN DURING SERVICE CHECK INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE INBOARD DRIVE LINK CRANK ASSY AND COMPLETED OPERATIONAL CHECKS IAW DC-8 MM 27-61-01-2.

Part: CAPACITOR — BLOWN · airframe 69,477 hrs · 22,786 cycles

#1 RADIO ALTEMETER CIRCUIT BREAKER OPENED. THE BREAKER WAS RESET ONCE AND OPENED AGAIN. MAINTENANCE REPLACED THE #1 RADIO ALTIMETER IAW DC8 MAINTENANCE MANUAL 34. INSPECTION OF THE RADIO ALTIMETER INDICATED THAT THE POWER SUPPLY INPUT CAPACITOR A6C1A EXPLODED, CAUSING POWER SUPPLY DAMAGE AND POSSIBLE FLAME. ADJACENT COMPONENTS WITHIN THE RADIO ALTIMETER WERE DAMAGED OR BURNT, AND THE UNIT WAS CONTAMINATED WITH CAPACITOR CHEMICALS. RADIO ALTIMETER S/N 11043 WAS SCRAPPED.

Part: PIN — SHEARED (NLG) · airframe 69,302 hrs · 22,641 cycles

AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE JET PUMP WOULD NOT TURN OFF AND AUTO PRESSURIZATION CONTROL WOULD NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE ANTI-RETRACTION SWIVEL PIN ON THE GROUND SHIFT MECHANISM. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,144 hrs · 22,516 cycles

CORROSION WAS FOUND AT FUSELAGE STATION 1200 - 1180 L34R INSIDE THE TORQUE BOX. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-39259 AND DC-8 SRM 51-1-20.

Part: SEAL — LEAKING (HYD SYSTEM) · airframe 69,026 hrs · 22,455 cycles

SLOW HYDRAULIC FLUID LOSS EN ROUTE; ARRESTED AT STANDPIPE DURING EMERGENCY CHECK LIST. VERIFIED LEAK AT SLOT CONTROL VALVE. REPLACED SEAL. COMPLIED WITH HYDRAULIC RESERVOIR SERVICE IAW DC8 29-16-00. LEAK CHECKED GOOD IAW DC8 MM.

Part: POWER PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT COME ON WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT PACK ASSY. OPS CHECKED GOOD.

Part: POWER PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 MM 33-50-00.

Part: BULB — CORRODED (COCKPIT)

DID NOT GET RIGHT MAIN GEAR GREEN LIGHT WHEN GEAR HANDLE PLACED IN DOWN POSITION. RECYCLED GEAR, DID NOT CHANGE INDICATION. CONTACTS ON BULBS WERE CORRODED. REPLACED BOTH INDICATION BULBS. SYSTEM OPS CHECKED GOOD IAW DC8 MM.

Part: WHEEL — FAILED (RT MLG)

BEAD FLANGE SEPARATED FROM NR 5 MAIN LANDING GEAR ASSEMBLY, DAMAGING NR 5 MAIN GEAR BRAKE ASSEMBLY. REPLACED NR 5 WHEEL ASSEMBLY AND NR 5 MAIN GEAR BRAKE ASSEMBLY.

Part: DOUBLER — CRACKED (BS 1640-4680)

DOUBLER CRACKED AT STATION 1640 TO 1680. REPAIRED DOUBLER IAW ABX REA D853-27021MR.

Part: BOSS — CORRODED (LT MLG)

CORROSION FOUND IN LEFT MAIN LANDING GEAR PIN BOSS HOLE. REPAIRED IAW ABX REA D832-26975 MR.

Part: DOUBLER — CORRODED (BS 1660-1700)

INNER DOUBLER AT STATION 1660 TO 1700 CORRODED. REPAIRED IAW ABX REA B853-26997MR.

Part: WINDOW TRIM — LOOSE (COCKPIT)

CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. FOUND LOOSE WINDOW TRIM. RESECURED TRIM, WINDOW OPERATED FREELY.

Part: EADI — DEFECTIVE (COCKPIT)

FIRST OFFICER'S EADI FAILED. DISPLAY UNIT WENT BLANK, ELECTRICAL SMELL/FUMES WERE NOTED IN THE COCKPIT. REPLACED FIRST OFFICER'S EADI IAW DC8 MM 34-21-0, OPS CHECKED GOOD.

Part: STRIKER — WORN (RT MLG DOOR)

GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF, WITH RT DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR TWICE AND LIGHT EXTINGUISHED. FOUND RIGHT MAIN GEAR DOOR STRIKER WORN. REPLACED STRIKER AND RAN GEAR IAW DC8 MM 32-31-4, OPS CHECKED GOOD.

Part: UPLATCH — LACK OR LUBE (RT MLG)

AFTER GEAR RETRACTION AND ALL GEAR INDICATION LIGHTS OUT, A FEW SECONDS LATER THE RED GEAR UNSAFE LIGHT CAME ON. CYCLED GEAR, LIGHTS WENT OUT. CLEANED AND LUBRICATED RIGHT GEAR DOOR UPLATCH ASSY. INSPECTED AND TESTED IAW DC8 MM 32-6.

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

GEAR UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. ASSOCIATED RT DOOR LIGHT ON FLIGHT ENGINEER PANEL WAS ALSO ILLUMINATED. LIGHTS EXTINGUISHED AFTER GEAR RECYCLE. FOUND LEFT GEAR DOOR MECHANISM OUT OF RIG. RIGGED AND CHECKED IAW DC8 MM 72-31-5.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STABILIZER L/E RIB CRACKED, STA ZFS 111.00 RT END. REPAIRED IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 660)

RT WING L/E AT STA XFS 660.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STABILIZER L/E RIB CRACKED STA ZFS 92.00 LT AFT END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STABILIZER L/E RIB CRACKED STA XFS 242.00 LT AFT END. REPAIRED SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STABILIZER L/E RIB CRACKED, STA ZRS 123.00 LT AFT END. REPAIRED IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STABILIZER L/E RIB CRACKED STA ZFS 104.00 LT AFT END. REPAIRED ANGLE IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 741.25)

RT WING L/E AT STA XFS 741.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 680)

FWD ACCY COMPT STA 680 RBL 24 THE SEAT TRACK SUPPORT FITTING IS CRACKED. FABRICATED REPLACEMENT FITTING IAW DWG 4645517 AND INSTALLED IAW SRM 51-1-29D.

Part: FITTING — CRACKED (CABIN)

FWD ACCY COMPT STA 68D BL 0 THE SEAT TRACK SUPPORT FITTING IS CRACKED. FABRICATED REPLACEMENT FITTING IAW DWG 4645517 AND INSTALLED IAW SRM 51-1-29D.

Part: FRAME — CORROSION (BS 1100)

FUSELAGE FRAME STA 1100 LONG 33R TO 34R FWD UPPER FLANGE, LWR SURFACE HAS EXFOLIATION CORROSION AT NUTPLATES.

Part: RIB — CRACKED (WS 778.75)

LT WING L/E RIB IS CRACKED XFS 778.75 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 810)

LT WING L/E RIB IS CRACKED AT XFS 810.00 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: FRAME — CRACKED (BS 66)

FWD ACCY COMP AT STA 66D BELOW STR 21R FRAME HAS 3 CRACK IN RADIUS. FABRICATED FRAME IAW SRM 53-2-0 AND DWG 3646688 AND INSTALLED IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 628.75)

LEFT WING L/E RIB IS CRACKED AT STA XFS 628.75 AFT UPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 616.25)

LT WING L/E RIB IS CRACKED AT XFS 616.25 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 610)

LT WING L/E RIB IS CRACKED AT XFS 610.00 AFT UPPER END. REPAIRED IAW SRM 52-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 828.75)

LT WING L/E RIB IS CRACKED AT STA XFS 828.75 AFT LWR END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: SPLICE — CRACKED (BS 440-460)

STR SPLICE CRACKED STA 440 TO 460 STR 30.L. REPLACED SPLICE IAW SRM 51-1-20D, 51-1-8 AND 51-1-11.

Part: RIB — CRACKED (WS 797.5)

LT WING L/E RIB IS CRACKED XFS 797.50 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 585)

LT WING L/E RIB IS CRACKED, XFS 585.00 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: STIFFENER — CRACKED (BS 782)

MAIN CABIN SUBFLOOR AT FS 782 RBL 46 STIFFENER FITTING IS CRACKED AT BOTTOM. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, 51-1-20D, AND DWG 3641126.

Part: SKIN — CORROSION (WS 786)

LT WING LEADING EDGE SKIN AT STP XFS 786 CORRODED BEYOND LIMITS. REPAIRED IAW SRM 57-2-1.

Part: FITTING — CORRODED (BS 1180)

BATH TUB FITTING EXFOLIATED OUT OF LIMITS FS 1180 L-35R TO 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 450)

LONGERON SPLICE FITTING HAS SEVERE CORROSION F/S 450 L-30L. REPAIRED LONGERON F/S 450 TO 465 IAW SRM 53-4-1, 51-1-20.

Part: RIB — CRACKED (WS 785)

LT WING L/E RIB IS CRACKED XFS 785.00 AFT UPPER END. REPAIRED IAW SRM 57-2-0 FIG 2, SRM 51-1-21, AND SRM 51-1-21.

Part: LONGERON — CORROSION (BS 8-25)

STR 30R STA 8 TO STA 25 HAS HEAVY CORROSION. FABRICATED REPLACEMENT LONGERON IAW DWG 3648667 AND INSTALLED IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 8)

LONGERON 30R END FITTING CORRODED FWD OF FRAME 8. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-1-0, 51-1-21, 51-1-20D AND DWG 4641704.

Part: INTERCOSTAL — CORRODED (BS 8-25)

FS 8 TO FS 25 STR 30R INTERCOSTAL ATTACH ANGLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 5615530.

Part: LONGERON — CORRODED (BS 70)

LONGERON 27R-CORRODED BEYOND LIMITS FS 8 TO FS 70. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3648666.

Part: RIB — CRACKED (WS 816.25)

LT WING L/E RIB IS CRACKED AT XFS 816.25 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 622.5)

LT WING L/E RIB IS CRACKED XFS 622.50 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 597.5)

LT WING L/E RIB IS CRACKED XFS 597.5 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 578.75)

LT WING L/E RIB IS CRACKED AT XFS 578.75 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 822.5)

RT WING L/E AT STA XFS 822.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-10, 51-1-20D AND 51-1-21.

Part: SKIN — CORROSION (WS 761)

LT WING LEADING EDGE SKIN AT STA XW 761 CORROSION REMOVAL BEYOND LIMITS. REPAIRED LT WING L/E STA XW 761 IAW SRM 57-2-1, SRM 51-1-8 AND SRM 51-1-20.

Part: RIB — CRACKED (WS 835)

LT WING L/E RIB IS CRACKED AT STA XFS 835.00 AFT LOWER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: CLIP — CRACKED (LT WING)

RT WING L/E STA XDLDI 6.225, THE UPPER INTERCOASTAL ATTACH CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-1-4 AND INSTALLED IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 697.5)

RT WING L/E AT STA XFS 697.5 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 603.75)

LT WING L/E RIB IS CRACKED XFS 603.75 AFT LWR END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 591.25)

LT WING L/E RIB IS CRACKED, XFS 591.25 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.

Part: RIB — CRACKED (WS 847.5)

RT WING L/E AT STA XFS 847.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 816.25)

LT WING L/E RIB AT STA 816.25 IS CRACKED AT THE AFT LOWER END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: FRAME — CRACKED (BS 1160)

STA 1160 FRAME IN C-3 PIT IS CRACKED IN 2 PLACES. STR 30R TO 32R AND STR 34R TO 35R. REPLACED FRAME IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 12)

FINGER DOUBLER CORRODED BEYOND LIMITS AT LONGERON 31R AT FS 12. FABRICATED FINGER DOUBLER IAW SRM 53-1-0 AND DWG 5613821. INSTALLED DOUBLER IAW SRM 51-1-21.

Part: INTERCOSTAL — CRACKED (BS 1520)

INTERCOSTAL FWD END CRACKED JUST AFT OF STA 1520 AT LONGERON 33L. REPAIRED INTERCOSTAL IAW SRM 53-2-0, 53-4-1, AND 51-1-8.

Part: RIB — CRACKED (WS 803.75)

RT WING L/E AT STA XFS 803.75 THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 766.25)

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

Part: RIB — CRACKED (WS 810)

RT WING L/E AT STA XFS 810.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 760)

RT WING L/E AT STA XFS 760.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 778.75)

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

Part: RIB — CRACKED (WS 816.25)

RT WING L/E AT STA XFS 816.250 THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 785)

RT WING L/E AT STA XFS 785.0 THE LOWER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 791.25)

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

Part: RIB — CRACKED (WS 835)

LT WING L/E RIB AT STA XFS 835.00 IS CRACKED AT THE AFT UPPER END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: RIB — CRACKED (WS 822.5)

LT WING L/E RIB AT STA XFS 822.50 IS CRACKED AT THE AFT LOWER END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1040)

STA 1040 TO 1060, STR 31L SPLICE FITTING IS CRACKED ON UPPER LEG FWD END. REPLACED FITTING AT STR 31L, STA 1040 TO 1060 IAW SRM 51-1-20.

Part: DRIVE LINK — CRACKED (RT TE FLAP)

DURING COMPLIANCE WITH AD 88-10-07 AND ASB A27-269, FOUND RIGHT INBOARD FLAP DRIVE LINK LUG CRACKED. REPLACED FLAP DRIVE LINK IAW DC-8 MM.

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

FIRST OFFICER'S CLEAR VIEW WINDOW HITS STUBS 61 PANEL WHEN TRYING TO OPEN WINDOW. RIGGED LOWER CLEAR VIEW WINDOW LOWER SIDE CHANNEL AND LUBED I/A/W DC-8 M.M. 56. OPS CHECKED GOOD.

Part: SEAT — MALFUNCTIONED (LT COCKPIT)

LEFT SIDE OF CAPTAIN'S SEAT DROPPED DOWN RIGHT AFTER ROTATION AND HAD TO BE LIFTED BACK UP TO GET IT TO LOCK IN POSITION. CAPTAIN'S SEAT OPS CHECKED GOOD IAW DC-8 MM.

Part: SWITCH — DEFECTIVE (LT MLG)

ON GEAR EXTENSION LEFT MAIN GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE. RECYCLED LANDING GEAR AND DOWNLOCK LIGHT DID NOT ILLUMINATE. DOWNLOCK LIGHT CAME ON DURING LANDING. CLEANED LEFT MAIN GEAR DOWNLOCK SWITCH CANNON PLUG AND REPLACED DOWNLOCK SWITCH. GEAR RETRACTION AND GEAR INDICATION CHECK WAS GOOD IAW DC-8 MM.

Part: BULB — FAILED (GEAR INDICATOR)

DURING LANDING GEAR EXTENSION, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. ABNORMAL LANDING GEAR PROCEDURES WERE COMPLETED. REPLACED LIGHT BULBS FOR THE LEFT MAIN LANDING GEAR INDICATOR AND THE BULBS ILLUMINATED DURING NEXT LANDING GEAR EXTENSION.

Part: SKIN — CRACKED (L 1 DOOR)

DURING 820AX C-CHECK INSPECTION, FOUND CRACK IN THE L-1 DOOR AFT LOWER CORNER SKIN AND DOUBLER. ALSO, A CRACK IN THE FORWARD LOWER CORNER. REPAIRED FORWARD ENTRY DOOR LOWER AFT CORNER AND SKIN IAW ABX REA D853-13085MR.

Part: SPAR — CRACKED (WS 69.5 LT)

DURING 820AX C-CHECK INSPECTION, FOUND LEFT HAND WING LOWER AT STATION 69.5, HOLES 2 THROUGH 5 UNDER SKI FITTING HAVE CRACK INDICATIONS BY HFEC INSPECTION. ALL CRACKS ARE IN SPAR AND ALL CRACKS ARE ON OUTBOARD SIDE OF HOLES. REPAIRED LEFT HAND LOWER REAR SPAR CAP AT HOLES 2 THROUGH 5 UNDER SKI FITTING AT STATION 69.5 IAW ABX REA D857-13087MR.

Part: TANK LANDING — CRACKED (WS 22.75)

DURING 820AX C-CHECK INSPECTION, FOUND RIGHT WING FUEL TANK LANDING AT PANEL 505F CRACKED. REPAIRED RIGHT WING ACCESS DOOR DOUBLER AT XRS=22.750 IAW ABX REA D857-13080MR.

Part: TANK LANDING — CRACKED (XRS 22.75)

DURING 820AX C-CHECK INSPECTION, FOUND LEFT WING FUEL TANK LANDING PANEL 505F CRACKED. REPAIRED LEFT WING TOP PANEL ACCESS DOOR DOUBLER AT XRS=22.750 IAW ABX REA D857-13018MR.

Part: SKIN — CORRODED (BS 1620-1640)

DURING 820AX C-CHECK INSPECTION, FOUND RIGHT HAND LONGERON 32 AND 33 AT STATION 1620 TO 1640 BULGED AND CORRODED BY SEALANT. REPAIRED CUT OUT IN FUSELAGE SKIN AND INNER DOUBLER AT FUSELAGE STATION 1620, LONGERON 32 AND 33, RIGHT HAND IAW ABX REA D853-13083MR.

Part: FRAME — CORRODED (BS 1040)

DURING 820AX C-CHECK INSPECTION, FOUND CORROSION ON FRAME AT FUSELAGE STATION 1040, FROM LONGERON 35R TO 33R. REPAIRED FRAME AT FUSELAGE STATION 1040, LONGERON 35R TO 33R IAW ABX REA D853-13088MR.

Part: RETRACT MECH — LACK OF LUBE (NLG)

AFTER TAKEOFF, THE LANDING GEAR RETRACTED NORMALLY, BUT THE UPLATCH CHECK WAS UNSATISFACTORY. THE LANDING GEAR WAS EXTENDED AND RETRACTED AGAIN AND A SQUEALING NOISE WAS HEARD FROM THE NOSE GEAR AREA. THE LANDING GEAR RETRACTED NORMALLY AND THE SECOND UPLATCH CHECK WAS GOOD. LUBRICATED THE NOSE LANDING GEAR AND PERFORMED SEVERAL RETRACTION CHECKS. NO NOISES WERE HEARD DURING THE RETRACTION CHECK AND THE UPLATCH CHECK WAS GOOD. THE LANDING GEAR RETRACTION CHECK WAS COMPLETED IAW DC8 MM, CHAPTER 32.

Part: EEL PWR PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHTS POWER PACK IAW DC-8 MM CHAPTER 33. OPS CHECKED GOOD.