N818UP

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT PER MM 33-50-01-2. OPS CHECK GOOD.

Part: SLIDE — MISINSTALLED (CABIN DOOR)

MAIN EXIT ESCAPE SLIDE IS IMPROPERLY LOCATED INSIDE HOUSING. PRESSURE CANNOT BE READ. REMOVED AND REPLACED MAIN EXIT ESCAPE SLIDE CONTAINER IAW MM 25-60-01-2. PRESSURE INDICATOR VISIBLE THROUGH WINDOW.

Part: FASTENER — FAULTY (ESCAPE ROPE)

INSPECTION TYPE:N/A CAPTAINS ESCAPE ROPE FELL OUT OF STOW LOCATION. CHECK FOR PROPER STOWAGE. REPLACED FASTENER FOR DOOR CLIP. REINSTALLED ROPE AND DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 FS 1360 L23R SPLICE FITTING IS CRACKED AT AFT END. REMOVED CRACKED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-3-0 AND SRM 51-1-20D, FABRICATED AND INSTALLED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-1-20D AND DWG 3755118.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 BATH TUB FITTING AT STA 1690 L32L IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING AT STA 1690 L32L IAW SRM 51-1-20D, AND DWG 4641326.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 STA 1690 L31R BATH TUB FITTING IS CRACKED. REMOVED BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-24, AND SRM 51-1-20D

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 DURING REMOVAL OF L-1 DOOR UPPER DOOR HINGE FITTING ASSY CRACKED. REMOVED AND REPLACED L-1 DOOR UPPER HINGE FITTING ASSY IAW SRM 51-1-2 0D, AND 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 C PIT STA 1228 BETWEEN L35R-36 BATH TUB FITTING CORRODED OUT OF LIMITS REMOVED BATH TUB FITTING AT STA 1228 BETWEEN L35R-36 IAW SRM 51-1-20D LOCATED AND DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1228 L35R-36 IAW SRM 51-1-20D, AND SRM 53-2-0 FIG 2D

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 C PIT STA 1220 BETWEEN L35R-36 BATH TUB FITTING INSIDE TORQUE BOX HAS EXFOLIATION CORROSION. REMOVED BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D, AND SRM 51-1-8

Part: SKIN — GOUGED (NR 3 MAIN TANK) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 PANEL LANDING AT ACCESS PNL 506C HAS DEEP GOUGE NR 3 MAIN TANK. TRIMMED OUT DAMAGED AREA OF LANDING IAW SRM 57-02-01 FIG 036. FABRICATED INSTALLED REPAIR FILLER, EXTERIOR DOUBLER, INTERIOR FILLER AND DOUBLER IAW SRM 57-02-01 FIG 036, 51-01-26-0, 51-3-2, AND SRM 51-1-8.

Part: FITTING — CRACKED (STRINGER) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 POSSIBLE CRACK ON STRINGER END FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 NR 1 ALT. REMOVED AND REPLACED FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 IAW SRM 51-1-20D AND 51-1-23.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 60 HOLE LONGERON 17L HAS PREVIOUS REPAIR, HOWEVER CRACK HAS EXTENDED PAST STOP DRILL. REMOVED DAMAGED L17L AT STA 1776 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON 17L AT STA 1766 IAW SRM 53-02-02-0, 51-3-02, AND SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 D-PIT STA 1340 BETWEEN L30R-31R FRAME CRACKED AND CORRODED. CUT OUT DAMAGED AREA STA 1340 FRAME BETWEEN L30R-L31R IAW 51-1-21D, FABRICATED AND INSTALLED REPAIR SPLICES AND FRAME SEGMENT AT STA 1340 BETWEEN L30R-L31R IAW SRM 53-02-00 FIG 2, AND DWG 52750825.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 3EA FITTINGS IN C-PIT DOOR TORQUE BOX CRACKED AT STA 1180-1200. REMOVED 3EA CRACKED TORQUE BOX FITTINGS IAW SRM 51-1-20D, INSTALLED NEW 3EA FITTINGS AT STA 1180-1200 C-PIT TORQUE BOX IAW SRM 51-1-24, 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 CRACK IN FITTING AT LT AFT OVERWING DOOR JAMB, UPPER AFT CORNER STA 824 L14L. REMOVED FITTING AT STA 824 L14L IAW SRM 51-3-0, AND 51-1-20D FABRICATED AND INSTALLED FITTING AT STA 824 L14R IAW DWG 4751643, AND SRM 51-3-2, AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK HEAVY CORROSION AT STA 70 LBL 24. REMOVED DAMAGED SEAT TRACK FROM STA 45-130 LBL 24 IAW SRM 51-03-00, FABRICATED AND INSTALLED SEAT TRACK SPLICE FROM STA 45-130 IAW SRM 53-02-03-0 FIG 014, SRM 51-3-0, AND DWG S-2440463.

Part: CUSP WEB — CORRODED (BS 370-470 L21R) · airframe 79,160 hrs · 27,128 cycles

RT FWD TYPE 1 DOOR LWR DOOR JAMB CUSP IS CORRODED. REMOVED CUSP AT STA 370-470 L21R IAW SRM 53-2-5 FIG 15, MILLED AND INSTALLED REPAIR CUSP AT STA 370 - 470 L21R IAW SRM 53-2-5 FIG 15.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

LEFT W/W TRAP FITTING CRACKED ALONG STA 902 FWD SIDE AT TOP VERTICAL BOLT THRU L24L. REMOVED AND REPLACED LEFT WHEEL WELL TRAP FITTING IAW SRM 51-1-20D, SRM 51-3-2, AND DC-8 AMM 51-03-01-0.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 A-PIT LEFT STA 325 LWR CUSP HAS VISIBLE CRACK IN RADIUS. CUT OUT SECTION OF CUSP AT STA 325 - 275 L21L IAW SRM 53-02-05-0. FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, -15 & -9 FRAME SPLICE DRILLED UP LEFT CUSP AND INSTALLED IAW SRM 53-04-01 FIG 40, SRM 51-1-4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

FOUND A/C COMPT RT SIDE L33R END FITTING CRACKED AT FS 8.00. REMOVED AND REPLACED END FITTING ON LONGERON END FITTING L33R IAW SRM 51-1-21, 51-01-27 AND 51-1-8.

Part: SPAR CAP — CRACKED (CENTER WING) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 WING CTR LOWER SPAR CAP CRACKED, LEFT W/W LBL 9-19 AND LBL 37-44. STOP DRILLED CRACKS AT WING LWR CTR SPAR CAP LBL 9-19 AND LBL 37-44. FABRICATED AND INSTALLED REPAIR PARTS AT WING CTR SPAR CAP LBL 9-19 AND LBL 37-44 IAW SRO8570009 REV A CONFIG 7013, UPS EODC8-5710- 24403-A, SAA EA 008-5710-01-A0199, BAC SERV REQ 1-192799561, AND FAA FORM 8100-9 ALL DATED 16 MAY 2006.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 (RT SIDE 17" ABOVE FLOOR PANEL). REMOVED, FAB`D AND REPLACED LONGERON FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 FRAME FITTING CRACKED AT FS 832, RT SIDE 19 INCHES ABOVE FLOOR PLANE. REMOVED FITTING AT STA 832 IAW SRM 51-1-20D, FABRICATED AND INSTALLED FRAME FITTING AT FS 832 IAW SRM 51-1-20D, AND DWG 3779874.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 19" ABOVE FLOOR PLANK RT SIDE. REMOVED FRAME TIE FITTING AT FS 860 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FRAME FITTING AT FS 860 IAW DWG 4750422, AND SRM 51-1-20D, AND SRM 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 670 L11R. REMOVED CRACKED FITTING AT STA 670 L11R IAW SRM 51-3-0, FABRICATED AND INSTALLED FITTING AT STA 670 L11R IAW DWG 5750540, SRM 51-3-2 AND SRM 51-1-20D.

Part: CUSP WEB — CORRODED (BS1310-1380 L21R) · airframe 79,160 hrs · 27,128 cycles

FUS CUSP CORRODED AT FS 1310 AND 1340 RT FWD AND AFT SIDES OF T-1 DOOR. REMOVED CUSP AT STA 1310-1380 RT FUSELAGE IAW 51-1-21, AND SRM 51-3-0, MILLED AND INSTALLED CUSP SPLICE REPAIR AT STA 1310-1380 IAW SRM 52-2-0 FIG 15.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 LONGERON TO FRAME FITTING CRACKED AT FS 855 19" ABOVE FLOOR PLANK RT SIDE. REMOVED CRACKED FITTING AT FS 855 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT FS 855 19" ABOVE FLOOR PLANK IAW DWG 3779498 AND SRM 51-1-20D, AND SRM 51-1-8.

Part: FITTING — CRACKED (FS 670 L6L) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 670 L6L. REMOVED END FITTING AT STA 670 L6L IAW SRM 51-1-20D, DRILLED UP AND INSTALLED END FITTING AT STA 670 L6L IAW SRM 51-03-02, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 FRAME ATTACH FITTING CRACKED AT STA 1180 L17R. REMOVED CRACKED FITTING AT FRAME STA 1180 L17R IAW SRM 51-1-20D, DRILLED REPLACEMENT FITTING AND INSTALLED AT STA 1180 L17R IAW SRM 51-1-20D.

Part: DOOR FRAME — CRACKED (FS 1400 L23L) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 HFEC AND VISUAL INSP DETECTED A .250 INCH CRACK ON THE D-PIT UPPER FWD DOOR JAMB CORNER. CUT OUT DAMAGED AREA ON C-PIT UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 021, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT THE C-PIT UPPER FWD DOOR JAMB CORNER (STA 1400 L23R) IAW SRM 53-2-0 FIG 21, AND T/R 53-140, 188.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,160 hrs · 27,128 cycles

INSPECTION TYPE:C1 COMPLY WITH MPI 17970 REGARDING PERM REPAIR TO DENT AFT OF LWR FWD PIT DOOR OPENING IAW ATTACHED WAN 1096454 AND MPI SUMMARY REPORT PAGE 1. REPAIRED DENT ON SKIN AFT SIDE OF -A- PIT DOOR CORNER IAW SAA EA 008-5320-01-A0189, DOUGLAS DWG 9754028, BOEING MESSAGE 1-189897625-2 DATED 05/15/06, AND FAA FORM 8100-9 DATED 05/15/06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERG EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD REF MM CH 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERG LIGHT BATTERY PACK. OPS CK GOOD.

Part: MOTOR — OVERHEATED (CABIN)

LAV FLUSH MOTOR OVERHEATED CAUSING SMOKE IN CABIN. REMOVED AND REPLACED LAV TIMER AND FLUSH MOTOR PER MM 20-10-03, 20-16-00-2. OPS CK NORMAL PER MM 38-30-00-1. NO LEAKS NOTED.

Part: CONTROL VALVE — CLOSED (LEFT)

BTB DUE TO SMOKE IN COCKPIT DURING PUSHBACK. SUSPECT LEFT PACK OPEN DUE TO DMI ON LEFT PACK. LEFT PACK SWITCH WAS IN THE OFF POSITION. FOUND LEFT PACK FLOW CONTROL VLV OPEN CLOSE VLV PER MEL ITEM 7 STEP 1 OPS CK LEFT AND RIGHT PACKS ON GROUND LEFT PACK IS CLOSED AND WIRED RT PACK IS OPERATIONAL.

Part: WINDOW — INOPERATIVE (COCKPIT)

CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED UPPER CATCH ON SLIDING WINDOW. OP CHECKS GOOD. WINDOW OPENS EASILY.

Part: WINDOW — STUCK (COCKPIT)

INSPECTION TYPE:N/A CAPT'S L2 WINDOW WILL NOT OPEN. UPPER WINDOW FRAME LOCK BAR STUCK WOULD NOT RELEASE. CLEANED & LUBRICATED MECHANISM. OPS CHECK NORMAL IAW MM 56-10-03-5.

Part: WINDOW — STIFF (COCKPIT)

INSPECTION TYPE:N/A CAPTAINS CLEARVIEW WINDOW HARD TO OPEN. OPENED AND CLOSED CAPTAIN'S SLIDING WINDOW THROUGH CYCLES. WINDOW OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. OK FOR CONTINUOUS SERVICE.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 783,702 hrs · 6,464 cycles

INSPECTION TYPE: C-2, FWD BAG PIT, L28L CORROSION BETWEEN FS 320 & 340. REMOVED CORR FROM L28L SIDE OF VERTICAL LEG AT FS 325, 330 & 335. ORIG THICKNESS VERTICAL LEG .063 IAW DAC DWG 9754913 MAT'L REMOVED .015, AMT REMAINING .048. OUT OF LIMITS. FAB -31 REPAIR ANGLE AND SHIM. ALODINED AND PRIMED. INSTALLED IAW DC8-SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, MARKER BEACON MOUNT AREA HAS HEAVY CORROSION (SKIN). BLEND CORROSION FOUND OUT OF LIMITS. REMOVED LT LOWER STRESS PANEL MAT ID 7075-T6, -.071, PO 434977.6 FOR DOUBLER IAW REO GO 9816. FAB REPAIR DOUBLERS IAW REO GO9816. ALODINED & PRIMED. INSTALLED DOUBLER IAW REO GO9816. RE-INSTALLED STRESS PANEL IAW DC8 SRM 51-3-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN FS 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071 PO 442960.1 FINGER DOUBLERS 7075-T6 PO 433440.5 DC8-SRM-53-2-1 FAB DOUBLER, FITTER, AND FINGER DOUBLER. ALODINED AND PRIMED. INSTALLED DOUBLER IAW SRM-53-2-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2, MAIN CABIN FS AT 995 SEAT TRACK -E- HAS CORROSION BETWEEN LUGS. REMOVED CORROSON FOUND TO BE OUT OF LIMITS. REMOVED FLOORBOARD 1000 TO 1060. CUT SEAT TRACK FROM STA 830 TO 1100 IAW EO DC8 5320517C DWG DC8 53B 003. MAT ID SEAT TRACK 2772660 PO SPO905314, & 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED. INSTALLED SEAT TRACK & 2 SPLICE FITTING, INSTALLED FLOORBOARD FROM STA 1000-1060 IAW DC8 SRM 51-3-0, 51-3-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 MAIN CABIN FS AT 995 SEAT TRACK "E" HAS CORROSION BETWEEN LUGS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT SEAT TRACK EO DC8-5320-5167C DWG DC8-53B-003. LOCATED, DRILL AND DEBURRED SEAT TRACK PLUS 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED SEAT TRACK. INSTALLED SEAT TRACK PLUS 2 SPLICE FITTING IAW DC8 SRM 51-3-0 AND 51-3-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 CORROSION ON FRAME AT FS 180 L35L-35R. REMOVED CORROSION, FOUND BLENDOUT BEYOND ALLOWABLE LIMITS IAW SRM 53-2-0 FIG 1F. FAB -9 DOUBLER, -11 FILLER IAW EO 11728-B AND UPS DWG 53A-011A. INSTALLED PARTS IAW EO AND DWG. ALODINED AND PRIMED IAW SRM-51-1-8.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 783,702 hrs · 6,464 cycles

INSPECTION TYPE: C-2, CORROSION ON FUSELAGE SKIN AND AROUND FASTENER HOLES FS 300-320 L29L. REMOVED CORROSION AND FOUND OUT OF LIMITS ORIG THICKNESS .063 THINNEST SPOT .034 720 IAW DC8 SRM 51-1-8 AND 53-2-0. FAB, ALODINED, PRIMED AND INSTALLED 31 REPAIR ANGLE IAW DC8 SRM 53-2-2 FIG 10, 51-1-8, AND 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 ALC, CORROSION AROUND FASTENERS, HOLE ON CABIN, FLOORBOARD PANEL FS 1040 RBL 45. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FLOORBOARD FROM 840 TO 1060 RT RBL 45, CUT SEAT TRACK FROM 870-1050 IAW EO DC853205167C, MAT ID SEAT TRACK AND 1 SPLICE FITTING P/N DC8-003-501 PO SPO94445 SEAT TRACK P/N 2772660 PO -O-. LOCATED, DRILLED, DEBURR & 2 SPLICES. ALODINED & PRIMED. INSTALLED SEAT TRACK. INSTALLED FLOORBOARD FROM 840-1060.

Part: DOUBLER — CORRODED (TAIL CONE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, AREA AROUND LOWER TAIL NAV LIGHT CORROSION & NUT PLATES BAD. REMOVED DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-21. LOCATED AND DRILLED NEW DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-21.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, MAIN CABIN L-2 DOOR TORQUE BOX AFT EDGE INT STRUCTURE SHEAR TIE GOUGED. BLENDED GOUGED AREA. ORIG MAT THICKNESS .080 DAC DWG 5616606. REMOVED INTERCOSTAL 8 & 9. REC'D PART FROM HEAT TREAT IN T6 CONDITION IAW DAC DWG 5616666 AND FAB NEW PART. ALODINED AND PRIMED IAW 51-1-8. OPEN WEB TORQUE BOX FOM. INSTALLED NEW PART ON L-2 TORQUE BOX IAW DC8 SRM 51-1-20-D AND 51-1-21.

Part: SPAR — CRACKED (RT WING) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2, RIGHT WING FWD SPAR AT XFS 520.00 HAS 500 HOLE WITH CRACK INDICATED. REPAIRED RIGHT WING FWD IAW DWG J060232-532 CONF AND REO GO9802

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2, FS 1400 D PIT EXTERIOR CUTOUT SKIN CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB REPAIRED DOUBLER IAW REO GO9822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D AND REO GO988.

Part: FITTING — CORRODED (L1766 30R) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, FWD OF AFT PRESSURE BULKHEAD AT BS 1766 LONGERON 30 SPLICE FITTING HAS CORROSION (DOT E 2880). REMOVED CRACKED FITTING. FOUND OUT OF LIMITS. REC'D LONGERON END FITTING P/N 4772398-1 PO 446277.2 IAW DWGS 4772398. LOCATED, DRILLED & DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-21. ALODINED & PRIMED IAW DC8 SRM 51-1-8.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION STA 1040-1080. NO MATERIAL LOSS IAW SRM 53-4-1 AND DAC DWG 9758507. FOUND WITHIN LIMITS. LONGERON SPLICE FOUND TO BE CRACKED. REC'D LOCATED AND DRILLED NEW LONGERON SPLICE. INTERCOSTAL STA 1040-1060 AND STRAP STA 1050 L35R IT IAW SRM 51-1-20D & 51-3-0

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2, AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35L HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. REMOVED LONGERON SPLICE CLIP AND INTERCOSTAL STA 1040-1060. LONGERON SPLICE FOUND TO BE CRACKED, REC'D LOCATED AND DRILLED NEW SPLICE. ALODINED AND PRIMED. INSTALLED NEW SPLICE FITTING AND REINSTALLED INTERCOSTAL AND CLIP STA 1040-1060 IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 FWD OR AFT PRESSURE BULKHEAD AT BS 1766 30L SPLICE FITTING HAS CORROSION. REMOVED FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS AND CRACKED. REC'D FITTING P/N 4772398-1 PO 446277. LOCATED AND DRILLED AND DEBURR FITTING INSTALLED FITTING P/N 4772398-1. ALL IAW SRM 53-2-0,51-1-21, AND 5 1-1-20D

Part: FITTING — CORRODED (FLOORBEAM) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, FLOORBEAM END FITTING AT STA 260 RT CUSP EXFOLIATED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-1- 24.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 AFT PIT LOWER BILGE FWD WALL AREA FRAME STA 1000 BETWEEN L27R AND 27L EXFOLIATED ON FWD SIDE IN NUMEROUS AREAS. REMOVED CORROSION OUT OF LIMITS. CUT OFF DAMAGED SECTION FROM L34L-L34R IAW DC8 SRM 53-2-0. LOCATED AND DRILLED FRAME SECTION AND REPAIRED SPLICES. LOCATED AND UP ANGLE. ALODINED AND PRIMED FRAME SECTION, SPLICES AND ANGLE. INSTALLED FRAME SECTION, ANGLE, REPAIR SPLICES, FRAME CAP, GASKETS AND BRACKETS IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2, FWD PIT STA 260-280, RBL, WL 0, CORROSION EMINATING, FROM BENEATH NUT PLATES AND NUT PLATES CORRODED FLOOR PLK B6014. REMOVED CORROSION FROM SEAT TRACK. FOUND TO BE OUT OF LIMITS MAT ID FOR SEAT TRACK IS 52772660 7075-T6 EXT PO SP0916641. MAT ID FOR SEAT TRACK SPLICE IS 7075-T6 (A&B PLATES) C PLATE IS 7075-T6 100 PO 4412585 FAB SPLICE A, B, C, 2 EACH, D 2 EACH, E 2 EACH, LOCATED & DRILLED HOLES REC'D UPS SPLICE PER EO DC853B003. ALODINED A-E SPLICES & PRIMED.

Part: CLIP — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 MAIN CABIN RT CUSP AT LWR FWD CORNER OF R2 DOOR (FS 1620) EXFOLIATION CORROSION. REMOVED CORROSION ON CLIP IAW DC8-SRM 51-1-8, OUT OF LIMITS. MAT ID AND FAB CUSP CLIP IAW DAC DWG 4773150 PERFORMED DYE PEN TEST. ALODINE AND PRIME CUSP CLIP IAW DC8-SRM 51-1-8 INSTALLED CLIP IAW SRM 51-1-20D.

Part: DOUBLER — GOUGED (T/E FLAP) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED DOUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER.

Part: STRUCTURE — BENT (RT TE FLAP) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE:C-2, RIGHT WING I/B FLAP I/B END (LIP) BENT AT AFT AREA, CHAFING FILLET PANEL 192 U. FABBED NEW WEB AND DOUBLER REPAIR IAW REO G09806.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,370 hrs · 26,464 cycles

INSPECTION TYPE: C-2 FUSELAGE SKIN CORRODED ALONG LONGERON 21R AT FS 8 AND FS55 EO DC8-5330-19540-A INSTALLED TEMP REPAIR, INSTALL PERMANENT REPAIR AT NEXT C- CHECK. GEN AND RECEIVED RFTS N818UP-1-20760. REMOVED FASTENERS STA-9 TO STA-70 L2OR -L24 RMVD TEMP REPAIR AND L22R STA-70 TO STA-8. REMOVED DAMAGED SECTION OF P/N 5613861-347 INNER DOUBLER, REMOVED CORRODED FROM INTERIOR OF SKIN P/N5613861 FOUND WITHIN LIMITS. FAB AND INSTALLED NEW SEC SKIN REPAIRED DOUBLER, FILLER AND FINGER DOUBLER REINSTALLED ALL FASTENERS. SRM53-2-1F7

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOPERATIVE, FOUND ON PREDEPARTURE CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS PER M/M 33-50-01. OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (COCKPIT)

OPS CK OF EMERGENCY LIGHTS FAILED TO LIGHT UP GLARESHIELD COCKPIT DOME, LAV / COURIER DOME, FWD ENTRANCE. REPLACED EMERGENCY LIGHT BATTERY PACK OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS FAILED OP CHECK. REMOVED AND REPLACED BATTERY PACK.

Part: FITTING — LOOSE (NR 3 ENGINE)

INSPECTION TYPE:N/A, AT 1 HOUR AND 35 MIN AFTER TAKEOFF, NR 3 ENGINE FLAMED OUT IN MODERATE TURBULENCE AND RAIN. FLAME-OUT OCCURRED AT 35,000 FEET AND MUCH .80. ATTEMPTED INFLIGHT ENGINE START AT 35,000, WAS UNSUCCESSFUL. PERFORMED FLAME-OUT INSP PER M/M 71-00-00, FOUND FUEL LEAKING AT MAIN FUEL INLET. TIGHTENED FITTING. RAN ENG AT VARIOUS PWR SETTINGS WITH NO PROBLEMS NOTED. A/C OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD IAW UPS DC8 MM 33-50-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 R2 UPPER AFT DOOR JAMB CORNER CRACKED 2ND OR 3RD LAYER AND INNER LAYER CRACKED. REPAIRED IAW EO DC8 5330-12075G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 SEAT TRACK E AT STA 1140 CORRODED AT POSITION-B. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3 AND UPS EO DC8-5320-5167C.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT PIT FS 1152 INTERCOSTAL FITTING AT L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, RECD LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 LONGERON 19R IS CRACKED AT BS 490 IS CRACKED AT BS 490 IN UPPER CARGO COMPT. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-2 FIG 10. FABBED NEW STRAPS IAW DC8 SRM 53- 2-2 FIG 10, INSTALLED LONGERON AND STRAPS IAW 51-1-11, 51-1-21, 51-1-20D. INSTALLED LONGERON SPLICE IAW DC8 SRM 51-1-20D, REINSTALLED SKIN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT PIT FS 1220 BANANA FITTING AT L32R L34R IS CRACKED. REMOVED AND REPLACED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 B-PIT DOOR AREA FWD JAMB CRACKED. FABBED AND HEAT TREATED IAW DC8 SRM 51-1-8 DAC DWG 3712791, DRILLED AND INSTALLED ANGLE IAW DC8 SRM 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 EMPENNAGE INTERIOR L17 RT CRACKED AT FS 1769. REPAIRED IAW DC8 SRM 53-2-3.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT PIT FS 1490 L32L SPLICE FITTING IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D & 51-1-21, INSTALLED IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 EMPENNAGE INTERIOR L17 RT CRACKED AT FS 1769. REPAIRED AREA IAW DC8 SRM 53-2-3.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT PIT FS 1490 L33L SPLICE FITTING IS CORRODED. REMOVED SPLICE FITTING RECD LOCATED DRILLED IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 BETWEEN LONG 34R - 35R Z-FITTING IS CORRODED. FOUND FITTING TO BE CRACKED UPON FURTHER INSPECTION. REMOVED FITTING IAW DC8 SRM 51-1-20D, FABBED REPAIR SPLICES IAW DC8 SRM 53-2-0, AND INSTALLED FITTING AND SPLICES IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 L1 LWR AFT DOOR JAMB CORNER CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE. FABBED FILLER AND DOUBLER IAW DC8 SRM 53-2-0 TR 53-128. INSTALLED FILLER AND DOUBLERS IAW DC8 SRM 53-2-0/TR 53-128.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1180 BETWEEN LONG 33R - 34R Z-FITTING IS CRACKED. REMOVED CORROSION PER DC8 SRM 51-1-8, FOUND TO EXCEED LIMITS PER DC8 SRM 53-2-0. REMOVED PLD FITTING PER DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING AND REPAIR ANGLES PER DC8 SRM 53-2-0 FIG G, INSTALLED FITTING AND ANGLES PER DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT FS 1190 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1180 T-BOLT BACK UP FITTING IS CRACKED. REMOVED AND INSTALLED FITTING IAW DC8 SRM 51-3-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED FITTING, LOCATED AND DRILLED EXISTING HOLES IAW DC8 SRM 51-3-2, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 BETWEEN L33R-L34R FITTING, Z-FITTING IS CORRODED AND HAS SHEARED FASTENERS. FOUND FITTING TO BE CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT FS 1170 T-BOLT BACK UP FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 & 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 L2 UPPER AFT DOOR JAMB CORNER HAS CRACK INDICATION JUST ABOVE DOOR STOP, INNER LAYER. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18 AND TR 53-134 AND 53-135.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1210 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED FITTING, LOCATED AND DRILLED EXISTING HOLES IAW DC8 SRM 51-3-2, INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1230 AT LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED IAW DC8 SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 FWD CARGO PIT AT FS 440-460 LONG 31R SPLICE FITTING IS CRACKED. REMOVED INTERCOSTAL AND SPLICE, PROCURED NEW SPLICE, LOCATED AND DRILLED HOLES, INSTALLED NEW SPLICE AND INSTALLED INTERCOSTAL IAW UPS DC8 SRM 51-1-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 IN MAIN CABIN BETWEEN STA 1140L & 1160L ABOVE HORIZONTAL SKIN SPLICE NEAR L16 FOUND SURFACE CORROSION ON LWR SIDE OF INTERCOSTAL. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-1-8 WITHIN LIMITS PER UPS DC 8 SRM 53-2-0, ALODINED IAW UPS DC8 SRM 51-1-8.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 CABIN (CARGO) SEAT TRACK AT RBL 25 BS 55 HAS BROKEN LOBES. BLENDED SEAT TRACK OUT OF LIMITS IAW DC8 SRM 53-2-3, FABBED SEAT TRACK IAW DC8 SRM 53-2-3 A&P IAW DC8 SRM 51-1-8. INSTALLED NEW TRACK AND FLOORBOARDS IAW DC8 SRM 51-3-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 MM 33-50-01, EMERGENCY EXIT LIGHTS CHECK NORMAL.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A NR 3 ENG FLAME-OUT IN CRUISE WITH NO KNOWN CAUSE. FL370 A/S M.80.OAT-54C 10.5 LBS ON FUEL. FOLLOWED FLAME-OUT CHECKLIST AND ENG RELIGHT WITH NO PROBLEMS. OPERATED NORMALLY REMINDER OF FLIGHT. CHECKED ENGINE IN ACCORDANCE M/M 71-00-00 PAGE 165. ALSO REMOVED AND REPLACED FUEL FILTER P/N 7588133, PACKING AND SEALS M-25988-1-156 1 EACH M25988-1-123 TWO EACH. ENGINE RUNUP AND CHECK FOR OPERATION AND LEAKS. FUEL FILTER REPLACED IN ACC 73-10-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,327 hrs · 25,716 cycles

INSPECTION TYPE:C13 LT EXT FUS SKIN HAS BULGES WITH SURFACE CORROSION L27L APPROX STA 1640-1670 AT FASTENERS. REMOVED CORROSION PER DC8 SRM 51-1-8, OUT OF LIMITS. FABBED REPAIR DOUBLERS, FINGER DOUBLERS, AND FILLER PER DC8 SRM 53-2-1 FIG 7. INSTALLED PER DC8 SRM 51-1-21.

Part: SMOKE DETECTOR — INOPERATIVE (CABIN)

CREW-PREFLIGHT MULTIPLE SMOKE DETECTORS INOP IN PIT 34. R&R BATT CLEARED DEFERRAL

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYSTEM)

INSPECTION TYPE:N/A ATB - ANTI-SKID INOP LIGHT ON APPROACH. R&R'D BAD ANTI-SKID CONTROL BOX. .

Part: COMPUTER — OUT OF ADJ (NR 4 ENGINE)

INSPECTION TYPE:N/A, PILOT REPORT NR 4 ENGINE WILL NOT MAKE T/O POWER. REMOVED AND REPLACED CDP P3 LINE AND ADJ MEC SPECIFIC GRAVITY.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, CENTER EMERGENCY LIGHT UNDER GLARESHIELD IS INOP. WRITTEN UP ON LP 409887, TRANSFERRED TO NRC.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LOWER CARGO STA 1280 RBL 60 FLOORBEAM ATTACH ANGLE CORRODED. CUT OUT DAMAGED FLANGE. MAT ID FOR REPLACEMENT TEE .125 7075-T6511 (PO NR 215124), MAT ID FOR REPAIR ANGLES .140 7075-T6511 (PO NR 317193) IAW STD-5310-001. FABBED REPLACEMENT TEE AND ANGLES IAW STD 5310-001. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR WITH HI-LOKS IAW STD 5310-001.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FS 1340 FROM LONG 35L - 35ER FRAME IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, MAT IS OUT OF LIMITS. FABRICATED STRAP, ANGLE AND DOUBLER IAW DC8 SRM 53-2-0, FIG 2 SHEET 6 & 7. ANGLE HEAT TREATED FROM 7075-0 TO 7075.T6 IAW TP-8 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED STRAP, ANGLE AND DOUBLER IAW DC8 SRM 51-1-20D & 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2 2 EE FITTING (P/N 3755842-503) HEAVILY CORRODED AT STA 1200 L32L - L33L. REMOVED FITTING CORRODED, RECEIVED NEW FITTING AND FABRICATED REPAIR ANGLES, ALODINED, PRIMED AND INSTALLED NEW FITTING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1220 - 1230 CROSS SLIDE AFT TORQUE BOX UPPER WEB CORRODED FROM LONG 33L - 34-R UNDERSIDE OF WEB. REMOVE FITTING, DOOR GUIDE AND GUIDE SPLICE. REMOVE CORROSION, ALODINE & PRIME. INSTALL NEW FITTING AND REINSTALL DOOR GUIDE AND GUIDE SPLICE.

Part: ATTACH ANGLE — CRACKED (CARGO BAY) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LOWER CARGO PIT CROSS SLIDE. DOOR RT FWD LWR ANGLE CRACKED. FABRICATE REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1200 BETWEEN L33R -L34R CROSS SLIDE DOOR 5TH FROM FWD LATCH FITTING CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED FITTING IAW DC 8 SRM 53-2-0 & 51-1-20D.

Part: SKIN — BENT (PAX DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, L-1 DOOR SKIN BENT LWR RT CORNER ACROSS BOTTOM OF DOOR. STRAIGHTENED DOOR SKIN EDGE IAW DC8 SRM 52-2-2. FOUND TO BE OUT OF LIMITS AND OIL-CANNED IAW DC8 SRM 52-2-2 PAGE 3. REMOVED LWR L-1 DOOR SEAL FOR ACCESS, ROUTED OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-0, 52-2-3 FIG 10 & 51-1-21. REINSTALLED LWR L-1 DOOR SEAL IAW DC8 SRM 51-3-0.

Part: ANGLE — CRACKED (WING BOX) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, ANGLE ON TOP OF WING BOX SKIN STA 847 - 857 RBL 27 IS CRACKED. REMOVED AND REPLACED ANGLE (P/N 4648710-2) IAW DC8 SRM 51-1-20D.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FWD LWR PIT AT STA 280 BETWEEN STR 35R TO 36R LWR PART OF TORQUE BOX STR 36R CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED Z-FITTING FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED LONGERON SECTION, SPLICES AND STRAP IAW DAC DWG 9754913, DC8 SRM 53-2-2, & REO-G07311. FABBED AND INSTALLED Z-FITTING, WEB DOUBLER IAW DC8 SRM 53-2-0, REO -G07311, & 51-1-20D, 51-1-21, 51-3-0, & 51-1-4.

Part: PAN — CRACKED (PAX DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FWD SERVICE DOOR AFT LWR DOOR PAN CRACKED. REMOVED AND REPLACED PAN IAW DAC DWG 5615700.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2 AFT LWR CARGO PIT AT FS 1270 LONG 31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FWD PIT STA 100 RT FLOORBEAM SUPPORT LOWER END CORRODED. REMOVED STANTION AT STA 100 RT IAW DC8 SRM 51-1-20D, OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW STANTION (P/N 3773077-510N), PO 256499, DRILLED STANTION IAW DAC 3773077. ALODINED AND PRIMED HOLES IAW DC8 SRM 51-1-8, INSTALLED STANTION IAW DC8 SRM 51-1-20D & 51-1-21.

Part: FINGER DOUBLER — CORRODED (CARGO BAY) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FWD PIT STA 207 BETWEEN L30R & L31R HAS CORROSION AROUND FINGER DOUBLER AND UNDER PRODUCTION SPLICE. REMOVED SPLICES L29R-31R, REMOVED FASTENER L29R - L33R FOR ACCESS IAW DC8 SRM 51-1-21A & 51-1-20D. REMOVED CORROSION OUT OF LIMITS, GEN & REC RFTS N818U P-17-20636. CUT OUT BAD SECTION, FAB NEW SECTION. INSTALLED FINGER DOUBLER, SPLICES AND FASTENERS, SEALED EDGE FINGER DOUBLER IAW DC8 SRM 51-1-8.

Part: FITTING — CORRODED (CABIN) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, RT CUSP AT STA 8, CUST TO FRAME FITTING HAS CORROSION. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-2 & 51-1-20D.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1190 BETWEEN L33R - 34R 3RD FROM FWD CROSS SLI DE DOOR LATCH FITTING CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC 8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, FITTING CORRODED AT FS 1200 L31L AFT LOWER CARGO COMPARTMENT. REMOVED CORRODED FITTING, LOCATE NEW FITTING AND DRILL EXISTING FAST ENER HOLES AND INSTALLED NEW FITTING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT PIT FS 1060 CORROSION ON LWR SURFACE OF UPPER FRAME FLANGE AT L36, L34L & L35L & ALSO ON FRAME CAP AT L36. REMOVED DAMAGED SECTION OF FRAME. FABBED REPAIR PARTS. ALODINED AND PRIMED REPAIR PARTS AND DAMAGED AREA. INSTALLED REPAIR IAW EO DC8-5310-1 1728 & UPS DWG DC8-53A-011.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LOWER CARGO PIT A FS 1195 BETWEEN L33R -L34R CROSS SLIDE DOOR 4TH FROM FWD LATCH FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED FITTING IAW DC8 SRM 51-1-20D & 53-2-0.

Part: WEB — CORRODED (CARGO DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LWR PIT AT FS 1180 BETWEEN LONG 33R - 34R DOORWAY WEB IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. GEN AND RECRFTS 818UP-14-20292 W/REO G07302. FAB DOUBLERS IAW REO G07302. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51-1-8 & INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, CABIN STA 1040 L21L AT ATTACH FITTING, FRAME, CRACKED AND CORRODED. REMOVED CORRODED FRAME SECTION AT FS 1040 TO L18L-L21L. FABRICATED NEW SECTION IAW DC8 SRM 53-0265. FABRICATED -29, -31, -33 & -35 REP AIR SPLICES IAW DC8 SRM 53-2-0. ALODINED AND PRIMED REPAIR SPLICES IAW DC8 SRM 51-1-8. INSTALLED FRAME AND SPLICES IAW DC8 SRM 53-2-0.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, CABIN STA 320 L21L, A FRAME TO CUSP ATTACH FITTING, CRACKED FRAME. REMOVED DAMAGED SECTION OF FRAME, INSTALLED NEW FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-0 FIG AND 51-7-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, MAIN CABIN STA 1540 AT L21L (CUSP) FRAME ATTACHMENT. REMOVED AND REPLACED FRAME SECTION IAW DC8 SRM 53-2-0, FIG 2.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, CABIN STA 409 L21L CUSP CORRODED AS MARKED. REMOVED CORROSION AND REPAIRED AREA IAW REO-G07299.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 75,760 hrs · 24,803 cycles

INSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1180 CROSSSLIDE DOOR WAY 2ND FROM FWD LATCH FITTING IS CORRODED AT LONG 33R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGE IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC 8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: BULB — SHORTED (NR 4 T HANDLE)

AT FL 350, NR 4 FIRE LIGHT INDICATION COMPLETED CHECKLIST. DECLARED EMERGENCY. DID NOT FIRE THE BOTTLE. INSPECTED NR 4 ENGINE LOOP AND DUCTING, NO DEFECTED NOTED. FOUND NR 4 T-HANDLE LIGHT BULB SHORTED TO GROUND. REPOSITIOND SAME, OPS CHK GOOD PER M-M 2610-00.

Part: DOUBLER — CORRODED (BS 1616)

INSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1616 BETWEEN L33 TO 32R ON INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DHC SK 818-913 AND SRM 51-1-8.

Part: FRAME — CORRODED (BS 1220)

INSPECTION TYPE-C, FS 1220 FRAME AND ANGLE CORRODED 33R TO 35R C-3 DOOR BATHTUB AREA. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK-818-903.

Part: DOUBLER — CORRODED (BS 1637)

INSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1637 BETWEEN L32 TO 33R INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DHC SK-818-916.

Part: SKIN — CRACKED (WS 610)

INSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 610 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 317.5)

INSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 317.5 IS CRACKED AT THE FRONT SPAR. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 578.75)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER AT STA XFS 578.75. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 616.25. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, THE D-PIT DOOR FRAME IS CRACKED IN 3 PLACES AT THE AFT UPPER CORNER. REPAIRED IAW SRM 52-4-1 AND 52-2-0.

Part: RIB — CRACKED (WS 597.5)

INSPECTION TYPE:C LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 597.5. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 610)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 610. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 735)

INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS .25 INCH CRACK BY ATTACH SCREW AT STA XFS 735. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE-C, 960 FITTING CRACKED ABOVE LONG 24R RT W/W. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 53-2-0.

Part: SKIN — CRACKED (WS 610)

INSPECTION TYPE:C LT WING L/E SKIN UPPER SURFACE CRACKED BY 2EA FASTENERS AT STA XFS 610.000. REPAIRED IAW SRM 57-2-1.

Part: PAN — CRACKED (LT TE FLAP)

INSPECTION TYPE-C, LT WING O/B SLOT O/B PAN CRACKED. REMOVED AND REPLACED SLOT PAN IAW SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 640)

INSPECTION TYPE-C, FS 640 BETWEEN LONG 26L AND 27L THE SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE IAW SRM 53-2-0 FIG 2A AND 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 660)

INSPECTION TYPE-C, FS 660 FRAME AT LONG 22R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW DWG 3646688 AND SRM 51-1-20D.

Part: SKIN — GOUGED (CARGO DOORWAY)

INSPECTION TYPE-C, THE FUSELAGE SKIN AT THE AFT LWR CORNER OF THE C-PIT DOOR IS GOUGED. REPAIRED IAW UPS EO DC8-5330-10808-A.

Part: ANGLE — CRACKED (VERT STAB)

INSPECTION TYPE-C, RT VERT STAB TO EMPENNAGE DRAG ANGLE CRACKED AND CORRODED IN HORIZONTAL LEG LOC APROX 11-14 AFT OF VERT STAB FRONT SPAR. REPAIRED IAW SRM 53-2-5.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED AT AFT O/B FASTENER AT STA XOLDI 6.225. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 379.0)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 379.0. STOP DRILLED CRACKED AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE-C, LT WING L/E VERTICAL ANGLE CRACKED AT LWR END AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.

Part: DOUBLER — CRACKED (WS 307)

INSPECTION TYPE-C, LT WING L/E LWR ACCESS PANEL DOUBLER CRACKED BETWEEN STA'S XFS 303 AND XFS 310.25. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.

Part: STARTER — FAILED (NR 1 ENGINE)

ENGINE NR 1 SHUTDOWN DUE TO OIL LOSS. REPLACED STARTER. FOUND STARTER SHEARED AND INTERNALLY FAILED. SHAFT AREA HAD DAMAGE ON STARTER.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, FOUND EMERGENCY LIGHT SWITCH IN THE ARMED POSITION WITH NO POWER ON A/C. BATT PACK DEPELETED. REMOVED AND REPLACED EMERGENCY BATT PACK PER MM33-50-01 PG 204, OPS CHECK GOOD.

Part: SKIN — DAMAGED (CARGO DOORWAY)

HOLE AND BULGE IN BELLY SKIN AT STRINGER 36 UNDER AND ABOUT 2 FT FWD OF NR 2 PIT DOOR. REPAIRED DAMAGED SKIN IAW EO DC8-5330-10030-A SEE EO FOR SIGN-OFFS.

Part: INTERCOSTAL — CRACKED (BS 1738)

INSPECTION TYPE-D, INTERCOSTAL CRACKED ON END ANGLE FS 1738 STR 27L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP ANGLE IAW SRM 51-1-21, 53-2-0 FIG 1B SHT 3, AND SRM 51-1-8.

Part: SPLICE PLATE — CRACKED (WS 421)

INSPECTION TYPE-D, FWD LWR SPAR TANG SPLICE PLATE CRACKED AT WING STA 421 LT WING JUST I/B NR 1 PYLON. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG SRO8570014.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING UPPER FUEL TANK ACCESS DOUBLER, PANEL 505F, LAND OB CORNER DOUBLER CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-1 FIG 36 AND DHC SK-818-082 (REF UPS ENRG FILE NR DC8-57- 0770.)

Part: FITTING — CRACKED (RT T1 DOOR)

INSPECTION TYPE-D, RT T1 DOOR LWR AFT FRAME FITTING IS CRACKED AND FWD END FITTING IS CRACKED. REMOVED EXISTING HINGE FITTINGS 2 EA ON LOWER FWD AND AFT FITTINGS, FABRICATED AND INSTALLED REPLACEMENT FITTINGS IAW SRM 51-1-21.

Part: DOUBLER — CRACKED (LT LE FLAP)

INSPECTION TYPE:D, LT WING L/E, INBD END OF THE OTBD SLOT, UPPER SKIN DOUBLER IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-3-3, AND 51-1-21.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:D, FITTING CRACKED AT FS 1140 FWD SIDE, THAT ATTACHES TO INTERCOSTAL AT LONGERON 33R. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:D, RT HORIZ STAB L/E RIB CRACKED 2 PLACES AT UPPER AFT END AND FWD CENTER AT FXS 116.25. STOP DRILLED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 55-2-0, 51-1-8.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:D, RT HORIZ STAB L/E AT FXS 47.5 UPPER AFT RIB IS CRACKED. REPAIRED IAW SRM 55-2-0, 51-1-8, 51-1-20.

Part: FITTING — CRACKED (NR 1 PYLON)

INSPECTION TYPE-D, AFT END UPPER FITTING NR 1 PYLON IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: INTERCOSTAL — CRACKED (BS 5)

INSPECTION TYPE-D, INTERCOSTAL CRACKED AT FS 5 RBL 46 COURIER AREA, CRACK IS APPROX 2.5 LONG. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 51-1-8 AND 51-1-20.

Part: DOUBLER — CORROSION (BS 5)

INSPECTION TYPE-D, FS 5 RBL 59 FINGER DOUBLER EXFOLIATED ON FWD END APPROX 5 BELOW C/B PANEL AT SUB FLOOR. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW SRM ADDEN 5350-7876, SRM 53-3-3, 51-1-21 AND DWG 5612298-269.

Part: SHEAR TIE — CRACKED (BS 1420)

INSPECTION TYPE-D, FS 1420 BETWEEN L-35L AND 36, SHEAR TIE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT IAW SRM 53-2-0 FIG 2B 51-1-8, 51-1-11, 51-1-21, AND 51-1-20.

Part: DOUBLER — CORRODED (BS 15)

INSPECTION TYPE:D, DOUBLER UNDER C/B PANEL I/B END FS 15 RBL 15 HAS EXFOLIATED CORROSION, AFTER PARTIAL CORROSION REMOVAL ON UPS N/R 611011 TO BE OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-01-0, AND 51-1-8.

Part: FRAME — CORRODED (BS 1420)

INSPECTION TYPE-D, C-4 CARGO FRAME CORRODED BEYOND LIMITS FS 1420 LONGERON 35R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FRAME PER SRM 53-4-1 FIG 1 AND SRM 51-1-20.

Part: SEAT TRACK — CORRODED (BS 990-1190)

INSPECTION TYPE-D, MAIN CABIN SEAT TRACK CORROSION BLEND OUT BEYOND LIMITS AT SEVERAL AREAS LBL 24 FS 990 TO 1350. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION FROM FS 990 TO 1190 IAW SRM ADDEN DC8-5230-5167-C, SRM 51-3-0, 53-7-3.

Part: SUPPORT — CORROSION (BS 1701)

INSPECTION TYPE-D, MAIN CABIN AFT SECTION-J FLOOR SUPPORT HAS CORROSION BEYOND LIMITS AT FS 1701 TO 1708 LBL 11 AND RBL 11. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORTS IAW SRM 51-1-21 AND 53-7-3 FIG 5.

Part: DOUBLER — CORRODED (BS 1450)

INSPECTION TYPE-D, LONGERON 31R, FS 1450 FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5615372 AND SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 1490)

INSPECTION TYPE-D, LONG 31L FS 1490 FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5615372 AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 1445)

INSPECTION TYPE:D, FS 1445 LONG 34R SUPPORT FITTING IS CORRODED. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-1-21.

Part: FITTING — CORRODED (BS 1140)

INSPECTION TYPE-D, C-3 CARGO COMPT AT FS 1140 LONG 35R FITTING CRACKED AND CORRODED AT FWD SIDE OF FRAME TO INTERCOSTAL. REMOVED AND REPLACED FITTING PER SRM 53-1-0 AND SRM 51-1-20.

Part: SHEAR TIE — CRACKED (BS 1445)

INSPECTION TYPE-D, FS 1445 L33R TO 34R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED IAW SRM 53-2-0 FIG 2B AND 51-1-20 D.

Part: FINGER DOUBLER — CORRODED (BS 1350)

INSPECTION TYPE:D, L 31R FS 1350 FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DOUGLAS DWG 5615372.

Part: TAIL SKID FTG — CORROSION (BS 1766)

INSPECTION TYPE-D, TAIL SKID FITTING INSIDE FUSELAGE AT FS 1766 HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-3-0, 51-3-1.

Part: FITTING — CORRODED (BS 270)

INSPECTION TYPE:D, STA 270 BETWEEN STR 35R-36 FITTING IS CORRODED (REF N/R 610832 ). REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2-0, 51-1-20D, 51-3-0, AND DWG 3755822.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:D, STA 70 END FITTING AT STRINGER 31R FWD SIDE TOP SPLICE FITTING HAS A CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 (REF N/R 610087 AND 610087 FOR INSTL).

Part: FRAME — CORRODED (BS 1380)

INSPECTION TYPE-D, BODY FRAME HAS EXFOLIATED CORROSION AT STA 1380 BETWEEN LONGERONS 3R AND 4R. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 7, 51-1-21 AND 51-1-20D.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING L/E VERTICAL ANGLE AT AFT OTBD CORNER OF SLOT HOUSING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-3-0 AND DAC DWG 5769859.

Part: INTERCOSTAL — CORROSION (BS 1120-1140)

INSPECTION TYPE-D, INTERCOSTAL AT LONG 33R FROM FS 1120 TO 1140 CORROSION BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 53-4-1, 51-1-21, AND 51-1-8.

Part: RIB — CRACKED (LT STUB WING)

INSPECTION TYPE-D, LT NR 2 ENG L/E STUB WING L/E RIB UPPER AFT END CRACKED, THIRD RIB FROM I/B END. FABRICATED AND INSTALLED ANGLE PER SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (BS 1738)

INSPECTION TYPE-D, EXTERIOR SKIN HAS FOUR CRACKS EXTRUDING FROM RIVETS ON LT SIDE OF FUSELAGE ABOVE LONGERON 28L AT FS 1738. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED FILLER, FINGER DOUBLER, AND EXTERNAL DOUBLER PER SRM 53-2-1 FIG 7 , AND INSTALLED REPAIR PARTS IAW SRM 51-1-8, 51-1-11, 51-1-21, AND 51-1-21A.

Part: BRACKET — CRACKED (BS 660)

INSPECTION TYPE-D, FWD ACCESSORY COMPT AFT DOOR TRACK FITTING CRACKED FS 660 L-36. REMOVED, FABRICATED AND INSTALLED BRACKET PER DWG 5755360 AND SRM 51-30-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-D, FS 680, RBL 48, BELOW FLOOR, SEAT TRACK SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 53-7-3, 51-1-20, AND DWG 5773275-58.

Part: SPAR CAP — CRACKED (LT WING)

INSPECTION TYPE-D HFEC INSP DETECTED A CRACK APPROXIMATELY .375 INCH LONG LOCATED AT SECOND FASTENER HOLE INBD OF NR 1 PYLON ON THE LT WING FRONT SPAR LOWER CAP. REEMED NR 10 HOLE TO .750 DIAMETER HOLE, COLD WORKED HOLE AND INSTALLED FREEZE PLUG, INSTALLED REPAIR PARTS IAW DWG JO60232, UPS EO DC8-5710-7761-A, AND DPS 270-2.

Part: STIFFENER — CRACKED (RT MLG WW)

INSPECTION TYPE:D, STIFFENER CRACKED ON UPPER END RT MLG W/W OB AT SPOILER CABLE BRACKET. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STIFFENER IAW SRM 53-8-3.

Part: CHORD — CORROSION (BS 70)

INSPECTION TYPE-D, FOUND AFT CHORD AT STA 70 STR 26, 27, 28 RT TO BE EXFOLIATED OUT OF LIMITS. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR SECTION OF CHORD IAW SRM 53-2-5 FIG 8C, SRM 51-1-20.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE: D. VERTICAL STABILIZER RIB AT STA. ZFS 104 IS CRACKED. REPAIRED IAW SRM 55-2-0 FIG 2 , SRM'S 51-1-21, AND 51-1-2D.

Part: SPLICE DOUBLER — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING L/E SECTION BTWN PYLONS AT STA XOLDI 6.225, SPLICE DOUBLER HAS SEVERAL FATIGUE CRACKS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5769891 AND SRM 57-3-3.

Part: FITTING — CORRODED (BS 70-80)

INSPECTION TYPE-D, STA 70 TO 80 LONG 31L LOWER END FITTNG IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING ON AFT SIDE OF FRAME IAW SRM 51-1-21 AND DHC SK-818-839 (REF UPS ENRG FILE NR DC8-53- 1777).

Part: FITTING — CORRODED (BS 70-80)

INSPECTION TYPE:D, STA 70-80 LONGERON 29L END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 53-1-0.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE-D, VERT STAB L/E AT STA ZFS 62 HAS A RIB END CRACKED. STOP DRILLED, FABRICATED AND INSTALLED REPAIR IAW SRM 55-2-0 FIG 2.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE:D, RT WING L/E O/B OF NR 4 AFT FILL VALVE, SLOT ISLAND MOUNT ANGLE IS CRACKED PAST STOP DRILL. REMOVED, FABRICATED, AND REPLACED IAW SRM 53-1-0.

Part: INTERCOSTAL — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING L/E SECTION BETWEEN PYLONS, BLEED AIR DUCT SUPPORT INTERCOSTAL O/B OF O/B UNDER-WING FUELING ADAPTER IS CRACKED ON THE O/B AFT END. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED IAW SRM 57-2-0, 51-1-21, 51-1-8, AND 51-1-29D.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING L/E SECTION BETWEEN PYLONS HAS ONE UPPER RIB CRACKED AT THE AFT END 48 O/B OF SLOT ACTUATORS. REPAIRED IAW SRM 57-2-0 AND 51-1-21.

Part: FLOORBEAM — CORRODED (BS 1700-1723)

INSPECTION TYPE-D, FLOORBEAMS AND STRUCTURE PLATE BETWEEN FS 1700 AND 1723 LT SIDE HAS CORROSION ON UPPER AND LOWER SURFACES. REMOVED PLATE, FABRICATED, AND INSTALLED REPLACEMENT PLATE IAW SRM 51-1-0 AND 51-1-20. REMOVAL OF LIGHT SURFACE CORROSION WAS WITHIN LIMITS ON THE REST OF SURFACE REF SRM 51-1-8, 53-2-0 FIG 1.

Part: FITTING — CORRODED (BS 79-80)

INSPECTION TYPE:D, STA 70-80 LONGERON 31R LWR END FITTING IS CORRODED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21 AND 53-1-0.

Part: INTERCOSTAL — GOUGED (BS 1300-1320)

INSPECTION TYPE-D, INTERCOSTAL BETWEEN FS 1300 TO 1320 HAS GOUGES BEYOND LIMITS LBL 48. FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B.

Part: SEAT TRACK — CORRODED (BS 980-1540)

INSPECTION TYPE-D, SEAT TRACK CORRODED FROM FS 980 TO 1540 RBL 59. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK FROM FS 980 TO 1580 IAW SRM ADDEN DC8-5320-5167, SRM 53-3-0 AND 51-1-21. ALSO, WORK DONE ON N/R 610139.

Part: CARGO TRACK — CORRODED (BS 1220)

INSPECTION TYPE-D, AFT LOWER CARGO SEAT TRACK AT LBL 26 STA 1220 IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM ADDEN DC8-5320-5167-C, SRM 51-3-0 AND 53-7-3 FROM FS 1190 TO 1350.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED AT PNEUMATIC DUCT ATTACH POINT JUST OB OF NR 2 ENGINE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 52-2-0, 51-1-8, 57-2-0 FIG 2, 51-1-20D.

Part: STRINGER — CORROSION (BS 1230-1240)

INSPECTION TYPE:D, CORROSION ON STR 29R BETWEEN STA 1230-1240. REMOVED, FABRICATED, AND INSTALLED NEW SPLICE IAW SRM 51-1-20 AND SRM 53-2-2 FIG 10.

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, STA 1260 TO 1280 STR 3L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20.

Part: CLIP — CRACKED (BS 1240)

INSPECTION TYPE:D, FRAME ATTACH CLIP, AT FS 1240 L-35L, IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 57-1-0 AND 51-1-20.

Part: SEAT TRACK — CORRODED (BS 1000-1020)

INSPECTION TYPE:D, AFT LWR CARGO SEAT TRACK AT BL 0 HAS SEVERAL CORRODED FASTENER HOLES, BETWEEN STA 1000 AND 1020. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-3-0, 53-7-3, 53-2-3.

Part: CLIP — CRACKED (BS 1240)

INSPECTION TYPE:D, FRAME ATTACH CLIP AT STA 1240 CRACKED L-35R. REMOVED AND REPLACED CLIP IAW SRM 51-1-20 AND 53-1-0.

Part: CLIP — CRACKED (BS 1260)

INSPECTION TYPE-D, BOTH INTERCOSTAL ATTACH CLIPS ARE CRACKED AT STA 1260 ABOVE LONGERON 33R. REMOVED CLIPS, FABRICATED AND INSTALLED REPLACEMENT CLIPS IAW SRM 51-1-20D AND DWG 4758514.

Part: INTERCOSTAL — CRACKED (BS 1240)

INSPECTION TYPE-D, RT INTERCOSTAL AT STR 33R FS 1240 HAS AFT FRAME CLIP CRACKED. REMOVED, FABRICATED, AND INSTALLED CLIP PER DWG 4758514 AND SRM 53-2-0.

Part: SKIN — CORRODED (BS 1400-1420)

INSPECTION TYPE-D, CORROSION BETWEEN STRINGERS 36 TO 35R AT FS 1400 TO 1420 LOWER BILGE. REMOVED AND REPLACED BELLY SKIN P/N 5615372-71N. REMOVED, FABRICATED AND INSTALLED INTERNAL DOUBLERS 2 EA P/N 5616674-115 AND 1EA -7 PLATE IAW DWG 5616674, SRM 51-1-21, 51-1-21D, 51-1-11, AND 51-1-8. NEW SKIN FROM FS 1350 TO 1490.

Part: SUPPORT — CORRODED (BS 1440-1540)

INSPECTION TYPE-D, RT FLOOR SUPPORT STRUCTURE FROM FS 1440 TO 1540 CORRODED, LWR BILGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT IAW SRM 53-1-0, 51-9-0, 51-1-20, AND DWG 5753284.

Part: RIB — CRACKED (WS 747)

INSPECTION TYPE: D. RIGHT WING L/E AT STA XFS 747, THE UPPER L/E RIB IS CRACKED AT AFT END. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2 SHT 2.

Part: SUPPORT — CORRODED (BS 6)

INSPECTION TYPE-D, STA 6 RBL 27 FLOOR SUPPORT T-ANGLE HAS HEAVY CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-2-0 FIG 1B, 51-1-20, AND 51-3-0.

Part: INTERCOSTAL — CRACKED (SERVICE DOOR)

INSPECTION TYPE-D, FWD SERVICE DOOR, TWO LOWER CENTER DOOR VERT INTERCOSTALS ARE CRUSHED AND CRACKED. REMOVED AND REPLACED INTERCOSTALS IAW SRM 52-3-1, 51-1-21, AND 51-1-20D.

Part: RIB — CRACKED (WS 804)

INSPECTION TYPE-D, RT WING L/E AT STA XFS 804.00 TO THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-D, STA 680 LBL 24, SEAT TRACK SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED, AND INSTALLED ANGLE IAW SRM 51-1-21, 53-7-3, AND 51-1-20.

Part: FITTING — CRACKED (BS 834)

INSPECTION TYPE-D, INTERCOSTAL SUPPORT FITTING IS CRACKED AT FS 834 RBL 66.8 BELOW FLOOR. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 AND 53-1-00.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:D, RT HORZ STAB L/E AT STA FXS 53.75 AFT END OF RIB CRACKED. REPAIRED IAW SRM 55-2-0 FIG 2 AND SRM 55-3-1.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-D, STA 680 RBL 24, BELOW FLOOR SEAT TRACK SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-21, 53-1-3, AND 51-1-21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYP-D, STA 680 LBL44 SEAT TRACK SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 53-7-3.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-D, STA 680 AT BL 0 SEAT TRACK SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED AND INSTALLED SUPPORT FITTING IAW SRM 51-1-21, 53-7-3, AND 51-1-20.

Part: RIB — CRACKED (LT HORIZ STAB)

INSPECTION TYPE-D, LT HORZ STAB L/E RIB AT STA FXS 1725 IS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED L/E RIB REPAIR IAW SRM 55-2-0, 55-3-1, AND 51-01-20.

Part: STRINGER — CORRODED (BS 100)

INSPECTION TYPE-D, STRINGER 25R HAS EXFOLIATION CORROSION AT FS 100. CORROSION IS FWD AND AFT OF FRAME. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW SRM 51-1-21, 53-4-1 AND 51-1-20D.

Part: FITTING — CRACKED (BS 902-920)

INSPECTION TYPE-D, LONGERON SPLICE FITTING CRACKED AT LONGERON 1 BETWEEN F/S 902-920. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 AND 53-1-0.

Part: FITTING — CRACKED (BS 822-834)

INSPECTION TYPE-D, AFT INTERCOSTAL SUPPORT FITTING CRACKED BETWEEN STA 822 TO 834 LONG 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20, DAC DWG NR 3779874, AND SRM 53-1-0.

Part: SEAT TRACK — CORROSION (BS 55)

INSPECTION TYPE-D, STA 55 RBL 44 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED SECTION OF TRACK FS 50 TO 130 IAW SRM 53-2-3 FIG 6, AND 51-01-20.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE-D, LT HORZ STAB L/E RIB AT STA FXS 47.5 IS CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0, 51-01-20, AND 51-1-8.

Part: FITTING — CORRODED (BS 70-80)

INSPECTION TYPE:D, INTERCOSTAL AT S-27R BETWEEN FS 70-80 IS CORRODED ON UPPER AND LOWER SIDES. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-21, 51-1-20D (INTERCOSTAL WITHIN LIMITS).

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:D, STA 680 STR 11R-END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 53-01-0.

Part: FITTING — CRACKED (BS 798)

INSPECTION TYPE: D. AFT INTERCOSTAL SUPPORT FITTING CRACKED AT STA 798 LONGERON 17L. REMOVED AND REPLACED FITTING PER SRM 51-1-21.

Part: CHORD — CORROSION (BS 70)

INSPECTION TYPE-D, FS 70 CHORD ANGLE BETWEEN STR 30R AND 34R HAS HEAVY CORROSION ON FWD END. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR SECTION IAW SRM 53-2-5 FIG 8C, SRM 51-1-20.

Part: INTERCOSTAL — CRACKED (L1 DOOR)

INSPECTION TYPE:D, INTERCOSTAL CRACKED ABOVE AND BEHIND FWD ENTRY DOOR BAYONET. REMOVED DAMAGED INTERCOSTAL PER SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-1-0 AND 51-1-21.

Part: WEB — CRACKED (BS 90)

INSPECTION TYPE-D, MAIN CABIN FS 90 LBL 66 WEB MEMBRANE CUSP AREA CRACKED BEYOND LIMITS. TEMPORARY REPAIR INSTALLED. REMOVED EXISTING REPAIR, REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-5330-2159-B.

Part: CLIP — CRACKED (BS 1766)

INSPECTION TYPE-D, INTERCOSTAL CLIP AT FS 1766 LONGERON 6L IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT PART IAW SRM 51-1-0, 51-1-20, 51-9-0, 51-1-29D, AND 51-1-11.

Part: STABILIZER — CRACKED (LT HORIZ STAB)

ON PRED. CHK FOUND 2 DENTS ON LEFT STAB L/E. DENT THAT IS APPROX. 46 INCHES OUT FROM STAB L/E ROOT AND HAS 2.6258 INCH CRACK. DENT INBOARD OF PREVIOUS MENTIONED IS 6 INCHES BY 2.50 INCHES. REMOVED DAMAGED L/E SKIN PER SRM 55-2-1. FABRICATED DOUBLERS FROM 7075-T6 050, INSTALLED INBOARD DOUBLER DC8-5510-7652A AND SRM 55-2-1.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON PREDEPARTURE, EMERGENCY LIGHT FAILED. REPLACED BATTERY PACK.

Part: CONTAINER — CRACKED (ESCAPE SLIDE)

CREW REPORTED, ESCAPE SLIDE NEEDS TO BE REPACKED THE OUTER COATING CRACKED. REPACKED SLIDE IN CONTAINER, CONTAINER ASSY ON ORDER.

Part: FITTING — CRACKED (FUSELAGE)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND B/T FITTING HAS HEAVY CORROSION AND CRACKED AT STA. 270, L33A-33BR. REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE BEAM — CORRODED (HORIZ STAB)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND THE LT UPPER SPLICE BEAM AND THE UPPER AND LOWER SHEAR FITTINGS CORRODED AT APPROX RUDDER STA 212.87-220.870. MAINTENANCE REMOVED AND REPLACED SPLICE ASSY AND UPPER AND LOWER SHEAR FITTINGS IAW BOEING DRAWING 65-16788 AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 355)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND STR 20 BS 355 TO BE CORRODED, RT. MAINTENANCE CLEANED CORROSION, FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-10-3 AND 53-10-1.

Part: FLOOR BEAM — CORRODED (CARGO BAY)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION FORWARD CARGO BAY IN NUTPLATE HOLES IN THE LOWER FLANGE OF THE S40 FLOOR BEAM LBL 17-RBL 58 WL 201. MAINTENANCE BLENDED CORROSION AND FOUND OUT OF LIMITS, CUT FLOOR BEAM LOWER FLANGE AND REPAIRED IAW E.O. B727-5310-7452-A.

Part: SKIN — CORRODED (BS 190-450)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELLY SKIN PANEL AT FS 190-450. MAINTENANCE REPLACED BELLY SKIN PANEL PER SRM 51-1-20D AND SRM 51-1-21.

Part: FRAME — CORRODED (FS 260)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELTFRAME, FS 260 BETWEEN LONGERONS 35L-35R. REPAIRED IAW DC8-5310-7474A.

Part: RIB — CRACKED (RUDDER)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BOTH HOLES IN UPPER RUDDER, UPPER THRUST LINK SUPPORT RIB CRACKED WHERE THE BOLTS GO THROUGH THE SPLICE BEAM. MAINTENANCE REMOVED AND REPLACED THE RIB ASSY IAW SRM 51-30-2 AND MM 27-20-21, 27-20-101, AND 27-20-141.

Part: STRAP — CORRODED (BS 504-658)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AROUND NUTPLATE HOLES ON THE BL ZERO STAB. STRAP. STA 504-658, LBL 2-RBL 2 WL 201. MAINTENANCE REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED THE DAMAGED PARTS, FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-10-1 AD E.O. 95-30-22.

Part: PULLEY QUADRANT — CORRODED (NLG DOOR)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND NOSE DOOR PULLY QUADRANT CORRODED. MAINTENANCE REMOVED AND REPLACED WITH NEW QUADRANT IAW MM 32-33-51, 32-31-51 AND 32-22-01.

Part: STRINGER — CORRODED (BS 350-360)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WEB CONNECTING BS 350 AND 360, WL 198 (STRINGER 19), LBL 60. MAINTENANCE REMOVED CORROSION FOUND OUT OF LIMITS, CUT OUT THE DAMAGED AREA, FABRICATED NEW WEB AND STIFFENERS AND INSTALLED IAW SRM 51-30-2, 53-10-1.

Part: FRAME — CORRODED (BS 1660)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 1660 BELT FRAME LOWER LIP AT LONGERON 36 HAS INTERGRANULAR CORROSION. MAINTENANCE REPLACED FRAME SECTION IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 260-300)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERONS 34L FS 260-300 L34RT BOTH CRACKED AND HEAVILY CORRODED. MAINTENANCE REPLACED LONGERON SECTIONS IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 230-320)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION AT FINGER DOUBLER FS 220-320, LONGERON 31L. MAINTENANCE REPLACED DOUBLER SECTION STA. 210-350 IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (BS 488)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT AILERON ACCESS PANEL NR 5H DOUBLER CRACKED AT STA. 488. REPAIRED IAW UPS E.O. DC8-5750-7469-A.

Part: DOUBLER — CORRODED (BS 190-200)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER, FS 190-200, LONGERON 31L. MAINTENANCE REPLACED DOUBLER SECTION IAW SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — CORRODED (BS 220-260)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT INNER SKIN DOUBLER AT FS 220-260 LONGERON 35L-30R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (BS 870)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION (53-224-05.00-01) BS 870 BODY FORGING WL 191 RBL 71 (MARKED). MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-30-1, AND E.O. B727-5310-7454-A.

Part: DOUBLER — CORRODED (BS 200-220)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON ANTENNA DOUBLER BETWEEN FS 200-220, LONGERONS 35L-35R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — CORRODED (BS 260-360)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INNER DOUBLER AT STA 260-360, LONGERONS 35L-38A. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — CORRODED (BS 360-400)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT INNER DOUBLER, FS 360-400, LONGERON 35L-30R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CORRODED (WING CTR SECTION)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF UPPER FUEL CELL SKIN BS 746-770 RBL 25-45 WL 203 (MARKED). MAINTENANCE REPAIRED WING CENTER SECTION UPPER FUEL CELL SKIN PER UPS E.O. 727-57-1653.

Part: FITTING — CRACKED (FS 960)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 960. REPLACED FITTING PER SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 380)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 380 BELT FRAME FLOOR SUPPORT ANGLE CRACKED AT LONGERON 33R. WELDED CRACK PER UPS 10225.

Part: LONGERON — CRACKED (FS 220-320)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 36, LT AND RT SIDES CRACKED AT FS 220 TO 320. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: SKIN — CRACKED (FS 335)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND THE AFT LOWER CORNER OF THE A-CROSS SLIDE DOOR CUTOUT HAS CRACK DAMAGE. REPAIRED PER UPS EO DC8-5310-7439-A.

Part: FITTING — CRACKED (FS 879)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 879. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 940)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 940. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 920)

WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 920. REPLACED FITTING PER SRM 51-1-20D.

Part: J ANGLE — CRACKED (AFT PRESS BULKHD)

MAINTENANCE REPORTED 'J' ANGLE CRACKED ON AFT PRESS BULKHEAD. REPAIRED PER UPS EO DC8-5310-6746.

Part: CONNECTOR — SHORTED (FLIGHT DECK)

PILOT REPORTED, DESENDING THROUGH 18,000 FT, GOT RED FLAG ON FIRST OFFICER'S ALTIMETER, STARTED TO SMELL ELECTRICAL SMOKE. TURNED OFF RIGHT EFIS MASTER, SMOKED STOPPED. REMOVED CANNON PLUG AND CLEANED MOISTURE ON IT AND REMOVED AND REPLACED FIRST OFFICERS ALTIMETER. GROUND CK OK.