N750UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS. OPS CKS GOOD.

Part: FUSE — BLOWN (COCKPIT)

SMOKE & ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACK GROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE-5 AMP. OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.

Part: FUSE — BLOWN (ENGINEERS PANEL)

INSPECTION TYPE:N/A SMOKE AND ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACKGROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE (5AMP) OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.

Part: GROUND WIRE — SHORTED (SMOKE DETECTOR)

CARGO SMOKE LIGHT ILLUMINATED - ALL POSITIONS. T/S SYS FOUND & REPAIRED BAD GROUND WIRE 8M OHMS ON SMOKE DETECTOR UNIT NR 1. FOUND & REPAIRED BAD GND WIRE ON SDU NR 3. FOUND AND REPAIRED BAD GNU D WIRE ON SDU NR 5. ALL OTHER SDU GND WIRES CKD GOOD PER WDM 26-11-01 PG 1. SYS OPS OK PER MM 26-10-07-2

Part: DOUBLER — CRACKED (NLG DOOR) · airframe 68,230 hrs · 28,358 cycles

NOSE SECTION FUSELAGE SKIN HAS 3/8" CRACK AT AFT HINGE ACCESS DOOR. REMOVED CRACKED DOUBLER AT NOSE EXTERIOR AFT SKIN IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG56126127 AND SRM 51-1-20E.

Part: FINGER DOUBLER — CORRODED (FS-67 TO -80) · airframe 68,230 hrs · 28,358 cycles

COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEAR HEAD RIVETS AND CORRODED AT STA -67 TO -80 RBL 60. REMOVED FINGER DOUBLER IAW SRM 51-1-21 AND 51-3-0. REMOVED CORROSION FROM WEB IAW SRM 51-1-8, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER AT STA -67 TO -80 RBL 60 IAW SRM 53-03-01 PG1 FIG 007, 51-1-8, AND SRM 51-1-20D.

Part: SPAR — CRACKED (RT WING) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 RIGHT KEEL BEAM AT FS 857 2.5 INCH CRACK ON LWR SPAR. STOP DRILLED CRACK AT XCW 4.0 IAW SRM 51-1-20D NDT HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED FILLERS VERTICAL FILLERS AND -136 ANGLE AND STIFFENERS AND INSTALLED REPAIR PARTS IAW SAA SK 750-847317, UPS ENG FILE NUMBER DC8-57-20134 AND BOEING MESSAGE 1-116364542-2.

Part: FITTING — CORRODED (FS210 L7R) · airframe 68,230 hrs · 28,358 cycles

HEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FRAME — CRACKED (FS 1890) · airframe 68,230 hrs · 28,358 cycles

FRAME ON 62 DOOR OPENING IS CRACKED INSIDE OPENING RT SIDE. FAB`D DOUBLER AND REPAIRED IAW SRM 53-05-01 AND 51-1-21A.

Part: FITTING — CRACKED (FS 280 RBL50) · airframe 68,230 hrs · 28,358 cycles

STA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS -8 L33L) · airframe 68,230 hrs · 28,358 cycles

FS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21.

Part: FLOORBEAM — CRACKED (FS 55 LBL 12) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 FLOORBEAM CRACKED AT FS 55 LBL 12. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 TEMP REV 53-152, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 TEMP REV 53-152 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1768 L17R) · airframe 68,230 hrs · 28,358 cycles

END FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D.

Part: SPLICE — CRACKED (FS 450 L33R) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 CRACKED SPLICE ANGLE INSIDE CHANNEL AT FS 450 L33R. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-21D, MACHINED AND INSTALLED LONGERON SPLICE AT STA 450 L33R IAW DWG 3750330.

Part: SPLICE — CRACKED (FS 450 L31R) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 SPLICE FITTING AT FS 450 L31R IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31R IAW DWG 5754814 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LT AILERON) · airframe 68,230 hrs · 28,358 cycles

LT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR DOUBLER IAW 57-02-00-0 AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 AND 57-08-00-0. REPAIR DOUBLER CENTERED AT AILERON HINGE LINE "D" VALUE EQUALS ZERO THEREFORE THERE IS NO NET CHANGE IN BALANCE IAW SRM 51-04-08 FIG 59R.

Part: RIB — CRACKED (XFS 766.250) · airframe 68,230 hrs · 28,358 cycles

LT LE UPPER RIB CRACKED AT XFS 766.250. FAB`D DOUBLER AND REPAIRED IAW DWG 5769470 AND SRM57-02-00 FIG 2.

Part: FITTING — CORRODED (FS1230 L32R) · airframe 68,230 hrs · 28,358 cycles

LWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED .500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTING AT FS 1230 L32R IAW SRM 51-3-2 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1150 L33R) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND INSTALLED FITTING AND INTERCOSTAL IAW DWG 4758514 AND DWG 9754949.

Part: RIB — CRACKED (XFS 707) · airframe 68,230 hrs · 28,358 cycles

LT WING LE UPPER RIB CRACKED AT XFS 707. FABED DOUBLER AND REPAIRED RIB IAW DWG 5769466, AND SRM 57-2-0 FIG 2.

Part: FINGER DOUBLER — CORRODED (FS -67 TO -52) · airframe 68,230 hrs · 28,358 cycles

COCKPIT SUBFLOOR FINGER DOUBLER HAS SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER DOUBLER AT FS -67 TO -52 LBL24. REMOVED AND REPLACED FINGER DOUBLER IAW SRM DWG 5612298 AND SRM 51-1-21 AND 51-1-20D.

Part: CUSP WEB — CRACKED (BS 1390-1430) · airframe 68,230 hrs · 28,358 cycles

CUSP HAS SHEAR HEAD FASTENER AND CRACK 1 INCH LONG FS 1420 L21R. REMOVED DAMAGED CUSP FROM BS 1390-1430 L21R IAW SRM 51-1-20D AND 51-1-2. FABRICATED AND INSTALLED REPAIR PARTS AND CUSP ANGLE IAW SRM 53-2-5 FIG 15 AND DWG 9754069 AT BS 1390-1430 L21R.

Part: FITTING — CRACKED (FS 1150 L19R) · airframe 68,228 hrs · 28,357 cycles

FITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FS1766 RBL48 L11) · airframe 68,230 hrs · 28,358 cycles

AFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007.

Part: LONGERON — CRACKED (FS 1746 L14R) · airframe 68,230 hrs · 28,358 cycles

LONGERON 14R CRACKED FS 1746. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 11.

Part: LONGERON — CRACKED (FS 1726 L15L) · airframe 68,230 hrs · 28,358 cycles

LONG 15L CRACKED AT FS 1726. REMOVED DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED REPAIR SPLICE FILLER AND REPAIR ANGLES AND INSTALLED IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 1766 L6R) · airframe 68,230 hrs · 28,358 cycles

C1 ANGLE CRACKED AT FS 1766 LONG 6R. REMOVED CRACKED ANGLE AT FS 1766 L6R IAW SRM 51-1-20D. FABRICATED AND INSTALLED ANGLE AT FS 1766 L6R IAW SRM DWG 5773844 AND SRM 51-1-20D.

Part: CUSP WEB — CRACKED (FS 1100 L21R) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 CUSP CRACKED FS 1100 L21R. REMOVED CUSP DOUBLER AT FS 1100 L21R AND REMOVED DAMAGED SECTION OF L21R IAW SRM 51-1-20A AND SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED SPLICE PLATE -3 AND -5, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-5 FIG 15 AND TR 53-179 AND BOEING MESSAGE NUMBER 1-115367837-2.

Part: LONGERON — CRACKED (FS 1746 L7R) · airframe 68,230 hrs · 28,358 cycles

LONGERON 7R CRACKED AT FS 1746. REMOVED DAMAGED AREA IAW SRM 53-02-02 FIG 11, FABRICATED AND INSTALLED REPAIR SPLICE FILLER AND REPAIR ANGLES IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.

Part: FITTING — CRACKED (STA 680 L2L) · airframe 68,230 hrs · 28,358 cycles

MAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0 .

Part: PAN — CRACKED (L1-DOOR) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 L1 DOOR LWR AFT CORNER JAMB INSIDE WEB CRACKED 2 INCHES LONG. REMOVED DOOR JAMB AND WEB CUT OUT DAMAGED AREA IAW DWG 5597646, FABRICATED DOUBLER AND SPLICE AND INSTALLED REPAIR PARTS IAW DWG 5597646.

Part: ANGLE — CRACKED (FS 1766 L6L) · airframe 68,230 hrs · 28,358 cycles

C1 ANGLE CRACKED AT FS 1766 LONG 6L. REMOVED ANGLE IAW SRM 51-1-20D AT FS 1766 LONG 6L. FABRICATED AND INSTALLED ANGLE AT FS 1766 LONG 6L DWG 5773844 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 834.5 L18R) · airframe 68,230 hrs · 28,358 cycles

FS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2.

Part: FITTING — CRACKED (FS 907 L8R) · airframe 68,228 hrs · 28,357 cycles

LONGERON END FITTING CRACKED FS 907 L8R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FS 781 L18R) · airframe 68,230 hrs · 28,358 cycles

FRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT FS 781 LONG 18R AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 857.125 L19L) · airframe 68,230 hrs · 28,358 cycles

FRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT F/S 857.125 L19L. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-21D AND 51-3-2.

Part: FITTING — CRACKED (FS 857 L5L) · airframe 68,230 hrs · 28,358 cycles

LONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FITTING — CRACKED (BS 759) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8

Part: FITTING — CRACKED (FS 822 L20L) · airframe 68,228 hrs · 28,357 cycles

FITTING CRACKED FS 822 L20L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS 680 L1L) · airframe 68,230 hrs · 28,358 cycles

CRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,51-1-20D AND 51-01-23 FIG 48.

Part: FITTING — CRACKED (FS 759 LBL 48) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG 3643110 AND 51-1-20D.

Part: FITTING — CORRODED (FS 980 LBL40) · airframe 68,230 hrs · 28,358 cycles

MAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTING AT FS 980 LBL 40 IAW SRM 51-3-0, 51-1-21, AND 51-3-2.

Part: FITTING — CRACKED (FS 923 L22L) · airframe 68,230 hrs · 28,358 cycles

MAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SRM 51-1-8. REMOVED AND REPLACED "T" FITTING IAW SRM 51-3-2 AND DWG 3649114.

Part: FITTING — CRACKED (STA 680 L2R) · airframe 68,228 hrs · 28,357 cycles

INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED (2 INCHES) STA 680 L2R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D,51-1-21,AND 51-1-23 .

Part: FITTING — CRACKED (FS 857 L10L) · airframe 68,230 hrs · 28,358 cycles

LONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0.

Part: FINGER DOUBLER — CORRODED (FS960-980 RBL 65) · airframe 68,228 hrs · 28,357 cycles

INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND SHEAR HEAD FASTENER A T STA 960 TO 980 RBL 65. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5645332 AND DC-8 SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 798 LBL48) · airframe 68,230 hrs · 28,358 cycles

CENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FS 925 LBL65) · airframe 68,230 hrs · 28,358 cycles

MAIN CABIN CENTER SUB FLOOR AT STA 925 LBL 65, FINGER DOUBLER AREA HEAVY CORRODED. REMOVED, FAB`D FINGER DOUBLER AND REPAIRED IAW DWG 5645332 AND SRM 53-0 7-01-0 FIG 010.

Part: FITTING — CRACKED (FS 834.500 L18L) · airframe 68,230 hrs · 28,358 cycles

FRAME TO INTERCOSTAL ATTACHED FITTING CRACKED AT F/S 834.500 L18L. REMOVED AND REPLACED INTERCOSTAL ATTACH FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FS 857 L1) · airframe 68,230 hrs · 28,358 cycles

LONGERON END FITTING CRACKED AT FS 857.125 L1 FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS 857 L18R) · airframe 68,230 hrs · 28,358 cycles

FITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420.

Part: PRESSURE PANEL — CORRODED (FS 940 L24L) · airframe 68,230 hrs · 28,358 cycles

POPPED RIVET, PILLOWED SKIN, LT W/W CEILING, STA 940 OB ABOVE L24L. REMOVED CORROSION AND FOUND OUT OF LIMITS AT STA 940 L24L IAW SRM 51-1-8, FABRICATED AND INSTALLED FILLER, SPLICE DOUBLER FINGER DOUBLER AND TAPERED FILLER AT STA 940 L24L IAW SAA SK 750-846380, DWG SRO8530026, BOEING MESSAGE NR 1-117725249, BOEING MESSAG E 1-118905200-4.

Part: SKIN — CRACKED (RT WING) · airframe 68,230 hrs · 28,358 cycles

INSPECTION TYPE:C1 RIGHT WING UPPER SKIN .25 INCH CRACK AT STA XCW 69 REAR SPAR AREA. CUT OUT CRACKED SECTION OF RIGHT WING AT XCW 69, NDT VERIFIED CRACK TERMINATION IAW HFEC INSP PER NDTSPM 06-10-01.001. FABRICATED -4 FILLER, -6 FILLER AND -8 DOUBLER IAW SRM 51-1-8, AND 51-1-26 FIG 1 SHT 1, AND INSTALLED REPAIR PARTS IAW SRM 51-1-20D AND 51-1-15.

Part: RIB — CRACKED (RT LE XFS 806) · airframe 68,228 hrs · 28,357 cycles

INSPECTION TYPE: C1, RT WING L/E LWR RIB CRACKED AT XFS 806. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-20D, AND 51-1-21.

Part: SKIN — CORRODED (LT WING) · airframe 68,230 hrs · 28,358 cycles

SEVERE CORROSION BETWEEN OUTER SKIN AND FRAME LOWER SURFACE AT SKIN SEAM IN FRONT OF THE LEFT SIDE FUEL DUMP MANIFOLD. REMOVED EXISTING DOUBLER, REMOVED DAMAGE, FAB`D FILLER AND DOUBLER AND INSTALLED IAW SRM 57-02-00-0, DWG 5649654.

Part: SKIN — CRACKED (FS 1746 L15L) · airframe 68,230 hrs · 28,358 cycles

FUSELAGE EXTERIOR SKIN CRACKED 1/2 INCH LONG AT STA 1746 L15L. REMOVED DAMAGED AREA FAB`D FILLER, DOUBLER AND FINGER DOUBLER AND INSTALLED IAW SRM 53-2-1 AND 53-2-1 FIG 7.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK OK IAW 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOP DUE TO POWER ON AC AND LIGHT SWITCH LEFT IN ARMED POSITION. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOP. BATTERY FAILED REPLACED EMERGENCY LIGHT BATTERY.

Part: LINE — FAILED (NLG STEERING)

INSPECTION TYPE:N/A, A/C TAXIED OUT CARGO RAMP NOSE WHEEL STEERING NOT EFFECTING AND WAS STIFF. LOSS OF ALL HYDRAULICS. ACP NLG LINE REPLACED PER STANDARD PRACT CH 20-10-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LTS INOPERATIVE. REMOVED AND REPLACED EMERG EXIT LTS BATTERY PACK. OPS CK GOOD IAW MM CH 33-50. P/N 60-1223-5, S/N ON 350, S/N OFF 10385, P/N OFF 5708458-503

Part: DOOR — OUT OF ADJUST (MAIN CARGO)

ON CLIMB THRU 26,000 THE MAIN CARGO DOOR SYSTEM "A" LIGHT ILLUM. THE SENSORS MUNE ON ACARS POPPED UP INDICATING MAIN CARGO DOOR OPEN. ABOU T 20 SECONDS LATER TWO BANGS WITH ACCOMPANING YAW. A/C PRESS STARTED T O CLIMB. SLOWED A/C AND STARTED DESCENT. ON FINAL APPROACH ALL THE IN DICATOR LIGHTS WENT OUT. REMOVED AND REPLACED 51-256 DOOR SWITCH IAW UPS DC8 M.M. 32-70-00. PRESSURIZED A/C UP TO 8.2 PSI IAW UPS DC8 M.M. 21-10-00. MCD "A" SYS LIGHT DID NOT ILLUMINATE AND OPS CHECKED GOOD IAW UPS DC8 M.M. 52-70-00. N/R 632638

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, UPPER MAIN DECK AT BALLMAT AREA STA 140 BL 0 SEAT TRACK SCALLOP WORN. SEAT TRACK SCALLOP OUT OF LIMITS (MAS .500 INCH, ACT .750 INCH) IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK IAW DC8 SRM 51-3-2, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE:C2 CABIN FLOOR TRACK -G- WORN SCALLOP AT FS 505.0. CUT OUT SEAT TRACK IAW DC8 SRM 53-2-3 & 51-3-0. INSTALLED SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, STRINGER S-61 HAS VERTICAL CRACK 1 ALT. REMOVEDD DAMAGED STRINGER SECTION. REPLACED CORRODED AFT END FITTING P/N 3640143-503, FABBED 2 EA SPLICE RPR ANGLES IAW DC8 SRM 57-2-2. LOC ATED AND DRILLED STRINGER SECTION, 2 EA SPLICE RPR ANGLES, & FITTING; ALODINED & PRIMED; INSTALLED ALL IAW DC8 SRM 51-1-8, 57-2-2, 51-1-24, 51-1-20D, 51-1-23, AND 51-3-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, FLOORBEAM CORRODED AT STA 980 LBL 58 MAIN CABIN. REMOVED CORROSION, OUT OF LIMITS IAW DC8 SRM 53-2-0, 51-1-8; CUT OUT DAMAGE IAW DC8 SRM 53-2-0. FABBED FILLER, ANGLE, SHIM FOR WEB IAW DC8 SRM 53-2-0 FIG 1B&G; ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED F ILLER, SHIM, 2 EA ANGLES AND WEB STIFFENER IAW DC8 SRM 53-2-0 FIG 1B &G, 51-1-24, 51-1-20D. FAB & INSTALLED ANGLE SPLICES IAW DC8 SRM 53-2-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, CABIN FLOOR TRACK -F- HAS WORN SCALLOPS FROM STA 740-770. REMOVED DAMAGED SEAT TRACK AND SPLICED NEW SEAT TRACK AND ADDED 2 SPLICE CHANNELS IAW UPS EO DC8-5320-5167. FABRICATED, LOCATED AND DRILLED HOLES IAW UPS EO DC8-5320-5167 AND DWG DC8-53B-003. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21D AND 51-3-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, MAIN CABIN STA 920 LBL 49 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. ORIG .340 INCH REMAINING .120 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLES, SHIM FOR ANGLES AND SHIM FOR BLENDED OUT DAMAGE IAW REO G09354. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES AND SHIMS IAW REO G09354 AND SRM DC8 51-3-0.

Part: PANEL — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, PNL 192E, SURFACE CORROSION AT BOLT HOLES, INNER SURFACE (MARKED). REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2 -0 FIG 1F. NEW PNL FABRICATED ON OP 50007 IAW DAC DWG 5750365.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, CENTER FLOOR TRACK BL 0 STA 1190 IS EXCESSIVELY WORN. BLENDED FLOOR TRACK (ORIG .420, REM .550) OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED FLOOR TRACK, LOCATED, DRILLED & DEBURRED NEW SEAT TRACK 60-15176 IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 53-2-3/51-3-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, CABIN SEAT TRACK AT STA 218/BL49L SCALLOPS ARE WORN. BLENDED SCALLOPS IAW DC8 SRM 53-2-3. ORIG WIDTH .600, .420 REMAINING OUT OF LIMITS IAW DC8 SRM 53-2-3. CUT OUT IAW DC8 SRM 53-2-3. ALODINED AND PRIMED CUTOUT IAW DC8 SRM 51-1-8. INSTALLED NUT CHANNEL P/N MS21064L4-8 ON TO CHANNEL P/N DC8-53B-007-006 IAW DC8 SRM 53-2-3 FIG 6D. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0 & 53-2-3 FIG 6D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, FWD PIT FS 272 AND L25L Z-FITTING CORRODED. REMOVED FITTING, FABBED SPLICE ANGLES 2 EA IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED HOLES ON NEW FITTING IAW DC8 SRM 53-2-0, INSTALLED NEW FITTING AND SPLICE ANGLES IAW DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (HORIZONTAL STAB) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE:C2 LT HORIZONTAL STAB INBOARD L/E T-ANGLE AT STA XFS 60 IS CRACKED. REMOVED LT HORZ STAB T-ANGLE. DRILLED AND LOCATED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED ANGLE IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, LONGERON 17R CRACKED AT STA 1770-1780 (INSIDE DOOR 60). REMOVED LONG 17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 5 649327. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 17 RT IAW DAC DWG 5649327.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, AFT ACCESSORY COMPT AT STA 1650 LT SIDE L23L IS CRACK AND CORROSION. REMOVED EXT REPAIR DOUBLER, FASTENERS AND DAMAGED LONG 23L FROM 1610 TO 1690. LOCATED & DRILLED NEW SPLICE & NEW LONGERON SECTION IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON SECTION, SPLICE AND EXT DOUBLER IAW DC8 SRM 51-1-21 & 51-1-20D. FAB FLOORBOARD SPLICE AND INSTALLED IAW DC8 SRM 53-2-3 & 51-3-0.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, AFT PIT STA 1200 STR 33L SHEAR TIE FITTING CORRODED. REMOVED CORRODED FITTING IAW DC8 SRM 51-1-20D. LOCATE AND DRILLED NEW FITTING AND FABRICATED SPLICE ANGLES IAW DC8 SRM 53-2-0 FIG 2D. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED 2 FITTING AND SPLICE ANGLES IAW DC8 SRM 53-2-0 FIG 2D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN CRACKED AT VERT FIN AND CENTER SPAR CANT BULKHEAD AT TACH POINT FS 1770 LONG 8L. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOULBER AND SKIN FILLER IAW DC8 SRM 53-2-1 FIG 7. PERFORMED HFEC IAW DC8 NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CORRODED (FUSE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, AFT ACCESSORY COMPT AT STA 1660 RT SIDE BELOW CUSP FITTING IS CORRODED. REMOVED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING IAW DAC DWG 4773143. ALODINE AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, FRAME CORRODED AT STA 1420 AT L25R ABOVE D-PIT DOOR OPENING. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED FRAME REPAIR DOUBLER IAW UPS EO DC8-5310-11728. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D.

Part: LONGERON — BENT (FUSELAGE) · airframe 67,355 hrs · 27,634 cycles

INSPECTION TYPE: C2, AFT PIT AT STA 1255 L29R LONGERON SPLICE BENT. REMOVED LONGERON SECTION. LOCATED & DRILLED NEW LONGERON SECTION AND SPLICES IAW DC8 SRM 51-1-24. INSTALLED LONGERON AND SPLICED IAW SR M DC8 51-1-20D.

Part: WEB — BULGED (PRESSURE PANEL)

INSPECTION TYPE: PFLT, LT W/W AREA HAS 3 POPPED RIVETS AND BULGE IN WEB. REMOVED 2 SECTIONS OF PRESSURE PANEL WEB IN LT WW AT STA 902. REMOVED CORROSION FROM FLOORBEAM FS 902 PER EO DC83107989 A-2. VERIFIED CORROSION REMOVAL & PERFORMED ULTRASOUND THICKNESS CHECK. ECA 43924-INSTALLED REPAIR STRINGER / SPLICES AT STA 902. INSTALLED STIFFNERS & PULLEYS SEALED ENTIRE AREA.

Part: SHEAR TIE — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CORRODED SHEAR TIE AT STA 1140 BETWEEN STR 35L AND 36L. REPAIRED SHEAR TIE IAW DC8 SRM 53-2-0 AS REQUIRED.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY, OPS CHECKED NORMAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 FWD BAG PIT Z FITTING CRACKED AT FS 300 LONGERON 27L. INSTALLED NEW Z FITTING P/N 3755822-515N IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 AFT PIT FS 1228 L35R-L34R Z FITTING IS CRACKED. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-24 & 51-1- 20D

Part: WEB — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 SUBFLOOR WEB AT FS 15 RBL 40 IS CRACKED. CUT OUT DAMAGE IN WEB & FABBED NEW REPAIR DOUBLERS & FILLERS INSTALLED FILLER & DOUBLER IAW SRM.

Part: FITTING — CRACKED (T/E FLAP) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 LT WING FLAP HINGE SUPPORT FITTING XF 409.6673 INBOARD CRACKED AS MARKED. REMOVED FLAP LEADING EDGES I/B & O/B OF FLAP HINGE FITTING TO FOM. LOCATED & DRILLED NEW BASE FITTING. INSTALLED BUSHINGS, INSTALLED SPRING COVER, TRACK BASE FITTING COVER PLATES LEADING EDGE ATTACH ANGLES, FLAP FAIRING ATTACH ANGLE & LEADING EDGES IAW DC8 SRM 510D, 51.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1,3 LT AFT PRESSURE BULKHEAD STA 1766 L11L IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 FS 680 L10R LONGERON END FITTING CRACKED. REMOVED CRACKED 3779762-1 LONGERON END FITTING. INSTALLED NEW LONGERON END FITTING IAW DC8 SRM 51-3-0, 51-1-23 AND 51-1-24.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 AFT PIT FS 1300 AT L36 FRAME IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED -49 REPAIR STRAP IAW DC8 SRM 53-2-0. INSTALLED -49 REPAIR STRAP IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1,3 DAMAGED FRAME AT FASTENER HOLE AND MISSING MOUNT CLIP AT FRAME 180 26R. FOUND FRAME DAMAGE TO BE CRACKED FLANGE AT ATTACHMENT HOLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 MAIN CABIN AT STA 740-810 & LBL 47 SEAT TRACK HAS CORROSION INBD & OTBD SIDES OF SEAT TRACK AROUND FASTENER HOLES (UNDER SIDE). REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TR ACK, FABED NEW SEAT TRACK, AND INSTALLED NEW SEAT TRACK IAW UPS SRM ADDENDUM & DC8 SRM 51-1-8

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 AFT CARGO CROSS SLIDE DOOR JAM T FITTING 3 (EA) HAS CORROSION UNDERNEATH CASTING. REMOVED CORROSION MAT'L OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING (2 EACH) P/N 3755772-501 TORQUE BOX LATCH ASSY LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION INTERNAL DOUBLER FROM FS 1100-1260 L27R-L33L (CORROSION). REMOVED INTERNAL DOUBLER IAW DC8 SRM 51-1-24. TRIM NEW DOUBLER LOCATE AND DRILL EXISTING FASTENER HOLES IAW DC8 SRM 51-1-24 AND INSTALL INTERNAL DOUBLER IAW DC8 SRM 51-1-20D & 51-1-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION EXTERIOR SKIN FROM FS 1050-1350 L31R-L31L DUE TO CORROSION. REMOVED AFT BELLY SKIN FROM FS 1050-1350. TRIM NEW SKIN LOCATE DRILL EXISTING FASTENER HOLES AND COUNTERSINK HOLES IAW DC8 SRM 51-1-24. INSTALL NEW SKIN IAW DC8 SRM 51-1-20D & 51-1-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 STA 1220 L35L TO L34L Z FITTING CORRODED. REMOVED AND REPLACED FITTING

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 AFT PIT FS 1220 L32R-L33R ZEE FITTING HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND MAT'L OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW FITTING P/N 3755840-1 LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1,3 INTERCOSTAL CRACKED IN FWD END OF UPPER RADIUS LONG 31L STA 1620 - 1640 AFT ACCESSORY COMPT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1,3 STA 470 TRACK G HAS CORROSION DOWN CTR. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53-2-3 FIG 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,196 hrs · 26,848 cycles

INSPECTION TYPE:C1/3 SEAT TRACK E AT STA 980 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK.

Part: WARNING LIGHT — MALFUNCTIONED (NLG)

INSPECTION TYPE:N/A, NOSE GEAR DOWN GREEN LT EXTINGUISHES. DOOR NOT LATCHED LIGHTS COME ON WHEN NOSE WHEEL STEERING IS ACTIVATED AND RELEASED TO NEUTRAL POS D208866. TRANSFERRED TO UPS NR 215073. ONE TIME FERRY FLT FROM ATL TO SAT (DHC) FOR REPAIR ON NOSE & MAIN GEAR FAULTS.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY BATTERY PACK AND TWO BAD PINS (12 AND 10) ON CONNECTOR PO1-1345. EMERGENCY LIGHTS TEST OK PER MM 33-50-01 PG 201.

Part: FASTENERS — MISSING (RT EMER EXIT)

INSPECTION TYPE:N/A, AFT RT EMERGENCY EXIT DOOR LWR EDGE HAS SEVEN MISSING FASTENERS. *S/D* REMOVED R5 DOOR, REPLACED NUT PLATE CHANNEL AND INSTALLED SCREWS IAW SRM 51-3-0. REINSTALLED DOOR REF LG 416910 ITEM 2.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A, 1 INCH CRACK UPPER AFT CORNER FUSELAGE PIT 34. *S/D* REPAIRED CRACK IAW SRM 53-02-00.

Part: SEAL — LOOSE (NLG DOOR)

ON DEPART, (C/O) NOTICED AFTER GEAR RETRACT, THE GEAR NOT LATCH LIGHT FLICKERED. DID UPLATCH CK AND LIGHT EVENTUALLY CAME ON STEADY. WENT TO GEAR NOT LATCH LIGHT ILLUMINATED. CKLIST AND C/W, THIS INCLUDED CYCLING GEAR AND LOOKING THROUGH PEEPHOLE TO CHECK IF N/G WAS DOWN AND LOCKED, IT WASN'T. ALSO, HEARD A BANGING TYPE NOISE. REMOVED AND REPLACED NOSE GEAR DOOR SEAL PER MM 32-30-00 PG 104 SECT D. LUBED UPLATCH MECHANISM PER MM 12-81-01. JACKED AIRCRAFT, CYCLED GEAR 5 TIMES, NO FAULTS NOTED AND INDICATOR LIGHTS OP'D NORMALLY.

Part: FRAME — CORRODED (BS 60)

INSPECTION TYPE:C2 FS 60 FRAME AT LBL 40 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: SEAT TRACK — CORRODED (BS 1480-1540)

INSPECTION TYPE:C2 FS 1480 TO 1540, RBL 52, THE SEAT TRACK IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SEAT TRACK FS 1470 TO 1580, SPLICED IN A NEW TRACK IAW SRM 53-2-3 FIG 8A.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C2 FS 1240 AT LONG 33R, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: RIB — CRACKED (WS 425.5)

INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 425.5 IS CRACKED AT THE AFT LWR END. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 1310-1420)

INSPECTION TYPE:C2 FS 1310, 1320 TO 1420, BL 0, THE CABIN SEAT TRACK IS CORRODED AT THE CLIPNUTS. CUT OUT DAMAGED SEAT TRACK FS 1310 TO 1430, FABRICATED, AND REPLACED TRACK AND INSTALLED IAW SRM 53-2-3.

Part: INTERCOSTAL — CORRODED (BS 1440-1460)

INSPECTION TYPE:C2 FS 1440 TO 1460, LBL 8, THE CEILING INTERCOSTAL IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 1B.

Part: DOUBLER — CRACKED (WS 372)

INSPECTION TYPE:C2 RT WING L/E AT XFS 372, THE LIFT TRANSDUCER DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769589 AND SRM 51-1-21.

Part: WEB — CORRODED (BS 512-520)

INSPECTION TYPE:C2 FS 512 TO 520, LONG 33R TO 35R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRM 53-2-0 FIG 23.

Part: ANGLE — CORRODED (BS 879-900)

INSPECTION TYPE:C2 MAIN CABIN FS 879 TO 900, LBL 61, THE HORZIZONTAL ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5645332 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:C2 FS 1260 TO 1280, LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1050)

INSPECTION TYPE:C2 LONGERON 31L SPLICE FITTING AT FS 1050 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 53-2-2 FIG 10.

Part: FITTING — CORRODED (BS 1152)

INSPECTION TYPE:C2 FS 1152, AT LONG 33R, THE TORQUE BOX BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, THE LONGERON 32R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, THE LONG 36 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED FS 1200 BETWEEN LONGERON 34R AND 33R. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, LONGERON 24R END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:C2 LONGERON 32L BETWEEN FS 1260 AND 1280, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D AND 53-2-2 FIG 10.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:C2 FS 1260 TO 1280, LONG 36 SPLICE IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 210)

INSPECTION TYPE:C2 FS 210, LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1150-1160)

INSPECTION TYPE:C2 LONGERON 31R FITTING, FS 1150 TO 1160 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: ANGLE — CORRODED (BS 1480)

INSPECTION TYPE:C2 VERTICAL SUPPORT ANGLE AT FS 1480, LONGERON 27L HAS HEAVY CORROSION. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3773157 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1400)

INSPECTION TYPE:C2 FS 1400 FRAME, AT LONG 35R IS CRACKED. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE:C2 FS 1200 BETWEEN LONG 35L AND 34L, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 3D.

Part: FITTING — CRACKED (BS 450)

INSPECTION TYPE:C2 LONGERON 31R SPLICE FITTING AT FS 450 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE:C2 FS 717, RBL 24, THE FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 789-834)

INSPECTION TYPE:C2 FS 789 TO 834, RBL 60, THE SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SEAT TRACK FROM FS 750 TO 842, FABRICATED AND INSTALLED IAW SRM 53-2-3 AND EO DC8-5320-5167C.

Part: LONGERON — CRACKED (BS 600-620)

INSPECTION TYPE:C2 LONGERON 33R IS CRACKED BETWEEN FS 600 AND 620. CUT OUT DAMAGED SECTION AND REPAIRED IAW DH SK750-128X.

Part: FITTING — CRACKED (NR 4 SPOILER)

INSPECTION TYPE:C2 LT WING T/E, THE NR 4 SPOILER OTBD HINGE FITTING IS CRACKED. REMOVED AND REPLACED THE HINGE FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: SEAT TRACK — CORRODED (BS 50-70)

INSPECTION TYPE:C2 FS 50 TO 70, RBL 48, THE SEAT TRACK HAS HEAVY CORROSION AROUND THE CLIPNUTS. CUT OUT DAMAGED AREA FROM FS 50 TO 100, FABRICATED REPLACEMENT TRACK AND INSTALLED IAW SRM 53-2-3 FIG 14.

Part: FITTING — CRACKED (BS 32)

INSPECTION TYPE:C2 COCKPIT SUB-FLOOR INTERCOSTAL VERTICAL SUPPORT FITTING IS CRACKED, FS -32.OO LBL 12. REPAIRED FITTING IAW DH SK750-913.

Part: DOUBLER — CRACKED (WS 598)

INSPECTION TYPE:C2 RT WING L/E AT XFS 598, THE INNER DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.

Part: SKIN — CRACKED (WS 425.5)

INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XFS 425, 5 FWD OF THE SPAR IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK & REPAIRED IAW E.O. DC8-5720-4087.

Part: RIB — CRACKED (WS 379)

INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 691.25)

INSPECTION TYPE:C2 LT WING L/E UPPER RIB AT XFS 691.25 IS CRACKED AT THE AFT FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C2 FS 55 FRAME BETWEEN LONG 24L AND 25L IS CRACKED AT THE DUCT SUPPORT. CUT OUT DAMAGED FRAME AND REPAIRED IAW SRM 53-2-0 FIG 2.

Part: RIB — CRACKED (NR 4 SPOILER)

INSPECTION TYPE:C2 LT WING T/E AT XRS 358, THE NR 4 SPOILER OTBD RIB IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-1-20D AND 51-3-0.

Part: DOUBLER — CRACKED (WS 566.25)

INSPECTION TYPE:C2 LT WING L/E LWR SKIN, INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.

Part: SKIN — CRACKED (WS 722.5)

INSPECTION TYPE:C2 LT WING L/E SKIN AT XFS 722.5 IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: FITTING — CRACKED (BS 851)

INSPECTION TYPE:C2 KEEL BEAM FITTING AT FS 851, RT SIDE, IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (WS 566.25)

INSPECTION TYPE:C2 LT WING L/E LOWER SKIN IS CRACKED AT XFS 566.25. STOP DRILLED CRACK AT REPAIRED IAW EO DC8-5720-7767A.

Part: SKIN — CORRODED (WS 485)

INSPECTION TYPE:C2 LT WING L/E UPPER SKIN AT XW 485 HAS BULGING, POPPED RIVET AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: DOUBLER — CRACKED (BS 280)

INSPECTION TYPE:C2 FS 280 BETWEEN LONG 12L AND 16L, THE PREVIOUS REPAIR DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5772787 AND SRM 51-1-21.

Part: EMERG BATT — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTING BATT PACK. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT'S INOP. SWITCH LEFT IN ON POSITION. REMOVED SERVICEABLE BATTERY PACK UNIT FROM A/C 868 AND INSTALLED INT O A/C 750. OPS CHK'S GOOD, ALL SECURE. INSTALLED (P/N 5708458-503) (S/N 10382) ON, (P/N 5708458-503) (S/N 925) OFF.

Part: BATTERY — DISCHARGED (BS 143)

INSPECTION TYPE-N/A, EMERGENCY LIGHT IN COCKPIT DID NOT TEST DURING PREFLIGHT. REMOVED AND REPLACED EMERG LIGHT BATT AND RELAY UNIT WITH REF MM 33-50-01, OPS CK'ED NORMAL AT THIS TIME. (P/N 5708458-503), (S/N 925/084).

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EEL COCKPIT ENTRY AND DOME DID NOT WORK. REPLACED EMERGENCY EXIT LIGHT BATT PACK PER MM 33-50-01, OP'S CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:DALY EMER EXIT LIGHT INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK PER DC8 MM 33-50-01. LIGHTS OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-W/E, EMERGENCY EXIT LIGHTS INOP ON WEEKEND CHECK. REPLACED RECHARGEABLE BATTERY PACK ASSY.

Part: RIB — CRACKED (BS 385.25)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED LWR ARM STA 385.250. REPAIRED IAW SRM 57-3-1.

Part: SEAT TRACK — CORRODED (BS 1660)

INSPECTION TYPE-C, SEAT TRACK CORRODED OUT OF LIMITS FS 1660 RBL 38 AFT ACCESSORY COMP. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE-C, FS 1180 BTWN STR 35R TO 36 STR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 35-55)

INSPECTION TYPE-C, FUSELAGE DOUBLER ABOVE L30R BETWEEN FS 35 TO 55 CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21.

Part: FITTING — CORRODED (BS 1200)

INSPECTION TYPE-C, FS 1200 BTWN STR 35R TO 36 TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 70)

INSPECTION TYPE-C, FS 70 LONG-33L SKIN CORRODED OUT OF LIMITS. REPAIRED IAW DHC SK-750-649.

Part: SKIN — CORRODED (BS 1690)

INSPECTION TYPE-C, FS 1690 L-28L CORROSION REMOVAL BEYOND LIMITS. INSTALLED EXTERNAL SKIN REPAIR DOUBLER IAW SRM 53-2-1.

Part: RIB — CRACKED (WS 728.75)

INSPECTION TYPE-C, LT WING L/E AT STA XFS 728.750 UPPER ARM CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CORRODED (BS 1200)

INSPECTION TYPE-C, FS 1200 BTWN STR 34L TO 35L TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-C, C-3 CARGO FS 1160 RT FLOORBEAM SUPPORT FITTING IS CRACKED ON LWR END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM51-3-0 AND DWG 9754024.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 UPPER RIB CRACKED 4. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (BS 960)

INSPECTION TYPE:C LONGERON 24L FITTING CRACKED AT F/S 960. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 53-2-0.

Part: LONGERON — CORRODED (BS 940)

INSPECTION TYPE:C LONGERON 24L FITTING HAS HEAVY CORROSION F/S 940. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: SEAT TRACK — CORRODED (BS 840-940)

INSPECTION TYPE-C, SEAT TRACK AT LBL 44 FS 840 AND 940 CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW ADDN DC8-5320-8309-B.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 772.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 400)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 400.00, THE EXTERNAL SKIN HAS CRACK. REPAIRED IAW SRM ADDN DC8-5720-7767.

Part: SEAT TRACK — CRACKED (BS 505)

INSPECTION TYPE-C, MAIN CABIN FS 505 BL 0 SEAT TRACK HAS HEAVY CORROSION AND CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW DC8-5320-5167-C.

Part: SEAT TRACK — CRACKED (BS 600)

INSPECTION TYPE-C, SEAT TRACK AT PLUG SLIT/CRACKED LBL 44 FS 600. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM ADDN DC8-5320-8309-B.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: SEAT TRACK — CRACKED (BS 1220)

INSPECTION TYPE-C, SEAT TRACK SPLIT AND CRACKED FS 1220 LBL 24. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW DC8-5320-5167-C.

Part: LONGERON — CRACKED (BS 879)

INSPECTION TYPE-C, LONGERON 24R FITTING AT FS 879 HAS CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0.

Part: SEAT TRACK — CORRODED (BS 1210)

INSPECTION TYPE-C, MAIN CABIN SEAT TRACK HAS HEAVY CORROSION FS 1210 BL 0. REPAIRED IAW UPS DC8-5320-5167-C.

Part: SEAT TRACK — CORRODED (BS 648)

INSPECTION TYPE-C, MAIN CABIN AT FS 648 RBL 59.5 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW DC8-5320- 5167-C.

Part: SEAT TRACK — CORRODED (BS 1138-1210)

INSPECTION TYPE-C, MAIN CABIN FS 1138 TO 1147 AND 1210 RBL 44, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 53-7-2.

Part: SEAT TRACK — CORRODED (BS 490-530)

INSPECTION TYPE-C, SEAT TRACK AT FS 490 TO 530 LBL 59.5 HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM ADDN DC8-5320-5167C.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 622.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 484.395)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XS 484.395. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 635.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 747.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 747.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 647.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 647.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 597.5)

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

Part: RIB — CRACKED (WS 466.651)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XS 466.651. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 297.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 297.50. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED ON LWR ARM BY AFT FASTENER STA 616.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA XFS 778.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 653.750. REPAIRED IAW SRM 57-2-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK, OP'S CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE-N/A, CORROSION ON BELLY SKIN AT LEFT SIDE OF MARKER BEACON ANTENNA. ALL WORK STEPS C/W ON MP OPENED ON LP 045045 ITEM 2 (REF EO DC8-5330-9829-A).

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE-N/A, REF LOGBOOK PAGE 045043 ITEM 3 WORK IN PROGRESS SUPPLEMENT STARTED FOR CORROSION ON BELLY SKIN AROUND MARKER BEACON ANT WIP FORM ATTACHED. THIS ACTION ITEM CONSIDERED MINOR IAW EO DC8-5330-9829-A.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK OK (P/N 60-1223-5) (S/N 322) ON, (S/N 10) OFF.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTING DID NOT TEST. REPLACED EMERGENCY EXIT LIGHTING BATTERY PACK.

Part: FRAME — CORROSION (BS 1060)

INSPECTION TYPE CS2, HEAVY CORROSION ON UPPER FWD SIDE OF BELTFRAME FS 1060 LONGERONS 30R TO 32L. REPAIRED PER UPS EO.

Part: SHEAR TIE — CRACKED (BS 1600)

INSPECTION TYPE-D, SHEAR TIE CRACKED AT FS 1600 BETWEEN LONGERONS 31R AND 30R. REPAIRED SHEAR TIE PER SRM 53-2-0, FIG 2B.

Part: SHEAR TIE — CRACKED (BS 1600)

INSPECTION TYPE-D, SHEAR TIE CRACKED AT FS 1600 BETWEEN LONGERONS 26R AND 27R. REPAIRED SHEAR TIE PER SRM 53-2-0, FIG 2A.

Part: FLOOR BEAM — CORROSION (BS-12)

INSPECTION TYPE CS2, CORROSION DAMAGE AT FLOOR BEAM LOWER HORIZONTAL FLANGE FS 12 LBL 45. REPAIRED PER UPS EO.

Part: BEAM — CORROSION (BS 780)

INSPECTION TYPE-CS2, HEAVY CORROSION FS 780 FLOOR BEAM UPPER LEG LBL 12. REPAIRED PER UPS EO.

Part: BULKHEAD FTG — CRACKED (BS 1800)

INSPECTION TYPE-D, BOTH ATTACHMENT FITTINGS TO CANTED BULKHEAD STRUCTURE ARE CRACKED AT FS 1800 LBL AND RBL 9. REPAIRED FITTINGS PER SRM 53-2-0, FIG 1B.

Part: SEAT TRACK — CORROSION (BS 1707)

INSPECTION TYPE-CS2, CORROSION OUT OF LIMITS ON SEAT TRACK NR 5, FS 1707. REPLACED SEAT TRACK SECTION FS 1670 TO 1707 PER SRM 53-2-3.

Part: FLOOR BEAM — CORROSION (BS 920)

INSPECTION TYPE-CS2, HEAVY CORROSION ON FS 920 FLOOR BEAM UPPER LEG AFT SIDE LBL 16. REPAIRED PER UPS EO.

Part: SPAR — CRACKED (RT WING)

INSPECTION TYPE CS2, RT LOWER AUX SPAR IS CRACKED AT BOLT HOLE. REPLACED AUX SPAR PER TASK CARD NR 1057.

Part: DOUBLER — CORROSION (BS 19-8)

INSPECTION TYPE-CS2, HEAVY CORROSION ON FUSELAGE NOSE SECTION PRESSURE DOUBLER STA 19 TO 8. REPAIRED PER UPS EO.

Part: DOUBLER — CORROSION (BS 52-42)

INSPECTION TYPE-CS2, HEAVY CORROSION ON SUBFLOOR AND FINGER DOUBLER AT LONGERON 24R FS 52 THROUGH 42. REPAIRED PER UPS EO.

Part: FRAME — CORROSION (BS 1060)

INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE AT BELTFRAME FS 1060 LONGERON 36. REPAIRED FRAME PER SRM 53-2-0.

Part: RIBS — CRACKED (RT HORIZ STAB)

INSPECTION TYPE-D, 2 RT HORIZONTAL STABILIZER LEADING EDGE LOWER RIBS CRACKED AT STA XRS82 AND XRS111. REPAIRED RIBS PER SRM 55-2-0.

Part: FRAME — CORROSION (BS 1060)

INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME FS 1060 BETWEEN LONGERONS 35L TO 36 UPPER CAP. REPLACED FRAME SECTION PER SRM 51-1-20D.

Part: SUPPORT ANGLE — CORROSION (BS 70)

INSPECTION TYPE-CS2, FS 70 SUPPORT ANGLE HAS MODERATE CORROSION AND CRACKED AT LONGERONS 30L TO 35R. REPAIRED SUPPORT ANGLE PER SRM 53-2-0.

Part: RIBS — CRACKED (RT WING LE)

INSPECTION TYPE-D, RT WING LEADING EDGE HAS 8 RIBS CRACKED AT STA XFS628, XFS616, XFS660, XFS660 LOWER, XFS666, XFS735, XFS800 AND XFS806. REPAIRED RIBS PER SRM 57-2-0 AND MM 57-00-00 FIG 801.

Part: FITTING — CORROSION (BS 340)

INSPECTION TYPE-CS2, HEAVY CORROSION ON BATH TUB FITTING AT FS 340, BETWEEN LONGERONS 27L TO 28L. REPLACED FITTING PER SRM 51-1-20D.

Part: RIBS — CRACKED (RT WING LE)

INSPECTION TYPE-D, 4 RIBS CRACKED ON LEADING EDGE RT WING UPPER AT STA XFS560, XFS5 72, XFS578 AND XFS610. REPAIRED RIBS PER SRM 57-2-0 AND MM 57-00-00 FIG 801.

Part: RIBS — CRACKED (LT HORIZ STAB)

INSPECTION TYPE-D, 3 LOWER RIBS CRACKED ON LT HORIZONTAL STABILIZER LEADING EDGE AT STA XRS35 INBD, XRS29 INBD AND XRS112 INBD UPPER RIBS. REPAIRED RIBS PER SRM 55-2-0.

Part: RIBS — CRACKED (LT HORIZ STAB)

INSPECTION TYPE-D, 2 LOWER RIBS ON LT HORIZONTAL STABILIZER LEADING EDGE ARE CRACKED AT STA XRS35 INBD AND XRS29 INBD. REPAIRED RIBS PER SRM 55-2-0.

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT SWITCH LEFT ON, LOW VOLTAGE. REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: SKIN — CRACKED (RT WING)

WHILE ON GROUND IN ORD, MAINTENANCE FOUND 3 INCH CRACK ON RIGHT WING JUST OUTBD OF PANEL 520A AND .25 INCH CRACK ON LT FWD NLG WHEEL WELL CUTOUT. REPAIRED IAW EO DC8-5720-7265A, DC8-5330-4154.

Part: FRAME — CRACKED (FS 1140)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME AFT ANGLE CRACKED AT F.S. 1140, LONGERON 35L. REPAIRED IAW DC8-5310-7129-A.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 INCH CRACK IN SKIN AT LOWER FORWARD CORNER AFT CARGO BIN DOOR CUT OUT. REPAIRED IAW DC8-5330-7124-A.

Part: FRAME — CRACKED (FS 1345)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON BELT FRAME 1.5, LONGERON AT F.S. 1345, LONGERON 21R. REPAIRED IAW DC8-5310-7120-A.

Part: FLOOR BEAM — CORROSION (FS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FLANGE LOWER SURFACE OF FLOOR BEAM F.S. 1680, UNDER NR 3 SEAT TRACK. REPAIRED IAW DC8-5310-7125-A.

Part: FITTING — CORRODED (FS 960)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME END FITTING, F.S. 960, LONGERON 22L. REPAIRED IAW DC8-5310-7126-A.

Part: FLOOR BEAM — CORROSION (FS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, F.S. 1580, LONGERON 22R. REPAIRED IAW DC8-5310-7128-A.

Part: FITTING — CORRODED (FS 880)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME LOWER FITTING AT BOLT HOLES AT F.S. 880, LT AT FLOOR BEAM.

Part: FLOOR BEAM — CORRODED (FS 1660)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM UPPER FLANGE LOWER SURFACE FORWARD SIDE AT F.S. 1660 UNDER NR 3 SEAT TRACK.

Part: PANEL — CORROSION (FS 12)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE UNDER REPAIR AT NOSE WHEELWELL CEILING ABOVE LIGHT F.S. 12. REPAIRED IAW DC8-5310-7121-A.

Part: LONGERON — CRACKED (FS 980)

WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED LONGERON 24L FS 980. REPAIRED IAW SRM 53-2-2.

Part: LONGERON — CRACKED (FS 857)

WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED LONGERON 24R ABOVE BOTTLE BOLT, FS 857. REPAIRED LONGERON IAW SRM 53-2-2, 51-1-20D.

Part: BULKHEAD DOME — CRACKED (FS 683)

WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED AFT PRESSURE BULKHEAD DOME FS 683, LONG 31L TO 30L. REPAIRED IAW EO DC8-5310-7080-A.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN C-CHECK MAINTENANCE, FOUND 1 CRACK FWD UPPER SKIN AROUND FUEL SERVICE DOOR. REPAIRED IAW SRM DC8-5310-7089-A.

Part: FRAME — CORRODED (CARGO DOOR)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BOTTOM FWD FRAME ON A CROSS SLIDE DOOR AND 2 INCH LONG CRACK. REPLACED FRAME SECTION IAW SRM 51-1-20A, 51-1-21.

Part: DOUBLER — CORRODED (FS 220-420)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON INNER DOUBLER FS 220 TO 420, LONG 31R. REPLACED DOUBLER IAW SRM 51-1-20D.

Part: CHANNEL — CORRODED (FS 857-880)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON CHANNEL BETWEEN FS 880 TO 857, LBL 15 TO 30. REPLACED CHANNEL IAW SRM 51-1-20D.

Part: SKIN — CORRODED (VERT STAB)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION AND CRACKS AROUND FASTENERS AT VERTICAL STAB LEADING EDGE ON UPPER EDGE LT SIDE. REPAIRED IAW SRM 55-2-0.

Part: ESCAPE SLIDE — SEPARATING (DOOR)

WHILE IN C-CHECK MAINTENANCE, FOUND ESCAPE SLIDE CASE SEPARATING AT THE TOP. REPAIRED IAW SRM 51-1-2.

Part: SKIN — CORRODED (FS 190-450)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION BULGES AT FUSELAGE BELLY SKIN STA 190 TO 450. REPLACED SKIN.

Part: SUPPORT — CORROSION (FS 70)

WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER RT HORIZ SUPPORT FS 70, BULKHEAD RBL 65. REPLACED SUPPORT IAW SRM 51-1-20D.

Part: FRAME — CORROSION (FS 460)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BELT FRAME FWD SIDE, FS 460 BETWEEN LONGS 29R TO 31R. REPAIRED IAW SRM 53-2-0.

Part: DOUBLER — CORROSION (FS 460)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BELT FRAME REINFORCEMENT DOUBLER AT FS 460, LONG 27R TO 29R. REPAIRED IAW SRM 53-2-0.

Part: DOUBLER — CORROSION (FS 200-220)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON ANTENNA DOUBLER FS 200 TO 220, AND FS 360 TO 380, LONGS 35L TO 35R. REPLACED DOUBLER IAW SRM 51-3-2.

Part: FITTING — CORROSION (FS 320)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 320, BETWEEN LONGS 34L TO 35L AND LONGS 34L AND 33L. REPLACED FITTINGS IAW SRM 51-1-20D, 53-2-0.

Part: DOUBLER — CORROSION (FS 400-450)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON FINGER DOUBLER AT FS 400 TO 450, LONG 31R. REPLACED DOUBLER IAW SRM 51-1-20D, 51-1-21.

Part: FITTING — CORROSION (FS 7075)

WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON END FITTING 30R AT FS 7075. REPLACED FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 240-387)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 35L, FS 240 TO 387. REPLACED LONGERON IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 1020)

WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER LONGERON 21R, FS 1020. REPAIRED IAW SRM 53-2-5.

Part: FITTING — CORROSION (FS 270/300)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 270 AND FS 300, BETWEEN LONGS 34R TO 35. REPLACED FITTINGS IAW SRM 53-2-0.

Part: FITTING — CORROSION (FS 280)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 280, BETWEEN LONGS 34L TO 35L AND LONGS 34R AND 35R. REPLACED FITTINGS IAW SRM 51-1-20D, 53-2-0.

Part: DOUBLER — CORROSION (FS 450-610)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON FINGER DOUBLER, FS 450 TO 610, LONG 31L AND FS 456, LONGS 32L TO 31R. REPLACED DOUBLER IAW SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1160)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 1160, FS 1200 BETWEEN LONGS 34R TO 35R. REPLACED FITTINGS IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 230-235)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 35R, FS 285, I/B SIDE AND O/B SIDE AT FS 230 TO 235. REPLACED LONGERON SECTION IAW SRM 51-1-20D.

Part: FITTING — CORROSION (FS 190-205)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 36 END FITTING, FS 190 TO 205. REPLACED FITTING IAW SRM 51-1-20D.

Part: J BEAM — CRACKED (AFT PRESS BULKHD)

DURING 'B' CHECK, MAINTENANCE REPORTED AFT PRESSURE BULKHEAD 'J' BEAM CRACKED 4TH BEAM UP FROM BOTTOM. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6694.