N810UP

Part: CIRCUIT BREAKER — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CONTROL C/B OPENED DURING ENGINE START. RESET C/B. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM SEVERAL TIMES. SYSTEM CHECKS NORMAL. NOTED BY MAINTENANCE. NO FURTHER ACTION REQUIRED REF AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY BATTERY/RELAY PACK AND TESTED IAW MM 33-50-01-2-2.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-00. OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AFTER BLOCKOUT WITH ENGINES RUNNING NORMAL, EMERGENCY LIGHTS OPERATED CONTINUOUSLY. REMOVED AND REPLACED EMERGENCY BATTERY PACK. RESET CIRCUIT BREAKER. OPS CHECK NORMAL PER AMM 33-50-01-2.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CHECK FAILED. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A FRONT FWD ENTRANCE EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK OK PER MM 33-50-02.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. SEATED CONNECTOR ON BATTERY PACK & LIGHTS TESTED NORMAL PER 33-50-01 -2.

Part: FITTING — CRACKED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 STRINGER END FITTING TO FRONT SPAR CRACKED BETWEEN XRS 463 TO XRS 450 NR 1 ALT TANK REMOVED STRINGER END FITTING FROM FWD SPAR BETWEEN XRS 463 TO XRS 450 IAW SRM 51-01-20D, FABRICATED AND INSTALLED STRINGER END FITTING AT WING STA XRS 463 TO XRS 450 IAW DWG 3644046, AND SRM 51-01-20D.

Part: LONGERON SPLICE — CRACKED (FS 1270 L31L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 SPLICE FITTING CRACKED (C-PIT) L31L STA 1270. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1270 L31L IAW SRM 51-1-20D, AND SRM 51-3-2.

Part: ANGLE — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 R/WING CENTER LEADING EDGE SLOT INBD SIDE "L" ANGLE CRACKED. STOP DRILLED CRACK ON "L" ANGLE AT R/WING CENTER L/E SLOT DOOR IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-02-00 FIG 002.

Part: SKIN — CRACKED (FS 1720 L15L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CRACKED IN 3 EA AREAS AT STA 1720 L15L. REPAIRED FUSELAGE SKIN AT STA 1720 L15L IAW SAA EA NR 008-5330-01-A 0923, UPS EO DC8-5330-27108-A, AND FAA FORM 8100-9.

Part: CHANNEL — CRACKED (T/E FLAP) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 LEFT UPPER TRAILING EDGE PANEL FROM OUTBOARD TO INBOARD SIDE Z-CHANNEL CRACKED. REMOVED CRACKED Z-CHANNEL AT LEFT TRAILING EDGE PANEL FROM OUTBOARD TO INBOARD SIDE IAW SRM 51-1-21D. FABRICATED AND INSTALLED REPAIR Z-CHANNEL IAW DWG 5707670, AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS45-48 L31R) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 EXFOLIATION CORROSION IN A/C COMPT AT STA 45 - 48 AT L31R. REMOVED CORRODED DOUBLER AT STA 45 - 48 L31R IAW SRM 51-1-20D LOCATED, DRILLED-UP, AND INSTALLED REPAIR DOUBLER AT STA 45 -48 L31R IAW SRM 51-3-2, AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 LEFT WING CENTER LEADING EDGE LOWER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-3-3 FIG 007, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 LEFT WING CENTER L/E RIB PUNCTURED AND CRACKED AT STA SX515. REMOVED AND REPLACED CRACKED RIB AT LEFT WING STA XS515 IAW SRM 57-2-0 FIG 2, AND SRM 57-3-03 FIG 4.

Part: LONGERON — CRACKED (FS 1766 L15L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L15L WHERE VERTICAL STAB ATTACHES TO LONGERON IS CRACKED. REMOVED SHEAR TIE AND DAMAGED LONGERON 15L SECTION AT STA 1766 IAW SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON REPAIR SPLICE AND STRAPS AT L15L STA 1766 IAW SRM 53-02-02-0 FIG 10.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE STA XFS 597 INTERNAL RIB IS CRACKED AT LWR END. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D.

Part: FITTING — CRACKED (FS 922 L21R) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 END FITTING CRACKED AT STA 922 L21R. REMOVED END FITTING AT STA 922 L21R IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED REPAIR END FITTING AT STA 922 L21R IAW SRM 51-1-24, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1766 L10L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L10L AT STA 1766 HAS CRACKED END FITTING. REMOVED AND REPLACED L10L END FITTING AT STA 1766 IAW SRM 51-03-02- O, AND SRM 51-01-20D.

Part: FRAME — CRACKED (FS 120 L31R) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 A-PIT STA 120 L31R, FRAME HAS CRACK EXTENDING PAST STOP DRILL. STOP DRILLED CRACK AT FRAME STA 120 L31R IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 120 FRAME L31R IAW SRM EO DC8-5320-6176-C.

Part: LONGERON — CRACKED (FS 1721) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L15R AT STA 1720 CRACKED. REMOVED DAMAGED LONGERON SECTION AT STA 1721 TO 1766 L15R IAW SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1721 TO 1766 L15R IAW SRM 53-02-02-0 FIG 10.

Part: RIB — CRACKED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 LEFT WING CENTER LEADING UPPER RIB CRACKED XS497. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-03-03 FIG 004, 51-1-20D.

Part: VANE — CORRODED (RT WING LE) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE SLOT VANE INBOARD UPPER SURFACE HEAVY CORROSION. CORROSION BLENDOUT WENT OUT OF LIMITS IAW SRM 57-03-00 FIG 23. FABRICATED AND INSTALLED FILLER AND DOUBLER AT RT WING CENTER L/E SLOT VANE INBOARD UPPER SURFACE IAW SRM 57-03-00-0 FIG 024 AND SRM 51-3-0.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 334. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D AND DWG 5769589.

Part: SKIN — CRACKED (L2 DOOR) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L2 DOOR INNER SKIN BROKEN AT LWR HINGE ARM CUTOUT. REMOVED BROKEN STRAP AT L2 DOOR ARM CUTOUT IAW SRM 51-3-0. FABRICATED AND INSTALLED REPAIR STRAP AT L2 DOOR ARM CUTOUT IAW DWG 5750988, AND SRM 51-3-0.

Part: WEB — PUNCTURED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L/WING INBD LEADING EDGE (AUX TANK) VERY INBD WEB HAS A PUNCTURE. REPAIRED L/WING INBD LEADING EDGE (AUX TANK) VERY INBD WEB IAW SAA EA NR 008-5710-01-A0921, UPS RAA NR DC8-57-20224, AND FAA FORM 8100-9

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE UPPER RIB CRACKED AT STA XS 497. STOP DRILLED CRACKED RIB AT STA XS 497 IAW SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XS 497 IAW 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 796. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-00 FIG 2, 51-1-20D.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 HAT CHANNEL HEAVILY CORRODED IN MAIN CABIN SUBFLOOR AT L1 DOOR STA 30 LBL 50. REMOVED HAT CHANNEL AT STA 30 LBL 50 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPLACEMENT HAT CHANNEL AT STA 30 LBL 50 IAW SRM DWG 3713239, AND SRM 51-01-20D.

Part: LONGERON — CRACKED (FS 320 L21L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 L21L AT STA 320 CRACKED. CUT OUT DAMAGED CUSP AT STA 275 - 330 L21L IAW SRM 53-02-05 FIG 15. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS AND CUSP SECTION AT STA 275 - 330 L21L IAW SRM 53-02-05 FIG 15.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT OUTBOARD LEADING EDGE LWR RIB CRACKED AT XFS 634. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW 57-02-0 FIG 02, 51-1-20D.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT SIDE OF VERTICAL STAB UPPER SKIN HAS 5 SHEARED FASTENERS AND POSSIBLE CORROSION UNDER SKIN. REMOVED PANEL NR 5647796-37 AND REMOVED CORROSION THAT WENT OUT OF LIMITS IAW SRM 51-03-00-0. REPLACED SKIN PANEL NR 5647796-37 IAW SRM 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C2 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 616. STOP DRILLED CRACKED RIB AT STA XFS 616 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 616 IAW SRM 57-02-00 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 672. STOP DRILLED CRACKED RIB AT STA XFS 672 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 672 IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 634. STOP DRILLED CRACKED RIB AT STA XFS 634 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 634 IAW SRM 57-02-00 FIG 2.

Part: BEAM — CRACKED (HORIZONTAL STAB) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RT HORIZONTAL STAB UPPER AFT H-ANGLE CRACKED. REMOVED RT HORIZ STAB UPPER AFT H-ANGLE IAW SRM 51-03-00-0. FABRICATED AND INSTALLED REPAIR H-BEAM ON RT HORIZ STAB IAW DWG 3702464, AND SRM 51-03-00-0.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR INNER DOUBLER POSSIBLE CRACK AT XFS 597 AROUND DRAIN HOLE. REMOVED INNER DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW 57-3-3 FIG 7, 51-1-21.

Part: BULKHEAD — CRACKED (FS 1766 L10R) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 AFT PRESS BULKHEAD RT L10R AREA 2EA CRACKS AT STA 1766. CUT OUT DAMAGED AREA AT STA 1766 L10R IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1766 L10R IAW SRM 53-2-5 FIG 14A, AND SRM TR 53-194. THIS REPAIR REQUIRES A DAMAGE TOLERANCE INSP INITIAL AT 16,000 LANDINGS AND REPETIVE INSP AT 4,000 THERE AFTER IAW TR 53-194.

Part: RIB — CRACKED (RT WING) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 722. STOP DRILLED CRACKED RIB AT STA XFS 722 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 722 IAW SRM 57-02-00 FIG 2.

Part: FITTING — CRACKED (FS 759 L18L) · airframe 79,027 hrs · 26,870 cycles

INSPECTION TYPE:C3 BOOT FITTING CRACKED AT STA 759 L18L. REMOVED AND REPLACED CRACKED BOOT FITTING AT STA 759 L18L IAW UPS EO DC8-5310-22792-B, AND SRM 51-1-20D.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

FOUND EMERGENCY LIGHTS INOP. FOUND WIRE NR L610A20 BROKEN AT TOGGLE SWITCH. REPAIRED WIRE IAW DCI WDM 33-50-01. TOGGLE SWITCH REPLACED AS PRECAUTION IAW DC8 AMM 20-50-01-4. CHECKS SERVICEABLE IAW DC8 AMM 33-50-02-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY PACK INOP. CLEANED AND TIGHTENED CONNECTOR ON EXISTING BATTERY PACK. OPS CKS OK, REF MM 33-50-01-2.

Part: TRACK — LOOSE (COCKPIT)

INSPECTION TYPE:N/A BTB - CAPT'S SLIDING WINDOW WILL NOT OPEN. FOUND TOP FWD WINDOW GUIDE OFF TRACK. TIGHTENED TRACK AND RE-INSTALLED GUIDE. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

ON PREFLIGHT, FOUND EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER MM 33-50-01-2, CHECKS OK.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01-2.

Part: SMOKE BARRIER — UNSECURE (COCKPIT)

SMOKE CURTAIN DIFFICULT TO SECURE ON GROUND. EN ROUTE SMOKE/FIRE CURTAIN DOES NOT REMAIN SECURE AT 6.0 (FL35) D320807 ASSIGNED. *S/D* REPLACED VELCRO PER EO DC8-2550-1873 FINAL REPAIR APP 8.2 COMP.

Part: RIB — CRACKED (LT WING)

CRACK IN RIB AT LT INBD GROUND SPOILER INBD MOUNT FITTING (MARKED). STOP DRILLED CRACK REF SRM 57-02-00 1199249 9/12/05. ACCOMPLISHED HFEC OF AREA NO DEFECTS NOTED. REPAIRED RIB AS PER DC8-SRM 57-02-00-51-1-20 SEE LOG PAGE 418971 M-3 FOR FITTING ASSY-END.

Part: SLIDE — MISINSTALLED (PAX DOOR)

UNABLE TO READ PRESSURE ON EMERGENCY SLIDE ON ENTRY DOOR, NEED TO BE REPACKED. REMOVED AND REPLACED COVER.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT)

02 MASK INOPERATIVE. DEFERRED M302656. REMOVED AND REPLACED 1ST OBSERVER'S 02 MASK PER MM 35-10-08. OPS CHECK NORMAL. THIS CLEARS M302656.

Part: OXYGEN MASK — WILL NOT TEST (COCKPIT)

F/O'S 02 MASK DOESN'T SEAL DURING TEST. REPLACED 02 MASK AT F/O'S POS. OPS & LEAK CHECK GOOD PER MM 35-10-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, TEE BOLT FITTING FROM A-PIT DOOR STA 285 HAS CORROSION AND MISDRILLED HOLES. REMOVED AND REPLACED TEE BOLT FITTING IAW SRM 51-3-0 & 51-1-20D.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

MAIN CABIN , CORROSION ON FLOORBOARD STA 1560,1600 AND 1660, LBL35. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLERS IAW 51-1-8, 53-02-00, 53-02-03 FIG 10 AND 51-1-21.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 REMOVED CORROSION ON FLOORBOARD F86 AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0, 53-2-3 FIG 10, AND 51-1-8.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, LOWER SURFACE OF CABIN FLOORBOARD CORRODED FROM STA 1555 TO 1563 & BL 0 TO RBL 9. BLENDED OUT OF LIMITS AND REPAIRED IAW SRM 53-02-03, 51-1-8, 51-1-21, 51-3-0 AND 51-1-15.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 SPLICE FITTING CRACKED ON L31R AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, B-PIT LONGERON SPLICE FITTING CRACKED (2) STA 610 L31L. REMOVED, MACHINED AND REPLACED LONGERON SPLICE IAW DWG 3750257, 51-1-20D AND 51-1-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 B-PIT DOOR AFT TORQUE BOX LWR FRAME AT STA 580 IS CRACKED BETWEEN L33R AND L33R. FABRICATED AND INSTALLED 2 DOUBLERS AND 1 FILLER AND INSTALLED IAW SRM 53-02-00-0 FIG 001B SHT 3, 53-2-0 FIG 1B, 51-1-21A, 51-1-21 AND EO DC-8 5320-6176-B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

ALL L31L SPLICE FITTINGS (3 TOTAL) CRACKED BETWEEN STA 440-520. REMOVED AND REPLACED ALL (3 EA.) SPLICE FITTINGS IAW SRM 51-20-00, 53-2-2 AND 51-1-20D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

HAT CHANNEL ATTACH ANGLE O/B SIDE CORRODED STA 920-940 RBL 58 RT W/W. REPAIRED BY REPLACEMENT OF I/B AND O/B HAT CHANNEL ATTACH ANGLES, WEB AND FINGER DOUBLER, REPAIR SPLICES. REPLACEMENT RETAINER AND REPLACEMENT PRESSURE PANEL ANGLE, IAW 51-1-21, 53-2-0, 51-3-0, 51-3-2 AND 51-1 -20D.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

C1 C PIT STA 1043 RT CUSP RBL 58, VIEW LOOKING UP AT DISHPAN, 2 CRACKS PERPENDICULAR TO EACH OTHER APPROX 2 INCH IN LENGTH EACH. REPAIRED BY STOP DRILLING AND INSTALLING DOUBLER IAW EO DC8 5330-2159B SRM 51-1-15, 51-1-21A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 A PIT AT DOOR CUTOUT APPROX STA 335 HAS 1 EA CRACKED BACK UP FITTING. REMOVED AND INSTALLED BACKUP FITTING AND SPLICES IAW SRM 53-02-00-05, AND 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, FRAME TO INTERCOSTAL FITTING CRACKED 3 INCH LONG, AT STA 900 L18L. REMOVED, FABBED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2-0, 51-1- 8, 51-1-20D, AND DWG 4779496.

Part: FLOORBOARD — CORRODED (STA 70-140 RBL55) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD CORRODED AT STA 70 TO 140 RBL 55. REMOVED CORROSION AND INSTALLED DOUBLER IAW SRM 51-1-8 AND 51-1-21.

Part: FINGER DOUBLER — CORRODED (WING BOX) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUB FLOOR, FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND CORROSION AT STA 960 TO 980 LBL 65. REMOVED FINGER DOUBLER AND REMOVED CORROSION ON SUB FLOOR. FOUND TO BE WITHIN LIMITS. REPLACED FINGER DOUBLER IAW SRM 51-1-8, DWG 5645332, 53-2-0 FIG 1F AND 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 77,932 hrs · 26,089 cycles

C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 6 INCH OB OF IB END. REPAIRED RIB IAW SRM 57-02-00-0.

Part: RIB — CRACKED (LT WING) · airframe 77,932 hrs · 26,089 cycles

C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 12 INCH OB OF IB END. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 57-2-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 LONGERON CRACKED 2 INCH LONG, AT STA 480 L20R, UPPER AND LOWER FLANGE. REMOVED DAMAGED LONGERON AND INSTALLED LONGERON AND SPLICES FROM FROM STA 460 TO 490 IAW SRM 53-02-02 FIG 11, 53-04-0, 53-04-01 AND 51- 1-8.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, MAIN CABIN AT STA 1280 L11L INTERCOSTAL HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DC-8 DWG 9756811, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

C1 FRAME TO CUSP FITTING CRACKED .25 INCH LONG AT STA 260 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE:C1 FRAME TO INTERCOSTAL ATTACH FITTING CRACKED 1 FT LONG AT STA 837 FWD L13R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (L13R) · airframe 77,932 hrs · 26,089 cycles

C1 FITTING CRACKED 2 INCHES LONG AT STA 760 L13R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, BANANA FITTING CRACKED.25 INCH LONG STA 1220 L33R. REMOVED AND REPLACED BANANA FITTING IAW SRM 51-01-20D AND 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, LONGERON CRACKED .25 INCH LONG AT STA 1726 L10 RT. REPAIRED LONGERON BY INSTALLING DOUBLER AND FILLER IAW SRM 53-02-02 FIG 11, 51-1-20, 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

C1 LONGERON CRACKED .25 INCH LONG AT STA 1746 L14R. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D AND 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

C1 LONGERON .25 INCH LONG CRACKED AT STATION 1726 L15L. REPAIRED LONGERON BY CUTTING OUT DAMAGE. INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, LONGERON CRACKED .5 INCH LONG AT STA 1746 L14L. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW RM 53-02-02, 51-1-20 AND 51-3-0.

Part: RIB — CRACKED (RT WING) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED .25 INCH LONG AT STA XW 754. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 51-1-21, 51-1-20D AND 57-2-0.

Part: SKIN — DAMAGED (STA 262-269 L32R) · airframe 77,932 hrs · 27,016 cycles

INSPECTION TYPE:C1 REMOVE C-1 DOOR JAMB LWR CORNER THAT DOES NOT COMPLY WITH SRM 53-2-0, FIG 22 AND REPAIR PER SRM. REPLACED C-1 DOOR JAMB, LOWER FORWARD CORNER IAW DC8 5330-22155, SAA SK 810-265, 8100-9.

Part: SKIN — DAMAGED (LT WING LE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, LT WING LEADING EDGE UPPER SURFACE 10 FT O/B OF NR 1 ENG STUB WING HAS FASTENER BULGING & PULLED THROUGHT SKIN. INSTALLED DOUBLER AND CONICAL WASHERS IAW SRM 51-1-26 & 57-2-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,932 hrs · 26,089 cycles

INSPECTION TYPE: C1, FUSELAGE EXTERIOR SKIN CRACKED .25 INCH LONG AT STA 1734 L16L-L17L. REPAIRED BY INTALLING FINGER DOUBLER AND DOUBLER IAW SRM 53-2-01, 53-02-01 FIG 007 SHEET 5, 51-1-8, 51-1-20, 51-1-20D, 51-1-21.

Part: SLIDE — DEPLOYED (COCKPIT)

MAIN CABIN EXIT EMERGENCY SLIDE DEPLOYED. REPLACED SLIDE IAW 25-60-00 SECURITY CK GOOD, THIS CLEARS M291801.

Part: SLIDE — DISLODGED (PAX DOOR)

EVACUATION SLIDE ON MAIN ENTRY DOOR FELL OUT OF THE CASE O/B CLIP. OK TO CONTINUE IN SERVICE IAW MEL 57-7-4.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 8 TO 25 AT STA 25 LONG 31L CLIP HAS CORROSION BETWEEN BOLTS. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. MAT ID FOR REP ANGLE 7075-0 .100 FILLER 7075-T6 .090 IAW DC8 SRM 53-3-3 AND REO G09155. HT TRT IAW TPS 1003 REV A 7075-0 CONDITION TO 7075-T6. FAB REPAIR ANGLE AND FILLER IAW G08155. INSTALLED REPAIR ANGLE AND FILLER IAW REO G09155.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, A/C ACCESSORY COMP BETWEEN STA 55 TO 70 BETWEEN LONG 35L TO 35R FRAME 55 IS CORRODED. REMOVED DAMAGED FRAME SECTION FROM L35R-L27L. FAB REPAIR ANGLES AND FRAME SECT IAW DC8 SRM 53-2-0. HEAT TREAT ANGLES & FRAME SECTION IAW TPS 1003 REV A. ALODINED & PRIMED REPAIR ANGLES AND FRAME SECTION IAW DC8 S RM 51-1-8. INSTALLED REPAIR ANGLES AND FRAME SECTION IAW DC8 SRM 53- 2-0 FIG 2 51-1-20D AND 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, A/C COMPARTMENT AT FS 25 L23L FRAME IS CORRODED BEHIND WIRE BUNDLE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE AND FAB REPAIR DOUBLER IAW UPS EO DC8310-11728/DWG DC8-53A-011. HEAT TREAT TO T6 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (C1 DOOR) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, C1 DOOR AFT TORQUE BOX FLOOR SUPPORT FITTING CRACKED AT TWO LOCATIONS. REMOVED SUPPORT FITTING. DRILLED AND INSTALLED NEW FITTING (P/N 97540 55-2).

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, R2 UPPER AFT DOOR JAMB CORNER CRACK NOTED AT LONG 11R EXTENDING FROM FASTENER HOLE. CUT OUT CRACKED AREA, FAB & INSTALLED SKIN FILLER -19 -21 DOUBLERS IAW DC8 SRM 53-2-0 FIG 16. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (JACKSCREW) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, LEFT SIDE VERTICAL ATTACH STRAP FOR JACKSCREW TRIM MOTOR SUPPORT BASE CRACKED AT FASTENER HOLE. REMOVED SUPPORT FITTING IAW DC8 SRM 51-1-21 & 51-3-0. LOCATED AND DRILLED UP SUPPORT FITTING 2649617 IAW DC8 SRM 51-1-21 & 51-3-0. INSTALLED SUPPORT FITTING IAW DC8 SRM 51-1-21 & 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, EMPENNAGE L17L END FITTING AND LONGERON CRACKED FROM FS 1768-1778. REMOVED OLD L17 LT & END FITTING TO FOM. LOCATED DRILLED DEBURRED NEW L17 LT, END FITTING AND INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, EMPENNAGE L17R END FITTING AND LONGERON CRACKED FROM FS 1768-1778. REMOVE L17 RT LONGERON AND FITTING REMOVED SHEAR CLIP AND TEAR STRIP AT FS 1766 & 1708. LOCATED AND DRILLED NEW LONGERON SECTION AND FITTING. INSTALLED LONGERON END FITTING SHEAR CLIP AND TEAR STRAP IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, MAIN CABIN FLOOR PANEL STA 220 PANEL-A FOUND SPLICE CORRODED. REMOVED FLOORBOARD SPLICE, FABRICATED NEW SPLICE IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SPLICE IAW DC8 SRM 5 3-2-3.

Part: FITTING — CRACKED (EMPENNAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, EMPENNAGE L10 LT END FITTING CRACKED FROM 1768-1773. PERFORMED HFEC IAW NDT SPM 06-10-01, .001 CRACK FOUND ON FITTING. REMOVED OLD FITTING TO FOM. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, EMPANAGE RT FITTING CRACKED FROM RBL2 - RBL 8 SECOND J-BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01, .001 CRACK FOUND ON FITTING. REMOVED FITTING TO FOM. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (EMPENNAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, EMPENNAGE LT FITTING CRACKED FROM LBL 2-LBL 8 SECOND J BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01. FOUND CRACK ON FITTING REMOVED FITTING TO FOM. LOCATED DRILLED DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE:C2, FS 1746 L15R-13R CRACKED FUSE SKIN AT VERT FIN CENTER SPAR CANT BLKHD. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR IAW DC8 SRM 53-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR IAW DC8 SRM 51-1-20D.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, STRINGER NR 59 HAS CRACK ABOUT 3 INCHES LONG XRS 408.000 505B 4 ALT. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SRM 51-1-20D AND 51- 3-0 & 51-1-23. LOCATED AND DRILLED AND DEBURRED FITTING (P/N 5644973- 502).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, LOWER RT SECTION FLOORBEAM CORRODED AT STA 879 BL60R WL 10. REMOVED AND FAB NEW SECTION OF FLOORBEAM IAW TIMCO REO G09098. ALODINED AND PRIMED BEAM IAW DC8 SRM 51-1-8. FAB 4 EA CLIPS IAW DAC DWG 5645332. ALODINED AND PRIMED CLIPS IAW DC8 SRM 51-1-8. INSTALLED CLIPS IAW DC8 SRM 51- 1-20D. FAB 4 SPLICE ANGLES IAW TIMCO REO G09098. ALODINED, PRIMED AND INSTALLED ANGLES IAW DC8 SRM 51-1-8 & TIMCO REO G09098.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, RT WING AT STA XF409.6 INBOARD FLAP SUPPORT FITTING CRACKED. REMOVED BOILER PLATE, SLIDER PANEL, INBOARD TRACK, SPRING PANEL, CLOSURE PANEL AND INBOARD BASE FITTING TO FOM. DRILLED AND LOCATED BASE FITTING IAW DAC DWG 5751175. INSTALLED BASE FITTING, CLOSURE PANEL, SPRING PANEL, INBOARD TRACK, SLIDER PANEL AND BOILER PLATE IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, L2 UPPER AFT DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT SKIN EDGE. CRACK LENGTH .1875 INCH LONG FOUND WITH EDDY CURRENT. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FAB FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0, TR 53-158. ALODINED AND PRIMED REPAIR PARTS IAW DC8 SRM 5 1-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 TR 53-158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 55 TO 70 BETWEEN LONG 24L TO 25L FRAME 55 IS CRACKED AT SUPPORT ROD. REPAIRED FRAME 55 BY THE FABRICATION AND INSTALLATION OF FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-0 51-1-21 AND 51-1-21D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 55 TO 70 BETWEEN LONG 24R TO 25R FRAME 55 IS CRACKED AT SUPPORT ROD. REMOVED FRAME SECTION AT FS 56 L21L-L26L. FAB NEW FRAME SECTION AND SPLINE IAW DC8 SRM 53-2-0. ALODINED AND PRIMED FRAME & SPLICE IAW DC8 SR M 51-1-8. INSTALLED FRAME AND SPLINE IAW DC8 SRM 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,958 hrs · 25,318 cycles

INSPECTION TYPE: C2, R1 LWR AFT DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED BETWEEN FASTENERS HOLES. CUT OUT DAMAGE IN SKIN IAW DC8 SRM 53-2-0. FAB FILLER DOUBLER AND TRIPLER IAW DC8 SRM TR 53-154. ALODINED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 TR 53-154 AND DC8 SRM 53-2-0.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY RELAY UNIT IAW MM 33-5 0-01. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: COALESCER BAG — CONTAMINATED (LEFT)

AFTER TAKEOFF AND LEFT PACK TURNED ON, CAUSTIC FUMES FILLED COCKPIT. DECLARED EMERGENCY. RAN FUMES EVAC CHECKLIST WHILE RETURNING TO LAND . AIR TURN BACK. R & R LEFT WATER SEPARATOR SOCK, INSPECTED R-SOCK FOUND NO DEFECTS. LEFT SOCK FUEL FUME SOAKED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, APPROX STA 1690 LONG 30 RT HAS CRACK AT VERY AFT END GEN RFTS N810UP-16-21382, REC REO G07872. FABBED AND INSTALLED REPAIR STRAP IAW REO G07872.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 34L. REPLACED FITTING IAW DC8 SRM 51-1-20D RETORQUED BOLT IAW DC8 SRM 51-3-1 TABLE 3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 34R. REPLACED FITTING IAW DC8 SRM 51-1-20D RETORQUED BOLT IAW DC8 SRM 51-3-1 TABLE 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FLOORBEAM HAS CORROSION UNDER PREVIOUS REPAIR. REPAIRED IAW REO-G07863.

Part: RIB — CRACKED (RT WING) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, RIGHT O/B FIXED L/E HAS CRACK ON L/E OF MATING SURFACE AT FASTENER ATTACH HOLES. FABBED NEW -8 ANGLE AND -11 DOUBLER IAW DAC DWG 9753297, LOCATED AND DRILLED NEW -4 RIB IAW DC-8 SRM 51-1-24. INSTALLED -8 ANGLE, -11 DOUBLER & -4 RIB IAW DC8 SRM 51-1-20D, 51-3-0, 51-1-21, 51-1-21A, 51-1-2 0B, 51-1-20A. INSTALLED FIXED L/E SECTION IAW DC-8 SRM 51-1-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FITTING CRACKED STA 1690 LONG 30R. REPLACED FITTING IAW DC8 SRM 51-1-20D. RETORQUED BOLT DC8 SRM 51-3-1 TABLE 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, SHEAR TIE AT FS 1746, BETWEEN L28R AND L26R CORRODED. REMOVED SHEAR TIE, FABBED NEW SHEAR TIE PER DAC DWG 5612148. ALODINED, PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21D.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, TAIL SKID SUPPORT FITTING CRACKED AT FS 1753 LONG 36. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND DAC DWG 375086 5.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, LEFT NWW TUNNEL, BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO INBD STIFFENER CORRODED. WEB REPAIRED IAW REO-G07874.

Part: PRESSURE PANEL — CORRODED (NLG WW) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, LEFT NWW TUNNEL BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO I/B STIFFENER CORRODED. WEB REPAIRED IAW REO G07874.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FS 1800 L28R LONG DOUBLER CORRODED. DRILLED NEW DOUBLER PER DC8 SRM 53-5-3. ALODINED AND PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.

Part: GUSSET — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PIT FS 1240 GUSSET AT L35R CRACKED. REMOVED DAMAGED GUSSET, FABRICATED NEW GUSSET IAW DAC DWG 9754949. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. GUSSET TO BE INSTALLED ON UPS NR 304036 TIMCO NR 21036.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, COCKPIT SUBFLOOR RT O/B SIDE BETWEEN FS -50.6 & FS -38.6 CORROSION ON FINGER WEB O/B AND BELOW F/E CONTROL PANEL LOWER PULLEY BRACKET ASSY. FABBED FINGER DOUBLERS -21 -27 -25 DOUBLERS FILLER AND -23 SPLICE IAW DAC DWG SRO 8530026. INSTALLED FINGER DOUBLERS DUCTS, PULLEY COVERS AND GROUNDING PANELS IAW DC8 SRM 51-3-0.

Part: GUSSET — CRACKED (AFTCARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PIT FS 1050 GUSSET L31L CRACKED. REMOVED AND REPLACED GUSSET IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO-G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. ALODINED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES INTERCOSTALS AND FITTING/CLIPS IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PIT FS 1240 FRAME CORRODED BETWEEN L36 AND L34R. *S/D* MAT ID FOR REPAIR ANGLES .080 7075-0 IAW REO G07850 CORROSION ON FRAME FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR ANGLES IAW DC8 SRM 51-1-24. ALODINED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES INTERCOSTALS AND FITTING/CLIPS IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FWD CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 340 - 350 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 34R - 35R FITTING IS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW 51-1-20D DC8 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FWD ACC COMPT AT FS 56 - 70 RT CUSP AT LONG 21R IS CORRODED AND CRACKED. *S/D* REMOVED AND REPLACED FITTING P/N 3610130501N IAW DC8 SRM 51-1-21 & 51-3-0.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PTI Z-FITTING CRACK AT STA 1220 BETWEEN L30L AND L29L IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20. REMOVED AND REPLACED FITTING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FWD LWR CARGO AT FS 440 - 460 LONG 34R IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED LONGERON 34R IAW DC8 SRM 51-1-20 DC8 SRM 51-1-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, EXTERIOR FUSELAGE SKIN HAS LG CORROSION BULGE AT LAP SEAM STA 1875.0 S-32-R. REPLACED SKIN PER DAC DWG 5649329.

Part: BULKHEAD — CRACKED (RT HORIZ STAB) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, RT HORIZ STAB JACKSCREW FWD MOUNTING BULKHEAD HAS CRACKS THAT HAVE GONE THROUGH STOP DRILLS 2 EACH. REPAIRED IAW DC8 SRM 53-2-0 FIG 23.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FWD LWR CARGO PIT AT FS 280 AT LONG 33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, FWD BAG PIT CRACK UNDER UPPER FLANGE OF FRAME 420 AT LONG 29L. REMOVED SUPPORT, FABBED SUPPORT, ALODINED, PRIMED AND INSTALLED CHANNEL SUPPORT IAW DAC DWG 3773159 DC8 SRM 51-1-21 & 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, MAIN CABIN L21RT SHORT FRAME TO CUSP FITTING CRACKED AT FS 1170. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: SPLICE — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1040 - 1060 LONG 35L IS CRACKED AT SPLICE FITTING. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.

Part: SPLICE PLATE — CORRODED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT PIT LONGERON 36 SPLICE PLATE CORRODED AT FS 1270. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: SPLICE PLATE — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: TORQUE BOX — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3 MAIN CABIN FS 390 L12RT TORQUE BOX WEB CRACKED. FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1200 BETWEEN LONG 27L-28L Z-FITTING IS CRACKED. REMOVED AND REPLACED FITTING. ALODINED AND PRIMED SPLICE IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1150 - 1160 AT LONG 33R Z-FITTING IS CRACKED. REMOVED CRACKED Z-FITTING, BACK UP FITTING DOOR JAMB FITTING AND ANGLE SPLICE. LOCATED AND DRILLED, DEBURRED NEW Z-FITTING INSTALLED NEW Z-FITTING BACK UP FITTING DOOR JAMB FITTING AND ANGLE SPLICE.

Part: FITTING — CORRODED (CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN L33R-L34R Z-FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 BETWEEN LONG 29L-30L Z-FITTING IS CORRODED. Z-FITTING OUT OF LIMITS IAW DC8 SRM 53-2-0. RCVD FITTING P/N 375584-2- 2N PO 699381 MAT ID FOR REPAIR ANGLES BAC 1505-101167 EXTRUSION .12 5 7075-T6571 IAW DC8 SRM 53-2-0. FABD REPAIR ANGLES IAW DC8 SRM 53-2- 0. ALODINED AND PRIMED IAW 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW 51-1-20D.

Part: SPLICE PLATE — CRACKED (AFT CARGO BAY) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3 AFT PIT LONGERON 31L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: SPLICE PLATE — CRACKED (AFT PIT) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3 AFT PIT, LONGERON 34L SPLICE PLATE CRACKED AT FS 1270. REMOVED CRACKED 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 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1220 - 1230 INSIDE X-SLIDE DOOR AFT TORQUE BOX AT LONG 33R Z-FITTING IS CORRODED. REMOVED Z-FITTING FOR ACCESS IAW DC8 SRM 51-1-20D. REMOVED CORROSION LONGERON AND PRIMED IAW DC8 SRM 51-1-8. Z-FITTING. REMOVED FOR ACCESS WAS NOTED CRACKED RECD LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, FAB REPAIR DOUBLERS IAW 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3, AFT LWR CARGO PIT AT FS 1160 - 1220 AT LONG 26L WEB SKIN IS PUNCTURED AND CRACKED. REMOVED DAMAGED WEB, FABBED NEW WEB IAW DAC DWG 9753776. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED WEB IAW DC8 SRM 51-1-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,657 hrs · 24,452 cycles

INSPECTION TYPE:C1/3 LT AFT PRESSURE BULKHEAD STA 1766 APPROX L11L IS CRACKED. REPAIRED AREA IAW DAC DWG SRO 8530007.

Part: INDICATOR — DAMAGED (NR 4 ENGINE RPM)

INSPECTION TYPE:N/A, PASSING 13,000 FT A SWEET CHEMICAL SMELL OR ODOR WAS NOTICED. TURNED A/C PACKS OFF ONE AT A TIME AND WHEN LEFT PACK WAS OFF ODOR DECREASED. AFTER LEVEL OFF ODOR GOT WORSE. DECIDED TO DIVERT TO MCO AND RAN FUMES EVACUATION CHECKLIST. AFTER LANDING AND OPENING COCKPIT WINDOW ODOR SEEMED TO DISSIPATE BUT STILL PRESENT IN COCK. T/S SYSTEM RUN, LT PACT NOTED SWEET SMELL. CHECK BOTH LT & RT ACM''S AND WATER SEPARATOR BAGS, NO PROBLEM NOTED. ALSO NOTED THAT THE NR 4 N2 RPM INDICATOR IS PEGGED AND DIGITAL DISPLAYED IS BLANK, C/B IS IN. REMOVED N2 INDI IT HAD A STRONG SWEET SMELL AND WAS VERY HOT. REPLACED AND CHECK A/C WIRING PER WDM77-10-01, ALL CHECKED NORMAL.

Part: GAUGE — INOP (HYD SYSTEM)

REVERSER HYDRALIC PRESS GAUGE INDICATES ZERO WITH HYD S/O SWITCH OFF WITH SWITCH IN THE OPEN POSITION ABLE TO GET ALL 4 REVERSORS ON LANDING ROLL. REPLACED HYD PRESS GAUGE AND TRANSMITTERS. OPS CHECK OK, NO LEAKS.

Part: SKIN — DENTED (NR 1 TR UNIT)

INSPECTION TYPE:N/A, DENT IN NR 1 ENGINE OUTBOARD THRUST REVERSER AT 4 O'CLOCK POSITION REF D175215. INSTALLED REPAIR DOUBLER PER CFM MM 78-30-00.

Part: ANGLE — CORRODED (BS 1320)

INSPECTION TYPE-C2, AFT PIT FLOORBEAM ATTACH ANGLE AT FS 1320 RBL10 CORRODED ON UPPER SURFACE. CUT OUT DAMAGED AREA AND FABRICATED ATTACH ANGLE AND SPLICE ANGLE IAW REO6375 AND DAC DWG 9887940.

Part: WEB — CRACKED (WHEEL WELL)

INSPECTION TYPE-C2, AFT L24L SUB-STRUCTURE DOOR JAM WEB HAS A CRACK IN FLANGE RADIUS ACID TEST FOR MATERIAL ID IAW MIL-STD-271F. RECEIVED MATERIAL VERIFICATION, FABBED DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 53-2-0.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-C2, FITTING CRACKED FS 940 AT L24R. FITTING INSTALLED ON UPS N/R 875503.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE:C2 BATHTUB FITTING AT FS 920 LEFT LONGERON 24 IS CRACKED AND CORRODED. DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-20D. FINAL INSTALLATION ON UPS N/R 875504.

Part: SKIN — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C2, LT ELEV UPPER SKIN CRACKED STA XE77. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1, FABBED REPAIR DOUBLER AND FILLER IAW DC8 SRM 55-2-1, ALODINED IAW DC8 SRM 51-1-8, COLD BONDED REPAIR AND SEALED DOUBLER IAW DC8 SRM 51-1-9A, INSTALLED DOUBLERS IAW DC8 SRM 51-1-21A.

Part: LONGERON — CORRODED (BS 1230-1240)

INSPECTION TYPE-C2, AFT PIT STA 1230 TO 1240 LONGERON 33L CORRODED. REMOVED LONG, SHEAR TIE AND FITTINGS, FABED LONGERON, SHEAR TIE SPLICE, SPLICE ANGLES FOR FITTINGS AND FITTINGS IAW DC8 SRM 51-1-8, DAC DWG 9758504, SRM 51-1-20D, 53-4-1, 53-2-0. INSTALLED ALL IAW DC8 SRM 51-1-20D, 53-4-1, 53-2-0.

Part: LONGERON — CORRODED (BS 1198)

INSPECTION TYPE-C2, LONG 33L AT STA 1190 CORROSION. FAB REPAIR ANGLE IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-2.

Part: FRAME — CORRODED (BS 1700)

INSPECTION TYPE:C2 CABIN AFT STA 1700 CANTER FRAME CORRODED AND CORROSION BETWEEN VERTICAL ATTACH PLATE L-36. CUT OUT CORRDED FRAME SECTION, VERTICAL ATTACH OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED NEW REPAIR ANGLE AND VERTICAL ATTACH PLATE AND SHIMS IAW REO 06339. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FRAME REPAIR AND VERTICAL PLATE IAW REO-06339 DC8 SRM 51-1-20D, 51-3-0, 51-1-8.

Part: FRAME — CORRODED (BS 1000)

INSPECTION TYPE:C2 AFT PIT UPPER FRAME CAP AT FS 1000 EXFOLIATION CORROSION ON FRAME CAP AT L34R AND 33 OUT OF LIMITS, MAT ID AND FABRICATED DOUBLER REPAIR END SHIM IAW REO-06348. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER REPAIR AND SHIM IAW REO-06348.

Part: INTERCOSTAL — CHAFED (BS 20)

INSPECTION TYPE:C2, FLT CABIN INTERCOSTAL CHAFED THROUGH AT STA 20 LBL 10 MAT ID, LOCATE, DRILL, DEBURRED, AND INSTALL IAW DC8 SRM 53-2-0, 51-1- 8, DWG 5641543.

Part: SUPPORT — CRACKED (BS 1460)

INSPECTION TYPE-C2, AFT PIT FS 1460 FLOOR SUPPORT CRACKED AT L34L. REMOVED CRACKED SUPPORT FITTING, FAB NEW FITTING, ALODINED AND PRIMED, INSTALLED IAW DC8 SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 960-980)

INSPECTION TYPE-C2, BELOW CABIN FLOOR STA 960 TO 980 X=0 CORR AT FINGER DOUBLER OUT OF LIMITS. ALSO, FOUND CRACK. FABRICATED DOUBLER, FILLER AND REPAIR DOBULER IAW REO-06349. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: FLOOR — CORRODED (BS 65)

INSPECTION TYPE:C2 FLT CABIN FLOOR PRESSURE PANEL DOUBLER BULGED AND NUMEROUS RIVETS POP PED AT STA 65 LBL OUT OF LIMITS. FABRICATED REPAIR DOUBLER IAW DAC DWG SRO8530026. FABRICATED CHANNEL DOUBLER IAW DAC DWG 5612289. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 920-940)

INSPECTION TYPE-C2, BELOW CABIN FLOOR, STA 90 TO 940 X=O FINGER DOUBLER CORRODED. REMOVED FINGER DOUBLER, FOUND DOUBLER OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0, FABBED NEW DOUBLER IAW DAC DWG 5645332, ALODINED AND PRIMED IAW DC- 8 SRM 51-1-8, INSTALLED DOUBLER IAW DC-8 SRM 51-1-8 AND 51-1-21.

Part: DOUBLER — CORRODED (CABIN)

INSPECTION TYPE:C2 FLT CABIN FLOOR PRESSURE PANEL DOUBLER BULGED AND NUMEROUS RIVETS POPPED AT STA 65 LBL 20 OUT OF LIMITS. FABRICATED FINGER DOUBLER REPAIR IAW DAC DWG 5612298. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 92)

INSPECTION TYPE-C, FUSE EXT, KEEL BEAM STA 92 RT BEAM FITTING HAS A VISIBLE CRACK IN INBOARD RADUS. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING (P/N 375851950 1) IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-C2, MAIN CABIN STA 680 AND 46 RBL 2-WL FITTING CRACKED AFT SIDE OF FLOORBEAM. REMOVED CRACKED FLOOR SUPPORT FITTING AT STA 680, RBL 46 LOCATED, DRILLED NEW FITTING IAW DC-8 SRM 51-3-2, INSTALLED NEW FITTING AT STA 68 0, RBL 46 IAW DC-8 SRM 51-1-20D.

Part: FRAME — CORRODED (BS 180)

INSPECTION TYPE-C2, FRAMED CORRODED STA 180, L35L TO L36. FABRICATED REPAIR DOUBLER (AFTER REMOVING CORROSION IAW DC8 SRM 51-1-8 IAW REO-06386 AND DC8 DWG DC08-53-0229. INSTALLED PER DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 80)

INSPECTION TYPE-C2, CABIN FLOOR PRESSURE PANEL DOUBLER BULGED STA 80 RBL 20. REMOVED FINGER DOUBLER, MAT ID FROM DOUBLER SRM 53-3-3. FAB DOUBLER IAW DAC DWG 5612298, INSTALLED IAW DC8 SRM 51-1-20D.

Part: SKIN — DENTED (RT AILERON)

INSPECTION TYPE-C, RT WING AILERON DENTED IN UPPER SKIN. CUT OUT DAMAGE, FABBED REPAIR DOUBLER IAW DC8 SRM 57-2-1- FIG 2, INSTALLED DOUBLER IAW DC8 SRM 51-1-21A (W & B DONE ON UPS NR 876762).

Part: FITTING — CRACKED (BS 1166)

INSPECTION TYPE:C2 C-3 DOOR, LOWER NR 1 T-BOLT FITTING CRACKED. REMOVED DOOR LATCH FITTING, DRILLED NEW FITTING, AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: LONGERON — CORRODED (BS 160-180)

INSPECTION TYPE-C2, FWD PIT STA 160 TO 180 LONGERON 36 CORRODED. REMOVED AND REPLACED LONGERON AND SPLICE REPAIR PER DC8 SRM 53-4-1, MAT ID IS IAW DC8 53-4-1. ALODINED, PRIMED AND INSTALLED IAW DC8 53-2-2.

Part: SUPPORT — CORRODED (BS 180)

INSPECTION TYPE:C2 CORROSION ON FLOORBOARD SUPPORT AT NUTPLATES FS180, 37 ABOVE L27R BLENDED BEYOND LIMITS IAW DC8 SRM 53-2-0, MATERIAL ID 7075-T6 X .050 AND 7075T6 X .032 PO NR 282694 AND PO NR 278914, DC8 SRM 51-2-0 AND DWG NR 37730777, FAB DOUBLER, LOCATE DRILLED AND DEBURRED IAW DC8 SRM 51-2- 0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1- 20D.

Part: FITTING — CRACKED (BS 702)

INSPECTION TYPE-C2, MAIN CABIN AT STA 702 AND 23 RBL AND 1-WL FITTING CRACKED AFT SIDE OF FLOORBEAM. REMOVED CRACKED FITTING AT STA 702, RBL 23, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2, INSTALLED NEW FITTING IAW DC8 51-1-20D.

Part: BRACE — CORRODED (BS 580)

INSPECTION TYPE-C, FLOORBEAM BRACE CORRODED AT STA 580, RT SIDE ABOVE L27R. REMOVED CORROSION IAW DC8- SRM 51-1-8, FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — GOUGED (BS 1040)

INSPECTION TYPE-C2, STA 1040 TRACK G SCALLOPS GOUGED. REMOVED DAMAGED SEAT TRACK, FAB SEAT TRACK AND SPLICES IAW DC8 SRM 5 3-2-3. ALODINED AND PRIMED IAW SRM DC8 51-1-8, INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-C2, MAIN CARGO DOOR AFT FRAME AT DOOR CUTOUT CRACKED ATTACH ANGLE DAMAGED TRIM. REMOVED FRAME SCUFFPLATE, FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51-1-8. INSTALLED DOUBLER ON FRAME SCUFFPLATE WITH RIVETS IAW DC8 SRM 51-1-21. INSTALLED FRAME SCUFFPLATE WITH RIVETS AND SCREWS IAW DC8S RM 51-1-21 AND 51-3-0.

Part: SEAT TRACK — GOUGED (BS 940)

INSPECTION TYPE-C2, STA 940 TRACK HAS A SCALLOP GOUGED AND TANG BROKEN OFF. REMOVED SEAT TRACK FROM SPLICE TO SPLICE. LOCATED AND DRILLED NEW SEAT TRACK (2 EA) AND SPLICE IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0.

Part: RUB STRIP — DAMAGED (LT MLG DOOR)

INSPECTION TYPE-C2, LT MLG DOOR FWD RUB STRIP WORN AND GOUGED. CUT OUT DAMAGED AREA, FAB REPAIR PARTS, FILLER ANGLES AND STRAP. WELDED DOUBLER, DYEPENNED CK REPAIR ANGLES. NO CRACKS. INSTALLED IAW REO 06324.

Part: LONGERON — CRACKED (BS 879)

INSPECTION TYPE-C, L24R CRACKED AT STA 879. REMOVED AND REPLACED L24R IAW TIMCO SERVICE SKETCH 010123, DC8 SRM 5 10-1-8, 51-1-24, 51-1-20D, 51-3-0, DC8 MM 20-50-01 AND WDM 32-60-03 AND 20-50-01.

Part: INTERCOSTAL — CORRODED (BS 1100-1120)

INSPECTION TYPE:C2 AFT PIT INTERCOSTAL AT L33R FS 1100-1120 CORRODED BEYOND LIMIT. REMOVED INTERCOSTAL FROM STA 1100 TO 1120 AND L33R. FORMED AND HEAT TREATED INTERCOSTAL IAW DAC DWG 9754969. LOCATED AND DRILLED IAW DAC DWG 9754949. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DAC DWG 975 4949 AND DC8 SRM 51-1-8.

Part: INTERCOSTAL — CORRODED (BS 1120-1140)

INSPECTION TYPE-C2, AFT PIT INTERCOSTAL AT L33R FS 1120 TO 1140 CORRODED BEYOND LIMIT. REMOVED INTERCOSTAL, FORMED NEW INTERCOSTAL IAW DAC 9754949. HEAT TREATED IAW DAC DWG 9754949. LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED IAW DAC DCWG 9754949 ADN DC8 SRM 51-1-20D.

Part: SKIN — DENTED (BS 1463)

INSPECTION TYPE-C2, SKIN AT STA 1463, LONG 24R DENTED. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND CUT OUT DAMAGE SKIN IAW SRM 53-2-1, FABRICATED DOUBLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8S SRM 51-1-8. INSTALLED DOUBLERS IAW SRM 53-2-1.

Part: FLOOR — CRACKED (CABIN)

INSPECTION TYPE:C2 AFT FLOOR PANEL F216A IS CRACKED. FABRICATED NEW PANEL IAW DAC DWG 5755032. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: SKIN — CRACKED (L1 DOOR)

INSPECTION TYPE:C2 L-1 DOOR LWR FWD CORNER, SKIN TORN AND CRACKED. REMOVED OLD DOUBLER REPAIR AND TRIM OUT DAMAGED AREA IAW DC8 SRM 52-2-0 MAT ID IAW DAC DWG 561-5403 AND DC8 SRM 52-3-1. HEAT TREATED IAW TPC 1003 REV A . FABRICATED CORNER FILLER IAW DC8 SRM 52-3-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20A AND 51-1-21.

Part: FITTING — CORRODED (BS 902)

INSPECTION TYPE-C2, SHIM BATHTUB FITTING AT STA 902 LT IS EXFOLIATED. REPLACED FITTING AND FABRICATED DOUBLER IAW REO-06350. INSTALLED ON N/R 876781.

Part: LONGERON — CORRODED (BS 70)

INSPECTION TYPE-C2, CORROSION BETWEEN LONGERON SPLICE FITTING AND LONGERON 34R AND BETWEEN FITTING AND FRAME STA 70. CORROSION OUT OF LIMITS. CUT OUT FRAME SECTION, REPLACED IAW DC8 SRM 51-1-24, 53-2-25, 51-3-0, 51-1-20D.

Part: FRAME — CORRODED (BS 1020)

INSPECTION TYPE-C2, AFT PIT UPPER FRAME FLANGE AT FS 1020 CORRODED UNDER NUT PLATE AT L35L AND L34R. CORROSION OUT OF LIMITS. FAB REPAIR ANGLE AND REPAIR FILLER IAW DC8 DD 53.0229. ALODINED AND PRIMED, REPAIRED PARTS AND INSTALLED IAW DC8 SRM 51-1-2, 51-1-20 D, AND 51-1-16.

Part: FRAME — CORRODED (BS 980)

INSPECTION TYPE-C2, AFT PIT FS 980 FRAME CAP CORRODED AT L35L AND BETWEEN L35R AND L34R. CORROSION OUT OF LIMITS. DYE PEN SHOWED CRACK IN FRAME CAP. REPLACED CAP ANGLE IAW REO-06336, FABED INTERCOSTAL IAW DWG 57299201.

Part: FRAME — CORRODED (BS 1060)

INSPECTION TYPE-C2, AFT PIT UPPER FRAME FLANGE AT FS 1060 L36 CORRODED BEYOND LIMIT. REMOVED FRAME CAP, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND FILLER, ALODINED AND PRIMED, INSTALLED REPAIR ANGLE FILLER AND FRAME CAP.

Part: RIB — CRACKED (BS 1910)

INSPECTION TYPE-C2, CRACKED RIB JUST FWD OF THE TAIL CONE ACCESS PANEL 62, RT SIDE FS AREA 1910. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0, STOP DRILLED CRACK IAW 53-2- 0, LOCATED AND DRILLED DOUBLER IAW DC-8 SRM 52-3-2, ALODINED AND PRIMED DOUBLER IAW DC-8 SRM 51-1-18, INSTALLED DOUBLER IAW DC-8 SRM 51-1-20 D.

Part: FRAME — CORRODED (BS 1120)

INSPECTION TYPE-C2, AFT PIT FRAME CAP AT FS 1120 HAS SEVERAL MISSING FASTENERS AND CORRODED NUT PLATES. FABRICATED REPAIR ANGLES, FILLERS, ALODINED AND PRIMED. REMOVED FRAME CAP, CLEANED CORROSION. REMOVED INTERCOSTAL, CLEANED CORROSION. INSTALLED REPAIR ANGLES, FILLERS, FRAME CAP AND INTERCOSTAL IAW DC8 SRM 51-1-21 AND TIMCO DWG DC08-53-0229.

Part: RIB — CRACKED (BS 1920)

INSPECTION TYPE-C2, TAIL CONE THRU PANEL 62 ACCESS, CRACKED RIB LT SIDE, FS 1920 AREA AT BRACKET. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0, STOP DRILLED IAW DC-8 SRM 53 -2-0, LOCATED AND DRILLED DOUBLER IAW DC-8 SRM 51-3-2, ALODINED AND PRIMED DOUBLER IAW DC-8 SRM 51-1-8, INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 240)

INSPECTION TYPE:C2 FWD PIT FS240 LONG 30R HAS CORROSION UNDER LONG SHIM FROM PREVIOUS BLEND OUT AREA OF SKIN. REMOVED LONG 30R AND END FITTING. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER IAW DC8 SRM 53-2-0. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: BRACKET — CORRODED (SPOILER CONTROLS)

INSPECTION TYPE:C2 LWW, FWD OF SPOILER LATERAL CONTROL MECHANISM BRACKET CORRODED. REMOVED SPOILER MINER MECHANISM AND REMOVED BRACKET AND VERIFIED MAT ID. BYE PEN TEST MIL STD 271F. NO CRACK NOTED. ALODINED AND PRIMED AND INSTALL. OPS CK TO BE DONE ON UPS T/C 875296.

Part: BATTERY PACK — DISCHARGED (CABIN)

EEL INOP. REMOVED AND REPLACED EEL BATTERY PACK, OPS CHK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EEL ONLY STAY ON FOR A FEW SECONDS IN TEST. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD P/N ON 5708458-503 P/N OFF 60-1223-5 S/N ON FTL 1007 S/N OFF 327.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE-N/A, RT WING LOWER ACCESS PANEL CRACKED AT O/B OF I/B SLOT CUTOUT. PANEL REPLACED.

Part: WEB — CRACKED (BS 859)

INSPECTION TYPE:C, VERTICAL WEB AT F/S 859 CRACKED AT OUTBD END OF WEB. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-4-0, DWG 5640720, SRM 51-1-21.

Part: STIFFENER — CRACKED (WS 520.168)

INSPECTION TYPE-C, L/W VERTICAL STIFFENER ON FWD SPAR AT NR 1 PYLON STUB WING I/B LWR ATTACH AREA IS CRACKED APPROX STA XS 520.168. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW SRM 51-1-20D.

Part: REAR SPAR — CRACKED (RT MLG WW)

INSPECTION TYPE-C, RT WHEEL WELL SPAR AT STA 860 RBL 39 TO RBL 61 CRACKED. REPAIRED IAW DOUGLAS SERVICE REWORK DWG SRO8570009.

Part: FITTING — CORRODED (BS 809)

INSPECTION TYPE-C, FS 809 LBL 50 FLOORBEAM ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 810-646.

Part: WEB — CORRODED (BS 808)

INSPECTION TYPE-C, WEB CORRODED FS 808 LBL 50 ABOVE CENTER WING BOX. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CORRODED (VERT STAB)

INSPECTION TYPE-C, VERTICAL STAB L/E SKIN AT STA ZFS 179.00 CORROSION OUT OF LIMITS. REPAIRED IAW SRM 55-2-1.

Part: SKIN — CORRODED (WS 272-276)

INSPECTION TYPE-C, THE L/WING I/B STUB WING UPPER SKIN STA XFS 272.75 TO 276 HAS CORROSION REMOVAL BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5720-7767A.

Part: DOUBLER — CRACKED (BS 120)

INSPECTION TYPE-C, FINGER DOUBLER BELOW PILOTS CONTROL COLUMN CRACKED AT FASTENER HOLE. REPAIRED IAW SRM 53-3-2, 53-2-0, 51-1-20D.

Part: SKIN — CORROSION (HORZ STAB)

INSPECTION TYPE-C, THE LT HORIZONTAL STAB L/E SKIN AT STA XFS 178.75 HAS CORROSION REMOVAL AREA BEYOND ALLOWABLE LIMITS. REPAIRED IAW SRM 55-2-1 AND 51-1-21.

Part: SKIN — CRACKED (WS 635)

INSPECTION TYPE:C, L/WING O/B L/E UPPER SKIN AT STA XFS 635.0 IS CRACKED BEYOND LIMITS. REPAIRED IAW SRM 57-2-1, 51-1-21, 51-1-29D.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE-C, SUPPORT FITTING CORROSION REMOVAL OUT OF LIMITS FS 879 LONGERON 24R IN RT WHEEL WELL. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-3-0, 53-2-0.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-C, CHANNEL CRACKED AND CORRODED FS 940 LONG 24L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 5710350.

Part: FLOORBEAM — CRACKED (BS 1660)

INSPECTION TYPE-C, FLOORBEAM CRACKED AT BOLT HOLE FS 1660 LBL 44. REPAIRED IAW DHC SK-810-602.

Part: SKIN — CORRODED (WS 18-32)

INSPECTION TYPE:C LT WING INBD L/E UPPER SKIN STA XFS 18.0 TO XFS 32.5 CORROSION REMOVAL WAS BEYOND LIMITS. REPAIRED IAW SRM 57-2-1.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE-C, LT WING L/E RIB IS CRACKED AT STA XOID 6.225 ABOVE THE PNEU DUCT. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 71.5)

INSPECTION TYPE-C, L/WING UPPER SKIN STA XRS 71.5 AT STR 11 IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-1.

Part: DOUBLER — CORRODED (BS 100)

INSPECTION TYPE-C, FINGER DOUBLER BELOW PILOTS CONTROL COLUMN IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-3-3 AND DWG 5612296.

Part: SEAT TRACK — CORRODED (BS 725/734/763)

INSPECTION TYPE-C, FS 725 TO 734 LBL 59.5 THE SEAT TRACK HAS HEAVY CORROSION. ALSO, AT FS 763. REPAIRED TRACK IAW SRM 53-2-3, 51-3-0.

Part: FITTING — CRACKED (BS 1149)

INSPECTION TYPE-C, FS 1149 ABOVE STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOOR STOP — CRACKED (BS 1200)

INSPECTION TYPE:C, C-3 CARGO COMP, F/S 1200 STR 27L, DOOR STOP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 53-2-0, AND DWG 3755854.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-C, THE LT WING L/E RIB AT THE OTBD END OF THE UPPER SLOT DOOR IS CRACKED PAST THE STOP DRILL. REMOVED AND REPLACED PAN ASSY IAW SRM 51-1-21, 51-1-20D, 51-3-0, AND DWG 5769857.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE-C, C-3 CARGO COMP AT DOOR OPENING AFT END FLOORBEAM SUPPORT FITTING IS CRACKED AT BOTTOM BTWN BOLT HOLES FS 1220. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 9754024.

Part: FITTING — CORRODED (BS 1159)

INSPECTION TYPE-C, FS 1159 ABOVE STR 35R (INSIDE TORQUE BOX) TIE DOWN FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 810-273.

Part: SKIN — CORROSION (RT TE FLAP SLOT)

INSPECTION TYPE-C, RT O/B SLOT VANE I/B END ON L/E HAS AREA OF HEAVY CORROSION AND SCREWS PULLING THROUGH SKIN. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CORROSION (CARGO COMPT)

INSPECTION TYPE-C, NR 3 PIT FLOORBEAM SUPPORT FITTING TO FLOORBEAM TIE FITTING HAS HEAVY CORROSION ON EDGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0, 51-1-21, 51-1-20D, AND DWG 9754002.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE C-1, CARGO COMP AT STA 280 RT SIDE, FLOORBEAM SUPPORT FITTING IS CRACKED AT TOP. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20 AND DWG 9754024.

Part: RIB — CRACKED (WS 696)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 696.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0.

Part: PULLEY BRACKET — CRACKED (RT MLG WW)

INSPECTION TYPE-C, L-ANGLE CRACKED ON BACK SIDE OF SPOILER PULLEY BRACKET RT W/W CENTER O/B. REMOVED AND REPLACED BRACKET IAW SRM 51-1-21.

Part: FITTING — CORROSION (BS 920)

INSPECTION TYPE-C, RT MLG W/W 920 FITTING ON TOP OF LONGERON 24 HAS BLOWN OUT CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: SKIN — CORRODED (WS 257)

INSPECTION TYPE-C, LT WING L/E SKIN AT STA XW257, AT THE L/E, JUST OTBD OF THE NR 2 PYLON, IS CRACKED AND HAS EXFOLIATED CORROSION. REPAIRED IAW SRM 57-2-1.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE:C, SUPPORT FITTING TO LONG 24R AT F/S 960 CRACKED FWD SIDE OF FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 397.75 IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.

Part: INTERCOSTAL — CRACKED (FS 70)

INSPECTION TYPE:C, C-1 PIT FWD BULKHEAD RT SIDE BOTTOM CORRODED AND CRACKED F/S 70. REPAIRED INTERCOSTAL IAW SRM 53-2-0 AND 51-1-21.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C C-1 CARGO COMPT AT F/S 280 RT SIDE, INSIDE TORQUE BOX. FITTING UNDER FLOOR BEAM SUPPORT FITTING IS CRACKED AT TOP MOUNT BOLT HOLE. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3754025.

Part: DOUBLER — CORRODED (BS 1652)

INSPECTION TYPE-C, FS 1652 BTWN STR 27R TO 32R, SKIN HAS HEAVY CORROSION AND EXTENDS UNDER FINGER DOUBLER AND TEAR STRAP (3 PLCS) FS 1663 ALSO. REMOVED DOUBLER, CORROSION ON SKIN (IN LIMITS), FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1, 51-1-21 AND DWG 5773311.

Part: FLOORBEAM — CRACKED (BS 1560)

INSPECTION TYPE-C, F/S 1560 FLOORBEAM IS CRACKED AT RT ATTACH FITTING (FWD SIDE). REPAIRED IAW DHC SK 810-059.

Part: DOUBLER — CORRODED (BS 1652)

INSPECTION TYPE:C, F/S 1652 BTWN STR 28L TO 32L, INTERNAL DOUBLER IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-20, AND DWG 5615377.

Part: FITTING — CRACKED (BS 1580)

INSPECTION TYPE-C, FS 1580 AT STR 21L FLOORBEAM END FITTING IS CRACKED BTWN 2 ATTACH BOLTS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DHC SK-810-058.

Part: FITTING — CRACKED (BS 640)

INSPECTION TYPE-C, FS 640 AT LONG 36, THE RT FRAME TO LONGERON FITTING IS CRACKED IN TWO. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 660)

INSPECTION TYPE-C, FS 660 AT LONG 36 BOTH THE LT AND RT FRAME TO KEEL BEAM ATTACH FITTINGS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTINGS IAW SRM 51-1-20D AND DWG 3750497.

Part: SPLICE — CRACKED (BS 640)

INSPECTION TYPE-C, FWD ACCY COMPT FS 640 TO 660, LONG 30.5R THE LONGERON SPLICE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2-0, 51-1-20D, AND DWG 5800471.

Part: ACTUATOR — DAMAGED (RT MLG)

CREW REPORTED, UPON LOWERING GEAR NO DOWN AND LOCKED INDICATION ON RT MAIN GEAR WITH ASSOCIATED GEAR INDICATION AND DOOR NOT LATCH LIGHTS. CYCLED GEAR AND CHECKED LIGHTS WITH NO HELP. COMPLETED FLY-BY AND ALL PERTINANT CHECKLISTS NORMAL LANDING AND ROLLOUT. REMOVED AND REPLACED RT MAIN GEAR BUNGEE ACT, OPS CK OK.

Part: FITTING — CORRODED (FS 1220)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON B/T FITTING LONGERON 33R-34R, F.S. 1220. REPLACED FITTING PER SRM 53-2-0.

Part: FLOORBEAM — CORRODED (FS 55)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FLOORBEAM FS 55 LBL 37. REPLACED PER UPS EO DC8-53-1547.

Part: SUBFLOOR WEB — CORRODED (FS 45)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON SUBFLOOR WEB FWD ENTRY DOOR FS 45. REPAIRED PER SRM 53-2-0 AND SRM 51-1-2.

Part: FITTING — CORRODED (FS 1220)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED B/T FITTING HEAVY CORROSION ON LONGERON 33R, F.S. 1220. REPLACED FITTING PER SRM 53-2-0.

Part: FLOORBEAM — CORRODED (FS 760)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK AT FLOORBEAM TO WING L-ATTACH ANGLE LBL 40 FS 760. REPLACED ANGLE PER SRM 51-2-20D.

Part: LONGERON — CORRODED (FS 490-510)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, HEAVY CORROSION ON OUTBOARD SIDE OF LONGERON 31L F.S. 490 - 510. REPAIRED PER UPS E.O.

Part: ANGLE — CRACKED (HORIZ STAB)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT HORIZ STAB LEADING EDGE I/B SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 330-360)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON LONGERONS 36 AND 35 AND FITTINGS F.S. 330-360. REPAIRED LONGERONS PER SRM 53-2-2, FIG. 10, AND REPLACED FITTINGS PER SRM 51-1-20D.

Part: ANGLE — CORROSION (FS 798)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON VERTICAL ATTACH ANGLE AND WEB FS 798, RBL 40. REPLACED ANGLE PER SRM 51-1-21.

Part: ATTACH ANGLE — CORRODED (FS 300)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ATTACH ANGLE, F.S. 300, LONGERON 27R. REPLACED ANGLE PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 802)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION ON MAIN CABIN VERTICAL ATTACH FITTING, FS 802, RBL 40. REPLACED FITTING PER SRM 51-1-20D.

Part: STIFFENER — CORRODED (BS 280-290)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON STIFFENER BETWEEN STA 280 - 290, LONGERON 31R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 260)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MAIN CABIN BELT FRAME END FITTING CRACKED AT FS 260 LONG 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: TORQUE BOX — CORRODED (FS 1660)

MAINTENANCE REPORTED, HEAVY CORROSION MAIN CABIN AT LOWER AFT TORQUE BOX AFT ENTRY DOOR FS 1660, LONG 21L. REPAIRED PER SRM 53-2-0 AND SRM 51-1-20D.

Part: FLAP TRACKS — CORRODED (WS 97)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION PITS ON FLAP TRACKS RT WING STA 97. REPLACED TRACKS PER MM 27-50-03.

Part: SLIDE — DAMAGED (PAX DOOR)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FWD ENT DOOR SLIDE PACK CANVAS GIRT BAR IS TORN AND FRAYED. REPLACED SLIDE ASSY PER MM 25-62-00.

Part: BATTREY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: IND LIGHT — MALFUNCTIONED (RT MLG)

PILOT REPORTED RIGHT LANDING GEAR DID NOT INDICATE SAFE WHEN HANDLE LOWERED. COMMENT NOTED BY MX.