N819UP

Part: SLIDE — DISLODGED (EMERGENCY EXIT)

INSPECTION TYPE:N/A THE MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE NEEDS TO BE ADJUSTED IN THE HOLDING CASE AS IT APPEARS TO BE SLIDING OUT AND IT IS DIFFICULT TO READ SLIDE PRESSURE. REPOSITIONED MAIN ENTRY DOOR EVACUATION SLIDE IN CONTAINER AND RE-INSTALLED W/REF TO MM 25-60-01-2. SLIDE IS SECURE.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A ON PREFLIGHT AIRCRAFT FAILED EMERGENCY EXIT LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY PACK IAW DC8 MM 33-50-1-2. OPS CHECKS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REMOVED EXISTING DOUBLER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. REAMED DISCREPANT FASTENER HOLES IAW SRM 53 53-02-0 FIG 21 AND SAA EA 008-5330-01-A0827.

Part: BRACKET — CRACKED (WING) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATED AND INSTALLED BRACKET IN NR 1 ALT TANK IAW SRM 51-01-20D, 51-03-02, AND DWG 76335150001.

Part: FINGER DOUBLER — CORRODED (FS -60 RBL 22) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 SEVERAL AREAS OF CORROSION AND POSSIBLE CRACK IN FINGER DOUBLER COCKPIT SUBFLOOR FS -60, RBL 22. REMOVED CORRODED FINGER DOUBLER AT STA -60 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -60 RBL22 IAW DWG 5612298, AND SRM51-1-21.

Part: FINGER DOUBLER — CORRODED (FS -25 RBL 22) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 CORROSION AND POSSIBLE STRESS CRACK ON FINGER DOUBLER COCKPIT SUB FLOOR FS -25 TO 8 RBL 22. REMOVED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW DWG5612298, AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 T-BOLT BACKUP FITTING CRACKED IN C-PIT TORQUE BOX, STA 1177 L33R UPPER AND LWR FLANGES. REMOVED DAMAGED FITTING AT STA 1177 L33R IAW SRM 51-1-20D. LOCATED DRILLED UP AND INSTALLED FITTING AT STA 1177 L33R IAW SRM 51-3-2 AND SRM 51-01-20D.

Part: FITTING — GOUGED (DOOR FRAME) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 LOWER FWD T-BOLT FITTING GOUGED AT C-PIT DOOR JAM. REMOVED AND REPLACED LWR FWD T-BOLT FITTING IAW SRM 51-3-2.

Part: ATTACH FITTING — CRACKED (FS 697 L18L) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 697 L18L. REMOVED CRACKED END FITTING AT STA 697 L18L IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 697 L18L IAW SRM 51-3-1, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 855 L10R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.

Part: ATTACH FITTING — CRACKED (FS 901 L19R) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 901 L19R. REMOVED CRACKED FITTING AT STA 901 L19R IAW SRM 51-1-20D. LOCATED DRILLED UP, AND INSTALLED REPLACEMENT FITTING AT STA 901 L19R IAW SRM 51-3-2, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 822 L22L) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 759 L22R) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 BOOT FITTING CORRODED AT STA 759 L22R. REMOVED CORRODED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-20D. PROCURED, LOCATED, DRILLED UP, AND INSTALLED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FS 756 L13L) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 756 L13L. REMOVED END FITTING AT STA 756 L13L IAW SRM 51-1-20D. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT FITTING AT STA 756 L13L IAW SRM 51-3-2, AND SRM 51-1-20D.

Part: CHANNEL — CRACKED (WING) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MAIN TANK IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0, AND SRM 51-01-08.

Part: DOOR FRAME — MISREPAIRED (FUSELAGE) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 L1 DOOR CUTOUT HAS RIVET WITH NO ED AT LWR HINGE CUTOUT. REMOVED, FABRICATED, AND INSTALLED L1 DOOR JAMB FRAME IAW SRM 51-1-21, 0D, 51-03-02,51-1-8,51-01-14, AND 51-3-0.

Part: SPAR CAP — CRACKED (WING TANK) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WEB AT STA XRS 168 NR 2 MAIN TANK IAW SAA EA 008-5710-01-A0808, UPS EO DC8-5710-26734-A, SRO8570015, AND FAA FORM 8100-9.

Part: SKIN — CRACKED (LT WING) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A0835, UPS EO DC8-5730-26787-A, AND FAA FORM 8100-9.

Part: ANGLE — CRACKED (FS 855 LBL 65) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 CENTER SECTION EXTERIOR L-ANGLE CRACKED THRU STOP DRILLED HOLE AT STA 855 LBL 65. REMOVED CRACKED L-ANGLE AT STA 855 LBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FILLER, AND ANGLE DOUBLER AT STA 855 LBL 65 IAW SRM 53-02-00 FIG 1B.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILED RIVETS. EXTERIOR ZR252-296 ALONG REAR SPAR. REMOVED AND REPLACED RIGHT VERT STAB SKIN IAW SRM 51-1-21, 51-1-20D, AND 51-3-0.

Part: RELEASE MECH — CONTAMINATED (NLG DOOR)

INSPECTION TYPE:N/A DIVERSION - LEFT NOSE GEAR DOOR OPEN IN FLIGHT. FOUND LEFT NOSE GEAR DOOR RELEASE TRIGGER JAMMED WITH DEBRIS. CLEANED TRIGGER IAW MM 32-20-00-01. GEAR DOOR LATCHES NORMALLY, A/C OK FOR SERVICE.

Part: ATTACH FITTING — CRACKED (FS 787 L13R) · airframe 72,498 hrs · 27,690 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 787 L13R. REMOVED FITTING AT STA 787 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON END FITTING AT STA 787 L13R IAW SRM 51-01-21-0, NAD SRM 51-1-20D.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND UNIT IAW MM 33-50-01-2-4. OPS CHECK GOOD.

Part: WINDOW — STICKING (COCKPIT)

CAPTAIN SIDE WINDOW HARD TO SLIDE. CLEARED DEBRIS FROM WINDOW TRACK. OPERATES AS REQUIRED, REF DC8 MM 56-10-00-0.

Part: LINE — LEAKING (HYD SYSTEM)

LOST HYD FLUID - DROPPED TO AUX - FOLLOWED BY MAIN SYSTEM PRESS FLUCTU ATIONS + - 1500 - 2000 PSI. DIVERT TO RICKENBACKER AFB (THIS INFO DIRE CTLY OFF LOGPAGE AS NOTED BY FLIGHT CREW). FOUND INBOARD HYD FLEX HOSE FROM NOSE GEAR RETRACT CYLINDER LEAKING. R/R HOSE IAW MM 20-12-00-2. LEAK IS GOOD.

Part: WINDOW — OBSTRUCTED (COCKPIT)

CAPTAIN'S EMERGENCY WINDOW WILL NOT FULLY OPEN. REMOVED TRIM ON L3 WINDOW AND DEFERRED PER GMM 3-6-10. WINDOW OPERATES NORMALLY. OK TO CONTINUE D332951.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT)

EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT, BREAKER POPPED, BREAKER RESET LIGHTS OPERATING NORMAL. OPS CK NORMAL ON GROUND PER MM 33-50-00, OK TO CONTINUE SERVICE.

Part: SPAR — CRACKED (RT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LONG PER NDTSPM 06=10-01.001. CRACK RUNS FROM FASTENER HOLE TO FASTENER HOLE. REPAIRED CRACK IAW DC-8 SRM 57-2 -6 FIG 10.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 C-PIT DOOR UPPER AFT CORNER HAS CRACK IN FIRST FASTENER HOLE ABOVE FITTING ATTACH LIP UNDER INTERIOR SKIN. REPAIRED C-PIT DOOR IAW DC-8 SRM 52-2-0 FIG 2.

Part: FITTING — CRACKED (WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, STRINGER END FITTING FWD INSIDE ACCESS PANEL 505E NR 3 MAIN CRACKED AT STRINGER 51. REMOVED AND REPLACED STRINGER 51 END FITTING IAW DC-8 SRM 51-1-20D.

Part: STRINGER — CRACKED (WING) · airframe 71,603 hrs · 27,023 cycles

C2 FOUND STRINGER CRACKED INSIDE FUEL PANEL 506B NR 2 MAIN STRINGER 71. REMOVED CRACKED SECTION OF STRINGER; FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW DC-8 SRM 57-2-2 FIG 3D AND E AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, 60 COMPT, 6 INCHES CRACK IN L-17L STA 1770. REMOVED LONGERON 17L IAW DC-8 SRM 51-1-21. FABRICATED LONGERON IAW DC- 8 SRM 53-5-3 AND SRM 51-3-2. INSTALLED REPLACEMENT LONGERON IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSLAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, AFT CARGO PIT STA 1200 LONGERON 34R BATHTUB FITTING CRACKED IN FWD AND AFT CORNERS. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 26 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,603 hrs · 27,023 cycles

C2 CRACKED CORNER FITTING IN C-PIT DOOR UPPER AFT CORNER. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-21A, AND 51-1- 20D.

Part: SUPPORT FITTING — CRACKED (FUSLEAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, 62 COMPARTMENT FITTING FOR "POGO STICK" CRACKED AT FWD RT ATTACH BOLT STA 1875. REMOVED AND REPLACED FITTING FOR "POGO STICK" IAW DC-8 SRM 51-1-21, 51 -3-0, AND 51-3-2.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, AFT CARGO DOOR -C- LOWER DOOR JAMB CUTOUT AFT REAR LOWER CORNER CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-1-0, 51-3-2, 51-1-20D, 51-1- 21, & 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 "A" PIT CARGO DOOR ENTRANCE L33R FWD CORNER BOTTOM BANANA FITTING HAS .400 INCH LONG CRACK. ROMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D & 51-1-21.

Part: FITTING — CRACKED (RT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 RT WING FLAP WELL STA 230 UPPER AREA HAS CRACKED WEB TO INTERCOSTAL ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-21D.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB .75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,603 hrs · 27,023 cycles

C2 VER. FIN L/E HAS CRACKED RIB 3/4 INCH AT ACCESS PNL 51I. STOP DRILLED CRACK IAW DC-8 SRM 55-02-00. REPAIRED RIB IAW 55-02-00, 51 -1-20D, AND 51-3-0.

Part: FITTING — CRACKED (RT FLAP) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 RIGHT FLAP STA 3 SUPPORT FITTING HAS APPROX 6.125 INCH CRACK ON BOTTOM OF FITTING. REMOVED AND REPLACED RIGHT FLAP STA 3 SUPPORT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D.

Part: RIB — DAMAGED (T/E FLAP) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INSTALLED REPLACEMENT RIB PER EO DC8-5750-16293-A AND DWG DC8-57-009.

Part: SPAR — CRACKED (RT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 POSSIBLE CRACK BETWEEN VERTICAL FASTENERS ON RT WING REAR SPAR LOWER T-CAP RIGHT W/W STA 857 RBL 28-32. NDT DETECTED A 4 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK PER DWG SRO8570009. REPAIRED REAR SPAR LOWER T-CAP PER DWG SRO8570009.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

C2 CEILING RIB CORRODED WITH CORROSION UNDER RADIUS FILLER RT W/W ABOVE FLAP BUSS DIRECTION CHANGE PULLEYS STA 930 RBL 58. REMOVED AND REPLACED HAT CHANNEL, STIFFENER, AND U-CHANNEL IAW DWG 5 645332, SRM TR 51-130, AND SRM 51-1-21 AND 51-2-1 FIG 1.

Part: RIB — CRACKED (HORIZONAL STAB) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, CRACKED LOWER RIB ON L/H HORIZONTAL LEADING EDGE 40 INCHES FROM IB END. STOPDRILLED CRACK IAW DC-8 SRM 55-2-0 FIG.2. REPAIRED CRACKED RIB IAW DC-8 SRM 55-3-1 FIG. 3, 55-2-0 FIG. 2, & 51-1-20D.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, CRACKED L-FITTING IN RT HORIZONTAL STAB L/E FWD SPAR AREA AT FUSELAGE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, LONGERON 15L IS CRACKED AT F/S 1750 AT CANTED FRAME. REMOVED AND REPLACE LONGERON FROM F/S 1735 TO F/S 1765 IAW DC-8 SRM 53 -2-0 FIG. 10, & 51-1-21.

Part: ANGLE — CRACKED (LT WING WW) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, ANGLE CRACKED AT UPPER WING SKIN, LEFT W/W, STA 940 AT GROUND SPOILER PULLYS O/B SIDE OF W/W, 27 INCHES BELOW CEILING. REMOVED CRACKED ANGLE IAW DC-8 SRM 51-1-21. FABRICATED REPLACEMENT ANGLE IAW DWG 5643403. INSTALLED REPLACEMENT ANGLE IAW DC-8 SRM 51-1-20D, 51-1-21, 51-3-0, & DWG 5643403.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, LONGERON 15R IS CRACKED AT F/S 1730 & F/S 1750 AT CANTED FRAMES. REMOVED AND REPLACED LONGERON SECTION IAW DC-8 SRM53-2-2 FIG. 10, 51-1 -21, & 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, EXTERIOR FUSELAGE LT APPROX. STA 1735 LONGERON 16 HAS ONE SMALL CRACK ( APPROX. .25" ) EXTENDING FROM FASTENER. REPAIRED CRACK IAW DC-8 SRM 53-2-1, 51-1-26, 51-1-21, & 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, LEFT L/E UPPER RIB CRACKED .5 INCH LONG AT STA 811. REPAIRED LT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1 20D.

Part: RIB — CRACKED (LH LE STA) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, LT L/E UPPER RIB CRACKED .25 INCH LONG AT STA 782. REPAIRED LEFT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, EXTERIOR FRUSLAGE SKIN LT APROX. STA 1746 LONGERON 14 HAS TWO SMALL CRACKS ( APROX. .25 ) EXTENDING FROM FASTENER. REPAIRED CRACKS IAW DC-8 SRM 53-2-1, 51-1-20D, & 51-1-21.

Part: SKIN — CRACKED (LT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE:C2 LEFT WING L/E LWR DRAIN HOLE HAS 2 INCH CRACK AT STA XFS 585. REMOVED DAMAGE, FABRICATED DOUBLER & FILLER, AND INSTALLED IAW DC-8 SRM 57-3-0, 57-2-0 FIG 6, 51-1-21, AND 51-1-20D.

Part: SKIN — CRACKED (RT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, RT WING UPPER SURFACE CRACKED 2 INCH LONG AROUND FASTENER HEAD AT STA XRS 76 STRINGER 16. REPAIRED RT WING UPPER SURFACE IAW DC-8 SRM 57-2-1 FIG 10.

Part: SKIN — CORRODED (LT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, LT LWR WING L/E HAS HEAVY CORROSION AT STA XFS 566. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 57-2-0 FIG 7. CUT OUT DAMAGED AREA AND REPAIRED IAW DC-8 SRM 57-2-1, 57-3-0, & 57-2-1.

Part: RIB — CRACKED (RT WING) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, RIGHT WING L/E UPPER RIB CRACKED .5 INCH LONG AT STA XRS 727, VIEW FROM PANEL 518A. REPAIRED RIGHT WING L/E UPPER RIB AT STA XRS 727 IAW DC-8 SRM 57-2-0.

Part: FITTING — CRACKED (KEELBEAM) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, FWD ACCESSORY COMPT FS 660 LT KEELBEAM ATTACH FITTING HAS 2.50 INCH CRACK ON VERTICAL FLANGE BETWEEN ATTACH BOLTS HEADS. REMOVED CRACKED ATTACHMENT FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3750497 AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,603 hrs · 27,023 cycles

INSPECTION TYPE: C2, FWD ACCESSORY COMPT FS 683 BULKHEAD CRACKED .5 INCH LONG AT LOWER END OF VERTICAL STIFFENER LBL 18. REPAIRED FS 683 BULKHEAD IAW DC-8 SRM 53-2-5 FIG 13, 51-1-21, AND 51-1-20D.

Part: SKIN — DELAMINATED (RT SPOILER)

INSPECTION TYPE:N/A RIGHT I/B SPOILER PANEL HAS DELAM ON O/B SIDE BOTTOM. REMOVED RIGHT I/B SPOILER IAW 27-61-01-2 TO STEP 10 PARAGRAPH NR 3. INSPECTED A/C STRUCTURE NO DEFECTS NOTED. OK TO INSTALL. INSTALLED RIGHT I/B SPOILER PANEL PER 27-61-01-2 TO STEP B6 PG 31. COMPLETED INSTALL 27-22-22-4.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, F/O UNDERGLARE SHIELD EMERGENCY LIGHT INOP. RELAMPED WITH NEW LAMPS. OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

ENTRY DOOR EMERGENCY LIGHTS, 1 AFT INOP. RELAMPED EMERGENCY LIGHTS, OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS DOME COCKPIT DOME COURIER FAIL TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK WITH REF TO MM 33-50-01, CKS GOOD AT THIS TIME.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3 L-1 DOOR LWR AFT CORNER SKIN CRACKED 2 EA BY CUTOUT MARKED. REPAIRED LOWER AFT DOOR CORNER IAW DC8 SRM 53-2-0 FIG 15, TR 53-128, TR 53-155 AND REO G09193

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, APPROX. STA 700, LONG 35 RT, SHEAR TIE (FRAME ANGLE) UNDER STRESS PN L IS CORRODED AND CRACKED REMOVED DAMAGED SECTION OF SHEAR TIE IAW DC8 SRM 51-1-20D, FABBED NE W SECTION IAW DWG 9753780, LOCATED AND DRILLED UP NEW SECTION IAW D WG 9753780 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED ON AIRCRAFT IAW DC8 SRM 51-1-20D

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, FWD ACCESSORY COMPARMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. HEAT TREATED FRAME SECTION AND SPLICES IAW TPS-1003 REV A. FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-24. ALODINED AND PRIMED ALL REPAIR PARTS IAW DC8 SRM 51-1-8 AND INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. MAT ID 7075-0 .07 1 PO 401846.1 FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 S RM 53-2-0, 51-2-24. ALODINED AND PRIMED ALL REPAIR PARTS IAW DC8 SRM 51-1-8 AND INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D

Part: SPAR — CRACKED (RT WING) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C-3, WHEN INSPECTING LWR FRONT SPAR ON RT WING, FOUND PREVIOUSLY REPAIRED HOLES TO EXCEED LIMITATIONS CALLED OUT IN EO. FABBED & INSTALLED RPR BUSHINGS FOR HOLES 3,5,&11. FABBED RPR ANGLES J060232-53/56/58/60.LOCATED, DRILLED, AND STRESS COINED REQ'D HOLES IN SPAR AND RPR STRAP & RPR ANGLES.ALODINED & PRIMED.INSTALLED RPR STRAP & RPR ANGLES.ALL IAW DAC DWG 4709980, J060232, REO G09212, DC8 SRM 51-1-25, 51-1-24, 51-1-8, 51-1-20D, & DPS 3.67-56

Part: FITTING — CRACKED (BOOST PUMP) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, NR 4 ALT FWD AND AFT BOOST PUMP MOUNT FITTINGS ARE CRACKED (2EA FITTIN GS) REMOVED FWD AND AFT CRACKED BOOST PUMP FITTINGS IAW DC8 SRM 51-1-20D . LOCATED, DRILLED AND DEBURRED 2 EA NEW FITTINGS P/N 3645612U PO SP O903876 AND 3645611U PO SPO903618 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (BOOST PUMP) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, NR 1 ALT AFT BOOST PUMP MOUNT FITTING IS CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D RECEIVED NEW FITTING P/ N 3645611U PO SP094626. LOCATED, DRILLED, AND DEBURRED IAW DC8 SRM 5 1-1-24. INSTALLED IAW DC8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD WEB FOWARD SIDE CRACKED AT RBL 26 TO 28 AND RBL 34 TO 38 ABOVE FLOOR LINE. CUT OUT CRACKED AREA IAW DC8 SRM 53-2-5. REMOVED 5772638-48 ATTACK ANGLE, FABBED -11, -19, -9, & 25-27 DOUBLERS IAW DC8 SRM 53-2-5 & DAC DWG SR08530007. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -9,- 11,-19 FILLERS & 25-27 DOULBERS -30 ANGLE IAW DC8 SRM 51-1-20D. INSTA LLED HAT CHANNEL, GILLINER ATTACH ANGLE IAW DC8 SRM 51-1-21 & 51-3-0.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, AFT PRESSURE BULKHEAD WEB FWD SIDE CRACKED AT LBL 23 TO 27 AND LBL 3 3 TO 37. 65 INCHES ABOVE FLOORLINE. REMOVED DAMAGE, FABRICATED -25, -27 DOUBLERS AND -29 ANGLE, -9, -11, -19 FILLERS IAW DAC DWG SR 08530007. ALODINED AND PRIMED REPAIRS IA W DC8 SRM 51-1-8. INSTALLED REPAIR IAW DAC DWG SR 08530007.

Part: LONGERON — CRACKED (CARGO DOOR) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE:C3 R2 DOOR LONGERON 11R IS CRACK AT UPPER AFT DOOR JAMB CORNER. REMOVED LONGERON IAW DC8 SRM 51-1-21 & 51-1-20D. REMOVED & REINSTALLED GILLINER & INSULATION IAW DC8 SRM 51-3-0. REC'D LOCATED & DRILLED NEW LONGERON IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, R2 UPPER AFT DOOR JAMB CORNER HAS 2 EA CRACKS AT L11R APPROX 1.25 INCH AND 2 INCH LONG. CUT OUT CRACKS IN INNER DOUBLER, FABRICATED DOUBLER, TRIPLER, AND SKIN FILLER IAW DC8 SRM 53-2-0 FIG 16 TR 53-156. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOULBER, TRIPLER AND SKIN FILLER IAW DC8 SRM 53-2-0 FIG 16 TR 53-156.

Part: FRAME — CRACKED (CUSP) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, BS 55 L21L CUSP FRAME CRACKED APPROX 6 INCH LONG. REMOVED FWD CORNER PAN AND FWD LOWER WEB FOR ACCESS FABBED NEW FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTAL LED IAW DAC DWG 5597646, 51-1-21, AND 51-1-20D. REINSTALLED FWD LOWE R WEB AND FWD LOWER CORNER PAN IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE:C3 BS 55 L21L CUSP FRAME CRACKED APPROX 6 INCHES LONG. REMOVED FWD CORNER PAN AND FWD LOWER WEB FOR ACCESS FABBED NEW FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTAL LED IAW DAC DWG 5597646, 51-1-21 AND 51-1-20D. REINSTALLED FWD LOWER WEB AND FWD LOWER CORNER PAN.

Part: FITTING — CRACKED (RT WING) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, NR 3 FUEL TANK STRINGER 74 STRAP CRACKED STA XRS 22 ACCESS PANEL 506C. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABBED 1 EA FITTING P/ N 5616869-2 FROM 7075-T6511 BAR STOCK PO 334935 IAW DAC 5616869. L OCATED DRILLED DEBURRED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW D C8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. LEAK CHECK TO BE ACCO MPLISHED ON UPS TASK CARD NO 8000 ITEM 38.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, CABIN SEAT TRACK F CRACKED AT STA 1571. REMOVED AND REPLACED SEAT SECTION IAW DC8 SRM 53-2-3 AND UPS EO DC8- 5320-5167

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 660 & L36 FRAME SPLICE FITTING CRACKED. RECEIVED NEW FITTING PN 3750498 LOCATED AND DRILLED HOLES IAW DC8 S RM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 660 & L36 FRAME AND FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW FITTING P N# 3750497-2N-5N TAG 477912 LOCATED & DRILLED HOLES IAW DC8 SRM 51-1 -24 INSTALLED FITTING IAW DC8 SRM 51-1-20D

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, CABIN SEAT TRACK F CRACKED AT STA 1571. REMOVED AND REPLACED SEAT SECTION IAW DC8 SRM 53-2-3 AND UPS EO DC8- 5320-5167.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, AFT FUSE L17R AT END FITTING CRACKED. REMOVED L17RT END FITTING TO FOM RECEIVED NEW LONG PO 5649327-44. LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW L17RT & END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, AFT FUSE L17LT AND END FITTING CRACKED AT FS 1770. REMOVED LONG 17LT & END FITTING. LOCATED AND DRILLING NEW END FITTING IAW DC8 SRM 51-1-24. INSTALLED LONGERON & END FITTING IAW DC8 SRM 51-1-20D.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,793 hrs · 26,378 cycles

INSPECTION TYPE: C3, AFT PIT RT AFT DOOR SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW DC8 SRM 51-3-0.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

ESCAPE SLIDE AIR PRESSURE GAUGE IN THE RED. EMERGENCY ESCAPE SLIDE CYLINDER PRESSURE WITHIN SERVICEABLE LIMITS PER MM 25-60-01 TEMPERATURE COMPENSATION CHART.

Part: ANGLE — CORRODED (RT WING)

INSPECTION TYPE:PFLT RIGHT W/W CORROSION FLAP WELL AREA. REPLACED ANGLE.

Part: PRESSURE PANEL — CRACKED (RT WING)

INSPECTION TYPE:PFLT RT W/W UPPER WEB CRACKED STA XW 5.00 FERRY 9151 TO SDF REF D243078. REPAIRED WEB PER SRM 57-2-0 FIGURE 2A.

Part: STIFFENER — CRACKED (FUSELAGE)

INSPECTION TYPE:PFLT RT W/W UPPER INBOARD STIFFENER CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

INSPECTION TYPE:PFLT RIGHT W/W AFT OPENING ATTACH ANGLE CRACKED. REMOVED ANGLE, DRILLED NEW ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20D.

Part: WEB — CRACKED (T/E FLAP)

INSPECTION TYPE:PFLT RT WHEEL WELL FLAP SUPPORT WEB ANGLE CRACKED. FERRIED TO SDF FOR REPAIR PERMIT 9151, D243076. REMOVED FASTENERS IN DAMAGED WEB & SUPPORT BRACKET. REPAIRED WEB PER SRM 57-2-0 FIG 2A. REINSTALLED WEB.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,596 hrs · 25,616 cycles

INSPECTION TYPE:C1 AFT PIT STA 1060 L36 FRAME HAS CORROSION ON UNDERSIDE OF J-CHANNEL A T-NUT PLATE. REMOVED CORROSION OF FRAME OUT OF LIMITS. LOCATED AND DRILLED NEW FRAME CAP, FABBED REPAIR ANGLES, ALODINED PRIMED INSTALLED FRAME CAP REPAIR ANGLES GUSSETTE IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,596 hrs · 25,616 cycles

INSPECTION TYPE:C1 AFT PIT STA 1020 L36 2 EA NUT PLATES WITH CORROSION ON FRAME UNDER NUT PLATES. REMOVED CORROSION MAT OUT OF LIMITS IAW 53-2-0. REMOVED FRAME CAP LT & RT GUSSET AND R & L SUPPORT ANGLES IAW DC8 SRM 51-1-21 MAT ID IS 7075-0 .090 PO 344427 FOR ANGLE REPAIR AND 7075-T6 .125 FOR FILLER. FAB REPAIR ANGLE AND FILLER IAW UPS EO DWG DC8-53A-011. HEAT TREAT REPAIR ANGLE, ALODINED AND PRIMED ANGLE AND FILLER IAW 51-1-8 INSTALLED IAW 51-1-20.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,596 hrs · 25,616 cycles

INSPECTION TYPE:C1 AFT PIT STA 1020 L36 2 NUT PLATES WITH CORROSION ON FRAME UNDER NUT PLATES. REMOVED CORROSION MAT ID 7075-T6 0.625 PO 334056. FAB IAW DWG DC8-53 A-011. HEAT TREATED, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. NEW FRAME CAP P/N 57643434507. LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-2-20D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,596 hrs · 25,616 cycles

INSPECTION TYPE:C1 FWD PIT - STN 90 - S33R - INTERCOSTAL UNDER CARGO TRACK IS BENT AND CRACKED. REMOVED AND FABBED NEW INTERCOSTAL P/N 5750726-70. ALODINED, PRIMED AND INSTALLED INTERCOSTAL CARGO TRACK IAW DC8 SRM 51-3-0 AND 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,596 hrs · 25,616 cycles

INSPECTION TYPE:C1 SKIN BELOW CUTOUT FOR AFT LT ENTRANCE DOOR CRACKED LWR FWD CORNER. REPAIRED AREA IAW REO G08018.

Part: SOCKET — INOPERATIVE (INDICATOR LIGHT)

INSPECTION TYPE:IN, LOADING CARGO SMOKE DET SYSTEM WOULD NOT TEST. BAD LIGHT SOCKET. REMOVED AND REPLACED TEST LAMP ASSY BASE, OPS CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD PER DC8 MM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK CHKS GOOD

Part: WINDOW — FAILED (CABIN)

INSPECTION TYPE:N/A, CAPTINS CLEARVIEW SIDE WINDOW ARCING. REMOVED AND REPLACED CAPTAINS CLEARVIEW WINDOW IAW MM 56-10-03. TEST ED PER 56-10-03. SYSTEM OPS CK NORMAL.

Part: FITTING — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT STA X 70 APPROX 18 INCHS IN FRONT OF SPAR VERTICAL SUPPORY FITTING CRACKED. REMOVED AND REPLACED FITTING DOUBLER IAW DC-8 SRM 55-2-0.

Part: FITTING — CORRODED (BS 940)

INSPECTION TYPE:C2 LONG 24 RT UPPER FITTING AT FS 940 HAS CORROSION AT BOTTOM ATTACHMENT HOLES. REMOVED CORRODED FITTING, LOCATE NEW FITTING DRILL REAMED EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51-1 -20D,CPCP.

Part: FITTING — CRACKED (BS 879)

INSPECTION TYPE:C2 RT LONG 24 UPPER FITTING AT FS 879 HAS CRACK AT ATTACHMENT HOLES. REMOVED CRACK FITTING, LOCATE NEW FITTING, DRILL, AND REAM EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51- 1-20D.

Part: FITTING — CRACKED (RT WING)

INSPECTION TYPE:C2, RT WING FLAP HINGE SUPPORT FITTING I/B SIDE GAVE CRACK INDICATION. REPLACED BRACKET.

Part: BASE — CRACKED (LT MLG WW)

INSPECTION TYPE:C CRACKED BASE FOR LEFT GEAR WELL HYD. RESERVOIR OUTBOARD FWD SIDE CRACK PREVIOUSLY REPAIRED IAW DC-8 SRM57-2-0, DOUBLER WAS INSTALLED.

Part: FITTING — CORRODED (BS 880)

INSPECTION TYPE:C LEFT WHEEL WELL FITTING AT STA 880, LONG 24R CORRODED DOT M940. REMOVED CORRODED FITTING FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2- 0, ALODINED AND PRIMED REPAIRED PARTS IAW DC-8 SRM 51-1-8. CUT NEW FITTING IAW DC-8 SRM 53-2-0 AND INSTALLED FITTING AND REPAIRED ANGLES IAW DC-8 SRM 51-1-20D. CPCP

Part: FITTING — CRACKED (RT MLG WW)

INSPECTION TYPE:C RT WHEEL WELL TRAP FITTING CRACKED IN AFT WEB DOT M942. REMOVED CRACKED TRAP FITTING, REPLACED TRAP FITTING AS PER JOB CARD NR 90432100 (UPS NR 929640).

Part: LONGERON — CRACKED (BS 940)

INSPECTION TYPE:C RT WHEEL WELL LONG 24R CRACKED AT STA 940 DOT M-944. REMOVED CRACKED LONGERON, REPLACED LONGERON 24R AS PER JOB CARD NR 904 53100.

Part: FITTING — MISDRILLED (CABIN)

INSPECTION TYPE:C2, MAIN CABIN C-3 TORQUE BOX HAS MISDRILLED HOLES L-20R. REMOVED FORWARD SECTION, REMOVED FITTINGS, LOCATED DRILLED FITTINGS, INSTALLED FITTINGS, FABBED INNER AND OUTER IAW DC8 SRM 51-1-20D AND 5 1-3-0.

Part: LONGERON — MISDRILLED (BS 1080)

INSPECTION TYPE:C GILINER NUT PLATES INSTALLED INCORRECTLY AT STA 1080 LONG 34-35 1100, LONG 32-33R. REMOVED DAMAGE, AND FABBED DOUBLER, STRAP AND FILLER IAW REO-06431 A ND DWG NR DC-8-53-229, LOCATED DRILLED PARTS PER DC-8 SRM 51-3-2. REPA IRS IAW DC-8 SRM 51-1-20D AND REO-0641 AND DWG. DC-8-53-229.

Part: BRACKET — CRACKED (NR 4 ENG TR UNIT)

INSPECTION TYPE:C, NR 4 ENGINE OUTBOARD T/R FWD LOWER CORNER BRACKET CRACKED. DYE PEN AREA IAW MIL-27IF, NO CRACKS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHT INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK PER M/M 33-50-01. (P/N T91189), (S/N 7).

Part: FORMER — CRACKED (BS 1600)

INSPECTION TYPE-N/A, AFT ACCESSORY COMPARTMENT, FORMER CRACKED AT STA 1600 BETWEEN L28R AND L29R. REMOVED DAMAGED SECTION OF FORMER IAW DC8 SRM 53-2-0. FABRICATED FOR MER REPAIR IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, EMER ENTRY DOOR (L-1) HAS A BAD LIGHT. RELAMPED EMER EXIT DOOR LIGHT AT PAX DOOR PER MM 33-50-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE N/A, EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATT PACK (P/N 5708458-503) ON, (P/N 60-1223-5) OFF, (S/N 588) ON, (S/N 219) OFF.

Part: CONTROL VALVE — FAILED (LT PACK)

CREW EVACUATED AIRCRAFT DUE TO SMOKE IN COCKPIT. CREW FOLLOWED EVACUATION CHECKLIST, FIRED ALL BOTTLES, SHUTDOWN ALL ENGINES AFTER AIRCRAFT WAS REPOSITIONED TO UPS RAMP, THEN MOVED A/C TO MERCURY CARGO RAMP. DETERMINED LEFT PACK WILL NOT SHUT OFF, SUSPECT FLOW CONTROL VALVE. REPLACED FLOW CONTROL VALVE AND WATER SEPARATOR BAG FOR LEFT PACK. OPS CK, LEFT PACK OPS CKS NORMAL. NO SMOKE OR FUMES NOTED IN COCKPIT.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: WEB — CRACKED (BS 1440-1450)

INSPECTION TYPE:D, C-4 DOOR AFT WEB FS 1440 TO 1450 HAS 2 CRACKS BETWEEN LONGERONS 31R AND 33R. REPAIRED IAW SRM 53-2-0, 51-1-21, AND 53-4-1.

Part: FRAME — CORRODED (BS 1446)

INSPECTION TYPE:D, UPPER FLANGE ON UPPER SURFACE AT FS 1446 ABOVE LONG 32, FRAME SECTION IS CORRODED BEYOND LIMITS. REPAIRED FRAME SECTION IAW SRM 53-2-0, 53-4-1, AND 51-1-20D.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:D, LONGERON 32L AT FS 1690 FITTING IS CORRODED, ENLONGATED HOLES, AND MISDRILLED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-0.

Part: DOUBLER — CORRODED (BS 980)

INSPECTION TYPE:D, FUSELAGE SKIN EXTERNAL DOUBLER CORROSION REMOVAL IS BEYOND LIMITS AT FS 980 BETWEEN LONGERONS 31L TO 32L. REPAIRED IAW DHC SK-819-697 REF UPS ENRG FILE NR DC8-53-1851 FROM FS 980 TO 1010.

Part: SKIN — CORROSION (BS 1660-1690)

INSPECTION TYPE:D, FUSELAGE SKIN HAS 3 AREAS OF CORROSION REMOVAL BEYOND ALLOWABLE LIMITS AND 1 EXISTING FREEZE PLUG FS 1660 TO 1690 STR 23 TO 29L. REPAIRED IAW DHC SK-819-660 REF UPS ENRG FILE NR DC8-53-1853.

Part: SKIN — CORRODED (WS 763)

INSPECTION TYPE:D, RT WING O/B T/E LOWER SKIN SURFACE AT APPROX STA XW763 CORRODED BEYOND ALLOWABLE LIMITS. FABRICATED AND INSTALLED SKIN IAW SRM 51-1-21, 51-3-0 AND 57-3-2.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:D, LONGER 27R END FITTING CRACKED ON AFT SIDE OF FS 70. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:D, LONGERON 28L END FITTING FWD SIDE OF FS 1690 CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-21.

Part: STRINGER — CRACKED (BS 1690)

INSPECTION TYPE:D, STRINGER CRACKED FS 1690 S 28L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER FROM FS 1670 TO 1690 IAW SRM 53-2-2 FIG 10.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D, STR 34L AT FS 70 END FITTING IS CORRODED ON INBD END. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-1-0.

Part: ANGLE — CRACKED (BS 850)

INSPECTION TYPE:D, CRACK ON ANGLE BRACKET ON FS 850 BULKHEAD 15 LEFT OF KEEL BEAM. REMOVED, FABRICATED AND REPLACED ANGLE WITH REPAIR ANGLE IAW SRM 53-8-3, 51-3-0, 51-1-21, 51-1-29D.

Part: INTERCOSTAL — CORRODED (BS 1060-1080)

INSPECTION TYPE:D, INTERCOSTAL LOWER ATTACHMENT TEE IS CORRODED BETWEEN FS 1060 TO 1080 LONG 35L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TEE IAW SRM 53-1-0, 51-1-20D.

Part: RIB — CORRODED (WS 404)

INSPECTION TYPE:D, RT WING LOWER RIB AT XFS 404 HAS CORROSION REMOVAL BEYOND LIMITS. REMOVED AND REPLACED RIB IAW SRM 51-1-21.

Part: FRAME — CORRODED (BS 380)

INSPECTION TYPE:D, FRAME AND T-1 DOOR INNER WEB SEVERLY CORRODED FS 380 BETWEEN LONG 12L AND 13L. REPAIRED IAW DHC SK-819-824, REF UPS ENRG FILE NR DC8-53-1850.

Part: RIB — CORROSION (WS 397.75)

INSPECTION TYPE:D, RT WING UPPER, LWR RIB AT STA XFS397.75 HAS CORROSION REMOVAL BEYOND LIMITS. REPAIRED RIB IAW SRM 57-2-0, 51-1-21.

Part: DOUBLER — CORRODED (BS 1490-1600)

INSPECTION TYPE:D FS 1490 TO 1600 AT ATR 31R FINGER DOUBLER HAS CORROSION THROUGHOUT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1, 51-1-21.

Part: DOUBLER — CORRODED (BS 1610-1655)

INSPECTION TYPE:D, FS 1610 TO 1655 AT STR 31L INTERNAL DOUBLER HAS HEAVY CORROSION BOTH SIDES. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-20, 51-1-21, AND 53-4-1.

Part: DOUBLER — CORRODED (BS 1600-1650)

INSPECTION TYPE:D, FS 1600 TO 1650 AT STR 31R INTERNAL DOUBLER HAS HEAVY CORROSION BOTH SIDES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW 51-1-21, 51-1-20D, 53-4-1.

Part: LATCH — CRACKED (CARGO DOOR)

INSPECTION TYPE:D, C-1 PIT DOOR LOWER T-LATCH FITTING IS CRACKED, 6TH FROM FWD END. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D.

Part: DOUBLER — CORRODED (BS 1655-1690)

INSPECTION TYPE:D, F/S 1655-1690 AT STR 31L, INTERNAL DOUBLER HAS HEAVY CORROSION ( BOTH SIDES ). FABRICATED REPLACEMENT DOUBLER IAW SRM 53-4-1.

Part: DOUBLER — CORROSION (BS 1490-1600)

INSPECTION TYPE:D, FS 1490 TO 1600 AT STR 31L FINGER DOUBLER HAS CORROSION THROUGHOUT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND 53-4-1.

Part: WEB — CORRODED (BS 1260)

INSPECTION TYPE:D, FS 1260 AT STR 36 WEB CORROSION REMOVAL OUT OF LIMITS. FABRICATED AND INSTALLED REPLACEMENT PLATE AND FRAME REPAIR IAW SRM 53-2-0 FIG 2 AND 51-01-20D.

Part: FITTING — CRACKED (BS 1182)

INSPECTION TYPE:D, C-3 DOOR AREA AT FS 1182 BETWEEN LONGERON 34R AND 33R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D, 53-2-0 FIG 2D.

Part: DOUBLER — CORRODED (BS 260-360)

INSPECTION TYPE:D, C-1 DOOR INTERNAL DOUBLER FS 260 TO 360 LONGERON 27R TO 36 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG NR 5755271, 9754003, SRM 51-1-20, 51-1-0, 51-1-20D.

Part: FITTING — CORRODED (BS 1120)

INSPECTION TYPE:D, AFT PIT AT THE DOOR FS 1120 I/B OF LONGERON 33R AND INTERCOSTAL FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0.

Part: SKIN — CORRODED (RT HORZ STAB)

INSPECTION TYPE:D, RT HORIZ STAB LOWER SURFACE HAS MODERATE CORROSION WHERE THE STAB MEETS THE CENTER BOX. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW 55-2-0, 51-1-21, 51-3-1, 51-3-0 AND DWG 5653617.

Part: LATCH — CORRODED (BS 1186)

INSPECTION TYPE:D, AFT PIT FS 1186 OTBD LONGERON 33R LATCH FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1186)

INSPECTION TYPE:D, AFT PIT AT THE DOOR AT FS 1186 I/B OF LONGERON 33R AND INTERCOSTAL, DOOR LATCH BACK UP FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-1-20D.

Part: FITTING — CORRODED (BS 1200)

INSPECTION TYPE:D, AFT PIT FS 1200 OUTB LONG 33R LATCH FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CORRODED (RT AILERON)

INSPECTION TYPE:D, RT AILERON UPPER L/E SKIN HAS HEAVY CORROSION AT BOTH CENTER BALANCE BAYS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN PANEL IAW SRM 51-1-21, 51-3-0, 57-8-1 AND DWG 5705334.

Part: FITTING — CORRODED (BS 1170)

INSPECTION TYPE:D, AFT PIT AT THE DOOR FS 1170 I/B OF LONGERON 33R AN INTERCOSTAL FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-2-0 FIG 2D.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:D, AFT PIT FS 1180 OUTB LONG 33R LATCH FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: WINDOW POST — CRACKED (BS 117)

INSPECTION TYPE:D, WINDOW POST AT STA 117.000 HAS A CRACKED FRAME. STOP DRILLED AND INSTALLED STACKED ANGLE REPAIR IAW SRM 53-2-0 FIG 1B.

Part: STIFFENER — CRACKED (BS 80)

INSPECTION TYPE:D, COCKPIT SUBFLOOR AT FS 80 LBL 56, VERTICAL STIFENER IS CRACKED. REPAIRED PER SRM 53-2-0 FIG 1B.

Part: FITTING — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STABILIZER, 3RD FROM TOP RUDDER HINGE SUPPORT FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5619438.

Part: STIFFENER — CRACKED (BS 80)

INSPECTION TYPE:D, COCKPIT SUBFLOOR AT FS 80 RBL 56 VERTICAL STIFFENER IS CRACKED AT BOTTOM. REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: INTERCOSTAL — CRACKED (BS 500-510)

INSPECTION TYPE:D, INTERCOSTAL BTWN FS 500 TO 510 AT LONG 33R HAS DOUBLE DRILLED HOLES AND IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 53-3-3, 53-4-1, 51-1-20 AND DWG 5750412.

Part: FITTING — CRACKED (BS 924)

INSPECTION TYPE:D, FS 924 AT LBL 67, PRESSURE PAN STIFFENER FITTING IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DHC SK 819-297, REF UPS ENRG FILE NR DC8-53-1848.

Part: DOUBLER — CORRODED (BS 400-450)

INSPECTION TYPE-D, CORROSION- REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1 51-1-21.

Part: CARGO TRACK — CORRODED (BS 1410-1540)

INSPECTION TYPE:D, FS 1410 TO 1540 ABOVE STR 33L CARGO TRACK HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 53-1-0, 51-1-20.

Part: SHEAR TIE — CRACKED (BS 260)

INSPECTION TYPE:D, SHEAR TIE AT FS 260 BTWN LONG 35L TO 36 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 53-2-0, 53-4-1, 51-1-20D.

Part: WEB — CRACKED (BS 1220)

INSPECTION TYPE:D, FS 1220 AT STR 33L WEB HAS 1 INCH CRACK FROM NUT PLATE TO NUT PLATE. REPAIRED IAW SRM 53-2-0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:D, LONG 33L END FITTING JUST AFT OF FS 1690 CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D AND 51-1-21.

Part: FRAME — CORRODED (BS 70)

INSPECTION TYPE:D, C-1 PIT FWD BULKHEAD HORZ FRAME AT FS 70 BL 0, 20 ABOVE LONG 36 HAS BLOWN OUT CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME IAW SRM 51-1-21, 51-1-20D, 53-1-0 AND DWG 5613064.

Part: FITTING — CRACKED (BS 1141)

INSPECTION TYPE:D, STA 1141 AT STR 35L INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED TIE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE:D, RT WING OTBD SLOT OTBD END CLOSURE RIB IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1221)

INSPECTION TYPE:D, FS 1221 AT STR 27R FLOORBEAM SUPPORT FITTING IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG NR 9754024 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE:D, FS 700 AT STR 13L INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FITTING — CRACKED (BS 825)

INSPECTION TYPE:D, FS 825 AT STR 18R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20, 51-1-20D, 51-3-0, AND DWG 4751640.

Part: SPLICE — CRACKED (BS 200-220)

INSPECTION TYPE:D, FS 200 TO 220 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, FABRICATED REF SRM 53-1-0.

Part: GUSSETT — CORRODED (WS 1660-1680)

INSPECTION TYPE:D, INTERCOSTAL ATTACH CLIPS CORRODED BEYOND LIMITS F/S 1660-1680 LONG- 33R. REMOVED AND REPLACED CLIPS IAW SRM 51-1-20D.

Part: SEAT TRACK — WORN (BS 600)

INSPECTION TYPE:D, FS 600, RBL 44, THE SEAT TRACK IS WORN BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-3-0, 53-2-3, AND 51-1-21.

Part: FITTING — CRACKED (BS 1221)

INSPECTION TYPE:D, FS 1221 AT STR 18R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D.

Part: SEAT TRACK — WORN (BS 215-276)

INSPECTION TYPE:D, MAIN CABIN AT FS 215.00, 246, AND 276, RBL 59 SEAT TRACK IS WORN BEYOND LIMITS AT EACH POSITION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-3-0, 53-2-3, 51-1-21 FROM FS 190 TO 290.

Part: SKIN — CORRODED (BS 1050-1350)

INSPECTION TYPE:D, FUSELAGE SKIN AT STA 1050 TO 1350 LONG 31L TO LONG 31R IS CORRODED. REMOVED AND REPLACED SKIN IAW SRM 51-1-20D AND 51-1-21.

Part: SKIN — CORROSION (RT WING LE)

INSPECTION TYPE:D, RT WING LWR L/E SKIN ABOVE THE NR 3 PYLON HAS HEAVY CORROSION EXFOLIATION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STRAP IAW DWG 5769857 SRM 51-1-21, 51-1-2D, 51-1-21A, 51-3-0.

Part: SKIN — CORROSION (BS 1350-1490)

INSPECTION TYPE:D, REPLACE SKIN AT FS 1350 TO 1490 LONG 31L TO 31R DUE TO CORROSION. REMOVED AND REPLACED SKIN IAW SRM 51-1-21 AND DWG 5615372.

Part: FITTING — BROKEN (CARGO DOOR)

INSPECTION TYPE:D, C-1 CROSS SLIDE DOOR JAMB AREA HAS LOWER T-BOLT BRACKET 4TH FROM FWD END BROKEN. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, REPLACED SKIN AT FS 1490 TO 1690 L31L TO L31R DUE TO CORROSION. REMOVED AND REPLACED SKIN IAW SRM 51-1-21, 51-1-29D, 51-1-11, AND DWG 5615374.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE:D, LT WING L/E RIB AT STA XFS 797.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 341.5)

INSPECTION TYPE:D, LT WING LWR L/E RIB AT STA XFS 341.5 IS CRACKED AT THE AFT GUSSET ATTACH HOLE. REPAIRED IAW SRM 53-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 385.25)

INSPECTION TYPE:D, LT WING LWR L/E RIB AT STA XFS385.25 IS CRACKED AT THE UPPER FLANGE AT THE AFT GUSSET RIVET HOLE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-3-0 AND 53-2-0.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE:D, LT WING L/E RIB AT STA XES760.0 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0.

Part: CARGO TRACK — CRACKED (BS 1320-1400)

INSPECTION TYPE:D, C-4 CARGO PIT SEAT TRACK RT FS 1320 TO 1400 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-O, AND DWG 5759223 AND SRM 51-1-21.

Part: SEAT TRACK — WORN (BS 472-492)

INSPECTION TYPE:D, FS 472 AND 492 RBL 59, THE SEAT TRACK IS WORN BEYOND LIMITS AT EACH LOCATION. REMOVED AND REPLACED SECTION OF TRACK FROM FS 390 TO 590 IAW SRM 53-2-3, 51-3-0.

Part: SKIN — CORROSION (BS 190-450)

INSPECTION TYPE:D, REPLACED SKIN AT FS 190 TO 450 LONGERON 31L TO 31R DUE TO CORROSION. REMOVED AND REPLACED SKIN IAW SRM 51-1-29D AND DWG 5755271.

Part: SKIN — DAMAGED (BS 70-80)

INSPECTION TYPE N/A, TEAR IN SIDE OF FUSELAGE FWD OF PIT 31 STA 70 TO 80. REPAIRED PER SRM 53-1-2, E0 DC8-5310-8335 AND EO DC8-5310-8335A.

Part: SWITCH — MALFUNCTIONED (LT MLG)

LEFT MLG GEAR SAFE LT INOP. CYCLED GEAR SEVERAL TIMES, NO HELP. RELAMPED AND NO HELP. PERFORMED EMERGENCY PROCEDURES AND LANDED. GEAR WAS PINNED AND AIRCRAFT MOVED OFF TAXIWAY. T/S TO BAD LT MLG DOWN LIMIT SWITCH. SWAPPED PINS TO AUX CONTACTS IN MLG DOWN LIMIT S/W. LIGHT THEN CHECKED NORMAL. PLACED ITEM ON LT MLG DOWN LIMIT SWITCH FOR REPLACEMENT ITEM DEFERRED REF NR D110662.

Part: LONGERON — CRACKED (FUSELAGE)

WHILE IN FOR B-CHECK, MAINTENANCE REPORTED CORROSION IN BELLY AND CRACKED LONGERONS. REPAIRED PER EO DC8-5330-8018.

Part: T-CHORD — CORRODED (BS 8)

WHILE IN FOR B-CHECK, MAINTENANCE REPORTED STATION 8 T-CHORD CORROSION REPAIR. BLENDED CORROSION INSTALLED 2 REPAIR STRAPS EQUALING 100 MATERIAL USING 7075-T6 MATERIAL PER EO DC8-5310-8015A.

Part: DOUBLER — CORRODED (AIR ACCESS DR)

WHILE IN FOR B-CHECK, MAINTENANCE REPORTED AIR ACCESS DOOR SUPPORT DOUBLER LOWER EDGE CORROSION REPAIR. REPAIRED PER EO DC8-5310-8016A.

Part: DOUBLER — CRACKED (X-SLIDE DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND C X-SLIDE DOOR, LOWER FORWARD EXTERNAL CUTOUT DOUBLER CRACKED AND BENT. MAINTENANCE REPLACED THE DOUBLER IAW SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CRACKED (BS 879-884)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L HAS A 5 INCH LONG CRACK AT FS 879 TO 884 LOWER FLANGE RADIUS. MAINTENANCE REPAIRED THE LONGERON IAW SRM 53-2-2.

Part: FITTING — CORRODED (BS 683)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FITTING HAS HEAVY CORROSION BETWEEN LONGERONS 36 TO 35R, BS 683. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20.

Part: BLKHD CHANNEL — CRACKED (BS 683)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A 1 INCH CRACK ON CHANNEL BS 683, BULKHEAD, LONGERON 28R. MAINTENANCE REPAIRED CHANNEL IAW SRM 53-2-0.

Part: BULKHEAD — CRACKED (BS 683)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 6 INCH CRACK AT PRESSURE BULKHEAD, BS 683 LONGERON 31R. ALSO, A 1.5 INCH CRACK RUNNING AT LONGERON 29R. MAINTENANCE REPLACED THE BULKHEAD ASSY IAW SRM 51-1-20D.

Part: SKIN — CRACKED (BS 165)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND EXTERIOR SKIN CRACKED 1 INCH LONG AT FS 165. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-2-0.

Part: GEAR INDICATION — MALFUNCTIONED (NLG)

PILOT REPORTED THAT AFTER TAKE OFF GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND COMPLIED WITH CHECKLIST BUT LIGHT REMAINED ON. DURING CHECK, NOSE GEAR WAS UP. PERFORMED GEAR UP LIMIT SWITCH CHECK PER MM 32-60-00. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF ALL THREE GEAR LATCHES. NO DEFECTS NOTED.

Part: BEAM — CRACKED (AFT BULKHEAD)

WHILE IN "B" CHECK MAINTENANCE FOUND CRACK ON AFT BULKHEAD LATERAL STRUCTURE, 4TH BEAM (J-BEAM) FROM THE BOTTOM, ON LWR LEG OF BEAM. REPAIRED PER UPS EO DC8-5310-6598.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMER EXIT LIGHTS INOP. REPLACED BATTERY PACK.

Part: UPLATCH MECH — OUT OF ADJUST (LT MLG DOOR)

PILOT REPORTED DURING DEPARTURE FROM DFW, THE GEAR NOT LATCHED LIGHT ILLUMINATED. THE ALTERNATE GEAR/DOOR WARNING SYSTEM INDICATED THE MAIN GEAR DOOR CLOSED. PERFORMED THE 'GEAR/DOOR NOT LATCHED LIGHT ILLUMINATED' CHECKLIST, AND HAD TO CYCLE THE GEAR 2 TIMES BEFORE SUCCESSFUL UPLATCH CHECK. FOUND LOCKING TAB SHEARED AND LOCKING NUT LOOSE, NOT SAFTIED ON LEFT GEAR DOOR UPLATCH CYL. FOUND LEFT GEAR DOOR UPLATCH MECHANISM OUT OF RIG. ALSO, RT GEAR DOOR UPLATCH PROX SWITCHES LOOSE. COMPLETED MM PROCEDURE 32-31-04. OPS CHECK NORMAL.

Part: UPLOCK MECH — OUT OF ADJUST (LT MLG DOOR)

PILOT REPORTED DURING DEPARTURE FROM DFW, THE 'GEAR NOT LATCHED' LIGHT ILLUMINATED. THE ALTERNATE GEAR/DOOR WARNING SYSTEM INDICATED THE MAIN GEAR DOOR CLOSED. WE PERFORMED THE 'GEAR/DOOR NOT LATCHED LIGHT' ILLUMINATED CHECKLIST AND HAD TO CYCLE THE GEAR 2 TIMES BEFORE SUCCESSFUL UPLATCH CHECK. FOUND LOCKING TAB SHEARED AND LOCKING NUT LOOSE AND NOT SAFETIED ON LEFT GEAR DOOR UPLATCH CYL. FOUND LEFT GEAR DOOR UPLATCH MECHANISM OUT OF RIGG. ALSO, RT GEAR DOOR UPLATCH PROX SWITCH WAS LOOSE. COMPLETED MM PROCEDURE 32-31-04. OPS NORMAL (P/N 4648615-5503, NAS513-7).

Part: ESCAPE SLIDE — REQD REPACK (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY EXIT SLIDE NEEDS REPACK. REINSTALLATION OF SLIDE INTO SLIDE HOLDER ON ENTRANCE DOOR.