N718UP

Part: INU — FAILED (NR 1)

INSPECTION TYPE:N/A EN ROUTE - CAPTAIN'S INS WARNING LIGHT ON EADI AND EHSI - LOST MULTIPLE SYSTEMS. CREW DECLARED EMERGENCY AND LANDED UNEVENTFULLY. REMOVED AND REPLACED NR 1 INU IAW MM 34-44-03. ADJUSTMENT TEST DUE. NR 1 INU CHECKS OK IN REF TO AMM 34-44-03.

Part: LINE — LEAKING (HYD SYSTEM)

CREW LOST HYDRAULIC QTY AND PRESSURE. AFTER TOP OF CLIMB, CREW DECLARED AN EMERGENCY. LANDED SAFELY AND A/C WAS TOWED TO GATE. FOUND HYD LINE FOR BOGIE TRIM CYL LOCATED ON REAR SIDE OF THE LT LANDING GEAR, LEAKING. REMOVED AND RE-INSTALLED A FLEX LINE AS NEEDED SECURED LINE. PRESSURED HYD SYS. OPS AND LEAK CHECK GOOD.

Part: GAUGE — WORN (L1 DOOR SLIDE)

ENTRY DOOR EMERGENCY ESCAPE SLIDE NEED TO BE REPOSITIONED IN ORDER TO READ THE GAUGE FOR BOTTLE AIR PRESSURE. REMOVED L1 EMERGENCY ESCAPE SLIDE. INSTALLED ADDITIONAL SUPPORT BLOCKS IN L1 EMERGENCY SLIDE CONTAINER REF BLUEPRINT AND INSTALLED ON L1 DOOR IAW MM 25-60-01-2.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2.

Part: FLOOR PANEL — CORRODED (FS 1120 RBL 50) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL CORRODED AT STA 1120 RBL 50. REMOVED FLOOR PNL AT STA 1120 RBL 50 IAW SRM 51-03-00. FABRICATED AND INSTALLED REPAIR FLOOR PNL AT STA 1120 RBL 50 REF EO DC8-5320- 9691C.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 C PIT STA 1260, LONG 35L SPLICE FITTING CRACKED. REPLACED CRACKED SPLICE FITTING AT STA 1260 AND LONG 35L PER SRM 51-01 20D AND SRM 51-03-00.

Part: BRACKET — CRACKED (LWS 28.00) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 LT AUX TANK MAIN PNUEMATIC MANIFOLD CENTER MOUNT BRACKET IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR MOUNT BRACKET AT LT AUX TANK STA XFS 28.000 IAW SRM 51-1-21 AND DWG 4766565.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 AFTER L28R WAS REMOVED FOUND END FITTING CRACKED AT STA 1690, AFT FITTING. REMOVED AND REPLACED LONG END FITTING AT STA 1690 AND L28R PER SRM 51-1-21 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1690 L28R) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 AFTER REMOVAL OF EXISTING REPAIR AT L28R STA 1690, FOUND L28R CRACKED AND INTERNAL DOUBLER CUT. REMOVED AND REPLACED L28R AND INTERNAL DOUBLER AT STA 1690 IAW SRM 53-05-01 FIG 007 AND DWG 5649328.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 D-PIT STA 1340 L34L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 1340 L34L IAW SRM 51-01-20, AND SRM 51-03-02.

Part: INTERCOSTAL — CORRODED (BS 300-320) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 300-320 RBL48 IN A-PIT HAS EXFOLIATED CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IN A-PIT BETWEEN STA 300 AND 320 AT RBL48 IAW WITH DWG 9754034, SRM 51-01-21, SRM 51-01- 20D, SRM 51-3-0, SRM 51-1-8 AND SRM 51-3-0.

Part: FLOORBOARD — DAMAGED (FS 660-760) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD LT OUTBD STA 660-760 HAS DAMAGED INSERT. REMOVED, FABRICATED, AND INSTALLED MAIN CABIN FLOORBOARD AT STA LT OUTBD 660-760 REF E0 DC8-5320-9691-C.

Part: LONGERON SPLICE — CORRODED (BS 1270 L31L) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 C CARGO COMPT STA 1270 AND L31L SPICE HAS CORROSION. REPLACED LONGERON SPLICE AT STA 1270 AND L31L PER SRM 51-1-20D, SRM 53-2-0 FIG 1F AND SRM 51-3-2.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 COCKPIT SUBFLOOR FINGER DOUBLER HAS 10EA POPPED RIVETS FROM CORROSION AT STA -32 TO -12 RBL 24. REMOVED CORROSION AT COCKPIT SUBFLOOR FINGER DOUBLER AT STA -32 TO -12 IAW SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -32 TO -12 RBL 24 IAW SRM 51-1-21 AND DWG 5612298.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL LT INBD STA 540-660 IS DAMAGED. REMOVED, FABRICATED, AND INSTALLED FLOOR PNL AT LT INBD STA 540 TO 660 REF EO DC8-5320-9691-C.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL RIGHT INBD STA 660-760 IS DAMAGED AT END OF PLANK. REMOVED, FABRICATED, AND INSTALLED MAIN CABIN FLOOR PNL AT RIGHT INBD STA 660-760 REF EO DC8-5320-9691-C.

Part: LONGERON SPLICE — CORRODED (BS 1280 L35R) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 C CARGO COMPARTMENT STA 1280, LONGERON 35R AND SPLICE HAVE CORROSION. REPLACED LONGERON 35R SPLICE FITTING REF SRM 51-01-20D AND SRM 51-01-24.

Part: FITTING — CORRODED (BS 340) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FITTING STA 340 RBL 46 HAS CORROSION IN A PIT. REMOVED FITTING, REPAIRED AND REINSTALLED PER SRM 51-1-20D, SRM 51-1 -8 AND SRM 51-02-00.

Part: FLOORBOARD — CORRODED (FS 1560 RBL 50) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD HEAVILY CORRODED STA 1560 RBL 50 REMOVED FLOORBOARD AT STA 1560 RBL 50. FABRICATED AND INSTALLED REPAIR FLOORBOARD AT STA 1560 RBL 50 REF EO DC8-5320-9691C.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 D-PIT STA 1380, L31R FLOOR BOARD SUPPORT IS CRACKED. STOP DRILLED CRACKS ON FLOOR SUPPORT IN D-PIT AT STA 1380, L31R IAW EO DC8-5320-6176.

Part: FLOORBOARD — DAMAGED (FS 880-1020) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOOR PANEL CENTER RT STA 880-1020 HAS BAD INSERT AND DAMAGED HOLE. REMOVED, FABRICATED AND INSTALLED MAIN CABIN FLOORBOARD PNL AT STA 880-1020 IAW EO DC8-5320-9691-C.

Part: FLOORBOARD — DAMAGED (FS 660-760) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL LT INBD STA 660-760 IS DAMAGED AND CRUSHED. REMOVED, FABRICATED AND INSTALLED MAIN CABIN FLOOR PNL AT STA 660- 760 REF EO DC8-5320-9691-C.

Part: CHANNEL — CRACKED (BS 732 RBL 65) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 RT BELLY PANEL LANDING FRAME CRACKED AT STA 732 RBL65. REMOVED, FABRICATED AND INSTALLED RT BELLY PANEL LANDING CHANNEL AT STA 732 AND RBL 65 PER DWG 5649893, SRM 51-1-21, SRM 51-1-20D AND SRM 51-01-24.

Part: STRINGER SPLICE — CRACKED (FS 1340 L35L) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 AT CARGO COMPT STA 1340 L35L SPLICE IS CRACKED. REMOVED AND REPLACED L35L SPLICE FITTING AT STA 1340 IAW SRM 51-01- 20D AND SRM 51-1-15.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,818 hrs · 47,299 cycles

INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 320-340 RBL 45 HAS CORROSSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL REF TRAVELER 78441190001, SRM 51-1-24, SRM 51-1-8, SRM 51-1-21 AND SRM 51-1-20D.

Part: FLOORBOARD — CORRODED (FS 540-660) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD RT OUTBD STA 540-660 IS DELAMINATED AND CORRODED. REMOVED, FABRICATED, AND INSTALLED MAIN CABIN FLOORBOARD AT RT OUTBD STA 540-660 REF EO DC8-5320-9691-C.

Part: WEB — CORRODED (BS 320-340 L23R) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 WEB ABOVE A PIT DOOR CUT OUT BETWEEN STA 320-340 HAS CORROSION. REPAIRED WEB ABOVE A PIT DOOR CUT OUT BETWEEN STA 320-340 PER SRM 53-02-00 FIG 23.

Part: DOUBLER — GOUGED (NR 3 SPOILER) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 NR 3 LT SPOILER BOARD REPAIR DOUBLER IS GOUGED INBD LWR EDGE. REMOVED AND REPLACED REPAIR DOUBLER ON NR 3 LT SPOILER BOARD IAW SRM 51-01-09A, AND SRM 57-07-01-0 FIG 005.

Part: FLAP TRACK — DAMAGED (LWS 340) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 LT FLAP TRACK MISSING CHROME AT STA 340. REPLACED LT FLAP TRACKS AT STA 340 IAW MM 27-51-9 AND MM 27-51-3.

Part: WEB — CRACKED (WING) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 NR 1 MAIN WEB CRACK JUST ABOVE CTR SPAR BET XRS255 AND XRS250 L/W. REPAIRED NR 1 MAIN WEB CRACK ABOVE CTR SPAR BET XRS 255 AND XRS 250 PER SRO 8570005 AND EA 008-5710-01-A1259.

Part: FRAME — CORRODED (BS 1973) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 TAILCONE LOWER NAV LIGHT CUTOUT HAS POPPED RIVET, CORROSION AND BARE METAL ON FRAME. REPAIRED TAILCONE FRAME AND DOUBLER AT STA 1973 IAW EA 008-5310-01-A1280 AND RAA DC8-53-20677.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FLOORBOARD PANEL NR 680 CRACKED AND BENT AND HAS CORROSION. REPAIRED FLOORBOARD PANEL NR 680 BY FABRICATION AND INSTALLATION OF SKIN TO 3 HAT CHANNELS IAW SRM 51-1-21, SRM 51-3-02 AND SRM 51- 1-8.

Part: FLOOR SUPPORT — GOUGED (FS -12.000) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FLOOR BOARD NR 676F HAT CHANNEL IS GOUGED. REMOVED AND REPLACED HAT CHANNEL ON FLOORBARD PANEL NR 676F IAW SRM 53-07-03-0.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FLOORBOARD PNL NR 682A HAS CORROSION ON NR 682 CUT OUT. REPAIRED FLOORBOARD PNL NR 682A PER SRM 53-07-01 FIG 1, SRM 51-01-21, AND SRM 53-2-0 FIG 1F.

Part: DOUBLER — CRACKED (RUDDER) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 INTERNAL DOUBLER CRACKED ON LOWER EYEBOLT ACCESS HOLE ON RUDDER. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER PER DWG 5655077 AND SRM 51-1-21.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FLOORBOARD PNL NR 680 HAT CHANNELS ARE CUT AND GOUGED AS MARKED. FABRICATED AND REPLACED 3 HAT CHANNELS ON FLOORBOARD NR 680 IAW SRM 53-07-03 FIG 1A SHT1, SRM 51-3-2 AND SRM 51-1-8.

Part: HINGE — CRACKED (FS 1160) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 D-PIT DOOR FWD DOOR LINK HINGE WEB CRACKED IN DOUBLER. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER ON D-PIT DOOR FWD LINK HINGE WEB IAW SRM 51-1-21, AND SRM 51-02-00-0, AND DWG 5616673.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 2 EA CREASED DENTS ON UPPER OUTBD SURFACE OF LT ELEVATOR. CUT OUT DAMAGE AT LT ELEVATOR STA XE 219 IAW SRM 55-02-01-0 FIG 008. FABRICATED AND INSTALLED SKIN SPLICE REPAIR AT LT ELEV UPPER SURFACE AT STA XE 219 IAW SRM 55-02-01.

Part: ANGLE — BROKEN (HORIZ STAB) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 RIGHT HORIZ STAB 2ND FROM AFT MOVEABLE FAIRING ATTACH "H" ANGLE BROKEN. REMOVED, FABRICATED, AND INSTALLED "H" ANGLE ON RIGHT HORIZ STAB 2ND FROM AFT MOVEABLE FAIRING IAW SRM 51-01-21-0, AND DWG 3702408.

Part: FRAME — CRACKED (BS 1580 L21R) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 RT STA 1580 FRAME CRACKED ABOVE CUSP, MAIN CABIN. REPAIRED RT STA 1580 FRAME ABOVE CUSP IAW SRM 53-02-00 FIG 02, SRM 51-1-8, AND SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON STA 834 FRAME BELOW RIGHT CUSP. REPAIRED LOWER FUSELAGE FRAME CENTER TO REAR SPAR FITTING AT STA 834 L21R IAW SAA EA 008-5320-01-A1254, UPS RAA DC8-53-20673, AND FAA FORM 8100-9.

Part: FLOORBOARD — CRACKED (FS -52.000) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 NUMEROUS HAT CHANNELS CRACKED FLT DECK FLOORBOARD NR 678. REMOVED AND REPLACED CRACKED HAT CHANNELS ON FLT DECK PNL NR 678 IAW SRM 51-1-21 AND DWG 3619353.

Part: FRAME — BROKEN (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 STA 1580 FRAME BROKEN ABOVE CUSP, LT SIDE L21L. CUT OUT DAMAGED AREA OF FRAME 1580 ABOVE CUSP LT SIDE IAW SRM 53-02 -00 FIG 02. FABRICATED AND INSTALLED FRAME SEGMENT AND 2EA REPAIR ANGLES ON FRAME 1580 L21L IAW SRM 53-02-00 FIG 002.

Part: FLOOR PANEL — CRACKED (FS 80 LBL 42) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FLOOR PNL F-45 CRACKED AT SCREW HOLE AFT RT SIDE OF LAV. FABRICATED AND INSTALLED REPAIR DOUBLER ON FLOOR PNL F-45 IAW SRM 53-02-03 FIG 010.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 AREA ABOVE HORIZ STAB FWD OF RUDDER PCU STA 1810 LBL 30 FLOOR WEB HAS CRACK. STOP DRILLED CRACKED WEB AT STA 1810 LBL 30 IAW SRM 53-02-00 FIG 1B. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 1810 LBL 30 IAW SRM 53-02-00 FIG 1B.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 2 EA EDGE CRACKS ON INBD LWR EDGE OF LT ELEVATOR. REMOVED AND REPLACED LWR SKIN PANEL AT STA XE 21.471-XE 49.143 IAW SRM 51-1-21, AND SRM 55-02-00 FIG 006.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 CABIN STA 5 RBL 48 AND RBL 50 FLOORBOARD SUPPORT CRACKED. REMOVED AND REPLACED FLOORBOARD SUPPORT IN MAIN CABIN AT STA 5 RBL 48-50 IAW DWG 5613327, AND SRM 51-01-20D.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 CRACKED FASTENER HOLE ON LT HORIZONTAL STAB T/E LIGHTENING HOLE OUTBOARD OF NR 1 ELEV ATTACH BRACKET. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT HORIZONTAL STAB T/E AT STA XET 21.471 IAW DWG 5652086, AND SRM 55-2-0.

Part: STOP FITTING — CORRODED (FS 320) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 A-PIT DOOR STOP PAD MOUNT AFT HAS EXFOLIATION CORROSION. REMOVED AND REPLACED A-PIT DOOR STOP PAD MOUNT FITTING AT STA 320 IAW SRM 51-03-00-0 AND SRM 51-1-21.

Part: DRAG ANGLE — CRACKED (NR 1 PYLON) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 NR 1 PYLON INBOARD DRAG ANGLE CRACKED 1/4" PAST STOP DRILL. STOP DRILLED CRACK ON NR 1 PYLON DRAG ANGLE IAW EO DC8-5740-07164, CRACK DOES NOT EXCEED LIMITS OF 3" PER EO DC8-5740-07164.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 FWD ACCESSORY COMPT AT L25R INTERCOSTAL HAS 2EA CRACKS AT FASTENER HOLES. REMOVED INTERCOSTAL AT L25R FWD ACCESSORY BAY IAW SRM 51-01-21, FABRICATED AND INSTALLED REPAIR INTERCOSTAL AT L25R FWD ACCESSORY BAY IAW DWG 5703478, AND SRM 51-01-21.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 REPAIR DOUBLER CRACKED ON R/MLG INBD DOOR INTERIOR SKIN, BOTTOM. REMOVED CRACKED REPAIR DOUBLER ON R/MLG INBD DOOR INTERIOR SKIN IAW SRM 51-01-21A. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/MLG INBD DOOR INTERIOR IAW SRM 52-06-00 FIG 1.

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED 2EA PLACES AT INBOARD LIGHTNING HOLE. REMOVED, FABRICATED, AND INSTALLED REPAIR WEB ON LT HORIZ STAB REAR SPAR AT INBOARD LIGHTNING HOLE IAE DWG 5652086, AND SRM 51-03-00.

Part: FAIRING — DELAMINATED (FS 1834) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 RT HORIZONTAL STAB FAIRING IS DELAMINATED. REMOVED DELAMINATED CORE AND SKIN ON R/HORIZ LWR STAB FARING IAW SRM 51-1-9A. FABRICATED AND INSTALLED REPAIR CORE PLUG AND DOUBLER IAW SRM 51-1-9A.

Part: LONGERON — CRACKED (FS 921 L24L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CRACK ON BOTTOM OF L24L STA 921. STOP DRILLED CRACK AT STA 921 L24L IAW SRM 53-02-02. AREA HAS EXISTING REPAIR PER SRM 53-02-02-0, NO FURTHER ACTION REQUIRED.

Part: BRACKET — CRACKED (RUDDER) · airframe 70,868 hrs · 47,279 cycles

INSPECTION TYPE:C2 RUDDER L/E FAIRING ATTACH BRACKET CRACKED IN 3 EA PLACES, BETWEEN TOP AND 2ND FROM TOP HINGE POINTS. REMOVED, FABRICATED AND INSTALLED REPAIR BRACKET ON RUDDER L/E IAW SRM 51-01-21, AND DWG 5701591.

Part: ACCESS PANEL — DISLODGED

AFTER T/O LOUD NOISE COMING FROM LEFT FORWARD WINDOW AREA. NOISE WAS SO LOUD DIFFICULT TO COMMUNICATE IN COCKPIT. PRESSURE HELD IN COCKPIT UP TO 11,000 FT FOUND CAPTS CLEARVIEW WINDOW EMERGENCY ACCESS PANEL POPPED IN. RESET CAPTS WINDOW EMERGENCY ACCESS PANEL IAW MM 56-10-03-6. OP CHECK GOOD ON CAPTS CLEARVIEW WINDOW.

Part: A/C PACK — ODOR (RIGHT)

FOWL ODOR EMITTING FROM RT PACK. OPERATED THE RT PACK WITH A GROUND CART AND WITH THE NR 3 AND NR 4 ENGINES SEPARATELY PER AMM 21-55-00-5. ENSURED NO FUMES OR ODORS CAME FROM THE RIGHT PACK. COMPLIED WITH H136216, NO FUMES OR ODORS DURING RIGHT PACK OPERATION. A/C IS OK FOR SERVICE.

Part: A/C PACK — ODOR (A/C BAY)

INSPECTION TYPE:N/A STALE ODOR IN FLIGHT APPEARS TO COME FROM RIGHT PACK. NO SMELL NOTED WHEN LEFT PACK RAN. TRANSFERRED RIGHT PACK INOP PER MEL 21-38-1. DEFERRAL M348809. PERFORMED ADJ/TEST OF RT PACK W/NO DEFECTS NOTED PER MM 21-55-00-5. DEFERRAL CLEARED.

Part: SLIDE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A DOOR SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED AT SDF. GIRT BAR WAS CORRECTLY STOWED. REINSTALLED SLIDE PER AMM 25-60-01-2.

Part: UNKNOWN — ODOR (COCKPIT)

INSPECTION TYPE:N/A THERE IS AN EXTREMELY FOUL -DIRTY SOCK- ODOR IN THE COCKPIT WITH PACKS ON. ACCOMPLISHED ADJ/TEST OF BOTH PACK SYSTEMS DURING ENGINE RUN. REF MM 21-50-00-5. ALL SYSTEMS CHECK NORMAL. NO ODORS NOTED. NO HISTORY.

Part: FITTING — CRACKED (BS 680 L36-L35L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 STA 680 BETWEEN LONG 36 AND 35L AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 21-1-20D.

Part: FITTING — CRACKED (BS 680 L36-L35R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 STA 680 BETWEEN LONGERON 36 AND 35R AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 1490 L32L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 LONGERON 32L END FITTING CRACKED AT STA 1490. REMOVED SPLICE END FITTING IAW SRM 51-1-21, LOCATED AND DRILLED REPLACEMENT END FITTING IAW SRM 51-3-2, DWG 3619434 AND SRM 51-1-21.

Part: DOUBLER — MISMANUFACTURED (BS 215 L22R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 FUSELAGE EXTERNAL SKIN DOUBLER REPAIR SEVERAL FASTENERS HAVE SHORT EDGE DISTANCE STA 215 L22R-L23R PER DC8- 5330-12800 REPAIR REF: NR 718-2R-11. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 FABRICATED AND INSTALLED REPAIR 2EA FINGER DOUBLERS AND REPAIR DOUBLER IAW SRM 53-02-01 FIG 7, 53-2-1 SRM 51-1-8, AND 53-02-01 FIG 007.

Part: SPLICE — CORRODED (FS 280-300) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 A-PIT AT LONG 36 BETWEEN STA 280-300 LONGERON SPLICE HAS HEAVY CORROSION. REMOVED SPLICE IAW SRM 51-1-20, FABRICATED AND INSTALLED LONG SPLICE FITTING AT STA 280-300 L36 IAW SRM 51-03-02, 51-1-8, 51-1-20D AND SRM 53-02-02 FIG 10.

Part: SPLICE — CORRODED (FS300 L36) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 A-PIT LONGERON 36 STA 300-320 2 EA LONG SPLICES HAVE HEAVY CORROSION. REMOVED 2 EA SPLICES IAW 51-1-20D, FABRICATED AND INSTALLED SPLICE ANGLES IAW SRM 51-03-02, 51-1-8, 51-1-20D, AND SRM 53-02-02 FIG 10.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 CARGO DOOR UPPER AFT CORNER HAS AN 1/2" CRACK WHICH RUNS FROM EDGE OF DOOR CORNER RIVET. CUT OUT DAMAGED AREA IAW SRM 53-2-O FIG 21, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLERS AT D-PIT DOOR UPPER AFT CORNER IAW SRM 53-2-0 FIG 21, 51-1-8 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS L35L-34R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 EXFOLIATION CORROSION ON SHEARTIE AT STA 1400 BETWEEN L35L AND L34R. REMOVED CORRODED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1400 L35L TO L34R IAW DWG 5640229, AND SRM 53-4-1, 51-3-2,AND SRM 51-1-21

Part: SHEAR TIE — CORRODED (FS1460 L32L,L34L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 HEAVY CORROSION ON SHEAR TIE AT STA 1460 L32L AND L34R. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1460 BETWEEN L32L AND L34R IAW DWG 5640323 AND SRM 53-4-1, 51-1-8, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1420 L34R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 LONGERON 34R CRACKED AT STA 1420. REMOVED LONG 34R IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONG 34R AT STA 1420 IAW DWG 3645937, SRM 51-1-8, AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 1394 L33-36R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 SHEARTIE AT STA 1394 L36R-33R CORRODED AND CRACKED REMOVED DAMAGED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1394 L33R-L36R IAW SRM 53-4-1 FIG 51, DWG 5641014, SRM 51-1-8, AND51-1-20D.

Part: SHEAR TIE — CORRODED (BS 1420 L36L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:CC3 SHEAR TIE AT STA 1420 L36L TO L32L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1420 L36L TO L32L IAW DWG5640230, AND SRM 53-4-1, 53-4-1 FIG 51, AND SRM 51-1-21.

Part: SHEAR TIE — CORRODED (BS1440 L36L-L33L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 D-PIT STA 1440 L36L TO L33L SHEARTIE HAS HEAVY CORROSION REMOVED CORRODED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1440 L36L TO 33L IAW DWG 5640231,AND SRM 53-4-1, 51-3-2,AND SRM 51-1-21

Part: SHEAR TIE — CORRODED (FS1480 L34L-33L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 HEAVY CORROSION ON SHEAR TIE AT STA 1480 L34L TO 33L. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1480 L34L TO L33L IAW DWG 5640233, AND SRM 53-4-1, 51-1-8, AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FS1380 L32L-35R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 EXFOLIATION CORROSION ON SHEAR TIE AT STA 1380 L32L TO L35R. REMOVED DAMAGE SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1380 L32L TO L35R IAW DWG 5755075, AND SRM 51-1-8, AND SRM 51-1-20D.

Part: SKIN — CRACKED (BS 1750 L14L) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 REPAIR SURVEY OF THE PRESS FUSELAGE AREA FOUND FUSELAGE EXTERIOR SKIN EXISTING DOUBLER HAS SHORT ED FASTENER AT STA 1750 L14L. REMOVED EXISTING DOUBLER IAW SRM 51-1-20D AND FOUND 2 INCH CRACK IN SKIN, CUT OUT DAMAGED AREA IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR FILLER, FINGER DOUBLERS AND DOUBLER IAW DWG 5772706-19, AND SRM 53-02-01-0 FIG 007.

Part: REPAIR — DAMAGED (FS 1742 L13R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 DURING REPAIR SURVEY OF THE PRESSURIZED FUSELAGE, FOUND 3 CATEGORY "D" REPAIRS AT STA 1742 BETWEEN L13R TO L17R EXTERNAL DOUBLERS. REMOVED 3 OLD REPAIR DOUBLERS IAW SRM 21-1-20D. CUT OUT DAMAGED AREA IAW EA 008-5330-01-A0018. FABRICATED AND INSTALLED -1, -2, -3, AND -4 FILLERS, AND -5 DOUBLER IAW EA008-5330-01-A0018, UPS EO DC8-5330-23674-A, FAA FORM 8100-9, BAC MESSAGE ID 1-151664370 -2,-4, DOUGLAS DWG 5649327, AND SRM CHPT 51 AND 53.

Part: REPAIR — MISREPAIRED (FS 400-200) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 DURING REPAIR SURVEY OF THE PRESSURIZED FUSELAGE, FOUND "A" PIT FWD AND AFT LWR DOOR CORNER REPAIRS NOT PER THE SRM REPAIRS. CUT OUT FUSELAGE SKIN AT L28R FWD AND AFT SIDE OF "A" PIT DOOR CUT OUT IAW SAA EA008-5320-01-A0008, FABRICATED AND INSTALLED -1,-5 -9 DOUBLER,-4,-7, AND -8 FILLERS, -2,-6, AND -10 TRIPLERS, AND -3 SKIN IAW UPS EO DC8-5320-23666-A,FAA FORM 8100-9 DATED 01/17/06, BAC SERV REQ 1-150449480-2, -4, -5, AD 2005-18-07, DWG SN08530001.

Part: FITTING — CRACKED (BS 1769 L10R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 L10R END FITTING CRACKED IN 60 COMPT STA 1769. REMOVED AND REPLACED LONGERON END FITTING AT STA 1769 L10R IAW 51-3-2, AND SRM 51-1-20D.

Part: SPAR CAP — CRACKED (FS 857 LBL41-47) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 NDT FOUND CRACK ON LM LWR SPAR CAP AT LBL41.5- 47 ON VERTICAL LEG. FS 857. REPAIRED LM LWR SPAR CAP IAW SRO 8570009.

Part: CHANNEL — CRACKED (FS 1926) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 INSIDE NR 60 HOLE, STA 1926 5TH SUPPORT CHANNEL RT CORNER CRACKED 1/2" LONG. STOP DRILLED CRACK IAW SRM 51-1-20, FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 1926 5TH SUPORT CHANNEL IAW SRM 53-5-1, AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FS880 LBL3) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 MAIN CABIN SUBFLOOR STA 880 LBL3, FINGER DOUBLER BULGING AND POSSILBLE CORROSION UNDER DOUBLER. REMOVED FINGER DOUBLER IAW SRM 51-1-21, NO CORROSION NOTED UNDER FINGER DOUBLER, FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5645332, AND SRM 51-1-21.

Part: FITTING — CRACKED (FS 781 L18R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 FRAME ATTACH FITTING CRACKED AT FS 781, L18R FWD SIDE REMOVED AND REPLACED FITTING AT FS 781, L18R IAW SRM 51-3-2, AND SRM 51-1-20A

Part: CUSP WEB — CORRODED (BS 1020 L21R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 RT CUSP EXTRUSION AT L21R BETWEEN STA 1020-1040, FOUND CORROSION BEYOND LIMITS IAW SRM 53-4-1 FIG 26A. CUT OUT DAMAGED AREA IAW SRM 51-3-0, FABRICATED AND INSTALLED 4 EA SPLICES, AND CUSP DOUBLER IAW DWG J060296, SRM 51-1-26 SRM 53-02-05-0, 51-1-8, AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 300 L33-34R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 A-PIT UNDER DOOR STA 300, L33R-L34R DOUBLER HAS EXFOLIATION CORROSION. REMOVED CORRODED DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED DOUBLER AT A-PIT STA 300 L33R-L34R IAW DRWG 3754065 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781 L18R) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 MAIN CABIN FRAME ATTACH FITTING CRACKED 2" LONG AT STA 781 L18R AFT SIDE. REMOVED FRAME ATTACH FITTING IAW SRM 51-1-20D. FABRCATED AND INSTALLED ATTACH FRAME FITTING AT STA 781 L18R IAW DWG 3750025, AND SRM 51-3-0, 51-1-8.

Part: KEELBEAM — CRACKED (FS 960-980) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 KEEL BEAM UPPER WEB (SEC STRUCTURE) CRACKED AT BOTH RIB NOTCHES, LT W /W STA.960-980 VIEW FROM ACCESS HOLE WITH MIRROR. REMOVED AND REPLACED WEB IAW DWG 3651959.

Part: SKIN — CORRODED (FS 610-779 L36) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 FWD ACCESSORY COMPT STA 670 BETWEEN L36 TO L35L FUSELAGE SKIN HAS HEAVY CORROSION. REMOVED CORRODED SKIN AT STA 610-779 L31L-L31R IAW SAA EA 008-5320-01-A0019, FABBED AND INSTALLED -1, -2, -3 DOUBLERS, -4. -5, -6, -7, AND -8 STRAPS, AND SKIN IAW UPS ENG FILE NR DC8-53-20527, FAA FORM 8100-9 DATED 01/13/06, BAC MSG NR 1-150178337-2 DATED 01/06-06, SLH-SAT 00009C, AND SAA EA008-5320-01-A0019.

Part: RIB — CRACKED (LT WING) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA XFS 868. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED REPAIR ANGLES AND INSTALLED ANGLES AT LEFT WING LEADING EDGE AT STA XFS 868 IAW SRM 57-02-00, 57-03-00, AND SRM 51-1-20.

Part: LONGERON — CRACKED (L24R BS 880) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 CRACK IN LOWER RADIUS OF L24R, RT W/W STA 880. STOP DRILLED CRACK IAW SRM 53-02-02, FABRICATED AND INSTALLED REPAIR ANGLES -23, AND -24 IAW DPS 7.00-1 SRM 53-02-02,51-3-2 51-1-8, AND SRM 51-1-20D.

Part: SKIN — CORRODED (FS1350-1490) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 REMOVE AND REPLACE LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R. REMOVED AND REPLACED LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3, RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 796. STOP DRILLED CRACK IAW SRM 57-03-01-0, FABRICATED REPAIR ANGLES AND INSTALLED REPAIR ANGLES AT RIGHT O/B LEADING EDGE STA XFS 796 IAW SRM 57-02-00-0, 51-1-8 AND SRM 51-1-20.

Part: RIB — CRACKED (RT WING) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 802. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE IAW SRM 57-03--01-0, AND INSTALLED REPAIR ANGLE AT RIGHT OUTBOARD LEADING EDGE WING STA XFS 802 IAW SRM 51-1-20D.

Part: SKIN — CRACKED (R-1 DOOR) · airframe 70,002 hrs · 46,581 cycles

INSPECTION TYPE:C3 R-1 DOOR FWD UPPER CORNER CRACKED 1/4" LONG. CUT OUT DAMAGED AREA IAW SRM 53-02-00, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT R-1 DOOR UPPER FWD CORNER IAW SRM 53-2-0 FIG 14, 51-1-8, AND SRM 51-1-20D.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERG LIGHTS BATTERY INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD REF MM 33-50-01-2.

Part: TAB — BINDING (RT ELELVATOR)

INSPECTION TYPE:N/A ON TAXI OUT, FOUND BINDING IN ELEV COLUMN MOVEMENT. RT ELEV CNTRL TAB BINDING FOUND PLAY (WEAR) BETWEEN DRIVE TUBE & CRANK-CONTROL TAB. NEED TO ACCOMPLISH A TEST OF THE ELEV & TAB PER MM 27-30-00. WORN BOLT HOLE IN CRANK & TORQ TUBE REPAIRED PER DC8-2730-23267-A. CONNECTED RT ELEV CNTL TAB PUSH ROD AFT BOLT, TIGHTENED & SAFT'D. RT ELEV CNTL TAB CRANK ASSY & O/B DRIVE TORQ TUBE REPAIR REF ABOVE EO&MM 27-30-02-2. GRD CHECKS GOOD. INSTALLED CRANK ASSY TO RT ELEV CNTL TAB O/B DRIVE TUBE REF MM 27-30-02-2&EO. INSTL'D RT ELEV CNTL TAB ACCESS DR. C/W ADJ/TEST ELEV & TAB. OPS GOOD.

Part: FITTING — CRACKED (FS 70 L35L) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP FS 70 L35L END FITTING IS CRACKED BETWEEN ATTACH FASTENER HOLES. REMOVED AND REPLACED END FITTING IAW SRM 51-3-2 AND 51-1-21.

Part: FITTING — CORRODED (BS 70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP FS 70 L30R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND SRM 51-1-21.

Part: FINGER DOUBLER — CORRODED (BS 70-190) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE: SP, FS 70 - FS 190 FINGER DOUBLER BETWEEN L30R - L32R IS CRACKED AND HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW 53-04-01 AND SRM 51-1-21.

Part: FITTING — CORRODED (FS 70 L35R) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP, STA 70 L35R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CORRODED (BS 100-190) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP LONGERON 36 FS 100 TO FS 190 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 36 IAW DWG 5779925 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 55) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP SHEAR TIE AT STA 55 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT STA 55 L34R - L34L IAW SRM 51-1-21 FABRICATED AND INSTALLED SHEAR TIE AT STA 55 L34R -L34L IAW DWG 5613836, SRM 51-1-21 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FS 35) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE: SP, SHEAR TIE AT FS 35 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT FS 35 L34R - L34L IAW SRM 53-2-0 FIG 1F FABRICATED AND INSTALLED SHEAR TIE AT FS 35 L34R - L34L IAW DWG 5613836, AND SRM 51-1-21, 51-1-20D.

Part: FITTING — CRACKED (BS 12) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP L33R END FITTING CRACKED AT STA 12. REMOVED AND REPLACED END FITTING AT STA 12 L33R IAW SRM 51-3-0 AND SRM 51-1-20D.

Part: STRUCTURE — CORRODED (FS 70 L28R-L33L) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP, STA 70 LOWER AFT CHORD HAS EXFOLIATION CORROSION AT APPROX L28R-L33L. CUT OUT CORRODED CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-1-21, 51-1-20D, 53-2-5 FIG 8C.

Part: LONGERON — CORRODED (FS 8-70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP L33R FS 70 TO FS 8.0 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 33R IAW DWG 3642838 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (A/C BAY) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP A/C DOUBLER BETWEEN L26R - L31R FS 30 TO 65 INTERNAL DOUBLER IS EXFOLIATED AT FS 55 TO FS 35. REMOVED AND INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21 & 51-3-0.

Part: DOUBLER — CORRODED (BS8-70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP INTERNAL DOUBLER HAS EXFOLIATION CORROSION AT FS 8 - FS 70 L29R L31R. REMOVED DOUBLER AT FS 8 TO FS 70 L29R TO 31R IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 5649028 AND SRM 51-1-21.

Part: FINGER DOUBLER — CORRODED (BS 8-70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP FINGER DOUBLER AT FS 8 TO FS 70 L31R HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 8 - FS 70 L31R IAW SRM 51-1-20D FABRICATED AND INSTALLED FINGER DOUBLER AT FS 8 TO FS 70 IAW DWG 5649028 AND SRM 51-1-21.

Part: LONGERON — CORRODED (BS 70-8.0) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP L27R FS 70 TO FS 8.0 LONGERON 27R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 27R AT FS 70 TO FS 8.0 IAW SRM 51-1-21 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 8-70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP L30R FS 70 TO FS 8, LONGERON 30R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 30R AT FS 70 - FS 8 IAW SRM 51-1-20 AND 51-20D.

Part: SKIN — CORRODED (BS 21-70) · airframe 69,876 hrs · 46,490 cycles

INSPECTION TYPE:SP TRANSFERRED FROM LOG PAGE 442150, REF DMI LOG D-309966 SKIN CORRODED AT STA 25 - 74 LONG 28R - 31L. REMOVED AND REPLACED BELLY SKIN AT STA -21.92 TO 70 LONG 31R TO L31L IAW EO DC8-5330-8942-D.

Part: LONGERON — CORRODED (FUSELAGE)

LONGERON CORROSION BELLY 30, 31 & 34. LOG PAGES REFERENCED 442142/2,3 & 4441243 REMOVED 52 RIVETS/HI LOKS AT F.S. 70. STA 28R-30R TO VERIFY CORR PERFO RMED LOW FQY, VERIFY MATL LOSS 10-12 SO 05571 QC REF DC8-5330-22862 RE MOVE RIVETS F.S. 35. STA 30R TO VERIFY CORR PERFORMED LOW FQY NO LOSS AT TIME. REMOVE 17 RIVETS FS 25. STR 32R-35R VERIFY CORR, PERFORMED LOW FQY ON STAT 32-32 (R)NO LOS STAT 32-35 20 PERCENT PLUS STAT 35-35 10 PERCENT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING LIGHT CK EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR DID NOT COME ON. PEANUT LIGHT UNDER FRONT INSTRUMENTS DO NOT COME ON AS WELL. REPLACED BATTERY PACK/ RELAY UNIT IAW MM SEC 33-50-01. OPS CHK GOOD.

Part: WINDSHIELD — FAILED (COCKPIT)

F/O'S WINDSHIELD SHATTERED WHEN TURNED ON. APPLIED SEALANT TO F/O WINDSHIELD, REF MM 56-10-02-2. D303437 CLOSED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A, COCKPIT AND ENTRY EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED GOOD PER MM 33-50-01-2.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: N/A AS REPORTED FROM THE FLIGHT CREW EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OK FOR SERVICE.

Part: FITTING — CRACKED (RT WING TANK) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 STRINGER END FITTING IS CRACKED AT NR 3 ALT TANK AT XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING I.A.W. DWG. 3704841 AND SRM.51-1-20D, 51-3-0.

Part: WEB — CORRODED (COCKPIT) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS STATION -67 TO -80 AT RBL 20. REMOVED FINGER DOUBLER,CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND FINGER DOUBLER IAW DWG. 8930026 AND SRM. 51-1-21.

Part: FITTING — CORRODED (AFT LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 1200 LONG.36 TO 35R. REMOVED AND REPLACED FITTING IAW DWG. 3755845 AND SRM. 53-2-0 FIG. 2D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS ATATION 1050 TO 1120 AT LONGERON 31R. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM. 53-4-1 FIG. 17, 51-1-20D,51-1-21.

Part: FINGER DOUBLER — CORRODED (AFT LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA. 1050-1130 AT LONGERON 31L. REMOVED,FABRICATED AND REPLACED FINGER DOUBLER IAW SRM. 53-4-1 FIG. 17 AND SRM. 51-1-20D,51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 965 AT LBL 64. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-7-1 FIG 10 AND SRM 51-1-21.

Part: SKIN — CORRODED (AFT LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, WHILE REMOVING FASTENERS AT STATION 1160-1220,LONG.32R-35R FOUND CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. REMOVED AND REPLACED SKIN BETWEEN STATION 1050 TO 1350 BETWEEN LONG.31L TO 31R IAW DWG. 5750322 AND SRM. 53-1-0,51-1-20D,51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 879-902 AT LBL 64. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-7-1 FIG 10, 51-1-21.

Part: FRAME — NICKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FRAME IS NICKED BEYOND LIMITS AT STATION 620 LONG 35L-35R. BLENDED AREA, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER, FILLER AND STRAP IAW DC8-53A-011,DC8-5310-11728-A

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 INTERCOSTAL WAS BROKEN BETWEEN STATION 500-520 BETWEEN LONG 33R AND 34R. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STA 1726 LONG. 14L IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON STATION 1716 TO 1736, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND STRAPS I.A.W. SRM. 53-2-2 FIG. 10

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 1746 LONGERON 15L IS CRACKED. REMOVED DAMAGE FROM LONGERON,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. SRM. 53-2-2 FIG. 11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 680 LONG 6R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 STATION 879 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5.

Part: INTERCOSTAL — CORRODED (DOOR FRAME) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, CARGO DOOR CUTOUT INTERCOSTAL IS CORRODED BEYOND LIMITS STATION 558 LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5616520 AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION -12 AT LONG. 27L HAS FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF SHUTTER BOX OPENING. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND IN STALLED FILLER AND DOUBLER IAW DC8-5330-4732.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 680 LONG. 5L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3779762 AND SRM. 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 1750 LONGERON 14L IS CRACKED. REMOVED DAMAGED LONGERON SECTION STA 1736 TO 1760, FABRICATED AND INSTALLED REPLACEMENT SECTION AND STRAPS IAW SRM. 53-2-2 FIG. 10.

Part: FITTING — CRACKED (FWD. LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, BATHTUB FITTING IS CRACKED AT STATION 320 BETWEEN LONG. 27L AND 28L. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822 AND SRM.53-2-0 FIG.2D.

Part: FITTING — CRACKED (CARGO DOORWAY) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, A-PIT DOOR FWD. BUMPER SUPPORT FITTING IS CRACKED AT STA. 300 LONG. 27L. REMOVED AND REPLACED FITTING IAW DWG. 3754041 AND SRM. 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 320 BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755824 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FWD. LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 A-PIT RT CARGO TRACK SUPPORT FITTING IS CRACKED AT STATION 100 AT LONG. 34R REMOVED,FABRICATED AND REPLACED FITTING IAW 8110-3 APPROVED DATED 11/24/03 SAA SK 718-027 DATED11/21/03,UPS ENGINEERING FILE NUMBER DC8- 53-20379 DATED 11/25/03 AND SRM. 51-1-20D.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, MAIN CABIN STATION 1360 INTERCOSTAL IS CRACKED AT LONG. 10L CUTOUT DAMAGE,FABRICATED AND INSTALLED ANGLE REPAIR I.A.W. SRM. 53-2-0 FIG. 1B

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1 STATION 1766 FWD SIDE OF AFT PRESSURE BULKHEAD FLOORBEAM ANGLE IS CORRODED BEYOND LIMITS BL 0 TO RBL26. REMOVED,FABRICATED AND REPLACED ANGLE IAW DWG. 5772638 AND SRM. 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, SHEAR TIE IS CRACKED AT STATION 1380 LONG. 29L TO 30L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM. 53-2-0 FIG. 2A.

Part: FITTING — CRACKED (LOWER FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, EXTERIOR FUSELAGE LOWER CENTER SECTION FRAME TO KEELBEAM FITTING IS CRACKED AT STATION 702 RT SIDE OF CENTERLINE. REMOVED AND REPLACED FITTING IAW DWG. 3753757 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, BATHTUB FITTING IS CRACKED AT STATION 1230 BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FITTING IAW DWG. 3755841 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 1140 LONG. 35L FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3758497 AND SRM. 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 1220 BETWEEN LONG 28L-29L. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (AFT LOWER CARGO) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, BATHTUB FITTINGS ARE CORRODED BEYOND LIMITS BETWEEN LONG. 35L TO 35R AT STATION 1150. REMOVED AND REPLACED FITTINGS IAW DWG. 3755845 AND SRM. 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 920 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, MAIN CABIN STA 1756, LONGERON 15R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND STRAPS IAW SRM. 53-2-2 FIG. 10.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, LONGERON 33L IS CORRODED BEYOND LIMITS, STATION 1240 TO 1270. REMOVED LONGERON SECTION BETWEEN STATION 1210 TO 1270,FABRICATED AND INSTALLED LONGERON AND STRAPS IAW SRM. 53-2-2 FIG. 10.

Part: FITTING — CRACKED (LT MLG WW) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE:C1 LT WHEEL WELL OB FITTING UPPER STA. 902 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3641004 AND SRM.53-2-0 FIG.8

Part: LONGERON — CRACKED (AFT CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 1760 LONG. 16L IS CRACKED. CUTOUT CRACKED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION I.A.W. SRM. 53-2-2 FIG.10.

Part: BULKHEAD — CRACKED (AFT CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1 AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT RBL 36, 65 INCHES ABOVE FLOOR LEVEL. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND REPLACEMENT DOUBLER I.A.W. DWG. SRO8530007

Part: BULKHEAD — CRACKED (AFT CABIN) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT LBL 36, 65 INCHES ABOVE FLOOR LEVEL. REMOVED EXISTING REPAIR DOUBLER,CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED FILLER AND REPLACEMENT DOUBLER I.A.W. DWG. SRO8530007,SRM 53-2-5 FIG. 14A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, STATION 1700 LONGERON 11L IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 1690-1700, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE IAW SRM. 53-2-2 FIG. 10.

Part: SKIN — CRACKED (RT WING LE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, RT WING LE UPPER SKIN IS CRACKED AT XFS 304. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. SRM.57-2-1 FIG. 38

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,173 hrs · 45,885 cycles

INSPECTION TYPE: C1, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1500 BETWEEN LONGERON 29L TO 31L. CUTOUT CORRODED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM.53-2-1 FIG. 7.

Part: DOOR FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE: ASV, CRACK IN FUSELAGE DOOR JAM, PIT 31. CRACK STARTS AT JAM GOES TO FIRST ROW OF RIVETS AND INCLUDES SECOND LAYER OF SKIN, LOWER AFT CORNER. *S/D* REMOVED DAMAGE, FABRICATED DOUBLER AND TRIPLER, INSTALLED REPAIR PER SRM 53-02-00-0.

Part: WINDOW — OUT OF ADJUST (COPILOT)

INSPECTION TYPE: PFLT, COPILOTS SIDE WINDOW WILL NOT OPEN DISCOVERED ON POST FLIGHT ADJUSTED WINDOW GUIDE AT TOP FORWARD CORNER OF F/O SLIDING WINDOW.

Part: SUPPORT — CRACKED (FUSELAGE)

INSPECTION TYPE:B CK FWD PRESSURE BULKHEAD SUPPORT FRAME CRACK. FORMED DOUBLER IAW 53-2-0 FIG 1B. FABRICATED DOUBLERS PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER 53-2-0.

Part: FINGER DOUBLER — CORRODED (FUSELAGE)

INSPECTION TYPE:PFLT CORROSION UNDER FINGER DOUBLER AT STA 24 LONGERON 31R AT E/E COMPARTMENT. INSPECTED OUTER SKIN FOR CORROSION LOSS USING LOW FREQUENCY E/E PER NDT STANDARD PRACTICE MANUAL 06-10-02 PROCEDURE NR 2 LOSS OF SKIN INDICATED AT 10 PERCENT C/W EO DC8-5310-16320A INTERIM REPAIR FOR CORROSION AT FINGER DOUBLER.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 68,243 hrs · 45,180 cycles

INSPECTION TYPE:SP STA 1510 FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 22L TO 30L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615372 AND SRM 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER HAS CRACKED SKIN, INTERNAL DOUBLER AND LONGERON 11R. TRIMMED CRACKED SKIN AND INTERNAL DOUBLER, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND STRAP IAW 8110-3 APPROVED SH SK 718-455, DC8-5330-15612-A, AND SRM 53-2-0 FIG 16.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1690 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER FITTING IS CRACKED AT O/B END BETWEEN XFS 47.5 TO XFS 60. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-21, 51-1-20D.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 190 LONG 36 SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3619434,AND SRM. 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 280 ST LONG 32R TO 33R CORNER T-FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3757794,AND SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 FINGER DOUBLER AND SKIN IS CORRODED BEYOND LIMITS STA 1350 LONG 34L-35L. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779915, CUTOUT CORRODED AREA, NDT FOR CRACKS, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 RT UPPER CUSP IS CORRODED BEYOND LIMITS STA 1000-1110 LONG 21R. REMOVED, FABRICATED, AND REPLACED SECTION OF CUSP FROM STA 1080-1110 IAW SRM 53-2-5 FIG 15.

Part: RIB — CRACKED (HORIZ STAB) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS 91.25. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2.

Part: RIB — CRACKED (HORIZ STAB) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 LT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1260 LONG 33R O/B AFT SIDE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1240 LONG 33R I/B INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1770 LONG 17R LONGERON AND END FITTING ARE CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-21, 51-1-20D, AND REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S-1616757, AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 940 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED, AND INSTALLED DOUBLERS IAW SRM 53-2-0 FIG 5.

Part: WEB — CRACKED (RUDDER) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 LOWER RUDDER MEMBRANE IS CRACKED BETWEEN ZR 54.2 AND ZR 61.156, VERTICAL MEMBRANE APPROX 12 INCHES AFT AF L/E. REMOVED, FABRICATED, AND REPLACED WEB/MEMBRANE IAW DWG 5655074, AND SRM 51-1-21.

Part: DOUBLER — CORRODED (TAIL CONE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 TAIL CONE INNER DOUBLER AT 62 ACCESS HOLE, AND LT OUTER SKIN IS CORRODED BEYOND LIMITS STA 1861-1890 APPROX. REMOVED, FABRICATED, AND REPLACED DOUBLER AND SKIN SECTION IAW DWG 5704650, AND SRM 53-1-0, 51-1-21, 51-1-20D.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1220 LONG 27R FLOORBEAM SUPPORT IS CRACKED AT LOWER END. REMOVED AND REPLACED SUPPORT IAW DWG 9754024, AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 LONG 35L IS CORRODED BEYOND LIMITS BETWEEN STA 1380 TO 1400. CUT OUT DAMAGED LONGERON SECTION, FABRICATED AND SPLICED IN SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 70 LONG 27R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1152 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 L-1 DOOR LOWER AFT CORNER DOUBLER DOES NOT CONFORM TO SRM 53-2-0, AND SKIN IS CRACKED AT STA 55 LONG 21L AREA. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1210 LONG 33R BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5894282,AND SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34R TO 35R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 1200 BATHTUB FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 INTERCOSTAL IS CRACKED AT STA 1435 BL 0 ABOVE D-PIT DOOR. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 A-PIT DOOR OPENING FWD LOWER CORNER SKIN IS GOUGED AND CRACKED AT STA 280 LONG 31R-32R APPROX. CUT OUT DAMAGED AREA, NDT FOR CRACKS AT CUTOUT, NO CRACKS NOTED, FABRICATED AND INSTALLED FILLER, DOUBLER, AND TRIPLER IAW SRM 53-2-0 FIG 20 AND SRO8530019.

Part: RIB — CRACKED (RT WING) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 RIGHT WING T/E UPPER RIB IS CRACKED AT XW 5. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 280 LONG 33R O/B BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827, AND SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 340 LONG 33R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755827,AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 L-1 DOOR FWD UPPER CORNER DOUBLER DOES NOT CONFORM TO THE SRM AND SKIN IS CRACKED AT STA 30 LONG 10L. REMOVED EXISTING DOUBLER AND CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW 8110-3 APPROVED DH SK 718-779.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 STA 883 BL 0 UPPER SURFACE OF WHEEL WELL PRESSURE WEB HAS A FINGER DOUBLER CORRODED BEYOND LIMITS REMOVED,FABRICATED,AND REPLACED DOUBLER IAW DWG 5645332,AND SRM 51-1-21.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 UPPER FUSELAGE ANGLE AT BASE OF VERTICAL STAB AT STA 1723.076 CANTED FRAME IS CORRODED BEYOND LIMITS CUT OUT CORRODED AREA,NDT CUTOUT,NO CRACKS NOTED FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-2-5 FIG 16A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1723.076 LONG 15R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, FINGER DOUBLERS, AND FILLERS IAW SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 L-2 DOOR FWD LOWER CORNER FUSELAGE SKIN AND INTERNAL DOUBLER ARE CRACKED AT STA 1620 AT LONG 21L, AND EXISTING DOUBLER DOES NOT CONFORM TO THE SRM. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLERS, DOUBLER AND TRIPLER IAW 8110-3 APPROVED DH SK 718-700.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,094 hrs · 45,077 cycles

INSPECTION TYPE:C2 UPPER FUSELAGE RIGHT SIDE ANGLE AT BASE OF VERTICAL STAB IS CORRODED BEYOND LIMITS AT STA 1722. CUT OUT CORRODED AREA, NDT AT CUTOUT,NO CRACKS NOTED,FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-2-5 FIG 16A.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,094 hrs · 45,027 cycles

INSPECTION TYPE:C2 NR 1 (A-PIT) CARGO DOOR SKIN IS DAMAGED AT LOWER AFT CORNER AT STA 330 LONG 32R. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED FILLER DOUBLER, AND SHIM IAW SRM 52-2-3 FIG 10A.

Part: HEAT SHIELD — CRACKED (NR 3 T/R)

INSPECTION TYPE:IN NR 3 ENG RT TRUST REVERSER HALF STAINLESS SHIELD ON FWD FACE 4 O`CLOCK CRACKED AND PIECE MISSING. ACCOMPLISHED EO DC-8 7830-15530-B.

Part: TAB — BROKEN (ESCAPE SLIDE)

INSPECTION TYPE:N/A, MAIN CABIN SLIDE COVER LOCKING TAB BROKEN OFF. REMOVED AND REPLACED LOCKING TAB BRACKET ON SLIDE CASE. THIS CLEARS M211497 PLACARD REMOVED.

Part: RELIEF VALVE — LEAKING (RT MLG)

INSPECTION TYPE:N/A, ON LANDING A/C LOST ALL HYDRAULIC FLUID. REPLACED THE RT MLG PRESS RELIEF VALVE. BLED SYSTEM CHECKS OK.

Part: BATTERY — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY ASSY, OPS CK GOOD.

Part: RUDDER — OUT OF RIG (TAIL)

INSPECTION TYPE:N/A, PILOT REPORT, RUDDER WENT FULL RT DEFLECTION ON APPROACH. COMPLETED ECA 04957 FOUND RUDDER CONTROL SYSTEM OUT OF RIG. RIGGED PER ECA. OPS CHECKS GOOD PER MM 22-10-00.

Part: SPAR — CRACKED (CENTER WING)

INSPECTION TYPE:C123, THE CENTER WING REAR SPAR LOWER CHORD WAS CRACKED AT XCW 0 TO XCW 2.5. STOP DRILLED CRACKS AND REPAIRED THE SPAR CHORD IAW DH SK718-583.

Part: FITTING — CRACKED (WS 508)

INSPECTION TYPE:C123, FITTING (P/N 5804007T6013) AT XRS 508, LT WING FOUND TO BE CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 5804007 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 340)

INSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS340 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (BS 1050)

INSPECTION TYPE:C123 LONGERON 35R IS CRACKED AT FS 1050. CUT OUT DAMAGED AREA AND SPLICED LONGERON IAW DH SK718-251.

Part: FITTING — CRACKED (WS 74.9)

INSPECTION TYPE:C123, RT WING O/B SIDE OF THE STA XRS 74.9, THE STR 51 AFT END FITTING WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D & 51-3-0.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 816.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 297.5)

INSPECTION TYPE:C123, RT WING L/E RIB AT FS 297.5 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE:C123, LT WING L/E RIB ATV STA XFS 772.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 835)

INSPECTION TYPE:C123, LT WING L/E RIB AT FS 835 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 841.25)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 841.250 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 810 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 454.976)

INSPECTION TYPE:C123, RT WING L/E RIB AT XS 454.976 WAS CRACKED AT THE AFT UPPER END. REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 305)

INSPECTION TYPE:C123 RT WING LWR L/E SKIN DOUBLER AT XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE:C123, RT WING L/E RIB AT FS 304.0 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 570.5)

INSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT FS 570.5 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.

Part: RIB — CRACKED (WS442.185)

INSPECTION TYPE:C123, RT WING L/E RIB AT XS 442.185 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 520.168)

INSPECTION TYPE:C123, RT WING LWR L/E SKIN INTERNAL DOUBLER AT XS 520.168 WAS CRACKED AND A PIECE WAS BROKEN OFF. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW SRM 57-3-1 FIG 5 AND 51-3-0.

Part: CLIP — CRACKED (WS 254.25)

INSPECTION TYPE:C123, RT WING L/E ABOVE AND FWD OF THE NR 3 PYLON CUTOUT STA FS 254.25, THE RIB FWD ATTACH CLIP WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 448.581)

INSPECTION TYPE:C123, RT WING L/E RIB AT XS 448.581 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 753.75)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 753.750 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 735)

INSPECTION TYPE:C123, RT WING L/E RIB AT FS 735 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: ANGLE — CRACKED (WS 520.168)

INSPECTION TYPE:C123, RT WING L/E, INBOARD SIDE OF THE XS 520.168 RIB, THE SLOT AFT BLKHD VERTICAL ATTACH ANGLE WAS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 335.25)

INSPECTION TYPE:C123, RT WING L/E RIB AT FS 335.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 722.5)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 722.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 466.651)

INSPECTION TYPE:C123, LT WING L/E RIB AT FS 466.651 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CORRODED (BS 1460)

INSPECTION TYPE:C123, THE FINGER DOUBLER AT FS 1460 AND LONG 31L WAS CORRODED. REMOVED, FABRICATED AND REPLACED THE FINGER DOUBLER IAW DWG 5615374 & SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:C123, LT WING L/E, FWD OF THE NR 2 PYLON CUTOUT THE L/E RIB FWD ATTACH CLIP WAS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1340)

INSPECTION TYPE:C123 LONGERON 31L BELOW THE FRAME AT FS 1340 IS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED LONGERON AND SPLICED IN A NEW SECTION OF LONGERON IAW DH SK718-829.

Part: RIB — CRACKED (WS 520.168)

INSPECTION TYPE:C123 LT WING L/E STUB WING RIB AT XS 520.168 IS CRACKED ABOVE THE ELECT CONDUIT. STOP DRILL THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:C123 LT WING L/E, INBD SIDE OF THE XS 250.089 RIB, THE INBD SLOT AFT BULKHEAD OTBD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.

Part: LONGERON — CRACKED (BS 215-220)

INSPECTION TYPE:C123, LONGERON 35L FS 215 - 220 WAS CRACKED BEYOND THE STOP DRILL AND CORROSION WAS FORMING INSIDE THE CRACK. CUT OUT THE DAMAGED LONGERON, FS 190 - 230 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (WS 347.75)

INSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS347.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 305)

INSPECTION TYPE:C123 LT WING L/E LWR SKIN DOUBLER AT STA XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-20.

Part: RIB — CRACKED (WS 227.335)

INSPECTION TYPE:C123, LT WING L/E RIB AT FS 227.335 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: DOUBLER — CORRODED (BS 1460)

INSPECTION TYPE:C123 STA 1460 LONG 31L FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5615374.

Part: LONGERON — CORROSION (BS 330-340)

INSPECTION TYPE:C123 BATH TUB FITTING AND BEAM HAVE HEAVY CORROSION INSIDE WEB AT FS 330 TO 340, LONGERON 36. REMOVED AND REPLACED THE FITTING AND THE BEAM (LONGERON) IAW SRM 51-1-20D AND 53-2-0 FIG 1F.

Part: RIB — CRACKED (WS 461.372)

INSPECTION TYPE:C123, LT WING L/E RIB AT FS 461.372 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1050)

INSPECTION TYPE:C123 LONGERON SPLICE FITTING IS CRACKED AT FS 1050, LONGERON 31L. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21.

Part: RIB — CRACKED (WS 476.897)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 476.897 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SPLICE — CRACKED (BS 1340-1360)

INSPECTION TYPE:C123, THE LONGERON 34R SPLICE FITTING WAS CRACKED BETWEEN FS 1340 AND 1360. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:C123 LT INBD L/E UPPER AFT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 5769646 AND SRM 51-3-0.

Part: ANGLE — CRACKED (WS 520.168)

INSPECTION TYPE:C123, LT WING LEADING EDGE I/B SIDE OF THE XS520.168 RIB, THE SLOT AFT BULKHEAD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: INGERCOSTAL — CRACKED (WS 115)

INSPECTION TYPE:C123 LT WING L/E AT XFS 115.0, JUST AFT OF THE ACCESS PANEL, THE INTERCOSTAL IS CRACKED AT THE 2ND FROM THE INBOARD FASTENER. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 3653679 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 0.7095)

INSPECTION TYPE:C123 LT WING L/E RIB AT XILD O.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 435.789)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1210)

INSPECTION TYPE:C123 BATHTUB FITTING CRACKED INSIDE WEB AT FS 1210, LONGERON 33R. REMOVED AND REPLACED THE FITTING IAW SRM 51-2-0 FIG 2D.

Part: RIB — CRACKED (WS 195)

INSPECTION TYPE:C123, LT WING L/E RIB AT FS 195.0 WAS CRACKED AT THE AFT LWR END. REPAIRED THE RIB IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C123 FS 1180, AT LONGERON 33R, THE BANANA FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 448.501)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 448.501 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 225)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA XOLDI6.225 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 304)

INSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT STA XFS 304.0 IS CRACKED FWD OF THE DOUBLER T/E. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 336.75)

INSPECTION TYPE:C123, LT WING L/E LWR SKIN INTERNAL DOUBLER AT FS 336.75 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769589 AND SRM 51-1-20D & 51-1-21.

Part: RIB — CRACKED (WS 250.089)

INSPECTION TYPE:C123 LT WING L/E AT XS 250.089, ABOVE THE WIRE BUNDLES. THE RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1340-1360)

INSPECTION TYPE:C123 BETWEEN FS 1340 AND 1360, LONGERON 30L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1306)

INSPECTION TYPE:C123 CORROSION AROUND UPPER CUSP FITTING MOUNT BOLTS INBD, FWD, AND AFT AND ON FLOORBEAM FS 1306, LT SIDE. REMOVED AND REPLACED THE CUSP FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: ANGLE — CRACKED (BS 1766)

INSPECTION TYPE:C123 SIX INCH CRACK AT FS 1766, UPPER CABIN BULKHEAD ANGLE BETWEEN LONGERON 10L AND 11L. STOP DRILLED CRACK AND REPAIRED THE ANGLE IAW SRM 53-2-5 FIG 1F.

Part: FITTING — CRACKED (RT HORIZ STAB)

INSPECTION TYPE:C123, VERTICAL LEG OF ANGLE (P/N 3701427-2) CRACKED AT O/B END. ANGLE INSTALLED AT I/B END OF THE RT HORIZ STAB, FWD OF ACCESS PANEL 64I. REMOVED AND REPLACED THE ANGLE FITTING IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FITTING — CORRODED (MAIN CABIN)

INSPECTION TYPE:C123 CORROSION AROUND THE UPPER CUSP FITTING MOUNT BOLTS AT FS 1306 LT. REMOVED AND REPLACED THE CUSP FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (BS 1717)

INSPECTION TYPE:C123, AFT FUSELAGE SKIN AT FS 1717, BETWEEN LONG 35R & 36 WAS CRACKED AND HEAVILY CORRODED. REMOVED AND REPLACED THE SKIN FROM FS 1690 TO 1890 IAW SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — CRACKED (LT AILERON)

INSPECTION TYPE:C123, THE LT I/B AILERON LOWER SURFACE INTERNAL DOUBLER FOR ACCESS PANEL 541 WAS BENT AND CRACKED. REPAIRED THE DOUBLER IAW DH SK718-668.

Part: ANGLE — CRACKED (BS 839)

INSPECTION TYPE:C123 LT SIDE OF THE LWR KEEL BEAM AT FS 839, BL 0, BETWEEN THE MLG DOORS, INTERCOSTAL ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 240)

INSPECTION TYPE:C123 FLOOR SUPPORT BEAM CRACKED AND ANGLE FITTING CRACKED AT FS 240, LBL 42. REMOVED AND REPLACED THE ANGLE FITTING AND REPAIRED THE FLOOR SUPPORT BEAM IAW DH SK718-388.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C123 RT WING LWR SKIN ABOVE THE NR 4 PYLON HAS A 5 INCH CRACK, JUST OUTBOARD OF THE OUTBOARD SLOT, OUTBOARD END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A FIG 1.

Part: SKIN — CRACKED (WS 628.75)

INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS628.75 2 FWD OD THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 591.25)

INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS591.25, 2 FWD OF THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 307)

INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS307.0 AT THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 738.75)

INSPECTION TYPE:C123, RT WING L/E RIBS AT FS 735.0 & 738.75 WERE CRACKED AT THE AFT UPPER ENDS. STOP DRILLED CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 572,577,610)

INSPECTION TYPE:C123, RT WING L/E UPPER SKIN WAS CRACKED AT 3 LOCATIONS: FS 572.0, FS 577.0, & FS 610. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38.

Part: DOUBLER — CRACKED (WS 341.5)

INSPECTION TYPE:C123, RT WING L/E AT FS 341.5, THE INTERNAL DOUBLER HAD A 7 INCH CRACK. REPAIRED THE DOUBLER IAW DH SK718-263.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE:C123, RT WING L/E RIBS AT FS 616.25 AND FS 622.5 ARE CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 257.5)

INSPECTION TYPE:C123, LT WING L/E UPPER SKIN AT STA XWS 257.5 IS CRACKED AT 6 HOLES AT L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.

Part: ANGLE — CRACKED (BS 680)

INSPECTION TYPE:C123 FWD ACCY COMPT, FS 680, BETWEEN LONG 22R AND 23R, THE ANGLE INSIDE THE A FRAME IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3642983 AND SRM 5-1-20D.

Part: SKIN — CRACKED (NR 4 PYLON)

INSPECTION TYPE:C123 NR 4 PYLON INBD SKIN AT STA YN 278 IS CRACKED THROUGH A SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK718-147.

Part: SKIN — CRACKED (BS 1750)

INSPECTION TYPE:C123, THE FUSELAGE SKIN WAS CRACKED AT FS 1750 AND LONG 14L. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-1 FIG 7.

Part: LIGHT — INOP (CABIN)

EMERGENCY LIGHT DISARM CHECK DOES NOT CHECK. RELAMPED EMERGENCY LIGHT SWITCH IND LIGHT CKS GOOD PER MM 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:W/,E EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. EMERGENCY LTS GROUND OPERATIONAL TEST NORMAL PER MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, DURING EMER LIGHT BATTERY TEST ALL EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED EMER BATTERY PACK PER MM 33-50-01, OPS CKS GOOD.

Part: SMOKE CURTAIN — TORN (CABIN)

INSPECTION TYPE:SV, MAIN CABIN SMOKE CURTAIN TORN. REMOVED AND REPLACED SMOKE CURTAIN IAW DC8-25-50-02.

Part: SWITCH — STUCK (COCKPIT)

INSPECTION TYPE-N/A, ON PREFLIGHT MOVING EMERGENCY LIGHTS ARM SWITCH TO ARM POSITION, WOULD NOT EXTINGUISH LIGHTS. DISARM LIGHT EMERGENCY LIGHT OPERATION WAS NORMAL. HOWEVER, WITH SWITCH IN ARMED POSITION. FOUND EMERGENCY LIGHT SWITCH STUCK IN TEST POSTION. RELAMPED BULB, OPS CHECK NORMAL.

Part: DOOR JAMB — CRACKED (CARGO COMPT)

INSPECTION TYPE-C/CK, FWD CARGO PIT AFT DOOR JAMB HAS 2 CRACKS AT LOWER CENTER OF DOOR JAMB. REMOVED CRACKED OUT AREA, FABBED DOUBLER IAW DAC DWG 5641013 AND UPS EO 5350 7876. INSTALLED PER UPS EO 5350 7876.

Part: CLIP — CRACKED (RT WING)

INSPECTION TYPE-C/CK, RIB TO STRINGER CLIP CRACKED NR 4 MAIN OUTBOARD. REMOVED AND REPLACED CLIP IAW DC8 SRM 51-1-24 AND 51-1-20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.

Part: INTERCOSTAL — CRACKED (BS 80)

INSPECTION TYPE-C/CK, FWD PIT FS 80 LONGERON 33 RIGHT INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL IAW DC8 SRM 51-1-21, FABBED NEW ONE IAW DC8 SRM 53-3-2 AND 51-1-4, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-21.

Part: PYLON — CRACKED (NR 4)

INSPECTION TYPE-C/CK, REPAIR CRACKED NR 4 PYLON STUB WING PER EO UPS DC8 5720 9700 A AND OPS 295. FABRICATED REPAIR PER DAC DWG SRO 8570014 AND UPS REO DC8 5720 970D. INSTALLED PER DAC DWG SRO 8570014 AND UPS REO DC8 5720 970D.

Part: FITTING — CRACKED (WS 740)

INSPECTION TYPE-C/CK, STRINGER ATTACH FITTING ON AFT SIDE OF 1ST STRINGER FWD OF REAR SPAR AT XRS 74 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D, ALODINED AND PRIMED AS REQUIRED PER DC8 SRM 51-1-8.

Part: FRAME — CORRODED (BS 1280)

INSPECTION TYPE-C/CK, AFT PIT STA 1280 AND L36 FRAME CORRODED. REMOVED CORROSION, FABBED REPAIR STRAP PER REO 03898. ALODINED AND PRIMED AS NEEDED IAW DC8 SRM 51-1-8. INSTALLED REPAIR STAP PER REO 038 98.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE-C/CK, MAIN FRAME FUSELAGE STATION 717 LEFT HAND SIDE HAS CRACK AT BOTTOM EDGE BELOW FLOOR. REMOVED FITTING, NEW FITTING FABBED ON OPERATION 50005 OP 197068. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1540-1550)

INSPECTION TYPE-C/CK, AFT ACCY COMPT LONGERON 29 RIGHT CORRODED, CRACKED AND HAS SHEARED RIVET AT STA 1540 TO 1550. REMOVED DAMAGED LONGERON FROM FS 1510 TO 1570 IAW DC8 SRM 51-1-21, FABBED NEW SECTION OF LONGERON IAW DC8 SRM 53-4-1 PG 160D AND DC8 SRM 51-1-24. FABBED REPAIR STRAPS IAW DC8 SRM 53-2-2 FIG 8. INSTALLED PARTS IAW DC8 SRM 51-1-21 AND 51-1-250D.

Part: FRAME — CORRODED (BS 360)

INSPECTION TYPE-C/CK, FWD PIT STA 360 CORRODED FRAME FROM L35L TO L35R. REMOVED CORROSION, FABBED REPAIR STRAP PER REO 03888. ALODINED AND PRIMED STRAP IAW DC8 SRM 51-1-8. INSTALLED STRAP PER REO 03888.

Part: LONGERON — CORRODED (BS 1395-1400)

INSPECTION TYPE-C/CK, AFT PIT STA 1400, 1395 CORRODED FROM LONGERON 27 RIGHT TO LONGERON 34 RIGHT. REMOVED CORROSION, FABBED WEB IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WEB IAW DC8 SRM 53-2-0 AND 51-1-21.

Part: FRAME — CRACKED (BS 1445)

INSPECTION TYPE-C/CK, AFT PIT STA 1445 AND LONGERON 354 RIGHT FRAME GOUGED AND CRACKED. BLENDED DAMAGED AREA, FABBED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALDOINED AND PRIMED AS NEEDED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 5-1-20D.

Part: FRAME — CORRODED (BS 1300)

INSPECTION TYPE-C/CK, CORROSION AROUND FASTENERS AT FUSELAGE STATION 1300 LONGERON 35 RIGHT TO LONGERON 34 LEFT. REMOVED CORROSION, FABBED REPAIR STRAP IAW REO 03901. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED STRAP IAW DC8 SRM 51-1-11 AN D 51-1-20D.

Part: SKIN — CORRODED (BS 1140)

INSPECTION TYPE-C/CK, KEEL PLATE AT LONGERON L36 STA 1140 SKIN BULGING. REMOVED CORROSION IAW DC8 SRM 51-1-8. REMOVED DAMAGED AREA, FABBED DOUBLER AND TRIPLER PER REO 03895. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20.

Part: STRINGER — CRACKED (WS 70.5)

INSPECTION TYPE:C, STA XRS 70.5 STRINGER 14 LEFT WING CRACKED. REMOVED CRACKS, AREA FABRICATED DOUBLER AND FILLER ALODINED AND PRIMED AND INSTALLED DOUBLER FILLER AND CONICAL WATCHERS IAW DC8 SRM 57-2-1 AND 51-1-8 AND 51-1-20D.

Part: ANGLE — CORRODED (BS 160)

INSPECTION TYPE-C/CK, CORROSION ON FRAME TO LONGERON ATTACH ANGLE AT STA 160 LONGERON 21 RIGHT. REMOVED ATTACH ANGLES, FABBED CUP, DRILLED AND INSTALLED CUP IAW DAC DWG 2649943 AND DC8 SRM 51-1-8.

Part: SKIN — CRACKED (BS 1700)

INSPECTION TYPE-C/CK, 1 INCH CRACK IN FUSELAGE SKIN STA 1700 LONGERON 17 RIGHT ALONG SHEAR CLIP FASTENERS. REMOVED CRACKED SKIN IAW DC8 SRM 53-2-1 FIG 7. FABBED DOUBLER AND FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21A AND 51-1-20D AND 51-1-21.

Part: TRAP PANEL — CORRODED (RT MLG WW)

INSPECTION TYPE-C/CK, RIGHT WING WHEEL WELL WHERE TRAP FITTING MEETS L24R HAS CORROSION BETWEEN FITTING AND LONGERON. REMOVED TRAP PLATE FOM, REMOVED CORROSION IAW DC8 SRM 51-1-8 FABBED AND INSTALLED 2 NEW LINES IAW UPS EO DC8 5340 0748 ABD REO 03891. INSTALLED FOOTBALL FITTING AND TRAP PLATE IAW DC8 MM 20-18-0.

Part: FITTING — CORRODED (BS 1580)

INSPECTION TYPE:C, STA 1580 LONGERON 21 RIGHT FRAME END FITTING CORRODED. REMOVED CORROSION. REMOVED FITTING FROM AIRCRAFT IAW DC8 SRM 51-1-8 AND 51-3-0 DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IT IAW DC8 SRM 51-1-20D AND 51-3-02.

Part: FITTING — CRACKED (BS 1580)

INSPECTION TYPE:C STA 1580, L21R FRAME END FITTING CORRODED. REMOVED CORROSION, REMOVED FITTING FROM FITTING AIRCRAFT IAW DC8 SRM 51-1-8 AND 51-3-0. DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IT IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: ANGLE — CORRODED (BS 1690)

INSPECTION TYPE:C/CK, STA 1690 LONGERON 21 RIGHT LOWER FRAME TO CUSP ANGLE HAS CORROSION. REMOVED ANGLE AT CUSP STA 1690 IAW DC8 SRM 51 3 0. DRILLED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED NEW ANGLE IAW DC8 SRM 51-3-0.

Part: SHEAR TIE — CRACKED (BS 710)

INSPECTION TYPE:C, BOTTOM FUSELAGE APPROX STA 710, RT KEEL AREA, SHEAR TIE CRACKED. FABBED SHEAR TIE IAW DC8 SRM 53-2-0 AND 51-1-4. HEAT TREAT IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SR M 51-1-20D.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE:C, FS 300, L28L HAS CRACKED Z FITTING. REPLACED Z FITTING. FABBED REPAIR ANGLES IAW DC8-SRM 53-2-0, LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE:C CORNER FITTING CRACKED INSIDE NR 3 ALT TANK AT STA 74, LOWER FRONT SPAR. FITTING FABBED AND TREATED ON TIMCO OPS 50043. INSTALLED FITTING IAW DC8 SRM 51-1-20D LK CHECK TO BE PERFORMED ON TC NR 1000-03.

Part: BATTERY PACK — DISCHARGED (RADIO SHELF)

EMERG LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK OK. P/N OFF/ON 60-1223-5 S/N OFF FTL064 S/N ON 230.

Part: INSULATION — SATURATED (E/ E COMPT)

A LINGERING SMELL AS STATED IN PREVIOUS WRITE-UPS. FOUND INSULATION IN FWD E/E BAY SATURATED IN LAV FLUID, REMOVED SAME. CLEANED AREA AND DEODORIZED. RAN PACKS. NO DEFECTS NOTED.

Part: LIGHTS — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. ARM SYST KILL POWER NO LIGHTS. PULL CONTROL CIRCUIT BREAKER. SYST. LIGHTS COME ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW M/M 33-50-01. EMERGENCY LIGHTS OPERATION TEST IAW M/M 33-50-01. P/N ON 5708458-503. S/N ON FTL064. P/N OFF 60-1223-5. S/N OFF 335.

Part: STOP — BROKEN (LT EMER EXIT)

INSPECTION TYPE-N/A, LT OVERWING EMERGENCY EXIT HATCH STOP BROKEN FROM BOTTOM OF HATCH, REQ NR A475379.