N814UP

Part: ANGLE — DAMAGED (FUSELAGE)

SIDE WALL STRUCTURAL DAMAGE IN POSITION 2/3 AREA, ATTACHED Z-ANGLE DAMAGED. *SUPPLEMENTAL SDR* FABRICATED AND INSTALLED Z-ANGLE ON 3RD FROM FLOOR AT POS 2/3 PER SRM 57-1-21.

Part: MOUNT — DAMAGED (RT MLG W/W) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RIGHT MLG DOOR SWITCH MOUNT HOLES ELONGATED. REPAIRED RIGHT MLG DOOR SWITCH HOLES IAW DWG 5653490, DC8-3260-16914 AND SRM 51-1-8.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 BOTH PILOTS LOWER SEAT TRACKS WORN, BOTH HAVE BEEN PREVIOUSLY REPAIRED. REMOVED AND REPLACED 2 EACH SEAT TRACKS, OPS CHECK GOOD IAW EO DC8-5340 -18315-B, SRM 51-1-8, 51-1-24.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 NR 1 ALT STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED AND REPLACED STRINGER 65 TO FRONT SPAR FITTING IAW DC 8 SRM 51-03-02, 51-01-20D, 51-01-12, AND 51-1-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CABIN INTERGRANULAR CORROSION ON FLOORBEAM STA 70 BETWEEN RBL 20 AND 48. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-7, 51-1-8, 51-2-0, 53-7-3.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 ALL FASTENER HOLES ON MAIN CABIN FLOOR PANEL F23 BARE WORN, KNIFEDGED, CRACKED, BROKEN OUT, OR CORRODED. PANEL SKIN IS CORRODED. REPLACED 1 EACH HAT CHANNEL, REPLACED SKIN ON PANEL IAW SRM 51-1-21, 51-1-8, 51-3-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CABIN CORROSION ON FLOORBEAM, STA 80 BETWEEN RBL 20 AND RBL 48 (TOP AND BOTTOM). REPAIRED FLOORBEAM AT STA 80 BETWEEN RBL 20 AND RBL 48 IAW SRM 51-02-00 FIG 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 COURIER AREA FLOOR PNL F23 IS CRACKED, CORRODED AND DELAMINATED IN SEVERAL AREAS. FABBED FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 5 SPOTS OF CORROSION ON TOP OF LAV AREA FLOOR PANEL, STA 62-75 RBL 30-37. REMOVED CORROSION WENT OUT OF LIMITS. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-3 FIG 10, 51-1-8.

Part: SEAT TRACK — BROKEN (CABIN) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 PIECE OF SEAT TRACK BROKEN AWAY IN MAIN CABIN STA 75, RBL 47. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-2, 51-3-0, 51-1-8.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 COCKPIT FLOOR PANEL 678 CRACKED AT NOTED LOCATIONS, LOOSE CHAFE STRIP DISBONDED BOOK SHELF BRACKET. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-21, 53-2-00 FIG 1B, 51-3-1.

Part: DOUBLER — CORRODED (RT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RT WING CENTER LE, STALL WARNING SENSOR DOUBLER IS CORRODED. REMOVED CORRODED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW SRM 51 -1-15, 51-1-21, 51-1-8, 51-3-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 END FITTING CRACKED AT STA 1695 L34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-2, 51-1-8, 51-1-11.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK GOUGED STA 270 LBL 65. REMOVED DAMAGE, INSTALLED SEAT TRACK PLUG IAW SRM 51-3-0, 53-2-3 FIG 12, 51-1-8.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK GOUGED STA 415 RBL 24. REPAIRED MAIN CABIN SEAT TRACK AT STA 415 AND RBL 24 IAW SRM 53-02-03-0 FIG 012 AND FIG 006D.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 FLOORBOARD SUPPORT CRACKED AT FWD CARGO PIT STA 520 BETWEEN L34R AND 33R. REMOVED DAMAGED AREA, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21A, 51-1-8, 51-1-24, 53-2-00.

Part: STRUCTURE — DAMAGED (CENTER WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 FH WING CENTER LE HAS LWR ATTACH SCREW HOLE DAMAGED AFT OF SLOT DOOR. REMOVED DAMAGED, FAB AND INSTALL REPAIR DOUBLER IAW SRM 57-3-1 FIG4, EO DC8-5720-4087 APPD C, 51-1-8.

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 INTERGRANULAR CORROSION IN UPPER T/E ATTACH ANGLE ON LEFT I/B AUX TANK NEAR STA XFS 67. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2-0 FIG 37.

Part: DOUBLER — BROKEN (WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 BROKEN REPAIR DOUBLER AT END OF RIB IN LT CENTER LE NEAR STA XFS341. REMOVED AND REPLACED REPAIR DOUBLER END OF RIB IN LT CENTER L/E AT XFS341 IAW SRM 51-1-20D, 57-3-3 FIG 5, 51-2-00 FIG 2, 51-1-8.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 3 DRILL STARTS IN COUNTERSINK ON TOP OF LEFT L/E AUX TANK, OUTBOARD END. OVERSIZED FASTENER HOLE, INSTALLED CONICAL WASHERS, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-1 FIG 37, 51-1-8, 51-3-4, 51-1-26.

Part: FRAME — CRACKED (WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 LT CENTER LE FRAME CRACKED AT AFT END BETWEEN PANELS 522A, 520B. STOP DRILLED CRACK. FABBED REPAIR ANGLE AND INSTALLED IAW SRM 51-1-857 -2-0 FIG 2, 51-1-20D, 51-3-1.

Part: DOUBLER — WORN (RT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RT WING CENTER LE HAS FRETTING WEAR AT OB MATING SURFACE. REMOVED INTERNAL DOUBLER, FABBED NEW DOUBLER AND INSTALLED IAW SRM 51- 3-0, 51-1-21, 57-3-3 FIG 5, 57-3-3 FIG 5, 51-1-8.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RIGHT CENTER L/E HAS LWR ATTACH SCREW HOLE DAMAGED O/B OF FUELING PORT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM EO DC8-5720 -4087, 51-1-8, 51-1-26.

Part: SKIN — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE EXTERIOR SKIN CRACKED AROUND SCREW HOLE AT I/B END. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-1 FIG H.

Part: DOUBLER — BROKEN (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 PIECE OF INTERNAL DOUBLER BROKEN, MISSING AT OB END OF LT WING OUTER L L/E. REMOVED BROKEN DOUBLER, FABBED AND INSTALLED REPLACEMENT INTERNAL DOUBLER AT OB END OF LW OUTER LE IAW SRM 51-1-21, 51-1-8, 51-3-2.

Part: RIB — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB L/E IB SECTION NEAR STA X FS 609, UPPER STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLERS ON L/W OB LEADING EDGE UPPER RIB AT XFS609 IAW SRM 57-3-3 FIG 6, SRM 57-2-0 FIG 2, 51-1-8

Part: SKIN — MISREPAIRED (BS 1690-1766 L28) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 L28R STA 1690-1766 HAS TWO EXISTING DOUBLER NOT CONFORMED TO DWG NR SRO8 5300032 NEED APPX E TO REPAIR. REMOVED DOUBLERS, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, SRO 8530032, 51-3-1.

Part: RIB — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 INNER RIB CRACKED AT AFT END IN LT WING OB LE IB SECTION NEAR STA XFS6 03. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-2 1, 51-1-21D, 51-1-8, 57-2-00.

Part: FITTING — CRACKED (BS 200 L21R) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CABIN STA 200 LONG 21R, CUSP FITTING IS CRACKED. REMOVED AND REPLACED CUSP FITTING.

Part: PANEL — CRACKED (T/E FLAP) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 LEFT I/B FLAP STRUCTURE CRACKED AT NUT PLATE FOR SURFBOARD PANEL INSTALLATION NEAR O/B TRAILING EDGE. STOP DRILL CRACK, FABBED DOUBLER AND INSTALLED IAW SRM 57-2-0, 51-1-21, 51-1-8, 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (LWS 598) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 POSSIBLE CRACK AT DRAIN HOLE, LT WING OB LE IB SECTION LOWER SURFACE NEAR STA XFS 598. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-1, E O DC85720-4087-B, 51-1-8.

Part: RIB — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB LE IB SECTION NEAR STA XFS6 27, UPPER STOPPED DRILLED CRACK. FABBED AND INSTALLED REPAIR DOUBLER.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 LT WING OB LE INTERNAL DOUBLER CRACKED, CHAFED AT IB END OF IB SECTION. REMOVED CRACKED DOUBLER, FABBED AND INSTALLED REPLACEMENT DOUBLER IAW SRM51-1-21, 51-1-15, 51-1-8, 51-3-2.

Part: SKIN — MISREPAIRED (BS 1690-1766 L28) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 L28L STA 1690-1766 HAS 3 EXISTING DOUBLERS, 1 INTERNAL AND 2 EXTERNAL NOT CONFORM DWG NR SRO8530032 NEED APX D TO REPAIR. REMOVED DOUBLER, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, SRO 8530032, 51-1-26

Part: RIB — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 UPPER RIB CRACKED AT END IN LEFT WING O/B LEADING EDGE NEAR STA XFS 809. FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, 57-2-00, 57-3-0 FIG 19.

Part: SKIN — GOUGED (RT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RT WING OB LE UPPER SCREW HOLE GOUGED AND DAMAGED,IB OF ACCESS PANEL51 7B. CUT OUT DAMAGE, FABBED REPAIR AND INSTALLED IAW SRM 57-2-1,51-3-1, 51- 1-8

Part: SKIN — GOUGED (RT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RT WING OB LE UPPER ATTACH SCREW HOLE GOUGED AND DAMAGED ABOVE PNL 518 C. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER,IAW SRM 57-2-1 FIG 38, 51-1-8, 57-2-0, 57-3-1.

Part: SUPPORT ANGLE — BENT (SPOILER) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 SPOILER LANDING SUPPORT FRAME BENT IN LT FLAP WELL I/B SIDE OF STA 98 FLAP HINGE. REMOVED DAMAGE AND FABBED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2, 51-1-8, 51-1-20D, 51-3-1, 51-1-21.

Part: DOUBLER — BROKEN (CARGO DOOR) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 MAIN CARGO DOOR AFT DOOR JAMB HAS A REPAIR DOUBLER WITH 1 INCH PIECE BROKEN OFF. REMOVED DAMAGED DOUBLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, 51-1-8, 52-4-0 FIG 4.

Part: SKIN — CRACKED (LT WING) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 SKIN AROUND LT CENTER L/E INBOARD HOIST ATTACH POINT IS BULGING AND CRACKED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-21, 57-2-00 FIG 2A, 51-1-8 , 51-1-26.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RIGHT AFT FUSELAGE EXTERIOR STA 1550, L24R, FUSE SKIN LOOSE/ POPPED FASTENERS. REMOVED FASTENERS, REMOVED AND REPLACED LONG 24R FROM 1510-1570, RE-INSTALLED FASTENERS.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 F/E AND OBSERVERS SEAT TRACK HAS ELONGATED HOLES AND BARE METAL. REMOVED AND REPLACED SEAT TRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 CORROSION AND MISSING FASTENERS ON FLOORBEAM AT STA 55 RBL 31-48. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, 5 1-2-0, 53-2-0 FIG 1F.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 A/C COMPT STA 8 FWD BULKHEAD RT SIDE LONGERON HAS ELONGATED HOLE. REPAIRED STA 8 FWD BULKHEAD RT SIDE LONGERON ELONGATED HOLE IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-2 AND SRM 51-1-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 RIVET HEAD MISSING ON LT FUSELAGE NOSE SECTION EXTERNAL SKIN. REPAIRED LT FUSELAGE NOSE SKIN IAW SRM 53-02-00, SRM 53-3-3 FIG 1, SRM 53-02-1 FIG 7 AND SRM 51-1-20D.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 STOP HOLES WORN IN F/E'S FOWARD SEAT TRACK. REMOVED AND REPLACED FWD SEAT TRACK IAW SRM 51-3-0, 51-1-8, 51-1-24.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 2ND OBSERVERS FWD SEAT TRACK CORRODED AT RBL 12-16 AROUND MOUNT SCREW COUNTERSINKS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-0, 51-1-8.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 80,477 hrs · 26,441 cycles

INSPECTION TYPE:C3 STOP HOLES WORN IN CO-PILOTS LOWER SEAT TRACKS. REMOVED AND REPLACED SEAT TRACKS IAW EO DC8-5340-18315-B, SRM 51-1-8, 51-1-20D.

Part: GAUGE — UNSERVICEABLE (SLIDE PRESSURE)

ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REPOSITIONED SLIDE IN CASE FOR PRESSURE GAUGE TO READABLE FROM WINDOW.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE)

ESCAPE SLIDE PRESSURE IND SLIDE DOWN BELOW VIEWING WINDOW. REPOSITIONED ESCAPE SLIDE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A ON PRE DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. REF DC8 AMM 24-00-00.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A PIT 33 HAS HOLE IN FLOOR ON LEFT SIDE APPROX 3 FEET AFT OF DOOR MARKED. REPAIRED PIT 33 FLOOR PANEL AS PER EO DC8-5320-8724-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A PIT 33 HAS HOLE IN FLOOR ON RT SIDE APPROX 3 FEET AFT OF DOOR MARKED. REPAIRED HOLE IN FLOOR PIT 33 AS PER EO DC8-5320-8724-A.

Part: GAUGE — OUT OF POSITION (SLIDE BOTTLE)

INSPECTION TYPE:N/A ENTRY DOOR SLIDE PRESSURE GAUGE NOT VISIBLE. REPOSITIONED SLIDE SO PRESSURE GAUGE CAN BE READ.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK WILL NOT CHARGE. EMERGENCY EXIT BATTERY PACK REPLACED IAW DC8 AMM 33-50-01-2.

Part: WINDOW — INOPERATIVE (COCKPIT)

F/O WINDOW (SIDE) INOP, WILL NOT OPEN. ADJUSTED F/O SLIDE WINDOW FOR PROPER OPERATION. OPS CHK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A TWO LIGHTS INOP AT FWD ENTRY DOOR. RELAMPED AS NEEDED. OPS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS FADE OUT DURING TEST. A/C POWERED FOR 2.5 HRS AND BATTERY CHARGE WITH A/C POWER IAW DC8 AMM 33-50-01. CHECKED SERVICEABLE.

Part: MANIFOLD — LEAKING (HYD SYSTEM)

ATB - HYDRAULIC SYSTEM QUANTITY LOSS. NO HYD BRAKE PRESSURE. AIR BRAKES STOPPED A/C. NR 1 & 2 T/R STOWED NR 3 & 4 WOULD NOT STOW. CHECKED ENGINE 2 & 3 EDP'S CASE DRAIN FILTER CHIP DETECTORS-NO DEBRIS FOUND. R&R RT HYD POWER MANIFOLD PER MM 29-10-20-02. OPS/LEAK CK GOOD PER MM 29-10-20. INSTALLED NEW BRAKE CTRL VLV ASSY PER MM 32-42-02-2. OPS/LK CK GOOD PER MM 32-42-02.

Part: SPLICE — CRACKED (FS 1260 L35R) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONGERON SPLICE FITTING IS CRACKED AT STA 1260-1280 L35R. REMOVED AND REPLACED SPLICE FITTING AT STA 1260-1280 L35R IAW SRM 51-03-02-0, AND SRM 51-1-20D.

Part: STRINGER — CRACKED (WING) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 STR END FITTING CRACKED ON STR 51 NR 3 MAIN TANK BETWEEN XRS 23-XRS 50. REMOVED AND REPLACED END FITTING AT STR 51 NR 3 MAIN TANK STA XRS 23 - XRS 50 IAW SRM 51-3-2 AND SRM 51-01-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONG 34R STA 1287-1295 IS CRACKED. REMOVED LONG 34R FROM STA 1270 TO 1350 IAW SRM 51-1-21. INSTALLED REPLACEMENT LONGERON AT STA 1270-1350 IAW SRM 51-01-20-D-0.

Part: FITTING — CRACKED (FS 1140 L34R) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1140 BETWEEN L34R AND L33R. REMOVED END FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED END FITTING AT STA 1140 BETWEEN L34R AND L33R IAW DWG 4758514 AND SRM 53-1-0 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1170 L10L) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 END FITTING CRACKED IN 60 HOLE L10L AT STA 1770. REMOVED END FITTING AT STA 1770 L10L IAW SRM 51-1-21, LOCATED AND DRILLED REPLACEMENT FITTING AND INSTALLED AT STA 1770 L10L IAW SRM 51-3-2, AND SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 FOUND LONG 35R STA 1287-1295 IS CRACKED. REMOVED AND REPLACED LONGERON AT STA 1270-1350 L35R IAW SRM 51-01-20D-0 AND SRM 51-1-21.

Part: FITTING — CRACKED (FS 1140 L35R) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1140 L35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (FS1260 L35L) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 L35L CRACKED AT STA 1260-1280. REMOVED AND REPLACED LONGERON 35L AT STA 1270 TO 1350 IAW SRM 51-1-21, 51-1-20D.

Part: FITTING — CRACKED (FS 1150 L35R) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1150 L35R. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON ATTACH CLIP BETWEEN FLOORBEAM AND FLOOR PNL AFT ACC COMPT CEILING STA 1680 LBL 13. REMOVED CORRODED FLOOR SUPPORT CHANNEL IAW SRM 53-2-0 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL IAW SRM 53-07-01 SRM 51-02-00 AND SRM 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C3 L16L CRACKED BEHIND CANTED FRAME, MAIN CABIN STA 1746 REMOVED END FITTING AND SHEARTIE AT STA 1746 L16L IAW SRM 51-03-00-0. FABRICATED AND INSTALLED LONGERON SPLICE FITTING AND SHEARTIE IAW SRM 53-02-02-0, 53-05-01-0 AND SRM 51-01-20D-0, 53-02-02-0 FIG 10.

Part: DOUBLER — CORRODED (FS 1181-1184 L32) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2, CORROSION ON C-PIT LOWER SKIN DOUBLER STA 1181-1184 BETWEEN L32R-33R. REMOVE, FABRICATE AND REPLACE DOUBLER IAW SRM DWG 3754065, SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1690 L3OL) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONGERON END FITTING AT L30L STA 1690 IS CRACKED. REMOVED AND REPLACED END FITTING AT STA 1690 L30L IAW SRM 51-01-21, AND SRM 51-1-20D.

Part: SPLICE — CRACKED (FS 1690 L24L) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONGERON 24L SPLICE FITTING AT STA 1690 IS CRACKED. REMOVED CRACKED FITTING AT STA 1690 L24L IAW SRM 51-3-0 AND SRM 51-1-21. LOCATED AND DRILLED REPLACEMENT SPLICE FITTING AND INSTALLED AT STA 1690 L24L IAW DWG 4641324, AND SRM 51-01-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

FOUND L34L AFT OF STA 1690 HAS POSSIBLE CRACK ON INSIDE OF FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONGERON SPLCE FITTING L22L JUST AFT OF STA 1690 IS CRACKED. REMOVED SPLICE FITTING IAW SRM 51-1-21, LOCATED AND DRILLED AND REAMED REPLACEMENT FITTING IAW DWG 4641324. INSTALLED SPLICE FITTING IAW SRM 51-3-0, 51-1-21, 51-1-21D, AND DWG 4641324

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONG 23R END FITTING AT STA 1698 CRACKED. REMOVED CRACKED END FITTING IAW SRM 51-1-21 AND SRM 51-3-0 LOCATED, DRILLED, AND DEBURRED REPLACEMENT END FITTING IAW DWG 4641324. INSTALLED REPLACEMENT FITTING AT STA 1698 L23R IAW SRM 51-1-20D AND SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONG END FITTING L30R END FITTING IS CRACKED AT STA 1690. REMOVED END FITTING IAW SRM 51-3-0, LOCATED, DRILLED AND DEBURRED REPLACEMENT END FITTING AT STA 1690 L30R IAW 51-03-02-0,51-01-20D AND SRM 51-03-01.

Part: FITTING — CORRODED (FS 1690 L24L) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LONGERON END FITTING AT STA 1690 L24L HAS CORROSION INSIDE OF FITTING. REMOVED END FITTING AT STA 1690 L24L CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-02-00-0, LOCATED AND DRILLED REPLACEMENT END FITTING AND INSTALLED IAW SRM 51-1-21, 51-1-20D AND SRM 51-3-0.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C3 HFEC INSPECTION DETECTED A .500" CRACK ON THE D PIT UPPER AFT DOOR JAMB. CUT OUT DAMAGE AT AFT UPPER CORNER IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLERS IAW SRM 53-02-00-0 FIG 21, AND SRM 51-01-20D-0.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 CRACKS ON I/B WEB SUPPORT ANGLES ON LT HORIZ STAB FRONT SPAR. REMOVED CRACKED UPPER AND LWR T-CAP ANGLES IAW SRM 51-03-00-0. LOCATED AND DRILLED UP REPLACEMENT T-CAP ANGLES AND INSTALLED IAW SRM 51-3-0, 51-3-2, 51-01-21, AND SRM 51-01-20D.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 CORROSION AND CRACK ON FINGER DOUBLER AT STA -52 TO -64 LBL 17-23. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA -52 TO -64 LBL 17-23 IAW DWG 5612298, AND SRM51-1-21, 51-1-20D.

Part: FINGER DOUBLER — CORRODED (BS 960-980) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 MAIN CABIN CENTER SUB FLOOR FINGER DOUBLER CORRODED AT STA 960 TO 980 RBL 65. REMOVED FINGER DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-07-03 FIG 004, 51-01-21, 53-07-03 FIG 4.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AT STA 925 LBL65. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA 925 LBL65 IAW SRM 53-07-03,53-07-03-0 AND SRM 51-1-21

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C3 STA 834 L22L FWD ATTACH FITTING CRACKED 2" LONG REMOVED ATTACH FITTING AT STA 834 L22L IAW SRM 51-01-20D-0, REPLACED ATTACH FITTING AT STA 834 L22L FWD IAW DC8 SRM 51-3-2 AND SRM 51-1-20D

Part: ANGLE — CRACKED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 CRACK AT STA 1766 LONG 4R ON "L" BRACKET. REMOVED DAMAGED ANGLE IAW 51-01-21, FABRICATED AND INSTALLED ANGLE ATTACHED TO AFT PRESS PANEL AT STA 1766, L4R IAW DWG 5773844, AND SRM 51-01-20D-0, 51-1-8.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER SUB FLOOR FINGER DOUBLER CORRODED AT STA 980 LBL 65. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA 980 LBL 65 IAW DWG 5645332, AND SRM 53-2-0 FIG 1F, 51-03-02,51-1-20D.

Part: SPAR CAP — CRACKED (FS 857) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 LT WHEEL WELL LOWER SPAR CAP HAS A 16 INCH CRACK. REPAIRED LT LWR SPAR CAP FS 857 IAW SRO 8570009.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C3 RT WW LWR SPAR ATTACH ANGLE CRACKED 1" LONG STA 857.125. MACHINED REPAIR ANGLE IAW DWG 5649893 AND INSTALLED REPAIR ANGLE AT RT WW STA 857.125 IAW SRM 51-1-21 AND SRO 8570009.

Part: SPAR CAP — CRACKED (FS 857 RBL30) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C2 RT WW LWR SPAR CAP CRACKED 1 INCH LONG RBL 30. REPAIRED LWR SPAR CAP STA 857 RBL 30 IAW SRO 8570009.

Part: RIB — CRACKED (RT WING) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 RT WING OB FLAPWELL RIB IS CRACKED 1/2 INCH LONG STA XRS 204. CUT OUT DAMAGED AREA IAW 57-02-00-0, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-02-00, 51-3-2 AND SRM 51-1-20D

Part: RIB — CRACKED (RT WING) · airframe 79,514 hrs · 25,692 cycles

RT WING OB LE UPPER RIB CRACKED 1/2" LONG XFS 693. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT UPPER OB RIB RT WING STA XFS 693 IAW SRM 57-02-00, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 RT WING LE UPPER RIB IS CRACKED AT XRS 636. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 57-02-00-0, AND SRM 57-02-00-0.

Part: SKIN — CRACKED (RWS 69.50) · airframe 79,514 hrs · 25,692 cycles

RT UPPER WING SKIN CRACKED 1/2" LONG, AT XCW69.500 REAR SPAR AREA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED 2 DOUBLERS AND 1 FILLER IAW SRM 57-2-1 FIG 20.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 79,514 hrs · 25,692 cycles

INSPECTION TYPE:C1 INTERGRANULAR CORROSION 2 1/2" BY 2 1/2" AREA WHERE LWR VERT STAB L/E AND MIDDLE VERT L/E MATE. REMOVED CORROSION IAW SRM 55-02-00-0, CUT OUT AREA IAW SRM 55-02-01. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55--2-01-0 FIG 4 AND SRM 51-01-21-0.

Part: CONTROL VALVE — BYPASSING (LEFT PACK)

FLT CREW REPORTED SMOKE IN COCKPIT AND PERFORMED AN EMERGENCY EVACUATION VIA ESCAPE SLIDE. SLIDE DEPLOYED NORMALLY. CREW REPORTED LEFT PACK TRIP PRIOR TO SMOKE IN C/P. LEFT PACK TRIP LIGHT ILLUMINATED. FOUND LEFT PACK S/O AND FLOW CNTRL VLV BYPASSING WHEN SELECTED CLOSED. REMOVED AND REPLACED VALVE IAW DC8 MM 21-55-05-4. PERFORMED 4 ENG TO DUPLICATE FLT. CREW CONDITIONS. NO ABNORMAL CONDITIONS NOTED. LEFT AND RIGHT A/C PACKS OPERATING NORMALLY. NO SMOKE/SMELLS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. RELAMPED PER M/M 30-50-02-2 AS NEEDED. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

NO EMERGENCY EVAC LIGHTS DURING BISE CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01-2, OPS CHECK GOOD.

Part: SLIDE — INOPERATIVE (GIRT BAR)

INSPECTION TYPE:N/A, DEPARTURE - ESCAPE SLIDE GIRT BAR WOULD NOT ATTACH TO THE FLOOR MOUNTS. DEFERRED PER MEL M290986. REMOVED AND REPLACED CONTAINER FOR EVAC SLIDE, OPS CKS GOOD. M290986 CLOSED.

Part: PANEL — INOPERATIVE (LANDING LIGHT)

DURING TROUBLESHOOTING OF M277846 LANDING LIGHT INOP, MTC FOUND OVERHEAD LANDING LIGHT PANEL BURNED INTERNALLY AND WIRING SHORTED. OVERHEAD LIGHTING PANEL REMOVED & PLACED IN 5X STORES. REPLACED SWITCH 31-58, 51-59 & 51-61 AND ACCOMPANING WIRES TO DISCONNECTED PER SWPM. CHECKED REMAINING WIRES, ALL OKAY.

Part: RETAINER — INOPERATIVE (RT MLG DOOR)

RT MLG DOOR OPEN IN FLIGHT. POSSIBLE PROBLEM WITH DOOR RETRACT SYSTEM. FERRY TO SDF FOR REPAIR. RMVD RT MLG IB DOOR. RMVD ACCESS COVER FOR ALT INDICATOR SINKER PLATE. INSTALLED MLG DOOR ALT IND STRIKER PLATE. OK TO REINSTALL ACCESS COV ER. OK TO INSTALL SERVICEABLE RT INBOARD GEAR DR. INSTALLED HINGE PINS. OK TO INSTALL HINGE PIN RETAINERS. INSTALLED HINGE PINS RETAINERS. INS TALLED & ADJUSTED RH MAIND GEAR DOOR IAW DC8 MM 32-12-01.

Part: SOCKET — LOOSE (EMERGENCY LIGHT)

INSPECTION TYPE: ASN, DOOR ENTRY AND EMERGENCY LIGHTING FIXTURE NOT SECURED. SECURED DOOR ENTRY AND EMERGENCY LIGHTING TO HOUSING.

Part: COALESCER BAG — DIRTY (AIR CONDITIONING)

ODOR OF SMOKE IN COCKPIT. DURING DEPARTURE UNKNOWN ORIGIN MAYBE COMING FROM PACKS LT READ 80 DEGREES, RT READ 200 DEGREES ALL OTHER GAUGES READ NORMAL, T/S FOUND WATER SEPERATOR VERY DIRTY INDICATION WAS A PACK OVERHEAT RAN PACKS ON GROUND WITH NO ODOR OF SMOKE OR ANYTHING ELSE O.K. FOR CONTINUED SERVICE.

Part: BEAM — CORRODED (C1 DOORWAY) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, FWD PIT C1 DOOR JAMB CORNER TORQUE BOX BEAM IS CORRODED BEHIND T-BOLT LATCHES. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND WITHIN LIMITS IAW DAC DWG 9754007, REO G09673. MAT ID FOR SHIM 4340 STEEL BAR PO 371199.1 IAW REO G0967 3, FABRICATED SHIM IAW REO G09673, PRIMED SHIM IAW DC8 SRM 51-1-8, INSTALLED SHIIM IAW REO G09673.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, REMOVED BATHTUB FITTING AT STA 879 AND FOUND THE SKIN UNDER FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. MATERIAL ID FOR FILLER IAW REO G09662, FABBED FILLER IAW REO G09 662. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER IAW REO G09662.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, CABIN STA 680 LONGERON 11 RIGHT SIDE FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-3-5. LOCATED NEW FITTING, DRILLED EXISTING FASTENER HOLES, DEBURRED IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-3-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, AFT PIT STA 1540 RBL 30 INTERCOSTAL ON AFT BULKHEAD CRACKED AT NUT PLATE. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE:C1 RIGHT WHEEL WELL AFT OTBD SIDE CANTED FRAME HAS SEVERAL AREAS OF CORROSION. REMOVED -3 FRAME WHICH WAS CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CANTED FRAME CLIP, SPLICE AND DOUBLER IAW REO G09664 AND DAC DWG 5646444. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED -3 FRAME, CLIP, SPLICE AND DOUBLER AND -36 PNL IAW REO G09664 AND DAC DWG 5646 444.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, AFT PIT STA 1540 L27L CORROSION ON UNDERSIDE OF FLANGE. REMOVED FITTING IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED NEW FITTING AND DRILLED EXISTING HOLES IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, AFT PIT STA 1140 L35L SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED NEW FITTING AND DRILLED EXISTING FASTENER HOLES IAW DC8 SRM 51-3-2 AND 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, STA 900 RT CUSP AREA WEB HAS SIGNS OF CORROSION. FOUND FINGER DOUBLER & WEB OUT OF LIMITS; CORROSION ON FLOORBEAM FS 879 FOUND DURING CORROSION REMOVAL. CUTOUT -3 WEB; REMOVED CORROSION ON FLOORBEAM (IN LIMITS); DYE PEN PANEL (NO CRACKS); FABBED 2EA FINGER DOUBLERS, 2EA INTERNAL SPLICES, 1EA F ILLER, 1EA EXT DOUBLER FOR WEB REPAIR. ALODINED & PRIMED; INSTALLED REPAIR; ALL IAW REO G09650, SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21, DWG 5645332, ASTM 1417.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, AFT PIT STA 1260-1280 LONG 36 SPLICE CORROSION CENTER OF SPLICE PLATE. REMOVED SPLICE PLATE IAW DC8 SRM 51-3-0 AND 51-1-20D. RECEIVED NEW FITTING SPLICE P/N 3759222-1N PO 0, LOCATED AND DRILLED IAW DC8 SRM 51-3-0 AND 51-1-20D. INSTALLED FITTING SPLICE IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, SEAT TRACK CRACKED AT STA 145. BLENDED CRACKED SEAT TRACK IAW DC8 SRM 53-2-3, OUT OF LIMITS IAW DC8 SRM 53-2-3 AND 53-2-0. REMOVED DAMAGED SEAT TRACK IAW DC8 SRM 51-3-0 & 51- 3-1. LOCATED, DRILLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 53-2-3. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK SPLICE IAW DC8 SRM 51-3-0 & 51-3-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, UPPER CARGO BETWEEN STA 1000-1020 AT LONG 13L SHEAR TIE IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. FABRICATED NEW SHEAR TIE IAW DC8 SRM 53-4-1 FIG 51 AND 51-1-24. HEAT TREAT TO 7075-T6 .080 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — MISREPAIRED (L1 DOOR) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, L1 DOOR UPPER FWD CORNER REPAIR IS NOT PER SRM. REMOVED EXISTING DOUBLERS ABOVE L1 DOOR UPPER FWD CORNER IAW DC8 SRM 51-1-21. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182 AND DC8 SRM 51-1-20D.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, R2 DOOR UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER AND L1 1R, FOUND BY RADIOGRAPHY. FAB DOUBLERS & FILLERS -19, -21, -23, & -25 IAW DC8 SRM 53-2-0. TRIMMED EXTERIOR SKIN AND INTERNAL DOUBLER IAW DC8 SRM 53-2-0 TR 130. REMOVED DAMAGED L 11RT STA 1570-1700. RECEIVED, LOCATED, & DRILLED NEW LONGERON P/N 377351 2-1, INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21. ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-0 TR130, TR183 AND REO G09643.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, SHEARED RIVET HEAD, BULGE & CORRODED SHEAR WEB ABOVE & BELOW L21R CUSP MAIN CABIN COURIER AREA FS 25. REMOVED FRAME FITTING AND FLOOR SUPPORTS TO FOM, REMOVED CUSP ANGLES AND FABRICATED NEW ANGLE IAW DC8 SRM 53-3-3 AND DAC DWG 5888479. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP ANGLES, FRAME FITTING AND FLOOR SUPPORTS IAW DC8 SRM 51-1-20D, 51-3-0.

Part: SKIN — NICKED (LT WING) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27.

Part: FITTING — GOUGED (C1 DOOR) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, FWD PIT CROSS-SLIDE DOOR T-BOLT FITTINGS GOUGED 6 EACH. BLENDED OUT LATCH FITTING IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DAC DWG 3754051. RECEIVED, LOCATED, & DRILLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-24 AND 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 78,668 hrs · 24,999 cycles

INSPECTION TYPE: C1, RIGHT MLG WW L24R AT STA 879 VERT BATHTUB FITTING HAS CORROSION ON FWD SIDE. REMOVED CORROSION & FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53 -2-0 FIG 1F. REMOVED FITTING, FABRICATED REPAIR SPLICES AND INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0 FIG 8.

Part: WIRE — LOOSE (BATTERY PACK)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS NOT PERATING PROPERLY. RESET CONNECTOR ON EMERGENCY LIGHT BATTERY PACK, OPS CK NORMAL.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY)

INSPECTION TYPE:N/A CARGO SMOKE WARNING INDI FOR POS NR 6, NO EMERGENCY DECLARED, NO ODOR OR VISUAL SMOKE. REMOVED AND REPLACED NR 6 SMOKE DETECTOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE: PFLT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. OPS CKS GOOD, OK FOR SERVICE.

Part: WIRE HARNESS — CHAFED (FIRE WARNING)

NUMEROUS INTERMITTENT FIRE WARNING ON NR 4 ENGINE INFLIGHT. PERFORMED ENG FIRE SEVERE DAMAGE CHECKLIST AND SECURED ENGINE. RECEIVED BOTH LIGHT AND FIRE BELL. INSPECTED FIRE WARNING HARNESS AND FOUND RT CORE CHAFED. REPAIRED WIRE PER EOM-2000-16032-A, GROUND RAN ENG AND OPS CHECK GOOD. FIRE WARNING CHECKS GOOD PER MM 26-10-00.

Part: CONNECTOR — LOOSE (FIRE LOOP)

NR 4 ENGINE FIRE WARNING SOUNDED INTERMITTENTLY (QUICK ON AND OFF) 3 TIMES. DID NOT SHUT ENGINE DOWN DUE TO WEATHER AND SHORT FINAL TESTED AND TESTED CIRCUITS TESTED GOOD, ENGINE ANTI-ICE ON WITH MODERATE PRECIPITATION. ACCOMPLISHED T/S PER M/M 26-10-00 PAR A, NO DEFECTS NOTED. VISUALLY INSPECTED ALL ENG FIRE LOOPS, FOUND CONNECTOR P1-7008 LOOSE. CLEANED A RESECURED CONNECTOR, REPLACED NR 4 FIRE CONTROL UNIT PRECAUTIONARY SYS, OPS NORMAL REF 26-10-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK PER UPS MM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS BATTERY LOW (LIGHTS WILL NOT STAY ON) 5 SEC MAX. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 LT LONG ATTACH FITTING HAS CORROSION. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING AND REPAIR IAW DC8 SRM 53-2-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT PIT FS 1152 FITTING AT L31R L33R IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW BANANA FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT PIT FS 1152 FITTING AT L31R - L33R IS CRACKED. REMOVED CRACKED BANANA FITTING AND INSTALLED NEW BANANA FITTING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C2, 3 FS 1240 L35L INTERCOSTAL ATTACH FITTING CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 BANANA FITTING STA 1160 CRACKED INSIDE TORQUE BOX LONG 33R.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 BANANA FITTING STA 1160 CRACKED INSIDE TORQUE BOX LONG 33R. PERFORMED HFEC IAW DOUGLAS IPM 06-10-01-001 AND FOUND CRACK. REMOVED CRACKED BANANA FITTING. INSTALLED FITTING SUPPORT ANGLES AND END FITTING IAW DC8 SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT LOWER CARGO FS 1240 L35R INTERCOSTAL ATTACH FITTING IS CRACKED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT LOWER CARGO FS 1060 FRAME CAP CORRODED AT L36. FABBED ANGLE AND INSTALLED REPAIR IAW DC8 SRM 51-1-16, 51-1-120D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C2, 3 AFT PIT FS 1050 L35L SPLICE FITTING CRACKED.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 MAIN CABIN AT STA 864 AND RBL 40 - 49 PULLEY BRACKET BASE PLATE HAS SHEARED RIVETS AND CORROSION ON MLG W/W CEILING AND SUBFLOOR AS SEEN FROM RT W/W. REPAIRED AREA IAW REO-G08475.

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT ACCY COMP EVIDENCE OF CORROSION BETWEEN INTERCOSTAL AND FUSELAGE SKIN AT FS 1600 L25R & L26R. REMOVED CORRODED AREA SKIN IAW DC8 SRM 53-2-1. FABBED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT CARGO PIT FS 1160 BETWEEN LONG 34R 33R Z-FITTING IS CORRODED. REMOVED CORRODED IAW DC8 SRM 51-1-20D, AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT CARGO PIT AT FS 1040-1060 L31L SPLICE FITTING IS CRACKED AT AFT O/B END. R&R FITTINGS IAW DC8 SRM 51-1-20D, 51-1-11.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT LWR CARGO CRACKED ATTACH FITTING L33R STA 1230. REMOVED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-24 & 51-1-20D.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 MAIN CABIN AT STA 922 & RBL 67 SUBFLOOR PANEL FITTING HAS CRACK AND CORROSION. REPAIRED AREA IAW REO G08477.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT PIT Z-ANGLE CRACKED AT FS 1180 L28L. REMOVED CRACKED Z-ANGLE, INSTALLED NEW FITTING P/N 3755842-505N IAW DC8 SRM 51-1-20D.

Part: STRINGER — CRACKED (WING) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 LW LWR SKIN AT XRS 453, STRINGER 64 IS CRACKED. FABBED AND INSTALLED FILLER IAW EO DC8-5730-9004. FABBED AND INSTALLED DOUBLER IAW EO DC8-57 30-9004.

Part: PANEL — WORN (T/E FLAP) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 LT WING TO BODY FAIRING AREA FLAP T/E PANEL LWR SURFACE OF PANEL IS WORN AND HARDWARE IS NOT SECURE. REMOVED DAMAGED PANEL IAW DC8 SRM 51-3-0, PANEL DAMAGED BEYOND REPAIR. FABRICATED NEW 5643117-5 PANEL IAW DAC DWG 5643117 AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-0.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT PIT ANGLE CORRODED AT FS 1160 AT L27L. R&R ANGLE IAW DC8 SRM 51-1-20D.

Part: PANEL — WORN (T/E FLAP) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 LT WING TO BODY FAIRING AREA FLAP TE PANEL LWR SURFACE OF PANEL IS WORN AND HARDWARE IS NOT SECURE. REMOVED DAMAGED PANEL IAW DC8 SRM 51-3-0, PANEL DAMAGED BEYOND REPAIR, FABRICATED NEW 5 643117-5 PANEL IAW DAC DWG 5643117 AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-0.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 AFT PIT ANGLE CORRODED AT FS 1160 BETWEEN L31L L35R. REMOVED ANGLE, REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED ANGLE IAW DC8 SRM 51-1-20D.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 KEEL BEAM FIG LT NR 5 FIG AT STA 839 CRACKED IN I/B CORNER. R&R FITTING IAW DC8 SRM 51-1-20D 51-3-0.

Part: SKIN — CRACKED (LT WING) · airframe 77,559 hrs · 24,183 cycles

INSPECTION TYPE:C23 LW APPROX XFS 880 L/E CRACKED. CUT OUT CRACKED AREA IAW DC8 SRM 57-2-1. INSTALLED DOUBLER & FILLER IAW DC8 SRM 51-1-21 & 51-1-15.

Part: SKIN — CORRODED (RIGHT WING) · airframe 77,507 hrs · 24,143 cycles

INSPECTION TYPE: SP, RIGHT WING UPPER SKIN BLENDOUT IS BEYOND LIMITS AT ACCESS PANEL 505B AT APPROX. STA. XRS489 AT STRINGER 7. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 36

Part: MICROPHONE — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A PREFLIGHT- FE O2 MIC INOP. *S/D* FOUND WIRE AT CONNECTOR R50-299 BROKEN. REPAIRED, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT DISARM DOES NOT WORK. RELAMPED EMERGENCY LIGHT SOCKET.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT BATTERY PACK PER MM 33-50-01

Part: LINK — BROKEN (NR 1 SPOILER)

INSPECTION TYPE:N/A, LEFT NR 1 SPOILER HAD 2 BROKEN LINKS. *S/D* REMOVED AND REPLACED BOTH NR 1 GROUND SPOILER PANEL CRANKS IAW 27-61-01. PERFORMED INSP/CHECK OF SPOILER ACT SYSTEM IAW 27-61-01, OPS CHECK NORMAL.

Part: LONGERON — CORRODED (BS 1766)

INSPECTION TYPE:C1 LONGERON 32R, FWD OF FS 1766 IS CORRODED OUT OF LIMITS UNDER THE SPLICE FITTING. CUT OUT DAMAGED SECTION OF THE LONGERON AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C1 FS 1230 FRAME ATTACH FITTING AT LONGERON 35L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: BULKHEAD CHORD — CRACKED (BS 70)

INSPECTION TYPE:C1 ACCOMPLISH APPENDIX C OF EO DC8-5310-10158-A, FS 70 BLKHD LWR CHORD AT LONGERON 33L IS CRACKED AND CORRODED. REPAIRED FS 70 BLKHD LWR CHORD AT LONGERON 33L IAW EO DC8-5310-10158-A APPX C.

Part: SKIN — CORRODED (BS 660&710)

INSPECTION TYPE:C1, FUSELAGE SKIN AT FS 660 AND 710 WERE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SKIN AND INSTALLED REPLACEMENT SECTION BETWEEN FS 610, FS 780, LONG 31L TO 31R IAW DH SK814-107.

Part: ANGLE — CRACKED (WS 522.168)

INSPECTION TYPE:C1 RT WING L/E OTBD VERTICAL ANGLE AT XS 522.168 IS CRACKED PAST THE STOP DRILL. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-3-0.

Part: TEE CHORD — CRACKED (WS 520.168)

INSPECTION TYPE:C1 RT WING L/E AT XS 520.168, THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. STOP DRILLED THE CRACK AND REPAIRED THE TEE CHORD IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1280)

INSPECTION TYPE:C1 INTERCOSTAL TO FRAME FITTING CRACKED, FWD SIDE FS 1280 AT LONGERON 33R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: DOUBLER — CORRODED (BS 879)

INSPECTION TYPE:C1 SHEARED FASTENERS AND CORROSION UNDER THE FINGER DOUBLER AT FS 879 TO FS 902, BL 0. REMOVED THE FINGER DOUBLER, REMOVED LIGHT CORROSION FROM WEB IAW SRM 51-1-8, WEB WITHIN LIMITS IAW SRM 53-2-0 FIG 1F. FABRICATED REPLACEMENT FINGER DOUBLER IAW DWG 5645332 AND REPLACED THE FINGER DOUBER IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 470)

INSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 470 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 390)

INSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 390 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (BS 187)

INSPECTION TYPE:C1, THE FUSELAGE SKIN AT FS 187, JUST ABOVE THE CUSP AT THE FWD SERVICE DOOR AFT LWR CORNER WAS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14.

Part: SKIN — CRACKED (SERVICE DOORWAY)

INSPECTION TYPE:C1, THE FUSELAGE SKIN AT THE FWD UPPER CORNER OF THE FWD SERVICE DOOR WAS CRACKED. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14.

Part: SPLICE — CORRODED (BS 1766)

INSPECTION TYPE:C1 LONGERON 32R END FITTING, FWD SIDE OF THE FS 1766 FRAME IS HEAVILY CORRODED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: JAMB — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C1, THE D-PIT DOOR JAMB WEB WAS CRACKED AND CORRODED AT SEVERAL FASTENER HOLES ACROSS THE BOTTOM. CUT OUT THE DAMAGED AREA, FABRICATED REPLACEMENT PARTS, INSTALLED REPLACEMENT PARTS IAW DWG 5641013 AND SRM 51-1-21A.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:C1 HEAVY CORROSION ON LONGERON END FITTING, FWD SIDE OF FS 1690 AT LONGERON 22R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 448.581)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (FUSELAGE)

INSPECTION TYPE:C1 MODERATE CORROSION ON THE LONGERON 18L INTERCOSTAL TO FRAME 822 ATTACH FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C1 LONGERON 32R END FITTING AT FS 1690 IS HEAVILY CORRODED AND CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21 AND 51-1-20D AND 51-3-0.

Part: SKIN — GOUGED (WS 246.6)

INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XS 246.6 IS GOUGED AND CORRODED AT THE FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW EO DC8-5720-7767-A.

Part: SKIN — CRACKED (WS 735)

INSPECTION TYPE:C1 L/H WING L/E UPPER SKIN CRACKED AT STA. XFS735.00. REPAIRED AREA I.A.W. SRM 57-2-1 FIG.38.

Part: FRAME — CRACKED (BS 220)

INSPECTION TYPE:C1 FUSELAGE FRAME AT FS 220, JUST ABOVE LONGERON 21R IS CRACKED AT A FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 1F.

Part: SKIN — CRACKED (WS 210.29)

INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 210, 29 FWD OF THE SPAR IS CRACKED. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767.

Part: SKIN — CRACKED (WS 610)

INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 610.0, 2 FWD OF THE SPAR IS CRACKED. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767.

Part: FITTING — CRACKED (BS 1160-1180)

INSPECTION TYPE:C1 CUSP FITTING CRACKED INSIDE RT TORQUE BOX BETWEEN FS 1160 AND 1180. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1, LT WING LWR L/E SKIN AT EXTERNAL DOUBLER ABOVE THE NR 2 PYLON WERE CRACKED. REMOVED CRACKED EXTERNAL DOUBLER, NDT VERIFIED SKIN CRACK WAS TERMINATED BY THE EXISTING STOP DRILL. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 57-2-1A FIG 1.

Part: SKIN — CRACKED (WS 257.75)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XW 257.75, JUST AFT OF THE L/E IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 2H.

Part: SKIN — CRACKED (WS 761.5)

INSPECTION TYPE:C1 RT WING L/E SKIN, AT THE L/E, AT XW 761.5, HAS MODERATE INTERGRANNULAR CORROSION AND IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-0 FIG 2H.

Part: SKIN — CRACKED (LT TE FLAP)

INSPECTION TYPE:C1 LT INBD FLAP OTBD T/E WEDGE SKIN IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FLAP WEDGE SKIN IAW DWG 5642960 AND SRM 51-1-21 AND 51-1-21A.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1, LT WING L/E UPPER SKIN BETWEEN XFS 703.75 AND 710 WAS CRACKED. STOP DRILLED THE CRACKS AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38.

Part: SKIN — CORRODED (WS 766.25)

INSPECTION TYPE:C1, LEFT WING L/E UPPER SKIN AT XFS 766.25 & 785.0 WAS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW DH SK814-312.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C1 FUSELAGE FRAME AT FS 55 AT LONGERON 24L IS CRACKED AT THE ATTACH ROD. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C1, FUSELAGE FRAME AT FS 55 WAS CRACKED AT THE ATTACH ROD AT LONG 24R. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, DURING BISE CHECK THE EMERGENCY EXIT LIGHT DO NOT ILLUMINATE. REMOVED AND REPLACED EMER EXIT LIGHTS BATTERY, OPS CHECK NORMAL.

Part: FLOORBEAM — DAMAGED (BS 1680)

INSPECTION TYPE-A, FLOORBEAM MOUNT HOLES ELONGATED AT STA 1680 AT LT O/B SEAT TRACK. THIS ITEM ACCOMPLISHED ON N/R CARD 544810.

Part: STRINGER — CORRODED (BS 1660-1667)

INSPECTION TYPE-A, STRINGER 24L HAS EXTENSIVE CORROSION FROM STA 1660 TO STA 1667. ITEM ACCOMPLISHED ON N/R CARD 544808.

Part: FRAME — CORRODED (BS 1667)

INSPECTION TYPE:A L/H CIRCUMFERENTIAL FRAME @ STA 1667 FROM STR 21 TO STR 23 HAS SEVER AL POPPED FASTENERS AND EXTENSIVE CORROSION. REMOVED LOWER SECTION OF CIR FRAME. THIS ITEM ACCOMPLISHED ON N/R CARD 544806.

Part: FLOORBEAM — DAMAGED (BS 1680)

INSPECTION TYPE:N/A, FLOORBEAM AT FS 1680 HAS ELONGATED HOLES FOR CENTER FASTENER OF SEAT TRACK AFT END. CLEANED UP HOLES TO .5 PER EO DC8-5310-11039-A.

Part: STRINGER — CORRODED (BS 1667)

INSPECTION TYPE:N/A, STR 24 AT STA 1667 HEAVLY CORRODED. REMOVED SECTION OF STRINGER SPLICED IN NEW SECTION PER 53-2-2.

Part: FLOORBEAM — CRACKED (BS 1680)

INSPECTION TYPE:A/CK, CRACK AT FLOORBEAM AFT OF SERVICE DOOR. UPON FURTHER INVESTIGATION FOUND CRACK AT CIRCUMFERENTIAL FRAME AT STA 1680 STR 21 NOT AT FLOORBEAM AS FIRST REPORTED. *S/D* REMOVED DAMAGED SECTION OF FRAME, FABED SPLICES AND INSTALLED REPAIR PER SRM 51-1-20 AND PER DOUGLAS DRAWING PLSRO8530008.

Part: FLOORBEAM — CORRODED (BS 1667)

INSPECTION TYPE:A/CK, CORROSION FOUND AT THE FLOORBEAM BY THE LT SERVICE DOOR. UPON FURTHER INVESTIGATION THE LT CIRCUMFERENTIAL FRAME AT STA 1667 FROM STR 21 TO STR 23 TO HAVE EXTENSIVE CORRISION. *S/D* REMOVED LOWER SECTION OF FRAME, FABED SPLICES AND INSTALLED PARTS PER SRM 53-02-00.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, MAIN ENTRY DOOR EMERG LIGHTS INOP. RELAMPED EMER LIGHTS, OPS CHECK GOOD.

Part: SKIN — CORRODED (BS 50)

CORROSION ON FUSELAGE BELLY APPROX STA 50, CORROSION ON CIRCUM. STA 70, CRACK ON CIRCUM STA 70 STRINGER 34. REPLACED BELLY SKIN TEMP. REPAIR ACCOMPLISHED ON CIRCUM FRAME IAW E/O DC8531010158A.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING INBD SLOT, OTBD CLOSE OUT RIB DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER PER DWG 5769859 AND SRM 57-3-1 FIG 6.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.760.00, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (COCKPIT)

INSPECTION TYPE-C, 2ND O/B FWD SEAT TRACK HAS CORROSION AROUND THE MOUNT FASTENERS. REMOVED AND REPLACED THE 2ND O/B FWD SEAT TRACK PER SRM 51-3-0.

Part: SKIN — CORRODED (WS 737)

INSPECTION TYPE-C, LT WING TIP JUST AFT OF FWD NAV LIGHT HAS SKIN CORROSION BEYOND LIMITS. REPAIRED AREA IAW SRM 57-2-1 FIG 2M.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE-C, FUSELAGE STA 1220, AT LONG 34R, THE BACK-UP FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 53-2-0 FIG 2G.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 660)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.660.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 735)

INSPECTION TYPE-C, RT WING LWR L/E RIB IS CRACKED AT THE AFT END AT STA XFS.735.000. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 766.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS766.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 603.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 822)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.822.800, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 597.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS597.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 603.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS797.500, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 672.5)

INSPECTION TYPE-C, RT WING L/E UPPER RIB IS CRACKED AT THE AFT END AT STA XFS672.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 876.)

INSPECTION TYPE-C, RT WING L/E AT STA XFS876.00, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 747.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS747.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 484.895)

INSPECTION TYPE-C, RT WING L/E AT STA XS484.895, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-C, RT WING L/E AT STA XFS810.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 622)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.622.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 741.250)

INSPECTION TYPE-C, RT WING L/E RIB UPPER ARM IS CRACKED AT THE AFT END AT STA XFS741, 250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 776)

INSPECTION TYPE-C, RT WING L/E STA XFS776.00, THE LWR L/E RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 610)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.610.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-C, RT WING L/E AT STA XFS635.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 822.8)

INSPECTION TYPE-C, RT WING L/E AT STA XFS822.800, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 450)

INSPECTION TYPE-C, FS 450 AT LONG 36 THE LONG SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 450)

INSPECTION TYPE-C, LONG SPLICE FITTING AT STA 450 AT LONG 32R IS CRACKED. REMOVED AND REPLACED THE LONG SPLICE FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING L/E SKIN ON BOTTOM, ABOVE THE NR 3 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED A NEW REPAIR DOUBLER PER SRM 51-1-20D AND 57-2-0.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 616.250 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (BS 960)

INSPECTION TYPE-C, FS 960 ABOVE LONG 24R THE FITTING IS CORRODED. REMOVED AND REPLACED FITTING PER DWG 3647117 AND SRM 51-1-20D, 51-1-3, 53-2-0 FIG 8.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING I/B SLOT O/B Z-ANGLE CLOSE OUT RIB IS CRACKED. REMOVED AND REPLACED Z-ANGLE PER DWG 5769859 AND SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE-C, STA 1200 AT LONG 34R, THE BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841.

Part: SKIN — CORRODED (BS 450-610)

INSPECTION TYPE-C, FUSELAGE SKIN AT STA 450 TO 610 STR 33R-33L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DWG 5779913 AND SRM 51-1-20D.

Part: TRANSFORMER — FAILED (OVERHEAD PANEL)

INSPECTION TYPE-N/A, ON DESCENT TO ONTARIO NOTICED SPARKS AND SMOKE FOR A SHORT MOMENT IN OVERHEAD PANEL BEHIND THE FIRE HANDLES. FOUND RED OVERHEAD SWITCH PANEL INTRAL LIGHTS C/B OUT. NO FURTHER SMOKE WAS DEVELOPED. CONNECTOR DC 26F-10-6SW BURNT. REMOVED AND REPLACED TRANSFORMER (P/N 16434) (S/N 3551) ON, (S/N 478). INSTALLED NEW PLUG LTS, OPS GOOD.

Part: SKIN — CORROSION (LT WING LE)

INSPECTION TYPE: CS2. LEFT WING LEADING EDGE ASSY OVER NR 2 PYLON HAS 69 COUNTER SINK ATTACH FASTENER HOLES CORRODED. REPAIRED PER UPS EO.

Part: SUPPORT — CRACKED (FS 717)

INSPECTION TYPE-CS2 FLOOR BEAM SUPPORT CRACKED AT FS 717 UNDER SEAT TRACK NR 5. REPLACED SUPPORT ASSY PER SRM 51-1-20D.

Part: FLOOR BEAM — CRACKED (FS 8)

INSPECTION TYPE-CS2, WEBBING ON TOP OF FLOOR BEAM IS CRACKED FS 8, RBL 1. REPAIRED WEB PER SRM DC8-5350-7876.

Part: FITTING — CRACKED (FS 1690)

INSPECTION TYPE-CS2, FITTING CRACKED AT FS 1690 LONGERON 26L. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-21.

Part: LONGERON — CORROSION (BS 1765)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 28L FS 1765 OUTBOARD LEG. REPAIRED PER UPS EO.

Part: LONGERON — CRACKED (BS 1740)

INSPECTION TYPE CS2, LONGERON 5R CRACKED AT THE VERTICAL STAB FS 1740. REPAIRED PER UPS EO.

Part: FITTING — CRACKED (BS 1692)

INSPECTION TYPE-CS2, HEAVY CORROSION AND CRACKED FITTING AT FS 1692 LONGERON 28R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 1210)

INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON C-DOOR LOWER JAMB T-BOLT BACK UP FITTING FS 1210. REPLACED FITTING PER SRM 53-2-0, FIG 2D.

Part: RIBS — CRACKED (LT WING LE)

INSPECTION TYPE CS2, 4 RIBS CRACKED LT WING LEADING EDGE AT WS XFS780, XFS800, XFS740 AND XFS 710. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: DOUBLER — CORROSION (BS 1470)

INSPECTION TYPE-CS2, HEAVY CORROSION DAMAGE AT 2 SEAT TRACK SPLICE DOUBLERS FS 1470 LBL 33 AND FS 1500 TO 1520, BL 0. REPLACED DOUBLERS PER SRM 53-2-3.

Part: WEB — CORROSION (BS 8-20)

INSPECTION TYPE-CS2, HEAVY CORROSION ON COCKPIT SUBFLOOR WEB UPPER HORIZONTAL SURFACE FS 20 TO 8 LONGERON 22L. REPAIRED PER UPS EO.

Part: LONGERON — CORROSION (BS 1706)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 26R, FS 1706. REPAIRED PER UPS EO.

Part: PANEL — DELAMINATED (RT NR 4 SPOILER)

INSPECTION TYPE-CS2, RIGHT HAND WING NR 4 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER MM 27-61-01.

Part: RIBS — CRACKED (LT WING LE)

INSPECTION TYPE CS2, 4 RIBS CRACKED AT LT WING LEADING EDGE WS XFS 623, XFS 633, XFS 648 AND XFS 653. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: SPAR WEB — CRACKED (RT HORIZ STAB)

INSPECTION TYPE CS2, RT HORIZONTAL STAB CLOSING REAR SPAR WEB HAS CRACKED HOLE AT STA XE 142. REPAIRED PER UPS EO.

Part: BULKHEAD FRAME — CRACKED (BS 980)

INSPECTION TYPE: CS2. HEAVY CORROSION ON BULKHEAD FRAME FS 980 LONGERON 25R, AND A 3 INCH LONG CRACK BETWEEN LONGERONS 23R-24R. REPAIRED PER UPS EO.

Part: SPAR — CRACKED (LT HOR STAB)

INSPECTION TYPE: CS2. LEFT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AROUND FASTENER HOLD STA XE119.52. REPAIRED PER UPS EO.

Part: FITTING — CRACKED (BS 1640)

INSPECTION TYPE-CS2, CRACKED FLOORBEAM ATTACH FITTING FS 1640 LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (WS 69.5)

INSPECTION TYPE-CS2, LT WING UPPER SKIN HAS A 3.25 INCH LONG CRACK AT STA 69.5 REAR SPAR. REPAIRED SKIN PER SRM 57-2-1, FIG 20.

Part: TRACK — CORROSION (LT TE FLAP)

INSPECTION TYPE-CS2, LT WING STA 3 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.

Part: TRACK — CORROSION (LT TE FLAP)

INSPECTION TYPE-CS2, LT WING STA 219 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.

Part: ANGLE — CRACKED (NR 4 PYLON)

INSPECTION TYPE-CS2, NR 4 PYLON DRAG ANGLE CRACKED .25 INCH LONG PAST STOP DRILL. REPAIRED ANGLE PER TASK CARD 8040-01, STEP 4.

Part: RIBS — CRACKED (RT WING LE)

INSPECTION TYPE CS2, THREE RIBS CRACKED AT RT WING LEADING EDGE ST XFS 304, XFS 310 AND XFS 341. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: TRACK — CORROSION (LT TE FLAP)

INSPECTION TYPE-CS2, LT WING STA 98 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.

Part: RIBS — CRACKED (LT WING LE)

INSPECTION TYPE CS2, LT WING LEADING EDGE ASSY 1 EA RIBS CRACKED AT WS XFS 580, XFS 620, 4 EA RIBS CRACKED AT WS XFS 766, 3 EA RIBS CRACKED AT WS XFS 800 AND 2 EA RIBS CRACKED AT WS XFS 820. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: TRACK — CORROSION (LT TE FLAP)

INSPECTION TYPE-CS2, LT WING FLAP STA 410 TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.

Part: TRACK — CORROSION (BS 1342)

INSPECTION TYPE CS2, NR 3 SEAT TRACK AT FS 1342 HAS MODERATE CORROSION. REPAIRED SEAT TRACK PER SRM 53-2-3.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE CS2, FITTING CRACKED ON FWD SIDE OF FS 857 AT LONGERON 18R. REPLACED FITTING PER SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FS 1100)

INSPECTION TYPE-CS2, SHEAR TIE CRACKED AT HOLE, FS 1100 LONGERON 11L. REPLACED SHEAR TIE SECTION PER SRM 51-1-20D.

Part: FITTING — CRACKED (AFT SERV DOOR)

INSPECTION TYPE-CS2, AFT SERVICE DOOR FITTING CRACKED INSIDE SECOND LIGHTENING HOLE FROM TOP ON FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.

Part: TRACK — CORROSION (RT TE FLAP)

INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON RT WING STA 219 FLAP TRACKS. REPLACED TRACKS PER MM 27-51-03.

Part: TAB — DELAMINATED (LT AILERON)

INSPECTION TYPE-CS2, LT AILERON GEAR TAB DELAMINATED. REPLACED TAB ASSY PER MM 27-13-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS ARE DIM DURING PREFLIGHT. CLEANED BATTERY PACK CONNECTION, CHANGED BATTERY PACK, OPERATIONAL TEST NORMAL.

Part: RELEASE PIN — DIRTY (LT MLG DOOR)

CREW REPORTED LOUD NOISE IN NOSE HEARD UPON GEAR RETRACTION. NOISE STOPPED WHEN GEAR EXTENDED. AIR TURN BACK. FOUND FWD LT DOOR LINK-RELEASED PIN DIRTY AND HALF HUNG UP. CLEANED AND LUBED LT DOOR LINK, OPS CK OK.

Part: ANGLE — CRACKED (VERT STAB)

WHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON RT VERT STAB TO FUSELAGE ATTACH ANGLE. INSTALLED REPAIR PER SRM 53-2-5.

Part: SKIN — DELAMINATED (NR 5 VANE ASSY)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON UPPER SURFACE NR 5 VANE. REPLACED VANE ASSY PER MM 27-51-14.

Part: FRAME — CORRODED (FS 200)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME AT FS 200, LONGERON 29R. REPAIRED FRAME PER SRM 53-2-3.

Part: DOOR TRACK — CRACKED (FS 1160)

DURING 'C' CHECK, MAINTENANCE FOUND FWD DOOR TRACK CRACKED AT FS 1160, LONGERONS 24R AND 29R. REPAIRED TRACKS PER UPS EO DC8-53-1351.

Part: FITTINGS — CORRODED (FS 1200)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1200 BETWEEN LONGERON 33-34R AND 33-34L. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D.

Part: SKIN — DELAMINATED (NR 3 VANE ASSY)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 3 VANE. REPLACED VANE ASSY PER MM 27-51-14.

Part: FITTING — CORRODED (BS 1400)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME END FITTING AT FS 1400, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: FRAME — CRACKED (RT MLG WW)

DURING 'C' CHECK, MAINTENANCE FOUND RT WHEELWELL DOOR CUTOUT FRAME CRACKED ON FWD I/B CORNER. REPAIRED FRAME PER SRM 57-2-0.

Part: FITTINGS — CORRODED (FS 1180/1220)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1180, LONGERON 33-34R AND FS 1220, LONGERON 33R. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D.

Part: SKIN — CRACKED (WS 703)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING LEADING EDGE LOWER SURFACE ATTACH HOLE SKIN CRACKED AT STA XFS 703. REPAIRED SKIN PER SRM 57-2-0.

Part: LONGERON — CORRODED (FS 395-415)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON LONGERON 21L AT FS 395-415. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5.

Part: FITTING — CORRODED (FS 1060)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTING AT FS 1060, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D.

Part: FRAME — CORRODED (FS 1320)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT FS 1320, LONGERONS 34-35R. REPAIRED FRAME PER SRM 53-2-0.

Part: SKIN — DELAMINATED (NR 2 VANE ASSY)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 2 VANE. REPLACED VANE ASSY PER MM 27-51-14.

Part: SKIN — CRACKED (BS 70)

DURING 'C' CHECK, MAINTENANCE FOUND CRACK IN FWD JACK POINT AT STA 70, LOWER BELLY SKIN. REPLACED SKIN PER UPS EO DC8-5330-6471.

Part: SKIN — DELAMINATED (NR 2 SPOILER)

DURING 'C' CHECK, MAINTENANCE FOUND LT WING NR 2 SPOILER DELAMINATED TOP AND BOTTOM SIDES AT I/B TRAILING EDGE. REPLACED SPOILER PANEL PER MM 27-61-1.

Part: PANEL — CORRODED (RT PANEL 519A)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT WING LEADING EDGE LOWER SURFACE PANEL 519A. REPLACED PANEL PER DRAWING NR 3646959.

Part: FITTINGS — CORROSION (FS 902, 940)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON 2 EA VERTICAL FLOOR BEAM STIFFENER FITTINGS AT FS 902 AND 940, BL 0. REPLACED FITTINGS PER SRM 51-1-20D.

Part: SKIN — CORRODED (RT XFS 29.6-33.3)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION BULGE AROUND RT AUX TANK UPPER ATTACH ANGLE SCREW ON SKIN AT STA XFS 29.6-33.35. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-57-0542.

Part: DOUBLER — CORRODED (FS 902-920)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER DOUBLER AT FS 902-920, BL 0, AT UPPER MAIN GEAR WHEELWELL PRESSURE DECK SURFACE. REPLACED DOUBLER PER SRM 51-1-21.

Part: LONGERON — CRACKED (FS 100)

DURING A WALKAROUND, MAINTENANCE REPORTED CRACK IN LOWER SIDE WITH 1 EACH POPPED FASTENER HEAD (RIVET). CRACK IS OPEN WITH VISIBLE CORROSION.