N851UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK IAW MM 33-50-01-2.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01-2. OPS CHECKS NORMAL.

Part: SLIDE — OUT OF POSITION (COCKPIT)

ESCAPE SLIDE ON CAPTAIN'S SIDE FELL OUT. 10-8-07 REINSTALLED CAPTAIN'S ESCAPE TAPE (ROPE) AND LINING IAW DC8 MM 25-61-13-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 CRACKED END FITTING AT STA 1240 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1240 L35R IAW SRM 51-1-20D AND SRM 51-3-2.

Part: WEB — CRACKED (RUDDER) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 RUDDER HAS 1.5 INCH CRACK IN LWR STRUCTURE JUST AFT OF TORQUE TUBE MOUNTING. REMOVED CRACKED WEB ON RUDDER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR WEB ON RUDDER STA ZR 59.54 IAW SRM 51-03-00-0, AND DWG 5701251.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON LWR FLANGE OF FRAME AT STA 1240 L35R. CUT OUT CORRODED AREA OF LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995. REPAIRED LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995, UPS RAA DC8-53-20650, AND FAA FORM 8100-9.

Part: LONGERON — CORRODED (FS 1220-1260) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 L-35R CORRODED FROM STA 1220-1260 ON INBD LONGERON. REMOVED AND REPLACED LONGERON AND BATHTUB FITTINGS FROM STA 1210 TO 12 0 IAW SRM 53-2-0 AND DWG 5750322.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 L-31R END FITTING CRACKED AT STA 1690. REMOVED AND REPLACED LONGERON END FITTING AT STA 1690 L31R IAW SRM 51-1-21, AND SRM 51-3-0.

Part: WEB — PUNCTURED (FS 70 L21L) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE: C2 WEB PUNCTURED AT STA 70 L21L. CUT OUT DAMAGED AREA ON WEB AT STA 70 L21L IAW SRM 53-02-00-0 FIG1F FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 70 L21L IAW SRM 53-03 -03-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 24 CRACKED AND CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 5 3-2-0, 51-02-00 FIG 1, 51-1-8, 51-1-20D, AND DWG 2759472.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 L36 SPLICE BETWEEN STA 1260 AND 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SAA EA 008-5310-01-A0987.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 LEFT ELEVATOR UPPER SKIN INBOARD OIL CANNED. REMOVED, FABRICATED, AND INSTALLED ELEVATOR SKIN IAW SRM 51-1-21, 55-0 2-01, 51-1-8 AND 51-1-21A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 C-PIT STA 1240-1260 BETWEEN L36 AND L34R INTERNAL DOUBLER HAS CORROSION AND EXTENDS UNDER L35R. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 1242 L35R IAW SAA EA 008-5330-01-A0985, UPS RAA DC8-53-20644, AD FAA FORM 8100-9.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 A-PIT STA 120 LBL 26 FLOORBEAM GOUGED AND FASTENER SHEARED. CUT OUT DAMAGED AREA ON FLOORBEAM AT STA 120 LBL 26 IAW SRM 51-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AT STA 120 LBL 26 IAW SRM 51-02-00 FIG 1, AND SRM 53-02-00 FIG 1F.

Part: ANGLE — CRACKED (FS 986 LBL 46) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE: C2 C-PIT FWD BULKHEAD STA 986 LBL 46, ANGLE CRACKED. STOP DRILLED CRACKED ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0 FIG 001B. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0, AND DWG 5704721

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 LEFT SIDE OF VERT STAB LWR ATTACH ANGLE CRACKED AT STA 1766. REPAIRED LEFT SIDE OF VERT STAB LWR ATTACH ANGLE AT STA 1766 IAW SRM 53-02-05-0 FIG 016A.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE CRACKED. REMOVED AND REPLACED RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE IAW SRM 51-3-0, 51-1-20D, SRM 51-3-2, AND DC8 AMM 55-10-00-2.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 RT HORIZ STAB MOVEABLE FAIRING 2ND AFT H-ANGLE UPPER, CRACKED. REMOVED CRACKED H-ANGLE ON RT HORIZ STAB MOVEABLE FAIRING IAW SRM 51-03-00-0. FABRICATED AND INSTALLED RT HORIZ STAB FAIRING ATTACH H-ANGLE IAW SRM 51-03-02, DWG 3702464, AND SRM 51-3-1.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 LT HORIZ STAB UPPER MOVEABLE FAIRING MOST AFT H-ANGLE CRACKED. REMOVED AND REPLACED LT HORIZ STAB MOVEABLE FAIRING AFT H-ANGLE IAW SRM 51-03-00-0, DWG 3702464, AND SRM 51-03-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 STA 70 FRAME CRACKED AND CORRODED BETWEEN L31R AND L32R IN A/C COMPT. REPAIRED CRACKED AND CORRODED FRAME AT STA 70 BETWEEN L31R AND L32R IN A/C BAY IAW SRM 53-02-05 FIG 08C2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 CREASE ON UPPER FUSE SKIN AT STA 1800 L9L. CUT OUT DAMAGED AREA ON FUSE SKIN AT STA 1800 L9L IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER AT STA 1800 L9L IAW SRM 53-2-1 FIG 7, AND SRM 53-5-3 FIG 1 SHEET 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 FUSE SKIN CRACKED AND BULGING AT STA 1692 L28R. REPAIRED FUSELAGE EXTERIOR SKIN AT STA 1692 L28R IAW UPS EO DC8- 5330-20248-D APPX E AND SRM SRO8530032.

Part: DOUBLER — PUNCTURED (T/E FLAP) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 LEFT WING INBOARD FLAP STA 110 UPPER SURFACE SKIN DENT AND EXISTING DOUBLER PUNCTURED. REMOVED DAMAGED DOUBLER ON LEFT WING INBOARD FLAP STA 110 UPPER SURFACE IAW SRM 51-01-21-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT WING UPPER SURFACE STA 110 IAW EO DC8-5720-7767-A, AND SRM 57-07-01-01.

Part: SKIN — GOUGED (LWS 100) · airframe 76,588 hrs · 26,366 cycles

INSPECTION TYPE:C2 LH INBD UPPER SURFACE SKIN EXSISTING REPAIR DOUBLER HAS DEEP GOUGE AT STA 100 REMOVED DAMAGED DOUBLER AT L/WING STA 100 IAW SRM 51-01-21-0 FABRICATED AND INSTALLED REPAIR DOUBLER AT LH WING INBD UPPER SURFACE STA 100 IAW SRM 57-07-01-0 AND EO DC8-5720-7767-A

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A FWD PASSAGEWAY AND EMERGENCY LIGHT NEXT TO EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED PASSAGEWAY AND EMERGENCY LIGHT. LIGHT OPS GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

AFTER TAKEOFF, EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH EXCEPT TO DISARM EMERGENCY LIGHTS. FOUND C/B PULLED. RESET C/B AND PERFORMED EMERGENCY LIGHTS. OPS CHECK PER MM 33-50-01-2. EMERGENCY LIGHTS, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A DURING PDC, EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 AMM 33-50-01-2. CHECK SERVICEABLE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

COURIER EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD 33-31-01-2.

Part: FAN — ODOR (CABIN)

RECIRC FAN VERY LOUD (NOISY) WITH A SLIGHT ODOR. REMOVED AND REPLACED RECIRC FAN PER MM 21-21-01-2. OPS CKS NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

FOUND EMERGENCY LIGHT BATTERY PACK DEAD ON PRE-FLIGHT. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND SYSTEM CHECK SERVICEABLE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER AMM 33-50-01-2. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY BATTERY PACK NEEDS REPLACING. REPLACED BAT PACK EMERGENCY LIGHT. OPS NORMAL. OK TO CONTINUE.

Part: WIRE — OPEN (RT MLG)

N/A RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE DURING LANDING. GEAR WAS DOWN. T/S. FOUND WIRE FROM RT GEAR SWITCH TO TERMINAL BLOCK OPEN. REMOVED AND REPLACED WIRE IAW SWP 20-00-00. OPS CK IAW AMM 32-60-00-2 (E) STEPS 1 TO 6. OPS CK OK ALL 3 GREEN OK.

Part: WINDSHIELD — CRACKED (COCKPIT)

INSPECTION TYPE:N/A, F/O'S WINDSHIELD TOP EDGE GLOWING. WINDSHIELD CRACKED AT 17K FT. REMOVED AND REPLACED F/O WINDSHIELD W/REF TO MM 56-10-02-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, CORROSION ON FLOORBEAM AT STA 60 RBL 45. REMOVED DAMAGE ON UPPER TEE CAP OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW SAA SK 851-857217.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

STA 70 RBL 48 UNDER THE SEAT TRACK INTERCOSTAL HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-20D, 51-3-2 AND DWG 5890314.

Part: SKIN — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 RH WING UPPER AFT SKIN PANEL AT XCW 69.500 CRACKED 1 INCH LONG. CUT OUT DAMAGE,FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-02-01 FIG. 20.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, COCKPIT SUBFLOOR STA -32 TO -12 RBL 48 FINGER DOUBLER HAS SEVERAL SHEA R HEAD FASTENERS AND POSSIBLE CORROSION. REMOVED FINGER DOUBLER, CORROSION ON FINGER DOUBLER FOUND OUT OF LIMIT S, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DC-8 SRM 5 1-1-21 AND DWG SRO8530026.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, COCKPIT SUBFLOOR AT STA -32 TO -52 RBL 60 FINGER DOUBLER CORRODED. REMOVED FINGER DOUBLER, CORROSION FOUND OUT OF LIMITS, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5612298 AND DC-8 SRM 51- 1-20D AND 51-1-15.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, CRACKED FITTING APPROX 2 INCHES ON LONGERON 32R STA 1200 C-PIT ENTRY WAY. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: SPAR CAP — CRACKED · airframe 75,626 hrs · 25,638 cycles

LT AFT LWR WING SPAR CAP F/S 857 IS CRACKED IN THREE PLACES FROM LBL27-LBL45. REPAIRED LT LWR SPAR CAP IAW SRO DWG 8570009, SRM 51-1-20D, 51-1-24.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, STA 1756 L4R CRACKED .250 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, MAIN CARGO STA 860 LONGERON 19R FITTING CRACKED APPROX. 2 INCHES ON FWD SIDE OF FRAME. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 C-PIT DOOR LOWER AFT CORNER REPAIR DOUBLER IS NOT PER SRM 53-2-0 FIG 22 AND THERE IS A CRACK IN THE REPAIR FILLER. REMOVED EXISTING REPAIR, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 22.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, MAIN CABIN STA 900 LONGERON 9R FITTING CRACKED APROX 3.0 IN. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, MAIN CABIN INTERIOR LT SIDE F/S 900 LONG 6L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-120D.

Part: FITTING — CRACKED (FUSLEAGE) · airframe 75,626 hrs · 25,638 cycles

MAIN CABIN INTERIOR LT SIDE FS 860 AFT SIDE L18L ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, LT MAIN CABIN INTERIOR LONGERON 10L SPLICE FITTING CRACKED AT FS 860. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-20D.

Part: SPAR — CRACKED · airframe 75,626 hrs · 25,638 cycles

FS 855 AFT SIDE OF REAR SPAR LOWER CHORD UPPER SURFACE FROM RBL36.5 -45.00 HAS 8.5" CRACK. REPAIRED REAR SPAR IAW SRO 8570009.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

DURING X-RAY INSPECTION AND VERIFIED BY HFEC, A CRACK WAS FOUND ON ZEE FITTING, STA 340, BETWEEN LONG 30-31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, CRACKED APPROX .5 INCH ON LONG 15 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RH SIDEWALL. REMOVED DAMAGE SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR I AW DC-8 SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

C1 LONG 15L AT APPROX STA 1744 HAS A CRACK AT UPPER FRAME ATTACH POINT. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FUSELAEG) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, STA 1220 BETWEEN L27R-L26R SPIDER FITTING HAS A CRACK RUNNING FROM BOLT HOLE TO LOWER RIVET. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

C1 LONG 16 AT APPROX STA 1745 IS CRACKED AT LWR FRAME TO LONG ATTACH POINT AT RADIUS, (LT CANTED FRAME). REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, MAIN CABIN STA 900 LONGERON 3L FITTING CRACKED APPROX. 4 INCHES. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D AND 51-1-2 1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, CRACKED FITTING AT F/S 760 BETWEEN LONGERONS 17 AND 18L. REMOVED CRACKED FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 51- 1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

C1 CRACKED APPROX .5 ON LONG 14 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RT SIDE WALL. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

C1 LONG 14L AT APPROX STA 1743 IS CRACKED AT BOTH UPPER AND LOWER FRAME ATTACH POINTS. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC- 8 SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 RH WING L/E UPPER RIB CRACKED AT XFS 728. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-3-3 AND 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 671. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.

Part: RIB — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 734. STOP DRILL CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC -8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.

Part: RIB — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 721. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLE IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.

Part: SKIN — SCRATCHED (NR 2 STUBWING) · airframe 75,626 hrs · 25,638 cycles

C1 DEEP SCRATCHS IN SKIN L/W UPPER SPAR CAP IB CORNER OF NR 2 STUB WING. SCRATCHS FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 26.

Part: SKIN — CRACKED (NR 2 STUBWING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, LW NR 2 STUBWING UPPER OB CORNER HAS A CRACK IN SKIN. STOP DRILLED THREE CRACKS, FABRICATED, AND INSTALLED REPAIR IAW DC-8 S RM 57-2-0, 57-5-0, AND 57-2-1 FIG 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

C1 RT WING LE LWR SKIN CRACKED 1 INCH LONG AROUND FASTENER HOLE AT XW 257. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5720 -4087-B APPENDIX C.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, AFT PRESSURE BULKHEAD IS CRACKED 0.5 IN LONG AT LBL 35 AND 66 IN FROM FLOOR. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER IAW DC-8 SRM 53-2-5 FIG 14. THE -27 AND -25 DOUBLERS INSTALLED BY PREVIOUS REPAIR.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, AFT PRESSURE BULKHEAD CRACKED 1.75 IN LONG AT RBL 26 AND 66 IN FROM FLOOR. CUT OUT DAMAGE SECTION, FABRICATED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, VERTICAL LEG CRACKED BETWEEN FASTENERS STA 1220 AT LONGERON 27R. REMOVED CRACKED VERT LEG FITTING AND REPLACED IAW DC-8 SRM 51-1-20D AN D 51-1-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 683 BULKHEAD CRACKED LBL 10 - RBL 24. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13.

Part: RIB — CRACKED (RT WING) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, RT WING UPPER L/E RIB CRACKED 0.5 IN LONG AT XFS 584. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 LWR FLOOR BEAM CRACKED ABOVE A-CARGO DOOR FRAME AT CUSP SAT 340. REMOVED AND REPLACED FLOORBEAM TO CUSP FITTING IAW DC-8 SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

STA 759 BOOT FITTING CRACKED BETWEEN L17L AND L18L. REPAIRED BOOT FITTING IAW UPS EO DC8-53-2048 AND SAA SK 851-856307.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

FLOORBEAM VERT ATTACH FITTING CRACKED STA 64 RBL 48. REMOVED CRACKED FITTING AND REPLACED IAW DC-8 SRM 51-1-21D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, LONG 11L CRACKED STA 670. REMOVED CRACKED LONGERON FITTING, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 5750540 AND DC-8 SRM 51-1-20D.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE: C1, FLOORBEAM VERTICAL ATTACH FITTING HAS HEAVY CORROSION. ALSO APPEARS TO BE CRACKED. STA 69 RBL 48. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0.

Part: SKIN — CRACKED (C-4 DOOR) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE:C1 C-4 DOOR UPPER FWD CORNER HAS A STEEL DOUBLER REPAIR AND MUST BE REPLACED WITH AN APPROVED REPAIR. REMOVED DOUBLER AND FILLER, FOUND CRACK AT PREVIOUS CUT OUT, CUT OUT DAM AGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 21 , 53-2-0 FIG 1D, AND DWG 5616674.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,626 hrs · 25,638 cycles

INSPECTION TYPE C-1, LT FUSELAGE EXTERIOR SKIN CRACKED 1 IN LONG AT STA 1746 BETWEEN L14L TO L15L. REMOVED DAMAGED AREA OF SKIN, FABRICATED, AND INSTALLED REPAIR DOUBLER, FINGER DOUBLERS, AND FILLERS IAW DC-8 SRM 53-2-1 FIG 7.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC8 MM 33-50-01-2. TEST OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY LIGHTS COME ON INITIALLY WHEN SELECTED, BUT EXTINGUISH WITHIN ONE MINUTE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AS REQUIRED REF M M 33-50-01. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTING WILL NOT WORK. REMOVED & REPLACED EMERGENCY BATTERY PACK OPS CK GOOD PER MM 33-50-01-2 P/N ON AND OFF SAME 60-1223-5. S/N ON 219 & OFF FTL070.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT IAW MM 33-50-01. SYSTEM OPS CHECKS GOOD ON GROUND.

Part: DOOR FRAME — MISLOCATED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C, MAIN CABIN AT STA 1660-R2 DOOR JAMB WEB HAS DOUBLE DRILLED HOLES. REM FASTENERS FROM DOOR JAMB WEB. REM AIR GRILL AND R2 DOOR DRAIN PAN. TRIMMED OUT DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 DWG DC8-53A-01 0 AND UPS EO DC8-5310-11728-A FAB 99 ANGLE, REP STRAP AND NEW DOOR JAMB WEB IAW DAC DWG 5772756 AND REO G09326. ALOD PRIMED IAW SRM 51-1-8. INSTALL WEB AND REPAIR STRAP IAW SRM 51-1-21 AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING. LOCATED, DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND REINSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSTALLED LONGERON END FITTING IAW SRM 51-1-21, 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, EXTERIOR FUSELAGE SKIN STA 670 ON CENTERLINE OF BELLY, SKIN AT ANTENNA MOUNT FOUND TO BE CORRODED. BLENDED CORROSION. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS AND FINGER DOUBLERS IAW DC8 SRM 51-1-20D & 51-1-20B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS AND FINGER DOUBLER ALL IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER, S KIN FILLERS AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE:C3 MAIN CABIN AT FS 1660, LONGERON 11R IS CRACKED. REMOVED OLD LONG 11RT TO FOM , LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 11RT IAW DC8 SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, LONGERON 17R CRACKED AT BS 1768. REMOVED L17R AND END FITTING IAW SRM 51-1-21. LOCATED AND DRILLED NEW LONGERON SECTION AND END FITTING IAW SRM 51-1-24. INSTALLED LONGERON AND FITTING IAW SRM 51-1-21 AND 51-1-120D.

Part: ANGLE — CRACKED (KEELBEAM COVER) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C, R/W/W KEEL BEAM INSIDE ACCESS DOVER STA 935, BEAM IS CRACKED REM MLG LT AND RT DOOR ACTUATORS, LT AND RT W/W WEBS TO FOM. LOC DRI LLED AND INSTALLED NEW SPLICE ANGLE IAW DAC DWG 5750371 P/N 5750042- 1N. FAB -51, -53, -55, -57 AND -59 REPAIR PARTS IAW DAC DRAWING 575041 2. INSTALLED REP PARTS, ATT COMPONENTS AND NEW SECTION OF WEB IAW DAC DWG 5750412, DC8 SRM 51-1-20D. INST MLG LT AND RT ACTUATORS.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE:C3 LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING LOCATED AND DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND INSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSTALLED LONGERON AND END FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (DOOR) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, L1 DOOR UPPER FORWARD CORNER SHOWS CRACK INDICATION WITH X-RAY INSPECTION. CUT OUT CRACK AND FABBED -15 DOUBLER, -17 DOUBLER, AND -19 FILLER IAW SRM 53-2-0 FIG 15 TR 53-155. ALODINED AND PRIMED IAW SRM 5 1-1-8. INSTALLED DOUBLERS AND FILLER IAW SRM 51-1-20D AND SRM 53-2-0 FIG 15 TR 53-155. DRILLED NEW SPLICE ANGLE PN 5597646-99 IAW SRM 51-1-24. INSTALLED ANGLE IAW SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 31L CRACKED REMOVED CRACKED LONGERON SPLICE IAW SRM 51-1-20D. REC'D, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 5 1-1-20D

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, L2 DOOR UPPER FWD CORNER SHOWS CRACK INDICATION WITH XRAY INSPECTION. REMOVED CRACKED INTERNAL SKIN DOUBLER AND PARTIALLY REMOVED WEB TO FOM. FAB NEW INTERNAL SKIN SPLICE DOULBER IAW DWG NR 4751734 AND PRIMED IAW DC8 SMR 51-1-8, THEN INSTALLED DOUBLER AND WEB IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-21A, 51-1-17 AND DAC DWG 4751734

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, R2 DOOR UPPER AFT CORNER SHOW CRACK INDICATION WITH S RAY INSPECTION. REMOVED DAMAGE IN SKIN AND INTERNAL DOUBLER IAW SRM 53-2-0. REMOVED WEB STA 1650-1660 L9-15 RT AND INTERCOSTAL STA 1620-1640 BTWN L10- 11R FAB DOUBLER, TRIPLER, AND FILLERS IAW SRM 53-2-0. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED DOUBLER, TRIPLER, FILLERS, AND INTERCOSTAL IAW SRM 51-1-20D AND 53-2-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,804 hrs · 24,952 cycles

INSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 36 CRACKED REMOVED CRACKED LONG 36 FS 1270-1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 36 FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK NORMAL.

Part: STATIC LINE — CONTAMINATED (PITOT/STATIC SYS)

INSPECTION TYPE:N/A EN ROUTE IMC CONDITIONS LOST ALL STATIC INSTRUMENTS, AIRSPEED INCLUDING STANDBY ALTIMETERS & ILLEG SELECTED ALT STATIC, NO HELP. DIVERTED TO CAE. DRAINED MOISTURE FROM STATIC SYSTEM AND CLEANED PITOT AND STATIC LINES. REMOVED AND REPLACED NR 1 AND NR 2 ADC IAW MM 34-11-01, TESTED PER 34-11-01, TESTED PER 34-11-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CABIN)

INSPECTION TYPE:N/A AT ENGINE START ALL MAIN DECK SMOKE DET LIGHTS ILLUMINATED. PERFORMED ADJ TEST OF SMOKE DETECTOR SYS PER MM 26-10-05, SYS TEST NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:LINE EXT FUSELAGE SKIN CRACKED AT STA 505 L27R. REPAIRED AREA IAW DC8 SRM 53-2-1 AND REO-G08474.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:LINE L27R CRACKED STA 505. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON IAW DC8 SRM 53-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS ON CREW PREFLT APPEARS INOP. REMOVED AND REPLACED BATTERY PACK, TESTED OK.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:X2 FWD CARGO PIT AT FS 500 - 520 INTERCOSTAL AT LONG 33R IS CRACKED. REMOVED OLD INTERCOSTAL, FABBED NEW PART TREATED AND PRIMED NEW PART, DRILLED, INSTALLED NEW PART ALL IAW DC8 SRM 51-1-8 AND DAC DWG 5616 520 & SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT FS 1270 LONGERON 35L CRACKED. REMOVED CRACKED SECTION OF LONGERON IAW DC8 SRM 51-1-20D, RECEIVED NEW SECTION, FAB'D P/N 3758593-1, LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24, INSTALLED SECTION OF LONGERON IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT FS 1220 - 1228 FITTING AT L31R HAS EXFOLIATED CORROSION. REMOVED AND REPLACED NEW FITTING IAW DC8 SRM 51-3-0 & 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:X2 AFT PIT FS 1152 FITTING AT L31R-L33R IS CRACKED. REMOVED BANANA FITTINGS AT STA 1152 & 1160 IAW DC8 SRM 51-1-20D, REC' D LOCATED AND DRILLED NEW FITTING AT STA 1152 IAW DC8 SRM 51-1-24 AND REINSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT STA 1230 INSIDE TORQUE BOX AT L32R FITTING CRACK. REMOVED AND REPLACED (2) BANANA FITTING (4) EACH LONGERON END FITTINGS AND SUPPORT ANGLE AT RT JAMB AREA IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT LONGERON 34L CRACKED FS 1482-1487. REMOVED DAMAGED PART OF LONGERON, INSTALLED NEW PART OF LONGERON AND NEW SPLICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT STA 1240 BETWEEN L35R-L34R FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, REC'D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 FWD CARGO PIT AT FS 200 ABOVE LONG 36 FRAME IS CORRODED AT LONGERON ATTACH FITTINGS. REMOVED CORROSION IAW DC8 SRM 51. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT C3 RAMP PANEL FOLDING DOOR HINGE IS CRACKED. REMOVED AND REPLACED HINGE (REP) DC8 SRM 51-3-2, 51-3-0.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:C2 AFT PIT FS 1270 L35L SPLICE FITTING IS CRACKED. REMOVED SPLICE IAW DC8 SRM 51-1-20D, FOUND LONGERON SPLICE FITTING CRACKED. RCVD NEW SPLICE PN 3759253-1N LOCATED, DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 73,512 hrs · 24,101 cycles

INSPECTION TYPE:X2 FWD CARGO PIT AT FS 600-620 LONG 31R SPLICE FITTING CRACKED. REMOVED SPLICE FITTING DRILLED NEW FITTING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: LINE — BLOWN (NR 2 ENG HYD SYS)

ATB FOR HYD LOST IN FLT, FOUND NR 2 EDP FLEX LINE BLOWN. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE. RAN ENGINES, LEAK CHECKED. OPS CHECK GOOD.

Part: BRACKET — BROKEN (COCKPIT)

INSPECTION TYPE:IN EVAC SLIDE BRACKET BROKEN (REFER TO M209762). REMOVED AND REPLACED BROKEN BRACKET ON SLIDE COVER. REINSTALLED SLIDE CHECKS OK. THIS CLEARS M209762.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C FUSELAGE BULGING AND POPPING HI-LOCKS BOTTOM OF BELLY AFT NR 3 PIT AREA. THIS ITEM TRANSFERRED FROM B-CHECK NON-ROUTINE 273672 CUTOUT CORRODED AREA AND INST DOUBLERAND TRIPER PER EO. DC8-5330-13596-A

Part: SWITCH — INOPERATIVE (COCKPIT)

MASTER FIRE WARNING RESET SWITCH FAILED AFTER TEST OF SECOND ENGINE. REPLACED MASTER FIRE WARNING SWITCH.

Part: TERMINAL — BROKEN (CORE COWL)

NR 3 ENG FIRE WARNING NO TEST. REPAIRED TERMINAL UNDER CORE COWL.

Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)

INSPECTION TYPE:PDC, AIRCRAFT EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01, OP CK GOOD.

Part: LONGERON — CORRODED (BS 600)

INSPECTION TYPE:C1, FWD PIT FS 600 L36 CORRODED. FABBED SPLICE SHIMS IAW TIMCO REO-06533, ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND TIMCO REO-06533.

Part: FRAME — DAMAGED (BS 480)

INSPECTION TYPE:C1, MAIN CABIN FRAME STA 480 L10R HAS HOLE FABBED REPAIR ANGLE IAW REO-06496. FABBED FILLER IAW REO-06496, ALODINED AND PRIMED REPAIR ANGLE AND FILLER IAW DC8 SRM 51-1-8, INSTALLED REPAIR WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: SKIN — CORRODED (BS 600)

INSPECTION TYPE:C1, FWD PIT FS 600 L36 CORROSION ON SKIN DOT 0441. REMOVED FASTENERS FOR ACCESS, REMOVED CORROSION, ALODINED AND PRIMED IAW UPS DC8 SRM 51-1-8. FASTENERS TO BE INSTALLED ON UPS N/R 936077.

Part: FRAME — CORRODED (BS 640)

INSPECTION TYPE:C1, FWD PIT FS 640 L33L CORROSION ON WALL TO FRAME AND ATTACH ANGLE DOT N 619. CLEANED CORROSION, CORROSION BEYOND LIMITS, FABRICATED REPAIR ANGLE PER DC8 DWG 56104-16 ANGLE PER DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 660)

INSPECTION TYPE:C1, CORROSION ON LONGERON 31R ACCESSORY COMPARTMENT STA 660. FABRICATED REPAIR ANGLE IAW REO 06502, ALODINED AND PRIMED IAW DC8 S RM 51-1-8, INSTALLED REPAIRED ANGLE IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — DAMAGED (BS 1680)

INSPECTION TYPE-AD, FASTENER HOLE OVERSIZED ON FLOORBEAM. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, ALODINED AND PRIMED, INSTALLED REPAIR ANGLE. ALL WORK DONE IAW TIMCO DWG DC08-53-0351 R A SHEET 3.

Part: FLOORBEAM — CORRODED (BS 1680)

INSPECTION TYPE-AD, STA 1680 FLOORBEAM VERTICAL LEG CORRODED BETWEEN UPPER TEE AND 2ND ROW OF FASTENERS 3 INCHES INBOARD FROM L21R. SMOOTHED AND BLENDED OUT DAMAGE, FABRICATED REPAIR ANGLE, ALODINED AND PRIMED REPAIR ANGLE AND FLOORBEAM, INSTALLED REPAIR ANGLE. ALL WORK DONE IAW TIMCO REO-06292 REV A.

Part: FLOORBEAM — CRACKED (BS 1660)

INSPECTION TYPE-D, FLOORBEAM CRACKED AT STA 1660 L21R AFT SIDE LOWER FLANGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND FILLER, ALODINED AND PRIMED REPAIR ANGLE FILLER IAW DC SRM 51, INSTALLED REPAIR ANGLE AND FILLER IAW TIMCO REO6262.

Part: BEARING — MISSING (NR 6 MLG TIRE)

LEFT MAIN GEAR AFT INBD TIRE SMOKING, A/C ABORTED TAKEOFF AND RETURNED TO RAMP WITH NR 6 MAIN TIRE MISSING AXLE NUT AND OUTER BEARING. FOUND NR 6 WHEEL AND BRAKE ASS. DAMAGED AND AXLE THREADS N.G. REMOVED AND REPLACED LT BOGIE PER MM 32-11-05 PN ON AND OFF 5759181-501 SN ON UP17253 SN OFF UP14318.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, DURING BITE TEST, EMERG LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. EMERGENCY LIGHTS, OPS CK GOOD.

Part: LIGHTS — FAILED (CABIN)

EMERGENCY LIGHTS FAILED TO TEST PRE-FLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS BATT PACK, OP'S CK'D OK.

Part: SEAT TRACK — CORROSION (BS 510-590)

INSPECTION TYPE:D SEAT TRACK HAS CORROSION OUT OF LIMITS AFT OF THE SPLICE F/S 510-590 LBL 59. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-1-21, 51-3-0, 51-1-11, AND 51-1-8.

Part: DOOR FRAME — CORRODED (BS 1400)

INSPECTION TYPE:D, C-4 CARGO DOOR PAN (FRAME) HAS HEAVY BULDGING AT F/S 1400 LONG-31R TO LONG-32R AND HAS HOLE AT LONG-33R. REMOVED PREVIOUS REPAIR AND REPAIRED IAW DHC SK-851-673 (REF UPS E.O. DC8-5330-9562-A).

Part: RIB — CRACKED (WS 854)

INSPECTION TYPE:D LT L/E UPPER RIB CRACKED AT XF854. REPAIRED IAW SRM 57-2-0, 51-1-21, AND 51-1-20D.

Part: FITTING — CORRODED (BS 1600)

INSPECTION TYPE:D, LONGERON END FITTING AT FS 1600 CORRODED LONGERON 34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CORRODED (BS 1600)

INSPECTION TYPE:D LONGERON END FITTING CORRODED FS 1600 LONGERON 34L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0 FIG 1F.

Part: FITTING — CORRODED (BS 1600)

INSPECTION TYPE:D, LONGERON END FITTING FS 1600 LONG 35L CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-2-0.

Part: FITTING — CORRODED (BS 1600)

INSPECTION TYPE:D, LONGERON END FITTING CORRODED FS 1600 LONGERON 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, LONGERON 35R CORRODED BEYOND LIMITS AT FS 1490 TO 1690. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2-2 FIG 10 AND DWG 5615374.

Part: FLOORBEAM — CORROSION (BS 55)

INSPECTION TYPE:D, FS 55 RBL 46 FWD SIDE OF FLOORBEAM HAS MODERATE CORROSION UNDER NUT PLATE CHANNEL. ALSO, WEB IS CRACKED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 1D.

Part: LONGERON — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, LONGERON 34L CORRODED BEYOND LIMITS AT FS 1490 TO FS 1690. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-4-1 FIG 51, 51-1-20D, AND DWG 5615374.

Part: LONGERON — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, LONGERON 35L CORRODED BEYOND LIMITS AT FS 1490 TO 1690. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-1-21, 53-2-2 FIG10 AND DWG 5615374.

Part: SUPPORT — CORRODED (BS 1680)

INSPECTION TYPE:D, CORROSION REMOVAL ON N/R 687442 WENT OUT OF LIMITS ON FLOOR SUPPORT AT FS 1680 RBL 2 THRU 24. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT IAW SRM 51-1-21, 53-3-0.

Part: LONGERON — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, LONGERON 34R CORRODED BEYOND LIMITS AT FS 1490 TO 1690. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20, 53-4-1 AND DWG 5615374.

Part: LONGERON — CORRODED (BS 1490-1690)

INSPECTION TYPE:D, LONGERON 36 CORRODED BEYOND LIMITS AT FS 1490 TO 1690. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D, AND DWG 5615374.

Part: SHEAR TIE — CORRODED (BS 270)

INSPECTION TYPE:D, TIE FITTING HAS SEVERE CORROSION AT FS 270 BETWEEN STR 32R AND 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE:D, FITTING AT F/S 1766 STR 30L CORROSION REMOVAL WENT OUT OF LIMITS ON N/R 688450. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 1690-1720)

INSPECTION TYPE:D, INTERNAL DOUBLER CORRODED BEYOND LIMITS FS 1690 TO 1720 LONG 28L. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-5-3 AND 51-1-21 AND DWG 5649329.

Part: FITTING — CRACKED (BS 1691)

INSPECTION TYPE:D, FS 1691 STR 30R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-1-20D.

Part: FITTING — CRACKED (BS 1691)

INSPECTION TYPE:D, FS 1691 STR 28R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-1-20D AND 51-1-11.

Part: DOUBLER — CORRODED (BS 1743-1779)

INSPECTION TYPE:D, INTERNAL DOUBLER ON FUSELAGE SKIN BETWEEN FS 1743 AND 1779 CORRODED. FABRICATED REPLACEMENT DOUBLER IAW SRM 53-01-0, 51-01-20, AND DWG 5649329.

Part: SPLICE — CRACKED (BS 380-400)

INSPECTION TYPE:D, FS 380 TO 400 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (BS 400-403)

INSPECTION TYPE:D, F/S 400-403 AT STR 31R, FINGER DOUBLER IS BROKEN OFF AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-2-0, AND 53-4-1.

Part: LONGERON — CRACKED (BS 280)

INSPECTION TYPE:D, STR 32L AT FS 280 IS CRACKED. REMOVED AND REPLACED LONGERON IAW SRM 53-1-0, 51-1-20.

Part: FITTING — CRACKED (BS 820)

INSPECTION TYPE:D, WING BOX, INTERCOSTAL/ATTACH FITTING CRACKED F/S 820 RBL 65. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 832)

INSPECTION TYPE:D, WING BOX INTERCOSTAL ATTACH FITTING CRACKED FS 832 RBL 65. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: SEAT TRACK — CORRODED (BS 740)

INSPECTION TYPE:D, HEAVY CORROSION INSIDE SEAT TRACK U-CHANNEL F/S 740 RBL 26. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-3-0, 51-1-0, 51-1-29D, 53-2-3, AND DC8-5320-5167-C.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:D, F/S 1230 AT STR 20R, ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-1-0, 51-1-20D, AND DWG 4750418.

Part: FITTING — CRACKED (BS 1261)

INSPECTION TYPE:D, F/S 1261 AT STR 19R, STR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 51-1-20D, AND DWG 4740418

Part: FITTING — CRACKED (BS 838)

INSPECTION TYPE:D, FS 838 AT STR 13L THE TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, 51-1-20D AND DWG 3779874.

Part: DOUBLER — CORRODED (BS 360-400)

INSPECTION TYPE:D, INTERNAL DOUBLER CORRODED F/S 360-400 STR 27R-36. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5755271.

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE:D, FS 1260 TO 1280 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE:D, FRAME FITTING FS 340 BETWEEN LONGERON 33R AND 34R HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-21.

Part: SEAT TRACK — CORRODED (BS 1130)

INSPECTION TYPE:D, FS 1130 RBL 24 SEAT TRACK HAS HEAVY CORROSION BTWN PLUGS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-3-0, DC8-5320-5167-C FROM FS 1110 TO 1270.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D, LONGERON 29L END FITTING HAS HEAVY CORROSION AFT OF FS 70 BULKHEAD. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D, LONGERON 28R END FITTING AFT OF F/S 70 HAS MODERATE HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-29D, AND 51-3-0.

Part: FITTING — CRACKED (BS 1238)

INSPECTION TYPE:D, FS 1238 AT STR 35L TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: LONGERON — CORRODED (BS 1502)

INSPECTION TYPE:D, F/S 1502 STR 26L HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 53-2-2 AND 53-4-1.

Part: FITTING — CORRODED (BS 289)

INSPECTION TYPE:D, FS 289 FITTING INBD OF NR 1 CARGO DOOR LATCH LONG 33R HAS CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D AND 53-1-0 AND 51-1-21.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STAB L/E RIB (ONE RIB ABOVE ZFS 104.750 ) IS CRACKED AT LT SIDE AFT END. REPAIRED IAW SRM 51-1-20D AND 55-2-0.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STAB L/E ONE RIB BELOW ZFS123.500 IS CRACKED LT SIDE AFT END. REPAIRED IAW SRM 55-2-0 AND 51-1-20D.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STAB L/E ONE RIB BELOW ZFS 104.750 IS CRACKED ON AFT END RT SIDE. REPAIRED IAW SRM 51-1-20D AND 55-2-0.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STAB L/E RIB STA 104.750 IS CRACKED AT LT AFT END. REPAIRED IAW SRM 55-2-0 AND 51-1-20D.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D VERT STAB L/E RIB ZFS 104.750 IS CRACKED AT THE RT SIDE AFT END. REPAIRED IAW SRM 55-2-0 AND 51-1-20D.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE:D, VERT STAB L/E ONE RIB BELOW ZFS 104.750 IS CRACKED LT SIDE AFT END. REPAIRED IAW SRM 55-2-0 AND 51-1-20D.

Part: CHORD — CORROSION (BS 857)

INSPECTION TYPE-D, FS 857 AT LBL 16 CENTER WING BOX UPPER AFT CHORD HAS HEAVY CORROSION. REMOVED AND REPLACED CHORD IAW SRM 51-1-21.

Part: RIB — CRACKED (WS 397)

INSPECTION TYPE:D, LEFT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS 397. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 811)

INSPECTION TYPE:D, LEFT WING L/E RIB CRACKED ON UPPER ARM AT WING STA 811. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.

Part: RIB — CRACKED (WS 817)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS817. REPAIRED IAW SRM 57-2-0, 51-1-21, AND 51-1-20D.

Part: RIB — CRACKED (WS 784)

INSPECTION TYPE:D, L-WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 784. REPAIRED IAW SRM 57-2-0 AND 57-3-3.

Part: RIB — CRACKED (WS 828)

INSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM STA XFS 828. REPAIRED IAW SRM 57-3-3 AND 57-2-0.

Part: RIB — CRACKED (WS 764)

INSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 764. REPAIRED IAW SRM 57-2-0 AND 57-3-3.

Part: RIB — CRACKED (WS 763)

INSPECTION TYPE:D, RT WING L/E AT STA XFS 763.00 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (WS 835)

INSPECTION TYPE:D, LEFT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS 835. REPAIRED IAW SRM 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 742)

INSPECTION TYPE:D, RT WING L/E AT STA XFS 742.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 802)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 802. REPAIRED IAW SRM 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 748)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS 748. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 823)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS 823. REPAIRED IAW SRM 57-3-3, 57-2-0, AND 53-3-1.

Part: RIB — CRACKED (WS 404)

INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS AT STA XFS 404.00. THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-3, 57-2-0.

Part: RIB — CRACKED (WS 679)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT WING STA XFS 679. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 848)

INSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 848. REPAIRED IAW SRM 57-2-0 AND 57-3-3.

Part: RIB — CRACKED (WS 647)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED ON UPPER ARM AT STA XFS 647. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS ON TOP, AT FRONT SPAR, SKIN HAS 2 AREAS OF MODERATE FLAKING CORROSION, 36 FROM I/B END. REPAIRED IAW SRM 57-2-1 AND 51-1-21.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D, LONGERON 32R CORRODED AT TIE FITTING MATING SURFACES FWD SIDE OF FRAME FS 70. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, COCKPIT OVERHEAD DOME EMERGENCY LIGHT AND CABIN EMERGENCY LIGHT INOP. REMOVED AND REPLACED CANNON PLUG AT EMERGENCY BATTERY PACK AND PIN. REMOVED AND REPLACED BATTERY PACK AND CKD OKAY (P/N 5708458-503) (S/N FTL 231) ON, (2054) OFF.

Part: LONGERON — CORRODED (BS 1350-1490)

INSPECTION TYPE: C. L34R, FS 1440-1460, IS CORRODED THROUGH VERTICAL LEG. REMOVED AND REPLACED L34R, FS 1350-1490.

Part: LONGERON — CRACKED (BS 1350)

INSPECTION TYPE: C. LONGERON 34R, FS 1350 IS CRACKED ON SPLICE FITTING. FABRICATED NEW FITTING IAW DAC DWG 3779919-1, INSTALLED FITTING IAW DC8 SRM 51-1-20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.

Part: WEB — CRACKED (LT TE FLAP)

INSPECTION TYPE: C. LEFT WING INBOARD END WEB IS CRACKED. REPAIRED LEFT FLAP WEB AT XCW=64.8 IAW TIMCO REO-02088 AND ENGINEERING FILE DC8 57-0697.

Part: INTERCOSTAL — CORRODED (BS 1440-1460)

INSPECTION TYPE: C. INTERCOSTAL, FS 1440-1460 AT L34R IS CORRODED. REMOVED INTERCOSTAL AND J-ANGLE, FABRICATED J-ANGLE PER DAC DWG 5616674 ALODINED AND PRIMED IAW DC8SRM 51-1-20D.

Part: DRAG ANGLE — CRACKED (NR 3 PYLON)

INSPECTION TYPE: C. NR 3 PYLON DRAG ANGLE HAS SHEARED FASTENER HEAD, AND CRACK INDICATIONS. REPAIRED NR 3 PYLON DRAG ANGLE FASTENER, AND CRACK INDICATIONS IAW REO 02062, REV IR.

Part: FRAME — CRACKED (FS 300)

INSPECTION TYPE: C. LEFT CIRCUMFERENTIAL FRAME HAS A 3 INCH CRACK IN RADIUS AT FS 300, IN LOWER AFT CORNER OF MAIN CARGO DOOR CUT-OUT. CUT OUT DAMAGED SECTION OF FRAME, FABRICATED NEW FRAME SECTION, IAW SRM 51-1-21 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (NR 1 PYLON)

INSPECTION TYPE: C. .050 INCH CRACK AT T/E OF TEE DOUBLER. TRIMMED OUT DAMAGE AREA OF TEE DOUBLER, SHOT PEENED EDGE OF TRIM RADIUS, AND AREA OF UPPER AND LOWER SURFACE IN TRIM AREA PER OPS 4.999 CORROSION PROTECT ALL BARE METAL AND REWORK AREA SRM 51-1-8 AND IAW TIMCO REO-02042.

Part: PANEL — OUT OF LIMITS (LT/RT WING)

INSPECTION TYPE: C. ACCOMPLISHED PERMANENT REPAIR TO LEFT AND RIGHT LEADING EDGE UPPER ATTACH HOLES PER SRM WAN NR 193191. REPAIRED LEADING EDGE SLANT PANEL UPPER CAP IAW TIMCO REO 02029 AND ENGINEERING FILE DC8 57-0695.

Part: SPAR CAP — CRACKED (NR 1 PYLON)

INSPECTION TYPE: C. CRACKS IN FRONT UPPER SPAR CAP AND 508 BULKHEAD FITTING. REPAIRED FRONT UPPER SPAR CAP AND 508 BULKHEAD FITTING, NR 1 PYLON POSITION IAW TIMCO REO-02058 AND ENGINEEERING FILE DC8-57-0690.

Part: SPAR CAP — CRACKED (RT WING)

INSPECTION TYPE: C. CRACKS IN RIGHT LOWER SPAR CAP IN HOLES 4, 5, 6, 7, AND 10 -XW 454. REAMED HOLE NR 10, ALODINED AND PRIMED IAW SRM 51-1-8, AND INSTALLED BUSHING IAW DWG J060232 HOLES 4, 5, 6, 7. REAMED HOLES, STRESS COINED HOLES IAW DPS 3.67-56 AND DAC DWG J060232. ALODINED AND PRIMED IAW 51-1-8, INSTALLED BUSHING IAW REO 02038 AND DAC DWG J060232 AND SRM 51-1-25. FABRICATED REPAIR STRAP IAW REO 02038 AND DWG J060232. ALODINED AND PRIMED IAW 51-1-8.

Part: DOOR JAMB — CRACKED (FS 300)

INSPECTION TYPE: C. MAIN CARGO DOOR JAMB HAS A 2 INCH LONG CRACK ON LOWER AFT CORNER. CUT OUT CRACKED SECTION, FABRICATED NEW FRAME/JAMB SECTION, NEW SHIMS, ALODINED, AND INSTALLED IAW REO-02036 AND DC8 SRM 51-1-21, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1700)

INSPECTION TYPE: C. LONGERON 34L CORRODED AT FS 1700 IN AFT ACCESSORY COMPT, AT TIE FITTING. REMOVED AND REPLACED CORRODED LONGERON SECTION IAW DC8 SRM 53-3-2, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERG BATTERY PACK HAD LOW VOLTAGE. THE LIGHT WOULD COME ON AND THEN DIM AND GO OUT. REPLACED BATTERY PACK, CHECK OK.

Part: FINGER DOUBLER — CORROSION (FS 275)

WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER SECTION ABOVE LONG 30L, FS 275. INSTALLED REPAIR IAW SRM 53-2-0.

Part: FITTING — CORROSION (SLIDE DOOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON C X-SLIDE DOOR NR 1 AND NR 4 LOWER T-BOLT BACK UP FITTINGS. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: FITTING — CORROSION (FS 339)

WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION AT B/T FITTING FS 339 BETWEEN LONG 33L-34L. INSTALLED REPAIR IAW SRM 53-2-0, PAGE 13 AND 14.

Part: SPLICE — CORROSION (FS 600-620)

WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONG 31L SPLICE FITTING FS 600-620. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (LT WING)

WHILE IN 'C' CHECK, MAINTENANCE FOUND LEFT WING FLAP HINGE SUPPORT FITTING CRACKED AT STA 409, INBD FITTING. INSTALLED REPAIR IAW DOUGLAS DRAWING B/P 5751189.

Part: FITTING — CORROSION (FS 301)

WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION ON B/T FITTING, FWD AND AFT SIDES BETWEEN LONG 28L-29L, FS 301. INSTALLED REPAIR IAW SRM 53-2-0, FIG. 2D.

Part: TIE DOWN TRACKS — CORROSION (FS80-260 360-450)

WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LOWER CARGO TIE DOWN TRACKS AT FS 80-260, LBL 36 AND FS 360-450, RBL 36. INSTALLED REPAIR IAW SRM 51-3-0.

Part: SKIN DOUBLER — CORROSION (FS 190)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED SKIN SPLICE DOUBLER HAS HEAVY INTERGRANULAR CORROSION AT FS 190, BETWEEN LONG 32L - 32R. INSTALLED REPAIR IAW SRM 51-1-20D AND SRM 51-1-21.

Part: LE SKIN — CRACKED (WS 310)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING L/E FASTENER HOLE 1 INCH CRACK AT STA XFS 310, UPPER SURFACE. INSTALLED REPAIR IAW SRM 57-2-0.

Part: VANE — DELAMINATED (NR 4 TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 4 FLAP VANE DELAMINATED ON BOTH SURFACES. INSTALLED REPAIR IAW MM 27-51-14.

Part: VANE — DELAMINATED (NR 4 TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP VANE NR 4 DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-51-14.

Part: VANE — DELAMINATED (NR 3 TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP VANE NR 3 DELAMINATED ON BOTH SIDES. INSTALLED REPAIR IAW MM 27-51-14.

Part: VANE — DELAMINATED (NR 3 TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 3 FLAP VANE DELAMINATED ON UPPER SIDE. INSTALLED REPAIR IAW MM 27-51-14.

Part: SKIN — DELAMINATION (NR 5 SPOILER)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED NR 5 SPOILER LEFT WING DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-61-01.

Part: VANE — DELAMINATED (NR 1 TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 1 FLAP VANE DELAMINATED AT BOTH SURFACES. INSTALLED REPAIR IAW MM 27-51-14.

Part: SPLICE — CRACKED (FS 440-480)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED FS 440-460, LONG 27L SPLICE FITTING CRACKED 3 INCHES LONG. INSTALLED REPAIR IAW SRM 51-1-21D.

Part: SPLICE — CRACKED (FS 1260-1280)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED FS 1260-1280, LONG 36 SPLICE FITTING CRACKED 12 INCHES LONG. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: HINGE FITTING — CRACKED (FS 409/339)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP HINGE SUPPORT FITTINGS CRACKED AT STA 409, INBOARD FITTING AND STA 339 OUTBOARD FITTING. INSTALLED REPAIR IAW DOUGLAS DRAWING 5751186.

Part: LE RIBS — CRACKED (LT WING)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING LEADING EDGE NR 11, NR 12, NR 13, NR 16, NR 17 RIBS CRACKED ON UPPER SIDE COUNTING OUTBOARD OF NR 1 PYLON. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801.

Part: LE RIBS — CRACKED (LT WING)

WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING OUTBOARD OF NR 1 PYLON NR 4, NR 5, NR 6, NR 9, NR 10 RIBS ON LEADING EDGE CRACKED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801.