N752UP

Part: EADI — FAILED (COCKPIT)

INSPECTION TYPE:N/A CAPTAIN'S EADI FAILED AND BURNT/SMOKE IN COCKPIT. ***SDR FILED OPEN***

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, COURIER AREA FLOOR PANEL F27 SPONGEY FABRICATED NEW FLOOR PANEL IAW, SRM,. 53-2-1, 51-1-8, 53-21-1, 51-1-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE:C2 AFTER REMOVAL FOUND 5803913-519 STRINGER 54 ATTACH FITTING BROKEN OFF A/C PART. LOCATED, DRILLED, REPLACEMENT STRINGER 54 ATTACH FITTING TO BE INSTALLED ON NR 207274.

Part: FITTING — CRACKED (RUDDER) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, RUDDER HINGE CUTOUT NR 2 FROM BOTTOM DAMPER ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM, 51-1-21, 51-1-8, 51=3-2.

Part: WEB — DAMAGED (RT MLG WW) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, RT MLG DOOR SWITCH STA 896.500 HAS 1 EACH ELONGATED HOLE AT SUPPORTING WEB. FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-9-0,EO-DC8-3260-16914- A.

Part: WEB — DAMAGED (BS 896) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, LT MLG DOOR SWITCH STA 896.500 HAS 1 EA ELONGATED HOLE AT SUPPORTING WEB. REPAIRED IAW EO DC8-3260-16914-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2 NR 4 ALT STRINGER -65 TO FRONT SPAR Z FITTING CRACKED. REMOVED AND REPLACED STINGER IAW SRM,51-1-20D, 51-1-8.

Part: STRINGER — CRACKED (NR 1 PYLON) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE:C2 NR 1 ALT STRINGER -54 CACKED APPROX. AT XRS 480- NR1 PYLON FABBED AND INSTALLED REPAIR IAW SRM, 51-1-8, 51-1-20D, 51-3-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE:C2, NR 1 ALT STRINGER -65 TO FRONT SPAR FITTING CRACKED REMOVED AND REPLACED FITTING IAW SRM, 51-1-20D, 51-1-8, 51-1-2451-1-12.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, FLOOR PANEL F94/F94A HAS SEVERAL ELONGATED HOLES AND A CRACK AT THE EDGE, CUT OUT DAMAGE IAW SRM 53-02-03 FIG 005A. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-03,AND 51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, FLIGHT COMP SUB-FLOOR AREA, BETWEEN STA 8 AND -12 LBL 60 HAS FINGER DOUBLER CORRODED WITH SEVERAL POPPED RIVETS. REMOVED FINGER DOUBLER,CLEANED SUBFLOOR AREA. FABRICATED AND INSTALLED FINGER DOUBLER. IAW DWG NR 5612298 AND SRM 51-1-21, 51-1-20D.

Part: SPAR CAP — CRACKED (WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, CRACK AT CENTER SPAR CAP WEB FLANGE JUST IB XRS255 NR MAIN. STOP DRILLED CRACK , FABBED AND INSTALLED REPAIR DOUBLER IAW. SRM., 51 -1-8, 57-2-0 FIG. 2, 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, FLIGHT COMP SUB-FLOOR ARERA AT STA.- 99.0, RBL27 HAS AN ANGLE SUPPORT CORRODED AND RIVET MISSING. REMOVED AND REPLACED ANGLE SUPPORT IAW SRM, 51-1-8, 51-1-21, 51-1-24

Part: SPAR — CRACKED (WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, POSSIBLE CRACK AT CENTER SPAR WEB FLANGE JUST IB XRS 358 NR 4 MAIN. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR IAW SRM., 57-2-0, 51-1- 8, 51-1-21.

Part: SPAR — DAMAGED (RT WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, RT WING FRONT SPAR T CAP HAS DOUBLE DRILLED HOLE XFS 92.5. CLEANED HOLE AND INSTALLED BUSHING IAW SRM, EO DC8-5710-29984-A, 51-1- 8, 51-1-24.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, RT WING LE AUX TANK UPPER T CAP HAS DOUBLE DRILLED HOLE STA. XFS 92. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-26, 57-2-1 F IG37.

Part: FITTING — CRACKED (BS 1660 L21R) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, MAIN CABIN RT/LT AFT SEVICE DOOR LWR AFT TORQUE BOX HAS CORROSION AND CRACKED STAS.1660 L21R. REMOVED AND REPLACED FITTING IAW SRM. 51-1-8, 51-1-21, 51-1-20D.

Part: FRAME — GOUGED (FS 360 L21L) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, GOUGE ON THE STA 360 LT FRAME JUST ABOVE THE UPPER SURFACE OF THE L21. REPAIRED GOUGE IAW SRM 53-02-00-0 FIG 001F.

Part: FRAME — GOUGED (FS 702-875 L21L) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, GOUGE ON THE STA 702.875 LT FRAME JUST ABOVE THE UPPER SURFACE OF CUSP EXTRUSION(LONGERON 210 IN MAIN CABIN). DRILLED HOLE TO REMOVE DAMAGE AND PLUGGED HOLE. IAW SRM 53-02-00 FIG 0 01F.

Part: STRINGER CLIP — CRACKED (FS 1766 L6R) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, L6R ATTACH CLIP CRACKED AT APB, STA 1766, MAIN CABIN. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW DWG 5773844 AND 5191-20D.

Part: FITTING — CRACKED (BS 1760 L10L) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, END FITTING CRACKED L10L, STA 1760. REMOVED AND REPLACED FITTING IAW, SRM. 51-1-20D, 51-1-8, 51-3-1.

Part: TORQUE BOX — DAMAGED (STA 1660 L-19R) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, MAIN CABIN, RT AFT SERVICE DOOR FRAME (TORQUE BOX) WEB HAS DOUBLE DRILLED AND EXTRA HOLES STA 1660 L-19R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00-0 FIG 001D, 5 1-01-21.

Part: WEB — CRACKED (RUDDER) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C1, CRACK HAS EXTENDED BEYOND STOP DRILL IN RUDDER HINGE CUT-OUT, NR 2 FROM BOTTOM. REMOVED AND REPLACED WEB IAW SRM,51-1-8, 51-1-21, 51-3-1.

Part: LONGERON — CRACKED (FS 1739-1720) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, L15L CRACKED AT CANTED FRAME, MAIN CABIN, STA 1729 REMOVED LONGERON SECTION FS 1739-1720. FABRICATED AND INSTALLED LONGER ON SPLICE AND REPAIR STRAPS. IAW SRM 53-02-02 FIG 10 AND 53-05-03.

Part: FRAME — GOUGED (BS 418) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, GOUGED ON THE BS 418 LT FRAME STRAP ABOVE THE UPPER SURFACE OF CUSP EXTRUSION IN MAIN CABIN. REMOVED AND REPLACED FRAME STRAP IAW SRM, 51-1-20D, 51-1-8.

Part: SKIN — DENTED (BS 1870-1885) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, FUSELAGE SKIN AROUND TAIL-STAND HANGER FIN IN VERY POOR CONDITION, NUMEROUS DENTS, SKIN DEFORMED,PUSHED IN, DAMAGED REPAIR DOUBLER, BAD PAINT STA. 1870-1885. REMOVED AND INSTALLED REPAIR DOUBLER IAW SRM,51-1-20 FIG.45, 51-1-8, 5 2-3-0 FIG. 1D.

Part: DOUBLER — CRACKED (BS 1766) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, POSSIBLE CRACK IN RADIUS OF REPAIR DOUBLER ON BOTTOM OF J-BEAM, APB, 60 COMPT. STA 1766 BL0. REMOVED CRACKED DOUBLER,FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 51-1-8, 53-2-5, 51-1-24, 51-1-20D, 51-3-1.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, OBSERVERS FWD SEAT TRACK HAS ELONGATED HOLES REMOVED AND REPLACED SEAT TRACK IAW, SRM, 51-3-2, 51-1-8, 51-3-0.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2 CAPT BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED CAPT'S LT AND RT SEAT TRACKS IAW SRM 51-01-24 AN AND 51-01-20D.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, EXTERIOR FUSELAGE HOLD OPEN RECEPTACLE FOR L1 DOOR HAS CRACKED REPAIR DOUBLER. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-5, 51-3-0.

Part: STRINGER — CRACKED (BS 1766-1772) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, L 17R CRACKED UNDER END FITTING , STA. 1766-1772, 60 COMPT. REMOVED AND INSTALLED NEW END FITTING IAW SRM, 51-1-8, 51-3-0, 53-5-1 FIG.F.

Part: SHEAR TIE — CRACKED (BS 1800 L3L) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, LARGE SHEER TIE BRACKET CRACKED AT LT END, 60 COMPARTMENT CEILING STA, 1800,L3L. REMOVED AND REPLACED SHEER TIE IAW SRM 51-1-8, 53-2-0 FIG F ,51-1-20D.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2 F/E'S AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED F/E'S AFT SEAT TRACK IAW SRM 51-01-24.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, F/O'S BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24, 51-3-1.

Part: FITTING — GOUGED (LT WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, LT WING FLAPWELL FITTING BENT AND GOUGED BELOW FLAP STA 98 ACTUATOR. REMOVED AND INSTALLED FITTING AT FLAP STA 98 IAW SRM 51-3-0, 51-1-8, 5 1-3-1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, AFT END OF RIB CRACKED IN RT HORIZ STAB L/E STA. XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 5 1-3-02, 55-02-00 FIG 2.

Part: SEAT TRACK — CORRODED (BS 1306-150) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, MCC FLOOR SEAT TRACK LBL 59 CORROSION AND WEAR MARKS BS 1306 TO 1350. INSTALLED 1EA PLUG AND 1 CHANNEL BS 1320-1326 LBL 59 IAW SRM 51-03- 01 (AREAS STA 1306-1319 AND 1326-1350 BLENDED AND WITHIN LIMITS IAW SRM 53-02-03 FIG 012).

Part: SEAT TRACK — BROKEN (BS 260) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, BROKEN SEAT TRACK LUG ON MAIN CARGO FLOOR STA 260 BL 0. CUT OUT DAMAGE IAW 53-02-03 FIG 006D INSTALLED 2EA PLUGS AND 2EA CHANN ELS IAW 51-03-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, CORRODED LOWER ATC-2 ANTENNA INSTALLATION AREA EXTERNAL SKIN AT STA. Y 427-5 RBL3. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 53-2-00 FIG 1F51- 3-2, 51-1-22.

Part: ATTACH BRACKET — GOUGED (RT WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, RT WING REAR SPAR AT IB HINGE OF NR4 SPOILER PARTITION RIB ATTACH BRACKET GOUGED AND BENT. REMOVED AND REPLACED GUSSET IAW SRM, 51-1-21,57-2-0, 51-1-8.

Part: LONGERON — CORRODED (L31R) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, AC COMPT. STA 62, HAS L31R WITH EXFOLIATION CORROSION. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-1- 8, 53-2-0 FIG. 1F, 51-1-21.

Part: FLOORBEAM — CORRODED (BS 55 RBL 38) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, A/C COMPT. BS 55, RBL 38, FLOORBEAM HAS EXFOLIATION CORROSION. REMOVED CORROSION, FABBED AND INSTALLED REPAIR IAW, SRM, 51-1-8, 51-2- 00, 51-1-21A, 51-3-0.

Part: BULKHEAD — CRACKED (BS 683 LBL21) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE:C2 FWD ACCESSORY COMPT BULKHEAD AT STA 683 LBL 21 BELOW FASTENER PATTERN ATTACHING BULKHEAD DOME TO WING LOWER FRONT SPAR WEB HAS 3 INCH CRACK. REMOVED WEB, REPLACED WEB IAW SRM 51-1-21.

Part: SKIN — DAMAGED (RT WING) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF R/W OB, L/E, FWD OF 3RD. PANEL FROM OB END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2- 0 FIG.7 51-1-21.

Part: NONE — NONE (SCHEDULED MAINT) · airframe 62,439 hrs · 26,361 cycles

INSPECTION TYPE-C2, COMPLY WITH MPI 19584 REGARDING REPLACEMENT OF EXISTING REPAIR AT AT L28R IAW WAN3 1369154 AND EO DC8-5330-20248-E APPX.E FABBED AND INSTALLED REPAIR DOUBLER IAW, EA NR 008-5330-01-A1449, SRO 853 0032. NOT AN SDR.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS STAY LIT FOR SHORT PERIOD OF TIME. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AND RELAY UNIT PER MM 33-50-01-2. OPS CHECK NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS DISARM CHECK BULB BURNED OUT. RELAMPED DISARM EMERGENCY LIGHT. OPS CHECKED GOOD PER MM 25-60-00.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND RELAY UNIT PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. EMERGENCY LIGHT BATT & RELAY REMOVED AND REPLACED ON L/P 686282. OPERATES NORMALLY AT THIS TIME, ALSO PER TECH REQUEST, PERFORMED VOLTAGE/CHARGING TEST IAW MM 33-50-01-2, NO FAULTS, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT IAW MM 33-50-01-2. TESTS OK.

Part: CONNECTOR — DISCONNECTED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTING INOP. RE-ATTACHED POWER SUPPLY CONNECTOR. OPS CHECK GOOD REF DC8 MM 38-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TURN ON PREFLIGHT CHECK. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND SYSTEM CHECK SERVICEABLE.

Part: WINDOW — STUCK (COCKPIT)

CAPTAIN'S WINDOW WILL NOT OPEN. INSPECTED WINDOW LATCH AND MECHANISM. REATTACHED SMALL TRIM PIECE. OPS CHECK GOOD.

Part: LINKAGE — STUCK (COCKPIT WINDOW)

PILOTS SLIDING WINDOW WILL NOT OPEN. ADJUSTED PILOT SLIDING WINDOW UPPER ACTUATING LINKAGE ROD PER AMM 56-10-03-56, OPS OK.

Part: SKIN — DELAMINATED (RT WING)

RT WING SPOILER AT XRS 247 TO 351 HAS TEAR AT RT. MID HINGE ON TOP AND WORN THIN UNDERNEATH NR 4 SPOILER. INSTALLED NEW NR 4 SPOILER PER MM 27-61-01-2 TO STEP B6. INSTALLED IAW MM 27-61-01-2. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING PDC, FOUND EMERGENCY LIGHTING INTERMITTENT. EMERG BATTERY PACK REPLACED AND FUNCTION TESTED SERVICEABLE IAW DC8 MM 33-50-01-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 STA 370 L28R HAS AREA OF DEEP INDENTATION AND RIVET HEAD MISSING. CUT OUT DAMAGED AREA AT STA 370 L28R IAW SRM 53-02-01-0 FIG 007. FABRICATED AND INSTALLED 2EA FILLERS, DOUBLER, AND 4EA FINGER DOUBLERS AT STA 370 L28R IAW SRM 53-02-01-0 FIG 007.

Part: SKIN — CRACKED (FS 1990 TAILCONE) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 AFTER REMOVAL OF TAIL CONE FOUND EXTERIOR SKIN DENTED, CRACKED, AND BROKEN OUT FWD END. REMOVED DAMAGED SKIN AT TAIL CONE EXTERIOR STA 1990 IAW SRM 53-02-00-0. RECEIVED, DRILLED UP NEW SKIN IAW SRM 53-02-00-0 AT TAIL CONE EXTERIOR SKIN STA 1990.

Part: FITTING — GOUGED (LT WING) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 LT WING FLAP STA 219 CANOE SIDE BRACES HAVE PLAY AT ACTUATOR UPON REMOVAL OF LT WING FLAP STA 219 CANOE, FOUND REAR SPAR FITTING GOUGED OUT OF LIMITS IAW SRM 57-51-12. MACHINED LT WING SPAR FITTING. FABRICATED AND INSTALLED FOUR SPACERS ALL IAW UPS RAA DC8-57-20171 SAA EA 008-5710-01-A0223, BAC SERV REQ 1-196088918, AND FAA FORM 8100-9 ALL DATED 6/1/06.

Part: FITTING — CORRODED (T/E FLAP) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 RT WING STA 219 FLAP ACTUATOR FITTING GOUGED AND CORRODED. REMOVED AND REPLACED RT STA 219 FLAP ACTUATOR FITTING IAW SRM 51-3-1, RIGGED AND TORQUED FLAP ACTUATOR IAW DC-8 MM 27-51-12, 20-14-00-2 AND DC-8 MM 27-51-09, OP'S CHECK GOOD.

Part: SPLICE — CRACKED (FS 1280 L36) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3SP D-PIT AT STA 1280 L36 SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 1280 L36 IAW SRM 51-1-20D, AND SRM 51-1-8.

Part: ATTACH FITTING — CRACKED (FS 340) · airframe 61,407 hrs · 25,631 cycles

INSPECTION TYPE:C3 CRACK ON LWR RT CUSP FLOORBEAM ATTACH FITTING STA 340. REMOVED, FABRICATED AND INSTALLED FITTING IAW 51-1-21 AND 51-1-20D DWG 9754022.

Part: FITTING — CRACKED (FS 380-400 L31L) · airframe 61,409 hrs · 25,631 cycles

FOUND SPLICE FITTING LONGERON 31L STA 380-400 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW SRM 51-11-20D.

Part: SPLICE — CRACKED (FS 1270 L34L) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 D-PIT STA 1270 L34L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING AT STA 1270 L34L IAW SRM 51-01-20D. DRILLED UP AND INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D, AND 51-1-8.

Part: DOOR FRAME — CRACKED (FS1220 L22R) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A .750" CRACK ON THE AFT UPPER DOOR JAMB OF THE C-4 DOOR. CUT OUT DAMAGED SECTION OF AFT UPPER DOOR JAMB OF THE C-PIT DOOR IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 21, AND SRM 51-01-26

Part: FITTING — CRACKED (FS 900 L25R) · airframe 61,409 hrs · 25,631 cycles

FOUND STA 900 L25R CRACK IN FITTING ON FRONT SIDE OF FRAME. REMOVED AND REPLACED FITTING AT STA 900 L25R IAW SRM 51-1-20D, AND SRM 51-3-2.

Part: BRACKET — CORRODED (FS 832 L28R) · airframe 61,409 hrs · 25,631 cycles

AT STA 832 AND L28R FORWARD SIDE OF FRAME BRACKET CORRODED. REMOVED, FAB`D AND INSTALLED BRACKET IAW SRM 51-01-20D, DWG 4753360.

Part: SKIN — CRACKED (FS 560 L34R) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A .500 INCH CRACK ON THE LWR FWD B-PIT DOOR JAMB CORNER. CUT OUT DAMAGED AREA IAW SRM 53-02-00-0 FIG 20. FABRICATED AND INSTALLED FILLER, DOUBLER, AND TRIPLER IAW SRM 53-02-00-0 FIG 20, AND SRM 51-8-1 AT STA 560 L34R (B-PIT LWR FWD DOOR CORNER).

Part: SEAT TRACK — GOUGED (BS 1140 RBL25) · airframe 61,409 hrs · 25,631 cycles

INSPECTION TYPE:C3 SEAT TRACK GOUGED FS 1140 RBL 25 MAIN CABIN. CUT OUT DAMAGED SEAT TRACK AT STA 1140 RBL 25 IAW SRM 53-02-03, MACHINED AND INSTALLED SCALLOPED SEAT TRACK AT STA 1140 RBL 25 IAW DWG S2400463, AND SRM 53-02-03-0.

Part: RIB — CRACKED (LT WING) · airframe 61,409 hrs · 25,631 cycles

FOUND LT LEADING EDGE AT STA XFS 841.250 RIB IS CRACKED. STOP DRILLED CRACK AT LT L/E AT STA XFS 841.250 IAW SRM 57-02-00-0 FIG 002. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLERS IAW DWG 5769470, AND SRM 57-02-00, AND SRM 51-1-21

Part: SKIN — CRACKED (RWS 467) · airframe 61,409 hrs · 25,631 cycles

FOUND CRACK ON LWR SURFACE BETWEEN F/S AND C/S JUST INBD OF XRS 463 NR 4 ALT TANK. CUT OUT SKIN DAMAGE AT WING STA XWS 467 IAW UPS EO DC8-5730-24293-A SAA EA NR 008-5710-01-A0156. FABRICATED AND INSTALLED -1 FILLER, -2 DOUBLER, -3 EXTERNAL TRIPLER,-4 INTERNAL DOUBLER, -5 INTERNAL TRIPLER, AT WING STA XWS467 IAW DWG 5612385, UPS EO DC8-5730-24293-A SAA EA 008-5710-01-A0156,BAC MESG1-85371798-2, FAA FORM 8100-9.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,409 hrs · 25,631 cycles

FOUND MAIN CABIN AFT LEFT FWD PRESS BULKHEAD LONGERON 12L CRACKED. REMOVED DAMAGED SECTION OF LONG 12L IAW SRM 51-01-21-0, AND 53-02-02-0 FIG 10. FABRICATED AND INSTALLED REPAIR SPLICES, AND LONGERON SPLICE AT STA 1734-1747 L12L IAW SRM 53-02-02-0 FIG 10, SRM 51-03-02-0 AND SRM 51-01-20D-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,409 hrs · 25,631 cycles

FOUND LONGERON 13R STA 1758 WERE VERTICAL STAB ATTACHES HAS A CRACK COMING OUT OF NUT ON BACK OF SHEARTIE. REMOVED LONGERON SECTION AT STA 1758 L13R IAW SRM 53-02-02 FIG 11. FABRICATED AND INSTALLED REPLACEMENT LONGERON SPLICE IAW SRM 53-02-02 FIG 11, AND 51-01-08.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,409 hrs · 25,631 cycles

INSPECT SMALL DENT AFT OF PIT NR 34 4 FT AFT. CUT OUT DAMAGE, FABRICATED, AND INSTALLED DOUBLER, FILLER FINGER DOUBLER IAW SRM 53-2-01 FIG 7.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

NO EMERGENCY EXIT LIGHT. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK CHECKED OK PER 33-50-02-2.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK GOOD IAW MM 33-10.

Part: PIN — DAMAGED (CONNECTOR)

INSPECTION TYPE:N/A BTB - EMERGENCY EXIT LIGHTS REMAINED ON DURING PUSHBACK SWITCH IN ARMED POSITION & GENERATOR NR 2 & NR 3 POWERING THE A/C. BLOCKED OUT AT 0221 BLOCKED IN 0232. FOUND PINS NR 9 & 10 PUSHED BACK ON CONNECTOR P1-1345. CLEANED AND RESET PINS. ALSO REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR PRECAUTIONARY. SYS OPS CHECKS NORMAL PER MM 33-50-01-2.

Part: SLIDE — DEPLOYED (PAX DOOR)

INSPECTION TYPE:N/A ESCAPE SLIDE DEPLOYED WHILE ATTEMPTING TO CLOSE MAIN ENTRY DOOR. REF M287491. REPLACED SLIDE AS PER MM 25-60-02-2, S/N INSTALLED 36-22 THIS CLEARS M287491.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 2 EA DIAGONAL STIFFENERS FOR STA 8 BULKHEAD HAVE PREVIOUSLY CUTOUT DAMAGE ON LOWER ENDS. FABBED REPAIR ANGLE DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D.

Part: BRACKET — CRACKED (NR 2 SPOILER) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 RIGHT WING NR 2 SPOILER O/B MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING 32 SPOILER O/B MOUNT BRACKET IAW UPS DC8 SRM 51-1-21, 51-1-20D, AND 51-3-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AT APPROX STA 20, L34R CRACKED AT LOWER RADIUS. FAB, LONGERON LOCATED, DRILLED AND DEBURRED, ALODINED AND PRIMED NEW LONGERON IAW DC8 SRM 51-1-24, 51-1-8, AND DAC DWG 4615293.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 EXT FUSELAGE AT FS 1700 APPROX BETWEEN L16R AND L17R FASTENER HOLE CRACKED RUNNING FWD. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-1. FABBED DOUBLER, FINGER DOUBLER, AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, MAIN CABIN FS 1727 FLOORBEAM AT RBL 34 & FLOOR SUPPORT CORRODED. REMVOED CORROSION FROM FLOORBEAM IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED TEE & L ANGLES IAW DAC DWG 575503. LOCATED AND DRILLED PARTS IAW DC8 SRM 51-1-24. INSTALLED FLOORBEAM AND SUPPORT AND ALL ATTACHING STRUCTURE THAT WAS REMOVED TO ACCESS IAW DC8 SRM 51- 1-20D, 51-3-0. ALOD & PRIME FLOORBEAM AND SUPPORT IAW DC8 SRM 51-1-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 MAIN CABIN FS 1660 FLOORBEAM AT LBL 20-LBL 30 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND PRE-EXISTING PLUG AT SEAT TRACK ATTACH HOLE OUT OF LIMITS. ROUTED OUT DAMAGE & FAB REPAIR ANGLE AND FILLER IAW DC8 SRM 51-2-1 FIG 1 SHT 7 TR 51-130. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-2-1 FIG 1 SHT 7 TR 53-138 AND DC8 SRM 51-1-20D FIG 4A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, LONGERON 6L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING, LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM DC8 20-14-00.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 INNER DOUBLER FOR BELLY SKIN FOUND TO HAVE PREVIOUS DAMAGE (CUT) AT APPROX STA 22 L31L-33L. REMOVED SPLICE DOUBLER. FABRICATED -53 SPLICE DOUBLER IAW DAC DWG 5613 862. INSTALLED IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-1.

Part: LONGERON — GOUGED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AT APPROX STA 22 L34L FOUND TO HAVE PREVIOUS DAMAGE. REMOVED LONGERON IAW DC8 SRM 51-1-21. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. RECEIVED NEW LONGERON, LOCATED, DRILLED IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.

Part: CHANNEL — CRACKED (LT WING) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 HAT CHANNEL FWD OF J-HOOK (FOR MLG DOOR RELEASE) IS CRACKED. REMOVED CRACKED HAT CHANNEL, FABRICATED NEW HAT CHANNEL IAW DAC DWG S-1 289798, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW HAT CHANNEL IAW DC8 SRM 51-3-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 CABIN STA 650 SEAT TRACK PITTED LBL 60. REMOVED CORRODED IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-3. ROUTED OUT DAMAGED IAW UPS DC8 SRM 53-2-3. LOCATED AND DRILLED HOLES IN SEAT TRACK TO LOCATE PLUG AND CHANNEL IAW UPS DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3 -0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 LONGERON 7R BATHTUB FITTING CRACKED AT STA 680. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 5 1-1-24, AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM 20-14-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 857 L9R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND MM 20-14-00.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 MAIN CABIN BETWEEN STA 1040 AND STA 1060 STR 1 SPLICE FITTING CRACKED. HFEC IAW DC8 NDT SPM 06-10-01.001. CRACK FOUND; REMOVED SPLICE FITTING AND REC'D NEW SPLICE LONGERON, LOCATED AND DRILL HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE LONGERON IAW DC8 SRM 51-1-20D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 REMOVE AND REPLACE FWD LOWER SKIN AT STA 825, L36 IAW UPS EO DC8-5330- 8942. REMOVED AFT SECTION OF SKIN IAW UPS EO DC8-5330-8942. FABBED NEW -93 & -94 DOUBLERS AND FABBED -1 RT & LT DOUBLER IAW DAC DWG 5612627. ALODINED & PRIMED IAW DC8 SRM 51-1-8; CUT OUT SKIN, LOC & DRILL AND INSTALLED BELLY SKIN, -93, -94 DOUBLERS & -1 RT & LT SPLICE DOUBLERS ALL IAW UPS EO DC8-5330-8942, DC8 SRM 51-1-20D, 51-1-21, 51-3-0, 51-3-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20 D, AND DC8 MM 20-1400.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1545 STR 26R INSIDE AND OUTSIDE OF LONGERON HAS CORROSION. REMOVED DAMAGED SECTION IAW DC8 SRM 51-1-21. RECEIVED NEW LONGERON SECTION. LOCATED AND DRILLED NEW LONGERON SECTION AND SPLICE IAW DC8 SRM 51-1-24. INSTALLED LONGERON AND SPLICE IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1702 STR 28L CORRODED. REMOVED STR STA 1680-1740; REC'D NEW LONGERON, LOCATED AND DRILLED IAW DC 8 SRM 51-1-21 AND 51-1-20D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8; REC'D NEW LONG SPLICE LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, FAB STRAPS IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONG SPLICE AND STRAPS IAW DC8 SRM 51-1-21, 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK DAMAGED AT STA 319 LBL 24 DOT A5804. BLEND CORROSION IAW DC8 SRM 51-1-8; OUT OF LIMITS IAW DC8 SRM 53-2-3; ROUTED OUT SEAT TRACK IAW DC8 SRM 53-2-3 FIG D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW UPS DC8 SRM 53-2-3 THEN REINSTALLED FLOORBOARD IAW UPS DC8 SRM 51-3-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1580 LBL B7 FLOORBEAM HAS CORROSION DOT (A5 619). REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED ANGLE REPAIR IAW DAC TR 53-124, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FLOORBOARD IAW DC8 SRM 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT ACCESSORY COMPT STA 1560 STR 33L CRACKED. REMOVED LONGERON SECTION FS 1490-1550, REC'D NEW LONG LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REMOVED 2EA LONG SPLICES, FOUND CRACKS REC'D NEW LONG SPLICES, LOCATED AND DRILLED IAW DC8 SRM 51-1-20D. INSTALLED LONG AND SPLICES IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 LONGERON 8L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED SERVICEABLE FITTING IAW DC8 SRM 51-1-20D, AND DC8 MM 20-14-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 IN CABIN AT FWD SIDE OF STA 680 L8R END FITTING IS CRACKED. REMOVED CRACKED LONGERON END FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AIR COND COMPT FS 24-36 L24R IS CORRODED. REMOVED CORROSION FROM L24R IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2- 0; MAT ID 2597242-3 LONGERON PO 439263.1. LOCATED AND DRILLED LONGERON IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON, END FITTINGS, STIFFENERS, INTERCOSTALS, AND DUCT CLAMP BRACKET IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20D, AND 51-1-21A.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, MAIN CABIN FS 1220 SEAT TRACK -E- GOUGED ON SCALLOPS. BLENDED GOUGED AREA IAW DC8 SRM 53-2-0. OUT OF LIMITS IAW DC8 SRM 53- 2-3. REMOVED SEAT TRACK STA 1180-1280. RECEIVED NEW SEAT TRACK AND FITTING. CUT AND DRILLED SEAT TRACK AND FITTING IAW UPS EO DC8-5320-5167-C. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK AND FLOORBOARDS IAW DC8 SRM 51-3-0 AND UPS EO DC8-5320-5167-C.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 980 BULKHEAD LWR ATTACH ANGLE CRACKED ABOVE LONG 36. REMOVED ANGLE IAW DC8 SRM 51-1-20D & 51-3-0. REMOVED & REINSTALLED INTERCOSTAL STA 1000-980, 2 GUSSET AND 2 CLIPS, ATTACH ANGLE EXT FUSELAGE IAW DC8 SRM 51-1-20D, 51-1-21 & 51-3-0. REC'D, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW DC8 SRM 51-1-20D, 51-3-0, AND 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1200 BETWEEN L33R-34R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0; REMOVED DAMAGED FITTING, REC'D, LOCATED, AND DRILLED UP FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 KEELBEAM FS 856 (AS SEEN FROM LT ANTENNA PNL AREA) FITTING HAS VERTICAL CRACK IN RADIUS. REMOVED CRACKED FITTING, INSTALLED NEW FITTING, LOCATED DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20 AND 51-3-1. LEAK CHECK TO BE ACCOMPLISHED ON UPS TC 8000, ITEM 14. INSTALLED HYD LINES IAW DC8 MM 20-12-01. LEAK CHECK GOOD IAW DC8 MM 20-12-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1160 AT L33R INSIDE CROSS SLIDE DOOR TORQUE BOX BANANA FITTING IS CRACKED. REMOVED CORSS SLIDE DOOR TRACK TO FOM IAW DC8 SRM 51-3-0. REMOVED BANANA FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. REC'D LOCATED, AND DRILLED UP FITTING 3755847-2 IAW DC8 SRM 51-1-24, INSTALLED FITTING AND CROSS SLIDE DOOR TRACK IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1180 AT L33R Z-FITTING AND DOUBLER IS CRACKED. REMOVED Z-FITTING IAW DC8 SRM 51-1-20D, REC'D, LOCATED, AND DRILLED UP FITTING, REPAIR ANGLES, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 26.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 AT L33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGED FITTING IAW DC8 SRM 51-1-20D, REC'D, LOCATED AND DRILLED UP FITTING IAW DC8 SRM 53-2-0 FIG 2G, AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2G.

Part: SKIN — CORRODED (WING) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, FWD UPPER LT W/W AT STA 857-000 UPPER SPAR CAP AND PLATING HAVE CORROSION BULGING AREA LBL 46. REMOVED CORROSION; (ORIG .270, REM .141) OUT OF LIMITS. FABRICATED REPAIR FILLER, DOUBLER, TRIPLER, PRESSURE PANEL ASSEMBLY DOUBLER, SHIMS, PANEL (P/N 5646674-25), FLOOR SUPPORT ANGLE SPLICE; ALODINED & PRIMED; INSTALLED REPAIR PARTS; ALL IAW DC8 SRM 51-1-8, 57-2-0, AND TIMCO REO G09719.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT PIT AT STA 1050 STR 31R LONGERON SPLICE CRACKED. REMOVED LONGER SPLICE IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AFT PIT BETWEEN STA 1100 AND 1120 APPROX AT STR 33R INTERCOSTAL HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIG THICKNESS .090, REMAINING THICKNESS .030. REMOVED INTERCOSTAL INQ DC8 SRM 51-1-20D. FABRICATED INTERCOSTAL IAW DAC DWG 9754949, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-21 & 21-1-20D.

Part: FITTING — CRACKED (KEELBEAM) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, FITTING AT STA 902 IN RIGHT WHEEL WELL OVER KEELBEAM IS CRACKED. RECEIVED NEW PART P/N 3643758-503. LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-3-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, AIR CONDITIONING ACCESSORY COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION. RECEIVED NEW -5 AND -17, -19 SPLICES. HEAT TREATED, LOCATED, DRILLED FRAME SECTION AND SPLICES. ALODINED AND PRIMED, INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 53-2-0 TR 53-125, 51-1-8, TPS-1003 REV A, AND DAC DWG 5614160.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE: C1, AIR COND ACCESSORY COMPT AT FS 56 L31R IS CORRODED. REMOVED CORROSION (ORIG MAT'L .090 REM .068) OUT OF LIMITS; FORMED REPAIR ANGLE IAW REO G09728. DYE PEN INSP; NO CRACKS NOTED; HEAT TREATED; LOCATED AND DRILLED; ALODINED AND PRIMED; INSTALLED ANGLE; ALL IAW DC8 SRM 51-1-8, 53-3-1, 51-2-0, 53-2-0 REO G09728, OHM 15-3-5, TPS 1003 REV A, AND 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,474 hrs · 24,907 cycles

INSPECTION TYPE:C1 AIR COND ACCESSORY COMPT AT FS 56 ABOVE L24L FRAME CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION AT FS 56 LT FROM CUSP TO L26L, RECEIVED NEW - 5 FRAME SECTON AND SPLICES -17, -19; HEAT TREATED; LOCATED & DRILLED; ALODINED & PRIMED; INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 53-2-0 TR 53-125, 51-1-8, TPS 1003 REV A, AND DAC DWG 5614160.

Part: DUCT — OVERTEMP (A/C COMPT)

VERY STRONG ODOR OF FUEL IN COCKPIT THROUGH ENTIRE FLIGHT. RAN PACKS ON GROUND FOR 30 MINS, COULD NOT DETECT ANY KIND OF ODOR IN COCKPIT. SUSPECT ODOR DUE TO OVERTEMP OF DUCT, NO DEFECTS NOTED ON GROUND.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,302 hrs · 24,764 cycles

CORROSION FOUND IN LONGERON 31 STATION 1338 AFT PIT FLOOR PANEL TEMP. INSTALLED REPAIR LONGERON 31L AT FS 1350 IAW REO G09527.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE: ASV, LOWER BELLY SKIN CORROSION; LONGERON L31 STA 1338. TRANSFERRED TO NRC 547382 AT TCO.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS DO NOT ILLUMINATE. FOUND ON PREDEPARTURE CK. INSTALLED NEW BATTERY PACK OPS CK GOOD. OPS CK GOOD IAW M/M CH 33-50 -01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK.

Part: RIB — CRACKED (SPOILER) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT-OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-24 & REMOVED SPOILER ATTACH IAW DC8 SRM 51-1-20 D & 51-1-21 LOCATED & DRILLED NEW SPOILER ATTACH FITTING IAW DC8 SRM 51-1-24 INSTALLED NEW WEB T/E INTERCOSTAL, CLOSING INTERCOSTAL.

Part: WEB — CRACKED (SPOILER) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-20D & 51-1-21. LOCATED AND DRILLED NEW WEB IAW DC8 SRM 51-1-24. REMOVED SPOILER ATTACH FITTING IAW DC8 SRM 51-1-20D, 51-1-21. LOCATED DRILLED NEW SPOILER ATTACH FITTING IAW 51-1-24, INSTALLED.

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

INSPECTION TYPE:C2 L2 UPPER FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.

Part: PAN — CRACKED (CARGO DOOR) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 C PIT DOOR PAN CRACKED AT UPPER FWD CORNER NEAR GRAB HANDLE. REMOVED DOOR PAN SECTION P/N 57542060 -17 & REPLACED IT WITH NEW DOOR PAN SECTION IAW 51-1-8, 51-3-0, 51-1-21, 51-1-20D.

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

INSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L2 DOOR JAMB EXTERIOR UPPER L2 UPPER AFT CORNER. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R END FITTING IS CORRODED. RECD LOCATED DRILLER FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 AFT PIT FS 1220 C3 DOOR JAMB SHROUD SUPPORT FITTING IS CORRODED. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-3-0.

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

INSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R IS CORRODED.

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

INSPECTION TYPE:C2 AFT PIT CORROSION FS 1060 ON L35L AT FRAME INTERSECT, LONGERON SPLICE FITTING FOUND TO BE CRACKED.

Part: PAN — CRACKED (CARGO DOOR) · airframe 73,897 hrs · 24,342 cycles

INSPECTION TYPE:C2 C PIT DOOR FRAME CRACKED AT UPPER AFT CORNER NEAR GRAB HANDLE. INSTALLED NEW DOOR PAN IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20D, 51-1-21A.

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

INSPECTION TYPE:C2 AFT ACCY COMPT STA 1660 FLOORBEAM WEB IS CRACKED I/B OF PREVIOUS REPAIR AT RBL 37.

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

INSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L1 DOOR JAMB EXTERIOR UPPER FWD CORNER. REPAIRED AREA IAW REO G08505 AND UPS EO DC8-5330-15976-A.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

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

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 MM 33-5-00 1, OPS CHECKS GOOD.

Part: DUCT — LOOSE (LEFT PACK)

LOST CABIN PRESSURE ON CLIMB-OUT. FOUND 3 DUCTS PULLED APART ON LEFT PACK. RE ATTACHED DUCTS AND SECURED. OPS CHECKS OK.

Part: FLOORBEAM — CORRODED (BS 920)

INSPECTION TYPE:C123, CORROSION ON SKIN AT FS 920L BELOW CUSP OVERWING CABIN AREA. REPLACED CORRODED SECTION OF FLOORBEAM WITH NEW IAW REO G-07058.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE:C123 FWD CARGO DOOR HAS CUT IN FRAME AT LOWER CTR EDGE. REMOVED DAMAGED AREA, FABRICATED DOUBLER IAW DC8 SRM 52-2-0. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.

Part: ANGLE — CRACKED (BS 70)

INSPECTION TYPE:C123, CUSP ANGLE AT STA 70 LEFT AT L1 DOOR IS CRACKED. FABRICATED DOUBLER IAW DC8 SRM 53-2-0. INSTALLED DOUBLER IAW DC8 SRM 53 -2-0. FABRICATED TITANIUM SPLICES AND INSTALLED IAW REO G-07097.

Part: SEAT TRACK — CORRODED (BS 1580 - 16805)

INSPECTION TYPE:C123, MAIN CABIN SEAT TRACK 'C' FS 1580-1680 IS CORRODED AND HAVE DOUBLE DRILLED HOLES. REMOVED CORROSION TRACK STA 1580-1680. DRILLED UP NEW TRACK IAW 2 DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-0 AND 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 560 - 580)

INSPECTION TYPE:C123 STATION 580 TO 560L SEAT TRACK A HAS CORROSION ON LOWER FLANGE. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2 -3. REMOVED SEAT TRACK A FROM 500-580. P/N 2772660-13500, HAT SPLICE, SPO U57799 TAG NR 00349073. LOCATED, DRILLED AND DEBURRED HOLES IAW DC8 SRM 51-3-0. ALODINE AND PRIME IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0.

Part: SKIN — CRACKED (DOOR JAMB)

INSPECTION TYPE:C123 AFT LOWER SKIN AT L-1 ENTRY DOORIS CRACKED. REMOVED DAMAGE SECTION OF SKIN. FABRICATED DOUBLERS AND FILLER IAW DC8 SRM 53-2-0. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 53-2-0.

Part: FLOOR PANEL — CORRODED (CABIN)

INSPECTION TYPE:C123 STATION 350 BL 29L FLOOR PANEL HAS CORROSION. REPLACED SECTION OF FLOORBOARD IAW DC8 SRM 51-3-0.

Part: FLOORBEAM — CORRODED (BS 1722 - 1726)

INSPECTION TYPE:C123 MAIN CABIN, FLOOR SUPPORT HAS CORROSION ON UPPER AND LOWER SURFACE AT STA 1722-1726.5, LBL 18..5-21. REMOVED CORROSION FROM FLOOR SUPPORTS IAW DC8 SRM 51-1-8. MAT REMOVAL OUT OF LIMITS IAW DC8 SRM 53-2-0, MAT ID FOR NEW SUPPORT 52912399 EXTRUSION IAW DC8 SRM 53-7-1. FABRICATED NEW SUPPORT, FILLER AND DOUBLERS FOR ATTCHING SUPPORT IAW DC8 SRM 53-2-0 AND DAC DWG 5755032. INSTALL FILLER, DOUBLERS AND SUPPORTS IAW DC8 SRM 51-3-0, 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 920 - 940)

INSPECTION TYPE:C123 POPPED RIVETS AND CORROSION BETWEEN FINGER DOUBLER RT CUSP FROM STA 9 20-940 OVERWING CABIN AREA. REMOVED CRACKED FITTING, CORRODED DOUBLERS, CUT OUT DAMAGED AND CORRODED PRESSURE PLATE. FABBED FILLER AND DOUBLER IAW REO G07022. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER, DOUBLERS, STIFFENERS AND ATTACH FITTING IAW DC8 SRM 51-1-20D AND 51-1-21. FLIGHT CONTROLS WILL BE REINSTALLED ON N/R 20431.

Part: FITTING — CORRODED (BS 1660)

INSPECTION TYPE:C123, FLOORBEAM END FITTING AT FS 1660 LT HAD INTERGRANULAR CORROSION. FABBED NEW FLOORBEAM END FITTING IAW REO G-07103 AND INSTALLED IAW R EO G-07103 & DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 960)

INSPECTION TYPE:C123 CABIN STA 960 SEAT TRACK PLANK AT RBL 48 CORRODED THROUGH. CUTOUT DAMAGED SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3. FABRICATED SPLICES IAW DC8 53-2-3. TRIMMED NEW SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 53-2-3 AND 51-3-0.

Part: FITTING — CRACKED (RT MLG WW)

INSPECTION TYPE:C123, AT RT WHEEL WELL, WING TO FVS FAIRING, VERTICAL SUPPORT FITTING CRACKED. FOR FABRICATION OF NEW VERTICAL SUPPORT FITTING SEE TIMCO PRINTED OP ERATION 50017. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0. TORQUED O/B SKI FITTING BOLT IAW DC8 SRM 51-3-1. INSTALLED UPPER TRUNNION PANEL IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1440 - 1540)

INSPECTION TYPE:C123, MAIN CABIN SEAT TRACK 'F' STA 1440-1540 HAD CORROSION ON BOTTOM. REMOVED FLOORBOARD SEAT TRACK. DRILLED SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK, SPLICES AND FLOORBOARD IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE:C123 RT WHEEL WELL BATH TUB FTG AT STA 920 IS CRACKED. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FLOORBEAM — CORRODED (BS 1660)

INSPECTION TYPE:C123 FLOORBEAM FS 1660 INBD AFT ENTRY DOOR HAS CORROSION. FABRICATED REPAIR ANGLE AND FILLER IAW REO G07052. INSTALLED REPAIR IAW REO G-07052 AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C123, AFT PIT FITTING LOCATED AT FS 1240 L35L CRACK. REMOVED AND REPLACED FITTING AT FS 1240 L35L AFTER ALODINING HOLES IAW DC8 SRM 51-1-8, 51-1-20D & 51-1-24.

Part: DOUBLER — CRACKED (LE FLAP)

INSPECTION TYPE:C123, R/W CTR L/E BOTTOM I/B INTERIOR DRAIN HOLE CRACKED. SRM DOUBLER REPAIR, FABRICATED REPAIR PARTS AND INSTALLED IAW DC8 SRM 57-2-0 & 51-1-21.

Part: FRAME — CORRODED (BS 1240)

INSPECTION TYPE:C123, AFT PIT FS 1240 FRAME SECTION CORRODED ABOVE L36-R. FABRICATED AND INSTALLED NEW FRAME SECTION, SPLICES, FILLER AND STRAPS IAW TIMCO REO NR G-07098 REV A. HEAT TREAT 7075-0 .080 MAT'L AFTER FORMING TO 7075-T6 IAW TPSICO3 REV A.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C123 LEFT WING CTR L/E SECTION IB END UPPER RIB CRACK ON INTERIOR. STOP DRILLED CRACKED RIB VERIFICATION OF REPAIR IAW 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALL REPAIR PER SRM 57-2-0 AND 51-1-2 0.

Part: PLUG — WORN (BS 1410)

INSPECTION TYPE:C123 STA 1410 TRACK C PLUG WORN.. REMOVED AND REPLACED PLUG IAW DC8 SRM 51-3-0.

Part: SKIN — CRACKED (RUDDER)

INSPECTION TYPE:C123 RUDDER AFT UPPER TRAILING EDGE HAS A CRACK. REPAIRED CRACKED RUDDER T/E BY REMOVING CRACKED, PAINT AND APPLYING A RESIN OVERLAY TO PROTECT EXPOSED GLASS AND PRIMED IAW DC8 SRM 51-1-19 AND 51-1-8.

Part: RIB — CRACKED (WS 300)

INSPECTION TYPE:C123, LEFT WING LEADING EDGE SECTION, LOWER RIB PREVIOUS REPAIR CRACKED STA XW 300 DOT D973 PARTS RACK. FABBED REPAIR ANGLE FROM 7075-T6511, FILLERS FROM 7075-T6 IAW DC8 SRM 57-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.

Part: RIB — CRACKED (ELEVATOR)

INSPECTION TYPE:C123, RT ELEVATOR I/B FWD VERTICAL RIB HAD CRACK, STA XE-28.843. FABBED DOUBLED PER DAC DWG 5655942. ALODINED AND PRIMED PER 51-1-8. INSTALLED DOUBLED PER DC8 SRM 53-1-21.

Part: STIFFNER — CRACKED (BS 420)

INSPECTION TYPE:C123, FWD PIT STA 420, L26R TO L28R, FRAME REINFORCEMENT CHANNEL UPPER FLANGE CRACKED. REMOVED REINFORCEMENT CHANNEL IAW DC8 SRM 51-1-21, MATERIAL ID 7075- 0 1.071 PO NR 294242 IAW DC8 DWG 3773159. HEAT TREATED SUPPORT TO 7075 T6 IAW DC8 SRM 51-1-1. FAB NEW SUPPORT IAW DC8 DWG 3773159. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SUPPORT IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C123, ANGLE CRACKED AT STA 857 STR 19R IN MAIN CABIN. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. CRACKED ANGLE IS THE FITTING.

Part: STRINGER — CRACKED (WS 74)

INSPECTION TYPE:C123, RIGHT WING-INTERNAL FUEL TANK NR 3 MAIN-FITTING AT XRS 74-STRINGER 51 HAS CRACKS AS MARKED. REMOVED FITTING, LOCATED AND DRILLED NEW FITTING (P/N 3704841-2), IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D & 51-3-0, SEALED IAW DC8 SRM 51-1-12.

Part: FITTING — CRACKED (BS 699)

INSPECTION TYPE:C123, CABIN STA 699 ABOVE L19R FITTING AT INTERCOSTAL LWR SIDE I/B FLANGE CRACKED DOT B878 REM FITTING. RECEIVED FITTING MOR NR 421433 (P/N 3779978-1). LOCATED AND DRILLED. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: STRINGER — CRACKED (WS 74)

INSPECTION TYPE:C123 IN NR 2 MAIN TANK ACCESS 505F JUST I/B OF XRS 74 STRINGER 51 END FITTING WAS CRACKED. REMOVED CRACKED FITTING, REV'D NEW FITTING (P/N 3704841-1), LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0, SEALED IAW DC8 SRM 51- 1-12.

Part: FLOORBEAM — CORRODED (BS 1723-1726)

INSPECTION TYPE:C123, REMOVED AND REPLACED FLOORBEAM DUE TO CORROSION BEING OUT OF LIMITS. FABRICATED NEW FLOORBEAM AND INSTALLED TO DC8 SRM 51-2-0.

Part: SKIN — CRACKED (PAX DOOR)

INSPECTION TYPE:C123, LT FWD ENTRY DOOR. BOTTOM AFT OUTER SKIN CRACKED. FABRICATED REPAIR DOUBLERS IAW DC8 SRM 52-2-0. INSTALLED DOUBLERS IAW DC8 SRM 51-1-21.

Part: FLOORBEAM — CORRODED (BS 1700 - 1708)

INSPECTION TYPE:C123, MAIN CABIN, CORROSION ON FLOOR SUPPORT AT FS 1700-1708 RBL 9.5-11.5. FABBED NEW PART IAW DC8 SRM 51-2-0 AND 51-1-8.

Part: CUSP — CRACKED (BS 1055)

INSPECTION TYPE:C123, RT CABIN AT FS 1055 CRACK IN CUSP. REPAIRED PER REO G07010.

Part: TORQUE BOX — CRACKED (BS 68)

INSPECTION TYPE:C123 CABIN STA 68 L13L, L1 DOOR TORQUE BOX INNER PANEL HAS CRACK AND EDGE DRILLED AT TOP OF LIGHTENING HOLE. SPLICED IN A REPLACEMENT SEGMENT OF THE 5597646-111 INNER SKIN PER DC8 SRM 53-2-0, FIG 23.

Part: FLOORBEAM — CORRODED (BS 1746)

INSPECTION TYPE:C123, MAIN CARGO FLOOR SUPPORT HAD CORROSION ON UPPER AND LOWER SURFACES FS 1746 LBL 1-31. REMOVED CORROSION ON FLOOR SUPPORT IAW DC8 SRM 51-1-8 (OUT OF LIMITS ). REMOVED FLOOR SUPPORT IAW DC8 SRM 51-3-0. FABRICATED AND INSTALLED IAW DC8 DAC DWG 5755032.

Part: LONGERON — CORRODED (BS 41)

INSPECTION TYPE:C123 NOSE WHEEL WELL AREA INSIDE LT NOSE WHEEL WELL TUNNEL, AT STA -41 (APPROX) FRAME TO LONGERON AND ATTACH CLIP HAS CORROSION RUNNING BEHIND CLIP AND ON LONGERON. (DOT B294) REMOVED CORROSION IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DC8 SRM 51-1-20D.

Part: WEB — CRACKED (BS 150)

INSPECTION TYPE:C123, STA 150 WEB ON FWD SIDE OF RT SERVICE DOOR CRACKED AT LIGHTING HOLE. FAB NEW WEB IAW DAC DWG 5615700. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTL IAW DC8 SRM 51-3-0.

Part: KEELBEAM — CORRODED (BS 1000)

INSPECTION TYPE:C123 CORROSION ON KEEL BEAM AT BOLTS FS 1000 AFT OF BOTTOM ROTATING BEACON. REMOVED BOLTS, REMOVED CORROSION. CORROSION FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED KEEL BEAM AREA AFT OF BOTTOM ROTATING BEACON IAW DC8 SRM 51-1-8. INSTALLED BOLTS IAW DC8 SRM 51-3-0.

Part: BULKHEAD — CRACKED (NLG WW)

INSPECTION TYPE:C123 ATTACH ANGLE CRACKED AT LOWER LT CORNER AT BULKHEAD AT FWD OF NLG C OMPARTMENT PANEL 601. REPAIRED AS PER SRM 53-2-0.

Part: FITTING — CRACKED (RT MLG WW)

INSPECTION TYPE:C123, IN RT WHEEL WELL L24R WAS CRACKED. PERFORMED HFEC IAW DC8 SRM 06-10-4-0012, CRACKS FOUND. REMOVED LONG 24R AND ASSOCIATED HARDWARE AND PARTS IAW DC8 MM 32-31-04, 20-13-0, 32-31- 03 AND UPS R/AA DC8-53-2747. INSTALLED NEW PART IAW SAME AND TIMCO JOB CARD 90453100/FORM TWC100.

Part: SKIN — CORRODED (BS 158 - 170)

INSPECTION TYPE:C123 FS 158 - FS 170 LONG 32R SKIN BULGING AT FASTENERS. REMOVED DAMAGED SECTION OF LONGERON AND SKIN IAW DC8 SRM 53-2-2 AND 53-2 -2, FABRICATED AND LOCATED, DRILLED, COUNTERSUNK, DEBURRED REPAIR PARTS FILLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1. ALODINE AND PRIME IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-2 AND 53-2-1.

Part: UNKNOWN — SMOKE (COCKPIT)

INSPECTION TYPE:N/A, DURING PREFLIGHT INSPECTION CREW REPORTED SMOKE IN COCKPIT.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: DOUBLER — CORRODED (BS 1620)

INSPECTION TYPE:SV, CORROSION BETWEEN SKIN AND DOUBLER FS 1620 L26R DOT E253. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW UPS DC8 SRM 53-4 -1, 53-2-1 FIG 7, 51-120D.

Part: FLOORBEAM — CRACKED (BS 1600 & 1620)

INSPECTION TYPE:N/A, FOUND FLOORBEAM CRACKS AT STA 1600 AND 1620. *S/D* REPAIR COMPLETED ON FLOORBEAM.

Part: FLOORBEAM — CRACKED (BS 1600)

INSPECTION TYPE:C123, CORROSION FLOORBEAM FS 1600 RT. REPAIRED IAW REO-06679, INSTALLED IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (NR 2 PYLON)

INSPECTION TYPE:N/A ON POST FLIGHT, ENGINEER AND MECHANIC VERIFIED A SMALL CRACK ON NR 2 PYLON. ACCOMPLISHED EO DC8-5430-11626-A APPENDIX B INTERIM REPAIR NR 2 PYLON OUTBOARD RAMP AT THE ENGINE FAN EXHAUST OUTLET. TRANSFERRED TO DMI LIST C/N D-175661 ASSIGNED.

Part: CONNECTOR — LOOSE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT DISARM LIGHT WILL NOT ILLUMINATE. REPLACED BULB TWICE AND STILL INOP. RESEATED CANNON PLUG AND RE-LAMPED, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMER LIGHTS DISARM CHECK INOP REF 120346 HISTORY. REMOVED AND REPLACED BATTERY PACK, OPS CK GOOD.

Part: WIRE — LOOSE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. TIGHTENED LOOSE WIRE ON EMERGENCY DISARM LIGHT SOCKET, OP'S CK GOOD. LIGHT ON WITH SWTICH IN DISARM POS.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PRFL, EEL FAILED CHECK ON PRE-FLIGHT. REMOVED AND REPLACED EMERGENCY BATT PACK.

Part: WIRE — BROKEN (CABIN)

NO LIGHT ON AFTER EMER EXIT LIGHTS DISARMED. SEE PREVIOUS WRITE UP P 294088. RECONNECTED BROKEN WIRE AT CONNECTOR P1-1345 PINS 7 AND 11 AT BATTERY PACK. OPS CK SYS NORMAL.

Part: SOLENOID VALVE — LEAKING (CARGO DOOR)

INSPECTION TYPE-N/A BLOCK TURNBACK, CREW HAD SMOKE IN COCKPIT. FOUND HYD LEAK IN LWR E & E, SUSPECT MAIN CARGO DOOR CONTROL VALVE HYD SUPPLY LINE. FOUND UPPER CARGO DOOR SOLENOID VALVE TO BE LEAKING ONTO PNUEMATIC DUCT. REMOVED AND REPLACED FWD UPPER CARGO DOOR SOLENOID SOV PER MM 52-36-00.

Part: ANGLE — CORRODED (WS 408)

INSPECTION TYPE-C, RT WING T/E SPAR AT XW 408 LOWER SPLICE ANGLE IS EXFOLIATED. REMOVED AND REPLACED SPLICE ANGLE IAW SRM 51-3-0.

Part: SUPPORT — CORRODED (BS 1040-1060)

INSPECTION TYPE-C, FS 1040 TO 1060 ABOVE STR 33R FLOOR SUPPORT ANGLE HAS CORROSION REMOVAL WENT OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 53-11-0 AND 51-1-21.

Part: FITTING — CORRODED (BS 8 RT)

INSPECTION TYPE-C, LONG 33R FITTING FS 8 CORROSION REMOVAL BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: TIE FITTING — CRACKED (BS 1232)

INSPECTION TYPE-C, FS 1232 AT STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-C, FS 440 TO 460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (NR 1 CARGO COMPT)

INSPECTION TYPE-C, NR 1 PIT AFT LWR T-BOLT STOP FITTING IS CRACKED ON THE LWR LEG. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE-C, MAIN CARGO DECK UPPER SURFACE WING CTR SECTION FS 781 RBL 62 CORROSION BETWEEN 2 FASTENERS AND CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-C, FS 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE-C, FS 600 TO 620 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORROSION (BS 274)

INSPECTION TYPE-C, LONGERON END FITTING AT FS 274 STR 31R HAS HEAVY CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-210D.

Part: SHEAR TIE — CORRODED (BS 300)

INSPECTION TYPE-C, SHEAR TIE FITTING AT FS 300 LONG 30L HAS MODERATE CORROSION AROUND FASTENERS. REMOVED AND REPLACED SHEAR TIE FITTING IAW SRM 53-2-0.

Part: SEAT TRACK — CORRODED (BS 260)

INSPECTION TYPE:C F/S 260 RBL 48 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM ADDM DC8-5320-8309.

Part: SEAT TRACK — CORRODED (BS 1024)

INSPECTION TYPE:C F/S 1024 LBL 59 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM ADDN DC8-5320-5167-C.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-C, LONGERON 33R END FITTING AFT SIDE OF FS 70 IS EXFOLIATED (HEAVY CORROSION). REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 628.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 628.750 THE L/E UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 635.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 678.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 678.750 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE:C, RT WING L/E AT STR XFS 653.750, THE L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 THE UPPER L/E RIB HAS A 2 INCH CRACK AT MID SPAN. REPAIRED IAW SRM 57-2-0.

Part: SEAT TRACK — CORRODED (BS 1207)

INSPECTION TYPE:C F/S 1207 LBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-7-2.

Part: BULKHEAD ANGLE — CORRODED (BS 70)

INSPECTION TYPE:C AFT SIDE OF F/S 70 O/B OF 33R LOWER BULKHEAD L ANGLE HAS HEAVY CORROSION AROUND BOLT AND BETWEEN IT AND LONGERON FITTING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD IAW SRM 53-2-5 51-1-20D, AND DWG 5613064.

Part: WEB — CRACKED (L-1 DOOR)

INSPECTION TYPE-C, MAIN ENTRY DOOR LWR AFT WEB IS BENT AND CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-3-2.

Part: DOUBLER — CORRODED (BS 35-55)

INSPECTION TYPE-C, HEAVY CORROSION BETWEEN INTERNAL DOUBLER AND SKIN AT LONGERON 31R AND BETWEEN FS 35 AND 55. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 53-3-1 AND 51-1-21.

Part: LONGERON — CORRODED (WS 35-55)

INSPECTION TYPE-C, LONGERON 30R FS 35 TO 55 HAS HEAVY CORROSION AND OUT OF LIMITS. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE-C, LONGERON 34R FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE-C, NR 1 PIT AT STA 600 TO 620 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 822.500. REPAIRED IAW SRM 57-2-0.

Part: FRAME — CRACKED (L-1 DOOR)

INSPECTION TYPE-C, MAIN ENTRY DOOR LWR FRAME HAS A CRACK AND DEEP GOUGE. REPAIRED CRACKED FRAME IAW SRM 52-2-0 FIG 2.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE:C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA 772.500. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 8 LT)

INSPECTION TYPE-C, LONGERON 33L FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 572.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 572.500. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CORRODED (BS 35-55)

INSPECTION TYPE-C, INTERNAL DOUBLER HAS HEAVY CORROSION O/B OF LONGERON 30R BETWEEN FS 35 TO 55. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5649028 AND SRM 51-1-20.

Part: INTERCOSTAL — CRACKED (PAX DOOR)

INSPECTION TYPE-C, MAIN ENTRY DOOR INTERCOSTAL HAS CRACK IN THE RADIUS AS VIEWED THRU UPPER FWD LIGHTENING HOLE. REPAIRED IAW SRM 52-3-2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 635.000. REPAIRED IAW SRM 57-2-0.

Part: SHEAR TIE — CRACKED (BS 641)

INSPECTION TYPE-C, STA 641 BETWEEN STR 26R TO 27R, SHEAR TIE HAS A 2 INCH CRACK. REMOVED FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 53-4-1 FIG 40 AND DWG 5750837.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ON W/E CK EMERG EXIT LTS FAILED TO TEST. SWITCH FOUND TO BE LEFT ON OVER EXTENDED LAYOVER. REMOVED AND REPLACED EMERG EXITS LTS BATT PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERG EXIT LIGHT DIM WHEN TESTED. SHELF LIFE ON NEW ASSY DUE 7\28. ALSO, DIM WHEN TESTED AOG BATTERY RACK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERG EXIT LIGHT INOP. TIGHTENED OVERHEAD PANEL RECEPTACLE R5-26, OPS CHK SYS NORMAL IAW MM 33-50-02 PG 204-205.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERG LT INOP. REPLACED EMERG BATTERY PACK AND CONTROL RELAY ASSY.

Part: END FITTING — CRACKED (NR 2 ALT TANK)

INSPECTION TYPE: C. STRINGER END FITTING CRACKED ON LOWER AFT STRINGER INSIDE NR 2 ALT TANK AT STA 74. REMOVED CRACKED FITTING, INSTALLED NEW FITTING IAW DC8 SRM 51-1-21D.

Part: LATCH — BROKEN (ESCAPE SLIDE)

WHILE ON GROUND, MAINTENANCE FOUND LATCH FOR ESCAPE SLIDE BROKEN. REMOVED AND REPLACED ESCAPE SLIDE CONTAINER AND SECURED.

Part: BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN DISARM AND OFF DISARM, CHECK POSITION LIGHT WAS OFF, IT SHOULD BE ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY AND LIGHT DIMING RELAY RS-60.

Part: BATTERY PACK — DISCHARGED (CABIN)

WHILE ON THE GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN DISARM AND OFF DISARM/CHECK POSITION LIGHT WAS OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSEMBLY AND LIGHT DIMING RELAY.

Part: RELIEF VALVE — LEAKING (HYD SYST)

PILOT REPORTED, HYD FLUID LOSS. PRESSURE AFTER LANDING, AIR BRAKES WERE USED. AUX PUMP PRODUCED NO PRESSURE, BUT FLUID QUANTITY DECREASED. FOUND RT GEAR BOGIE UNLOCK PRESS RELIEF VALVE LEAKING. CAPPED OFF BOGIE UNLOCK CYLINDER HYD LINES AT STRUT MANIFOLD. PLACED ON MEL 32-6 ON M97762, LEAKING RELIEF VALVE REMOVED.

Part: STIFFENER — CORRODED (FS 120)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON RT VERTICAL STIFFENER AT STA 120, LONGERON 22R-27R. REPLACED STIFFENER PER SRM 51-1-20.

Part: SEAT TRACK — CORRODED (FS 1685-1700)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON NR 5 SEAT TRACK AT FS 1685-1700. REPLACED SEAT TRACK PER SRM 53-2-3.

Part: LONGERON — CORRODED (FS 1698)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON LONGERON 30L, FS 1698. REPAIRED LONGERON PER SRM 51-1-20, 53-2-0.

Part: FRAME — CORRODED (FS 1140)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON BELTFRAME CAP AT FS 1140, LONGERON 31R-31L. REPLACED CAP PER SRM 51-1-21.

Part: FRAME — CORRODED (FS 1140)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON BELTFRAME AT FS 1140, LONGERON 33L-35R. REPLACED FRAME PER SRM 51-1-20.

Part: DOUBLER — CORRODED (FS 1332-1335)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON GUSSET DOUBLER AT FS 1332-1335, LONGERON 33R. REPLACED DOUBLER PER SRM 51-1-20.

Part: LONGERON — CORRODED (FS 1360-1380)

DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 36 CORRODED AT FS 1360-1380. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6637A.

Part: LONGERON — CRACKED (FS 860-880)

DURING 'C' CHECK, MAINTENANCE REPORTED RT WHEEL WELL LONGERON 24R CRACKED AT FS 860-880. REPAIRED PER UPS EO DC8-5310-6636A.

Part: DOUBLER — CORRODED (FS 220-260)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON INNER DOUBLER AT FS 220-260, LONGERON 35L-30R. REPLACED DOUBLER PER SRM 51-1-20.

Part: FITTING — CORRODED (FS 920)

DURING 'C' CHECK, MAINTENANCE REPORTED VERTICAL ATTACH FITTING CORRODED AT STA 920, LBL 1. REPLACED FITTING PER SRM 51-1-20.

Part: FLOOR BEAM — CORRODED (FS 55)

DURING 'C' CHECK, MAINTENANCE REPORTED FLOOR BEAM CORRODED AT FS 55, RBL 12. REPAIRED PER UPS EO DC8-5310-6638A.

Part: DOUBLER — CORRODED (FS 960-980)

DURING 'C' CHECK, MAINTENANCE REPORTED DOUBLER CORRODED AT FS 960-980, UPPER SURFACE OF WHEEL WELL, RBL 69. REPLACED DOUBLER PER SRM 51-1-20D.

Part: FLOOR BEAM — CORRODED (FS 1725)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION AT FLOOR BEAM AT FS 1725, RBL 24. REPAIRED BEAM PER UPS EO DC8-5310-6604A.

Part: DOUBLER — CORRODED (FS 857-879)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON DOUBLER AT FS 857-879, LBL 5, RBL 5. REPLACED DOUBLER PER SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 1660-1680)

DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN DOUBLER AT FS 1660-1680, LONGERON 27L-28L. REPAIRED DOUBLER PER SRM 51-1-20.

Part: FITTING — CORRODED (FS 1265)

DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 36 SPLICE FITTING CORRODED AT FS 1265. REPLACED FITTING PER SRM 51-1-20.

Part: LONGERON — CRACKED (FS 55)

DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 24L CRACKED AT FS 865 AND AT FS 895. REPLACED LONGERON PER SRM 51-1-20D.

Part: LONGERON — CRACK (FS 220)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 35R I/B SIDE CRACKED AT FS 220. INSTALLED REPAIR IAW SRM 53-2-2.

Part: BELTFRAME — CRACK (FS 1580)

DURING 'C' CHECK MAINTENANCE FOUND FS 1580 LONGERON 21R BELTFRAME CRACKED. INSTALLED REPAIR IAW SRM 53-2-0, FIG. 3.

Part: END FITTING — CRACKED (FS 700)

DURING 'C' CHECK MAINTENANCE FOUND BELTFRAME END FITTING CRACKED 1 INCH LONG AT FS 700 LONGERON 21L. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: ANGLE — CRACK (NR 1 PYLON)

DURING 'C' CHECK MAINTENANCE FOUND NR 1 PYLON OUTBOARD ATTACHMENT ANGLE CRACKED. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: TRACKS — CORROSION (RT TE FLAPS)

DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 410. INSTALLED REPAIR IAW MM 27-51-03.

Part: FRAME — CRACKED (FS 1580)

DURING 'C' CHECK MAINTENANCE FOUND BELT FRAME HAS 2 INCH LONG CRACK AT FS 1580, LONGERON 21L. INSTALLED REPAIR IAW SRM 53-2-0.

Part: TRACKS — CORROSION (RT TE FLAPS)

DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 3. INSTALLED REPAIR IAW MM 27-51-03.

Part: SKIN — CRACK (RT WING)

DURING 'C' CHECK MAINTENANCE FOUND 3 INCH LONG CRACK ON RT WING LEADING EDGE SKIN AT STA XFS 182.5 LOWER SURFACE. INSTALLED REPAIR IAW SRM 57-2-0.

Part: FRAME — CORROSION (FS 1890)

DURING 'C' CHECK MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON AFT SIDE OF FRAME WEB, LONGERON 36, FS 1890. INSTALLED REPAIR IAW UPS EO DC8-53-1320.

Part: FRAME — CRACKED (A X-SLIDE)

DURING 'C' CHECK MAINTENANCE FOUND "A" X-SLIDE FLOOR FRAME CRACKED 2 EACH PLACES INSIDE UPPER LIGHTING HOLE BETWEEN 5 AND 6 T-HOOKS. INSTALLED REPAIR IAW SRM 52-2-2, FIGURE 2.

Part: LONGERON — CRACK (FS 1227)

DURING 'C' CHECK MAINTENANCE FOUND FS 1227, LONGERON 19R END FITTING CRACKED 1/2 INCH LONG. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: TRACKS — CORROSION (RT TE FLAPS)

DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 340. INSTALLED REPAIR IAW MM 27-51-03.

Part: ANGLE — CORROSION (FS 70)

DURING 'C' CHECK MAINTENANCE FOUND A/C COMPT. FS 70, LONGERON 31L ATTACH ANGLE HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-21.

Part: DOUBLER — CORROSION (FS 20)

DURING 'C' CHECK MAINTENANCE FOUND FLIGHT DECK SUBFLOOR FINGER DOUBLER HAS MODERATE CORROSION AT FS 20, LBL 62. INSTALLED REPAIR IAW SRM 51-1-21.

Part: SKIN — DELAMINATED (RT NR 2 SPOILER)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING NR 2 SPOILER DELAMINATED ON UPPER SURFACE. REPLACED SPOILER PANEL PER MM 27-60-01.

Part: LONGERON — CRACKED (FS 190 LON 35L)

DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 35L HAS 3 CRACKS AT O/B ENDS BETWEEN STA 190-390. REPLACED LONGERON PER SRM 51-1-20.

Part: LONGERON — CRACKED (FS 85-95)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 21L, STA 85-95 LIGHTENING HOLES 3 EACH WITH CRACKS ON WEB. INSTALLED REPAIR IAW SRM 51-1-21.

Part: VANE — DELAMINATION (NR 3 TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 3 FLAP VANE DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-51-14.

Part: SKIN — CRACKED (FS 380)

DURING 'C' CHECK, MAINTENANCE FOUND SKIN CRACKED AT FASTENER HOLE AT FS 380, BETWEEN LONGERONS 30L-29R. REPAIRED SKIN PER SRM 53-2-1.

Part: LONGERON — CRACKED (FS 75)

DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 32R CRACKED AT FS 75. REPAIRED LONGERON PER SRM 53-2-2.

Part: FITTING — CRACKED (FS 902)

DURING 'C' CHECK, MAINTENANCE FOUND LONGERON END FITTING CRACKED AT FS 902, LONG 16L. REPLACED FITTING PER SRM 51-1-20.

Part: FITTING — CRACKED (FS 781)

DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 34L END FITTING CRACKED AT FS 781. REPLACED FITTING PER SRM 51-1-20.

Part: LONGERON — CRACKED (FS 1750)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 13 RT, FS 1750 HAS 1.5 INCH CRACK. INSTALLED REPAIR IAW SRM 53-2-2.

Part: LONGERON — CRACKED (FS 25)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 12R AT FS 25 HAS 1 INCH CRACK. INSTALLED REPAIR IAW SRM 53-2-2.

Part: VANE — DELAMINATION (NR 1 TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 1 FLAP VANE DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-61-01.

Part: DOUBLER — CRACKED (FS 32)

DURING 'C' CHECK, MAINTENANCE FOUND RT AND LT HEAT EXCHANGER DOUBLER CUT OUT CRACKED ON AFT CORNER AT FS -32. REPAIRED PER UPS EO DC8-5330-4732.

Part: SKIN — CRACKED (RT AILERON)

DURING 'C' CHECK MAINTENANCE FOUND RT I/B AILERON LOWER SKIN HAS 2 EACH .25 INCH LONG CRACKS AT INBOARD EDGE. INSTALLED REPAIR IAW SRM 57-2-0.

Part: RIB — CRACKED (LT HORIZ STAB LE)

DURING 'C' CHECK, MAINTENANCE FOUND LEFT HORIZONTAL STAB I/B LEADING EDGE RIBS CRACKED, 1ST, 2ND, AND 3RD RIBS FROM INBOARD END. REPAIRED RIBS PER SRM 55-2-0.

Part: LONGERON — CRACKED (FS 130-390)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 35L AND 34R CRACKED AT FS 190-390. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: RIBS — CRACKED (LT WING)

DURING 'C' CHECK, MAINTENANCE FOUND LEFT WING LEADING EDGE RIBS CRACKED AT STATIONS XFS 313, 369, 622, 672, 790, 796 UPPER, AND XFS 790 LOWER. REPAIRED RIBS PER MM 57-00-00.

Part: LONGERON — CRACK (FS 220-255)

DURING 'C' CHECK MAINTENANCE FOUND LONGERON 36 I/B SIDE CRACKED AT FS 220-255 AND FS 220-360. INSTALLED REPAIR IAW SRM 51-1-20D.