N852UP

Part: RETAINER — BROKEN (ESCAPE SLIDE)

SLIDE CONTAINER IS OPEN. DEFERRED M385289 ASSIGNED. SLIDE CONTAINER RETAINER BROKEN DEFERRED MAIN ENTRY ESCAPE SLIDE PER MEL 52-7-4. SLIDE REMOVED AND ROUTED TO AMDC. COURIER SEATS NOT TO BE OCCUPIED. INSTALLED EVACUATION SLIDE PER AMM 25-60-01. PLACARDS REMOVED.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CORROSION ON FLOOR PANEL AT STA 580 AND RBL 24. REPAIRED CABIN FLOOR PANEL AT STA 580 AND RBL 24 IAW SRM 53-02-03 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 BROKEN FITTING IN FWD ACC COMPT STA 640 L35R-L36. FABRICATED AND REPLACED FITTING AT STA 640 AND L35R-L36 IAW DWG 3750 834, SRM 51-1-8, SRM 51-01-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 LOWER FLANGE OF SEAT TRACK EXTRUSION EXFOLIATED IN MAIN CABIN, STA 1455-1462 LBL 60. REPAIRED CABIN SEAT TRACK AT STA 1455-1462 LBL 60 IAW SRM 53-02-03-0, AND SRM 53-02-03-0 FIG 008A.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CORROSION ON SEAT TRACK AT STA 1470 LBL 45. FABRICATED AND REPLACED CABIN SEAT TRACK SECTION AT STA 1470 AND LBL 45 IAW SRM 51-03-00, SRM 51-03-02, SRM 51-03-01 AND SRM 51-1-8.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CABIN STA 1590 TO STA 1600 LBL 45 SEAT TRACK GOUGED. FABRICATED AND INSTALLED SEAT TRACK AT STA 1590 TO STA 1680 IAW DWG S-2400463, SRM 51-03-00, SRM 51-03-02, SRM 51-01-08, SRM 51-03-01, SRM 53-21-01-4.

Part: FITTING — CRACKED (WING) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 NR 1 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. REPLACED NR 1 ALT FRONT SPAR FITTING BETWEEN XRS 428 AND XRS 463 IAW DWG 3644046, SRM 51-03-02, SRM 51-01-08, SRM 51-01-20D AND SRM 51- 01-12.

Part: FITTING — CRACKED (SPAR) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 NR 4 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. FABRICATED AND INSTALLED FRONT SPAR FITTING IN NR 4 ALT XRS 428 TO XRS 463 IAW DWG 3644046 AND SRM 51-1-8 AND SRM 51-01-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 NR 2 MAIN THRU 560F AT XRS 23 1ST CLIP FROM R/S CRACKED. FABRICATED AND REPLACED NR 2 MAIN TANK CLIP AT XRS 23 IAW DWG 3755028, SRM 51-01-08, SRM 51-01-20D, SRM 51-03-01.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 COCKPIT, FE'S FWD SEAT TRACK HAS WORN SEAT LOCKPIN HOLES. REPAIRED FE'S FWD SET TRACK BY REPLACEMENT IAW SRM 51-01-24 AMD SRM 51-03-00.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 LT INBOARD FLAP STA 98 EXTERIOR SKIN REPAIR DOUBLER GOUGED. REPAIRED LT INBOARD FLAP STA 98 EXTERIOR SKIN REPAIR DOUBLER IAW SRA 51-1- 21A, SRM 57-07-01 FIG 001 AND SRM 51-3-2.

Part: FRAME — CRACKED (BS 100 L34L) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CRACK AT FWD CARGO PIT STA 100 LONG 34L. FRAME REPAIRED AT STA 100 AND L34L IAW EO DC8-5320-6176-6 AND SRM 51-1-8.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 VERT FIN TO FUSELAGE ATTACH ANGLE CRACKED AND CORRODED LT SIDE STA 1766. REPAIRED VERT FIN TO FUSELAGE ATTACH ANGLE IAW SRM 53-02-05-FIG 16A.

Part: DOUBLER — BULGED (LH WING) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 LT WING O/B UPPER AND LOWER SURFACE TE WEDGE DOUBLER HAS 2 UPPER FASTENERS PULLING THROUGH AND DOUBLER BULGED. REPAIRED L-WING O/B TE IAW SRM 57-02-00 FIG 002A, SRM 51-01-21A.

Part: LONGERON — CRACKED (BS 1750 L15L) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 AFT CABIN L15L CRACKED AT CANTED FRAME STA 1750. REPAIRED LONG 15L AND SPICE AT CANTED FRAME STA 1750 IAW SRM 53-02-02 FIG 10, SRM 51-1-24 AND SRM 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 AFT CABIN L15R CRACKED AT CANTED FRAME STA 1750. REPAIRED L15R AT STA 1750 CANTED FRAME IAW SRM 51-1-21, SRM 51-3-0, SRM 53-2-2 FIG 10, EO DC8-5320-28843-A AND EA 008-5320--01-A1314.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 AFT CABIN L14R CRACKED AT CANTED FRAME STA 1755. REPAIRED L14R AT STA 1755 CANTED FRAME IAW SRM 51-3-0, 53-2-2 FIG 10, 51-1-8, EO DC8-5320-28843A AND EA 008-5320-01-A1314.

Part: ANGLE — CRACKED (RUDDER) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 RUDDER L ANGLE CRACKED, JUST ABOVE LOWER HINGE CUT-OUT AT BALANCE WEIGHT. REPAIRED CRACKED L ANGLE BY FABRICATION AND INSTALLATION PER DWG 56562 26, SRM 51-3-0 AND SRM 51-1-21.

Part: FLOORBOARD — ELONGATED (BS 785-1000) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 RT STA 785-1000 FLOORBOARD F94A/F94B HAS SEVERAL ELONGATED FASTENER HOLES. REPAIRED RT F94A/F94B FLOORBOARD FASTENER HOLES IAW DWG 5758265 AND SRM 53-02-03-0 FIG 010.

Part: LONGERON — CRACKED (BS 1755 L14L) · airframe 62,754 hrs · 23,100 cycles

INSPECTION TYPE:C2 AFT CABIN L14L CRACKED AT CANTED FRAME STA 1755. REPAIRED L14L STA 1755 CANTED FRAME IAW SRM 51-3-0, 53-2-2 FIG 10 AND AND 51-1-8, EO 008-5320-28843A AND EA 008-5320-01-A1314.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED AT FASTENER HOLE INBD OF INBD HINGE. REPAIRED HORIZ STAB REAR SPAR WEB CRACK AT FASTENER HOLE, INBD OF INBD HINGE IAW SRM 55-02-00 FIG 004, SRM 55-02-00 FIG 002 AND SRM 51-1-21.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED AT FASTENER HOLES IN 2 PLACES O/B OF I/B HINGE. REPAIRED LT HORIZ STAB REAR SPAR WEB IAW SRM 55-02-00 FIG 002 AND SRM 5 1-1-21.

Part: FLOORBOARD — CRACKED (COCKPIT) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 FLT DECK PANEL 682A HAS DOUBLE DRILLED HOLES WITH NO ED AND ALL HAT CHANNELS CHAFED. FABRICATED AND INSTALLED 1 WEB AND 6 HAT CHANNELS IAW DWG 56935 7 AND S275589.

Part: SEAT TRACK — GOUGED (BS 1520) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CABIN STA 1520 LBL60 SEAT TRACK GOUGED. CABIN SEAT TRACK AT STA 1520 AND LBL 60, REPAIRED IAW EO DC8-5340-7779-B.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 FLT, DECK FLOOR PNL 678 HAS MANY BADLY BUCKED RIVETS WITH SOME HAT CHANNEL RADIUS, ALSO CORROSION AROUND FASTENER HOLES. FABRICATED FLT DECK FLOOR PANEL NR 678 IAW SRM 57-07-00 FIG 049B.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 CABIN STA 1500 LBL 45 SEAT TRACK AND PLUG GOUGED. REPLACED CABIN SEAT TRACK SECTION AT STA 1500 AND LBL 45 IAW SRM 51-3-0, SRM 51-3-01 AND SRM 53-21-01-04.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 A/C COMPARTMENT STA 55 L24L FRAME IS CRACKED AT DUCT ATTACH ROD CLIP. REPAIRED A/C COMPARTMENT FRAME AND SHEAR TIE AT STA 55 AND L24L IAW SRM 53-02-00 FIG 002, SRM 53-02-00 FIG 2B, SRM 51-9-0 FIG 068A.

Part: FLOORBOARD — DAMAGED (COCKPIT) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 COCKPIT FLOORPANEL 680 HAS LARGE FIELD REPAIR, DAMAGE CHANNELS AND SKIN. FABRICATED COCKPIT FLOORPANEL 680 IAW DWG 3619352 AND S2755898, SRM 51 -1-8 AND SRM 51-01-21.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 FLOOR PNL F25 HAS CRACKED U-CHANNEL. REPAIRED FLOOR PANEL F25 IAW SRM 53-07-03 FIG 001, SRM 51-1-21 AND SRM 51-1-8.

Part: PANEL — CORRODED (COCKPIT) · airframe 62,753 hrs · 23,100 cycles

INSPECTION TYPE:C2 COCKPIT FLOOR PNL 676E HAS CORROSSION. REPAIRED COCKPIT FLOOR PNL, BY FABRICATION IAW SRM 53-07-03 FIG 001.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS CAME ON AT TAKEOFF WITH THE SWITCH IN THE "ARMED" POSITION. THE LEFT EMERGENCY BUSS WAS OPERATING NORMAL. T/S EMERGENCY EXIT LIGHT SYSTEM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01-2. SYSTEM OPS CKS GOOD ON GROUND.

Part: CIRCUIT BREAKER — INOPERATIVE (EMERGENCY LIGHTS)

ON PREFLIGHT, EMERGENCY LIGHTS WILL NOT DISARM. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLACED SAME PER DOUGLAS STANDARD MANUAL 20-60-01. SYS OPS CKS NORMAL PER MM 33-50-02-2. OK FOR SERVICE.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

ON PREFLIGHT, EMERGENCY EXIT LIGHTS CAME ON WHEN ARMED. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLACED SAME PER MANUAL 20-60-01. SYS OPS CKS PER MM 33-50-02-2. OK FOR SERVICE.

Part: CONTROL VALVE — INOPERATIVE (BRAKE ASSY)

A/C CAME TO A STOP WHEN CLEARING THE ACTIVE RUNWAY AND WAS UNABLE TO MOVE WITH BRAKES OFF. THE ANTI-SKID LIGHT CAME ON WITH THE SWITCH ON WHEN CLEARING THE RUNWAY. FOUND CABLE AT BRAKE CONTROL VALVE COMING OFF OF FWD QUADRANT AND GUIDE PIN DAMAGED. REPLACED GUIDE PIN, REPOSITIONED CABLE, INSPECTED QUADRANT AND CABLE. NO DEFECTS NOTED. NO ADJUSTMENT REQUIRED OR MODE, TESTED BRAKE VALVE SYSTEM IN REF TO MM CH 32-42-02-02. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (PAX DOOR)

GROUND CREW OPENED ENTRY DOOR FROM OUTSIDE REMOVING ESCAPE SLIDE FROM COVER NEEDS REPACKING. REINSTALLED SLIDE IAW DC8 MM 25-60-01-2.

Part: FITTING — CORRODED (FS 1690 L28L) · airframe 62,508 hrs · 22,951 cycles

INSPECTION TYPE:SP L28L STA 1690 AFT END FITTING CORRODED OUT OF LIMITS. REMOVED AND REPLACED LONGERON END FITTING AT STA 1690 L28L IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1690)

CORROSION FOUND ON OUTER FUSELAGE SKIN AT L28 LT AND FUSELAGE STATION 1690. AREA TOTALS APPROX 10 SQ INCHES. REPAIRED EXTERNAL SKIN CRACKS AT STA 1690, 1718, 1746, L28L IAW SRO 8530032.

Part: SKIN — CORRODED (BS 1746)

CORROSION FOUND ON OUTER SKIN AT L28 LT AND FX STATION 1746. AREA TOTALS APPROX 1 SQ INCH. SKIN APPEARS TO BE SEPARATED AND CRACKED AT 1 EACH FASTENER. REPAIRED EXTERNAL SKIN CRACKS AT STATION 17-1721 L28L IAW SRO 8530032.

Part: SKIN — CORRODED (BS 1746 L28L)

INSPECTION TYPE:N/A PULLED RIVETS AND SKIN CORROSION AFT OF PRESSURE BULKHEAD. A/C FERRIED TO SAA 9047. REPAIRED EXTERNAL SKIN CRACKS AT STA 1746 L28L IAW SRO 8530032.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. EMERGENCY LIGHTING OPS NORMAL IN REF TO AMM 33-50-00.

Part: LIGHT — ILLUMINATED (COCKPIT)

INSPECTION TYPE:N/A DURING FLIGHT - EMERGENCY LIGHTS ILLUMINATED, UNABLE TO RESET. TRIED RESETTING ALL 3 CIRCUIT BREAKERS WITHOUT SUCCESS, TURNED EMERGENCY LIGHTS TO DISARM THEN OFF. RESET EMERGENCY EXIT LIGHT CONTROL C/B, ELIMINATED DISCREPANCY. ALL SYSTEMS NORMAL.

Part: ENGINE — FLAMED OUT (NR 4)

INSPECTION TYPE:N/A AT FL370, NR 4 ENGINE FLAMED OUT. NOTED NR 4 BOOST PUMP OFF. RESTARTED AFTER SECOND ATTEMPT. REMOVED AND REPLACED NR 4 MAIN FUEL FILTER IAW DC8 MM 73-10-02-4. FILTER WAS CLEAN. INSP CHIP DETECTOR IAW DC8 MM 79-20-05-2. RAN ENG. STARTED AND RAN OK. CHECKED EDP PRESS & IDLE (19 PSI) PER DC8 MM 73-10-01-2. COULD NOT DUPLICATE PROBLEM.

Part: UNKNOWN — ODOR (COCKPIT)

MUSTY SMELL COMING FROM A/C SYSTEMS. RAN SUPPLEMENTAL HEAT, NO MUSTY SMELL AT THIS TIME. HAS AIR TO GROUND CLEAN TOILET AND COCKPIT.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY UNIT. TESTS GOOD, REFERENCE MM 33-50-01.

Part: WINDOW — LEAKING (COCKPIT)

CAPT'S SLIDING WINDOW IS STILL LEAKING AND VERY NOISY (REPEAT WRITE- UP) NOTE AT FL 360, HAD TO INCREASE FLOW ON BOTH PACKS TO 80 PERCENT IN ORDER TO KEEP CABIN FROM CLIMBING. RESEALED CAPT'S SLIDING WINDOW PER DC8-MM 56-10-03-8. APPROVED REPAIRS, UP TO STEP 7C. TEST SEALANT ON F/ES TABLE SEALED. PRESSURIZED AIRCRAFT, NO WINDOW LEAKS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT)

INSPECTION TYPE:N/A CAPT'S LEFT WINDSHIELD SHATTERED. INSTALLED NEW WINDOW PER MM 56-10-02-2. A/C OK FOR SERVICE.

Part: ADAPTER — DAMAGED (RT MLG)

DURING MAINTENANCE POST FLIGHT INSPECTION, A NOSE JACK ADAPTOR PAD WAS FOUND WEDGED IN THE TRAILING EDGE FLAP AFT OF THE RIGHT MAIN LANDING GEAR. THIS RESULTED IN AN APPROXIMATE 6" BY 4" PUNCTURE THROUGH THE FLAP. A/C TO BE FERRIED TO SDF (FERRY 9013)- D336801. REMOVED RT I/B FLAP PER MM 27-51-01-4 & PACR 8-27-MM-06 3024. OK TO INSTALL REPLACEMENT FLAP. INSTALLED FLAP UP TO STEP 4 IAW 27-51-01-4. COMPLETED INSTALLATION OF RT I/B FLAP PER MM 27-51-01-4. ALL CHECKS NORMAL. DEFERRAL CLEARED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-01-2. OPS CK GOOD.

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT)

CAPT'S SMOKE GOGGLES SCRATCHED. REMOVED AND REPLACED CAPTAIN'S SMOKE GOGGLES. OK TO CONTINUE.

Part: A/C PACK — ODOR (COCKPIT)

A BURN SMELL WAS NOTED IN THE COCKPIT APPROXIMATELY ONE HOUR AFTER LEVEL OFF. THE SMELL WENT AWAY IN APPROX 2 MINUTES. A SEARCH OF CABIN AT COURIER AREA FOUND NO OBVIOUS PROBLEMS. INSPECTED ALL ACCESSIBLE FLT DECK COMPT'S FOR ANY VISUAL DAMAGE OR ODORS. ADJUSTED ALL COCKPIT LIGHTING TO VARIOUS INTENSITY. NO DISCREPANCIES WERE NOTED. OK TO CONTINUE.

Part: FITTING — CRACKED (FS 1240 L35R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 C-PIT STA 1240 L35R FWD FITTING JUST AFT OF TORQUE BOX IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D AND DWG 3758495.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB ANGLE STRUCTURE IS CRACKED AT AFT LWR CORNER. REMOVED DAMAGED ANGLE IAW SRM 51-1-21, FABRICATED AND INSTALLED MAIN CARGO DOOR JAMB ANGLE LWR CORNER IAW DC8 DWG 5772786, AND SRM 51-1-8, AND SRM 51-1-20D

Part: SKIN — CRACKED (LT WING) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 LT WING I/B T/E POSSIBLE CRACK FROM TOP OF STOP DRILL. REMOVED PREVIOUS REPAIR DOUBLER. CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 51-1-21 ,51-3-0, 51-1-20D, 57-05-2 AND 57-02-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 ANGLE CRACKED AT STA 857 RBL 40 REMOVED CRACKED ANGLE IAW 51-1-20D, LOCATED AND DRILLED NEW ANGLE AND INSTALLED AT STA 857 RBL 40 IAW SRM 51-1-21 AND SRM 51-1-20D.

Part: FRAME — CRACKED (FS 1766) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 TAIL SEC 60 COMPT AFT PRESSURE BULKHEAD STA 1766 3RD "J" FRAME FROM BOTTOM HAS A 3" CRACK AT C/L. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 ANGLES, 4 CLIPS, 4 SHIMS AND WASHERS IAW SRM51-1-21,53-2-5 FIG 26, AND 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (BS 852 LBL 60) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CORROSION ON FLOORBOARD SUPPORT CHANNEL AT STA 852 LBL60, MAIN CARGO COMP. CUT OUT CORRODED AREA IAW SRM 51-1-8 AND 53-2-0 FIG 1F, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-07-03, 53-02-00C, AND SRM 51-1-21 AND 51-1-20D.

Part: SPAR — CRACKED (FS680 RBL 13,18,) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 3 POSSIBLE CRACKS ON FWD SIDE OF STA.680 BETWEEN FASTENERS COMMON LOWER SPAR AT RBL 13,18 AND 31. CUT OUT DAMAGED WEB. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS AND FINGER DOUBLER AT WEB STA. 680 IAW SRM 53-2-5 FIG 13, 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (BS 280 L21L) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE FITTING HAS HEAVY INTERGRANULAR CORROSION. REMOVED CORRODED FITTING IAW SRM 51-1-21 LOCATED AND DRILLED NEW FITTING AND INSTALLED AT MAIN CARGO DOOR JAMB IAW SRM 51-3-2, 51-1-21, AND SRM 51-3-0.

Part: ATTACH ANGLE — CRACKED (MCD THRESHOLD) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE,THRESHOLD ATTACHED ANGLE CRACKED 1/4" AT FWD LATCH SPOOL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE IAW SRM 51-3-0 AND DWG NR 5772786. TVL # 7268745.

Part: FITTING — CRACKED (BS 702 L13R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 MAIN DECK STA 702 L13R SPLICE FITTING IS CRACKED ON O/B SIDE. REMOVED CRACKED FITTING IAW SRM 51-1-20C, FABRICATED AND INSTALLED SPLICE FITTING IAW DWG 3779978, AND SRM 51-1-8, AND 51-1-20D AT STA 702 L13R

Part: SPAR CAP — CRACKED (FS 857 RBL12-47) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 RT W/W FWD BULKHEAD STA 857 PRESSURE WEB LOWER ATTACH ANGLE CRACKED FROM RBL 24-33. REMOVED PRESS PANEL AND CUT OUT CRACKED AREA IAW SRM 51-1-21, AND 51-1-20D. FABRICATED AND INSTALLED -15 SPAR SECTION, -3, -5, AND -15 FILLERS, AND -14 STRAP IAW SRM 53-02-05 FIG 16, 53-2-5 FIG 6, 51-3-0, AND SRM 51-1-20D AT STA 857 RBL 12.66 - RBL 47.

Part: FITTING — CRACKED (BS 1195 L34R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACKED BATHTUB FITTING IN AFT CARGO TORQUE BOX STA 1195 FWD SIDE ACCESS HOLE I/B OF CENTER DOOR LATCH. REMOVED AND REPLACED BATHTUB FITTING AT STA 1195 L34R IAW SRM 51-3-2, 51-1-8 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1160 L35R-36) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 BATHTUB FITTING CRACKED IN C-PIT STA 1160 BETWEEN L35R AND L36. REMOVED FITTING, FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 53-02-00, 51-1-20D.

Part: FITTING — CRACKED (FS 1185) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACKED LATCH BACKUP FITTING IN AFT CARGO COMP TORQUE BOX STA 1185 OF DOOR CUTOUT AT FWD FASTENER OF 3RD LATCH. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-3-00.

Part: LONGERON — CRACKED (BS 1720 L10L) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 LONG 10L IS CRACKED ON LWR SIDE AT CANTED WEB STA 1720 AT LWR NUT. CUT OUT DAMAGED AREA IAW SRM 53-2-2 FIG 11 FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER AT STA 1720 L10L IAW SRM 53-2-2 FIG 11, SRM 51-1-8 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1168) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACKED BATHTUB FITTING IN AFT CARGO COMPT TORQUE BOX JUST I/B OF DOOR CUTOUT AT STA 1168. REMOVED AND REPLACED BATHTUB FITTING AT STA 1168 IAW SRM 51-1-21, 51-1-20D, AND SRM 51-03-02-0.

Part: FITTING — CRACKED (FS 1180 L27L) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACKED FRAME FITTING BELOW DOOR STOP FITTING IN AFT CARGO COMPT STA 1180 AFT SIDE OF FRAME L27L. REMOVED AND REPLACED FITTING AT STA 1180, L27L IAW EO DC8-5350-7876-A, AND SRM 51-1-21, 51-1-20D. FAB`D AND INSTALLED REPAIR DOUBLER IAW EO DC8-5350-7876-A, AND SRM 51-1-21, AND SRM 51-1-20D.

Part: FRAME — CORRODED (FS1060 L28L) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CORROSION ON AFT CARGO COMP FRAME UPPER SURFACE STA 1060 BETWEEN LONGERON 28L AND 29L. FOUND CORROSION OUT OF LIMITS IAW SRM 53-2-0 FIG 1F, CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG 2. FABRICATED AND INSTALLED 2EA REPAIR ANGLES, LOCATED AND DRILLED FRAME SEGMENT IAW SRM 51-1-8 DWG 5001269, AND SRM 51-1-20D

Part: FRAME — CORRODED (FS 1060 L30R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 (EXFOLIATION) CORROSION ON AFT CARGO FRAME AROUND FASTENER HOLE STA 1060 ABOVE L30R. REMOVED DAMAGED AREA. FABRICATED SPLICES AND INSTALLED REPLACEMENT FRAME AND SPLICES IAW SRM 53-2-0 FIG 2, 51-1-20D AND 51-1-21.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 LT UPPER AFT I/B SURFACE OF HORIZONTAL STAB HAS 3 CREASES. REMOVED, FABRICATED AND INSTALLED HORIZONTAL STAB SKIN PANELS 2 IAW DWG 5651747, SRM 51-1-21.

Part: FITTING — CRACKED (FS 985 L34R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACKED FITTING IN AFT CARGO COMP BILGE STA 985 JUST O/B OF LONGERON 34R UNDER FWD END OF CARGO TRACK. REMOVED, FABRICATED AND INSTALLED FITTING, AT STA 985 L34R IAW SRM 51-1-20D AND SAA EA 008-5310-01-A0016.

Part: FRAME — CORRODED (FS1060 L31L-L32L) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CORROSION ON AFT CARGO FRAME STA 1060 UPPER SURFACE IN 3 AREAS JUST ABOVE L31L AND L32L AROUND FASTENERS HOLES, ALSO ON LWR SURFACE OF UPPER FLANGE AROUND NUT PLATE ABOVE 32L. REMOVED AND REPLACED UPPER FRAME CAP IAW SRM 51-03-02, 51-1-21 AND 51-1-20D.

Part: SHEAR TIE — CRACKED (FS 1160 L34-35R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 CRACK ON SHEAR TIE FITTING IN AFT CARGO COMP AFT OF STA 1160 FRAME INSIDE POCKET BETWEEN L34R-L35R. REMOVED AND REPLACED SHEAR TIE FITTING IAW SRM 53-2-0 FIG 2D AND 51-1-20D.

Part: SKIN — CRACKED (BS 1726 L17R) · airframe 61,722 hrs · 22,380 cycles

INSPECTION TYPE:C1 RT STA 1726 AT L17R, HAIRLINE CRACK IN THE SKIN AFT OF THE RIVET. CUT OUT DAMAGED AREA IAW SRM 53-02-01-0 FIG 007 FABRICATED AND INSTALLED FILLER, FINGER DOUBLER, AND REPAIR DOUBLER IAW SRM 53-02-01-0 FIG 007, 53-05.01-0 FIG 001, AND SRM 51-1-20D

Part: WINDOW — JAMMED (COCKPIT)

CAPT SLIDING WINDOW W/NOT OPEN. PER IMPACTS A/C STATUS SLIDING WINDOW JAMMED AND OVER CTR MECHANISM IS WORN TO A POINT OF CAUSING JAM PROBLEM. REMOVED AND REPLACED CAPT CLEARVIEW WINDOW ASSY IAW 56-10-03-4. ALTERNATE P/N USED PER EO DC8-5610-23421-A. WINDOW OPENS NOW.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOP; FAILS TEST BUT BATTERY SEEMS TO BE GOOD. INSTALLED REPAIRED BATTERY PACK IAW 33-50-01-2.

Part: DOWNLOCK SWITCH — FAILED (RT MLG)

RIGHT LANDING GEAR GREEN DOWN INDICATION FOR SAFE AND LOCKED INOP WITH FLAPS AT 35 DEGREES AND BEYOND NO UNSAFE WARNING HORN PRODUCED. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWN SNAP SWITCH IAW DC-8 M/M 32-60-00-2 AND CONNECTOR AS REFERENCED ON ITEM 3 THIS L/P OPS CHECKS GOOD AT THIS TIME. A/C OK FOR CONTINUED SERVICE.

Part: FAN — FAILED (E&E BAY)

SMOKE IN COCKPIT PASSING 25,000 BEGAN TO FILL THE COCKPIT WITH STRONG ELECTRICAL FIRE SMELL. DECLARED EMERGENCY AND LANDED ASAP. FOUND RECIRC FAN INTERNAL FAILURE. REMOVED RECIRC FAN 67302. INSTALLED NEW FAN IAW 21-01-2, OPS CHECK NORMAL. OK FOR CONTINUED SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS STAY ON CONTINOUSLY WHEN IN ARMED POSITION. LIGHT WILL NOT ILLUMINATE. WHEN SWITCH SELECTED TO DISARM CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT & PERFORMED ADJ/ TEST IAW MM 33-50-01-2. OPS CHECK GOOD.

Part: FITTING — CRACKED (T/E FLAP) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE:C3 FLAP SUPPORT ASSY 5642342-2 CRACKED RT WING STA XW3.125 LOC AND DRILL NEW FITTING, ALODINED, PRIMED, AND INSTALLED 2 EA BUSHINGS, 1 EA BEARING, FITTING, AND ALL PARTS REMOVED FOR ACCESS; ALL IAW DC8 51-1-24, 51-1-8, 51-1-20, 51-1-21, 51-3-1, AND DAC DWG(S) 5642342. VERIFIED ALIGN OF TORQUE TUBE ARM; TORQUED DRIVE LINK TO FLAP FITTING; TENSIONED CABLES; ALL IAW DC8 MM 27-51-06, 27-50-00, AND DAC DWG 5642900.

Part: WEB — CORRODED (RT MLG WW) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, CORROSION FOUND IN RT W/W OB WEB STA 3 JUST BEHIND FLAP BUSS DRUM. 5643403-4 PANEL AND -6 DBLR FOUND CORRODED OUT OF LIMITS; CUTOUT CORR ARE A OF -4 PANEL AND -6 DBLR;FAB -4 PANEL AND -6 DBLR;HEAT TREAT;LOC, DRILL 2EA REPAIR DBLRS AND 2 EA RPR FILLERS;ALODINED AND PRIMED;INSTALLED DBL RS, FILLERS, AND 2 EA STIFFNERS;ALL IAW DC8 SRM 53-2-0, 51-1-24, 51-1-8, 51-1-20D, AND TR 53-166.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, CORROSION ON SEAT TRACK FS 570, LBL46. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 5 3-2-3. INSTALLED NEW SEAT TRACK S4755395 AND 4 FITTING SEAT TRACK SUPPORT AND 2 SPLICES IAW UPS EO DC8-5320-8309-D AND DC8-5320-5167-C.

Part: FITTING — CRACKED (RT WING) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, ATTACH FITTING AT XRS 624.000 REAR SPAR CRACKED. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001. CRACK NOTED. REMOVED AILERON SUPPORT FITTING CRACKED ATTACH FITTING AND MOUNTING STUD IAW DC8 SRM 51-1-20 AND 51-3-0. LOCATED AND DRILLED ATTACH FITTING IAW DC8 SRM 51-1-24 . INSTALLED ATTACH FITTING, REINSTALLED MOUNTING STUD AND REINSTALLED AILERON SUPPORT FITTING AND TORQUED IAW DC8 MM 20-10-00.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, AFT ACCESSORY COMP DOUBLER AROUND OUTFLOW VALVE CORRODED AT FWD CORNER. REMOVED EXISTING EXT DBLR AT FS 1620 L32R IAW DC8 SRM 51-1-20D. CUTOUT CORRODED INNER DBLR AND SKIN , FABBED REPAIR DOUBLER, FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7 AND REO G09567 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER, FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7 AND REO G09567.

Part: FINGER DOUBLER — CORRODED (COCKPIT) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, CORROSION AND SHEARED RIVETS ON WEB FINGER DOUBLER COCKPIT SHEAR WEB UNDER F/E STA RT CUSP FS -12.000 TO -32.000. REMOVED CORRODED FINGER DOUBLER IAW DC8 SRM 51-1-21, CUT OUT DAMAGE IN WEB IAW DWG SRO8530026, REMOVED CORROSION ON CUSP IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED CUSP IAW DC8 SRM 51-1-8 FABBED - 15 WEB FILLER, -13 FINGER DBLR, -17 AND -3 SPLICES IAW DWG SRO8530026. ALODINED, PRIMED, AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, AFT PIT FS 1020 CORROSION UNDER NUTPLATES ON LOWER SURFACE OF UPPER FRAME FLANGE FROM L36-L34R. REMOVED CORROSION IAW DC8 SRM 51-1-8. ORIG .080, REMOVED .060 REMAIN .020 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FRAME CAP OUT OF LIMITS IAW DC8 53-2- 0. FABBED REPAIR ANGLE -3 & -5 FILLER IAW REO G09556. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, RECEIVED, LOCATED, AND DRILLED NEW FRAME CAP IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE:C3 (C) PIT DOOR OUT LOWER SIDE WEB CORRODED NR 3 AND NR 6 (T) BOLT FITTING CORRODED. REMOVED (2) LATCHES. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA WITHIN LIMTS IAW DC8 SRM 53-2-0. PRIMED LONGERON AND INSTALLED FITTINGS IAW DC8 SRM 51-1-20D

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, AIR CONDITIONING ACCY COMPARTMENT AT STA 46 RBL 44. FLOORBEAM MISSING TWO FASTENERS. UPON INSP OF MISSING FAST FOUND FLOORBEAM TO BE CORRODED, REMOVED CORRODED IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED FLOORBOARD AN D 2 EA FLOOR SUPPORT ANGLES. FABBED TEE CAP REPAIR ANGLE IAW TR 53-152 AND FLR SUPPORT ANGLE IAW DAC DWG 4774654. ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 51-3-0, AND TR 53-152 FIG 1H.

Part: SKIN — CRACKED (PAX DOOR) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, L2 AFT PAX DOOR LOWER AFT CORNER HAS SEVERAL AREAS OF CRACK INDICATION ON EXTERNAL SKIN AREAS MARKED CRACK AND BULGING SKIN NOTED IAW DC8 SID NDT MAN 53-10-12 PSE 53.08.04 1. CUT OUT CRACKED 2 EA AREAS; PERFORMED HFEC, NO CRACKS AFTER CUT OUT; FAB DBLR, TRIPLER, AND FILLERS; ALODINED, PRIMED AND INSTALLED DOUBLER, TRPLR, AND FILLERS; ALL IAW DC8 SRM 53-2-0, TR 53-134,53-185, NDT SRM 06-10- 01.001, DC8 SRM 51-1-8, REO G09548.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, FWD PIT STA 280 TORQUE BOX HAS AREA OF LIGHT CORROSION. ACCOMPLISHED REPAIR IAW REO G09550 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,881 hrs · 21,637 cycles

INSPECTION TYPE: C3, FUSELAGE DENTED FS 160, BETWEEN LONGERON 25-26 LT, BLEND OUT GOUGE IAW DC8 SRM 53-2-0, ORIG THICKNESS .071 IAW DC8 SRM 53 -4-1, REMOVED .020, REMAINING .051 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, RMVD DAMAGED AREA IAW DC8 SRM 53-24-0 & 53-4-1, FABBED AND LOCATED HOLES IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: WEB — CRACKED (RH INBD FLAP)

RIGHT INBOARD FLAP, INBOARD CLOSEOUT WEB CRACKED. REMOVED EXISTING DOUBLER & ACCESS PANEL. REMOVED EXISTING SUPPORT ANGLE AND HAT CHANNEL FOR ACCESS. DRILLED OFF I/B WEB ASSY FOR REPLACEMENT. CLEANED AND PRIMED MATING SURFACES OF RIB & DOUBLER AS PER DC8 SRM 51-1-8 DP 70236. 1ST INNER DOUBLER TO NEW WEB IAW SRM 51-1-20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW M/M 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE: ASV, EMERGENCY BATTERY PACK LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER 33-50-00 OPS NORMAL.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: ASV, BULGE LT SIDE RUDDER. RUDDER HAS SKIN BULGE AT APPROX 4 FEET BELOW TIP AND 8 INCHES FROM TRAILING EDGE (BETWEEN LOWER STATIC WICKS) ON LT SIDE OF RUDDER. REMOVED RUDDER IAW MM 27-21-01 P401-P406 INSPCTED VERTICAL STRUCTURE FOR RUDDER SUPPORT. NO DAMAGE OK TO INSTALL RUDDER INSTALLED RUDDER PER MM 27-21-01 TO STEP 14L.

Part: SLIDE — INOPERATIVE (MAIN CABIN)

MAIN CABIN EXIT SLIDE INOP M247198. REPLACED SLIDE CONTAINER AND SLIDE PER MM-25-60-01

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A CRACK AT PIT 34 UPPER FWD CORNER FUSELAGE SKIN. INSTALLED REPAIR DOUBLERS PER EO DC-8 53-10-17222-A.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:PFLT SHEET METAL CRACK ON PIT 34 FWD UPPER DOOR CUTOUT AREA. A/C FERRIED TO SDF 9146. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-2-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A AFTER ENG START, WENT DARK, EMERGENCY LIGHTS CAME ON, WENT TO DISARM, THEN DISARM CHECK, DISARM, THEN BACK TO ARM. LIGHTS CAME BACK ON. PULLED AND RESET EMERGENCY LIGHTS CONTROL CB AND EMERGENCY LIGHTS CB TO GET THEM TO WORK NORMALLY. REMOVED, REPLACED AND TESTED EMERGENCY LIGHTS BATTERY PACK IAW MM 33-50-01.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR)

INSPECTION TYPE:N/A ESCAPE SLIDE GIRT BAR WOULD NOT ENGAGE. REPACKED AND INSTALLED EVACUATION SLIDE ON MAIN CABIN DOOR IAW DC8-MM 25-60-01.

Part: BATTERY PACK — NOT SEATED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT REMAIN ON AND CANNOT BE EXTINGUISHED. RESET EMERGENCY LIGHTS BATTERY PACK, OPS CHECKS GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHTS ILLUMINATED BUT UNABLE TO EXTINGUISH AFTER RESET AND ARMED. PERFORMED OPERATIONAL CHECK PER MM 33-50-01 OPS CHECKS OK.

Part: SKIN — CORRODED (VERTICAL STAB)

INSPECTION TYPE:N/A CORROSION AND PILLOWING OF SKIN ON VERTICAL STAB AFT LT SIDE. REMOVED PANEL AND ROUTED TO VENDOR FOR FABRICATION. TRIMMED AND INSTALLED NEW PANEL.

Part: SWITCH — FAULTY (COCKPIT)

INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED CAN BE RESET BY CYCLING ARMING SWITCH. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS SWITCH IAW M/M 20-50-00, OPERATIONAL CHECK IAW M/M 33-50-01.

Part: SMOKE DETECTOR — CONTAMINATED (CARGO BAY)

INSPECTION TYPE:N/A LOWER CARGO SMOKE LIGHT ILLUMINATED ON TAKEOFF. WARNING INDICATED SECTION C. AIR TURNBACK. INSPECTED PIT 33 DETECTORS, FOUND WATER INTRUSION ON ALL DETECTOR UNITS. DRIED ALL DETECTORS AND DEFERRED SYSTEM. OPS CHECK NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 160 LONG 10R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 FLOORBEAM IS CORRODED BEYOND LIMITS AT STA 1360 AT LBL 48. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 852-652.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 SEAT TRACK IS CORRODED BEYOND LIMITS STA 740-840 LBL 65. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 1020 LBL 60 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.

Part: WEB — CRACKED (RUDDER) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 RUDDER LOWER CLOSURE WEB IS CRACKED FWD OF ACCESS PLATE 81. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5701251, AND SRM 51-1-21.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 SEAT TRACK IS WORN BEYOND LIMITS AT STA 300 AT RBL 63. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SKIN — CORRODED (RT WING) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 RT WING LOWER SKIN IS CORRODED BEYOND LIMITS AT XRS795 BETWEEN STRINGER 52 AND 53. REPAIRED SKIN IAW 8110-3 DH SK 852-762.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 SEAT TRACK AT STA 65 LBL 50 HAS LUGS BROKEN. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 940-960 RBL 60-65. REMOVED FABRICATED AND REPLACED DOUBLER IAW DWG 5645332, AND SRM 53-1-0, 51-1-21.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 SEAT TRACK WORN BEYOND LIMITS AT STA 860-875 RBL 45-51. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 VERTICAL STAB REAR SPAR FWD SIDE FITTING IN 4TH LIGHTENING HOLE FROM THE TOP IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 36480113, AND SRM 51-1-20D.

Part: PRESSURE PANEL — CRACKED (COCKPIT) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE: C2, COCKPIT SUBFLOOR PRESSURE WEB IS CRACKED AT STA. -67 AT RBL. 60 REPAIRED WEB I.A.W. SRO 8520026

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 940 FRAME TO FLOORBEAM FITTING IS CRACKED AT LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 5751966, AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 1770 LONG 17L AND END FITTING ARE CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON AND FITTING IAW DWG 4772397, AND DWG 5649327 AND SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STA 1214 BETWEEN LONG 34R-35R. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 852-409.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 1770 LONG 17R AND 17R END FITTING ARE CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649327, AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (RT WING) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 RIGHT WING LOWER SKIN IS CRACKED AT FRONT SPAR AT LONG 64 END. REPAIRED SKIN IAW EO DC8-5730-9004 APPX E.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STA 1260 LONG 35R. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 852-822. FABRICATED DOUBLER PER SRM 51-2-1 FIG 7, INSTALLED FILLER PER SRM 51-126.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 1640 LONG 32R INTERNAL DOUBLER IS CORRODED BEYOND LIMITS. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 852-817.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA 1690 LONG 36 END FITTING IS CORRODED BEYOND LIMITS AND LONG 36 IS CRACKED. R&R FITTING, AND REPAIRED LONGERON IAW DWG 4641324, AND SRM 53-2-2 FIG 8, AND 51-1-21, 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 STA. 8 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG. 24R-29R REMOVED,FABRICATED AND REPLACED CHORD I.A.W. 8110-3 APROVED DH SK 852-708

Part: SKIN — DENTED (NR 4 PYLON) · airframe 59,792 hrs · 20,828 cycles

INSPECTION TYPE:C2 NR 4 PYLON OUTBOARD SKIN HAS FOUR DENTS BEYOND LIMITS BETWEEN YN335 TO YN353. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 852-534.

Part: SLIDE — OUT OF POSITION (DOOR)

INSPECTION TYPE:N/A DEPARTURE-ESCAPE SLIDE GIRT BAR WOULD NOT LOCK IN PLACE. *S/D* REPACKED SLIDE, OPS CHECKS GOOD REF M217781.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.

Part: RELAY — FAILED (NR 2 BUSS TIE)

INSPECTION TYPE:N/A, BEFORE BLOCK OUT NR 2 BUS WENT OFF LINE AND LIGHT SMOKE WAS OBSERVED IN THE COCKPIT. REMOVED AND REPLACED NR 2 BUS TIE RELAY W/REF TO M/M 24-20-03. RAN ALL ENGINES, NR 2 BUS TIE OPERATES NORMALLY, W/REF TO M/M 24-20-00. NO SMOKE OBSERVED IN COCKPIT.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN, EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33. OPS CK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:PFLT, LEFT AFT SERVICE DOOR HAS CRACK IN UPPER AFT RADIUS. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND DRILLED UP REPAIR DOUBLER PER SRM 53 2. DAMAGE REMOVED, OK TO INSTALL. INSTALLED DOUBLER IAW SRM 53 2 1 COMPLETED TEMP REPAIR PER SRM 53 2 1 TRANSFERED TO D208115. INSTALLED LINER ON MAIN DECK AFT OF LT AFT SERVICE DOOR. CLEARED D208115.

Part: REGULATOR — DAMAGED (CREW OXYGEN)

INSPECTION TYPE:N/A, CAPT OXYGEN REGULATOR NEEDLE FELL OFF. REPLACED REGULATOR.

Part: UPLOCK — INOPERATIVE (RT MLG)

INSPECTION TYPE:N/A, AFTER TAKEOFF RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED. CHECKLIST WAS FOLLOWED WITHOUT FIXING THE PROBLEM. AIR TURNBACK TO ONT DUE TO THIS PROBLEM. CLEANED AND LUBED RT MAIN DOOR UPLATCH MECHANISMS. OPS CK NORMAL IAW MM 32-32-06.

Part: FITTING — CRACKED (BS 1350)

INSPECTION TYPE:C1, LONGERON SPLICE FITTING IS CRACKED AT STA 1350 LONG 23R & 24R. REMOVED AND REPLACED FITTINGS IAW DWG 3755118 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1320-1340)

INSPECTION TYPE:C1, STA 1320-1340, THE RT CUSP UPPER SURFACE HAS HEAVY CORROSION. REPAIRED AREA BY SPLICING NEW SECTION OF CUSP FITTING IAW SRM 53- 2-5 FIG 15A (STA 1290 TO 1380).

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C1, FLOORBEAM LWR TIE FITTING IS CRACKED AT STA 759, LBL 48. REPAIRED AREA IAW 8110-3 APPROVED DH SK 852-726.

Part: HINGE ROD — OUT OF ADJUST (CREW DOOR)

CREW ENTRY DOOR WILL NOT OPEN. LWR HINGE ASSY W/N RETRACT WHEN TURNING HANDLE TO OPEN DOOR, CANNOT BE OPENED UNLESS HINGE IS HELD UP. FWD ENTRY LOWER HINGE CONTROL ROD ASSY PER 52-11-01, OPS CK GOOD PER 52-11-01.

Part: ARM BAR — NOT ATTACHED (ESAPE SLIDE)

INSPECTION TYPE:N/A, THE ESCAPE SLIDE ARM BAR WOULD NOT ATTACH TO THE HOLDING BRACKET. RE-PACKED EMERGENCY ESCAPE SLIDE AND INSTALLED.

Part: JAMB — DAMAGED (LT MLG DOORWAY)

INSPECTION TYPE:N/A, LEFT MAIN GEAR DOOR CUTOUT AT REAR SIDE INNER CORNER HAS CURLED SHEET METAL AND A .5 INCH LONG TEAR. *S/D* REPAIRED AREA IAW SRM 51-1-20 AND SRM 53-4 -1.

Part: SLIDE — MISINSTALLED (EMER EXIT DOOR)

INSPECTION TYPE:N/A, EMERGENCY SLIDE WOULD NOT CONNECT TO LATCHES, PACKED INCORRECTLY. REPACKED ESCAPE SLIDE, OPS CHECK GOOD.

Part: COWL — DAMAGED (NR 1&4 ENGINE)

NR 1 AND NR 4 ENGINE COWLINGS CONTACTED RUNWAY ON LANDING. REMOVED AND REPLACED FAN COWL ON BOTH NR 1 AND NR 4 ENGINES. REPLACED DRAIN MASTS. ALSO, ACCOMPLISHED HARD LANDING INSPECTION NACELLE CONTACT INSP AS PER M\M REF 05-56-00.AND EO DC8-7830-11028. (WAN NR 386924).

Part: SKIN — DAMAGED (FWD FUSELAGE)

INSPECTION TYPE-N/A, SKIN AND RIVETS ERODED JUST AFT OF RADOME AT 12 O'CLOCK POSITION. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-2-1 AND ALODINED PER SRM.

Part: DOOR FRAME — CORRODED (BS 1620)

INSPECTION TYPE-D, FS 1620 RT FRAME CORRODED BEYOND REPAIR AND SEVERAL MISDRILLED HOLES. REPAIRED IAW DHC SK-852-611.

Part: SEAT TRACK — CORRODED (BS 808-870)

INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 808 AND 870 LBL 45. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 781-798)

INSPECTION TYPE-D, SEAT TRACK CORRODED BEYOND LIMITS AT FS 781 AND 798. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-7-2, 53-2-3, AND 51-1-21.

Part: SEAT TRACK — CORRODED (BS 902)

INSPECTION TYPE-D, SEAT TRACK CORROSION REMOVAL BEYOND LIMITS FS 902 LBL 60. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION IAW SRM 53-7-3.

Part: DOUBLER — CORRODED (BS 200-220)

INSPECTION TYPE-D, DOUBLER AT FS 200 TO 220 LONG 28L EXFOLIATED OUT OF LIMITS (INTERNAL). REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5773863.

Part: SEAT TRACK — WORN (BS 861)

INSPECTION TYPE-D, SEAT TRACK AT FS 861 RBL 47 IS WORN BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5340-7779.

Part: DOUBLER — CORRODED (BS 879-940)

INSPECTION TYPE-D, MAIN GEAR WHEEL WELL PRESSURE FLOOR UPPER SURFACE DOUBLERS CORRODED BEYOND LIMITS FS 879 TO 940 LBL 6 TO RBL 6. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 51-1-21 AND DWG 5645332-123, 125, AND 127.

Part: DOUBLER — CORRODED (BS 40)

INSPECTION TYPE-D, COCKPIT SUBFLOOR FINGER DOUBLER CORRODED FS -40 RBL 55. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5612298.

Part: SEAT TRACK — WORN (BS 420)

INSPECTION TYPE-D, MAIN CABIN SEAT TRACK AT FS 420 RBL 60 HAS LUG WORN BEYOND LIMITS. REPAIRED IAW SRM 53-2-3.

Part: FLOOR PAN — CORRODED (BS 1740-1750)

INSPECTION TYPE-D, MAIN CABIN FLOOR PAN AT FS 1740 TO 1750 LBL 12 TO LBL 20 CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT IAW SRM 51-1-21 AND DWG 5755032.

Part: DOUBLER — CORRODED (BS 8-70)

INSPECTION TYPE-D, INTERNAL DOUBLER AROUND A/C ACCESS CORRODED BEYOND LIMITS FS 8 TO 70 L-34R TO L-33R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5649028.

Part: SUPPORT — CORRODED (BS1680)

INSPECTION TYPE-D, MAIN CABIN FLOOR BOARD SUPPORT CORROSION REMOVAL BEYOND ALLOWABLE LIMITS FS 1680 RBL 5 TO RBL 28. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW SRM 57-7-3 FIG 5A.

Part: SUPPORT — CORRODED (BS 1715)

INSPECTION TYPE-D, MAIN CABIN FLOOR BOARD SUPPORT CORROSION REMOVAL BEYOND LIMITS FS 1715 RBL 10 TO LBL 10. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW DWG 5755032, SRM 53-7-3 AND 51-1-20.

Part: DOUBLER — CORRODED (BS 960-980)

INSPECTION TYPE-D, MAIN W/W PRESURE FLOOR UPPER SURFACE FINGER DOUBLER CORRODED BEYOND LIMITS F/S 960 TO 980 RBL 62 TO 69. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5645332 AND SRM 51-1-21.

Part: LONGERON — CORRODED (BS 220)

INSPECTION TYPE-D, LONGERON 36 AT FS 220 CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONG IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE-D, TORQUE BOX FITTING CRACKED AT FS 280 BETWEEN L-35L AND L-36. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: SPAR CAP — CRACKED (HORIZ STAB)

INSPECTION TYPE-D, LT HORIZ STAB ATTACH ANGLE INSIDE AUX SPAR AREA CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20 AND 51-1-21.

Part: SEAT TRACK — CORRODED (BS 808-870)

INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 808 LBL 22.5 AND AT FS 870. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 776)

INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 776 BL 0. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-1-7 AND 53-2-3.

Part: FLOORBEAM — CORRODED (BS 960)

INSPECTION TYPE-D, FLOORBEAM FS 960 LBL 60 FWD UPPER FLANGE EXFOLIATED. REPAIRED IAW DHC SK-852-159.

Part: FLOORBEAM — CORRODED (BS 702)

INSPECTION TYPE-D, FLOORBEAM FS 702 RBL 40 UPPER AFT FLANGE EXFOLIATED. REPAIRED IAW DHC SK 852-198.

Part: FITTING — CRACKED (BS 798.5)

INSPECTION TYPE-D, FLOORBEAM TO CENTER WING BOX ATTACH FITTING CRACKED FS 798.5 LBL 47. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: CLIP — CORRODED (BS 220)

INSPECTION TYPE-D, LONGERON 1 ATTACH CLIP CORRODED BEYOND LIMITS FS 220. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP IAW SRM 51-1-21 AND DWG 2643619.

Part: DOOR WEB — CRACKED (BS 70)

INSPECTION TYPE-D, FWD MAIN ENTRY DOOR WEB AT FS 70 STR-17L IS CRACKED 2 PLCS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-21 AND DWG 5597646.

Part: DOUBLER — CRACKED (BS 450)

INSPECTION TYPE-D, FS 450 LONG 34L TO 34R FINGER DOUBLER CRACKED AND CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5755271.

Part: SEAT TRACK — WORN (BS 55-360)

INSPECTION TYPE-D, MAIN CABIN SEAT TRACK LBL 62 FS 55 TO 360 IS WORN BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-7-3.

Part: DOUBLER — CRACKED (BS 1420-1440)

INSPECTION TYPE-D, FINGER DOUBLER CORRODED AND CRACKED BEYOND LIMITS AT FS 1420 TO 1440 L-31L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5615372 SRM 51-1-21, 51-1-20D, AND 53-4-0.

Part: SKIN — CORRODED (BS 190-450)

INSPECTION TYPE-D, FUSELAGE SKIN CORRODED BEYOND LIMITS AND INTERNAL DOUBLERS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 51-1-21 AND DWG 9755878-1 AND 9754011-505. REMOVED AND REPLACED SKIN IAW SRM 51-1-20D AND 51-1-21.

Part: SKIN — CRACKED (WS 250.089)

INSPECTION TYPE:D, LT WING L/E OUTBOARD SIDE OF THE STA XS250.089 RIB, THE UPPER SKIN INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SKIN IAW DWG 5769589 AND SRM 51-1-21.

Part: WEB — CRACKED (BS 194)

INSPECTION TYPE-D, MAIN CABIN 3.0 INCH CRACK IN RT FWD SERVICE DOOR CUTOUT WEB, FS 194. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-20D, 51-1-21, AND DWG 5615700.

Part: SKIN — CRACK (PAX DOORWAY)

INSPECTION TYPE-D, CRACK IN SKIN FWD LOWER CORNER OF AFT ENTRY DOOR. REPAIRED IAW UPS EO DC8-5330-9985-A.

Part: DOUBLER — CORRODED (BS 20)

INSPECTION TYPE-D, SEVERAL POPPED FASTENERS AND BULGING CORROSION UNDER FINGER DOUBLER AT LBL 24 FS -20 COCKPIT SUBFLOOR. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-3-1 AND DWG 5612298.

Part: SKIN — CORRODED (RT AILERON)

INSPECTION TYPE-D, RT WING OTBD AILERON T/E PNL, DELAMINATING AND SHOWS SIGNS OF CORROSION. REPAIRED IAW SRM 51-1-9A.

Part: ANGLE — CORRODED (BS 1540)

INSPECTION TYPE-D, SUPPORT ANGLE HAS HEAVY CORROSION AT LONGERON 33L FS 1540. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW DWG 5646608 AND SRM 51-1-20D.

Part: WEB — CRACKED (BS 200)

INSPECTION TYPE-D, RT FWD SERVICE DOOR AFT WEB FS 200 BTWN LONG, 14 AND 15 HAS 2 CRACKS IN WEB. REPAIRED IAW SRM 51-1-21 AND 53-2-0.

Part: CLIP — CRACKED (WS I6.225)

INSPECTION TYPE-D, RT WING L/E CLIP CRACKED AT STA XOLDI 6.225 (ABOVE PNEUMATIC DUCT). REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP IAW DWG 5769589 AND SRM 51-1-29D.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-D, RT LONG 27 END FITTING IS CORRODED AT FS 70 LWR FWD PIT. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 616.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 691.25)

INSPECTION TYPE-D, RT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER STA XFS691.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 448.581)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XS 448.581. REPAIRED IAW SRM 57-2-0.

Part: CARGO TRACK — CORRODED (BS 240/255/180)

INSPECTION TYPE-D, CARGO TRACK CORRODED OUT OF LIMITS FS 240 S 33R AND FS 255 AND STA 180. REMOVED AND REPLACED TRACK IAW SRM 51-3-0.

Part: CARGO TRACK — CORRODED (BS 120)

INSPECTION TYPE-D, CARGO TRACK CORRODED BEYOND LIMITS FS 120 ABOVE L-33L LWR FWD CARGO PIT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0.

Part: FITTING — CORRODED (BS 330)

INSPECTION TYPE-D, CORRODED BACKUP FITTING LOCATED AT THE NR 6 LATCH AT FWD LWR CARGO DOOR STR 33R FS 330. REMOVED AND REPLACED FITTING.

Part: SEAT TRACK — CORRODED (BS 370)

INSPECTION TYPE-D, SEAT TRACK CORRODED AT FS 370 ABOVE LONG 33R LWR FWD CARGO PIT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK FROM FS 320 TO 520 IAW SRM 51-3-0, 53-2-5, AND DWG 5759623.

Part: DOUBLER — CORRODED (BS 8-70)

INSPECTION TYPE-D, FINGER DOUBLER CORRODED BEYOND LIMITS RT SIDE L-31R FS 8 TO FS 70. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5613862.

Part: ANGLE — CRACKED (WS I6.225)

INSPECTION TYPE-D, RT WING L/E RIB LWR SUPPORT ANGLE CRACKED BY AFT FASTENER AT STA XOLDI 6.225. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 697.5)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER XSF 697.500. REPAIRED IAW SRM 53-2-0.

Part: SEAT TRACK — CORRODED (BS 560-640)

INSPECTION TYPE-D, SEAT TRACK RT FROM FS 560 TO 640 CORRODED BEYOND LIMITS ABOVE LONGERON 33R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK FROM FS 500 TO 640 IAW SRM 53-2-5 AND DWG 5759623.

Part: RIB — CRACKED (WS 672.5)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 672.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE-D, RT WING L/E RIB CRACKED AT UPPER ARM BY AFT FASTENER HOLE AT STA 760.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 828.750. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CORRODED (BS 200-220)

INSPECTION TYPE-D, RT FINGER DOUBLER UNDER STR 31R IS CORRODED BETWEEN FS 200 TO 220 LWR FWD PIT. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1 AND 51-1-21.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 778.750. ALSO LWR ARM CRACKED BY AFT FASTENER. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 728.75)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 728.750. REPAIRED IAW SRM 53-2-0 AND 57-2-0.

Part: RIB — CRACKED (WS 728.75)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 728.750. REPAIRED IAW SRM 53-2-0.

Part: WEB — CRACKED (BS 260-280)

INSPECTION TYPE-D, HEAVY CORROSION AND CRACK IN FLOOR WEB LT CUSP AREA EXTENDING UNDER FLOOR SUPPORT FITTING FROM FS 260 TO 280. REPAIRED WEB IAW SRM ADDN DC8-5330-2159-B.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-D, FS 1160 RT FLOORBEAM END FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3754946.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 772.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: SUPPORT — CORRODED (BS 120)

INSPECTION TYPE-D, RT FLOORBEAM SUPPORT TO FRAME IS CORRODED OUT OF LIMITS AT FS 120 FWD LWR PIT. REMOVED AND REPLACED FITTING IAW SRM 51-01-20.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 810.000. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (HORIZ STAB)

INSPECTION TYPE-D, LT HORIZ STAB I/B L/E SECTION SKIN EXTERNAL SURFACE AT APPROX STA XFS 293 HAS CRACK. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 55-3-1, 53-2-0, AND 51-1-20.

Part: CUSP — CRACKED (BS 120-130)

INSPECTION TYPE-D, LT CUSP FROM FS 120 TO 130 IS CRACKED. REPAIRED IAW SRM 51-1-21 AND EO DC8-5330-2159-B.

Part: RIB — CRACKED (WS 753.75)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 753.750. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (LT HORIZ STAB)

INSPECTION TYPE-D, LT HORZ STAB I/B L/E SECTION EXTERIOR SURFACE AT STA XE29 CRACKED. REPAIRED IAW SRM 55-2-0.

Part: RIB — CRACKED (WS 722.5)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 722.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 566.25)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 566.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-20-0.

Part: RIB — CRACKED (WS 722.5)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 772.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 454.976)

INSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FSTA XS 454.976. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING L/E SKIN ABOVE THE NR 1 PYLON IS CRACKED. REPAIRED IAW SRM 57-2-1A.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XOLDI 6.225 (ABOVE THE PNEU DUCT) IS CRACKED. THE CRACK IS OVER 2 INCHES LONG. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 435.788)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XS 435.788 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 397.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-3-3 AND SRM ADDN DC8-5720-4087.

Part: SKIN — CRACKED (GALLEY DOORWAY)

INSPECTION TYPE-D, SKIN CRACKED IN UPPER FWD CORNER OF FWD GALLEY DOOR. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 53-2-0, 51-1-21, AND 51-1-20D.

Part: FITTING — CRACKED (CARGO COMPT)

INSPECTION TYPE-D, CARGO COMPARTMENT AFT LWR X SLIDE DOOR T-LATCH BRACKET CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: DOOR MECHANISM — INOPERATIVE (CREW ENTRANCE)

ON LANDING ANC, UNABLE TO OPEN CREW ENTRANCE DOOR, HAD TO BE OPENED FROM THE OUTSIDE ADJUSTED DOOR PER MM 52-11-01. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (PTC ACTUATOR)

INSPECTION TYPE-N/A, ON LANDING ROLLOUT NOTICED SMOKE AND BURNING ODOR IN FLT DECK. *S/D* REPLACED PTC ACTUATOR CANNON PLUG THAT WAS DAMAGED, OPS CHK OK.

Part: SLOT — CRACKED (LT WING)

WHILE ON GROUND, MAINTENANCE FOUND LEFT WING INBD SLOT-INBD LWR CORNER HAS A 1 INCH CRACK IN IT. REPAIRED AS PER E.O. DC8-5730-7218A.