N729UP

Part: ESCAPE ROPE — LOOSE (EMERGENCY EXIT)

CAPTAIN'S ESCAPE ROPE UNSECURE AND COVER LOOSE. RESECURED CAPTAIN'S ESCAPE ROPE AND COVER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK PER MM 33-50-02-2. CK'S NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT WHEN GROUND POWER TO BATTERY, EMERGENCY LIGHTS DID NOT WORK. REPLACED EMERGENCY BATTERY PACK PER MM 33-50-02-2. CK'S NORMAL.

Part: SLIDE — OUT OF POSITION (CREW DOOR)

INSPECTION TYPE:N/A CREW DOOR ESCAPE SLIDE PRESSURE INDICATOR IS BELOW VIEWING WINDOW. REPOSITIONED SLIDE SO THAT PRESSURE INDICATOR IS BETTER VISIBLE.

Part: LIGHT — NO TEST (EMERGENCY EXIT)

EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED BATTERY RELAY PACK PER MM 33-50-01-2, PARA 4.

Part: FITTING — CRACKED (BS 280 L35-36L) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 BATHTUB FITTING CRACKED AT STA 280 BETWEEN L35L-L36. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 53-02-00-0 FIG 002D AND 51-1-20D.

Part: SKIN — CRACKED (FS 1750 L17R) · airframe 74,302 hrs · 49,317 cycles

THE REPAIR HAS LESS THAN THREE ROWS OF FASTENERS BEYOND THE DAMAGE AREA AND FOUND AT STA 1751 L15R 1" CRACK. REMOVED AND REPAIRED DOUBLER AT STA 1750 L17R IAW SAA EA NR 008- 5320-01-A0419 AND UPS DC8-5330-25186.

Part: STRINGER CLIP — CRACKED (XRS 204) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 CLIP AT STRINGER 66 AND XRS 204 IS CRACKED NR 4 MAIN REMOVED CRACKED STRINGER CLIP AT STA XRS 204 NR 3 MAIN TANK IAW SRM 51-1-20D. FABRICATED AND INSTALLED CLIP AT STA XRS 204 NR 3 MAIN TANK IAW SAA EA NR 008-5710-01-A0421, UPS RAA DC8-57-20191, FAA FORM 8100-9,AND BOEING SRID 1-228171918

Part: STRINGER CLIP — CRACKED (WING) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 LWR SURFACE CLIP CRACKED AT XRS 23 AND STRINGER 74 NR 3 MAIN TANK. REMOVED CLIP AT WING STA XRS 23 STRINGER 74 NR 3 MAIN TANK IAW SRM 51 -1-20D. FABRICATED AND INSTALLED CLIP AT WING STA XRS 23 STRINGER 74 NR 3 MAIN TANK IAW SRM 51-1-8, SRM 51-3-2, SAA EA NR 008-5710-01-A 0421, UPS RAA DC8-57-20191, FAA FORM 8100-9, AND BOEING SRID 1-228171918.

Part: BRACE — CORRODED (T/E FLAP) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 L/H FLAP CANOE FITTING INBD SIDE BRACE STA 219 CORRODED AND PITTED OUT OF LIMITS. REMOVED AND REPLACED LT CANOE FITTING INBD SIDE BRACE AT STA 219 IAW SRM 57-2-00 FIG 6, AND DC8 MM 27-51-12-2.

Part: SKIN — CORRODED (BS1490-1690) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 SKIN CORRODED OUT OF LIMITS AT STA 1490-1690 L31L-L31R. REMOVED AND REPLACED SKIN AT STA 1490-1690 L31L-L31R IAW SRM 51-1-21 AMD 51-1-20D.

Part: LONGERON — CORRODED (FS 300 L35R) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 LONGERON 35 RIGHT IS BLOWN OUT FROM STA 300 TO 320. REMOVED AND REPLACED LONGERON SECTION AT L35R STA 300 TO 320 IAW SRM 53-02-02 AND SRM 51-1-8.

Part: LONGERON — CORRODED (BS 1560 L36) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE-C3 L36 AT STA 1560 CORRODED OUT OF LIMITS. REMOVED L36 AT STA 1490-1690 AT STA 1560 IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON 36 AT STA 1560 IAW SRM 53-04-01-0 FIG 43, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 280-300 L36) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 L36 FROM STA 280-300 IS CRACKED. CUT OUT DAMAGED LONGERON. FABRICATED AND INSTALLED LONGERON, 2 SPLICES AND 4 BATHTUB FITTINGS IAW SRM 51-1-21, 51-1-20D 53-02-00-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 L10R END FITTING CRACKED AT STA 1769 IN 60 HOLE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21, 51-3-0 AND 51-1-20D.

Part: FITTING — CORRODED (BS 1620 L35L) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE-C3 LONG 35L END FITTING AT STA 1620 CORRODED (OFF A/C PART). LOCATED, DRILLED UP, AND INSTALLED END FITTING ON L35L IAW SRM 53-02-00-0 FIG 001F, AND SRM 51-1-20D.

Part: FITTING — CRACKED (RT TE FLAPS) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 RT FLAP STA 3 FITTING CRACKED. REMOVED RT FLAP FITTING AT STA 3 IAW 51-1-21. LOCATED, DRILLED UP REPLACEMENT FITTING AND INSTALLED AT RT FLAP STA 3 IAW SRM 51-3- 2, 51-1-21A.

Part: RIB — CRACKED (LT CTR WING LE) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 13TH FROM IB UPPER RIB CRACKED ON LT WING CENTER LE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-03-01 FIG 004, 57-02-00-0 FIG 02.

Part: RIB — CRACKED (RWS 298) · airframe 74,302 hrs · 49,317 cycles

RT CENTER LE UPPER RIB CRACKED AT XFS 298. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED T XFS 304. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS. IAW SRM 57-02-00-0 FIG 2,57-03-01-0 FIG 4 AND 51-1-20D.

Part: LONGERON — CRACKED (BS 1750 L15R) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE-C3 LONGERON 15R AT STA 1750 IS BROKEN AT LWR FLANGE REMOVED DAMAGED LONGERON SECTION AT STA 1750 L15R IAW SRM 53-02-02- 0 FIG 10, FABRICATED AND INSTALLED LONGERON SECTION AT STA 1750 L15R IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05-03-0.

Part: RIB — CRACKED (LT WING CTR LE) · airframe 74,302 hrs · 49,317 cycles

C3 3RD FROM IB UPPER RIB CRACKED ON LT WING CENTER LEADING EDGE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2, 57-3-1 FIG 4 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 74,302 hrs · 49,317 cycles

INSPECTION TYPE-C3 RT OB LE UPPER RIB CRACKED AT XFS597. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES. IAW SRM 57-2-00 FIG 2, 57-2-0 FIG4 AND 51-1-20D.

Part: SKIN — CRACKED (BS 1728 L17R) · airframe 74,302 hrs · 49,317 cycles

FOUND EXTERIOR FS CRACKED AT FS 1728 L17R. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 007, 51-1-20D.

Part: BLEED AIR SYS — ODOR (COCKPIT)

INSPECTION TYPE: N/A AT FL 330, WE OPERATED ENG ANTI-ICE AND SCOOPS. AN ODOR OF BURNING RUBBER BEGAN, AFTER SECURING ANTI-ICE/ SCOOPS ODOR DISIPITATED. R MANIFOL D WAS 270 AND L MANIFOLD WAS 260 DEG/C, R PACK TEMP 160 AND L PACK 80 DEG/C. RAN ENG 1,2,3,4 BLEED AIR TEMP NORMAL IAW MM 36-20-00. RAN BOTH PACKS OPS CK GOOD IAW MM 21-55-00. NO ODOR NOTED DURING ENG AND PACK OPERATION. IAW MM 36-00-00 TROUBLESHOOTING, IF ANTI-ICING INADVERTENTLY OPERATED ABOVE 30,000 FEET AIR TEMP BLEED MAY EXCESS 250 DEG/C.

Part: RELIEF VALVE — STUCK (LT MLG)

INSPECTION TYPE:N/A 100 MILES OUT OF SLC F/O NOTICED A LOSS OF HYDRAULIC QTY. CREW RAN CHECKLIST AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. FOUND LT BOGIE SWIVEL UNLOCK CYC - RELIEF VALVE STUCK IN THE OPEN POSITION. REMOVED AND REPLACED LT RELIEF VALVE PER DEQ MM CH 32-53-02-2. NO LEAKS NOTED.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY DISCHARGE LIGHTS INOP. EMERGENCY DISCHARGE SWITCH WAS FOUND IN ARMED POS DURING PREFLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY IAW MM 33-50-00. CHECK'S OK.

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT)

FIRST OFFICERS SMOKE GOGGLES SCRATCHED AND DIRTY. REPLACED FO'S SMOKE GOGGLES, REF AMM 25-60-05-2.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY ASSY IAW MM 33-50-01-2.

Part: CLIP — BROKEN (SLIDE)

EVAC SLIDE CONTAINER LOOSELY ATTACHED. FOUND CLIP BROKEN ON HOUSING, DEFERRED EVAC SLIDE INOP PER MEL 52-7-4. SLIDE REMOVED FROM DOOR AND SECURED IN COURIER SEATS PER MEL1 D318486. REPLACED LATCH ON EVAC SLIDE COVER. INSTALLED SLIDE AND CONTAINER ON FWD ENTRY DOOR PER MM 25-60-01-2. M318486 CLEARED.

Part: ESCAPE ROPE — DEPLOYED (COVER)

CAPT SIDE ESCAPE ROPE DEPLOYED, COVER WON'T STAY ON. STOWED ESCAPE ROPE AND PROPERLY INSTALLED COVER ASSY. OK FOR SERVICE.

Part: THROTTLE — STUCK (ENGINE)

NR 2 THROTTLE STUCK IN IDLE DURING VISUAL APPROACH. NR 2 AND NR 3 REVERSERS USED IN FLIGHT PRIOR TO APPROACH. DURING T/S RAN ENG NR 2 & CYCLED T/R 3 TIMES AFTER CYCLING T/R THROTTLE CLD ONLY ADVANCE 2-3 BEFORE JAMB WITH ENG SHUTDOWN THROTTLE WLD MOVE FULL TRAVEL W/O JAMMING KN 0558726. PERFORMED VISUAL INSP OF NR 2 ENG T/R CAM ASSY ON PYLON, INSP THROTTLE BOX LINKAGE. RAN ENG AND SYC T/R & THROTTLE NORM C/W 76-11-00-2 A/C OK FOR SERVICE.

Part: DOOR — OPEN (CARGO BAY)

NR 3 PIT DOOR OPENED ON LANDING A/C OOS. 11832 ASSIGNED TO THIS WRITE UP 0557984 C/W ALL ITEMS ON ECA FORM 11832, SYS OPS CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK. OPS CK NORMAL.

Part: SPRING — FAILED (PEDESTAL LOCKOUT)

NR 1 & 4 ENGINE REVERSERS WENT INTO REVERSE IN FLIGHT. REINSTALLED NR 1 & 4 T/R LOCKOUT SPRINGS PER MM 76-11-00, OPS CHECK GOOD. REINSTALLED PNLS 573A AND 573B PER MM 53-21-01 AND REINSTALLED CAPT AND CO-PILOTS SEATS PER MM 25-11-01. RESET STALL WARNING C/B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, A-PIT DOOR AFT TORQUE BOX FS 340 FWD UPPER FRAME HAS EXFOLIATION CORROSION FROM L33R TO L34R. REPAIRED DAMAGED FRAME AT FS 340 IAW SRM 53-2-0 FIG 2. REMOVED, FABRICATED & INSTALLED 2 INTERCOSTALS IAW DWG 9754020 & SRM 51-1-21 & 51-1-21 & 51-1-20D. FABRICATED & INSTALLED REPAIR DOUBLER FOR TORQUE BOX WEB IAW SRM ADDENDUM DC8-5350-7876-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE-C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, STA 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, MAIN CARGO FS 781 RBL 62 BOOT FITTING CRACKED AT RADIUS FWD AND AFT SIDES BELOW FLOORLINE. REMOVED BOOT FITTING AT FS 781 RBL 62 IAW SRM 51-1-21. FABRICATED BOOT FITTING IAW SAA SK 729-576. INSTALLED BOOT FITTING IAW SRM 51-1-20D & 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, FS 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, AFT MAIN CARGO FS 1750 L36 INTERCOSTAL FWD OF VERTICAL BEAM CRACKED. REMOVED INTERCOSTAL IAW SRM 51-1-21 & 51-3-0. FABBED INTERCOSTAL ON TRAVLER 0007 PER DWG 5773844. INSTALLED REPLACED INTERCOSTAL IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (LONGERON) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, LONGERON 10R END FITTING CRACKED AT FS 674. REMOVED AND REPLACED LONGERON 10R END FITTING FS 674-680 IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (CUSP WEB) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, RIGHT UPPER CUSP FITTING CRACKED STA 1174. REMOVED AND REPLACED CRACKED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE:C1, LONGERON 5R END FITTING CRACKED STA 850. REMOVED AND REPLACED FITTING IAW SRM 51-1-21-1-200.

Part: FITTING — CRACKED (LONGERON) · airframe 73,508 hrs · 48,720 cycles

INSPECTION TYPE: C, LONGERON 6R END FITTING CRACKED STA 674. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, OP CHECKED GOOD.

Part: BATTERY — INTERMITTENT (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON EMERGENCY EXIT & EMERGENCY EXIT CONTROL C/B`S PULLED AND RESET EMERGENCY EXIT LIGHTS STILL ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY UNIT PER MM 33 50 01 2, OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE: PFLT, 2 INCH GOUGE IN NR 4 PIT SLOPING WALL 3 FT ALT OF BULKHEAD AFTER PULLING BACK THE LINER, FOUND FRAME CRACKED. REMOVED FLOOR PANEL IN NR 4 PIT RIGHT SIDE FWD TO INSPECT FLOOR SUPPORT FRAME FOR DAMAGE . KMA 56755 / ACCOMPLSIHED PERMANENT REPAIR PER APP C E.O. DC8-5320-8724-A. KMA 56755 REINSTALLED FLOOR PANEL.

Part: SMOKE BARRIER — TORN (COCKPIT)

INSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE CURTAIN HAS A 8 INCH TEAR & HAS COME UNSCURED BOTH IN THE LOWER LT OUTBOARD SIDE. PERFORMED INTERIM REPAIR EO DC8 -2550-1872B TRASFERD TO D-258389 FINAL SMOKE CURTAIN REPAIR ACCOMPLISHED PER UPS E.O. #DC8-2550-1872, APPENDIX 8.3, OK FOR SERVICE.THIS CLEARS D258389

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED NAD REPLACED BATTERY AND RELAY UNIT AND OPS CHECKED GOOD PER MM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.

Part: ATTACH ANGLE — CRACKED (BULKHEAD) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, INTERCOSTAL TO AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT LONGERON 5L AT STA. 1766. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.5773844,AND SRM. 51-1-20D

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, R-1 FWD. SERVICE DOOR HAS INTERCOSTAL CRACKED UPPER AFT CORNER AFT SIDE OF INNER WEB STA. 200-220 LONG. 13R REMOVED INTERCOSTAL,FABRICATED DOUBLER AND FILLER AND INSTALLED I.A.W. SRM. 53-2-0 FIG. 23

Part: FILLER — CORRODED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, SEVERAL STRESS FASTENERS AT STA. 1660 LONG. 31 RT. OPENED SKIN FOUND FILLER CORRODED BEYOND LIMITS, FABRICATED AND REPLACED FILLER IAW DWG. 5773311,AND CLOSED SKIN I.A.W. SRM. 51-1-21,51-1-20D

Part: FRAME — CRACKED (CARGO DOOR) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, A-PIT DOOR FRAME IS CRACKED ABOVE BOX WEB STA. 300 AT LONG. 31R REMOVED,FABRICATED AND INSTALLED FRAME SECTION,DOUBLER AND INSTALLED I.A.W. SRM. 52-2-0 FIG. 2

Part: LONGERON — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE:C2 STA. 1746 LONG. 16L IS CRACKED. CUTOUT DAMAGED AREA FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE I.A.W. SRM. 53-2-2 FIG. 10

Part: INTERCOSTAL — CRACKED (COCKPIT) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, STA. -12 TO -32 INTERCOSTAL BEAM IS CRACKED AT LBL 12 CUTOUT DAMAGE,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 53-2-0 FIG. 1B

Part: FINGER DOUBLER — CORRODED (COCKPIT SUBFLOOR) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, STA. 8 TO -25 AT LBL 60 FINGER DOUBLER IS CORRODED BEYOND LIMITS REMOVED,FABRICATED AND INSTALLED DOUBLER I.A.W. DWG.5612298,AND SRM. 51-1-21,51-1-20D

Part: RIB — CRACKED (RT WING LE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE:C2 RT WING LE UPPER RIB IS CRACKED AT XFS 797.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG. 2

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, C-PIT DOOR HAS A CRACKED INTERCOSTAL ABOVE LOWER DOOR HOOK AT STA. 1176 AT LONG. 32R AREA ON DOOR. CUTOUT CRACKED INTERCOSTAL, FABRICATED INTERCOSTAL SECTION, AND DOUBLER I.A.W. SRM. 52-2-0 FIG. 2

Part: FITTING — CORRODED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, STA. 1600-1620 LONGERON 36 AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED,AND REPLACED LONGERON SECTION AND END FITTING I.A.W. DWG. DC8-53B-009-39,AND SRM. 53-2-2 FIG. 10

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, CARGO DOOR HAS FWD ANGLE UNDER SEAL AREA, CRACKED AT STA 280 BETWEEN LONG 28 TO 31 RT. REMOVED AND REPLACED ANGLE IAW DWG 5754260,AND SRM. 51-1-21

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,641 hrs · 48,033 cycles

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

Part: ATTACH FITTING — CRACKED (MAIN CABIN) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE:C2 STA. 822 FLOORBEAM ATTACH FITTING IS CRACKED AT RBL. 24 REMOVED AND REPLACED FITTING I.A.W. DWG.4646547,AND SRM. 51-1-20D

Part: SKIN — CRACKED (LEFT WING) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, LT WING UPPER SKIN IS CRACKED AT XRS AT STRINGER 9 CUTOUT CRACKED AREA,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM. 57-2-1 FIG. 10

Part: INTERCOSTAL — CRACKED (RT AFT SERVICE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, R-2 AFT RT SERVICE DOOR INTERCOSTAL IS CRACKED AT STA. 1630 AT LONG. 14R APPROX. REMOVED CRACKED INTERCOSTAL SECTION,FABRICATED REPLACEMENT SECTION, DOUBLERS AND INSTALLED I.A.W. SRM. 52-2-0 FIG.2

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STA 1746 BELOW DOUBLER ABOVE LONGERON 16LT. REMOVED DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLERS, AND FINGER DOUBLER I.A.W. SAA SK729-255

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-1 DOOR UPPER FWD CORNER CUTOUT AND REPAIR PER SRM. 53-2-0 FIG. 15. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM.53-2-0 FIG. 15

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-2 DOOR LOWER FWD. CORNER STA. 1620 LONGERON 20L-21L. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SAA SK729-250,AND SRM 53-2-0 FIG. 18

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, FUSELAGE SKIN HAS 2 CRACKS AT CANTED FRAME 1702 AT LONGERON 17L AT STATION 1740. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SAA SK 729-255

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-1 DOOR UPER AFT CORNER AND REPAIR PER SRM. 53-2-0 FIG. 15. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM. 53-2-0 FIG. 15

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM R-2 DOOR UPPER AFT CORNER AND REPAIR PER SRM. AT STA. 1660 LONG. 11RT. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER I.A.W. SAA SK 729-895 AND EO DC8-5330-17661-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, REMOVED STEEL DOUBLER FROM R-1 DOOR UPPER AFT CORNER AND REPAIR PER SRM. 53-2-0 FIG. 14. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER I.A.W SRM 53-2-0 FIG. 14

Part: DOUBLER — MISREPAIRED (FUSELAGE) · airframe 72,641 hrs · 48,033 cycles

INSPECTION TYPE: C2, DOUBLER & TRIPLER REPAIR DOES NOT CONFORM TO SRM. ON L-2 DOOR UPPER AFT CORNER STA. 1660 LONG. 11L APPROX. REMOVED EXISTING REPAIR,NDT EXISTING CUTOUT AND VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER I.A.W SRM.53-2-0 FIG. 18

Part: LIGHT — INOPERATIVE (ENTRY DOOR)

INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. OPS CHECK NORMAL, NO DEFECTS NOTED.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE: N/A SKIN CRACK L/T FUSELAGE STATION 1500 ITEM DEFERRED D240904. INSTALLED REPAIR DOUBLER PER EO DC8-5330-17101A.

Part: SWITCH — FAILED (CABIN)

INSPECTION TYPE:N/A NUMBER 2 INS FAILED ON THE WAY TO DFW, RED FLAG APPEARED BUT NO FAULT CODE. IN ATTITUDE REF MODE SMELLED SMOKE TURNED INS OFF AND PULLED CIRCUIT BREAKER. REMOVED AND REPLACED INU BATTERY AND BLOWER VANE SWITCH REF L/P 722257 ITEM 1 AND 722 256 ITEM 3, INS OPS CKS GOOD IAW MM 34-44-00.

Part: WINDOW — OUT OF ADJ (COCKPIT)

INSPECTION TYPE:N/A CAPT SLIDE WINDOW WILL NOT OPEN. PERFORMED ADJUSTMENT OF CAPTS SLIDING WINDOW PER MM 56-10-03 OPS CK GOOD

Part: SEAT — LOOSE (COCKPIT)

INSPECTION TYPE:N/A PILOT REPORT-CAPT SEAT LOOSE. *S/D* REMOVED AND REPLACED CAPTS SEAT, OPS CHECK GOOD IAW MM 25-11-01.

Part: SEAL — LEAKING (COCKPIT PBE)

PBE. IN FLIGHT DECK HAS AIR TIGHT SEAL BROKEN. R & R PBE IN FLIGHT DECK AS REQ''''D. OK FOR SERVICE. S/N

Part: SKIN — CRACKED (SERVICE DOOR)

INSPECTION TYPE:N/A R1 SERVICE DOOR HAS 1 .125 INCH CRACK IN LOWER AFT RADIUS D208801. *S/D* TRANSFERRED TO UPS NON ROUTINE 936452 TO CLEAR D208801. ONE TIME FERRY PERMIT ORD/GSO FOR REPAIR OF R1 DOOR.

Part: SKIN — CRACKED (PAX DOORWAY) · airframe 71,639 hrs · 47,346 cycles

INSPECTION TYPE:L/S R-1 SERVICE DOOR HAS A 1/8 INCH CRACK IN THE LOWER AFT RADIUS OF THE FUSELAGE SKIN. ROUTED OUT CRACKED SKIN, VERIFIED NO CRACK REMAINING IAW DC8 SRM NDT SRM 06-10-11-001. FABBED DOUBLERS AND FILLERS, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 AND DC8 SRM 51-1-8. PERFORM A NDT INSPECTION PROCEDURE S/N 08550001-7001 AT RECOMMENDED INSP INTERVALS PSE NO 53.08.039 FWD OF STA 9-680.50, APPLIES TO THIS FIGURE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

INSPECTION TYPE: BTB - ABORTED TAKEOFF TWICE DUE MASTER WARNING LIGHT FLICKERED ON AND OFF AT 40 KTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: LONGERON — CRACKED (CABIN) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1640 AFT SIDELONG 34L IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON SEGMENT IAW DWG 3647110 AND SRM 51-1-20D, 51-1-21.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123 A PITT CROSSLIDE DOOR FRAME/BEAM IS CORRODED BEYOND LIMITS AT STA. 330 LONG. 22R ON DOOR REPAIRED FRAME I.A.W. SRM. 52-2-0 FIG. 2

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 172.5. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.

Part: FRAME — CORRODED (AFT LOWER CARGO) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1380 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: SKIN — DAMAGED (RT WING L/E) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123 RIGHT WING L/E UPPER SKIN IS DAMAGED BEYOND LIMITS AT XFS 397.750. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 370 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21.

Part: FITTING — CORRODED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 300 LONG 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1770 LONG 17R END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 600 - 620 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1770 LONG 17L END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 600 - 620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XS 478.897, XFS 372.75, XFS 379 AT FASTENER END. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 360.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW 5769589, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (RIGHT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 297.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 803.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT FASTENER END AT XFS 347.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 566.25, 610, 628.75 AT FASTENER END. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1770 LONG 19R SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE.

Part: RIB — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT FASTENER END AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RIGHT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT STA XFS.347.75. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (LEFT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS250. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1180 BATHTUB FITTING BETWEEN LONG 34R - 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1140 - 1153 LONG 33R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (CABIN) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1690 LONG 26L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1153 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, A CARGO PIT CROSS-SLIDE DOOR FRAME IS CORRODED BEYOND LIMITS AT STA 300 LONG 22R ON DOOR. REPAIRED FRAME IAW SRM 52-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT STA XFS 653.750. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1690 LONG 26R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D, 51-3-0.

Part: FLOORBEAM — MISDRILLED (ACCESSORY BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1620 FLOORBEAM HAS MISDRILLED HOLES AT RBL 20. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 729-533.

Part: FITTING — CORRODED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1050 LONG 35L SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 1050 LONG 23R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750159 AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 55 - 70 LONG 36 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3702969 AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (RT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER SKIN IS CRACKED AT XS 435.789. REPAIRED SKIN IAW DC8-5720-7787-A.

Part: ANGLE — CRACKED (CABIN) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, STA 700 LONG 5R INTERCOSTAL ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5714175 AND SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING LE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER SKIN IS CRACKED AT XS 435.789, 7 INCHES AFT OF SLOT PANEL. REPAIRED SKIN IAW DC8-5720-7787-A.

Part: SKIN — CRACKED (RT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER SKIN IS CRACKED AT XS 248.089. REPAIRED SKIN IAW DC8-5720-7767.

Part: SKIN — CRACKED (RT WING) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 385.25 TO XFS 391.5. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: VANE — CORRODED (LT WING LE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, LEFT WING LEADING EDGE O/B SLOT VANE IS CORRODED BEYOND LIMITS AT XOLDI 6.225. REPAIRED VANE SKIN IAW SRM 57-2-1 FIG 2H.

Part: SKIN — CRACKED (RT WING LE) · airframe 71,411 hrs · 47,192 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER SKIN IS CRACKED AT STA XFS 207.5. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-00-00.

Part: INTERCOM — INOP (RT COCKPIT)

INSPECTION TYPE:N/A, F/O'S OXYGEN MASK INTERCOM DOES NOT WORK. REMOVED AND REPLACED F/O'S O2 MASK. PERFORMED LEAK CK AND OPS CK GOOD PER MM 35-00.

Part: SKIN — CRACKED (LT WING)

MAINTENANCE FOUND LEFT WING LOWER SURFACE, APPROX 16 INCHES INBOARD OF NR 1 PYLON, CRACKED SKIN APPROX 4 INCHES LONG. ROUTED OUT CRACKED AREA IAW REO-06635. FABRICATED FILLER, INTERNAL DOUBLERS AND TRIPLERS, EXTERNAL DOUBLER AND TRIPLER IAW REO-O6635. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 81-1-20D AND REO-O6635.

Part: SHEAR TIE — CORRODED (BS 640)

INSPECTION TYPE-C, CORROSION AT FS 640 AT LONG 36 AND 34R, LWR FWD BULKHEAD LWR T-CHORD SHEAR TIE IS BLOWN OUT WITH HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5616509 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 428)

INSPECTION TYPE-C, RT WING LWR SKIN AT STA XRS 428 AND BETWEEN STR 62 TO 64 IS CRACKED. REPAIRED AREA IAW DHC SK 729-237.

Part: SHEAR TIE — CRACKED (BS 280)

INSPECTION TYPE:C SHEAR TIE FITTING AT F/S 280 BETWEEN L-35L TO 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (WS 70)

INSPECTION TYPE-C, RT WING UPPER SKIN STA XRS 70 AT STRINGER 16 HAS A STRESS CORROSION CRACK. REPAIRED IAW SRM 57-2-1.

Part: FITTING — CRACKED (BS 270)

INSPECTION TYPE:C FWD LOWER CARGO BATHTUB FITTING CRACKED AT F/S 270 BETWEEN LONG 35L- 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING LE)

INSPECTION TYPE-C, LT WING L/E INNER DOUBLER AROUND SMALL LWR SWING DOWN PANEL UNDER I/B FIRE BOTTLE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5641252.

Part: FITTING — CRACKED (BS 450)

INSPECTION TYPE-C, LONGERON 31L SPLICE FITTING CRACKED AT FS 450. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (BS 680)

INSPECTION TYPE-C, FS 680, RBL 24, THE FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 4645517 AND SRM 51-1-20D.

Part: WEB — CRACKED (BS 680)

INSPECTION TYPE-C, STA 680 LWR PRESS WEB AT LBL 29 IS CRACKED. REPAIRED AREA IAW SRM 53-2-5.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE-C, CRACKED FITTING FS 700 AT UPPER CUSP IN MAIN CABIN LT. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: LONGERON — CRACKED (BS 270-280)

INSPECTION TYPE:C FWD LOWER CARGO LONG 36 HAS A CRACK ON THE LOWER FLANGE BETWEEN F/S 270-280. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-2-2.

Part: FLOORBEAM — CRACKED (BS 1160)

INSPECTION TYPE:C F/S 1160 AT THE RT CUSP, THE FLOORBEAM TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3754946.

Part: FITTING — CRACKED (BS 270)

INSPECTION TYPE-C FS STA 270 AT LONG 33R TO 30R THE TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1334)

INSPECTION TYPE-C, FS 1334 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1288)

INSPECTION TYPE-C, FS 1288 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-2OD AND SRM 51-3-0.

Part: RIB — CRACKED (WS 250.09)

INSPECTION TYPE-C, LT WING L/E RIB AT XS 250.089 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1280)

INSPECTION TYPE-C, STA 1280 AT STR 21L, THE FRAME TO CUSP LWR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9755536 AND SRM 51-1-20D.

Part: SKIN — CRACKED (SERVICE DOOR)

INSPECTION TYPE-C, AFT SERVICE DOOR NR 17 FWD LWR CORNER CRACK ON INNER SKIN FROM EDGE TO FASTENER .625 INCH LONG. REPAIRED IAW UPS EO DC8-5330-10839-A.

Part: RIB — CRACKED (WS 691.25)

INSPECTION TYPE-C, LT WING L/E RIB AT XFS 691.250 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: CARGO TRACK — CORRODED (BS 1330-1410)

INSPECTION TYPE:C LOWER CARGO TRACK CORRODED F/S 1330-1410 L-34L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5779223.

Part: RIB — CRACKED (WS 385.25)

INSPECTION TYPE-C, LT WING L/E RIB AT XFS 385.25 IS CRACKED 16 FWD OF THE T/E. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: WEB — CRACKED (PAX DOOR)

INSPECTION TYPE-C, FWD ENTRY DOOR INNER SKIN AT THE BAYONET CUTOUT IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 52-2-0.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING L/E VERTICAL FWD ANGLE CRACKED AT O/B END OF THE I/B SLOT. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE-C, STA 1220 RT SIDE, THE FLOORBEAM SUPPORT FITTING HAS A 5 INCH CRACK. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1396)

INSPECTION TYPE-C, STA 1396 AT STR 21L, THE FRAME TIE FITTING HAS A 9 INCH CRACK. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755584.

Part: LONGERON — CRACKED (BS 290)

INSPECTION TYPE-C, STA 290 AT STR 35L O/B LEG IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (WS 98)

INSPECTION TYPE-C, THE RT LWR AUX SPAR TO REAR SPAR STA 98 TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 729-846 AND SRM 51-3-0.

Part: SKIN — CRACKED (WS 163.75)

INSPECTION TYPE-C, RT WING L/E LWR SKIN AT XFS 163.75 IS CRACKED JUST FWD OF THE REPAIR DOUBLER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2A.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE-C, TR WING UPPER SKIN AT XRS 74 AND STR 12 HAS A STRESS CORROSION CRACK. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 10.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING L/E SKIN INTERNAL DOUBLER AT THE NR 3 PYLON CUTOUT IS CRACKED AT THE OPENING. REPAIRED IAW SRM 57-2-1.

Part: FITTING — CORRODED (BS 960)

INSPECTION TYPE-C, FITTING LT W/W AT LONG 23L FS 960 HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 8.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE-C, RT WING L/E VERTICAL ANGE JUST I/B OF XS 250.089 AND AFT OF THE SLOT IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (WS 258)

INSPECTION TYPE-C, RT WING L/E SKIN AT THE L/E XW 258 IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: RIB — CRACKED (WS 691)

INSPECTION TYPE-C, RT WING L/E RIB AT STA 691.25 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 622.5&629.75)

INSPECTION TYPE-C, RT WING L/E UPPER SKIN XFS 622.5 AND 628.75 IS CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-C, RT WING L/E RIB AT XFS 653.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE-C, THE RT I/B AILERON UPPER L/E SKIN AT THE ACTUATOR IS CRACKED AT ONE SCREW HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-1-21 AND DWG 5705334.

Part: LONGERON — CORRODED (BS 285-295)

INSPECTION TYPE:C LONGERON 35L CORRODED F/S 285-295. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2-2.

Part: STIFFENER — CORRODED (BS 8)

INSPECTION TYPE-C, A/C COMPT FS 8 AT LONG 28R, THE VERTICAL STIFFENER IS CORRODED. REMOVED, FABRICATED AND REPLACED VERTICAL STIFFENER IAW DWG 5615530 AND SRM 51-1-21 AND 51-1-20D.

Part: DOUBLER — CORRODED (FWD LAV SERVICE)

INSPECTION TYPE:C FWD EXTERNAL RT FUSELAGE CORROSION ON PANEL LAND AT DEACTIVATED LAVATORY SERVICE PANEL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, DWG 5755443, AND DHC SK-729-598.

Part: SKIN — CORRODED (FUSELAGE)

TWO RIVETS POPPED ON FUSELAGE SKIN ABOUT SIX FEET AFT OF NR 4 PIT DOOR. COMPLIED WITH EO DC8-5330-10186A.

Part: INPUT ROD — BINDING (LT ELEVATOR TAB)

AIR TURN BACK, BINDING IN ELEVATOR, FULL TRAVEL, DURING CLIMB-OUT. A/C LANDED AT 261.0, MAX LANDING WEIGHT 258.0. FOUND INPUT ROD ON LT ELEVATOR CONTROL TAB BINDING. LOOSENED CASTLE NUT ON CONTROL ROD BOLT TO RELIEVE BINDING. ELEVATOR OPS CHKS GOOD PER MM 27-30-00.

Part: AIR DISTR — ODOR (COCKPIT)

INSPECTION TYPE-N/A, 25 MINUTES INTO FLIGHT STRONG ODOR SMELLED LIKE BURNING RUBBER. DONNED OXYGEN MASK, EMERGENCY DECLARED AND ALL CHECKLIST COMPLIED WITH. SMELL SEEMED STRONGER IN COCKPIT, NO VISIBLE SMOKE. RAN ALL 4 ENGINES, ALL ELECTRICAL SYSTEMS POWERED UP, BOTH PACKS ON FULL FLOW, CYCLED ENGINE BLEEDS AND COULD NOT DUPLICATE PROBLEM. INSPECTED AIR CONDITION BAYS, LOWER E AND E COMPARTMENTS, RADIO RACKS, C/B PANELS, EQUIPMENT COMPARTMENTS UNDER AND NEXT TO F/E DESK, NO DISCREPANCIES NOTED AT THIS TIME.

Part: LIGHTS — INOPERATIVE (CABIN)

INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS WOULD NOT DISARM. RELAMPED, CHECKED GOOD.

Part: LONGERON — CORROSION (BS 8-70)

INSPECTION TYPE SPEC, LONGERON 32L HAS HEAVY CORROSION AT FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-21 AND SRM 51-3-0.

Part: DOUBLER — CORROSION (LT/RT NLG DOOR)

INSPECTION TYPE SPEC, LT AND RT NOSE LANDING GEAR DOOR ACCESS PLATE INNER DOUBLERS HEAVILY CORRODED. REPLACED INNER DOUBLERS PER SRM 51-1-20D AND SRM 51-1-21.

Part: LONGERON — CRACKED (BS 70-60)

INSPECTION TYPE SPEC, LONGERON 36 CRACKED AT FS 70 TO 60. REPLACED LONGERON SECTION FS 60 TO 70 PER SRM 51-1-21 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 60-70)

INSPECTION TYPE SPEC, LONGERON 335R CRACKED AT FS 60 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-20D AND SRM 51-1-21.

Part: SHEAR TIE — CRACKED (BS 55)

INSPECTION TYPE SPEC, SHEAR TIE CRACKED ON OUTBOARD END AT LONGERON 34L FS 55. REPAIRED SHEAR TIE PER SRM 53-2-0.

Part: LONGERON — CORROSION (BS 8-70)

INSPECTION TYPE SPEC, HEAVY CORROSION ON LONGERON 33R, FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-3-0.

Part: SKIN — CORROSION (BS 25)

INSPECTION TYPE SPEC, INTERIM REPAIR DUE TO HEAVY CORROSION, NEED PERMANENT REPAIR AT FUSEL AGE SKIN, FS 25 LONGERON 36. REPLACED SKIN SECTION FS 70 TO 8 LONGERONS 31L AND 31R PER DRAWING NR DAC56138 62 AND UPS EO.

Part: SKIN — CORRODED (FS 1690-1720)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE AFT SKIN BUCKLED AND CORRODED BEYOND LIMITS AT FS 1690 TO FS 1720, LONG 33L TO LONG 33R. CUT OUT DAMAGED AREA AND SPLICED IN NEW SKIN PANEL PER SRM 53-2-1, FIG 8.

Part: FITTING — CORRODED (BS 300)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED STA 300 LONG 33R. REMOVED AND REPLACED FITTING AT LONG 33R STA 300 IAW SRM 52-2-0 FIG 2D.

Part: ANGLE — CORRODED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RING SUPPPORT ANGLE FS 1690 CORRODED BEYOND LIMITS, RB 3434 LONG 35L TO 33R. CUT OUT DAMAGED AREA PER SRM 53-2-5 FIG 8C. FABRICATED AND INSTALLED DOUBLER ANGLES AND FILLER PER SRM 53-2-5 FIG 8C.

Part: DOUBLER — CORROSION (BS 1350)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FINGER DOUBLER, ONE EAR BROKEN OFF, STA 1350 LONG 29R TO 30R. REMOVED CORROSION, FOUND SKIN TO BE WITHIN LIMITS AND FINGER DOUBLER TO BE OUT OF LIMITS. FABRICATED FINGER DOUBLER AND INSTALLED ALL PARTS PER UPS SRM 51-1-8, 53-4-1, 51-1-20D AND 51-1-21.

Part: ANGLE — CRACKED (WS 98)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SUPPORT ANGLE CRACKED LWR TWO BOLT HOLES VERTICAL ANGLE O/B FLAP ACT BKT WS 98R. REMOVED, FABRICATED AND INSTALLED ANGLE PER DOUG DWG 3643320 AND SRM 51-1-20, 51-1-20D.

Part: FRAME — CORRODED (BS 180)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED BEYOND LIMITS STA 180 LONG 36. REMOVED, FABRICATED AND INSTALLED FRAME SECTION PER UPS SRM 53-2-0 FIG 2 AND 51-1-21.

Part: WEB — CORROSION (BS 340)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND C-1 PIT BASKET WEB SEVERELY CORRODED FWD OF STA 340 AT LONG 33R. REMOVED DAMAGED PART OF WEB AND REPAIRED PER DHC SK 729-179.

Part: FITTING — CRACKED (LE NR 3 PLYON)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLANGE ON FITTING CRACKED L/E AT PYLON NR 3. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 51-1-20D, 51-1-20, 51-1-21 AND DOUG DWG 5754705.

Part: FITTING — CORROSION (BS 1540)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND AFT ACC COMPT STA 1540 LONG 33R END FITTING CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 53-4-1, 51-1-21, 51-1-21, SEALED PER 51-1-11.

Part: FITTING — CRACKED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CRACKED AT FS 1690 LONG 34R. REMOVED AND REPLACED FITTING IAW SRM 53-1-01.

Part: FITTING — CORRODED (BS 305)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED STA 305 LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (BS 340)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING AT STA 340 LONG 33R IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG D.

Part: DOUBLER — CORRODED (BS 1340-1360)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FINGER DOUBLER FLS 1340 TO 1360 LONG 30L TO 31L. REMOVED DAMAGED FINGER DOUBLER 31L STA 1350 T0 1430, FABRICATED FINGER DOUBLER AND INSTALLED PER SRM 53-4-1 AND 51-1-21.

Part: RIB — CRACKED (WS 226)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING RIB CRACKED UPPER AFT END XFS226. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIRS AND DICTS PER M/M 20-16-00 AND UPS SRM 51-3-0, 57-2-0, 51-1-21, 51-1-20D AND M/M 36-11-00 AND 36-11-01.

Part: DOUBLER — CORROSION (BS 240-260)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERNAL ANTENNA DOUBLER CORRODED BEYOND LIMITS STA 240 TO 260 LONG 34L TO 35L. REMOVED, FABRICATED AND INSTALLED ANTENNA DOUBLER PER UPS SRM 51-9-0, 51-1-21.

Part: ANGLE — CRACKED (BS 280)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND ANGLE CRACKED AT STA 280 ABOVE LONG 36 FWD END OF PIT DOOR. REMOVED AND REPLACED ANGLE PER UPS SRM 53-1-0.

Part: FITTING — CRACKED (BS 1350)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CRACKER AT FWD I/B WALL STA 1350 LONG 36. REMOVED AND REPLACED SPLICE FITTING PER UPS SRM 51-1-20.

Part: STRINGER — CRACKED (WS 484)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND NR 4 ALT TANK STRINGER 54 AT APPROX STA XW484 IS CRACKED ALMOST IN TWO. FABRICATED STRINGER, STRINGER SPLICES AND INSTALLED PER SRM 57-2-2, FIG 3D AND DC8-5710-7559-A.

Part: CHORD — CRACKED (RT WING L/E)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E AT THE OTBD END OF THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. THE CRACK IS APPROX 1.8 INCH. STOP DRILLED CRACK IAW SRM 57-2-0. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-2-0 FIG D.

Part: FITTING — CRACKED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CORRODED AND CRACKED AT FS 1690 LONG 3LR. REMOVED AND REPLACED FITTING IAW SRM 53-1-01.

Part: DOUBLER — CORRODED (BS 70-210)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER CORRODED BEYOND LIMITS, STA 210 TO STA 70 AT LONG 31R. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 51-1-21 AND 53-4-1.

Part: LONGERON — CORRODED (FS 90)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 31L HAS CORRISION AND PREVIOUS REPAIR AT FLIGHT STA 90. REPLACED LONG PER SRM 53-2-2 AND 53-4-1 FIG FROM FS 70 TO FS 210.

Part: FRAME — CORRODED (FS 1320)

WHILE IN FOR D-CHECK, MAINTENANCE FRAME CORRODED BEYOND LIMITS FS 1320 LONG 35L-35R. REPAIRED FRAME PER SRM 51-1-0, 51-1-8, 51-1-11, 51-1-20D AND EO DC8-5310-7547A.

Part: RIB — CRACKED (WS 653.75)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED LOWER AFT END XFS 653.75. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-20.

Part: FITTING — CORRODED (BS 100)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED BEYOND LIMITS FS 100 LONG 36. REMOVED AND REPLACED LONG END FITTING PER SRM 53-1-0 AND 51-1-21.

Part: FITTING — CORRODED (BS 80)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING FS 80 LONG 36 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED END FITTING FROM STATION 70 TO STA 80 AT LONG 36 PER SRM 53-1-0 AND SRM 51-1-21.

Part: SUPPORT — CRACKED (BS 1520)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CRACKED FRAME TO FLOORBEAM SUPPORT FS 1520 LONG 26L. REPAIRED IAW SRM 53-2-0.

Part: SPLICE — CRACKED (FS 1696)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BUTT SPLICE CRACKED AND CORRODED AT LONG 28L AT FS 1696. REMOVED AND REPLACED IAW SRM 51-1-21.

Part: FITTING — CRACKED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION INSIDE BOTH TUB FITTING AT STA 169 LONG 31R.

Part: LONGERON — CORRODED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE LONGERON 36 CORRODED BEYOND LIMITS FS1690. REMOVED DAMAGED SECTION OF LONGERON FS 1690 TO 1717, FABRICATED AND INSTALLED SPLICE SECTION IAW SRM 53-1-0 AND 53-2-2 FIG 10.

Part: DOUBLER — CORRODED (BS 70-90)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND ANTENNA DOUBLER CORRODED BEYOND LIMITS BS 70 TO BS 90 LONG 35L TO 35R. REMOVED, FABRICATED, AND INSTALLED REPLACMENT ANTENNA DOUBLERS PER SDAC DWS 3649127 SRM 51-1-21, 53-1-0.

Part: LONGERON — CORRODED (FS 1340)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND STA 1340 LONG 36 LOWER CHORD RADIUS IS OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-2-0.

Part: RIB — CRACKED (WS 6.225)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED ABOVE PNUEMATIC DUCT. STOP DRILLED CRACK, FABRICATED ANGLE DOUBLER, FILLED AND INSTALLED IAW SRM 57-20 AND 51-1-20D.

Part: FITTING — CRACKED (BS 440-460)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG SPLICE FITTING CRACKED STA 440 TO 460 LONG 17R. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 51-1-20, DOUG DWG 3887799.

Part: FITTING — CRACKED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CRACKED AND CORRODED BEYOND LIMITS, LONG 36 FS 1690. REMOVED AND REPLACED FITTING IAW SRM 53-1-01.

Part: SHEAR TIE — CORRODED (BS 1700)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHEAR TIE CORRODED BEYOND LIMITS LONG 35R STA 1700. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 53-5-1 AND 51-1-21.

Part: LONGERON — CRACKED (BS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 34R CRACKED ON END STA 1690. REMOVED AND REPLACED DAMAGED SECTION PER UPS SRM 53-2-2 AND 5351.

Part: SKIN — CRACKED (WS 711)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING, LE SKIN CRACKED AT SCREW HOLE XFS 711 ON L E LOWER SIDE. CUT OUT DAMAGED AREA PER SRM 57-2-0, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 57-3-0 AND SRM 57-2-0 AT LT WING LOWER SKIN XFS 711.

Part: JAMB FITTING — CRACKED (LT FWD EXIT)

WHILE IN FOR D-CHECK, MAINTENANCE LT FWD TYPE 1 DOOR JAMB, UPPER FWD CORNER FITTING IS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH SRM 51-1-40.

Part: TIE CLIP — CORRODED (FS 1120)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1120 BETWEEN LONG 36 AND 35R, TIE CLIP IS OUT OF LIMITS. REPAIRED TIE CLIP IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 32R CORRODED BEYOND LIMITS AND CRACKED STA 1690. REMOVED DAMAGED SECTION, REPLACED WITH LIKE SECTION PER UPS SRM 53-2-2 AND 53-5-1.

Part: FITTINGS — CORRODED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1690 AT LONG 34L AND 35L BATHTUB FITTINGS ARE CORRODED. REMOVED AND REPLACED 2 BATHTUB FITTINGS IAW SRM 53-1-01.

Part: SKIN — CORRODED (BS 80)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE SKIN BS 80 AT LONGERON 36 CORRODED BEYOND LIMITS FWD OF ANTENNA. REMOVED CORRODED SKIN PANEL FS 70 TO 190 LONG 31L TO 31R PER SRM 51-1-21. FABRICATED REPLACEMENT SKIN PANEL PER DWG 5779925 AND SRM 53-4-1 AND INSTALLED PER SRM 51-1-21 AND SEALED PER SRM 51-1-17.

Part: LONGERON — CORRODED (FS 1540)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 35L CORRODED BEYOND LIMITS STA 1540. FABRICATED LONG SECTION, REMOVED DAMAGE AND INSTALLED FABRICATED SECTION PER SRM 51-1-20D, 53-2-2.

Part: FITTING — CRACKED (BS 270)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG FITTING CRACKED AT STA 270 LONG 31R. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 51-1-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 70)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND I/B END FITTING CRACKED AT STA 70 LONG 31R. REMOVED AND REPLACED I/B END FITTING AT STA 70 LONG 31R PER SRM 51-1-0 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 365)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE CRACKED UNDER GUSSET, WS 365 PANEL 522B ACCESS. FABRICATED PARTS AND INSTALLED REPAIR IAW SRM 57-2-0 AND 51-1-2D.

Part: SPAR CAP — CORRODED (LT AUX SPAR)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING I/B LOWER ANX SPAR CORRODED BEYOND LIMITS. REPLACED LT ANX SPAR PER DOUGLAS BWG 561508 AND SRM 57-1-0.

Part: RIB — CRACKED (WS 811)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED UPPER AFT END STA XFS 811. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21.

Part: RIB — CRACKED (WS 722.5)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING AT BD L/E RIB AT STA XFS 72.25 CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 57-2-0 AT STA XFS 72.25.

Part: RIB — CRACKED (VERT STAB)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB LE LOWER INTERIOR SECTION HAS THE ENDS OF FRAME RIBS CRACKED AT XFS 104.75 LT AND RT, XFS 111.15 AND LT XFS 122.75. STOP DRILLED CRACKS, FABRICATED REPAIR ANGLE AND INSTALLED REPAIR PER SRM 55-2-0 AND 51-1-20D.

Part: RIB — CRACKED (WS 628.75)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING O/B LE RIB STA 628.75 CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE DOUBLER IAW SRM 57-2-0.

Part: RIB — CRACKED (ELEVATOR)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT ELEV WEB CRACKED AT HOLE CUTOUT STA XE 26. REMOVED AND REPLACED WEB AT STA XE 26 IAW SRM 51-1-21 AND 51-1-21A.

Part: RIB — CORRODED (WS 11.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LEFT WING LE UPPER RIB STA XFS 1125 IS CORRODED BEYOND LIMITS. REMOVED RIB, FABED AND INSTALLED RIB IAW SRM 57-2-0 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 610)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LE RIB CRACKED AFT LOWER END XFS 610. STOP DRILLED CRACK, FAB DOUBLER AND INSTALLED PER SRM 57-20 AND 51-1-20D.

Part: LONGERON — CORRODED (FS 100-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 36 CORRODED THROUGH AFT AT FS 100 TO FS 190. REMOVED AND FABRICATED LONGERON 36 FROM FS 100 TO FS 190 AND INSTALLED IAW SRM 53-4-12 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 741.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 212.75)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED UPPER AFT END XFS 212.75. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-3-0 AND 51-30-2.

Part: FITTING — CORRODED (FS 70)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35R END FITTING CORRODED BEYOND LIMITS AT FS 70. REMOVED AND REPLACED END FITTING AT STA 70, LONGERON 35R PER SRM 53-1-0 AND SRM 51-1-21.

Part: LONGERON — CORRODED (BS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35R CORRODED BEYOND LIMITS FROM STA 70 TO 190. REMOVED, FABRICATED AND REPLACED LONGERON 35R FROM STA 70 TO STA 190 IAW SRM 51-1-4 AND SRM 51-1-20D.

Part: SPAR CAP — CORRODED (RT AUX SPAR)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING I/B LOWER AUX SPAR CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANX SPAR RT WING LOWER I/B IAW DWG 5615058 AND SRM 51-1-20.

Part: LONGERON — CORRODED (BS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35L STA 70 TO 190 HAS CORROSION THROUGHOUT AND OVERSIZED HOLES. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-3-2 AND 53-4-1 FIG L9.

Part: FITTING — CRACKED (BS 852.)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERM FITTING CRACKED STA 852, LONG 5R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FITTING — CRACKED (FS 670)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CABIN LONGERON TERMINAL FITTING CRACKED STA 670 LONG 11R. FABRICATED FITTING PER DWG 5750540 AND REPLACED FITTING PER SRM 51-1-20D AND 51-3-0.

Part: LONGERON — CORRODED (FS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32 CORRODED FROM STA 70 TO 190. REMOVED AND FABRICATED REPLACEMENT LONGERON IAW SRM 52-4-1 FIG 29, INSTALLED REPLACEMENT LONGERON 32L STA 190 IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 680)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON SKIN FS 680 FRAME AND LONG 34R. REMOVED FASTENERS AND CORROSION PER SRM 51-1-21, 51-1-20D AND 51-1-8, REPLACED FASTENERS AND REPAIRED PER.

Part: SKIN — CORRODED (BS 660-680)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON SKIN, LONGERON AND TIE CLIP AT FS 660 TO 680 LONG 34L TO 33L. REMOVED FASTENERS SEALANT AND CORROSION PER SRM 51-1-21, 51-1-20D AND 51-1-8. TREATED, PRIMED AND REINSTALLED FASTENERS AND SEALANT PER SRM 51-1-21, 51-1-20D AND 51-1-8.

Part: RIB — CRACKED (WS 741.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 741.25 IS CRACKED AT THE AFT LOWER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21.

Part: RIB — CRACKED (WS 484.895)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XS 484.895 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR IAW SRM 51-1-21, 51-1-20D AND SRM 57-2-0.

Part: SEAT TRACK — CRACKED (FS 281)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN SEAT TRACK RBL 24 POSITION 3 APPROX STA 28 HAS MODERATE CORROSION. REMOVED DAMAGED AREA IAW SRM 53-2-3 FIG 6D AND TR 53-89. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED PLUG IAW SRM 51-1-7 AND SRM 53-2-3 FIG 6D.

Part: LONGERON — CORROSION (FS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 34 LEFT HAS CORROSION THROUGHOUT ENTIRE LENGTH AT FS 70 TO FS 190. FABRICATED AND INSTALLED LONGERON AT FS 70 TO FS 190, LONGERON 34L IAW SRM 53-22 AND SRM 53-4-1 FIG 29.

Part: SHEAR TIE — CORRODED (FS 1702)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHEAR TIE CORRODED STA 1702 BETWEEN LONG 35 AND 34L. REMOVED SHEAR TIE, FABRICATED SHEAR TIE PER SRM 53-5-1 AND INSTALLED IAW SRM 51-1-21.

Part: RIB — CRACKED (WS 448.581)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE RIB AT STA XFS 5448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-21.

Part: INTERCOASTAL — CRACKED (BS 1240)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERCOASTAL CRACKED AT STA 1240 LONG 10L. REPAIR ANGLE FABRICATED AND INSTALLED SRM 53-2-0.

Part: DOUBLER — CORRODED (FS 80-140)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER HAS CORROSION AND GROUND OUT THROUGHOUT AND BULGE AT LONG 31L AT FS 80 TO FS 140. REMOVED FINGER DOUBLER FROM FS 70 TO FS 210, FABRICATED REPLACEMENT DOUBLER IAW SRM 53-4-1, 53-1-0 AND INSTALLED IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 674.)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERM FITTING CRACKED STA 674 LONG 4L. REMOVED FITTING AND INSTALLED REPLACEMENT FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 796)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 796 RBL 02 KEEL BEAM SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTSALLED NEW FITTING IAW DAC DWG 3750727 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 691.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 691.25 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 691.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 766.25 CRACKED AT THE AFT UPPER END. INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D, SRM 51-1-21 AND 57-2-0.

Part: FITTING — CRACKED (FS 852)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERMINAL FITTING CRACKED STA 852 LONGERON 9R. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW SRM 51-1-0, 51-1-20D AND 51-3-1.

Part: RIB — CRACKED (WS 597.5)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED AFT LOWER END XFS 597.5. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 57-2-0, 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 442.185)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE RIB AT STA XFS 442.105 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 57-20 AND 51-1-21.

Part: RIB — CRACKED (WS 26.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LE TANK RIB AT STA XFS 26.25 IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FAB AND INSTALLED ANGLE REPAIR IAW SRM 57-3-0, TREATED AND PRIMED IAW SRM 51-1-8.

Part: SPLICE — CRACKED (WS 67.5)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE RT WING FRONT SPAR UPPER CAP SPLICE ANGLE AT STA XWS 67.5 IS CRACKED. FABRICATED CAP SPLICE ANGLES AND INSTALLED AT STA XWS 67.5 RT WING IAW SRM 57-6-1 AND 51-1-20D.

Part: LONGERON — CORRODED (BS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32L, STA 70 TO 190 CORRODED THROUGHOUT ENTIRE LENGTH BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-2-2 AND 53-4-1.

Part: FITTING — CRACKED (FS 670)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 11L TO FRAME ATTACH FITTING CRACKED BS 670. REMOVED CRACKED FITTING IAW SMR 51-1-20, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 5750540 SRM 51-1-20D AND 51-3-0.

Part: TIE RIB — CRACKED (RT WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD TIE RIB, 1ST RIB OTBD OF THE WHEEL WELL IS CRACKED. REPAIRED CRACK IAW SRM 51-1-2.

Part: STRINGER — CRACKED (RT WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CRACK INDICATION NOTED ON STRINGER 63, AFT FLANGE AT 4TH FASTENER OUTBOARD OF RT PYLON WING INTERSECTION OUTBOARD BRACKET. CRACK EXTENDS FROM FASTENER HOLE EDGE TO THE EDGE OF STRINGER. CUT OUT DAMAGED AREA PER SRM 57-2-2 FIG 3E, FABRICATED AND INSTALLED SECTION STRINGER 63 FROM XRS 378 TO XRS 420 AND TWO SPLICES PER SRM 57-2-2.

Part: RIB — CRACKED (WS 467.323)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE RIB AT XFS 467.323 CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0.

Part: LONGERON — CORROSION (FS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 34R HAS HEAVY CORROSION THROUGH AT FS 70 TO 190 AND OVER SIZE HOLES BEYOND LIMITS. REMOVED AND REPLACED LONG 34R AT FS 70 TO FS 190 IAW SRM 53-2-2, SRM 53-4-1, FIS 29 AND SRM 51-1-20D. FABRICATED REPLACEMENT LONG PER SRM 53-4-1 FIG 29.

Part: RIB — CRACKED (WS 610)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING O/B LE RIB AT STA XFS 610.0 IS CRACKED AT AFT UPPER END. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 SRM 51-1-20D.

Part: RIB — CRACKED (VERT STAB)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB SECTION INTERIOR HAS TWO RIB ENDS CRACKED AT STA ZFS 279 AND ZFS 273. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 55-2-0 AND 51-1-20D.

Part: RIB — CRACKED (WS 70.95)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD L/E RIB AT STA XILD 70.95 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 57-2-0.

Part: RIB — CRACKED (WS 227.335)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD L/E RIB AT STA XS 227.335 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-2-0, 51-1-20D, AND SRM 51-1-21.

Part: LONGERON — CORRODED (BS 70-190)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 33L HAS CORROSION THROUGHOUT ENTIRE LENGHT FROM STA 70 TO 190. REMOVED LONG 33L FROM FS 70 TO 190 PER SRM 53-2-2, 53-4-1 AND 51-1-20D.

Part: RIB — CRACKED (WS 616.25)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LEADING EDGE RIB CRACKED AT XFS 616.25 AT AFT LWR END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0.

Part: FITTING — CRACKED (FS 1690)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BATHTUB FITTING CRACKED AT STATION 1690 LONG 16L. REPLACED FITTING PER SRM 51-1-21 AND 51-3-0.

Part: SKIN — CRACKED (RT WING LE)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT OUTBD LEADING EDGE LOWER SKIN ABOVE NR 4 PYLON IS CRACKED AT PYLON CUTOUT, APPROX 3.4 INCHES LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-1A AND SRM 51-1-20D.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND WHILE DOING A PRE-DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. ATA 25-60-00. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK - OPS CK'D SYSTEM SATISFACTORY.

Part: HYD LINE — CHAFED (RUDDER)

(SUPPLEMENTAL MRR) PILOT REPORTED DURING CLIMBOUT, EXPERIENCED LOSS OF HYD FLUID. FLUID QTY DOWN TO APPROX 6 GALLONS WHEN QRH PROCEDURE COMPLETED. FLUID LEVEL ROSE TO APPROX 7 GALLONS. EMERGENCY PROCEDURES ACCOMPLISHED. ITEM DEFERRED WITH TEMP FLEX HOSE INSTALLED. TEMP FLEX HOSE REPLACED. LK CK OK.

Part: ENGINE — FLAME OUT (NR 1)

PILOT REPORTED NR 1 ENGINE FLAMED OUT AT F/L .350 OAT -59 DEGREES CELSIUS, DURING CYCLING OF NR 1 CROSSFEED. ACCOMPLISHED FUEL TANK TRANSFER CHECKS - ALL NORMAL. INSPECTED INLET/TAIL PIPE NR 1 ENGINE - NO DAMAGE NOTED. REPLACED NR 1 ENGINE FUEL FILTER PRECAUTIONARY - NO FOREIGN MATERIAL. RAN ENGINE - NO LEAKS. NORMAL OPERATION.