N812UP

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.

Part: TAB — PUNCTURED (ELEVATOR)

INSPECTION TYPE:N/A LEFT ELEVATOR INBOARD CONTROL TAB HAS A .3125 INCH PUNCTURE ON BOTTOM OF TAB. TRANS TO NRC 107944. CHECKED LEFT I/B ELEVATOR AREA ON AIRCRAFT SIDE FOR HARDWARE/ATTACH FITTING. NO DISCREPANCY FOUND. OK TO INSTALL ELEVATOR CONTROL TAB. INSTALLED SERVICEABLE LEFT ELEVATOR CONTROL TAB. REF AMM 27-30-02-2. LP 868935.

Part: BATTERY PACK — FAULTY (COCKPIT)

INSPECTION TYPE:N/A DURING PREFLIGHT EMERGENCY LIGHTS BATTERY CHARGING C/B POPPED AND WOULD NOT RESET. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A PIT 31 HAS HOLE IN FLOOR PANEL. A .375 INCH HOLE IN PIT 31 FLOOR PANEL IS LOCATED 33 INCHES AFT OF DOORSILL AND 41 INCHES LEFT OF CENTERLINE. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5320-8724, APPROX A. DEFERRAL OPENED FOR PERMANENT REPAIR WITHIN 30 DAYS. PIT IS USABLE DURING THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT INOP. FOUND EMERGENCY EXIT LIGHT BATTERY PACK LOW DURING PREDEPARTURE CHECK

Part: WIRE — CHAFED (COCKPIT)

SMOKE IN THE COCKPIT FROM BEHIND FE PANEL CLEARED AFTER 30 SECONDS DECLARED EMERGENCY AND LANDED ASAP. OCCURRED DURING DESCENT 12000' 275KTS. REPAIRED CHAFED WIRE L 893L20 BEHIND NR 4 M FUEL QUANTITY GAUGE IAW AMM 20 50 01 8 P 3.

Part: DOUBLER — CRACKED (FS 1766 L34R) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 EXTERIOR OF TAILSKID FAIRING JUST FWD OF DOUBLER HAS RIPPED FASTENER HOLE AND AFT EDGE IS GOUGED. REMOVED DOUBLER IAW SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLER,AND FILLER AT STA 1766 L34L TO L34R IAW SRM 53-02-01 FIG 7, 51-01-08, AND SRM 51-03-02.

Part: INTERCOSTAL — CRACKED (FS 520 L31R) · airframe 76,521 hrs · 25,374 cycles

FOUND CRACKED INTERCOSTAL AT FS 520 BELOW L31R. REMOVED CRACKED INTERCOSTAL AT FS 520 BELOW L31R IAW SRM 51-1-21. FABRICATED, DRILLED, REAMED AND INSTALLED INTERCOSTAL AT FS 520 L31R IAW DWG 51616520, SRM 51-3-2,51-01-08, AND SRM 51-01-20D-0.

Part: STRUCTURE — CORRODED (FS70 L31R-32R) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 EXFOLIATION CORROSION FOUND AT STA 70 STRUCTURE BETWEEN L31R AND L32R. CUT OUT DAMAGED STRUCTURE AT STA 70 BETWEEN L31R AND L33R IAW SRO 08538006, AND SRM 53-02-05. FABRICATED AND INSTALLED DOUBLER CHORD, AND SPLICES IAW SRO 08538006, AND SRM 53-2-5 FIG 8, 53-02-05, 51-1-24, 51-1-8.

Part: SKIN — CORRODED (FS 518 L27R) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 AFTER REMOVAL OF B-PIT SCUFF PLATE TO FOM NDT INSP IAW E0 DC8 5330-20206-D FOUND CORROSION ON SKIN STA 518 L27R. CUT OUT DAMAGED AREA AT STA 518 L27R IAW SAA EA NR 008-5330-01-A0150. FABRICATED AND INSTALLED -2 FILLER, -3 TAPERED SHIM, -4 DOUBLER, -5 TRIPLER AT STA 518 L27R IAW UPS EO DC8-5330-24169-A, SAA EA#008- 5330-01-AO150, BAC MSG#1-179077370-2, BAC MSG NR 1-180512937-2, AND FAA FORM 8100-9 ALL DATED 4/18/06.

Part: FITTING — CORRODED (FS 340 L30L) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 STA 340 L30L FITTING EXFOLIATED, FINGER DOUBLER CORRODED AND MISSING HILOCK COLLAR. REMOVED FITTING AT STA 340 L30L IAW SRM 51-1-20D. REMOVED CORROSION FROM FINGER DOUBLER AND FOUND TO BE WITHIN LIMITS PER SRM 51-1-8. INSTALLED END FITTING AT STA 340 L30L IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1150 L36R) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 STA 1150 BETWEEN L36 AND L35R BATHTUB FITTING CORRODED AND GOUGED. REMOVED BATHTUB FITTING AT STA 1150 L36 AND L35R IAW SRM 51-1-20D. FABRICATED REPAIR ANGLES IAW SRM 53-02-00. INSTALLED REPAIR ANGLES AND NEW BATHTUB FITTING AT STA 1150 L36 AND L35R IAW SRM 53-02-00 SRM 53-02-00 FIG 002D.

Part: FRAME — CORRODED (BS 1120 L36R) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:CC1 STA 1120 AT L36 FRAME HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SECTION OF FRAME AT STA 1120 L36 IAW SRM 53-2-0 FIG 2. FABRICATED AND INSTALLED FILLER, ANGLES, AND FRAME REPAIR ANGLE IAW SRM 53-02-00-002, 53-02-00 FIG 2, AND SRM 51-1-8.

Part: CUSP WEB — CRACKED (FS1280 L21L) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 STA 1280 CUSP CRACK AT LT FITTING. REMOVED DAMAGED CUSP AT STA 1260-1300 LT IAW SRM 53-02-05-0 FIG 015A. FABRICATED AND INSTALLED EXTERNAL DOUBLER, CUSP SEGMENT AND FRAME FITTINGS AT STA 1280 LT STA 1260-1300 IAW SRM 53-02-05-0 FIG 015A, AND SRM 51-01-20D.

Part: FRAME — CORRODED (FS 1700 L36-35R) · airframe 76,521 hrs · 25,374 cycles

FOUND HEAVY CORROSION ON STA 1700 FRAME L36-L35L FWD SIDE. CUT OUT SECTION OF CORRODED FRAME FROM STA 1700 BETWEEN L36 AND L35R IAW SRM 53-2-0. FABRICATED AND INSTALLED 4 REPAIR SPLICES, -7 SPLICE AND FRAME SECTION REPAIR IAW DWG 5612142, AND SRM'S 53-02-00 53-2-0 FIG 2, AND 51-1-20D.

Part: FITTING — CRACKED (FS 902 L4R) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 902 LONGERON 4R FITTING IS CRACKED. R & R END FITTING AT STA 902 LONGERON 4R IAW SRM 51-1-20D, AND SRM 51-1-21.

Part: ANGLE — CRACKED (FS 1766 L6R) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 1766 LONGERON 6R BRACKET CRACKED. REMOVED ANGLE BRACKET AT STA 1766 L6R IAW SRM 51-01-20D. FABRICATED AND INSTALLED ANGLE BRACKET AT STA 1766 L6R IAW DWG 5773844, AND SRM 51-1-20D.

Part: ATTACH ANGLE — CORRODED (FS 820 RBL65) · airframe 76,521 hrs · 25,374 cycles

ATTACH ANGLE AT STA 820 UNDER FLOOR AT RBL65 FWD OF FRAME HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING STA 820 RBL 65 IAW SRM 51-3-2 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1160 L20R) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 1160 L20R FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20D AND DWG NR 9750419.

Part: FITTING — CRACKED (FS 1690 L24R) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 1690 LONGERON END FITTING CRACKED LONGERON 24R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-1-21 AMD 51-3-0.

Part: FITTING — CRACKED (FS 902 L9L) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 902 L9L FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FS 680 L2L) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 680 L2L FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 902 L4L) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 STA 902 LONGERON 4L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L4L IAW SRM 51-3-2, 51-1-20D AND SRM 51-1-21.

Part: FITTING — CRACKED (FS680 L6L) · airframe 76,521 hrs · 25,374 cycles

STA 680 LONGERON 6L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-1-20D, SRM 51-1-21, 51-3-0.

Part: FITTING — CRACKED (FS 680 L3L) · airframe 76,521 hrs · 25,374 cycles

FOUND STA 680 LONGERON 3L FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L3L IAW SRM 51-01-20D, 51-03-00-0, 51-03-01-0.

Part: STIFFENER — CORRODED (FS 857 LBL 45) · airframe 76,521 hrs · 25,374 cycles

HEAVY CORROSION UNDER VERTICAL STIFFENER ON LT W/W 857 BULKHEAD LBL 45, 13" BELOW CEILING. REMOVED VERT STIFFENER AT FS 857 LBL45 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR ANGLE, REPLACEMENT STIFFENER AND SUPPORT ANGLES AT FS 857 LBL45 IAW DWG 5643433, SRM 51-01-24, 51-1-20D.

Part: SKIN — CORRODED (FS 857 L24L) · airframe 76,521 hrs · 25,374 cycles

FOUND STRUCTURE CORRODED FWD OF LT BOTTLE BOLT BARREL NUT, LT W/W FWD UPPER OB CORNER. REPAIRED EXTERNAL SKIN CORROSION AT STA 857 LONGERON 24L AT BAYONET FITTING IAW UPS ENGINEERING FILE NR DC8-53-20543, SAA EA NR 008-5320-01-A0137, BAC SERVICE REQUEST 1-176290103, BAC ROD SKETCH 06-03-31-001, AND FAA FORM 8100-9 ALL DATED 31 MARCH 2006.

Part: STIFFENER — CORRODED (BS 857 RBL40) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 RT W/W STA 857 BULKHEAD VERTICAL STIFFENER CORRODED BEYOND LIMITS RBL 46, 13" BELOW CEILING. REMOVED VERTICAL STIFFENER AT STA 857 RBL40 IAW SRM 51-01-21, AND SRM 51-01-20D. FABRICATED AND INSTALLED ANGLES,"L" ANGLES, AND VERTICAL STIFFENER AT STA 857 RBL 40 IAW DWG 5643433, AND SRM 51-1-8, 51-01-20D.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 76,521 hrs · 25,374 cycles

INSPECTION TYPE:C1 EXTERIOR SKIN CRACK, TORN ON RMLG IB DOOR AT STRUT EXTENSION. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-06-03, 52-02-00-0, AND 51-1-21.

Part: SKIN — CORRODED (FS 1890 34L-34R) · airframe 76,521 hrs · 25,374 cycles

FUSELAGE SKIN AT SPLICE BETWEEN FUSELAGE AND TAILCONE BETWEEN LONGERON 34L- 34R HAS CORROSION APPEARS TO GO UNDER DOUBLER ON FUSELAGE SIDE STA 1890. REMOVED DOUBLER, REMOVED CORROSION FROM SKIN AND FOUND TO BE WITHIN LIMITS. FABRICATED AND INSTALLED DOUBLER IAW SRM51-1-21,51-1-8, 53-2-00 FIG 23.

Part: SKIN — DENTED (FS 1670 L17L) · airframe 76,521 hrs · 25,374 cycles

DENTS 2 EACH AFT OF SERVICE DOOR L-2 AT STA 1670 L17L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM53-2-1 FIG 10.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK)

CAPTAINS O2 MASK MIC INOP.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHTS BATTERY LOW ON PREFLIGHT CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. ALL SWITCHES & BREAKERS WERE OFF PRIOR TO TEST. REPLACED BATTERY PACK, OPS CHECK OK.

Part: SLIDE — DETERIORATED (CABIN)

GIRT BAR CABLE UNHOOKED FROM RAFT. UPON FURTHER INSPECTION FOUND SEVERAL AREAS OF DETERIORATION ON SLIDE. REMOVED AND REPLACED DOOR SLIDE IAW MM 25-60-01-2.

Part: CONTROL PANEL — FAILED (NR 4)

N/A DURING TAXI OUR AND JUST BEFORE TAKEOFF, WE GOT A BUSS POWER FAIL LIGHT AND NR 4 GEN UNPARRALLED LIGHT ON. SMOKE BEGAN TO ACCUMULATE IN THE COCKPIT. TAXIED BACK TO RAMP. FOUND NR 4 GCP TO HAVE A HARD FAILURE. SUSPECT NR 4 GCP AS CAUSE OF SMOKE. RAN A/C PNEUMATIC SYSTEM, CHECKS NORMAL. REMOVED AND REPLACED NR 4 GCP IAW MM 24-20-0 6-2. PERFORMED OPERATIONAL CHECK IAW MM 24-20-00-0, OPS CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 786 TO 798 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 750 TO 810 IAW SRM 53-2-3 FIG 14.

Part: WEB — CORRODED (AFT LOWER CARGO) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, STATION 1190 LONG 33L UPPER WEB IS CORRODED BEYOND LIMITS, WEB BELOW C-PIT DOOR. BLENDED OUT CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 25.

Part: FITTING — CORRODED (LT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS IAW SB 27-164.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 25 AT LONG 21L ANGLE IN FWD ENTRY DOOR FWD JAMB IS CRACKED. REMOVED, CRACKED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL IAW DWG 5597646 AND SRM 51-1-20D, 51-1-21.

Part: FRAME — CORRODED (AFT LOWER CARGO) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, STATION 1040 FRAME IS CORRODED AT LONG 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1150 AT LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 4758514 AND SRM 51-1-20D.

Part: FRAME — CORRODED (AFT LOWER CARGO) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, STATION 1040 FRAME AND FRAME CAP ARE CORRODED BEYOND LIMITS AT LONG. 35L CUTOUT DAMAGED FRAME AT STATION 1040 LONG. 35L, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8-53A-010 AND REPLACED FRAME CAP IAW SRM. 53-1-0,51-1-20D,51-1-21

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 1000 BETWEEN LONG 28L TO 29L SHEAR TIE IS CORRODED. REMOVED, FABRICATED AND REPLACED SPLICE PLATE AND FILLER IAW SRM 53-2-0 FIG 2A AND 2B.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1140 AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 1060 FRAME IS CORRODED BEYOND LIMITS AT LONG 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 CIRCUMFERENTIAL TIE BRACKET IS CRACKED AT LONG 3L AND 3R AT APPROX STATION 1790. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 5612148 AND SRM 51-1-21, 51-1-20D.

Part: SPLICE — CRACKED (FUSLEAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 LONG 35L SPLICE FITTING IS CRACKED STATION 1040-1060. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 1746 LONG 15R IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 1736-1760, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED LONG SPLICE REPAIR IAW SRM 53-2-2 FIG 10.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 1766 LEFT SIDE THE LOWER ATTACH ANGLE AT UPPER CANTED BULKHEAD IS CRACKED BETWEEN LONGERON 9L AND 10L. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 5772706 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2

Part: ANGLE — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING L/E STUBWING HAS VERTICLE ANGLE CRACKED AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753295 AND SRM 51-1-20D, 51-3-0.

Part: SUPPORT ANGLE — CORRODED (FWD LOWER CARGO) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, TORQUE BOX SUPPORT ANGLE IS CORRODED BEYOND LIMITS AT STATION 280 LONG. 33R. REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. 9754020 AND SRM. 51-1-20D.

Part: FITTING — CORRODED (RT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CANOE FITTING I.A.W. DWG. 5614372,M/M.27-51-12, SAA SK 812-411,AND UPS ENGINEERING FILE NUMBER DC8-57-20109

Part: FITTING — CRACKED (CABIN SUBFLOOR) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, SUBFLOOR TO WEB FITTING IS CRACKED AT STA 925 AT LBL 63. REMOVED AND REPLACED FITTING IAW DWG 3649114 AND SRM 51-3-0, 51-1-20D.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CENTER POST UPPER ATTACH ANGLE IS CRACKED STATION 1766 BL 0. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773844 AND SRM 51-1-21, 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 1734 LONG 15L IS CRACKED. CUT OUT DAMAGE LONGERON BETWEEN STATION 1710 TO 1760, FABRICATED AND INSTALLED LONGERON, STRAPS AND SPLICE FITTINGS IAW SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RIGHT WING O/B LEADING EDGE RIB IS CRACKED AT XFS 603.75. CRACK TERMINATES AT FASTENER HOLE, NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 STATION 922 BLB 63 FINGER DOUBLER AND PRESSURE WEB IS CORRODED BEYOND LIMITS. REMOVED FINGER DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FINGER DOUBLERS, FILLER SPLICE STRAP AND REPAIR DOUBLER IAW SRO8530026.

Part: STIFFENER — CRACKED (LT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, LT WING I/B STUB WING HAS VERTICLE STIFFENER CRACKED AT LOWER END AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 LEFT WING I/B STUB WING VERTICAL ANGLE IS CRACKED AT LOWER END AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT PNEUMATIC DUCT SUPPORT AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (LT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER BOLTS AND BRACKET AT LT MLG. RETRACT ACTUATOR LOWER BOLTS ON UPPER MOUNT BRACKET. OVERSIZED FWD. UPPER MOUNT HOLE FOR RETRACT ACTUATOR,FABRICATED AND INSTALLED BUSHING IAW E.O. DC8-5740-1636

Part: RIB — CRACKED (RT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 RIGHT WING L/E LOWER RIB IS CRACKED AT XS 429 AT I/B END OF SLOT HOUSING. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, LEFT WING LEADING EDGE UPPER RIBS ARE CRACKED AT XFS 747.5 AND XFS 753.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: FINGER DOUBLER — CORRODED (FWD LOWER CARGO) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 82 LONG. 31R REMOVED,FABRICATED AND REPLACED FINGER DOUBLER IAW DWG. 5779916 AND SRM. 51-1-20D,51-1-21

Part: RIB — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING LEADING EDGE UPPER RIB IS CRACKED AT XFS 803.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 304 AT PNEUMATIC DUCT SUPPORT. CUT OUT AND STOPDRILLED CRACKED AREA, NDT VERIFIED NO CRACKS AT STOPDRILLS AND CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (RT WING) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER FWD. UPPER BOLT OF RIGHT MAIN LANDING GEAR RETRACT ACTUATOR UPPER MOUNT BRACKET SPOT FACED LUG,OVERSIZED HOLE,FABBED AND INSTALLED FILLER AND REPLACE- MENT BUSHING IAW E.O. DC8-5740-1636

Part: RIB — CRACKED (LT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 810. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (RT H-STAB.) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 91.25 TO XFS103.75, XFS 135-147, XFS 216-228. BLENDED OUT CORROSION, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW SRM 55-2-1 FIG 4.

Part: SKIN — CORRODED (LEFT H-STAB.) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 LEFT HORIZONTAL STAB L/E UPPER SURFACE IS CORRODED BEYOND LIMITS XFS 153.75 TO XFS 161. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4.

Part: RIB — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING LE LOWER RIB IS CRACKED AT XFS 335.25. CUT OUT DAMAGE, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (RT WING LE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE: C3, RT WING CENTER LE. INNER SKIN IS CRACKED AT FASTENER HOLES XW408 TO XS520. REMOVED, FABRICATED AND REPLACED INNER SKIN AND DOUBLER IAW DWG. 5769759 AND 5769857 AND SRM. 51-1-20D,51-1-21

Part: SKIN — DENTED (FUSELAGE) · airframe 75,659 hrs · 24,674 cycles

INSPECTION TYPE:C3 FUSELAGE SKIN HAS A DENT AT STATION -48 LONG 20L. CUT OUT DAMAGE, FABRICATED FILLER, INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: GIRT BAR — OUT OF POSITION (PAX DOOR SLIDE)

INSPECTION TYPE: PFLT, MAIN CABIN DOOR GIRT BAR WON'T ATTACH TO FLOOR MOUNTS. MAIN CABIN DOOR SLIDE DEFERRED PER MEL 52-7-4 REF M271227. REPOSITIONED GIRT BAR, CHECKS OK. REF LP90923

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT COME ON AND GO OFF DURING FLIGHT. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AND RELAY UNIT. PERFORMED OPERATIONAL TEST PER MM 33-50-01. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY AND RELAY UNIT IAW MM 33-50-01. CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A, CORROSION FOUND AT FUSELAGE STATION 1680 STRINGER 28L IN FUSELAGE SKIN. REPAIRED CORROSION PER EO DC8-5330-17295-A IN SKIN PANEL.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS DIM WHEN PERFORMING TEST PER A-CK METHODS. PERFORMED TEST OF POWER SUPPLY VOLTAGE CHECKS OK FOR CONTINUED SERVICE.

Part: SPAR — CRACKED (LT WING)

INSPECTION TYPE:N/A LEFT WING AFT SPAR UPPER CHORD CRACKED. DEFERRED PERMANENT REPAIR PER MM 28-10-01 PG 207 D234849 ASSIGNED.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A CREW REPORTED EMERGENCY EXIT LIGHT INOP. RELAMPED BULB TO EMERGENCY EXIT LIGHT, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT'S BATTERY PACK, OPS CHECK GOOD IAW MM CHAPTER 33.

Part: CONTAINER — DAMAGED (ENTRY DOOR)

INSPECTION TYPE:N/A DEPARTURE, ESCAPE SLIDE FELL OUT WHEN FWD ENTRY DOOR CLOSED. DEFERRED SLIDE CONTAINER DUE TO DAMAGE.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT ARM/DISARM LIGHT INOPERATIVE. RELAMPED AND OPS CHECK GOOD

Part: WINDOW — CRACKED (COCKPIT)

INSPECTION TYPE:IN CAPTAINS CLEARVIEW WINDOW RIGHT LOWER CORNER APPEARS TO BE CRACKED. REMOVED AND REPLACED CAPTS CLEARVIEW WINDOW PER MM 56-10-03 WINDOW CHECK NORMAL.

Part: CIRCUIT BOARD — DIRTY (FIRE DETECTION)

INSPECTION TYPE:N/A, NR 4 ENGINE FIRE DETECTION, NO TEST. CLEANED AND RE-RACK CARD A-6, OP CK NORMAL, WAIT NO HELP. OPENED NR 4 THRUST COWLING AND CLEANED ELECTRICAL CANNON PLUG AT PYLON. GROUND CHECK PERFORMED AND FOUND OK.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1, STA 270 - 280 LONG 27R INTERCOSTAL ATTACH ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754020 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1, WING BOX STA 680 LBL 60 FITTING IS CRACKED, UPPER SPAR CAP TO FRAME FITTING. REMOVED AND REPLACED FITTING IAW DWG 3642974 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C123 LONG 19R INTERCOSTAL ATTACH FITTING CRACKED FS 834. REMOVED, FAB AND REPLACED FITTING IAW DWG 3779874 & SRM 51-1-20D.

Part: FRAME — CORRODED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1260 FRAME IS CORRODED BEYOND LIMITS AFT SIDE AT LONG 36. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 208 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755211 AND SRM 51-1-20D.

Part: SKIN — CRACKED (PAX DOOR) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LT CABIN AFT ENTRY DOOR INNER SKIN IS CRACKED AT CENTER CUTOUT AREA STA 1440 LONG 12L. REPAIRED IAW SRM 52-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XW 454. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 CROSS SLIDE DOOR FITTING CRACKED FS 320 AT LONG 27L. REMOVED, FAB & REPLACED SPLICE FITTING IAW DWG 9751879 & SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 320 LONG 27L FRAME DOOR STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW 4897274, AND SRM 51-3-0.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (NOSE) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 FRAME IN RT NOSE TUNNEL CRACKED FS 12. REMOVED, FAB & REPLACED INTERCOSTAL IAW SRM 53-3-3 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 280 A PIT DOOR ANGLE SUPPORT FITTING IS BROKEN BETWEEN LONG 26R AND 27R INSIDE LIGHTENING HOLE. REMOVED AND REPLACED FITTING IAW DWG 3754025, AND SRM 51-1-21.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1242 LONG 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 635. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1260 - 1280 LONG 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1160 LONG 27R FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024, AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1580 RBL 48 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-3 FIG 14.

Part: FITTING — CORRODED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1340 - 1360 LONG 30L SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4646163, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 679 LBL 59 FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3642983, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1260 - 1280 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 600 - 620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 FRAME FS 660 CRACKED ABOVE LONG 23R. REMOVED CRACKED SHEAR TIE, FAB AND REPLACED AT FS 660 LONG 23R.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E HAS CRACKED RIBS UPPER SIDE AT XFS 735, 741.25, 778.75, 803.75, 828.75 AND LOWER SIDE AT XFS 785. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 379 AND XS 461. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 797.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XS461.372. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1040 - 1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED IAW DWG 3750257 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1620 RBL 45-48 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW DWG 5758266, AND SRM 53-2-3 FIG 12 AND 51-3-0.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1, STA 1270 - 1280 LONG 35R IS CRACKED ON LOWER SIDE UNDER SPLICE FITTING. REPAIRED IAW 8110-3 APPROVED DH SK 812-345.

Part: RIB — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 716.25 AND XFS 722.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 717 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 341.5. REPAIRED IAW SRM 57-3-3 FIG 5.

Part: SPAR CAP — CORRODED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING AUX TANK UPPER SPAR CAP CORROSION REMOVAL IS BEYOND LIMITS BETWEEN XFS 116 - 126.25. REPAIRED IAW SRM 57-2-1 FIG 37.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 759 RBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (MAIN CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 781 RBL 50 FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 3643111, AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1120 - 1140 LBL 24 SEAT TRACK HAS HEAVY CORROSION AROUND SEAT TRACK PLUGS. REPAIRED IAW SRM 53-2-3 FIG 12.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LOWER FLOORBEAM TO CUSP FITTING CRACKED FS 280 AT LONG 21R. REMOVED, FAB AND REPLACED CUSP FITTING IAW SRM 51-1-21 & 51-3-0.

Part: SKIN — CORRODED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E CORRODED BEYOND LIMITS AT XFS 900. REMOVED, FABRICATED AND REPLACED L/E SKIN IAW DWG 9751896 AND SRM 51-1-21.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 280 AT LONG 27R VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 1766 AFT PRESSURE BULKHEAD ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772398 AND SRM 51-1-21.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 SEAT TRACK CORRODED BEYOND LIMITS AT FS 155 0 BL. REMOVED FAB REPLACED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: ANGLE — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 717 FLOORBEAM SUPPORT ANGLE IS CRACKED AT BL 0. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275 AND SRM 51-1-20D.

Part: FRAME — CRACKED (ACM BAY) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 55 FRAME IS CRACKED BETWEEN LONG 23R AND 24R. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 347.75. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E LOWER SKIN IS CRACKED AT NR 3 PYLON CUTOUT XS 220.190. REPAIRED IAW SRM 57-2-1A FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 603.75 AND XFS 628.75. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 316.5. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CORRODED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: RIB — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 285.25. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E EXT SKIN IS CRACKED AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 781 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750025, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 635.75 AND XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 647.5 AND XFS 655. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: FITTING — CRACKED (CABIN) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 STA 680 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LT WING) · airframe 73,237 hrs · 23,153 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 572.5. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ON PRE-DEPARTURE FOUND EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMER EXIT LIGHT BATT PACK, OPS CKS OK. (P/N 570 8458-503) (S/N 177) ON, (P/N 60-1223-5) (S/N 356) OFF.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS, OPS CK GOOD PER MM 34-50-01. (P/N 60-1223-5) (S/N 356) ON, (P/N 5708458-503) (S/N UPS2964) OFF.

Part: SEAT TRACK — CORRODED (BS 1240-1280)

INSPECTION TYPE-C/CK, RIGHT HAND AFT LOWER CARGO PIT FLOOR TRACK AT STATION 1240 TO 1280, LONGERON 21 RIGHT HAS CORROSION. REMOVED DAMGED SECTION OF TRACK STATION 970 TO 1580 DRILLED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 514. INSTALLED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 51-3-0.

Part: DOUBLER — CORRODED (BS 1480-1680)

INSPECTION TYPE:C/CK AFTER REMOVAL OF SKIN STA 14801 TO 1680 FOUND INTERNAL DOUBLERS AT LONGERON 32 LEFT AND 32 RIGHT TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED DOUBLERS, FABBED DOUBLERS AND FILLER AND ALODINED AND PRIMED AND INSTALLED IAW REO 04866 AND SRM 51-1-8.

Part: LONGERON — CORRODED (BS 1540)

INSPECTION TYPE:C/CK CORROSION AND CRACK LONGERON 33 LEFT STATION 1540. REMOVED DAMAGED SECTION AND FABRICATED STRAPS AND LONGERON. ALODINED AND PRIMED AND INSTALLED IAW DC8 SRM 53-2-2, 51-1-8, 51-1-20D.

Part: JAMB — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-C/CK, MAIN CARGO DOOR AFT JAMB DRILLED HOLE IS CRACKED AND A PIECE IS BROKEN OFF. MATERIAL ID FOR REPAIR .063 2024 T4 IAW DOUGLAS DWG 57772787, HEAT TREATED MATERIAL FROM 2024-0 TO 2024 T4 IAW TPS-1003 REV A. MATERIAL ID FILLER .063 2024 T4 IAW DOUGLAS 5772787. FAB DRILLED DOUBLER AND FILLER FROM 2024 T4 IAW DC8 SRM 53-2-00. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER AND A FILLER IAW DC8 SRM.

Part: FLOORBEAM — CORRODED (BS 1700)

INSPECTION TYPE:C/CK FLOORBEAM FUSELAGE STATION 1700, SEVERLY CORRODED BLO TO LBL 3. REMOVED DAMGED AREA FROM BEAM. FABRICATED INTERNAL DOUBLER, ANGLE, AND FILLER AND SHIMS IAW REO-04822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51-1-20D.

Part: WEB — CRACKED (LT AILERON)

INSPECTION TYPE-C/CK, LEFT HAND INBOARD AILERON, INBOARD WEB, CENTER ACCESS PANEL MATING SURFACE OF THE WEB IS TORN AND CRACKED. FABRICATED REPAIR DOUBLERS AND ALODINED AND PRIMED IAW REO 04825 AND DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04825 AND DC8 SRM 51-1-21, 51-1-21A.

Part: FRAME — CORRODED (BS 1725)

INSPECTION TYPE:C+S2 FS 1725 LONGERON 16R FRAME IS CORRODED/EXFOLIATED NEXT TO LONGERON ATTACH BOLTS. FABBED ANGLE IAW REO-04829 AND INSTALLED IAW DC8 SRM 51-1-21D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE:C+S2 IN NR 3 MAIN TANK JUST OUTBD OF XRS74 LOWER STRINGER NR 51 IS CRACKED IN TWO SEPARATE PLACES ON THE FWD SIDE AND BETWEEN 3 FASTENERS ON THE AFT SIDE. REMOVED CRACKED END FITTING. DRILLED NEW FITTINGS IAW 51-3-2. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (WS 66)

INSPECTION TYPE:C+S2 IN NR 3 MAIN TANK ON INBD SIDE AT APPROX STA XRS 66 TO APPROX XRS 61 LOWER STRINGER NR 51 IS CRACKED ON THE AFT SIDE. REMOVED END FITTING IAW DAC DWG 3704841 PART NR 3704841-501. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN)

INSPECTION TYPE:C/CK STATION 1220 RBL 25 SEAT TRACK SPLIT WITH CORROSION. FABRICATED SEAT TRACK IAW DC8 SRM 53-2-3, ALODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C+S2 FS 280 LONG 35R -36 ZEE FITTING IS CORRODED. INSTALLED NEW FITTING IAW DC8 SSRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 1700)

INSPECTION TYPE:C/CK CORROSION SEAT TRACK D ON UPPER/LOWER SURFACE OF TOP FLANGE AT FUSELAGE STATION 1700. CUT OUT DAMGED SECTION OF TRACK IAW DC8 SRM 51-1-24. DRILLED NEW SPLCIE SECTION IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE SECTION AND NEW SEAT TRACK SECTION IAW DC8 SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 370)

INSPECTION TYPE:C+S2 AFT BANANA FITTING CRACKED AT C-1 DOOR FS 370 AT LONGERON 32R. REMOVED CRACKED FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2, INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: SKIN — DAMAGED (CENTER WING)

INSPECTION TYPE-C/CK, RT WING CENTER LEADING EDGE INBOARD UPPER SKIN 2 SCREW COUNTERSUNK DAMAGED. FABRICATED BUSHING IAW REO 04899, FABRICATED REPAIR DOUBLER IAW REO 04899. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21, INSTALLED REPAIR BUSHING IAW DC8 SRM 51-1-25.

Part: WEB — BROKEN (CARGO DOOR)

INSPECTION TYPE-C/CK, MAIN CARGO DOOR FWD BETWEEN LIGHTENING HOLES 4, 5 HAVE EDGES BROKEN OUT INSIDE. FABRICATED WEB REPAIR, FRAME REPAIR ANGLE AND REPAIR SPLICE ANGLE IAW REO 04929, INSTALLED WEB REPAIR AND ANGLE IAW REO 04929 AND DC8 SRM 51-1-20D, AND 51-1-21.

Part: FLOORBEAM — CORRODED (BS 1580)

INSPECTION TYPE:C/CK FLOORBEAM AT STATION 1580 HAS CORROSION ON FWD LIP IN THE AREA OF LONGERON 22 AND 23 LEFT. REMOVED CORROSION FROM FLOORBEAM MAT REMOVED 50 PERCENT IAW DC8 SRM 53-2-0. FABRICATED FILLER AND 2 ANGLE DOUBLER REPAIR IAW REO 04839 ALODINED AND PRIMED FILLER AND 2 ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04839 AND DC8 SRM 51-1-21.

Part: FLOORBEAM — CRACKED (BS 760)

INSPECTION TYPE:C+S2 CABIN STA 760 X=23 FLOORBEAM FITTING ON AFT SIDE CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: STIFFENER — CRACKED (BS 683)

INSPECTION TYPE:C+S2 CABIN STA 683, X=0 ABOVE C/W BOX VERT STIFFENER CRACKED. MAT ID IAW DOUGLAS DWG-5773275 -1002024-0 PO NR 185371, HEAT TREATED ANGLE FROM 2024-0 .100 TO 2024-T4 .100 IAW TPS -1003. REV AS FABBED ANGLE IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-20D.

Part: STRINGER — CORRODED (BS 450)

INSPECTION TYPE:C+S2 FS 450 LONG 31R CORRODED AND CHIPPED METAL ALONNG EDGES AND FASTENER HOLES AT THE FWD END OF FITTING. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW WITH DC 8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. BLENDED DAMAGE IAW DC8 SRM 53-2-0 DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (VERT STAB)

INSPECTION TYPE:C+S2 VERT STAB AFT SPAR STA ZR297 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: WEB — CRACKED (VERT STAB)

INSPECTION TYPE:C+S2 VERT STAB CLOSEOUT WEB AT ST ZR297 IS CRACKED. CLEANED AREA IAW DC8 SRM 51-1-8. PERFORMED HFEC IAW MIL-STD-271F ON VENT CLOSE OUT WEB ZR297 AFTER CLEANING AREA FOUND CORROSION AROUND RIVET. REMOVED RIVET IAW DC8 SRM 51-1-21. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-1. INSTALLED RIVET IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (BS 702)

INSPECTION TYPE:C+S2 CABIN-STA 702 X=69 (CUSP) AT FLOORBEAM ATTACH FITTING CRACKED. REMOVED OLD FITTING DRILLED UP NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1540)

INSPECTION TYPE:C+S2 CORROSION ON LONGERON 30R AT STA 1540. REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. MAT ID 7075-T6 .050 PO NR 260338, 7075-T6 .080 PO NR 262218, 7075-T6 .160 PO NR 254127 IAW DC8 SRM 53-2-2 FIG 8. FABRICATED REPAIR STRAPS IAW DC8 SRM 53-2-2 FIG 8. ALODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED REPAIR STRAPS IAW DC8 SRM 53-2-2 FIG 8.

Part: FLOORBEAM — CRACKED (BS 702)

INSPECTION TYPE:C+S2 CABIN STA 702 X=23 AT CABIN FLOORBEAM UPPER CHORD UNDER SEAT TRACK CRACKED. REMOVED AND REPLACED FITTING SUPPORT IAW DC8 SRM 51-1-20D.

Part: STIFFINER — CRACKED (BS 683)

INSPECTION TYPE:C/CK COMPLIED WITH FWD BULKHEAD VIEWS FROM CABIN FLOOR STATION 683 X= -2 3 TOP OF VERTICAL STIFFENER BRACKET CRACKED. MATERIAL ID 2024-0 IAW DWG 5773275, HEAT TREATED 2024-0 TO 2024 T4, .100 IAW TPS- 1003 FABRICATED IAW DC8 SRM 51-1-4 AND 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: LINKAGE BOX — CRACKED (HORIZ STAB)

INSPECTION TYPE-C/CK, LEFT HAND HORIZONTAL STABILIZER OUTBOARD GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 216. REMOVED TAB LINKAGE COVER IAW DC8 SRM 51-1-21, WELDED BOX IAW DC8 1 0.301 AND DAC DWG 5652086, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REINSTALLED IAW DC8 SRM 51-1-21.

Part: SPAR — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C+S2 LT HORIZONTL STAB I/B GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 137. REMOVED AND REPLACED IB GEAR TAB LINKAGE BOX IAW DC8 SRM 51-1-21 WELDED EFFECTED AREAS IAW DPS 10.225. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8.

Part: ANGLE — CORROSION (WS 558)

INSPECTION TYPE:C+S2 CORROSION ON RIGHT WING TRAILING EDGE PANEL SUPPORT ANGLE AT XRS 558 .00. ORDER NEW ANGLE RECEIVED NEW ANGLE DRILLED HOLES AND INSTALLED ANGLE IAW DC8 SRM 51-1-21.

Part: SPAR — CRACKED (RT HORIZ STAB)

INSPECTION TYPE:C+S2 RT HORIZONTAL STABILIZER OB GEAR TAB LINKAGE BIX CRACKED AND GOUGED XRS 216. REMOVED RT OB HORIZONTAL STAB GEAR TAB LINKAGE BOX IAW DC8 SRM 51-1- 21 WELDED BOX IAW DPS 10.225 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REINSTALLED BOX IAW DC8 SRM 51-1-21.

Part: STRAP — CRACKED (VERT STAB)

INSPECTION TYPE-C/CK, VERTICAL STABILIZER TO FUSELAGE STRAP, RIGHT HAND SIDE HAS A CRACK AT FASTENERS HOLE FUSELAGE STATION 1765. FABRICATED REPAIR ANGLE AND FILLERS AND ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER AND REPAIR ANGLE IAW DC8 SRM 51-1-20D.

Part: DOOR — CRACKED (LT MLG DOOR)

INSPECTION TYPE:C+S2 LT MLG DOOR CRACKED AT FWD AND AFT DRAIN HOLES OBS EDGE, 2 PLACES LT MLG INBD DOOR, MAT ID 7075-T6 .050 SUBSTITUTED TO 2024-0 .050 HEAT TREATED TO T4 FABRICATED, ALODINED AND INSTALLED ALL IAW DC8 SRM 52-6-1, TP91003 REV A 51-1-8 AND 51-1-21.

Part: LONGERON — CRACKED (BS 290)

INSPECTION TYPE-C/CK, LONGERON 35 LEFT CRACKED FUSELAGE STATION 290. REMOVED AND REPLACED LONGERON 35 LEFT IAW DC8 SRM 51-1-20D AND 51-1-24.

Part: FRAME — CORROSION (BS 80)

INSPECTION TYPE:C+S2 FRAME STA 80 HAS DAMAGE AT L21RT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED SPLICE REPAIR ANGLES AND FRAME SEGMENT IAW DC8 SRM 53-2-0. ALODINED AND PRIMED SPLICE REPAIR ANGLE AND FRAME SEGMENT. INSTALLEDSPLICE REPAIR ANGLES AND FRAME SEGMENT IAW DC8 SRM 53-2-0 IAW DC8 SRM 51-1-8 AND 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (WS 69.500)

INSPECTION TYPE:C+S2 RW UPPER INBD AFT SKIN PANEL AT APPROX STA XCW 69.500 IS CRACKED. CUT ATTACHMENT ANGLE TO FWD END OF CRACK, BLENDED AREA OF CRACK IAW DC8 SRM 57-20-0 FIG 7 FOUND TO BE WITHIN LIMITS, PERFORMED HFEC IAW MIL-STD-271F. FOUND NO CRACKS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA IAW DC8 SRM 51-1-8. FABRICATED ANGLE SPLICE IAW DC8 SRM 53- 20-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SPLICE IAW.

Part: SKIN — CRACKED (L-2 DOOR)

INSPECTION TYPE-C/CK, L-2 DOOR AT FWD LOWER CORNER HAS CRACKED LINE ABOUT 4 INCHES LONG. CUT OUT DAMAGED IAW REO 04856, FABRICATED FILLERS IAW DC8 SRM 53-2-0, 51-1-24, AND REO 04856. FABRICATED DOUBLERS IAW DC8 SRM 53-2-0 AND REO 04856 AND INSTALLED FILLERS AND DOUBLERS IAW DC8 SRM 53-2-0, 51-1-20D AND REO 04856.

Part: PAN — CRACKED (R1 DOORWAY)

INSPECTION TYPE-C/CK, R1 DOOR JAMB AFT LOWER PAN REPAIR IS CRACKED. REMOVED DAMGED SECTION, FABRICATED PAN SECTION SPLICE ANGLE IAW RE O 04777. FABRICATED SEAL DEPRESSOR IAW DAC 5615700. RECEIVED EXTERNAL STRAP FROM SHOP (P/N 3887438-501) PER REO 04777 AND OP 50025. FABRICATED INNER SKIN IAW DAC DWG 5615700. FABRICATED EXTERNAL STRAP IAW DC8 SRM 51-3-2. INSTALLED INNER SKIN PAN, EXTERNAL STRAP.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-WKD, DURING WEEKEND INSPECTION FOUND EMERGENCY LIGHTS DID NOT TEST. SWITCH WAS FOUND IN ON POSITION PRIOR TO TEST. REMOVED, REPLACED AND TESTS EMERGENCY LIGHT BATTERY PACK IAW MM 33-5 0-1. (P/N 5708458-503) ON, (P/N 60-1223-5) OFF, (S/N 404) OFF.

Part: PIN — CRACKED (LT MLG ACT)

INSPECTION TYPE-N/A, NO LEFT GREEN GEAR DOWN LIGHT AND LOUD NOISE. CREW PERFORMED FLY-BY TO CONFIRM LT GEAR DOWN. FOUND GEAR RETRACT ACTUATOR PIN (LWR) SHEARED, IPC 32-10-05 FIG 10. ALSO, FWD/LWR DOWN LOCK LINK BROKEN IPC 32-30-01. REPLACED LOWER RETRACT CYL ATTACHMENT PIN. REPLACED FWD AND AFT LOWER DOWN LOCK LINKS PERFORMED GEAR SWING, ALL CHECKED OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DON'T TEST. REMOVED AND REPLACED EMER EXIT BATTERY PACK, OPS CKS NORMAL.

Part: PROX SENSOR — FAILED (RT MLG)

INSPECTION, INTRANSIT LIGHT SHOWING. REPLACED FAILED RT MLG PROX SENSOR.

Part: PROX SWITH — FAILED (RT MLG)

INSPECTION TYPE N/A, WHEN GEAR EXTENDED, LEFT AND NOSE GREEN, NO GREEN ON RT SIDE, BOTH GEAR AND DOOR RED LIGHTS ON. ALT DOOR LIGHTS ON WITH GEAR RETRACTED AND DOOR RED LIGHTS ON. ALT DOOR LIGHTS ON, FLY-BY INDICATED GEAR DOWN, DOORS CLOSED. DECLARED EMERGENCY PULLED GPWS C/B, L/G C/B. GEAR PINS INSTALLED, A/C TAXIED TO GATE. REMOVED AND REPLACED PROXIMITY BOX (P/N 287) OFF, (P/N 751) ON. SELF TEST ON BOX OK, RUN OPS CHK OF DOOR AND GEAR WARNING LIGHTS PER MM 32-60-00, SYS OPERATES PER CHK 007.

Part: HOOK ASSY — FAILED (MLG)

AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RAN CHECKLIST. SAW SOMETHING WHITE FLAPPING ON RIGHT SIDE OF STRUT. AIR TURN BACK TO DEN. FOUND HOOK ASSY SEPARATED FROM ANTI-RETRACTION ACTUATOR DUE TO CORROSION OF HOOK ASSY. REPLACED HOOK ASSY. GROUND SHIFT CHK NORMAL.

Part: ENGINE — FAILED (NR 1)

INSPECTION TYPE-N/A, LOSS OF OIL QTY FOLLOWED BY LOSS OF OIL PRESSURE AFTER APPROX 2 HRS ON NR 1 ENGINE. INFLIGHT SHUTDOWN ACCOMPLISHED BEFORE PRESSURE GOT BELOW 10 PSI. REPLACED ENGINE.

Part: FITTING — CRACKED (WS 5.812)

RIGHT WING STA ZERO FLAP COVE FWD OF NR 1 FLAP DRIVE FWD PIVOT FITTING CRACKED ABOVE 90 DEGREE SPOILER CABLE BEND PULLEYS. REPLACED FITTING PER SRM 51-1-20D AND EO DC8-5310-8226D.

Part: DOUBLER — CRACKED (WS 22.75)

INSPECTION TYPE-SPEC, LT WING UPPER ACCESS PANEL DOUBLER HAS A 1.5 INCH LONG CRACK WS XRS 22.750 STRINGER NR 6. REPAIRED PER UPS EO.

Part: GIRT BAR — NOT CONNECTED (ESCAPE SLIDE)

MAINTENANCE REPORTED, UNABLE TO ENGAGE METAL BAR OF ESCAPE SLIDE IN ITS ARMED POSITION. REPACKED BOTTOM OF SLIDE DOOR SETS PROPERLY.

Part: ENGINE — FAILED (NR 3)

CREW REPORTED ON CLIMBOUT THROUGH 12,500 FT, NR 3 ENGINE SHUTDOWN WITH LOUD BANG AND RAPID SPOOL DOWN. ADVISED TO RETURN TO SDF. IN PROCESS OF REMOVING AND REPLACING NR 3 ENGINE.

Part: SENSOR — DIRTY (LANDING GEAR DR)

CREW FOUND ON TAKEOFF WHEN GEAR RAISED, GOT DOOR NOT LATCHED LIGHT. DID UPLATCH CHECK THEN GEAR HANDLE BACK UP, LIGHT WENT OUT. INSPECTED, CLEAN AND LUBED DOOR LATCH AND DOOR SENSOR.

Part: SEAT TRACK — CORRODED (FS 70-120)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM OF SEAT TRACK NR 9 F.S. 70-120, RT SIDE. REPLACED IAW SRM 53-02-03.

Part: FITTING — CORRODED (FS 1690)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING F.S. 1690, LONGERON 36 AFT SIDE. REPLACED FITTING IAW SRM 51-1-20D.

Part: ANGLE — CORRODED (FS 330)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ATTACH ANGLE, LONGERON 21R, F.S. 330. REPLACED IAW SRM 51-1-20D.

Part: CHANNEL — CORRODED (FS 1395)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF CHANNEL, F.S. 1395, LONGERON 35R. REPAIRED IAW SRM 53-2-0.

Part: DOUBLER — CORRODED (FS 220-260)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER F.S. 220-260, LONGERONS 32R-35L. REPLACED IAW SRM 51-1-20D, SRM 51-1-21.

Part: FITTING — CORRODED (FS 1270)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE FITTINGS AT F.S. 1270, LONGERONS 35L AND 35R. REPLACED IAW SRM 51-1-20D.

Part: SKIN — CORRODED (FS 1050-1350)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN F.S. 1050-1350. REPLACED SKIN IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 80-145)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32R, F.S. 80-145. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1180/1190)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING F.S. 1180 AND F.S. 1190 BETWEEN LONGERONS 33A-33B, RT SIDE. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 878)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME ATTACH FITTING LT STA. 878. REPAIRED IAW E.O. DC8-5310-7069-A.

Part: SKIN — CORRODED (FS 70-190)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN STA 70-190. REPLACED SKIN IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1175)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING BETWEEN LONGERONS 33A-33B RT, F.S. 1175. REPLACED IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 1220)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L F.S. 1220. REPAIRED IAW SRM DC8-5310-7070A.

Part: FITTING — CORRODED (FS 1346)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CUSP FITTING F.S. 1346, LONGERON 21L. REPLACED IAW SRM 51-3-0.

Part: LONGERON — CORRODED (FS 280-300)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R F.S. 280-300. REPAIRED IAW SRM 53-2-2, 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN UNDER D BAGG IN SCUFF PLATE. REPAIRED IAW DC8-5330-7108-A.

Part: FITTING — CORRODED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON 3RD AND 4TH T-LOCK FITTINGS END OF C X-SLIDE DOOR. REPLACED FITTINGS IAW SRM 51-1-20D, 51-3-0.

Part: FITTING — CORRODED (FS 1240)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING I/B SIDE OF LONGERON 33A, RT F.S. 1240. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1160)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING BETWEEN LONGERONS 35R-36, F.S. 1160. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1400)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING F.S. 1400, LONGERON 21R. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1220)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING AT F.S. 1220, LONGERONS 34R-33R. REPLACED IAW SRM 53-2-0.

Part: FRAME — CORRODED (FS 1060)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON AFT BAG BIN ON TOP OF BELT FRAME B.S. 1060, LONGERONS 35L AND 35R. REPAIRED IAW SRM 53-2-0.

Part: SEAT TRACK — CORRODED (FS 340-380)

WHILE IN C-CHECK, MAINTENANCE FOUND NR 1 SEAT TRACK CORRODED F.S. 340-380. REPLACED IAW SRM 53-2-3.

Part: SKIN — CORRODED (FS 240-260)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION BULGE AT F.S. 240-260, LONGERON 35L. REPAIRED IAW DC8-5330-7046-A.

Part: FRAME — CORRODED (FS 1240)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME F.S. 1240, LONGERON 36. REPAIRED IAW SRM 53-2-0,51-1-20D.

Part: FITTING — CRACKED (FS 760)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM SPLICE FITTING AT FS 760, RBL 20. REPLACED IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FUSELAGE INNER DOUBLER AT RIVET HOLE. REPAIRED IAW DC8-53-1376.

Part: FITTING — CRACKED (FS 1230)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED BANANA FITTING ON AFT SIDE OF FS 1230, BETWEEN LONGS 33R AND 30R. REPLACED IAW SRM 51-4-20D.

Part: FITTING — CRACKED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM END FITTING AT FS 120. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FS 800)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM SPLICE FITTING AT FS 700, FS 720 AND FS 800, RBL 20. REPLACED IAW SRM 51-1-20D.

Part: UPLATCH MECH — OUT OF ADJUST (MLG DOORS)

PILOT REPORTED AFTER GO AROUND, GEAR DOOR NOT LATCHED LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR, LIGHT REMAINED ON. FOUND LT AND RT MLG DOOR UPLATCH MECHANISM HOOK TO ROLLER CLEARANCE NON-EXISTANT, ADJ MAIN GEAR DOOR UPLATCH MECHANISM PER MM 32-31-04. OPS CK OK.

Part: BEAM — CRACK (COMPT. 60)

DURING 'B' CHECK MAINTENANCE FOUND AFT BULKHEAD CRACKED AT HORIZONTAL "J" BEAM SUPPORT, 3RD SUPPORT FROM BOTTOM. INSTALLED REPAIR IAW EO DC8-5310-6669A.