N700UP

Part: BATTERY PACK — DISCHARGED (COCKPIT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK PER AMM 33-50-01-2-4. OPS GOOD.

Part: CONNECTOR — BROKEN (RT MLG)

INSPECTION TYPE:N/A UNSAFE INDICATION RT MLG CYCLED TWICE. WHILE HOLDING FOR 20 MINUTES, CAME ON. IN UNSAFE CONDITION LIGHT CHECK DID NOT WORK. CHANGED LIGHTS WITH UNSAFE INDICATION & FLAPS 35 - THERE WAS NO HORN. FOUND RT MLG DOWNLOCK IND CONNECTOR CORRODED, PIN 5 WOULD NOT LOCK IN, & BACKSHELL ADAPTOR BROKEN. REPLACED CONNECTOR REF SWM 20-31-12. TEMP REPAIRED BACK/CONDUIT WITH REF TO EO DC8-3260-27089A. TEMP REPAIR TO RT MLG DOWNLOCK INDICATION SWITCH CONDUIT IAW EO DC8-3260-27089A TO BE PERMANENTLY REPAIRED IN 30 DAYS.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A IFSD - NR 3 ENGINE FLAMED OUT AT 35000FT W/BOOST PUMP OFF. CREW VERBALLY REPORTED, LEFT NR 3 MAIN BOOST PUMP SWITCH OFF. THIS WILL NOT ALLOW FUEL TO FILL RESERVOIR. ACCOMPLISHED IDLE HIGH FUEL RUN WITH BOOST/FUEL PUMP SWITCH OFF AND NASH PUMP FUEL PRESSURE WAS 18 PSI IDLE 28 PSI AT FULL.

Part: A/C PACK — OVERHEATED (A/C BAY)

NR 3 ENG RUNNING DURING PUSHBACK, ELEC BUSS FAILURE. SMOKE IN FLIGHT DECK WHILE BEING TOWED BACK IN. SDR FILED OPEN, NR 2 PACK OVERHEAT WAS DETERMINED TO BE THE CAUSE OF SMOKE. [SUP 05-07-07] NR 2 PACK WAS FOUND TO BE CAUSE OF SMOKE IN C/P. R&R NR 3 ENG GEN CONT PANEL PER MM 24-20-00. RAN NR 3 ENGINE MANY TIMES WITH LOAD APPLIED. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS INOP, OP PRE-DEP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OP CHECKS GOOD PER MM 33-50-01-2.

Part: BATTERY — NO TEST (EMERGENCY EXIT)

INSPECTION TYPE:N/A ON PREFLIGHT A/C FAILED EMERGENCY EXIT LIGHT PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW DC-8 AMM 33-50-01-2. OPS TEST GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP, LOW VOLTS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A ON DESCENT PASSING 15,000 FT THE LOWER CARGO FIRE AND MASTER CAUTION LIGHTS ILLUMINATED. ACCOMPLISHED CHECKLIST - LIGHTS EXTINGUISHED BETWEEN 5-10,000 FT. DIVERTED TO IAD. COMPLIED WITH OPERATIONAL CHECKS PER MM 26-18-4. NO DEFECTS NOTED, COULD NOT DUPLICATE. DEFERRED LWR CARGO FIRE DET SYS PER MEL 26-10. REMOVED AND REPLACED CENTRAL CONTROL UNIT PER MM 26-18-04-4 PER UPS SAFETY. OPS CHECKS GOOD. THIS CLEARS M340705.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT DURING CRUISE AT FL300. ALL INDICATIONS WERE NORMAL & THE ENGINE WAS RELIT AT FL250. NORMAL OPS REMAINDER OF FLT. PERFORMED T/S PER MM 71-00-00, FIG 139. NO DEFECTS NOTED AT THIS TIME.

Part: ACTUATOR — LEAKING (RT LANDING GEAR)

ATB - LOSS OF MAIN SYS HYD QUANTITY APPROACHING TOP OF CLIMB. CREW DECLARED AN EMERGENCY. REMOVED BOTTOM 90 ELBOW FITTING AND LINE. REPLACED LOWER MG ACTUATOR LOWER LINE AND ELBOW ON CYL. LEAK CHECKED PER 32-32-02-2. LEAK CHECK GOOD. SERVICED HYD RESERVOIR AND HEAD PRESS AS REQUIRED.

Part: SKIN — BROKEN (NR4 SPOILRER) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE-C2 WING UPPER SKIN BROKEN AT IB NOTCH FOR NR 4 SPOILER HINGE, LT WING. CUT OUT DAMAGED AREA ON LT WING SKIN NR4 SPOILER IB HINGE IAW SRM 51-1-21, FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER ON LH WING SKIN HINGE NOTCH AT NR 4 SPOILER IAW SRM 57-02-00 FIG 002

Part: RIB — CRACKED (RT WING) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE-C2 RT WING CRACKED RIB AT STA XS 165. CUT OUT DAMAGED AREA AT RT WING STA XS 165 IAW SRM 57-02-00 FIG002 FABRICATED AND INSTALLED REPAIR DOUBLER ON RIB AT RT WING STA XS 165 IAW SRM 57-02-00 FIG2.

Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 STA 340 RT ACTUATOR ATTACH FITTING CORRODED ON SIDE BRACE ATTACH LUGS. REPAIRED RT FLAP ACTUATOR ATTACH FITTING AT XRS 340 IAW SAA EA NR 008-2760-01-A0364, UPS RAA NR DC8-27-20084, BAC SERV REQUEST ID NR 1-220094385, AND FAA FORM 8100-9.

Part: FITTING — CRACKED (FS 70 L31R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT FS 70 L31R FWD SIDE. REMOVED, LOCATED, DRILLED UP AND INSTALLED END FITTING AT STA 70 L31R IAW SRM 51-1-8 AND DWG 4614397.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 CRACKED LONGERON 23L AT STA 73. REMOVED CRACKED LONGERON 23L IAW SRM 53-02-02-0. LOCATED, DRILLED UP AND INSTALLED LONGERON AND SPLICE FITTING AT STA 73 L23L IAW SRM 53-02-02 FIG 10 AND SRM 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 RT CENTER LE UPPER RIB CRACKED AT XFS416. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57 -2-0, 57-02-00 FIG 2, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1200) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE: C3 FLOORBEAM END FITTING CRACKED BETWEEN OB VERTICAL BOLTS ON FRONT OF PART, STA 1200 RT, IN C-PIT DOOR JAMB. REMOVED CRACKED END FITTING AT STA 1200 LBL 64 IAW SRM 51-1-21 FABRICATED AND INSTALLED END FITTING AT STA 1200 LBL 64 IAW DWG 3754923, AND SRM'S 51-3-2, 51-1-20D, AND 51-1-21

Part: FITTING — CRACKED (FS 1160) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 FLOORBEAM END FITTING CRACKED BETWEEN UPPER I/B VERTICAL BOLTS, COCKPIT DOOR JAMB, STA 1160 RT. REMOVED CRACKED END FITTING AT STA 1160 COCKPIT DOOR JAMB IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED FLOORBEAM END FITTING AT STA 1160 COCKPIT DOOR JAMB IAW SRM 51-03-02, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1766 L17R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 LONGERON CRACKED 1" LONG AT STA 1766 L17R. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-1-21, 53-05-01 FIG 7.

Part: ATTACH ANGLE — CORRODED (FS 1761-1766) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 ATTACH ANGLE CORRODED BEYOND ALLOWABLE LIMIT AT BASE OF APB VERTICAL BEAM, LEFT SIDE, STA 1760-1766. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-1-21 AND 51-3-2D.

Part: ATTACH ANGLE — CORRODED (FS 160) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 STA 160 RT CUSP ATTACH ANGLE IS CORRODED OUT OF LIMITS. REMOVED CORRODED ATTACH ANGLE AT STA 160 RBL 64 IAW SRM 51-1-20D, FABRICATED AND INSTALLED CUSP ATTACH ANGLE AT STA 160 RBL 64 IAW DWG 2649943, SRM 51-3-2 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 880 L24R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 CRACK ON BOTTOM OF L24R, RT WHEEL WELL STA 880, BETWEEN 2 BOLTS. FABRICATED AND INSTALLED -22, -24, -28 AND -30 REPAIR ANGLES, -34 AND -25 SHIMS AT STA 880 L24R IAW SRM TR 53-123, SRM 53-2-2.

Part: FRAME — CRACKED (FS 418) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 CRACK ON AFT FRAME OF TYPE 1 DOOR AT CUSP STA 418 RT. REMOVED DAMAGED SECTION OF FRAME AT STA 418 RT CUSP IAW SRM 51-03-00-0. FABRICATED AND INSTALLED REPAIR ANGLES AT STA 418 RT CUSP IAW SRM 51-1-20D, DWG 46417934.

Part: LONGERON — CRACKED (BS1736-1756 L15L) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE: C2 LONGERON CRACKED AT STA 1736 L15L (AND STA 1756 HAS 2EA. CRACKS). REMOVED FABRICATED AND REPLACED LONGERON SECTION. IAW SRM 51-1-20, 53-02-02-0 FIG 10, 51-1-20D.

Part: BULKHEAD — CRACKED (FS 1766 L11R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 RBL 34 L11R CUT OUT DAMAGED AREA AT AFT PRESS BULKHEAD IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -9, -11,-13 AND -19 FILLERS,-15 AND -17 DOUBLERS AT STA 1766 RBL 34 L11R IAW SRM 53-2-5 FIG 14A.

Part: FINGER DOUBLER — CORRODED (FS-49 TO -52) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE: C2 PILLOWED SKIN, POPPED RIVET HEADS, AND CORROSION UNDER FINGER DOUBLER, COCKPIT SUB FLOOR STA 49 TO 52. REMOVED FINGER DOUBLER, REMOVED CORROSION FROM PRESS BOX IAW SRM 53-02-00 FIG 1F, AND 51-1-20D, FOUND PRESS. BOX SKIN TO BE WITHIN LIMITS IAW SRM 53-02-00 FIG 1F. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -49 TO -52 IAW SRM 53-03-01 FIG 1F, AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (BS 52-67) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 PILLOWED SKIN, POPPED RIVETS UNDER FINGER DOUBLER FLT DECK SUB-FLOOR STA-52 TO-67 RBL 20. REMOVED CORRODED FINGER DOUBLER, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER STA-52 TO-67 RBL20 IAW SRM 53-3-01 FIG 7, SRM 51-01- 08, SRM 51-01-20D, AND DRAWING 5612298.

Part: SKIN — CORRODED (FS 848 L24R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE-C2 HEAVY CORROSION ON L24R WING-TO-BODY STRUCTURES FWD OF MAIN BARREL NUT STA 848 RT W/W UPPER FWD. REPAIRED STRUCTURE AT STA 848 L24R FWD OF MAIN BARREL NUT RT W/W IAW SAA EA NR 008-5320-01-A0357, UPS RAA NR 53-20577, MFG DWG NR5646674 REVJ, BAC SERV. MSG NR 1-218619854, AND FAA FORM 8100-9.

Part: FITTING — CORRODED (FS 1420) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 FRAME FITTING AT STA 1420 UPPER CUSP RT SIDE IS CORRODED OUT OF LIMITS. REMOVED FRAME FITTING AT STA 1420 RT CUSP IAW SRM 51-3-0. FABRICATED AND INSTALLED FITTING AT STA 1420 RT CUSP IAW SRM 51-3-2-0 AND SRM 51-03-00-0.

Part: FINGER DOUBLER — CORRODED (STA 67-80 RBL20) · airframe 67,689 hrs · 26,786 cycles

FOUND CORROSION UNDER FINGER DOUBLER FLT DECK SUBFLOOR STA -67 TO -80 RBL-20. FABRICATED AND INSTALLED FINGER DOUBLER FLT DECK SUB FLOOR STA -67 TO -80 RBL-20 IAW SRM 53-03-01, AND SRM 51-1-20D.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 CORROSION UNDER REPAIR STRAP AND UNDER DOUBLER ON RT W/W STA 900-904 RBL 50-56. REPAIRED DOUBLER AND STRAP AT STA 900-908, RBL 50-56 IAW SAA EA 008-5320-01-A0338, UPS EO DC8-5330-24908-A, BAC MSG 1-216936088-2, 1-216936088-4, 1-216936088-5, BOEING ROD SKETCH 06-08-09-002, AND FAA FORM 8100-9.

Part: SUPPORT ANGLE — CRACKED (NR 3 FLAP TRACK) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2, LT WING IB FLAP STA 3 FLAP TRACK SUPPORT ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-20D, 51-1-21, 51-2-00, DWG 5643117.

Part: SKIN — CRACKED (FS 1726 L17R) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1726 L17R. CUT OUT DAMAGED AREA AT STA 1726 L17R IAW SRM 53-02-00 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLERS, AND FINGER DOUBLER AT STA 1726 L17R IAW SRM 51-02-00 FIG 7 AND SRM 51-1-20D.

Part: SKIN — CRACKED (FS 1726 L17L) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1726 L17L. CUT OUT DAMAGED AREA AT STA 1726 L17L IAW SRM 53-02-01-0. FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLER AT STA 1726 L17L IAW SRM 53-02-01-0 FIG 7 AND SRM 51-1-20D.

Part: SKIN — DENTED (BS 70-210 L21L) · airframe 67,689 hrs · 26,786 cycles

INSPECTION TYPE: C2 REMOVE STEEL DOUBLER FROM LWR FWD CORNER OF MAIN CARGO DOOR AND REPAIR IAW SRO8530027. REMOVED STEEL DOUBLERS, REMOVED AND REPLACED SKIN FROM FS 70-210, L21L-L31L, DUE TO EXISTING CUTOUT IS OUT OF TANGENT AREA. REINSTALLED DOUBLER. IAW SRM 51-1-21,51-3-0 AND SAA EA NR 008-5310-01-A0396.

Part: O-RING — DAMAGED (OIL CAP)

NR 3 ENG OIL PRESSURE DROPPED TO 15 PSI AND LIGHT ILLUMINATED THEN WENT OUT WITH OIL QTY DECREASING TO 8 QTS INITIALLY THEN CONTINUED TO 6 QTS. INFLIGHT ENG SHUT DOWN ACCOMPLISHED IAW CHECKLIST. WINDMILL TIME 25 MINUTES W/ POSITIVE OIL PRESSURE. PER PILOT REPORT SHUT DOWN ENG AS PRECAUTION. EMERGENCY DECLARED. APPROACH AND LANDING UNEVENTFUL. PERFORMED ENGINE TROUBLESHOOTING ON NR 3 ENGINE REF DC-8 MM 71-00-00-1 FIG 141. FOUND O-RING ON OIL FILLER CAP DAMAGED. SERVICED ENGINE WITH 8 QTS OF ENG OIL. REMOVED AND REPLACED OIL FILLER CAP. RAN ENGINE FOR 5 MINUTES. FOUND NO OIL LEAKS, ALL INDICATIONS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW DC-8 AMM 30-50-01. OPS CK GOOD.

Part: LIFE VEST — TORN (COCKPIT)

INSPECTION TYPE:N/A, F/O'S LIFE VEST WORN. REMOVED AND REPLACED F/O'S LIFE VEST. TAG# 956523.

Part: WEB — CORRODED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE:C3 CUT OUT WEB ON RIGHT STA 3 AT RIVET AREA AND CHECK FOR CRACKS. REMOVED AND REPLACED RIGHT STA 3 FITTING.

Part: WEB — CORRODED (MLG WW) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, LEFT MAIN LANDING GEAR WHEEL WELL, AFT AND BEHIND FLAP CABLE DRUM WEB IS CORRODED. REMOVED AND REPLACED LEFT STA 3 FLAP SUPPORT FITTING AND REPAIRED CORRODED WEB.

Part: FITTING — GOUGED (CARGO DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRILLED AND DEBURRED FITTING. INSTALLED FITTING IAW SRM 51-1-21,51-1-24.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED FLOOR PANELS FS 70-170 IAW SRM 51-3-1.

Part: FIRST AID KIT — WORN (C1 DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, C-1 DOOR FWD LOWER GUIDE PIN FITTING WORN. REMOVED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. ORIG MAT .250 IAW DAC DWG 5754075 MAT REMAINING .130, LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, CABIN OVERWING AREA FS 960 FLOORBEAM CRACKED UNDER CUSP LOWER SIDE OF LIGHTENING HOLE RT. REMOVED DOUBLE SEAT TRACK & SPLICES. REMOVED WEB, GRILL & FASTENERS FROM FLOORBEAM. CUT OUT DAMAGED FLOORBEAM IAW DC8 REO GO9893 MAT ID FOR SPLICE ANGLE 7075-T660-6833 PO 444113. FAB SPLICE ANGLE. REC'D, LOCATED, DRILLED & DEBURRED FLOORBEAM. ALODINED & PRIMED REPAIR SPLICE ANGLE & FLOORBEAM. INSTALLED SPLICE ANGLE, FLOORBEAM, SEAT TRACK, WEB, GRILL.

Part: BRACKET — GOUGED (C2 DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C-3, B-PIT DOOR LINK HINGES ARE GOUGED/ WORN PORTION ON AIRFRAME (NOT DOOR). REMOVED 2 EACH EXISTING C2 DOOR LINK HINGE FITTINGS. RECEIVED NEW FITTING 2 EACH PN 4654281. LOCATED AND DRILLED TRANSFER HOLES FOR NEW HINGE FITTINGS IAW SRM 51-1-24. INSTALLED NEW DOOR LINK HINGE 2 EACH FIT TINGS IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA, MAT ID PLUG SEAT TRACK P/N 53B-007-002 PO S P0906208 AND CHANNEL SEAT TRACK P/N 53B-007-006 PO SP09768935. INSTALLED PLUG SEAT TRACK AND CHANNEL SEAT TRACK IAW SRM 51-3-0.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW SRM 51-3-0, 51-3-1, 53-2-3 FIG 9, 51-1-8, AND 53-2-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, SEAT TRACK-C HAS WORN LUGS AND SCALLOPS BETWEEN FS 1300-1315 (DOT D976). BLENDED OUT OF LIMITS IAW DC8 SRM 53-2-3. DIMENSION AFTER BLEND OUT OUT OF LIMITS. REMOVED DAMAGE FROM SEAT TRACK MAT ID FOR PLUG 7452952 -3 MAT ID FOR SEAT TRACK CH 7452952-7. LOCATED, DRILLED, DEBURRED PLUG AND CHANNEL. ALODINED AND PRIMED. INSTALLED PLUG IAW DC8 SRM 51-3-0, 53-2-3, 53-7-1, 51-2-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LUGS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK AND EXISTING REPAIR SPLICES @ FS 1550-1590 LBL 24. LOCATED, DRILLED, AND DEBURRED SEAT TRACK. ALODINED AND PRIMED AND INSTALLED SEAT TRACK AND SPLICES. IAW SRM 53-2-0,53-7-1,51-2-0,53-2-3.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LIMITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW SRM 53-2-0, 53-2-3, AND 51-3-0.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3 B- PIT DOOR FRAME AFT SIDE CRACKED DOT NR Y52Y. MAT ID 2024-0 .071 PO 4255761 IAW SRM 52-2-0 AND 52-4-1. RECEIVED MATERIAL USED FOR REPAIR DOUBLER FROM HEAT TREAT. HEAT TREATED FROM 2024-T4 IAW TPS 1003 REV A. FABRICATED REPAIR DOUBLER IAW SRM 52-2-0. ALODINED IAW SRM 51-1-8. PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLE R IAW SRM 51-1-21.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51-3-0 AND 51-3-1.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 51-3-1, 51-1-8, AND 51-2-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-20D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — WORN (PIT DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, A PIT DOOR FWD UPPER LOCK PIN GUIDE FITTING WORN. REMOVED DAMAGED GUIDE FITTING IAW DC8 SRM 51-3-0. ORIG THICKNESS IS .250 REMAINING MAT .108 IAW DAC DWG 5754075. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 52-2-0. REC'D, LOCATED, DRILLED NEW GUIDE FITTING IAW DC8 SRM 51-1-24. REMOVED FASTENERS IN WEB. INSTALLED FITTING & FASTENERS IN WEB IAW DC8 SRM 51-1-21, 51-1-20D, & 51-1-20A.

Part: FITTING — WORN (C-1 DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, A PIT DOOR AFT UPPER LOCK PIN GUIDE WORN. REMOVED DAMAGED FITTING DC8 SRM 51-3-0. ORIG MAT IS .250 IAW DAC DWG 5 754075. MAT REMAINING IS.104 AND FOUND TO BE WITHIN LIMITS IAW DC8 SRM 52-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: WEB — CORRODED (FUSELAGE) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND SPLICES 7075T6 .125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED WEB FROM STA 1160 TO 1220 L35R AND SPLICES IAW SRM 51-1-20D. AND T/R- 53-166.

Part: FRAME — CORRODED (FS 600RBL12LBL12) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAPS. SPLICES HEAT TREATED, ALODINED AND PRIMED ON ALL PARTS OF REPAIR. LOCATED AND DRILLED AND INSTALLED REPAIR. IAW SRM 53-20, 51-1-8, AND 53-4-1.

Part: SKIN — BENT (L2 DOOR) · airframe 66,867 hrs · 26,150 cycles

INSPECTION TYPE: C3, CABIN FWD LOWER CORNER OF L2 DOOR BENT AND TURN METAL. FAB ANGLE DOUBLER, Z-ANGLE SHIM, INNER SKIN SHIM, AND DOUBLER SKIN. ALODINED 2 SHIMS, DOUBLER INNER, PRIMED 2 SHIMS & DOUBLER INNER SKIN. RECEIVED HEAT TREAT. LOCATED & DRILLED. ALODINED ANGLE DOUBLER. PRIMED ANGLE DOUBLER, INSTALLED ANGLE DOUBLER, 2 SHIMS, DOUBLER INNER SKIN. ALL IAW DC8 SRM 51-1-21, 52-2-5, 51-1-8, 52-3-1, 52-2-0.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: AS, EMERGENCY LIGHT IN COURIER AREA INOP. RELAMPED EMERGENCY LIGHT.

Part: SLIDE — DISLODGED (CABIN DOOR)

ESCAPE SLIDE FELL OUT OF PACK UPON CLOSING DOOR. STOWED FED SLIDE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS WERE LEFT IN ARMED POSITION. BATTERY IS DEAD. CHECKED EMERGENCY LIGHTS. FOUND BATTERY PACK DISCHARGED AND ONE BATTERY SPLIT OPEN. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL 33-50-00.

Part: SLIDE — DETERIORATED (PAX DOOR)

INSPECTION TYPE: PFLT, CREW ENTRY DOOR ESCAPE SLIDE COMING APART. RE-ATTACHED CREW ENTRY ESCAPE SLIDE COVER & SECURED TO DOOR.

Part: BATTERY PACK — WILL NOT TEST (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CKS NORMAL.

Part: SMOKE DETECTOR — WILL NOT TEST (CARGO BAY)

INSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE DETECTORSPAA0200058S NR 1, 5, 6, 7 WILL NOT PROPERLY SELF TEST. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 STA 1700 STRINGER 34L HAS CORROSION. BLENDED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED NEW REPAIR AND STRAPS IAW DC8 SRM 53-4-1 & 53-2-2. INSTALLED NEW PARTS IAW DC8 SRM 53-2-2 FIG 8.

Part: WEB — CRACKED (L1 DOOR) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 L1 DOOR FWD CENTER TORQUE BOX WEB CRACKED. REMOVED DAMAGED WEB. FABRICATED NEW WEB IAW DWG 5597646. INSTALLED WEB IAW DC8 SRM 51-3-0

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1, CABIN FLOOR SUPPORT BRACKET HAS EXFOLIATED CORROSION AT STA 1754, BL 0. REMOVED CORRODED FITTING BRACKET IAW DC8 SRM 51-3-0, BRACKET WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, INSTALLED FITTING SUPPORT BRACKET IAW DC8 SRM 51-3-1, 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN INTERCOSTAL AT STA 67, RBL 44 IS CORRODED. TRIMMED OUT CORROSION AREA IAW DC8 SRM 53-2-0, FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0, INSTALLED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0 AND DC8 SRM 51-1-20.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN UNDER FLOOR AT STA 67 RBL 40 BULGING. BLENDED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED T EXTRUSION IAW TIMCO REO G08633, ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1, STRINGER END FITTING CRACK STRINGER 51 2 MAIN. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 INSIDE DOOR 60-VERT STAB CENTER SPAR CANTED BULKHEAD SHEAR TIE IS CRACKED BETWEEN L9L & L10L. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 & 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 FLOOR SUPPORT ANGLE CORRODED AT FS 1723 BL19R. REMOVED CORRODED SUPPORT ANGLE AT STA 1723 BL19R IAW DC8 SRM 51-3-0, SUPPORT ANGLE 5755032-26, DETERMINED TO BE CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-0. INSTALLED NEW PART IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 PROBLEM WITH FLOORBEAM CRACK UNDER FLANGE FS 1746 BL 2L. FABBED REPAIR PARTS IAW DC8 SRM 53-2-0. INSTALLED REPAIR PARTS IAW DC8 SRM 536-2-0 AND 51-2-20D.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 C-PIT TORQUE BOX WEB AND FITTING HAVE ELONGATED HOLES. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 FABBED & INSTALLED DOUBLER IAW SRM 53-2-0.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 COCKPIT VERT WEB I/B SIDE AT FS 6 RBL 14. BLENDED CORROSION ON WEB IAW DC8 SRM 51-1-8, WITHIN LIMITS DC8 SRM 53-2-0. REMOVED L-ANGLE IAW DC8 SRM 51-1-21 OUT OF LIMITS IAW DC8 SRM 53-2-0, AND INSTALLED L-ANGLE IAW DC8 SRM 51-1-8 AND 51-1-21.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 R-1 DOOR CUTOUT UPPER FWD CORNER SHOWS CRACK INDICATION ON THE FIRST FASTENER HOLE IN THE FIRST ROW OF RIVETS. REPAIRED DOOR CORNER IAW DC8 SRM 53-2-0 FIG 14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 L-2 DOOR CUTOUT LOWER FWD CORNER SHOWS CRACK INDICATION ON FIRST FASTENER HOLE ABOVE DOOR PAN. FABRICATED DOULBERS IAW DC8 SRM 53-2-0 FIG 18. INSTALLED DOUBLERS IAW DC8 SRM 51-1-8 & 51-3-0.

Part: FITTING — CRACKED (T/E FLAP) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED BLOCK IAW DC8 DWG 5894377. INSTALLED FITTING IAW DC8 DWG 5751174 & 5894377.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 AFT PIT FLOORBEAM CORRODED AT STA 1440 UPPER FWD FLANGE AT RBL 60. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FOUND AFT FLANGE CORRODED REMOVED AFT FLANGE OF FLOORBEAM IAW TRSM 95T0345001 STD 6310-001. FABBED REPAIR IAW REO G08652, INSTALLED REPAIR IAW DC8 SRM 51-1-20D & REO G08652.

Part: ATTACH ANGLE — GOUGED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 832 RBL 38 AFT SIDE OF INTERCOSTAL ATTACH ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE IAW DC8 SRM 51-1-20D & DAC DWG 5773 275.

Part: SUPPORT FITTING — CRACKED (T/E FLAP) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED BLOCKS IAW DC8 DWG 5894377. LOCATED, DRILLED AND DEBURRED 3751728-502 FITTING & BASE FITTING IAW DC8 DWG 5894377. INSTALLED 5751 186-508, 3751728-502, 5894377-5 & -27 AND 3655134N2 IAW DC8 DWG 5751 174 & 5894377.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,353 hrs · 65,890 cycles

INSPECTION TYPE:C1 MAIN CABIN TOP MLG PRESSURE WEB AREA FLOORBEAM IS CRACKED AND CORRODED ON FWD & AFT LEG AT STA 900 LBL 44. REMOVED MVD CORROSION FROM FLOORBEAM, OUT OF LIMITS. FABBED REPAIR PARTS IAW R EO G08638 MPI OF REPAIR PARTS IAW ASTM E1444. NO CRACKS NOTED. INSTALLED REPAIR PARTS IAW SRM 51-1-21, 51-1-20D, 51-3-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 C-PIT FRAME REINFORCEMENT ANGLE HAS SEVERAL CRACKS & AN IMPROPER REPAIR STA 1150, L32R. REMOVED ATTACH ANGLE IAW DC8 SRM 51-1-21D, FABRICATED REPLACEMENT PARTS IAW DC8 SRM 51-1-20D, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 AFT PIT - STA 1060 CABIN FLOORBEAM UPPER AFT FLANGE IS CRACKED HORIZONTALLY ACROSS AFT EDGE AT RBL 60. CUTOUT CRACKED AREA IAW REO G08643. FABRICATED REPAIR ANGLE IAW REO G08643. INSTALLED REPAIR ANGLE AND FLOOR PANEL IAW DC8 SRM 51-1-20D, 51-1-11, & 51-3-0.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 CTR FUSE SHEAR TIE CRACKED ON TOP OF FRAME STA 680 BL 0. REMOVED BRACKET DRILLED UP AND INSTALLED NEW BRACKET IAW DC8 SRM 51-1-8 AND DAC DWG 615535.

Part: FRAME — BENT (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 240 BETWEEN STR 19R & STR 20R FRAME IS BENT AND IMPROPERLY REPAIRED. REMOVED OLD REPAIR. FABRICATED AND INSTALLED FRAME REPAIR IAW DC8 SRM 53-2-0 FIG 2A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 STA 220 STR 20R FRAME CRACKED. REMOVED DAMAGE FRAME SECTION AND REPAIRED PER DC8 SRM 53-2-0 FIG 2 AND 51-1-8.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 345 STR 17R INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. REMOVED DAMAGE INTERCOSTAL AND GUSSET, FABBED NEW INTERCOSTAL AND GUSSET, INSTALLED INTERCOSTAL AND GUSSET IAW TPS 1003 DC8 SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 LT MLG W/W STA 891 FITTING OVER LONG 24 CORRODED. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1, A-PIT DOOR TORQUE BOX FRAME HAS EXFOLIATION CORROSION AT STA 280 L 32-33R INSIDE LIGHTNING HOLE. REMOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FRAME REPAIRED IAW TIMCO REO G08626.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 A-PIT TORQUE BOX WEB HAS BROKEN SHEAR TIE AT STA 280 L33R. FABRICATED WEB IAW DAC DWG 5753892. FABRICATED SPLICE DOUBLER IAW DC8 SRM 53-2-0. INSTALLED WEB AND SPLICE IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 MAIN CABIN RT SIDE STA 759 L13R ATTACH FITTING CRACKED. REMOVED DAMAGED PART AND INSTALLED NEW PART IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (RT MLG) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1, RT MLG W/W TRAPEZOID TO WING LOWER OUTBOARD FITTINGS CRACKED. REMOVED FITTINGS, DRILLED UP AND INSTALLED NEW FITTINGS IAW DAC DWGS 5656229, 3641117 AND 3656004. REINSTALLED STIFFENER AND ACCESS PNLS IAW DC8 M/M 51-1-20D AND 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 A-PIT L35R HAS 1 INCH LONG CRACK AT STA 343. FABBED AND INSTALLED NEW SECTION OF LONGERON AND U-CHANNEL IAW TIM CO REO G068621 AND DC8 SRM 53-2-2 FIG 10 AND 51-1-20.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 ABOVE RT CUSP AT STA 1170-1180 C PIT TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1, RT MLG W/W LONG 2R CRACKED BY UPLOCK MOUNT. FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-2 TR 53-123. INSTALLED REPAIR IAW DC8 SRM 53-2-2 TR 53-123 AND DC8 SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 A-PIT L-31-L STA 380-400 SPLICE IS CRACKED 4 INCHES LONG. REMOVED CRACKED FITTING SPLICE IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING, INSTALLED AT LONG 31L, STA 390 IAW DC8 SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C-1 MAIN CABIN LT SIDE STA 780 L14L FRAME TO LONGERON ATTACH FITTING IS CRACKED. REMOVED FITTING & INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 LT WW FITTING AT STA 880 L4L HAS CORROSION. REMOVED FITTING, CUT NEW FITTING AND FABRICATED SPLICE PARTS IAW DC8 SRM 53-2-0 FIG 8. INSTALLED FITTING IAW DC8 SRM 53-2-0 FIG 8 AND DC8 SRM 51-1-20D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,890 hrs · 25,353 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN BLENDOUT AT BS 550 RIGHT HAND SIDE ABOVE CARGO COMP DOOR EO DC8-5330-15732A, REPAIR AT C-CHECK. FABBED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 20.

Part: WINDSHIELD — CRACKED (COCKPIT)

INSPECTION TYPE:N/A ATB- CAPT'S WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD PER MM 56-10-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:IN CRACK IN COCKPIT DOOR FRAME, JUST ABOVE AND OUTBOARD OF DOOR (CLOSED) CATCH. INSTALLED DOUBLER ON DOOR FRAME AT DOOR CATCH PER DC-8 SRM 53-2-0.

Part: DOOR FRAME — CRACKED (ENTRY DOOR)

INSPECTION TYPE:IN COCKPIT DOOR DAMAGED - CREW FWD ENTRY DOOR HAS A CRACK IN THE AFT DOOR FRAME NEAR LATCH. REMOVED 2 DOOR STOP FITTINGS AND FASTENERS 6 INCHES ABOVE AND BELOW DAMAGE. DYE PEN INSPECTED DAMAGED AREA. STOP DRILLED 1.125 INCH CRACK. VERIFIED STOP DRILL ENDS OF CRACK. INSTALLED REPAIR IAW EO DC8-5310-1 5740 COMPLETED.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. R/R EMERGENCY LIGHTS BATTERY PACK. OPS CKS GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:P/F, LIGHTS FAIL TO TEST PRIOR TO FLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LT WHEEL WELL PRESSURE PANEL IS CORRODED OUT OF LIMITS AT STA 970, LBL8. REPAIRED AREA IAW SRM 53-2-0.

Part: CAP — CRACKED (CENTER WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, STA 857 CENTER WING TANK UPPER CHORD CRACKED AND CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW SPAR CAP IAW SRM 51-1-20D & 51-1-21.

Part: DOUBLER — CORRODED (COCKPIT) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, COCKPIT SUBFLOOR CAN DOUBLER AND FINGER DOUBLER ARE CORRODED BEYOND LIMITS AT STA -18 AT RBL 8. REMOVED, FABRICATED AND REPLACED DOUBLERS IAW DWG 5612298, SRO8530026 AND SRM 51-1-21, 51-1-20D.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LT HORIZ STAB I/B FWD UPPER T-ANGLE FITTING CRACKED STA XFS 60.00. REMOVED, FAB AND INSTALLED FITTING IAW SRM 51-1-20D & 51-1-11.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2 WING BOX TO FLOORBEAM ATTACH ANGLE CRACKED STA 798 RBL-50. REMOVED, FAB AND INSTALLED ATTACH ANGLE IAW DWG NR 3643112 & SRM 51-1-20D.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, WING BOX TO FLOORBEAM ATTACH ANGLE CRACKED STA 798 LBL-50. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-1-20D & 51-1-21.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, STA 680 LBL -24 SEAT TRACK SUPPORT FITTING CRACKED. REMOVED, FAB AND INSTALLED SEAT TRACK SUPPORT FITTING IAW DWG NR 5773275 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (CENTER WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 730 - 780 ,LBL 8 -RBL 8, THE CENTER WING UPPER EXTERNAL DOUBLER HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5643130.

Part: FITTING — CORRODED (CABIN) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 960 - 980, LBL 8 ON THE SUB FLOOR, THE FRAME TO WEB TIE FITTING HAS HEAVY CORROSION ON THE MATING FLANGE. REMOVED AND REPLACED FITTING IAW DWG 3640887U AND SRM 51-1-20D.

Part: ANGLE — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, RIGHT WING L/E STIFFENER ANGLE CRACKED STA XOLDI 6.225. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 & 51-1-20D.

Part: RIB — CHAFED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E RIB HAS HOLE CHAFED IN IT AT XS 503.379. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, RIGHT WING L/E AT STA XOLDI 6.225 THE LWR RIB CRACKED. STOP DRILLED CRACK IAW SRM 57-2-0. FAB AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 51-1-11, 57-3-1 & 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LEFT WING LEADING EDGE THE I/B UPPER RIB CRACKED STA XS 520.1. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR ANGLES IAW 51-1-20 & 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LEFT WING LEADING EDGE LWR RIB CRACKED STA XFS 360.250. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D.

Part: STIFFENER — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LEFT WING NUMBER 2 STUB WING VERTICAL STIFFENER CRACKED APPROX STA XS256. REMOVED, FAB AND INSTALLED IAW DWG NR 9753294 AND SRM 51-1-8, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 467.233. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21 & 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, FRAME CAP FS 1040 CORRODED OUT OF LIMITS. REMOVED AND REPLACED FRAME CAP FS 1040 IAW SRM 51-1-20 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RT WING L/E RIBS ARE CRACKED AT STA XFS 283.00 AND XFS 401.00. STOP DRILLED CRACK AND REPAIRED BOTH RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RT WING L/E RIB IS CRACKED AT STA XFS 385.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 1241 LONG 35R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498, AND SRM 51-1-20D.

Part: SPAR CAP — CORRODED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING AUX TANK UPPER SPAR CAP IS CORRODED BEYOND LIMITS AT XFS 20. REPAIRED IAW SRM 57-2-1 FIG 37.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, STA 380 TO 400 LONG 31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2 SEAT TRACK CRACKED STA 380 RBL48. REMOVED, FABBED AND INSTALLED SEAT TRACK SECTION IAW EODC8-53-20- 8309 APPENDIX-B AND SRM 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 200 - 220 LONG 31R SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3755217 AND SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, STA 280 FRAME RAIL ABOVE LONG 34L - 35L HAS HEAVY CORROSION. REMOVED AND REPLACED FRAME RAIL IAW SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 1120 FRAME IS CORRODED BEYOND LIMITS LONG 35L-35R. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 1040 FRAME AT STR 36 HAS HEAVY CORROSION ON UPPER FLANGE UNDER SIDE. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 1746 LBL 29 INTERCOSTAL IS CRACKED AT AFT END. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5755032 AND SRM 51-1-21.

Part: SKIN — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E LOWER SKIN IS CRACKED AT FASTENER HOLES BETWEEN XFS 640 - 649. REPAIRED IAW EO DC8-5720-4087-B.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 785. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 283.25. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E EXTERIOR SKIN IS CRACKED AT STA XFS288.00 ON THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.

Part: DOUBLER — CORRODED (RT WING LE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E BETWEEN STA 772.500 TO XFS 760.00. THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LEFT WING CENTER L/E RIB CRACKED STA XOLDI 6.225. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED DOUBLER IAW 57-2-0 FIG-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 440 - 460 AT STR 31R, THE STRINGER SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT STA XS.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RT WING L/E AT STA XFS 792.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 250.089. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLERS IAW SRM 51-1-20D & 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, RT UPPER CUSP FITTING CRACKED STA 324. REMOVED, FABBED AND INSTALLED CUSP FITTING IAW DWG NR 3754031 & SRM 51-1- 20D.

Part: SKIN — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E (NR 3 STUB WING) AT STA XS207.500. THE L/E SKIN IS CRACKED AT FRONT SPAR. REPAIRED AREA IAW DC8-5720-7767-A.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E AT STA XFS.792.250. THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, LEFT WING CENTER L/E LWR SKIN CRACKED STA XW 257. STOP DRILLED CRACK IAW ADDUM DC8-5720-4087-B. FAB AND INSTALLED DOUBLER IAW DC8-5720-4087-B.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 646. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LT WING EXTERNAL SKIN IS CRACKED AT STA XFS 310.250 (LOWER SURFACE). REPAIRED AREA IAW SRM 57-3-3 FIG 5.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (RT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, RIGHT WING L/E SKIN HAS INTERNAL CORROSION AT STA XFS710.00. REPAIRED AREA IAW 8110-3 APPROVED DH SK 700-025.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, FUSELAGE SKIN AT STA 1746.621 AND LONGERON 15R IS CRACKED. REPAIRED AREA IAW SRM 53-2-1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, SEAT TRACK CRACKED AND HAS HEAVY CORROSION STA 1160 RBL 48. REMOVED DAMAGED SEAT TRACK IAW SRM 51-1-20D. FAB SEAT TRACK AND SPLICE, INSTALLED IAW EO DC8-5320-8309C.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, A- PIT STA 280 LONG 27R TORQUE BOX FITTING CRACKED. REMOVED AND INSTALLED FITTING IAW SRM 51-1-21D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C-2, UPPER LT FUSELAGE SKIN AT CANTED FRAME 1746.621 AT LONG 15L SKIN CRACKED. CUT OUT CRACKED AREA IAW SRM 53-2-1 FIG 7. FABBED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7 & 51-1-20D.

Part: RIB — CRACKED (LT WING LE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LT WING CENTER L/E UPPER RIB IS CRACKED AT STA XFS 410.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 80 LONG 24L IS CRACKED. REPAIRED IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 600 - 620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, LT WING L/E AT STA XFS 597.5, THE LOWER INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,438 hrs · 24,396 cycles

INSPECTION TYPE:C2, STA 55 FRAME CRACKED AT STR 24L. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: ENGINE — FAILED (NR 3)

NR 3 ENGINE FLAMEOUT IN FLT DURING CLIMB THROUGH FLIGHT LEVEL 380. ENGINE RESTARTED AFTER NR 3 THROTTLE MOVED TO IDLE PER MM 71-00-00, TROUBLE SHOOTING PAGE 165. NO DEFECTS NOTED. POWER ASSURANCE RUN CHECKS OK. NO DEFECTS NOTED, OKAY FOR SERVICE.

Part: SLIDE — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, L-1 DOOR EVAC SLIDE INOP REF M183941.

Part: SKIN — CRACKED (CARGO DOOR)

LOWER PIT DOOR 33 CRACKED AT LOWER END OF REPAIR BELOW HANDLE. REPAIRED CRACKED DOOR SIN OF NR 3 PIT DOOR IAW SRM 52-2-0.

Part: WINDOW — LACK OF LUBE (RT COCKPIT)

F/O WINDOW WILL NOT OPEN. GUIDE PIN JAMMED. FREEDED UP TRACK PIN AND LUBED TRACK OPS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK.

Part: WIRE — CHAFED (NR 3 GENERATOR)

NR 3 UNPARELLED LIGHT CAME ON AFTER LANDING. TOTAL ELECTRICAL FAILURE APPROX 1-2 MIN. THEN DETECTED SMOKE IN COCKPIT, EVACUATED A/C. REF L/P 183785 ITEM 2. FOUND WIRE W103-T1-5X2 (WDM 24-20-03) INSIDE NR 3 GEN CURRENT X-FORMER CHAFFING WITH COVER MOUNTING SCREW EXPOSING STRAND OF WIRE. ALSO, FOUND TERMINAL LUG OF ABOVE WIRE HAS NO CLEARENCE WITH FWD LOWER NUT. REPAIRED CHAFED AREA OF WIRE REMOUNTED CLIP NUT 180 FOR CLEARENCE. ACFT POWER SYSTEMS, OPS CK OK.

Part: RETRACT MECH — OUT OF ADJUST (NLG)

INSPECTION TYPE-N/A, THE LANDING GEAR WOULD NOT RETRACT AFTER T/O. RAN THE GEAR HANDLE JAMMED CHECKLIST. THE GEAR RETRACTED AFTER PUSHING THE GEAR HANDLE LATCH FLIGHT RELEASE BUTTON. FOUND THE NOSE GEAR GROUND SHIFT MECHANISIM WOULDN'T PULL THE ANTI-RETRACTION LEVER FAR ENOUGH. ADJUSTED NOSE GEAR GROUND SHIFT PER MM 32-23-01, SYS OPS OK WITH A/C ON JACKS GEAR HAND AND ANTI-RETRACTION DEVICE CHECK NORMAL.

Part: RETRACT MECH — MALFUNCTIONED (NLG)

INSPECTION TYPE-N/A, NOSE GEAR WOULD NOT RETRACT AFTER T/O. AIR TURNBACK. PER TROUBLESHOOTING PG 101 NOSE GEAR FAILS TO RETRACT, CHECKED CONTROL VALVE, RIGGING AND CABLE TENSION PER MM 32-31-00 PG 204. NO DEFECTS NOTED. GEAR OPERATES NORMAL. NO DEFECTS NOTED.

Part: ENGINE — FAILED (NR 3)

NR 3 ENG SEIZED ON SHORT FINAL. N2 BECAME 0 PERCENT RAN THE ENG FIRE AND SECURE ENGINE CHECK LIST. REMOVED AND REPLACED ENGINE IN WORK FOUND METAL IN OIL SYSTEM (CHIP DETECTOR) SUSPECT BEARING FAILURE.

Part: JAMB — CRACKED (L2 DOOR)

INSPECTION TYPE:C/CK L2 DOOR JAMB, AFT PAN CRACKED AT UPPER DOOR STOP. CUT OUT DAMAGED SEGMENT OF 9 DOOR PAN IAW REO 04645. FABRICATED AND DRILLED NEW- 9 PAN SEGMENT AND PAN SPLICE DOUBLERS IAW REO 04645. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED -9 PAN SEGMENT AND PAN SPLICE DOUBLERS IAW DC8 SRM 51 1 20D AND REO 04645.

Part: INTERCOSTAL — CORRODED (BS 1660-1680)

INSPECTION TYPE:C, INTERCOSTAL CRACKED, FS 1660 1680, L32R. REMOVED, FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG 5613064. ALODINED AND PRIMED AND INSTALLED IT IAW DC8 SEM 51 1 8 AND 51 1 20D.

Part: INTERCOSTAL — CRACKED (BS 80)

INSPECTION TYPE:C/CK INTERCOSTAL CRACKED, FS 80 AT L30R. REMOVED INTERCOSTAL FABBED AND INSTALLED NEW ONE IAW DC8 SRM 51 1 20D, 51 1 8 AND DOUGLAS DWG 5613064.

Part: FRAME — CORRODED (BS 1060)

INSPECTION TYPE:C, FRAME CORRODED AT CAP STALL 1060 L35 36R. FABBED REPAIR STRAP AND INSTALLED IAW REO 04646. INSTALLED STRAP IAW 51 1 20D.

Part: SUPPORT — CRACKED (COCKPIT)

INSPECTION TYPE:C/CK CRACK, CORROSION ON FLOOR SUPPORT AT STA 8 TO STA 25. FABRICATED DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. REMOVED CORROSION IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW DC 8 SRM 51 1 21.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:C/CK, ANGLE REPAIR CRACKED FOR STIFFENER RUNNING BETWEEN NR 1 AND NR 2 RIBS AT LEFT HAND LEADING EDGE FUEL TANK. FABRICATED NEW REPAIR ANGLE 7075 T6 IAW DC8 SRM 57 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW DC8 SRM 57 2 0.

Part: CLIP — CRACKED (BS 680)

INSPECTION TYPE:C/CK, MAIN CABIN STA 680 AND BTL 25 RIGHT FLOORBEAM CLIP CRACKED. REMOVED ANGLE FABBED AND INSTALLED NEW ONE IAW DC8 DWG 5773275. INSTALLED IAW DC8 SRM 51 1 20D AND 51 1 8.

Part: PLUG — CORRODED (BS 680)

INSPECTION TYPE:C, SEAT TRACK PLUG CORRODED STA 680 BL25R. REMOVED AND REPLACED PLUG IAW DC8 SRM 53 3 2, 51 3 0, 51 1 8.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE:C/CK, MAIN CARGO FITTING CRACKED AT STA 717, LONGERON 22 RIGHT. REMOVED FITTING FABBED NEW ONE IAW DAC DWG 3616947. INSTALLED IT IAW DC8 SRM 51 1 15 AND 51 1 20D.

Part: MEMBRANE — CORRODED (BS 1580)

INSPECTION TYPE:C, CORROSION/CRACKED REAR CABIN FLOOR MAIN FRAME SUPPORT CLIP AFT ACCESS RY COMP. RT CRSP STA 1580 REAR SIDE OF FLOORBEAM REMOVED CLIP AND FABBED NEW SUPPORT CLIP ALODINED AND PRIMED IAW DC8 SRM 51. INSTALLED CLIP IAW DC8 SRM 51.

Part: FLOORBEAM — DAMAGED (BS 680)

INSPECTION TYPE:C/CK MAIN CABIN STA 680 AND RBL 50 FLOORBEAM GOUGED, CHAFFED AND CORRODED UNDERSIDE. FABRICATED REPAIR STRAP IAW REO 04670. ALODINED, PRIMED AND INSTALLED REPAIR STRAP IAW DC8 SRM 51 18 AND REO 04670.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C/CK MAIN CABIN FLOORBEAM FITTING AT STA 781 AND BTL 50R CRACKED. REMOVED FITTING, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 5130, 51 1 20D, AND 51 3 2.

Part: FITTING — CRACKED (BS 758)

INSPECTION TYPE:C, FITTING CRACKED STA 758 BL50R IN MAIN CARGO. REMOVED FITTING INSTALLED NEW ONE IAW DC8 SRM, 51 3 0 AND 51 1 20D.

Part: SEAT TRACK — CORRODED (BS 1634-1680)

INSPECTION TYPE:C/CK, CORROSION, SEAT TRACK E AT STA 1634 TO 1680. REMOVED DAMAGED SECTION, STA 1600 TO 1680. FABBED AND INSTALLED NEW SECTION IAW DC8 SRM 51 3 0 AND UPS EO DC8 5320 5167.

Part: FITTING — CRACKED (BS 834)

INSPECTION TYPE:C, MAIN CABIN FRAME FITTING CRACKED AT STA 834 AND LONG 22R UNDER FLOOR. REMOVED DAMAGED FITTING DRILLED AND REAMED HOLES INTO NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (BS 834)

INSPECTION TYPE:C/CK, MAIN CABIN FRAME FITTING CRACKED AT STA 834 AND LONGERON 22 RIGHT. REMOVED DAMAGED FITTING, DRILLED AND REAMED HOLES INTO NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM, 51 1 20D.

Part: FITTING — CRACKED (BS 855)

INSPECTION TYPE:C/CK, MAIN CABIN FRAME FITTING AT STA 855 AND LONGERON 22 RIGHT CRACKED. REMOVED FITTING FABBED NEW ONE IAW DAC DWG 577994 ALODINED AND PRIMED AND INSTALLED IT IAW DC8 SRM 51 1 8 AND 51 1 20D.

Part: FLOORBEAM — CORRODED (CABIN)

INSPECTION TYPE:C/CK, CABIN FLOORBEAM STATION 8 RBL 26 HAS CORROSION AND UPPER FWD FLANGE LOWER SURFACE AT ATTACH LUG BOLT BROKEN OFF IN LUG. FABRICATED REPAIR STRAP IAW REO 04644. INSTALLED REPAIR STRAP IAW DC 8 SRM 51 1 20D BAD REO 04644. REF TO UPS NR 542659 FOR COPY OF REO.

Part: SEAT TRACK — CORRODED (BS 55-72)

INSPECTION TYPE:C/CK STA 55 TO 72 SEAT TRACK 11 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 53 7 3 AND DC8 SRM 51 1 8.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C/CK STA 680 LONGERON 8L FWD BATHTUB FITTING CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23.

Part: FRAME — CRACKED (BS 1680)

INSPECTION TYPE:C/CK FRAME CRACKED AT STA 1680 LONGERON 22 RIGHT. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51 1 21. FABRICATED NEW FRAME SECTION IAW DC8 SRM 51 1 4 HEAT TREATED NEW FRAME SECTION FROM 7075 0 TO 7075 T6, .071 IAW TPS 1003 REV A ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (CABIN)

INSPECTION TYPE:C/CK STA 680 LONGERON 4 L FWD BATHTUB FITTING CRACKED. REMOVED FITTING FABBED AND INSTALLED NEW ONE IAW DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23.

Part: FLOORBEAM — CRACKED (BS 55)

INSPECTION TYPE:C/CK, FLOORBEAM STA 55 AT RBL 5 UPPER T CAP AFT FLANGE CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED T CAP REPAIR IAW REO 04620, DC8 SRM 53 3 3 AND 51 1 21 AND 51 1 8 AND 51 1 11.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE:C, MAIN CABIN STATION 980 AND LONG 22R FUSELAGE BRACE FITTING IS CRACKED IN TWO PLACES. REMOVED DAMAGED FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: STIFFINER — CRACKED (BS 940)

INSPECTION TYPE:C/CK RT W/W VERTICAL STIFFENER AT FS 940 FOR OB WW CLOSE OUT WALL HAS CRACK, JUST FWD OF FLAP BUS CABLE DRUM. FABRICATED DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW SRM 53 2 0 AND 51 1 20D.

Part: FLOORBEAM — CORRODED (BS 8)

INSPECTION TYPE:C/CK CABIN FLOORBEAM, STA 8 RBL 26, HAS CORROSION ON FWD FLANGE. FABRICATED REPAIR STRAP AND INSTALLED IT IAW REO 04644 (ATTACHED TO UPS NR 542659) AND DC8 SRM 51 1 8, 51 1 20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C/CK STA 680, LONGERON 7R FWD BATHTUB FITTING CRACKED. REMVOED FITTING, DRILLED AMD INSTALLED NEW ONE IAW DC8 SRM 51 3 0 A ND 51 1 20D.

Part: FITTING — CORRODED (BS 940)

INSPECTION TYPE:C/CK LONGERON 24 RIGHT OF FLOOR FITTING HAS CORROSION ON AFT FACE AND CRACKED ON AFT UPPER LEG AT FS 940. REMOVED FLOOR FITTING FABRICATED SPLICE ASSY IAW DC8 SRM 53 2 0. ALODINED AND PRIMED SURFACE IAW DC8 SRM 51 1 8 AND INSTALLED SPLCIE ASSY IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (CABIN)

INSPECTION TYPE:C/CK, STA 680 LONGERON 6 RIGHT FWD BATHTUB FITTING CRACKED. REMOVED FITTING INSTALLED NEW ONE IAW DC8 SRM 51 1 20D NAD 51 3 0 AND 51 1 23.

Part: FLOORBEAM — CORRODED (BS 1580)

INSPECTION TYPE:C/CK, FLOORBEAM AT STA 1580 RIGHT HAND TUNNEL AREA CORRODED. REMOVED CORROSION, OUT OF LIMITS IAW DC8 SRM 51-1-8. FABRICATED TWO ANGLES AND FILLERS IAW REO 04682. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED ANGLES AND FILLERS IAW REO 04682.

Part: FITTING — CORRODED (BS 940)

INSPECTION TYPE:C, MAIN CABIN STATION 940 AND LONG 22L FUSELAGE FRAME FITTING CORRODED. REMOVED FITTING FOR FABRICATION OF NEW FITTING SEE OPS 50018 FOR FABRICATION ALODINED AND PRIMED FITTING IAW DC8 SRM 51 MAT ID FOR WEB DOUBLER IAW DC8 SRM 53 4 1 .032 2024 T 3. FABRICATED REPAIR IAW DC8 EO DC8 5350 7876. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51 1 8. INSTALLED FITTING AND DOUBLER IAW DC8 SRM 51 1 20D AND 51 1 21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C/CK STA 680 LONGERON 2L AND BATHTUB FITTING CRACKED. REMOVED CRACKED FITTING STA 680 L-2 LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23.

Part: FRAME — CORRODED (CARGO COMPT)

INSPECTION TYPE:C/CK, FUSELAGE STATION LONGERON 35 RIGHT FRAME HAS CORROSION AT NUT PLATE HOLES. FABRICATED FRAME SPLCIE IAW DC8 SRM 53 2 0, ALDOINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D.

Part: SEAT TRACK — CORRODED (BS 160)

INSPECTION TYPE:C/CK FWD PIT STA 160 180 FLOOR POST SEAT TRACK AND SPLICES CORRODED. REMOVED CORROSION FROM POST AND SPLICES ALODINED AND PRIMED IAW DC8 SRM 51 1 8. REMOVED DAMAGED SEAT TRACK DRILLED AND INSTALLED NEW SECTION IAW DC8 SRM 51 1 8 AND 51 3 0 AND 51 1 24.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE:C/CK, RIGHT INBOARD AILERON UPPER SKIN CRACKED AT OUTBOARD END. FABBED REPAIR STRAP TREATED AND INSTALLED IAW REO 04638 REV A.

Part: CHANNEL — CORRODED (LT MLG WW)

INSPECTION TYPE:C/CK, CORRODED U CHANNEL AT UPPER PRESSURE PANEL. REPAIRED PER REO 04626 ON UPS NR 542514.

Part: FITTING — CRACKED (BS 660)

INSPECTION TYPE:C/CK MAIN CABIN STA 660 680 LONGERON 11 LEFT CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW PART IAW DC8 SRM, 51 1 20 D AND 51 3 0 NAD 51 1 8.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE:C/CK, RIGHT AILERON UPPER SKIN OUTBOARD END CRACKED. ROUTED OUT CRACK, FABBED PRIMED AND INSTALLED DOUBLER IAW REO 04658.

Part: JAMB — CRACKED (PAX DOOR)

INSPECTION TYPE:C/CK, LEFT AFT ENTRY DOOR JAMB WEB CRACKED AT ATTACH HOLE, TOP AFT CORNER REMOVED DAMAGED WEB, FABRICATED NEW WEB, REPAIR ANGLES, SPLICES AND BUSHINGS IAW REO 04632. ALODINED AND PRIMED ALL PARTS AND WORK AREA IAW DC8 SRM 51-1-8. INSTALLED NEW WEB, REPAIR ANGLES, SPLICES AND BUSHING IAW REO 04632.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE:C/CK, RIGHT OUTBOARD AILERON TOP LEADING EDGE AREA AND SKIN CRACKED ON OUTBOARD END. REPAIRED SKIN IAW REO 04658 REO ATTACHED TO UPS NR 542301.

Part: CHANNEL — CORRODED (BS 980)

INSPECTION TYPE:C/CK CORROSION ON UPPER PRESSURE PANEL U CHANNEL AT FUSELAGE 980 LT WW 2ND FROM MOST O/B CHANNEL. REPAIRED REO 04626 REF UPS CARD 542514.

Part: CHANNEL — CORRODED (BS 980)

INSPECTION TYPE:C/CK CORROSION ON UPPER PRESSURE PANEL U CHANNEL AT FS 980 LT W/W THE MOST O/B. FABBED NEW HAT CHANNELS AND SPLICES IAW REPAIR ENGINEERING ORDER REO 04626. ALODINED AND PRIMED HAT CHANNELS AND SPLICES IAW DC8 SRM 51 1 8. INSTALLED HAT CHANNELS AND SPLICES IAW REO 04626 AND DC8 SRM 51 121.

Part: STIFFINER — CORRODED (BS 1723)

INSPECTION TYPE:C/CK INTERIOR AFT 6 FUSELAGE FLOOR STIFFENER HAS CORROSION ON UNDERSIDE AT STATION 1723 LONGERON 34 RIGHT. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53 2 0. FABRICATED WEB IAW DOUGLAS DRAWING 5755032 ALODINED AND PRIMED IAW DC8 SRM 5 1 1 8. INSTALLED WEB IAW DC8 SRM 51 1 20D.

Part: BULKHEAD FITTING — CRACKED (FWD PRESS BLKHD)

INSPECTION TYPE:C/CK, FWD PIT AFT 6 BULKHEAD FITTING CRACKED, LONGERON 33 RIGHT. REMOVED FITTING DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C/CK, STA 1690 END FITTING CRACKED, LONGERON 29 LEFT. REMOVED FITTING INSTALLED NEW FITTING. FABBED ON OPS 50013 IAW DC8 SRM 51 1 24, AND 51 1 21.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE:C/CK, FITTING AT LONGERON 17 RIGHT TO FRAME STA 1200 CRACKED. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C/CK, STA 1690, LONGERON 31 RIGHT END FITTING CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 51 1 21 AND 51 1 20D. FABBED FITTING IAW DAC DWG 4641324.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C/CK, FITTING AT LONGERON 20 RIGHT FRAME STATION 1230 CRACKED. LOCATED AND DRILLED NEW FITTING 750419 502 IAW DC8 SRM 51 1 24. INSTALLED FITTING IAW DC8 SRM 51 1 20D.

Part: SKIN — CRACKED (RT ELEV)

INSPECTION TYPE:C/CK RIGHT ELEVATOR LOWER SKIN IS CRACKED OUT AT TRAILING EDGE STA XH 282. FABRICATED NEW DOUBLER IAW DC8 SRM 55 21. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51 1 8 AND 51 1 21A.

Part: SEAT TRACK — CORRODED (CABIN)

INSPECTION TYPE:C/CK SEAT TRACK B HAS CORROSION BETWEEN FS 980 1000. REMVOED SEAT TRACK B FS 980 1000. DRILLED NEW SEAT AND INSTALLED IAW DC8 SRM 51 1 24 AND 51 3 0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C/CK, STA 1690 LONGERON 29 RIGHT END FITTING CRACKED AND CORRODED. REMOVED FITTING DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 51 3 0, 5 1 1 20D, AND 51 1 24.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, C4 DOOR LOWER FWD CORNER ABOVE SCUFF PLATE GLS CRACK FROM EDGE TO RIVET. REMOVED DAMAGE IAW DC8 SRM 53 2 0, FABBED REPAIR DOUBLER FILLER IAW D C8 SRM 53 2 0 AND 51 1 20D. ALODINED AND PRIMED REPAIR DOUBLER AND FILLER IAW DC8 SRM 51 1 8. FABBED TRIPLER IAW DC8 SRM 51 1 20D AND 53 20. INSTALLED INTERCOSTAL IAW DC8 SRM 51 1 20D, WELD REPAIRED SCUFF PLATE IAW DPS 10225 LOCATED DRILLED HOLES INSTALLED SCUFF PLATE.

Part: FITTING — CRACKED (BS 900-920)

INSPECTION TYPE:C/CK MAIN CABIN STA 900 TO 920 LONGERON 7L END FITTING CRACKED. REMOVED OLD FITTING FROM AC LOCATED AND DRILLED NEW FITTING IAW DC 8 SRM 51 3 2. INSTALLED NEW FITTING IAW DC8 SRM, 51 3 0.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE:C/CK, Z FITTING CRACKED STA 1150 LONGERON 33 RIGHT TO 34 RIGHT. REMOVED Z FITTING CUT NEW FITTING AND FABBED SPLICES IAW DC8 SRM 53 2 0 FIG 2G. INSTALLED IAW DC8 SRM 51 1 20D.

Part: FORMER — CORRODED (BS 1080)

INSPECTION TYPE:C, AFT PIT FORMER CORRODED STA 1080, L36 TO 35L. REMOVED CORROSION, FABBED STRAP REPAIR AND SAM IAW REO 04666 AND DC.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE:C, AFT PIT STA 1150 AND LONG 33R AND 34R Z FITTING IS CRACKED. REMOVED Z FITTING FABBED REPAIR ANGLE AND FILLERS IAW DC8 SRM 53 2 0 FIG 2. ALODINED AND PRIMED REPAIR ANGLES AND FILLER IAW DC8 SRM 51 1 8. CUT NEW Z FITTING AT LOMATION AS SPECFIFIED IN DC8 SRM 53 2 0 FIG 2A. INSTALLED Z FITTING REPAIR ANGLES AND FILLER IAW DC8 51 1 20D.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE:C, RIGHT HAND WING REAR SPAR I/B AILERON I/B CENTER HINGE FITTING ATTACH ANGLE BENT AND CRACKED. REMOVED CRACKED ANGLE FABBED NEW ONE ON TPA 1003 REV A INSTALLED IAW DC8 SRM 51 3 0.

Part: ANGLE — CRACKED (BS 46)

INSPECTION TYPE:C/CK FLOOR SUPPORT ANGLE AT FS 46 IS CRACKED IN AREA BETWEEN LBL 50 TO LBL 62. FABRICATED FLOOR SUPPORT ANGLE AND ANGLE REPAIR IAW DC8 SRM 53 7 1. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 2 0D.

Part: SEAT TRACK — CORRODED (BS 480-500)

INSPECTION TYPE:C/CK CORROSION IN SEAT TRACK D BETWEEN FS 480 AND 500. REMOVED 4 HOLE PLUG AND ROUTED OUT FOR NEW 5 HOLE PLUG IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 PUT 5 HOLE PLUG IAW DC8 SRM 53 2 3. INSTALLED FASTENERS IAW DC8 SRM 51 3 0.

Part: FITTING — CORRODED (BS 1230)

INSPECTION TYPE:C/CK, STA 1230 LONGERON 35 RIGHT TO LONGERON 36 Z FITTING CORRODED. REMOVED FITTING CUT AND INSTALLED NEW FITTING WITH SPLICES IAW DC8 SRM 53 2 0 AND 51 1 8 AND 51 1 20D.

Part: SEAT TRACK — CORRODED (BS 70-280)

INSPECTION TYPE:C, STA 45 TRACK A CORROSION REMOVED FLOOR PANEL 1 AFS 70 TO FS 280. REMOVED CORRODED SEAT TRACK A FS 570 TO FS 280. PUT NEW SEAT TRACK, DRILLED HOLES IAW DC8 SRM 5 1 1 24. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW SEAT TRACK FS 70 TO FS 280 IAW DC8 SRM 51 3 0. INSTALLED FLOOR PANEL IAW D C8 SRM 51 3 0.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C, MAIN CABIN FITTING AT STA 781 LONG 13L CRACKED. DRILLED UP NEW FITTING IAE DC8 SRM 51 1 24. INSTALLED FITTING IAW DC8 SRM 51 1 20D. REF TO OP 50026 FOR FITTING FAB.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C/CK, LONGERON 11 RIGHT TIE FITTING FOR LONGERON CRACKED STA 680. DRILLED AND REAMED NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D AND DC8 SRM 51 3 0.

Part: FITTING — CORRODED (BS 35)

INSPECTION TYPE:C/CK, FRAME TO FLOOR FITTING AT FUSELAGE STATION 35 RIGHT SIDE IS CORRODED ON AFT FACE. REMOVED 4597643 1 ATTACHED FITTING AT FS 35 RECEIVED NEW 4597643-1. ATTACHED FITTING FROM STORES DRILLED 4597643-1 ATTACHED FITTING IAW DC8 SRM 51 1 24. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED 4597643-1, FITTING IAW DC8 SRM 51 3 0 AND DC8 SRM 51 1 20D.

Part: SKIN — CRACKED (WS 157.5)

INSPECTION TYPE:C/CK CRACKED SKIN AT RIGHT WING LEADING EDGE AUX FUEL TANK LOWER SURF XFS 157.5. FABRICATED NEW DOUBLER AND FILLER IAW DC8 SRM 57 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW DOUBLER AND FILLER IAW DC8 S RM 51 1 20D.

Part: FORMER — CORRODED (BS 1060)

INSPECTION TYPE:C/CK AFT PIT STA 1060 AND LONGERON 36 FORMER CORRODED. REMOVED FORMER FABRICATED NEW ONE IAW DWG DC8 53 0229 AND DC8 SRM 51 1 8. INSTALLED IAW DAC DWG 53 0229.

Part: SKIN — CRACKED (LT ELEVATOR)

INSPECTION TYPE:C/CK, LEFT ELEVATOR UPPER SKIN HAS 1 CRACK 2 INCHES AFT OF SPAR AT STA XE77 STOP DRILLED CRACK. FAB REPAIR IAW DC8 SRM 55 2 1 FIG 7. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 AND INSTALLED IAW DC8 SRM 51 1 21A.

Part: ANGLE — CRAKCED (EMER EXIT DOOR)

INSPECTION TYPE:C/CK RIGHT HAND FWD EMERGENCY EXIT DOOR INNER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE IAW DC8 SRM 52 7 1 HEAT TREATED 0807075-0 TO 0 80 7075 T6 IAW DC8 TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 INSTALLED IAW DC8 SRM 51 3 0.

Part: FITTING — CRACKED (AFT FUSELAGE)

INSPECTION TYPE:C/CK, LONGERON END FITTING CRACKED, 27 LEFT AT AFT PRODUCTION SPLICE. INSTALLED NEW FITTING IAW DC8 SRM 51 1 24 AND 51 1 20D AND 51 1 21 A ND 51 3 0.

Part: SKIN — CRACKED (WS 219.5)

INSPECTION TYPE:C/CK, RIGHT WING LEADING EDGE SKIN CRACKED AT XFS 219.5. CUT OUT DAMAGED AREA IN SKIN AND FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM 57 2 1. ALODINED AND PRIMED REPAIR PART A/C STRUCTURE IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW DC8 SRM 51 1 21 AND 51 1 20 D, SEALED IAW DC8 SRM 51 1 15 AND 51 1 17.

Part: SKIN — CRACKED (NR 1 PYLON)

INSPECTION TYPE:C/CK, OUTBOARD SIDE OF PYLON NR 1 CRACKED. REPAIRED PER EO 04609 AND DC8 SB 54 95 BY INSTALLING REPAIR DOUBLERS.

Part: SKIN — CORRODED (LT ELEVATOR)

INSPECTION TYPE:C, LT ELEVATOR LOWER SKIN CORRODED AROUND FASTENER AT CLOSING CHANNEL STA XE 310. MRR FILED OPEN NO CORECTIVE ACTION.

Part: RIB — CRACKED (BS 960)

INSPECTION TYPE:C, INNER RIB BETWEEN MLG DOORS FS 960 HAS CRACKS. REMOVED RIB FABBED NEW ONE ON DAC DWG 5616306, INSTALLED IAW DC8 SRM 51 1 4 AND 51 1 20D.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C/CK ZEE FITTING AT FS 1160, LONGERON 34 RIGHT TO LONGERON 33 RIGHT CRACKED. REMOVED FITTING DRILLED NEW ONE IAW DC8 SRM, 53 2 0 FIG 2G WITH SPLICES. INSTALLED IAW DC8 SRM 51 1 20D.

Part: BRACKET — CRACKED (LT SPOILER)

INSPECTION TYPE:C/CK PERMANENT REPAIR TO LEFT HAND WING INBBOARD SPOILER BRACKET PER REO DC8 5720 6998. FABRICATED REPAIR ANGLES ALODINED AND PRIMED AND INSTALLED REPAIR IAW REO DC8 5720 6998, DC8 SRM 57 2 0 FIG 2 AND DC8 SRM 51 1 8.

Part: COALESCER BAG — DIRTY (LT PACK)

OILY SMELL IN COCKPIT COMING FROM LEFT PACK. REMOVED AND REPLACED LT PACK COALESCER BAG FOR OILY OR DIRTY SMELL, RAN PACK IN BOTH HOT AND COLD SETTINGS. NO SMELL OR OIL PRESENT, LEFT PACK CK'D OK AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS NOT WORKING ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY, OPS CHK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK, CKS OK (P/N ON AND OFF 5708458-503) (S/N OFF ED-2) (S/N ON FTL 209).

Part: DOUBLER — CORRODED (BS 1120.7)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON REPAIR DOUBLER AT FUSELAGE STA 1120.7. MRR FILED OPEN.

Part: SKIN — CORRODED (AFT FUSELAGE)

WHILE ON GROUND, MAINTENANCE FOUND SKIN CORROSION AFT OF AIR COND BAY DOOR. MRR FILED OPEN.

Part: DOUBLER — CORRODED (BS 1120)

SUPPLEMENTAL MRR: WHILE ON THE GROUND, MAINTENANCE FOUND CORROSION ON REPAIR DOUBLER AT FUSELAGE STATION 1120. REMOVED PREVIOUS DOUBLER REPAIR, BEGAN TO REMOVE DAMAGE IN REFERENCE TO SRM 53-02-01, FIGURE 7. REMOVED REMAINDER OF VISIBLE CORROSION. DOUBLER INSTALLED PER EO DC8-5330-7556A.

Part: SKIN — CORRODED (FUSELAGE)

SUPPLEMENTAL MRR: WHILE ON THE GROUND, MAINTENANCE FOUND CORROSION ON THE SKIN AFT OF THE AIR CONDITIONING BAY DOOR. MAINTENANCE REMOVED THE AREA OF CORROSION AS PER SRM 53-2-1. REPAIR DOUBLER WITH BLIND FASTENERS AS PER SRM 53-2-1.

Part: FLUID — LOST (HYD SYST)

CREW REPORTED EXPERIENCE LOSS OF HYDRAULIC PRESSURE AND FLUID. PERFORMED LOSS OF HYDRAULIC CHECK LIST, CONTINUED TO MCO. NOTIFIED MIA CENTER TO INCOMING MCO APPROACH CONTROL OUR EMERGENCY AND ASKED FOR EMERGENCY EQUIPMENT TO STAND-BY. LANDING UNEVENTFUL, TAXIED CLEAR ON RUNWAY AND STOPPED. MCO MX TOWED A/C TO RAMP. MRR FILED OPEN.

Part: O-RING — FAILED (SLOT CNTRL VALVE)

CREW REPORTED HYDRAULIC SYSTEM LOST FLUID RAPIDLY IN CRUISE EMERGENCY SHUT-DOWN. HYD FLUID FELL TO STANDPIPE. FOUND O-RING BLOWN ON SLPT INLET CHECK VALVE ON SLOT CONTROL VALVE. REPLACED O-RINGS ON CHECK VALVE. LEAK CHK NORMAL PER DC8 MM 27-80-04, PG.201. CHANGED NR 3 ENG HYD PUMP AND FILTERS IAW MM 29-10-12. SERVICED HYD RESERVOIR IAW 12-30-01.

Part: O RING — FAILED (SLOT CHECK VALVE)

SUPPLEMENTAL MRR: CREW REPORTED LOSS OF HYDRAULIC PRESSURE AND FLUID. PERFORMED LOSS OF HYDRAULIC CHECK LIST, CONTINUED TO MCO. NOTIFIED MIA CENTER TO INCOMING MCO APPROACH CONTROL OUR EMERGENCY AND ASKED FOR EMERGENCY EQUIPMENT TO STAND BY. LANDING UNEVENTFUL, TAXIED CLEAR ON RUNWAY AND STOPPED. MCO MX TOWED A/C TO RAMP. MAINTENANCE FOUND O-RING BLOWN ON SLOT INLET CHECK VALVE ON SLOT CONTROL VALVE. REPLACED O-RINGS ON CHECK VALVE. OPS AND LEAK CHECK NORMAL PER DCI MM 27-80-04, PAGE 201.

Part: LONGERON — CORRODED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32R AT FS 1650. REPLACED IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 1690)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING AT L-32R AT FS 1690. REPLACED IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1690)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 32R END FITTING AT F.S. 1690. REPLACED IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 902)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 24L AT FS 902 FWD OF TRAPEZOID FITTING. REPAIRED IAW SRM 53-2-2.

Part: SKIN — DELAMINATED (NR 4 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED LT AND RT NR 4 SPOILER PANEL. REPLACED IAW M/M 27-01-01.

Part: SKIN — CRACKED (RT ELEVATOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED RT ELEVATOR LOWER SURFACE AT AFT I/B TRAILING EDGE. REPLACED IAW M/M 27-30-00.

Part: FITTING — CRACKED (BS 1640-1660)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 32R END FITTING AT F.S. 1640-1660. REPLACED IAW SRM 51-1-20D.

Part: BULKHEAD — CRACKED (BS 683)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED PRESSURE BULKHEAD ON LT SIDE TOP AT F.S. 683. REPAIRED IAW SRM 53-2-5.

Part: ANGLE — CRACKED (BS 1810)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED CENTER SPAR/AFT SPAR ANGLE ON SLANTED BELT FRAME BETWEEN HORIZONTAL STAB AT F.S. 1810, BETWEEN LONGERONS 2L-2R. REPLACED IAW SRM 51-1-21.

Part: BEAM — CRACK (STA 1766)

MAINTENANCE REPORTED APPROX 1.75 INCH CRACK AT BOTTOM RADIUS OF NR 3 ANGLE (BEAM) ON PRESSURE BULKHEAD AT CENTER. INSTALLED REPAIR IAW EO DC8-6310-6306A, TEMP REV 53-81, 53-7-0.