N840UP

Part: LINE — LEAKING (NR 4 ENG OIL)

NR 4 ENG LOW OIL PRESSURE AND QTY ON DESCENT INTO SDF. REMOVED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW MM 20-12-00-2. LEAK AND OPS CHECK GOOD IAW MM 71-00-00.

Part: OIL SYSTEM — LOW PRESSURE (NR 4 ENGINE)

NR 4 ENGINE LOST PRESSURE, SHUT DOWN WITH 20 PSI N1 16 PERCENT, N2 9.4 PERCENT 5 QUARTS INDICATED 6000 FT/200 KTS. REMOVED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW M/M 20-12-00-2. LEAK AND OPS CHECK GOOD IAW M/M 71-00-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

AT CRUISE, THE DOME LIGHT AND PEANUT LIGHTS CAME ON BY THEMSELVES NO SWITCHES WERE THROWN, NO ABNORMAL INDICATIONS OF F/E PANEL WHEN WENT TO DC TIE WITH THE FREQ SELECTOR, THE LIGHTS WENT OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. OPS CHECK GOOD.

Part: LONGERON — CRACKED (BS 1756 L14L) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 L14L STA 1756 UPPER VERT FLANGE HAS A .25 INCH CRACK FROM ATTACH FASTENER HOLE. REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON, AND SPLICE FITTING IAW SRM 51-1-21, 53-02-02 FIG 10, 51-1-8, 51-1-20D.

Part: PRESSURE PANEL — CORRODED (NLG WW) · airframe 72,646 hrs · 46,140 cycles

INSPECTION TYPE:C1 RIGHT NLG TUNNEL INTERGRANULAR CORROSION AND GUSSET MISSING ON UPPER PRESSURE DECK (CEILING) STA -32 RBL 58. REMOVED FINGER DOUBLER AND CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRO 8530026, SRM 51-1-21, 51-20D AND APPROVED EA RESPONSE.

Part: FLOORBEAM — CORRODED (FS 1760 BL0) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 CORROSION ON FLOOR SUPPORT FITTING ON AFT VERTICAL BEAM, FS 1760 BL 0. REMOVED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW SRM 51-03-00-0. FABRICATED AND INSTALLED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW DWG 5773846, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 834 L18L) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 834 L18L. REMOVED END FITTING AT STA 834 L18L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 834 L18L IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 857 L19L) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 857 L19L AFT. REMOVED FITTING AT STA 857 L19L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 857 L19L IAW DWG 4750422, AND SRM 51-1-20D.

Part: SKIN — CRACKED (NLG DOOR) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 LEFT NLG DOOR SKIN IS CRACKED ON OUTBOARD SIDE. CUT OUT DAMAGED SKIN ON LT NLG DOOR IAW SRM 52-02-03. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER ON LEFT NLG DOOR IAW SRM 52-02-0 FIG 2, AND 51-1-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,646 hrs · 25,496 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN CORRODED AT FS 60 BETWEEN L34R AND L35R. REMOVED AND REPLACED FUSELAGE SKIN FROM STA - 21.92 - STA 70 L31L TO L31R IAW UPS EO DC8-5330-8942-D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKED OK. P/N ON 5708458-503, S/N ON 10389.

Part: WIRE — SHORTED (SLIDING WINDOW)

INSPECTION TYPE: PFLT, CREW PREFLT - SMOKE IN COCKPIT. F/O'S SLIDING WINDOW ANTI-FOG WIRES SHORTED TO GROUND AT WINDOW FLEX CONDUIT AND C/B FAILED IN THE POWER CLOSED POS. WIRES & C/B REPLACED, SEE NRC 271362 - 271369 FOR DETAILS OF REPAIRS & CKS. ALL CHECKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A EO DC8-5330-24525 - A FUSELAGE SKIN DAMAGE REPAIRS AT STA 1420 LONGERON 29L AND STA 1460 LONGERON 29L. COMPLIED WITH EO DC8-5330-24525-A APPENDIX A AND APPENDIX B REPEAT INSPECTIONS DUE AT C-CHECK PERMANENT REPAIR DUE WITH IN 6000 FLT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A CREASE LEFT FUSELAGE AT STA 1340 THRU 1400. A/C FERRIED TO HEAVY MX VENDOR FOR REPAIR. RMVD DMG. PER SRM 53-02-01-0, FIG.7;VERIFIED DMG RMVD; COMPLETED REPAIR BY INSTALLING DOUBLER PER SRM 53-02-01-0,FIG 7; PRIMED & PAINTED REPAIR DOUBLER ON NRC 924844, 924845 & 924846. FUSELAGE SKIN DMG REPAIRS AT STA. 1420/29L & 1460/29L C/W EO DC8-5330-24525-A. RE- PEAT INSP. DO AT C CK. PERM. REP DUE W/IN 6000 FLT CYCLES.

Part: BATTERY PACK — INOPERATIVE (COCKPIT)

EMERGENCY LIGHT BATTERY INOP. REPLACED BATTERY PACK.

Part: UNKNOWN — CORRODED (MLG WW)

FOUND CORROSION IN LT W/W. AIRCRAFT BEING FERRIED NR 9157 TO SAA FOR REPAIR. CUT OUT CORROSION FROM EXTERNAL SKIN, AND FAB'D AND INSTALLED REPAIR PARTS FOR SKIN REPAIR. ALL WORK PERFORMED IAW SAA SK 840-727258 & UPS EO DC8-53-20523.

Part: WINDOW — JAMMED (COCKPIT)

F/O'S SLIDING WINDOW JAMMED.

Part: MECHANISM — STUCK (WINDOW)

F/O'S EMERG (CLEAR VIEW, DV WINDOW) WILL NOT OPEN. CLEANED AND LUBED F/O'S WINDOW SLIDE MECH. OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PNT EMERGENCY EXIT LIGHTS FAILED TEST REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY INOP. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY & RELAY ASSY & OPS CK GOOD IAW MM 33-50-01-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C-3. RT FS 70 L31R AND L32R, DEEP GOUGES ON EXTERIOR SKIN. REMOVED DAMAGED SKIN SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW EO DC8-53-20473 AND SAA SK840-808375.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

AFTER REMOVAL OF L33R END FITTING STA 8 FOUND L33R CORRODED OUT OF LIMITS STA 8. REF N/R 807385. REMOVED AND REPLACED LONGERON 33R STA 8 TO 70 IAW SRM 51-1-21, 1-1-21D AND 51-3-2.

Part: RIB — CRACKED (LT WING) · airframe 71,743 hrs · 24,867 cycles

LT WING CENTER L/E AT XFS 335 RIB CRACKED ON L/E LOWER SURFACE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-20D, AND 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

DEEP CORROSION AROUND SHEAR TIE FASTENER HEADS AFT SIDE OF FRAME, STA 1300 LONGERON 36. REMOVED CORROSION AND FOUND FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C-3. WING BOX BOOT FITTING CRACKED APPROX 5 IN LONG STA 759 BETWEEN L17L-L18L. CUT OUT CRACKS, FABRICATED AND INSTALLED REPAIR PARTS IAW SAASK 840-808203 AND EO DC853-20469.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

CRACKED FITTING ON TORQUE BOX AT CARGO DOOR AT FS 1160 BETWEEN L31 AND L32 R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

CRACK APPROX 3 INCHES LONG ON LONGERON 35R AT FS 1270. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 51-1-20D AND DWG'S 3758593 AND 575 0322.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L36. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT CENTER WING L/E LWR RIB CRACKED AT XFS 304. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER & ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: SKIN — DAMAGED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER L/E LWR SURFACE FASTENER HOLES ELONGATED AT XFS 527. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-11, AND 51-1-21.

Part: FUEL TANK — DAMAGED (RT WING) · airframe 71,743 hrs · 24,867 cycles

RT AUX TANK UPPER SURFACE FASTENER HOLE ELONGATED AT XW 208. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1 FIG 37, 51-1-26, 51-1-20D, AND 51-1-21.

Part: PANEL — CORRODED (LT WW) · airframe 71,743 hrs · 24,867 cycles

HEAVY CORROSION ON LT WW CEILING STA 860 LBL 61. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EO DC8-5310-22401-A AND SAA SK 840-807868.

Part: RIB — CHAFED (RT WING) · airframe 71,743 hrs · 24,867 cycles

RT CENTER WING L/E RIB CHAFED THROUGH AROUND PNEUMATIC DUCT SUPPORT ROD CONNECTION AT XFS 513. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3, RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 495. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 291. CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3, CENTER WING L/E UPPER INNER DOUBLER CRACKED .5 INCH LONG AT XFS 422. REMOVED INNER DOUBLER, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769891.

Part: RIB — CRACKED (R WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 623.500. CRACK TERMINATES AT FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: SPLICE — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERNAL DOUBLER SPLICE CRACKED .5 INCH LONG AT XFS 42 9. REMOVED 2 EA CRACKED SPLICES, FABRICATED, AND INSTALLED 2 EA REPLACEMENT SPLICES IAW DC-8 SRM 51-1-20D, DWG 5769589-15 & -17.

Part: SKIN — CRACKED (L1 DOOR) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C-3. EXTERNAL FUSELAGE L1 DOOR CUTOUT UPPER AFT CORNER, SKIN VISUALLY CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW EO DC8 5330-22342-A AND SAA SK 840-807798.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3, RIGHT CTR WING L/E LWR INNER DOUBLER AROUND DRAIN HOLE CRACKED .5 INCH LONG AT XFS 335. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INNER DOUBLER IAW DC8 SRM 57-3-3 FIG 5 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

RT CENTER WING L/E PNEUMATIC DUCT ATTACH POINT UPPER RIB CRACKED 3 INCH LONG AT XFS 304. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-15, AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 416. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RT CENTER WING L/E UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3, RIGHT OUTBOARD L/E LWR RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 603.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 609. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 778. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT OUTBOARD L/E INNER DOUBLER HAS 2 EA CRACKS AROUND DRAIN HOLE AT XFS 579. REMOVED CRACKED INNER DOUBLER, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769600-40, AND INSTALLED IAW DC-8 SRM 51-1-20D AND 51-1-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C-3. MAIN CABIN SUB FLOOR STA 960 RBL 60 UNDER FLOORBEAM AREA CORRODED. CUT OUT DAMAGE ON SUBFLOOR STA 960 RBL60. REMOVED CORROSION ON FLOORBEAM. FABRICATED AND INSTALLED FILLER, 2 FINGER DOUBLERS, 2 DOUBLERS AND 1 SPLICE DOUBLER IAW EO DC8-5310-22416-A AND SAA SK 840-8 07643.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 660. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 772.250. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: SKIN — CORRODED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT OUTBOARD L/E SKIN HAS CORROSION AT XFS 554. CUT OUT DAMAGED AREA OF L/E SKIN IAW DC-8 SRM 57-02-01 FIG 14. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-02-01 FIG 14, 51-1-26, AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE RIB CRACKED AT XFS 678.750 (LOWER RIB). STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 CRACKED LONGERON AT STA 1756 L15L AND LOOSE BOLT. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3, MAIN CABIN FLOORBEAM, EXISTING REPAIR UNDER AREA HAS HEAVY CORROSION AT STA 940 RBL 65. REMOVED EXISTING 2 FLOORBEAM REPAIRS, 1 FILLER AND FLOORBEAM. FABRICATED AND INSTALLED FLOORBEAM AND 4 REPAIR ANGLES IAW EO DC8-53-20466 AND SAA SK840-807575.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 LONGERON 15R CRACKED AT STA 1756. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

FWD ACCESSORY COMPARTMENT 680 BULKHEAD HAS CRACKS IN 4 PLACES. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13, 51-1-20D, AND 51-1-21.

Part: SKIN — CHAFED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C-3. D PIT DOOR CUTOUT AFT SIDE CHAFED AND FASTENER HAS SHORT E.D. AT STA 1440. REMOVED FASTENER AND CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, TRIP AND 2 FILLERS IAW EO DC8 5330-22423-A AND SAASK 840-807058.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE: C3, FUSELAGE SKIN CRACKED AT STA 1746 L15R. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER IAW DC-8 SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,743 hrs · 24,867 cycles

INSPECTION TYPE:C3 FUSELAGE SKIN CRACKED .25 INCH LONG AT STA 1746 L15L. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBL ER, FINGER DOUBLER, AND FILLER IAW DC-8 SRM 53-2-1 FIG 7, 51-1-20D, 51-1-21.

Part: SCREW — CORRODED (EMERGENCY DOOR)

TWENTY SCREWS & NUTPLATES CORRODED OUT OF BOTTOM OF LEFT REAR L1 TYPE DOOR. REPAIRED LEFT REAR TYPE 1 EXIT DOOR PER DC8 EO DC8-5220-19783F.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

NR 2 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY DISARM/ARM SWITCH ASSY. SWITCH TESTS OK.

Part: LIGHT — WILL NOT TEST (COCKPIT)

EMERGENCY LIGHTS WILL NOT TEST. REMOVE AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01-2 OPS CK OKAY. P/N 60-1223-5, S/N 322 OFF, P/N 5708458-503, S/N FTL010 ON.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 70,864 hrs · 24,203 cycles

INSPECTION TYPE:SP UPPER ATTACH FITTING AT STRINGER 61 IS CRACKED AT XRS 255. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4614390 AND SRM 51-1-20D.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, AFT PIT FS 1127 AT RBL 49 LOWER FLANGE OF SEAT TRACK IS CRACKED. REMOVED DAMAGED SEAT TRACK. REC'D NEW SEAT TRACK, DRILLED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, MAIN CABIN FLOORBEAM T-CAP FOUND BLENDED ON FROM AN EXISTING REPAIR STA 1620 LBL 48. FABBED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 1B. ALODINED & PRIMED ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-20D.

Part: CAP — CRACKED (L/H HORZ STAB) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE:C-2 LT HORIZ STAB INBOARD LOWER CAP CRACKED. REMOVED LT HORIZ L/E CAP, PERFORMED HEFC IAW NDT SPM 06-10-001.01. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21/51-1-20D.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, RT HORZ STAB INBOARD BOX LOWER CAP CRACKED. REMOVED RT HORZ LEADING EDGE CAP LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766-1806 LONG 17L IS CRACKED. REMOVED CRACKED LONG 17L AND END FITTING AND REPLACED WITH NEW LONG 17L AND END FITTING IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 5 1-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766 - 1806 LONG 17R IS CRACKED. REMOVED L17R AND END FITTING TO FOM. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED L17R & END FITTING IAW DC8 SRM 51-1-21/51-1-20D.

Part: FITTING — CRACKED (STRINGER) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, NR 56 STRINGER HAS AFT STRINGER END FITTING CRACKED, NR 4 ALT. REC'D NEW FABBED FITTING, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. DRILLED, LOCATED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, LT HORZ STAB INBOARD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. REMOVED LT HORZ STAB INBOARD BOX T-CAP, REC'D NEW FITTING LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, MAIN CABIN - FLOORBEAM TO FUSE ATTACHMENT FRAME STA 915 RBL 66 APX CORRODED. REMOVED CORROSION ON FRAME FITTING, OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING, LOCATED, DRILLED, AND DEBURRED FITTING IAW DAC DWG 5643483. INSTALLED FRAME FITTING IAW DC8 SRM 51-1-20D, 51-3 -0 AND DAC DWG 5643483.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, RT HORIZONTAL STAB INBD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. PERFORMED E/C INSP OF LOWER TEE CAP IAW NDT SPM 06-10-01.001 CRACKED AT RADIUS. REMOVED ANGLE LOCATED AND DRILLED NEW ANGLE IAW DC8 SRM 5 1-1-24, INSTALLED NEW ANGLE IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D.

Part: LATCH — CRACKED (CARGO DOOR) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, C-PIT CROSS SLIDE DOOR LOWER JUST AFT OF CENTER LATCH HOOK CRACKED. REMOVED FASTENERS IN WEB IAW DC8 SRM 51-1-21 & 51-3-0 FOR ACCESS. REMOVED CRACKED LATCH HOOK IAW DC8 SRM 51-1-21. INSTALLED LATCH HOOK AND WEB IAW DC8 SRM 51-1-21, 51-1-20D, AND 51-3-0.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER, DOOR PAN AND DOOR SEAL CRACKED. REMOVED SEAL DEPRESSOR, DOOR PAN. FABBED REPAIR DOUBLER FOR DRAINPAN AND FABBED NEW SEAL DEPRESSOR. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, MAIN CABIN TRACK CORRODED ON LOWER SIDE IN CARGO PIT RT TUNNEL STA 1243 RBL 62. REMOVED EXISTING SEAT TRACK SECTION. LOCATED, DRILLED & DEBURRED NEW SECTION OF TRACK AND SPLICES (P/N 60-15176), DC8-53B-003-502 (2) IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-3-0.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, AFT CARGO PIT RT TUNNEL FUSELAGE SKIN AND L22R REPAIR NOT PER SRM STA 1230-1240 L22R-L21R. REMOVED OLD DOUBLER AND LONG AND SPLICE FABBED NEW DOUBLER, TRIPLER, LONGERON SECTION. INSTALLED DOUBLER, TRIPLER, LONGERON SECTION LONGERON SPLICE, END FITTING IAW DC8 SRM 53-2-2 & 51-1-20D.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, FWD PIT STA 320 LBL 27 FLOORBOARD, TRACK CORRODED. REMOVED CORROSION, WITHIN LIMITS IAW DC8 SRM 53-2-3. FOUND SCALLOP ON UPPER SURFACE WORN BEYOND LIMITS IAW DC8 SRM 53-2-3. REMOVED AND REPLACED TRACK SECTION IAW DC8 SRM 51-3-0, 53-2-3 FIG 14 AND UPS DWG 53B-0 03. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED UPS SPLICE DC8- 53B-003-501 IAW UPS DWG DC8-53B-003.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, R1 DOOR JAMB UPPER AFT CORNER CRACKED 2 EACH, FOUND WITH NDT. REMOVED DAMAGE IAW DC8 SRM 53-2-0, FABBED FILLER, DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0, TR 53-126 & ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 53-2-0 AND TR 53-126.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, BS 50 - 54 S-21L CUSP FRAME CRACKED APPROX 4.5 INCH LONG. FABBED -31 FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -31 FRAME IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, L1 DOOR JAMB LOWER AFT CORNER CRACKED 1 EA MARKED FOUND WITH NDT. REMOVED FLOORBOARD INBOARD OF L1 DOOR FOM, CUT OUT CRACK AND FABBED DOUBLERS AND FILLER IAW DC8 SRM 53-25-0 TR 53-128 TR 53-155. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-20D. INSTALLED FLOORBOARD IAW DC8 SRM 51-3-0, INSTALLED SEAL DEPRESSOR IAW DC8 SRM 51-1-21.

Part: ANGLE — CRACKED (KEELBEAM) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, CRACK IN ANGLE ATTACHING TO KEELBEAM AT STA 902 BETWEEN MLG DOORS. REMOVED AND REPLACED FITTING (P/N 4775262-501) IAW DC8 SRM 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, L2 DOOR JAMB UPPER AFT CORNER CRACKED 1 EA MARKED FOUND WITH NDT. FAB AND INSTALLED -11, -13 DOUBLERS AND -23 FILLER IAW DC8 SRM 53-2- 0 FIG 18. ALSO, INSTALLED INTERCOSTAL TO SKIN ATTACH ANGLE WEB AND 2 END FITTINGS AT APPROX L10L-L11L FS 1640 LT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE:C-2 FWD PIT RBL 45 STA 70 FLOORBEAM CORRODED. BLENDED OUT CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SRM 51-1-21 & 51-3-0. RESECURED SEAT TRACK AND INSTALLED 4 EA FLOORBOARDS IAW DC8 SRM 51-3-0.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,808 hrs · 24,125 cycles

INSPECTION TYPE: C-2, L1 DOOR FRAME UPPER FWD CORNER CRACKED 4 EA MARKED FOUND WITH NDT. REMOVED CRACKED AREAS IAW DC8 SRM 53-2-0 FIG 15 AND TR 53-128. FABBED DOUBLER, TRIPLER AND FILLER IAW D8 SRM 53-2-0 FIG 15. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER, TRIPLER, & FILLER IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, ON PREFLIGHT EMERGENCY EXIT LIGHTS INOP, SAME MALFUNCTION ON 3/19/03. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: MODULE — DEFECTIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT MODE PANEL UNARMED STAYS ON IN ARMED POSITION. FOUND PANEL DEFECTIVE REPLACED EMERGENCY LIGHTS MODULE AND OPS CHECKS NORMAL.

Part: ACCESS PANEL — LOOSE (FUSELAGE)

INSPECTION TYPE:N/A PASSING 12,000 FEET LOUD BANG FROM RT FRONT SIDE OF AIRCRAFT FOLLOWED BY AIRCRAFT DEPRESSURIZATION. SUSPECT HAIL STORM PRIOR TO TAKEOFF EMERGENCY ACCESS FOR F/O SLIDING WINDOW DISLODGED RE-INSTALLED ACCESS PNL, OK FOR CONTINUED SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 EXTERNAL FUSELAGE STA 1740 L28R - L30R SKIN HAS A BULGE AND ONE FASTENER HEAD BELOW SKIN. REMOVED FASTENER IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT-OF-LIMITS IAW DC8 SRM 53. FAB EXTERNAL DOUBLER FINGER DOUBLER AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 AFT PIT FS 1160, L36-L35 BATHTUB FITTING IS CRACKED. REMOVED DAMAGED FITTING, FABBED SPLICE ANGLES, ALODINED AND PRIMED. INSTALLED NEW FITTING AND SPLICE ANGLES IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.

Part: SKIN — CRACKED (NR4 PYLON) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 NR 4 PYLON O/B WEB PNL FWD ACCESS HOLE HAS APPROX 1 INCH CRACK ON LWR SIDE. REMOVED FASTENER -22 & -28 IAW REO G08127 DC8 SRM 51-1-21 51-1-20D & 51 -3-0 MAT ID FOR -3 -5 DOUBLERS .125 7075-T6 PO 340779 IAW REO G08127. LOCATED AND DRILLED -3 -5 DOUBLERS IAW REOG008127 DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED -22 -28 STIFFENERS AND -3 -5 DOUBLERS IAW REO G08127 DC8 SRM 51-1-11, 51-1-20D, 51-1-21, 51-3-0.

Part: STOP FITTING — CORRODED (CARGO DOOR) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 AFT PIT D-DOOR LT STOP CORRODED. REPLACED DOOR STOP IAW DC8 SRM 51-1-24.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 AFT PIT FS 1140 L35R INTERCOSTAL ATTACH FITTING IS CRACK. REMOVED AND REPLACED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FASTENER — LOOSE (RT WING) · airframe 69,713 hrs · 23,344 cycles

INSPECTION TYPE:C1 1 FASTENER LEAKING FUEL AT XRS 500 BOTTOM NR 4 ALT. REMOVED FASTENER IAW DC8 SRM 51-1-20D OVERSIZED HOLE FOR BUSHING INSTALLATION AS REQD PER REO G0123, FABBED BUSHING AND INSTALLED PER REO G0812 3. INSTALLED NEW DOUBLER -502 IAW DC8 SRM 51-1-20D AND REO G08123.

Part: BATTERY — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER M33-50-01.

Part: STRUCTURE — LOOSE (KEELBEAM)

INSPECTION TYPE:IN, KEEL BEAM STRUCTURE BETWEEN MAIN GEAR DOORS LOOSE.

Part: FITTING — CRACKED (BULKHEAD)

INSPECTION TYPE:IN, LT W/W OUTBOARD FWD BULKHEAD HAS 4 CRACKS AROUND HYD LINE BULKHEAD FTG (MARKED). *S/D* REMOVED DAMAGED MATERIAL. INSTALLED DOUBLER PER SRM 53-2-0 FIG 23.

Part: SEAT TRACK — CORRODED (CABIN)

INSPECTION TYPE:C3, FS 1300, 1310, 1320 AND 1340, RBL 45 THE SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C3, FS 55 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: FLOORBEAM — CORRODED (BS 70)

INSPECTION TYPE:C3, FS 70 FLOORBEAM AT RBL 48 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DHC SK840-349.

Part: SKIN — CORRODED (BS 1654)

INSPECTION TYPE:C3, FUSELAGE SKIN AND DOUBLER AT FS 1654 AND LONG 31L ARE CORRODED BEYOND LIMITS. REPAIRED SKIN AND INTERNAL DOUBLER IAW DHC SK840-923.

Part: LONGERON — CORRODED (BS 1665)

INSPECTION TYPE:C3, LONG 23L AT FS 1665 HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION FABRICATED AND REPLACED LONGERON IAW DWG 5646666 AND SRM 51-1-20D.

Part: SKIN — DAMAGED (BS 1280-1300)

INSPECTION TYPE:C3, FUSELAGE SKIN AT FS 1280 TO 1300 LONG 25R TO 27R REQUIRES REPAIR. REPAIRED FUSELAGE SKIN IAW DHC SK840-064.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:C3 FS 1220 FRAME, FWD FLANGE AT LONGERON 33R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — DAMAGED (BS 55)

INSPECTION TYPE:C3, FS 55, LBL 54 TO RBL 54, THE FLOOR SUPPORT FITTINGS REQUIRE REPAIR. REPAIRED DAMAGED FLOOR SUPPORT FITTINGS IAW DHC SK840-196 AND DHC SK840-172.

Part: LONGERON — CRACKED (BS 540)

INSPECTION TYPE:C3, LONG 18L AT FS 540 IS CRACKED. REMOVED DAMAGED SECTION, FABRICATED, AND REPLACED LONGERON IAW SRM 53-2-2.

Part: FITTING — CRACKED (BS 55)

INSPECTION TYPE:C3 SUPPORT FITTING AT FS 55, LBL 48 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: DOUBlER — CRACKED (BS 1360-1390)

INSPECTION TYPE:C3, FS 1360 TO 1390, LT CUSP, THE FINGER DOUBLER IS CRACKED IN 2 PLACES. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5779936 AND SRM 51-1-21.

Part: FRAME — CORRODED (BS 1000)

INSPECTION TYPE:C3, FS 1000 FRAME AT LBL 32 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 2.

Part: INTERCOSTAL — CORRODED (BS 1280)

INSPECTION TYPE:C3, FS 1260-1280 AT LONG 33R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1060)

INSPECTION TYPE:C3 FS 1060 FRAME AT LONG 35L TO 35R IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPAIRED FRAME IAW SRM 53-2-0.

Part: FITTING — CORRODED (BS 1270)

INSPECTION TYPE:C3, LONG 35R SPLICE AT FS 1270 IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 370-530)

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, FS 370 TO 530, RBL 60, LWR FLANGE IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK FROM FS 370 TO 530, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 55)

INSPECTION TYPE:C3, MAIN CABIN SUPPORT FITTING AT FS 55, RBL 48, FWD OTBD IS CRACKED. REMOVED AND REPLACED FITTING EAW SRM 51-1-20D AND 51-1-21.

Part: SKIN — CORRODED (VERTICAL STAB)

INSPECTION TYPE:C3 VERTICAL STAB L/E SKIN AT ZFS 30.5 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1 FIG 4.

Part: SKIN — DAMAGED (BS 1260-1280)

INSPECTION TYPE:C3, REPAIR FUSELAGE SKIN AT LONG 31R BETWEEN FS 1260 AND 1280 IAW DH SK 840-431. COMPLIED WITH DH SK 840-431.

Part: FLOORBEAM — CORRODED (BS 180)

INSPECTION TYPE:C3 FS 180 FLOORBEAM AT RBL 24 IS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM IAW DH SK840-665.

Part: FRAME — DAMAGED (BS 100)

INSPECTION TYPE:C3 FS 100 FRAME AT LONG 20R HAS A HOLE DRILLED IN THE RADIUS. REPAIRED FRAME IAW DH SK840-071.

Part: RIB — CRACKED (WS 847.5)

INSPECTION TYPE:C3 RT WING L/E RIB AT XFS 847.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CORRODED (BS 1020)

INSPECTION TYPE:C3, FUSELAGE FRAME AT FS 1020 AND LONG 34L HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0.

Part: FRAME — DAMAGED (BS 1240)

INSPECTION TYPE:C3, FS 1240 FRAME ABOVE LONGERON 21L HAS A HOLE DRILLED THRU THE RADIUS. REPAIRED FRAME IAW DH SK840-049.

Part: SPLICE — CORRODED (BS 1100)

INSPECTION TYPE:C3, FS 1100 FRAME UPPER LIP AT LONG 27R HAS HEAVY CORROSION. REMOVED DAMAGED SPLICE, FABRICATED AND REPLACED IAW DWG 3773159 AND SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (BS 120-140)

INSPECTION TYPE:C3 FS 120-140 AT LONG 14R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IAW DWG 5615614 AND SRM 51-1-21.

Part: CUSP — CORRODED (BS 1320-1365)

INSPECTION TYPE:C3, RT CUSP FS 1320 TO 1330 & 1340 TO 1365 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED CUSP IAW SRM 53-2-5.

Part: CUSP — CORRODED (BS 390-400)

INSPECTION TYPE:C3 LT CUSP AT FS 390 TO 400, THE UPPER SURFACE IS CORRODED BEYOND LIMITS. REMOVED CUSP BEAM FROM FS 370 TO 470. FABRICATED CUSP AND REPAIR ANGLES IAW SRM 53-2-5 FIG 15A. CPCP

Part: FITTING — CORRODED (BS 1150)

INSPECTION TYPE:C3, BATHTUB FITTING AT FS 1150 AND LONG 35R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:C123, STA 1180, THE LONGERON END FITTING IS CORRODED (STR 35R). REMOVED AND REPLACED FITTING IAW DWG 3753845-1.

Part: LONGERON — CRACKED (BS 1270)

INSPECTION TYPE:C3, LONG 35L IS CRACKED AT FS 1270. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE:C3 INBD SIDE OF THE STA XRS 74 BULKHEAD, THE STRINGER 51 AFT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (WS 74.5)

INSPECTION TYPE:C3, RT WING O/B OF THE XRS 74.5 BULKHEAD, BOTH STRINGER 51 END FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (WS 74.5)

INSPECTION TYPE:C3 INBD SIDE OF THE XRS 74.5 BULKHEAD, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-1-23.

Part: ANGLE — CRACKED (WS 7.5)

INSPECTION TYPE:C3 LT WING INBD L/E UPPER INBD AFT L/E ATTACH ANGLE IS CRACKED, STA XFS 7.5. REMOVED, FABRICATED, AND INSTALLED ANGLE IAW DWG 5269646 AND SRM 51-3-0.

Part: RIB — CRACKED (WS 841.25)

INSPECTION TYPE:C3 RT WING L/E RIB AT XFS 841.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 828.750 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 435.789)

INSPECTION TYPE:C3 LT WING L/E RIB AT XS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 847.5)

INSPECTION TYPE:C3 LT WING L/E RIB AT XFS 847.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 603.75)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 603.75 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 735)

INSPECTION TYPE:C123, RT WING L/E RIB AT STA FS 735.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 647.5)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 647.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 372.75)

INSPECTION TYPE:C3 LT WING L/E RIB AT XFS 372.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 598)

INSPECTION TYPE:C3 LT WING L/E AT XFS 598, THE LWR SKIN T/E DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND INSTALLED DOUBLER IAW DWG 5641255 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 572.5)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 572.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 835)

INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 835 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 461.372)

INSPECTION TYPE:C3 LT WING L/E RIB AT XS 461.372 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C3 MAIN CABIN, FS 742 AT RBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: CLIP — CRACKED (LT WING)

INSPECTION TYPE:C3 LT WING UPPER L/E RIB, ABOVE THE NR 2 PYLON STA XW 239, THE FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED CLIP IAW DWG 9753294 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 741.25)

INSPECTION TYPE:C123, RT WING L/E RIB AT STA FS 741.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C3 LONG 1 END FITTING AT STA 70 IS CRACKED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-1.

Part: SKIN — CORRODED (WS 761)

INSPECTION TYPE:C3 LT WING L/E SKIN AT XW 761 IS CORRODED BEYOND LIMITS. REPAIRED IAW EO DC8-5720-7767.

Part: RIB — CRACKED (WS 484.895)

INSPECTION TYPE:C3 LT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: CUSP — CORRODED (BS 1305)

INSPECTION TYPE:C3, LT CUSP AT FS 1305 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-5 FIG 15A.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C3 FS 1690, THE AFT LONG 32R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123, MAIN CABIN AT STA 680 BL 0, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C123, MAIN CABIN AT STA 781 AND RBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 822)

INSPECTION TYPE:C123, MAIN CABIN AT STA 822 LBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C3 MAIN CABIN AREA, FS 781, LBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D.

Part: SEAT TRACK — CRACKED (BS 789)

INSPECTION TYPE:C3, FS 798 AT RBL 24, THE FRAME IS CRACKED AT THE SEAT TRACK ATTACH POINT. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123, MAIN CABIN AT STA 680 AND RBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE:C123 MAIN CABIN AT STA 717 AND RBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1690)

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

Part: FITTING — CORRODED (BS 1347)

INSPECTION TYPE:C3, LT FLOORBEAM TO FUSELAGE FRAME FITTING AT FS 1347 HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754047 AND SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1690)

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

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C123 STA 1690, THE AFT LONG 30R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 798)

INSPECTION TYPE:C3, FS 798 AT RBL 24, THE SEAT TRACK ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:C3 FS 1220 AT 34R, THE BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 610)

INSPECTION TYPE:C123, STA 610, THE STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750257 AND SRM 51-1-20D.

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

INSPECTION TYPE:C3, FS 560 TO 580, LBL 60, THE SEAT TRACK UPPER FLANGE LWR SURFACE HAS HEAVY EXFOLIATION CORROSION UNDER AND AROUND THE CLIP NUTS. CUT OUT DAMAGED SEAT TRACK SECTION, FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-2-3 FIG 84.

Part: FITTING — CRACKED (BS 902-920)

INSPECTION TYPE:C3 LONG 4L END FITTING AT FS 902 TO 920 IS CRACKED. REMOVED AND REPLACED THE END FITING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1178)

INSPECTION TYPE:C3 FS 1178 AT LONG 21R, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 275-305)

INSPECTION TYPE:C3, FS 275 TO 305, LBL 45, THE SEAT TRACK UPPER FLANGE, LWR SURFACE HAS MODERATE CORROSION AROUND THE CLIP NUTS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 380-400)

INSPECTION TYPE:C123 STA 380-400 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 320)

INSPECTION TYPE:C123 STA 320 AT LONG 27L, THE FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 375041 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220-1240)

INSPECTION TYPE:C123 STA 1220-1240 STR 4L SPLICE FITTING IS CRACKED. REMOVERD AND REPLACED FITTING IAW DWG 4646163 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE:C3 FS 300, ABOVE LONG 27L, THE FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 260)

INSPECTION TYPE:C3 FS 260 SHEAR TIE BETWEEN LONG 32R AND 31R IS CRACKED. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A.

Part: FITTING — CRACKED (BS 902-920)

INSPECTION TYPE:C3, LONGERON 5L END FITTING AT FS 902-920 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: STRAP — CORRODED (BS 902)

INSPECTION TYPE:C3 FS 902 FRAME STRAP AT LONGERON 18L HAS HEAVY CORROSION. REMOVED, FABRIACTED, AND INSTALLED STRAP IAW DWG 5750020 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 55-70)

INSPECTION TYPE:C3, FS 55 TO 70, LBL 60, THE 9G NET ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5890314 AND SRM 51-1-20D AND 51-1-21.

Part: SEAT TRACK — CRACKED (BS 1040)

INSPECTION TYPE:C3, SEAT TRACK RBL 24 AT FS 1040 IS CRACKED AND CORRODED. REMOVED SEAT TRACK FROM FS 970 TO 1090, FABRICATED AND INSTALLED SEAT TRACK IAW EO DC8-5320-5167.

Part: SEAT TRACK — CORRODED (BS 500)

INSPECTION TYPE:C3, HEAVY CORROSION AROUND SEAT TRACK PLUG AT FS 500, RBL 48. REMOVED DAMAGED SEAT TRACK FROM FS 450 TO 727. FABRICATED, AND INSTALLED SEAT TRACK IAW SRM 53-2-3.

Part: SEAT TRACK — CRACKED (BS 1220)

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, RBL 48 AT FS 1220 IS CRACKED AND CORRODED. CUT OUT SEAT TRACK, FS 1170 TO 1270, FABRICATED AND SPLICED IN A NEW SECTION IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 675-683)

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK IS CORRODED AT FS 675 TO 683, RBL 48. REMOVED DAMAGED SEAT TRACK, FS 480 TO 727, INSTALLED NEW SECTION IAW SRM 51-3-0.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:C3 LONG 32L END FITTING AT FS 70 IS GOUGED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C3, FS 280 AT LONG 27R, IN THE TORQUE BOX, THE SUPPORT CHANNEL ATTACH FITTING IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 600)

INSPECTION TYPE:C3 HEAVY CORROSION ON SEAT TRACK FS 600, RBL 24. REMOVED CORRODED SEAT TRACK, FS 580 - 610. FABRICATED, AND REPLACED SEAT TRACK IAW SRM 53-2-3, CPCP.

Part: SEAT TRACK — CRACKED (BS 950)

INSPECTION TYPE:C3, SEAT TRACK RBL 48 AT FS 950 IS CORRODED AND CRACKED. REMOVED DAMAGED SEAT TRACK, FABRICATED AND REPLACED IAW SRM 53-2-3.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C3 LT WING L/E LWR SKIN AT THE INBD AFT CORNER OF THE INBD SLOT IS CRACKED, STA XILD .7095. REPAIRED L/E SKIN IAW EO DC8-5720-4087.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE:C3 LT WING L/E SKIN ABOVE THE NR 2 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED, FABRICATED REPAIR DOUBLER IAW SRM 57-2-1A FIG 1.

Part: FITTING — CRACKED (RT WING)

INSPECTION TYPE-C3, RT WING T/E AT WS 5.812. THE FLAP SUPPORT FITTING ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 4652201 AND SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1560-1580)

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK INBD FLANGE HAS HEAVY CORROSION, FS 1560-1580, RBL 59. CUT OUT DAMAGE SECTION OF SEAT TRACK FS 1560-1600 IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C123, STA 1690, THE STR 28R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:C3 LONG 28L END FITTING IS CRACKED JUST FWD OF FS 1690. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1567)

INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK UPPER INBD FLANGE HAS HEAVY CORROSION UNDER THE DOME AT FS 1567, LBL 59. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK, FS 1550-1667 IAW SRM 53-2-3.

Part: CONNECTOR — CORRODED (CABIN)

AFTER T/O, THE EMERGENCY LIGHTS ILLUMINATED FOR NO APPARENT REASON. CYCLED THREE EM LT CBS TO NO AVAIL. CLEANED CONNECTOR AT BATT PACK CK OK MM 33-50-01.

Part: CONTAINER — DAMAGED (ESCAPE SLIDE)

INSPECTION TYPE-N/A, ESCAPE SLIDE KEEPS FALLING OUT OF ITS CONTAINER. INSTALLED NEW CONTAINER AS REQUIRED, ESCAPE AND GRIP BAR OPS NORMAL.

Part: SKIN — CORRODED (BS 1150)

INSPECTION TYPE-N/A, BULGED SKIN AT STA 1150 LONGERON 15L. ALSO, HAS TWO POPPED HI-LOK, POSSIBLE CORROSION. REPAIRED DAMAGED AREA AS PER EO DC8-5330-10018 APPX B AND C ONLY.

Part: SKIN — CORRODED (BS 1220)

INSPECTION TYP-N/A, SKIN BULGED AND HAS TWO POPPED HI-LOKS STA 1220 LONGERON 36. POSSIBLE CORROSION JUST UNDER AFT SIDE OF NR 3 PIT. REPAIRED PER UPS EO DC8-5330-10018A APPX B AND C ONLY.

Part: BUNGEE ACTUATOR — LEAKING (LT MLG)

INSPECTION TYPE-N/A, AIR TURNBACK DUE TO HYD LEAK SHORTLY AFTER TAKEOFF. LOST HYD DOWN TO AUX PUMP QUANTITY. FOUND LMLG BUNGEE ACTUATOR LEAKING. REPLACED ACTUATOR PER MM 32-32-03 AND SERVICE BULLETIN 32-133. PERFORMED GEAR SWING, OPS AND LEAK CHK GOOD.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-C, L-WING UPPER SKIN CRACKED AT FASTENER HOLE UNDER FUEL ACCESS PANEL 505F. REPAIRED IAW SRM 57-2-1.

Part: RIB — CRACKED (BS 778.75)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED STA 778.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 828.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 828.250 THE UPPER L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 735.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 735.250, THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 822.500 THE UPPER L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 478.897)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA XS 478.897. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 853.75)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 853.750. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING L/E INNER DOUBLER CRACKED JUST AFT AND INBD OF O/B SLOT DOOR. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW SRM 51-1-20D AND DWG 5769891.

Part: RIB — CRACKED (WS 790)

INSPECTION TYPE-C, LT WING L/E RIB LOWER ARM CRACKED AT FSTR HOLE STA 790. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-C, RT WING L/E RIB LWR ARM CRACKED BY AFT FSTR AT XFS 810.00. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 291.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 291.50. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-C, LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 641.25)

INSPECTION TYPE-C, LT WING STA 641.250 L/E RIB (UPPER) CRACKED AND HOLES WITH NO PITCH. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21, AND DWG 5769400.

Part: RIB — CRACKED (WS 772)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 772.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 816.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 810.00, THE L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 803.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 803.750 UPPER RIB CRACKED. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 753.75)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 753.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 722.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 722.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE-C, RT WING L/E O/B OF O/B SECTION O/B END, L/E HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW UPS EO DC8-5720-4087-B APDX C.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 797.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 741.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 741.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 810)

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

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 778.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA 785.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 772.5)

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

Part: RIB — CRACKED (WS 716.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 716.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 678.75)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED AT AFT FASTENER HOLE AT FS 678.75. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 647)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 647.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0, 51-1-21, AND 51-1-20D.

Part: RIB — CRACKED (BS 760)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 760.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 816.250. REPAIRED IAW SRM 57-2-0.

Part: JAMB — CRACKED (SERVICE DOOR)

INSPECTION TYPE-C, EXT FUSELAGE RT FWD SERVICE DOOR UPPER FWD DOOR JAMB HAS CRACK. REPAIRED IAW SRM 53-2-0.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA 791.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 635.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0.

Part: RIB — CRACKED (BS 753.75)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA 753.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 616.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 735)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED AT AFT FSTR STA 735.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING O/B SLOT UPPER O/B PANEL LAND RIB CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 741.25)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED STA 741.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (BS 747.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 747.500. REPAIRED IAW SRM 57-2-0.

Part: STRAP — CRACKED (WS 597.508)

INSPECTION TYPE-C, RT WING L/E AT STA XFS597.508 THE UPPER RIB TIE STRAP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STRAP IAW SRM 51-1-21 AND DWG 5655441.

Part: RIB — CRACKED (WS 672.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 672.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0.

Part: RIB — CRACKED (WS 803.75)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 803.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 610)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 610.00. REPAIRED IAW SRM 57-2-0.

Part: WEB — CRACKED (BS 65-70)

INSPECTION TYPE-C, WEB BETWEEN FRAMES AT FS 65 AND 70 AND BETWEEN LONGERONS 21L AND 13L HAVE NUMEROUS DOUBLE DRILLED HOLES, OPEN HOLES, AND CRACKS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-21 AND DWG 5597645.

Part: SEAT TRACK — CORRODED (BS 1420-1470)

INSPECTION TYPE-C, SEAT TRACK LBL 45 HAS HEAVY CORROSION FS 1464 TO 1470 AND MODERATE CORROSION FS 1420 TO 1430. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.

Part: FITTING — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING UPPER STRINGER END FITTING CRACKED JUST AFT OF MLG ACTUATOR. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE-C, NR 3 CARGO COMPT AT FS 1150 STR 33R, INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1141)

INSPECTION TYPE-C, NR 3 CARGO COMPT FS 1141 STR 33R, BOTH INTERCOSTAL TIE FITTINGS FWD END ARE CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-20D AND DWG 4758514.

Part: FITTING — CRACKED (CARGO COMPT)

INSPECTION TYPE-C, NR 3 CARGO COMPT AFT LWR T-BOLT BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1540-1560)

INSPECTION TYPE-C, FS 1540 TO 1560 STR 26R HAS SEVERE CORROSION IN BOTTOM CHANNEL AND SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2-2.

Part: INTERCOSTAL — CRACKED (BS 1150)

INSPECTION TYPE-C, NR 3 CARGO COMP AT FS 1150 STR TO 33L INTERCOSTAL TIE FITTING CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-C, LONGERON END FITTING 33L FWD SIDE OF FS 70 CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: SHEAR TIE — CRACKED (BS 1580)

INSPECTION TYPE-C, FS 1580 FRAME FWD SIDE 2 EA SHEAR TIES ARE CRACKED BTWN STR 25R AND 28R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIES IAW SRM 51-1-21, 51-1-20D, AND 51-4-1.

Part: STRINGER — CRACKED (BS 1540-1560)

INSPECTION TYPE-C, FS 1540 TO 1560 STR 24R HAS SEVERE CORROSION AND CRACKING ON TOP INSIDE FLANGE. REMOVED DAMAGE, FABRICATED, AND INSTALLED SPLICE IAW SRM 53-2-2.

Part: FITTING — CRACKED (BS 1231)

INSPECTION TYPE-C, NR 3 CARGO COMPT FS 1231 STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4758514-519.

Part: WIRE — LOOSE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DISARMED CAME ON DURING CLIMB, COULD NOT RESET. FOUND LOOSE WIRE ON SWITCH 2TL11-S6M. RESECURED, OPS CHECK GOOD IAW MM 33-50-01.

Part: COALESCER BAG — CONTAMINATED (LT PACK)

INSPECTION TYPE N/A PIREP, LEFT PACK TRIPPED, RESET AND SELECTED WARMER TEMP, SELECTED LEFT PACK ON AND GOT PACK SMOKE IN COCKPIT. REPLACED CONTAMINATED COALESCER BAG IAW 21-55-03, OPS CHECK GOOD (P/N 22D10).

Part: DOOR JAMB — CRACKED (FS 1350)

WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED AFT BAG BIN DOOR JAM CRACKED .50 INCH LONG AT FS 1350, LONGERONS 32R-33R. REPAIRED PER UPS EO DC853-1615.

Part: DOUBLER — CRACKED (FS 1595-1600)

WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED FS 1595-1600, FINGER DOUBLER CRACKED AT LONGERON 31R. REPLACED FINGER DOUBLER PER SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1580 SHEAR TIE CRACKED AT LONGERON 31, 32 AND 34R. REPAIRED SHEAR TIE PER SRM 53-3-0 AND 51-1-20D.

Part: LONGERON — CRACKED (FS 1600)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1600 LONGERON 31R CRACKED. REPLACED PER UPS EO DC8-53-1613.

Part: FITTING — CORROSION (FS 280)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED B/T FITTING HAS HEAVY CORROSION AT FS 280 BETWEEN LONGERONS 32R AND 33R. REPLACED FITTINGS PER SRM 51-1-21D.

Part: FITTING — CRACKED (FS 280)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BANANA FITTING CRACKED AT FS 280 LONG 32R. REPLACED FITTING PER SRM 51-1-20D.

Part: DOUBLER — CORROSION (FS 155)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ADF ANTENNA INNER AND OUTER DOUBLERS HAVE HEAVY CORROSION AT FS 155 LONGERONS 35L AND 36L. REPLACED BOTH DOUBLERS PER SRM 51-1-21.

Part: LONGERON — CRACKED (FS 242)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 34R I/B SECTION CRACKED AT FS 242. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: DOUBLER — CRACKED (FS 70-80)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 70 TO 80, LONGERON 31L FINGER DOUBLER CRACKED. REPLACED DOUBLER PER SRM 51-1-20D AND 53-2-0.

Part: LONGERON — CORROSION (FS 280-300)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON I/B SIDE OF LONGERON 34R BETWEEN FS 280 TO 300. REPLACED LONGERON ON T/C 43627 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FS 80)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE CRACKED AT FS 80, LONGERON 34R AND 35R. REPLACED SHEAR TIE PER SRM 53-2-0.

Part: STRAP — CRACKED (NR 2 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRAP CRACKED AT NR 3 PYLON INSIDE FWD TANK AT NR 2 STR. REPLACED STRAP PER SRM 51-1-20D.

Part: FLOOR BEAM — CORROSION (FS 80)

WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED WEB JUST ABOVE OUTBOARD END OF FS 80, FLOOR BEAM HAS HEAVY CORROSION. REPLACED WEB SECTION PER SRM 51-1-20D.

Part: SHEAR TIE — CORROSION (FS 1080)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE HAS CORROSION DAMAGE AND BROKEN AT FS 1080 O/B OF LONG 35R. REPLACED SHEAR TIE PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1230)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING FS 1230 LONG 35R TO 36. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 70-190)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 80 HEAVY CORROSION ON LONGERONS 35R. REPLACED LONGERONS FS 70 TO 190 PER SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 215-260)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 36L HAS MODERATE CORROSION AT FS 215 TO 260. REPLACED LONGERON SECTION PER SRM 51-1-21.

Part: LONGERON — CORROSION (FS 194-246)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON LONG 35L I/B FS 194 TO 246. REPLACED LONG SECTION PER SRM 51-1-20D.

Part: DOUBLER — CORROSION (FS 260-360)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 'A' CSD INNER DOUBLER HAS CORROSION REPAIRS ON FS 260 TO 360 LONGERONS 27R TO 35L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21.

Part: DOUBLER — CORROSION (FS 180-335)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER HAD HEAVY CORROSION AT LONGERON 31L FS 180 TO 335. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CORROSION (FS 215-260)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AND CRACK AT LONGERON 36 RT SIDE AT FS 215 AND FS 260. REPLACED LONGERON SECTION PER SRM 51-1-21.

Part: FRAME — CORROSION (FS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1680 BELTFRAME HAS HEAVY CORROSION AND CRACKED AT LONGERON 21L. REPAIRED FRAME PER SRM 53-2-0 FIG 2.

Part: LONGERON — CORROSION (FS 216-246)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 35L O/B HAS CORROSION DAMAGE AT FS 216 TO 246. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: DOUBLER — CORROSION (FS 220)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 'A' CSD FWD DOUBLER HAS CORROSION AT FS 220 TO 260 LONGERONS 30R TO 35L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21.

Part: DOUBLER — CORROSION (FS 1540-1655)

WHILE IN FOR "C" CHECK MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER, FS 1540-1655, LONGERONS 29R-31R. REPLACED INNER DOUBLER PER SRM 51-1-21.

Part: FITTING — CORROSION (FS 140)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD AND AFT SIDES OF FITTING TOP SIDE HAS HEAVY CORROSION ON LONGERON 21R FS 140. REPLACED FITTING PER SRM 51-1-20D.

Part: FRAME — CORROSION (FS 140)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 140 LONGERON 36 HAD HEAVY CORROSION ON BELTFRAME. REPLACED FRAME PER SRM 53-2-0.

Part: FRAME — CORROSION (FS 180)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE BEYOND LIMITS AT BELTFRAME FS 180 BETWEEN LONGERONS 35R AND 36. REPAIRED FRAME PER SRM 53-2-0, FIG 2.

Part: DOUBLER — CORROSION (FS 160-170)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 160 TO 170, LONGERON 31R HAD HEAVY CORROSION ON FINGER DOUBLER. REPLACED PER SRM 51-1-20D AND 51-1-21.

Part: AILERON — CORROSION (RT INBD WING)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B AILERON HAS INTERNAL CORROSION. REPLACED AILERON ASSY PER MM 27-11-01.

Part: FRAME — CORRODED (FS 52)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FRAME BELOW LONGERON 21L, FS 52.

Part: FITTING — CORROSION (FS 1440)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON LONGERONS 21L FITTING FS 1440. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1580 LONGERON 21L HAS HEAVY CORROSION AFT SIDE. REPAIRED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 280)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 280 LONGERON 21L FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 881)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED ATTACH ANGLE ON BOTTOM SIDE OF FITTING HAS .75 INCH CRACK AT STA 881. REPLACED ANGLE PER SRM 51-1-20D.

Part: SKIN — CRACKED (FS 1660)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACK ON SKIN AND LONGERON UPPER AFT CORNER OF RT SERVICE DOOR CUTOUT. REPAIRED PER UPS EO DC8-53-1612.

Part: ANGLE — CRACKED (NR 1 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 PYLON I/B DRAG ANGLE CRACKED BEYOND STOP DRILL. REPAIRED ANGLE PER SRM ADDENDUM DC8-5740-0716.

Part: VANE ASSY — DELAMINATED (NR 3 TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT NR 3 WING FLAP VANE DELAMINATED. REPLACED FLAP VANE ASSY PER MM 27-50-00.

Part: SKIN — CORROSION (FS 70-190)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE BELLY SKIN FS 70 TO 190. REPLACED BELLY SKIN SECTION PER DAC DRAWING NR 5779925.

Part: SKIN — CORROSION (FS 190-450)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BULGES ON FUSELAGE BELLY SKIN FS 190 TO 450. REPLACED BELLY SKIN PANEL PER DRAWING NR 5755271.

Part: LATCH CABLE — FRAYED (PAX DOOR SLIDE)

WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED FORWARD ENTRAHCE DOOR, EVACUATION SLIDE GIRT BAR LATCH ASSY, CABLE FRAYED. REPLACED ASSY. REP MM 25-61-01.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT NR 3 SPOILER PNL DELAMINATED AT LWR SIDE. REPLACED SPOILER PNL PER MM 27-61-01.

Part: CONTL VLV — FAILED (LT MLG BRAKES)

WHILE ON TAXI OUT IN DFW, LT BRAKES FAILED DUE TO BROKEN ARM AT BRAKE CONTROL VALVE. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 1 ENGINE)

WHILE IN CRUISE, NR 1 ENG FIRE DETECTOR SHORT CIRCUIT LIGHT CAME ON MOMENTARILY. ALL OTHER ENGINE INSTRUMENTS NORMAL, OPS CHECKED, FIRE WARNING SYSTEM IAW ED DC8-2610-1268. GROUND RAN AIRCRAFT, SYS CHECKED GOOD. OK FOR SERVICE.

Part: FITTINGS — CRACKED (RT FUSELAGE)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACKED RT FITTINGS, 3 ON TOP OF LONG 24, FS 879, 940, 960. REPLACED IAW EO DC8-5310-7191-A.

Part: SKIN — CRACKED (NLG WW)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACK IN FUSELAGE SKIN AFT LT CORNER ON NOSE LANDING GEAR WHEEL WELL CUTOUT. REPAIRED IAW EO DC8-5330-4154-B.

Part: FITTING — CRACKED (FS 970)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACKED RT LONGERON T-FITTING AT FS 970. REPLACED IAW SRM 51-1-20D, 51-3-0.

Part: TRAP FITTING — CRACKED (LT FUSELAGE)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACK IN LT TRAPEZOIDAL FITTING ON TOP OF LONGERON 24 AT FS 879, 920, 940, 960. REPLACED IAW SRM 51-1-20D, 51-2-0.

Part: FITTING — CORROSION (FS 960)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CORROSION ON LONGERON 24L LOWER SUPPORT FITTING AT BOLT HOLES AT FS 960. REPLACED IAW SRM 51-1-20D.

Part: FRAME — CORRODED (FS 870)

WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CORROSION ON LT WHEEL WELL MAIN GEAR CHANNEL FRAME AT FS 870 LBL 60. REPAIRED IAW SRM 53-2-0.

Part: LONGERON — CRACKED (FUSELAGE)

WHILE ON GROUND, MAINTENANCE FOUND CRACK ON LONGERON 24. REPAIRED IAW DC8-5310-6259.

Part: PROX SENSOR — INOP (LT MLG)

PILOT REPORTED DURING UPLATCH CHECK GEAR NOT LATCHED LIGHT ILLUMINATED, CYCLED GEAR, 2ND UPLATCH CHECK SAME RESULT, CYCLED GEAR 3RD TIME, GEAR UPLATCH CHECK NOSE GEAR CAME DOWN. FOURTH TIME, GEAR UPLATCH CHECK GEAR NOT LATCHED LIGHT AND DOORS LATCHED LIGHT ILLUMINATED, CYCLED GEAR 5TH TIME, UPLATCH CHECK GEAR NOT LATCHED LIGHT ILLUMINATED NOSE GEAR DID NOT FALL OUT. REPLACED LT MLG GEAR PROXIMITY SENSOR SWITCH PER DC8 MM 32-60-00. PERFORMED GEAR SWING, OPS CK NORMAL (UPLOCK PROXIMITY SENSOR).

Part: WARNING LIGHT — MALFUNCTION (LANDING GEAR)

WHILE A/C WAS IN COLOGNE, MAINTENANCE REPORTED UPLATCH CHECK DOOR NOT LATCHED LIGHT ILLUMINATED AND NOSE GEAR EXTENDED.