N797UP

Part: WEB — CRACKED (CARGO DOOR)

PIT NR 31 CARGO DOOR WEB CRACKED. AT STA 40, APPROX. 12 INCHES BELOW MAIN DECK FLOOR. REMOVED DAMAGED SECTION OF WEB. T G 35574 10-6-02 FABRICATED & INSTALLED REPLACEMENT SECTION OF WEB PER DC-8 SRM 53-2-0

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE:N/A PIT 31 DOOR AFT TOP CORNER OUTER SKIN HAS 4 INCH CRACK THROUGH 3 RIVETS. REMOVED DAMAGED REPAIRED IAW 52-2-0 FIG 2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CKS OK P/N ON-OFF 5708458-503, S/N OFF FT L 158 ON 2085.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT HORIZONTAL STAB. L/E. SKIN IS CRACKED AND DENTED BEYOND LIMITS XFS 150. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 140 FLOORBEAM IS CORRODED BEYOND LIMITS BETWEEN RBL. 50 AND RBL. 60. REPAIRED FLOORBEAM I.A.W. 8110-3 APPROVED DH SK 779-363

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 327. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: DOUBLER — CRACKED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE: C2,3. RIGHT WING OB L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-21

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 660 SHEAR TIE CLIP IS CRACKED BETWEEN LONG. 26L-27L REPAIRED SHEARTIE I.A.W. SRM. 53-2-0 FIG. 2A

Part: FITTING — CORRODED (LOWER CARGO) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA 320 BATHTUB FITTING IS CRACKED BETWEEN LONG. 29L-30L REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM.51-1-20D

Part: FITTING — CRACKED (CABIN) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 100 UPPER FRAME TO CUSP FITTING IS CRACKED AND CORRODED BEYOND LIMITS AT LONG. 21R REMOVED AND REPLACED FITTING I.A.W. DWG. 4597643,AND SRM. 51-1-20D

Part: FITTING — CORRODED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 29L-30L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM. 51-1-20D

Part: ANGLE — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. ATTACH ANGLE IS CRACKED AT XW454. REMOVED, FABRICATED, AND REPLACED ANGLE I.A.W. DWG. 9753297,AND SRM. 51-1-20D,51-1-21

Part: FITTING — CORRODED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 28L-29L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM.51-1-20D

Part: FITTING — CRACKED (LOWER CARGO) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 450 LONG. 36 SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D

Part: STRAP — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 465 STRAP IN MIDDLE OF LONG. 33R IS CRACKED REMOVED,FABRICATED,AND REPLACED STRAP I.A.W. DWG. 3750349,AND SRM. 51-1-20D,51-1-21

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 372.750. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 FUSELAGE EXTERNAL SKIN IS CORRODED BEYOND LIMITS AT STA. 857 BETWEEN LONGERON 16R-17R. REPAIRED SKIN I.A.W. SRM. 53-2-0 FIG. 22A

Part: DOUBLER — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. INTERNAL DOUBLER IS CRACKED AT XW 257.5. REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-20D,51-1-21

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 366.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 347.75. REPAIRED RIB I.A.W. SRM. 57-2-0 ,FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 722.5. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 920 LONG. 18R EXTERNAL SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-908

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 442.185. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 448.581. REPAIRED RIB I.A.W. SRM.57-2-0 FIG.2

Part: FITTING — CORRODED (A/C BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 70 LOWER CUSP TO FRAME FITTING IS CORRODED BEYOND LIMITS AT LONGERON 21R. REMOVED AND REPLACED FITTING I.A.W. DWG. 3610130,AND SRM. 51-1-21, 51-3-0

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XW 466.651. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: LONGERON — CRACKED (LT MLG WW) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 879-902,LONG. 24L IS CRACKED. REPAIRED LONG. I.A.W. SRM. 53-2-2 FIG. 5

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 390 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473-1N,AND SRM. 51-1-20D

Part: RIB — CRACKED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS. 360.250. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 772.5. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE: C2,3 STA. 1580 FLOORBEAM IS CORRODED BEYOND LIMITS AT RBL. 48. REPAIRED FLOORBEAM I.A.W. 8110-3 APPROVED DH SK 797-605

Part: SKIN — CORRODED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RIGHT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 37 & 38

Part: SKIN — CORRODED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RT AUX TANK UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 20-26.25 REPAIRED SKIN I.A.W. SRM. 57-2-0 FIG. 37 & 38,AND DHM. ENGINEERING RESPONSE.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1766 LONG. 17L IS CRACKED AND CORRODED REPAIRED LONGERON I.A.W. SRM.53-2-2 FIG. 10

Part: SKIN — CORRODED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RT. WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS XFS 603.75 AT IB SLING ATTACH POINT. REPAIRED SKIN I.A.W. SRM. 57-3-0 FIG. 18,AND E.O. DC8-5720-7767-A

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RT. H-STAB. L/E. SKIN IB. SIDE OF STA. XFS 178 IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4

Part: PAN — CRACKED (CARGO DOOR) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 C-PIT DOOR PAN IS CRACKED AT STA. 1180 AT LONG. 32R APPROX. REPAIRED PAN I.A.W. SRM. 52-2-0 FIG. 4

Part: SKIN — CORRODED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 341 TO XOLDI 6.225. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-486

Part: SKIN — CORRODED (LEFT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 760. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 38

Part: SKIN — CRACKED (LEFT WING LE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE: C1, 3, LEFT WING CENTER L/E SKIN IS CRACKED AT XW 257.5 REPAIRED SKIN I.A.W. E.O. DC8-5720-7767-A

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1150 BETWEEN LONG. 35R-34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755843,AND SRM. 53-2-0 FIG. 2D

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LT. KEEL BEAM WEB IS CRACKED AT STA. 879. REPAIRED WEB I.A.W. SRM. 53-2-0 FIG. 23

Part: FITTING — CORRODED (MAIN CABIN) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 879 RBL. 63 CUSP TO FRAME FITTING BELOW FLOOR PANEL IS CORRODED BEYOND LIMITS REMOVED AND REPLACED FITTING I.A.W. DWG. 5643483,AND SRM. 51-1-20D, 51-1-21

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1240, LONG. 35L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3758495,AND SRM. 51-1-20D

Part: SKIN — CORRODED (LT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 LEFT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193, 8-10 INCHES AFT OF L/E. REPAIRED SKIN I.A.W. SRM. 57-2-0 FIG. 2A

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1180 BATHTUB BETWEEN LONG. 27L-28L IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755842,AND SRM. 53-2-0 FIG. 2D

Part: FITTING — CORRODED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1160 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 36 TO 35R. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755845,AND SRM. 53-2-0 FIG. 2D

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1180 LONG. 34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755841,AND SRM. 53-2-0 FIG. 2D

Part: LONGERON — CRACKED (AFT CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 1260-1280 LONG. 35L IS CRACKED. REPAIRED LONGERON I.A.W. 8110-3 APPROVED DH SK 797-370

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 280 BANANA FITTING IS CRACKED AT LONG. 33R REMOVED AND REPLACED FITTING I.A.W. DWG.3755827,AND SRM. 51-1-20D

Part: FITTING — CRACKED (CARGO BAY) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 STA. 280 LOWER FLOORBEAM TO CUSP FITTING IS CRACKED AT LONG. 21R REMOVED AND REPLACED FITTING I.A.W. DWG. 9754022,AND SRM. 51-1-20D,& 51-1-21

Part: DOUBLER — CRACKED (RT WING) · airframe 65,958 hrs · 24,431 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 297.5 REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-21,51-1-20D

Part: SKIN — CRACKED (BS 93-99)

INSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASE AND TORN STA -99 TO-93, L31R TO L28R. REMOVED DAMAGED SECTION OF SKIN AND DAMAGED FRAME, FABRICATED NEW SKIN SECTION AND DOUBLERS IAW REO -06765, LOCATED NEW FRAME SKIN SECTION AND DOUBLERS, DRILLED UP IAW DC8 SRM 51-24. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (BS 80-85)

INSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASED AND TORN STA -85 TO -80 L31L TO 28L CRACKED APRROX 15.0. REMOVED DAMAGE SECTION OF SKIN, FABBED DOUBLER, FILLER AND SPLICE DOUBLER IAW REO-06778, INSTALLED DOUBLER, FILLER AND SPLICE DOUBLER IAW DC8 SRM 51-1-20D, 51-1-21 & 51-3-0. FILLET SEALED IAW DC8 SRM 51-1-15.

Part: DOUBLER — CORRODED (BS 8-70)

INSPECTION TYPE:SV STA 8 TO 70 FINGER DOUBLER RT SIDE HAS CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51-1-21, 53-3-1.

Part: FRAME — CRACKED (BS 117)

INSPECTION TYPE:S/V, STA-117 FRAME CRACKED AT BOTTOM FWD OF NOSE GEAR. FABBED AND INSTALLED REPAIR IAW REA-O6756 DYE PENNED REPAIR PARTS IAW ASTM-E-7417-95A. NO CRACKS NOTED IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (BS 105)

INSPECTION TYPE:S/V STA-105 FRAME CRACKED BOTTOM FWD OF NOSE. FAB REPAIR ANGLES AND FILLERS IAW REO 06767 DYE PENNED REPAIR PARTS IAW MIL STD 15378, NO CRACKS NOTED ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC 8 51-1-20D.

Part: FRAME — DAMAGED (BS 80)

INSPECTION TYPE:SV, FUSELAGE FRAME AT STA 80 LT O/B NOSE WHEEL WELL IS DAMAGED. REC'D SERVICEABLE FRAME SECTION FROM AIRCRAFT (S/N 46038), HEAT TREATED REPAIRS DOUBLERS 7075-0--063 TO 7075-T6 IAW TPS 1003 REV A. FABBED DOUBLERS IAW REO 06791. DYE PENT REPAIR DOUBLERS IAW MIL STD .153 7B. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D & 51-1-11.

Part: STRUCTURE — DAMAGED (NOSE)

INSPECTION TYPE:N/A, FUSELAGE NOSE SECTION, INTERM, REPAIR EO DC8 5300-11498A TO INCLUDE REMOVAL OF NOSE LANDING GEAR DOORS, BOTH PAC'S INOP (REF DEFERRAL M- 177745) RT PNEUMATIC PRESSURE INDICATION INOP (REF DEFERRAL M-177744 ) REF INCIDENT NUMBER RS99-288. COMPLIED WITH REPAIRS REF TIMCO REO NR'S 06734, 06743, 06756, 06765, 06767 REV B, 06776, 06778, 06791, 06797 REV B, 06800, 06802 REV A, 0 6820.

Part: COWL — DAMAGED (NR 3 ENGINE)

INSPECTION TYPE:N/A, NR 3 ENG FAN COWL (O/B) DAMAGED WHEN NOSE GEAR COLLAPSED, SEE LOG PAGE 208929 ITEMS 1 AND 2. OPENED COWL TRANSFERRED TO UPS NON-ROUTINE 544690.

Part: FRAME — DAMAGED (BS 87)

INSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 LEFT O/B NWW. FABBED AND INSTALLED FRAME AND REPAIR PARTS (SPLICES) IAW REO 06776 & DC8 SRM 51-1-20D.

Part: FRAME — DAMAGED (BS 87)

INSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 RT O/B OF NWW. REC'D SERVICEABLE FRAME SECTION FROM A/C (S/N 46038). HEAT TREATED REPAIR PARTS 7075-0 TO 7075 T6.063 IAW TPS-1003 REV A. INSTALLED SERVICEABLE FRAME SECTION IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR SPLICES IAW DC8 SRM 51-1-20D. FABBED AND INSTALLED NEW (P/N 5613861-68) CHANNEL IAW DWG 5613861 & DC8 SRM 51-1-20D.

Part: GIRT BAR — FAILED (CABIN)

INSPECTION TYPE:N/A, ESCAPE SLIDE GIRT BAR RETAINER FAILED UPON EGRESS OF A/C, SLIDE SEPARATED FROM A/C. STILL I/W ON LOG PAGE 208929/2. FOLLOW UP ACTION SCHEDULED FOR REMAINDER OF DC-8 FLEET. *S/D* INSTALLED HARDWARE IAW EO DC-8-2560-11700, OPS CK NORMAL WITH GIRT BAR.

Part: LANDING GEAR — COLLAPSED (NLG)

INSPECTION TYPE:N/A, AFTER LANDING AND COMING TO A STOP ON RUNWAY 32R, THE NOSE GEAR COLLAPSED INTO THE WHEEL WELL. *S/D* ALL REQUIRED EO'S IE DC8-5300-11498A HAVE BEEN C/W BY TIMCO. PER FERRY FLIGHT PERMIT NR 9086 ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPLISHED AND AIRCRAFT IS IN SAFE OPERATING CONDITION FOR FERRY FLIGHT. ISSUED DMI.

Part: BULB — FAILED (RT MLG)

INSPECTION TYPE:N/A, ON FINAL APPROACH LOWERED LANDING GEAR, RT MAIN GREEN LIGHT DID NOT ILLUMINATE. CYCLED GEAR, SAME INDICATION. ALSO, RED NOT LATCHED LIGHTS DID NOT ILLUMINATE. AFTER MISSED APPROACH RAISED GEAR, REPLACED BULBS, LOWERED GEAR, RT MAIN ILLUMINATED AS NORMAL. SYSTEM OPS CHECKED NORMAL.

Part: WIRE — FAILED (CABIN)

COCKPIT DOME LIGHT DOSE NOT ILLUMINATE ON PREFLIGHT CHECK OF EMERGENCY LIGHTS DETERMINED 3 EACH PWR WIRES ARE INOP AT JUNCTION. REF WDM 33-50-01 REPAIRED WIRES, OPS CHECK GOOD.

Part: FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:C1 RT FWD TYPE 1 DOOR LOWER AFT FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3888406 AND SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE:C1 WING STA XRS74.0, THE STR 51 END FITTING IS CRACKED (LT WING). REMOVED AND REPLACED FWD AND AFT END FITTINGS IAW DWG 3704841 AND SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE:C1 RT WING, THE STRINGER 51 END FITTING AT STA XRS74.00 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1030)

INSPECTION TYPE:C1 STA 1030 AT STR 19L, THE EXTERNAL SKIN HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK797-045.

Part: SKIN — CORRODED (WS 341)

INSPECTION TYPE-C1, RT WING L/E SKIN HAS HEAVY CORROSION AT STA XFS 341. REPAIRED AREA IAW SRM 57-3-1.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE-C1, RT WING L/E RIBS AT THE FOLLOWING STA'S ARE CRACKED: FS 467.323, FS 442.185, XOLDI6.225, FS 366.500, FS 360.250 AND FS 354. STOP DRILLED CRACK'S AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (BS 270)

INSPECTION TYPE-C1, STA 270 AT LONG 30R, THE SUPPORT FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SUPPORT FITTING IAW DWG 3754916 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 1400)

INSPECTION TYPE:C1, SEAT TRACK AT STA 1400, LBL58 HAS HEAVY CORROSION. SPLICED TRACK FROM STA 1370-1430 BLB58 IAW SRM 53-2-3.

Part: FRAME — CORRODED (BS 1380)

INSPECTION TYPE:C1 STA 1380 AT STR 19L, THE FRAME HAS HEAVY CORROSION. REPAIRED FRAME IAW DH SK797-464.

Part: FRAME — CORRODED (BS 1100)

INSPECTION TYPE:C1 STA 1100 BTWN STR 10L-11L, THE FRAME IS CORRODED OUT OF LIMITS. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: RIB — CRACKED (WS 634)

INSPECTION TYPE:C1 LEFT WING L/E RIB AT STA XFS 634.000 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 640)

INSPECTION TYPE:C1 LEFT WING L/E AT STA XFS640.00, THE L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (BS 960)

INSPECTION TYPE:C1 RT WHEEL WELL AT STA 960 AND LONGERON 24R, THE FITTING ABOVE THE LONGERON IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 3647117 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE-C1, STA 1220 AT STR 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C1 STA 55 FRAME AT STR 24L IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE-C1, STA 1180 AT STR 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1020-1040)

INSPECTION TYPE-C1, STA 1020 TO 1040 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 75)

INSPECTION TYPE:C1 STA 75 AT STR 31R, THE STR END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4614397 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 390)

INSPECTION TYPE-C1, STA 390 AT STR 31L, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 260)

INSPECTION TYPE-C1, STA 260, LONGERON 35L IS CRACKED ON TOP. REPAIRED AREA BY SPLICING IAW SRM 53-2-2 FIG 10.

Part: SHEAR TIE — CRACKED (BS 1420)

INSPECTION TYPE:C1 STA 1420 AT STR 21L-25L, THE SHEAR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING (SHEAR TIE) IAW DWG 5641015 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1040-1060)

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

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-C1, STA 680 AT LONG 11L, THE LONGERON END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625 AND SRM 51-1-20D.

Part: SKIN — CRACKED (RUDDER)

INSPECTION TYPE:C1 RUDDER SKIN IS CRACKED IN 2 PLACES LEFT SIDE JUST ABOVE THE TAB. REMOVED AND REPLACED RUDDER ASSY IAW MM 27-21-01.

Part: SKIN — CORRODED (RT HORIZ STAB)

INSPECTION TYPE-C1, RT HORIZ STAB L/E SKIN AT MID SPAN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED AREA IAW SRM 55-2-1 FIG 4.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C1 STA 742 AT STR 13L, THE TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING)

INSPECTION TYPE-C1, LT WING CENTER L/E HAS UPPER RIB THAT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (BS 710)

INSPECTION TYPE-C1, STA 710 AT STR 18R, THE TIE FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4751640-1.

Part: DOUBLER — CRACKED (RT WING)

INSPECTION TYPE:C1, RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED FWD OF ACCESS PANEL 524B. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-21.

Part: SKIN — CRACKED (WS 431.798)

INSPECTION TYPE-C1, RT WING LOWER SKIN AT STA FS 431.798, 5 INCHES FWD OF THE FRONT SPAR IS CRACKED AT 2 FASTENERS. REPAIRED AREA IAW DC8-5720-4087.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-C1, WING BOX FLOORBEAM SUPPORT ANGLE IS CRACKED AT STA 680, LBL 25. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 902)

INSPECTION TYPE-C1, STA 902 AT RBL 48, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM STA 889 TO 1050 RBL 48 IAW SRM 53-2-3.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE-C1, RT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED AT THE I/B UPPER SIDE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 580-600)

INSPECTION TYPE-C1, STA 580 TO 600 AT RBL 60, THE SEAT TRACK HAD HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM STA 550 TO 650 RBL 60 IAW SRM 53-2-3 FIG 8A.

Part: AUX TANK — CORRODED (LT WING)

INSPECTION TYPE:C1 LEFT WING AUX TANK AT STA XFS 1.250 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 291.5)

INSPECTION TYPE-C1 LT WING L/E UPPER RIB IS CRACKED AT FS 291.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-C1, WING BOX FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 680 AT LBL 48. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 250.089)

INSPECTION TYPE:C1, RT WING L/E RIB AT STA XS 250.089 IS CRACKED. REPAIRED AREA IAW SRM 57-3-0.

Part: SEAT TRACK — CORRODED (BS 1140)

INSPECTION TYPE-C1, MAIN CABIN AT STA 1140 AND RBL 48, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 1050 TO 1190 AT RBL 48 IAW SRM 53-2-3.

Part: SKIN — CRACKED (WS 16.225)

INSPECTION TYPE-C1, LT WING L/E LOWER SKIN AT STA, XOLDI6.225 IS CRACKED. REPAIRED AREA IAW DC8-5720-7767A.

Part: RIB — CRACKED (WS 250.089)

INSPECTION TYPE:C1 LEFT WING L/E RIB AT STA XS250.089 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 590)

INSPECTION TYPE-C1, MAIN CABIN AT STA 590, LBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED TRACK FROM STA 570 TO 690 AT LBL 60 IAW SRM 53-7-1.

Part: SKIN — CRACKED (WS 257)

INSPECTION TYPE:C1 LEFT WING L/E SKIN AT STA XW257.000 IS CRACKED AT THE I/B END. REPAIRED AREA IAW DC8-5720-7767.

Part: SKIN — CRACKED (WS 533.375)

INSPECTION TYPE:C1, NR 1 STUB LWR SKIN IS CRACKED AT STA XFS533.375 AND XOLDO57.500. REPAIRED AREA IAW SRM 57-2-1A.

Part: RIB — CRACKED (WS 227.335)

INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT STA FS 227.335. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C1 STA 680 AT RBL 24, THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 440-460)

INSPECTION TYPE:C1 STA 440-460 STR 14L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 759-766)

INSPECTION TYPE-C1 MAIN CABIN AT STA 759 TO 766 RBL 60, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 749 TO 970 AT RBL 60 IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 270)

INSPECTION TYPE:C1 STA 270 AT STR 30R-31R, THE DOOR JAMB FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827-501 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 660)

INSPECTION TYPE:C1 LEFT WING L/E AT STA XFS 660.0, THE UPPER L/E RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 766.25)

INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT FS 766.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C1, LT WING L/E LWR RIB AT STA FS 778.750 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE-C1, LT WING L/E AT STA FS 816.250, THE LWR RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (WS 560)

INSPECTION TYPE:C1 LEFT L/E OUTBOARD OF THE NR 1 PYLON HAS MODERATE CORROSION ON THE LWR SKIN AT STA XFS560. REPAIRED AREA IAW EO DC8-5720-7767-A.

Part: SKIN — CRACKED (WS 257)

INSPECTION TYPE-C1, RT WING L/E SKIN AT FS 257 IS CRACKED ON TOP. REPAIRED AREA IAW SRM 57-2-1.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT STA FS 816.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 660)

INSPECTION TYPE:C1 LEFT WING L/E RIB (LWR) IS CRACKED AT STA XFS660.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 249 & 250)

INSPECTION TYPE-C1, RT WING L/E UPPER SKIN IS CRACKED AT STA XS 249 AND 250 AT THE SPAR. STOP DRILLED CRACK AND REPAIRED IAW DC8-5720-7767.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE:C1 LEFT WING L/E RIB IS CRACKED AT STA XFS622.500, (LWR RIB). STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 660)

INSPECTION TYPE:C1 LEFT WING L/E LWR RIB IS CRACKED AT STA XFS 660.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (CARGO DOORWAY)

NR 4 PIT DOOR FRAME SKIN CRACKED IN UPPER AFT CORNER EO DC8-5330-4067A ISSUED. INSTALLED TEMP REPAIR TO DOOR JAM CORNER PER EO DC-8 5330-4067.

Part: PANEL — CORROSION (WS 114-137.5)

INSPECTION TYPE-C, FOUND CORROSION ON LEFT WING LEADING EDGE ACCESS PANEL 520E, XFS 114-137.5. REMOVED AND REPLACED ACCESS PANEL 520E IAW DC8 SRM 51-3-0.

Part: SKIN — CORRODED (BS 1890)

INSPECTION TYPE-C, FOUND CORROSION ON BOTTOM OF FUSELAGE SKIN FWD OF DOOR G2 AT STA 1890. REMOVED CORROSION, CUT OUT CORRODED AREA, FABRICATED FILLER AND REPAIR DOUBLER, DRILLED TREATED PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 FIG 1, 51-1-8, 51-1-21.

Part: SKIN — DAMAGED (WS 493-503)

INSPECTION TYPE-C, FOUND FASTENER ROW LOOSE AND PULLED THROUGH SKIN AT RT WING LEADING EDGE ABOVE NR 4 PYLON APPROX XS 493 TO 503. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW REA 97762 AND DACO ROD SKETCH 97-10-29-003.

Part: SKIN — CORROSION (BS 680)

INSPECTION TYPE-C, FOUND CORROSION ON FUSELAGE SKIN AROUND FASTENER IN LONGERON 35 LEFT AT Y=680. REMOVED CORROSION .003 BEYOND DC8 SRM LIMIT. REMOVAL FOUND ACCEPTABLE PER (A) BCAG FAX MISC-A099/RRR, ATA:8-53-02-03 (B) AEROCORP MACON INC FAX FILE 102197-2/RS (C) DC8 SRM 51-1-08, PARA 6F AND 7E.

Part: CLIP — CORRODED (BS 8-13)

INSPECTION TYPE-C, FOUND CORROSION ON SUPPORT CLIP ON PRESS BULKHEAD STA 8 TO 13, X 38 LT, -Z37. FABRICATED, DRILLED, TREATED AND INSTALLED NEW CLIP IAW DC8 SRM 53-2-0, PAGE 1, PAR 3, 51-1-20D AND 51-1-8.

Part: LID — CRACKED (NR 2 TANK)

INSPECTION TYPE-C, FOUND NR 2 MAIN TANK ACCESS LID 506C HAS CORROSION CRACK AT ATTACH HOLE STA XRS 5. REMOVED CORROSION/CRACK, FABRICATED REPAIR DOUBLER, DRILLED,TRATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1 FIG 43, 51-1-8, 51-1-21.

Part: SKIN — CRACKED (LT WING LE)

INSPECTION TYPE-C, FOUND CRACK AT SCREW HOLE ON UPPER SURFACE OF LEFT WING LEADING EDGE AT XOLD 6.2. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLER, DRILLED, TREATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D AND 57-2-0 PAGE 10A.

Part: SKIN — CRACKED (LT WING LE)

INSPECTION TYPE-C, FOUND 2 INCH CRACK AT ATTACH HOLES ON UPPER SURFACE OF LEFT WING CENTER LEADING EDGE AT XFS 285. FABRICATED REPAIR DOUBLER, DRILLED, TREATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2A SHEET 1, 51-1-21, 51-3-0 AND 51-1-8.

Part: AIR DISTR — ODOR (COCKPIT)

INSPECTION TYPE-N/A, NOTICED STRONG FUEL SMELL IN COCKPIT DURING DESCENT. INSPECTED WINGS AND PYLONS FOR FUEL LEAKS, NONE NOTED. RAN ALL ENGINES AND BOTH PACKS, NO FUEL ODOR NOTED IN COCKPIT OR CARGO BAY AREA.

Part: CONTROL VALVE — OUT OF ADJUST (NLG STEERING)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BLOCK TURN BACK RUDDER PEDAL STEERING STIFF TO THE RIGHT. ADJUSTED NOSE WHEEL STEERING CNTRL VALVE. OPS CHECKED GOOD PER MM 32-51-01.

Part: LONGERON — CORROSION (FS 683)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31R O/B SIDE HEAVY CORROSION AT FS 683. REPAIRED PER UPS EO DC8-53-1602.

Part: DOUBLER — CORRODED (FS 683-780)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON DOUBLER AROUND FASTENERS AT STA 683 TO 780 LBL 10 RBL 10. REPAIRED PER UPS EO.

Part: DOUBLER — CORROSION (FS 1600-1650)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER DOUBLER, FS 1600-1650, LONGERONS 21R-31R. REPLACED DOUBLER SECTION PER SRM 51-1-21.

Part: DOUBLER — CRACKED (FS 1050)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE FINGER DOUBLER HAS HEAVY CORROSION AND CRACKS ON LONGERONS 31R AND 31L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21.

Part: SPLICE STRAP — CORROSION (FS 1050)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE STRAP DOUBLER HAS HEAVY CORROSION ON LONGERONS 31R AND 31L. REPLACED STRAP PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 683)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON KEEL TEE FITTING FS 683 LONG 36. REPLACED PER UPS EO DC8-53-1598.

Part: FITTING — CORRODED (FS 1190)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FITTING, FS 1190 LONGERONS 32 TO 33R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1180)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED T-FITTING HEAVY CORROSION AT FS 1180 LONG 34R. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CORRODED (LT HORIZ STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB L/E SKIN AT ATTACHING SCREW HOLES HAD HEAVY CORROSION AT STA XFS 125 AND 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1.

Part: LONGERON — CRACKED (FS 1260)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 21L IS CRACKED FS 1260. REPAIRED LONGERON PER SRM 53-2-5.

Part: FITTING — CORRODED (FS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, FWD SIDE OF FS 1680 LONG 31R. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B AILERON SKIN AND LOWER DOUBLER CRACKED AT THE I/B CLOSURE RIB. REPAIRED PER UPS EO DC8-57-0652.

Part: FITTING — CORRODED (FS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, AFT SIDE OF FS 1680 LONG 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1290)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31L SPLICE FITTING CRACKS AT FS 1290. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1270)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 34L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1270)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 35L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1228)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON FITTING FS 1228 LONG 27 TO 28L. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1394)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CORNER FITTING FS 1394 INSIDE LONG FWD TORQUE BOX HOLE. REPLACED FITTING PER SRM 51-1-20D.

Part: SPLICE — CORRODED (FS 1540-1520)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE AT SPLICE LONG 31L BETWEEN FS 1520 TO 1540. REPLACED SPLICE PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1160)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION LONGERON FITTING. REPLACED FITTING PER SRM 53-2-0 AND 51-1-20D.

Part: LONGERON — CORRODED (FS 1380-1400)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 34L FS 1380 TO 1400 FS 1520 TO 540. REPLACED LONGERON SECTION PER SRM 51-2-2.

Part: BOLTS — CORRODED (FS 145-255)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01 (T/C 420269).

Part: DOUBLER — CORROSION (FS 1227-1264)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER BETWEEN LONG 31L TO 33R FS 1227 TO 1264. REPLACED PER EO DC8-53-1599.

Part: FRAME — CORRODED (FS 1360)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD SIDE OF FRAME FS 1360 ABOVE LONG 36. REPAIRED FRAME PER SRM 53-2-0, FIG 2.

Part: ANGLE — CORROSION (FS 702)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON LOWER ATTACH ANGLE UNDER MAIN CABIN SEAT TRACK NR 4, FS 702, BL ZERO. SPLICED ANGLE PER SRM 53-2-0.

Part: SEAT TRACK — CORROSION (FS 759-822)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON MAIN CABIN SEAT TRACK NR 5 AROUND FLOOR BEAM ATTACH HOLES FS 759-822, RBL 22. REPLACED TRACK SECTION PER SRM 53-2-3.

Part: SKIN — CORROSION (FS 1600-1650)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER SKIN, STA 1600-1680, LONGERONS 21R-31R. REPLACED SECTION PER SRM 51-1-21.

Part: ANGLE — CORRODED (FS 781-759)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LOWER SUPPORT ANGLE UNDER SEAT TRACK NR 7 FS 781 TO 759. REPAIRED PER UPS EO.

Part: DOUBLER — CORRODED (FS 980)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD RADIUS DOUBLER, FS 980 LONG 36. REPLACED RADIUS DOUBLER PER SRM 51-3-0.

Part: FLOOR BEAM — CRACKED (FS 920)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AND CRACK AT FWD BEAM, FS 920 LBL 65 AFT SIDE. REPAIRED PER UPS EO.

Part: SEAT TRACK — CORROSION (FS 759-781)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SEAT TRACK NR 1 HAS CORROSION DAMAGE AND CRACKS AT FS 759-781, LBL 55. REPLACED TRACK SECTION PER SRM 53-2-3.

Part: FRAME — CORRODED (FS 160)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME FS 160 LONG 36 TO 35R. REPAIRED PER SRM 53-2-0 FIG 2 AND SRM 51-1-20D.

Part: ATTACH ANGLE — CORRODED (FS 360)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY INTERGRANULAR CORROSION ON FRAME ANGLE FS 360 LONG 27L. REPAIRED PER SRM SRM 51-1-20D.

Part: SPAR — CRACKED (RT WING RT)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR AT WW IS CRACKED AT LOWER HORIZONTAL CAP RBL 30 FS 857. REPAIRED PER UPS EO DC8-5710-8088A.

Part: ANGLE — CORRODED (FS 100)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ATTACH ANGLE AT FS 100 LONG 31R. REPLACED ANGLE PER SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 50-67)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION DAMAGE ON FINGER STR DOUBLER FS 50 TO 67 LONG 21L. REPLACED FINGER DOUBLER PER SRM 51-1-21.

Part: FITTING — CORROSION (FS 980)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 980 FWD OF FRAME FITTING LONGERON 20R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (LT HORIZ STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB FITTING HAD CORROSION DAMAGE AT NR 4 STR STA XFS 135 BOTTOM INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 920)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 920 FITTING AFT OF LONG 24R. REPLACED FITTING PER SRM 53-2-0.

Part: SKIN — CORROSION (WS 700)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING T/E, STA XW700 TO STA XW 710 HAS CORROSION BULGES ON SKIN. REPAIRED SKIN IAW DOUG DRAWING NR 5644654.

Part: FITTING — CORRODED (FS 145)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD JAMB HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0.

Part: SKIN — CORROSION (VERT STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STABILIZER T/E, BOTH SIDES HAVE CORROSION BETWEEN NR 4 RUDDER SUPPORT FITTING. REPLACED SKIN PANEL BY REBONDING NEW ONES IAW SRM 51-1-19.

Part: SPAR — CRACKED (WS 615-659 LT)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 6 CRACKS TOTALING 13 INCHES LONG AND HEAVY CORROSION AT LT WING REAR SPAR STA XRS615 TO STA XRS659. REPAIRED PER UPS EO DC8-57-0651.

Part: DOUBLER — CORROSION (FS 857)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON BOLT FRAME DOUBLER FS 857 LONGERON 19R. REPLACED FRAME DOUBLER PER SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FS 1265)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 1265 LONGERON 11R AT INTERCOSTAL. REPAIRED INTERCOSTAL PER SRM 51-1-20D, 53-2-0.

Part: SPAR — CRACKED (RT WING)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACK IN TOP SIDE OF RT WING STA XRS 358 SPAR CAP. REPAIRED PER SRM 57-2-0 AND UPS EO DC8-5720-487.

Part: SKIN — CRACKED (RT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 5 INCH LONG CRACK AT RT WING EXTERNAL LEADING EDGE ABOVE PYLON NR 4. REPAIRED L/E SKIN PER SRM 57-2-1A.

Part: SPLICE — CORROSION (FS 210)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LONGERON 8R SPLICE FS 210. REPLACED SPLICE FITTING PER SRM 51-1-20D.

Part: SKIN — CORROSION (FS 1612)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FUSELAGE SKIN AT THE CUTOUT FOR THE AFT ENTRY DOOR HOLD OPEN HOOK. REPAIRED PER UPS EO DC8-53-1608.

Part: VANE — DELAMINATED (LT WING TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 5 FLAP VANE DELAMINATED. REPLACED VANE ASSY PER MM 27-51-14.

Part: SKIN — DELAMINATED (NR 1 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 SPOILER DELAMINATION ON UPPER SURFACE. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: SKIN — CRACKED (LT WING LE)

WHILE ON GROUND, MAINTENANCE FOUND CRACK ABOUT 1.25 INCHES LONG ON WING L/E LOWER OUTBOUND OF NR 2 ENGINE, 8 INCHES AFT OF FIRE BOTTLE INSP PLATE INBOUND. REPAIRED PER UPS ENGINEERING FILE NR DC8-57-0615.

Part: BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS DO NOT DISARM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: WIRE — SEPARATED (GEAR DOOR SWITCH)

PILOT REPORTED AIR TURN BACK AS GEAR RETRACTION DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. FOLLOWED CHECK LIST. RECYCLED GEAR. NO HELP. FOUND WIRE 376D24 SEPARATED FROM TERMINAL STRIP S339, REPAIRED WIRE. DOOR WARNING LIGHT SYS. OPS CHECK NORMAL. ALSO, REPLACED DOOR WARNING LIGHT SWITCHES.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND IN SDF, MAINTENANCE FOUND EMERGENCY BATTERY PACK LOW. REPLACED PACK, OPS CHECK GOOD ON GROUND.

Part: SMOKE DET — INOPERATIVE (NR 2)

MAINTENANCE REPORTED DURING SMOKE DETECTOR TEST, WARNING LIGHT REMAINED ON. RECYCLED SELECTOR SWITCH AND FOUND NR 2 SMOKE DETECTOR WOULD NOT TEST. DEFERRED NR 2 SMOKE DETECTOR PER MEL 26-6-1. CONTROL M90343 ASSIGNED.

Part: CONNECTOR — LOOSE (LT MLG)

PILOT REPORTED, LEFT MLG DOES NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN. CYCLED GEAR 3 TIMES. ERM CHECKLIST COMPLETED WITH REQUIRED VISUAL FLY BY (CHANGED BULBS-DID NOT WORK). FOUND PLUG P1-213 LOOSE AND CONTAMINATED. CLEANED AND SECURED PLUGS AND PINS ON SWITCH PS1-208 AND REINSTALLED PLUG. CKD INSTALLATION AT S1-208 MECH SWITCH PER M/M 32-60-00 PG 201. LEFT MAIN DOWN AND LOCKED INDICATON NOW NORMAL.