N707UP

Part: STRINGER — CRACKED (RT WING) · airframe 74,234 hrs · 48,413 cycles

INSPECTION TYPE:C1,3 RIGHT WING STRINGER 58 IS CRACKED AT XRS 172. REPAIRED STRINGER I.A.W. SRM. 57-2-2 FIG. 3D

Part: SKIN — CRACKED (RT WING) · airframe 74,234 hrs · 48,413 cycles

INSPECTION TYPE:C1,3 RIGHT WING LOWER SKIN IS CRACKED AT XRS 172 BETWEEN STRINGERS 56 & 58. REPAIRED SKIN I.A.W. 8110-3 DH SK 707-212

Part: SKIN — CRACKED (RT WING)

RT WING STATION 172.000 INBD OF NR 3 ENGINE. SKIN CRACKED RT WING LOWER SURFACE, SKIN CRACKED AT WS 172 AFT OF CENTER SPAR. JUST 8 INCHES I/B OF NR 4 MAIN TANK MID FUEL DRAIN VALVE. AREA (APPROX 7 1/4 INCHES) PERFORMED INTERIM REPAIR OF RT INNER WING AFT BOTTOM SKIN PANEL CRACK FOR PURPOSE OF FERRY FLIGHT PER E.O. DC-8-5730-14248C

Part: BATTERY — FAILED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP, SWITCH APPEARS TO BE AT FAULT R & R 'D A/C MAIN BATTERY PER MM 24-30-01 AND 33-50-01 OPS CK GOOD

Part: BATTERY — INOPERATIVE (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. SWITCH APPEARS TO BE AT FAULT. R&R'D A/C MAIN BATTERY.

Part: CONNECTOR — LOOSE (CONTROL UNIT)

INSPECTION TYPE:PFLT NR 1 ENG SHORT CIRCUIT LIGHT ILLUMINATED. ***SUPPLEMENTAL*** RESEATED NR 1 ENG FIRE DETECTION AMPLFIER, CLEANED & RESECURED R2-7000 RELAY SHORT CIRCUIT INDICATOR LIGHT EXTINGUISHED CHECKS GOOD ON TEST.

Part: ODOR — DETECTED (COCKPIT)

INSPECTION TYPE:N/A, AIRCRAFT HAS BURNING SMELL WHEN ANTI ICE IS SELECTED ON. SMELL WENT AWAY WHEN ANTI ICE SELECTED OFF. PACK TEMPS WERE BOTH AT 25 DEGREE C AND BOTH MANIFOLD TEMPS WERE AT 200 DEGREES C. REPEAT WRITE UP, STILL TROUBLESHOOTING AT THIS TIME.

Part: RIB — CRACKED (NR 5 SPOILER)

INSPECTION TYPE:N/A, LEFT WING INBOARD SPOILER OUT HINGE POINT ATTACH FRAME APPEARS TO HAVE A CRACK. *S/D* REMOVED CRACKED FRAME BPT 92716 4-30-00, FABRICATED NEW FRAME PER SRM 57-5-1. NEEDS HEAT TREAT BPT 5-2-00 RB 09282 MF 33016, INSTALLED NEW FRAME AND I/B ATTACH BRACKET PER SRM 51 STANDARD PRACTICES.

Part: RIB — CRACKED (WS 335)

INSPECTION TYPE:C123 LEFT WING CENTER L/E.. RIB CRACKED AT XFS 335.25. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: PAN — CRACKED (WS 520)

INSPECTION TYPE:C123 RIGHT WING L/E SLOT PAN AT STA XS 520.158 IS CRACKED. REMOVED AND REPLACED SLOT PAN IAW DWG 5769857, AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1400)

INSPECTION TYPE:C123, STA 1400 AT LONG 35R FRAME WAS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 2B.

Part: WEB — CORRODED (BS 80)

INSPECTION TYPE:C123, WEB BACKSIDE OF -80 AT LBL 60 COCKPIT SUBFLOOR WAS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5613785 AND SRM 51-1-21, 51-1-20D.

Part: SUBFLOOR — CORRODED (BS 67 - 80)

INSPECTION TYPE:C123 STA -67 TO -80 COCKPIT SUBFLOOR CORRODED BEYOND LIMITS. REPAIRED IAW SRO 8530026.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE:C123 STA 8 LONGERON 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4616250, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123 STA 680 LONGERON 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123 STA 680 LONGERON 4L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762-1N, AND SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (WS 440)

INSPECTION TYPE:C123, STA 440 STRINGER 64 SPLICE WAS CRACKED AFT OF FWD SPAR. REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG 3644046 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C123 STA 70 LONGERON 31L END FITTING CRACKED INBD AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 1540)

INSPECTION TYPE:C123 STA 1540 RBL 34 FLOORBEAM AFT FACE WEB AREA CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 DH SK 707-471.

Part: FITTING — CORRODED (BS 1280)

INSPECTION TYPE:C123 STA 1280 LONGERON 21R FLOOR BEAM TO CUSP FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 9754064, AND SRM 51-1-20D.

Part: SKIN — CRACKED (BS 70)

INSPECTION TYPE:C123, STA 70 SKIN CRACKED BETWEEN LONG 36 AND 35R. REPAIRED IAW SRM 53-2-1 FIG 7.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:C123, STA 70 LONG 34R FITTING WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 240)

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB WAS CRACKED AT XS240. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (BS 1620)

INSPECTION TYPE:C123, STA 1620 AT LONG 17R FRAME WAS CRACKED. REPAIRED IAW SRM ADDENDUM DC8-5310-11728-A.

Part: FITTING — CRACKED (BS 900 - 920)

INSPECTION TYPE:C123 STA 900-920 LONGERON 1 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521, AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 250)

INSPECTION TYPE:C123, LEFT WING L/E VERTICAL RIB WAS CRACKED AT XS 250. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (BS 25 - 42)

INSPECTION TYPE:C123, STA -25 TO -42 LBL 10 COCKPIT SUBFLOOR INTERCOSTAL WAS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 1D.

Part: RIB — CRACKED (WS 256)

INSPECTION TYPE:C123, LEFT WING L/E RIB WAS CRACKED AT XS256.25. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:C123, VERTICAL L/E RIB WAS CRACKED AT FS 248.38. REPAIRED IAW SRM 55-2-0 FIG 8.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:C123, VERTICAL L/E RIB CRACKED AT FS 279.687. REPAIRED IAW SRM 55-2-0 FIG 2.

Part: DOUBLER — CORRODED (BS 32 - 52)

INSPECTION TYPE:C123, STA -32 TO -52 LBL 60 FINGER DOUBLER WAS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB WAS CRACKED AT XFS 772.5. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769471 AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER WAS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 6769600 AND SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CRACKED (WS 297.5)

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER CRACKED AT XFS 297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-21.

Part: DOUBLER — CRACKED (WS 257)

INSPECTION TYPE:C123 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 257. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21, 51-1-21A.

Part: INTERCOSTAL — CRACKED (BS 1750)

INSPECTION TYPE:C123, STA 1750 BL 0 FLOOR SUPPORT INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5755032 AND SRM 51-3-0.

Part: SKIN — CRACKED (BS 1660)

INSPECTION TYPE:C123, STA 1660 AT LONG 10L SKIN WAS CRACKED AT DOOR CUTOUT. REPAIRED IAW 8110-3 APPROVED DH SK 707-940.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (BS 1660)

INSPECTION TYPE:C123, STA 1660 LONG 10R SKIN CRACKED AT UPPER AFT CORNER AFT SERVICE DOOR CUTOUT. REPAIRED IAW SRM 53-2-0 FIG 16.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C123, STA 70 LONG 33R FITTING WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067 AND SRM 51-1-20D.

Part: FITTING — CRACKED (A/C BAY)

INSPECTION TYPE:C123, STA 8 LONG 31R UPPER FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4640929, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 297.5)

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER WAS CRACKED AT XFS297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (WS 628.75)

INSPECTION TYPE:C123, LT WING L/E HAD RIBS CRACKED AT XFS 628.75 UPPER AND LOWER, AND XFS 616.25 LOWER. REPAIRED PER SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 485)

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER CRACKED AT XW485. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE:C123 STA 717 LONG 19L FITTING IN LT FWD EMERGENCY EXIT DOOR WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE:C123 RIGHT WING L/E RIB ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753294, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 789)

INSPECTION TYPE:C123, STA 798 LONG 19R END FITTING IN RT AFT EMERGENCY EXIT DOOR WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 572)

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (WS 250)

INSPECTION TYPE:C123 LEFT WING L/E UPPER RIB IS CRACKED AT XS250.089. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE:C123 STA 1150 LONGERON 33R-34R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 426)

INSPECTION TYPE:C123 STA 426 LOWER RT SIDE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754047, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123 STA 680 LBL 24 SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4645517, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 980 - 1050)

INSPECTION TYPE:C123 STA 980-1050 LONGERON 31L HAS HEAVY CORROSION. REPAIRED IAW SRM 53-4-1 FIG 43.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123 STA 680 LONGERON 2L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C123, STA 680 LONG 3R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG 377962 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 340 - 350)

INSPECTION TYPE:C123 STA 340-350 BETWEEN LONGERON 34L-35L BATHTUB FITTING INSIDE TORQUE BOX HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 380 - 400)

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

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C123 STA 860 LONG 4R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 1240 - 1260)

INSPECTION TYPE:C123, STA 1240-1260 INTERCOSTAL AT LONG 10L WAS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C123 STA 1140 LONGERON 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 484)

INSPECTION TYPE:C123, LEFT WING CENTER L/E UPPER RIB CRACKED AT XS484.895. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 285 & 341)

INSPECTION TYPE:C123, LEFT WING L/E HAD RIBS CRACKED AT XFS 285.25 AND XFS 341.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SHEAR TIE — CRACKED (BS 1420)

INSPECTION TYPE:C123 STA 1420 LONGERON 31L SHEAR TIE IS BROKEN AT CORNER. REMOVED, FABRICATED, AND REPLACED SHEAR TIE IAW DWG 5640240, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C123 STA 1230 BETWEEN LONG 34R-35R FITTING INSIDE TORQUE BOX IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:C123 STA 1220 FLOORBEAM TO FRAME FITTING IS CORRODED BEYOND LIMITS AT LONGERON 21R. REMOVED AND REPLACED FITTING IAW DWG 3754047, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 335.25)

INSPECTION TYPE:C123, LEFT WING CENTER L/E INTERNAL DOUBLER CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5769589, SRM 51-1-21.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C123, STA 860 LONG 7L END FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1694)

INSPECTION TYPE:C123, STA 1694 LONG 29R END FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 223)

INSPECTION TYPE:C123 LEFT WING L/E RIB EXTENSION ANGLE IS CRACKED AT XW 223. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5769859, AND SRM .51 -1-20D

Part: FITTING — CRACKED (BS 1020)

INSPECTION TYPE:C123, STA 1020 LONG 20L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB CRACKED AT XILD.7095. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (BS 320)

INSPECTION TYPE:C123 STA 320 FRAME CRACKED AT LONGERON 11R. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1040)

INSPECTION TYPE:C123, STA 1040 LONG 19L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 660 - 680)

INSPECTION TYPE:C123, STA 660-680 LONG 11R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540, SRM 51-1-21, 51-1-20D.

Part: STIFFNER — CRACKED (WS 250)

INSPECTION TYPE:C123 RIGHT WING L/E AT STA XS250.089 VERTICLE STIFFENER IS CRACKED. REMOVED, FABRICATED, AND REPLACED STIFFENER IAW DWG 9753293, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1228 - 1240)

INSPECTION TYPE:C123 STA 1228-1240 LONGERON 20R TORQUE BOX TO FRAME SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3758513, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C123, STA 742 LONG 11L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE:C123 STA 940 LONGERON 19R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C123 STA 742 SFT SIDE LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE:C123, STA 960 LONG 19R INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C123, STA 759 LONG 18R INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: STIFFNER — CRACKED (WS 246)

INSPECTION TYPE:C123 RIGHT WING L/E AT STA XS246.313 FRONT VERTICLE STIFFENER ANGLE IS CRACKED. REPAIRED IAW SRM 57-6-2 FIG 2.

Part: RIB — CRACKED (WS 250)

INSPECTION TYPE:C123, RIGHT WING L/E AT STA XS 250.089 UPPER RIB WAS CRACKED. REPAIRED PER SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C123, STA 857 LONG 13R INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1020)

INSPECTION TYPE:C123, STA 1020 LONG 20L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C123, STA 1180 LONG 20R INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C123 STA 857 LONGERON 19L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750422, AND SRM 51-1-20D.

Part: STIFFNER — CRACKED (WS 97)

INSPECTION TYPE:C123 RIGHT WING T/E AT FLAP HINGE STA 97 INBD VERTICLE STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER IAW DWG 3643319, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:C123, STA 902 LONG 20L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 220)

INSPECTION TYPE:C123, STA 220 LONG 11R SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5644985 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1080)

INSPECTION TYPE:C123 STA 1080 LONGERON 20L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750438, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE:C123, STA 920 LONG 20L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 227.335)

INSPECTION TYPE:C123 LEFT WING L/E. UPPER RIB CRACKED AT XS227.335 REPAIRED I.A.W. SRM 57-2-0 FIG. 2

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C123, STA 857 LONG 20L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779979 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C123, STA 1180 LONG 17R INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 660)

INSPECTION TYPE:C123, STA 660 FRAME SPLICE WAS CRACKED BETWEEN LONG 21R TO 22R. REMOVED AND REPLACED FRAME SPLICE IAW DWG 5646688 AND SRM 51-1- 20D, 53-4-0 FIG 30.

Part: FRAME — CRACKED (PAX DOOR)

INSPECTION TYPE:C123, LEFT AFT ENTRY DOOR HAD A CRACKED FRAME. REPAIRED IAW SRM 52-2-0 FIG 2.

Part: SKIN — CRACKED (BS 80)

INSPECTION TYPE:C123 STA -80 ST LONGERON 32L, NOSE LANDING GEAR DOOR CENTER HINGE AREA ON FUSELAGE SKIN IS CRACKED.. REPAIRED IAW EO DC8-5330-4154-B.

Part: FITTING — LEAKING (RUDDER)

INSPECTION TYPE:N/A, AFTER MORE INVESTIGATION FOUND DURING CRUISE ACFT HAD ERRATIC HYD SYSTEM PRESSURE FOLLOWED BY HYD FLUID LOSS DOWN TO STANDPIPE FLUID. DECLARED EMERGENCY, LANDING IN SDF WAS UNEVENTFUL. OBTAINED FLAPS 3 5 FOR LDG AND NORMAL GEAR FREE FALL. MX FOUND HYDRAULIC RUDDER PRESSURE SWITCH LEAKING AT 3 FITTINGS. UNION SECURED ALL FITTINGS AND REMOVED AND REPLACED O-RING AT UNION BB08473 2. OPS AND LEAK CHECKS GOOD PER MM 29-30-07.

Part: INU — FAILED (LEFT)

INSPECTION TYPE-N/A, AIR TURNBACK CPATS INS FAILED ON T/O ROLL (DUMP FUEL DOWN TO 46.00). REMOVED AND REPLACED NR 1 INU PER M/M 34-44-03, OPS CK GOOD. (S/N 1172) OFF, (P/N 463001-6110-0412) OFF, (S/N 1307) ON, (P/N 463001-6130-0412) ON.

Part: MEC — FAILED (NR 3 ENGINE)

INSPECTION TYPE-N/A, NR 3 ENG FLAMED OUT IN CRUISE FLT AT FL 350 ON ATTEMPTED RE-IGT, EGT CLIMBED RAPIDLY TO 900 DEG, SHUT DOWN ENG. FOB AT TIME WAS 50.0 WITH 12,750 LBS IN NR 3 MAIN NORMAL CONFIG. REPLACED NR 3 ENG MEC PER MM-73-20-01, T/C 1037/1038 SYSTEM LEAK AND OPS CHK OK. (P/N 8063-211) OFF, (P/N 8063-212) ON, (S/N WYG34934) OFF, (S/N WYG35140) ON.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERG EXIT LIGHT INOP ON BATT POWER. REMOVED AND REPLACED EMER BATT PACK , OPS CHECK GOOD, P/N ON/OFF 5708458-503, S/N OFF FTL157 S/N ON 976.

Part: ANGLE — CORRODED (BS 780)

INSPECTION TYPE-C, FLOORBEAM ATTACH ANGLE AT STA 780 HAS HEAVY CORROSION AND IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE AT STA 780 RBL 45 TO 69 IAW DWG 3643111 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:C F/S 1690 LONGERON 28L. LONGERON TO FRAME FITTING IS EXFOLIATED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: SHEAR TIE — CRACKED (BS 1200)

INSPECTION TYPE-C, SHEAR TIE CRACKED FS 1200 STR 33R TO 34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-C, STA 1160 AND STR 33R AND 34R SHEAR TIE IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 1766)

INSPECTION TYPE-C, BOTH TAIL SKID BACKUP FITTINGS CRACKED AT FS 1766. REMOVED, FABRICATED, AND REPLACED FITTINGS IAW SRM 51-3-0 AND DWG 3750866.

Part: FITTING — CRACKED (BS 1750)

INSPECTION TYPE-C, AFT FUSELAGE TAIL SKID FITTING IS CRACKED AT BOTH END BOLT HOLES AT STA 1750 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1480)

INSPECTION TYPE-C, FS 1480 LWR FRAME CORRODED BEYOND LIMITS BETWEEN LONG 35R TO 36. REPAIRED IAW SRM 53-2-0.

Part: SHEAR TIE — CRACKED (BS 1520)

INSPECTION TYPE-C, AFT PIT FS 1520 SHEAR TIE BETWEEN LONGERONS 31L TO 32L LEFT SIDE IS CRACKED. REPAIRED IAW SRM 53-2-0.

Part: SPLICE — CRACKED (BS 1350)

INSPECTION TYPE-C, SPLICE FITTING AT LONG 24L FS 1350 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 51-1-20D AND DWG 4646163.

Part: DOUBLER — CRACKED (BS 640)

INSPECTION TYPE-C, FS 640 BETWEEN LONG 35R AND 35L INTERNAL DOUBLER IS CRACKED. REPAIRED IAW DHC SK-707-712.

Part: SKIN — CORRODED (BS 1690-1890)

INSPECTION TYPE-C, FS 1690 TO 1890 REMOVE AND REPLACE TAIL SKID LWR SKIN DUE TO CORROSION. REMOVED AND REPLACED SKIN IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE-C, BATHTUB FITTING IS CRACKED AT FS 1200 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1160)

INSPECTION TYPE-C, CORROSION BETWEEN BATHTUB FITTING AND SKIN AT STA 1160 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 435)

INSPECTION TYPE:C LT WING L/E RIB AT STA XS 435.0 CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CORRODED (BS 1766)

INSPECTION TYPE-C, LWR INTERNAL DOUBLER CORRODED FS 1766 LBL 3. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5649329.

Part: CUSP — CORRODED (BS 453)

INSPECTION TYPE:C F/S 453 CORROSION REMOVAL RT CUSP BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5330-2159-B.

Part: FRAME — CORRODED (BS 260)

INSPECTION TYP-C, STA 260 BTWN LONGERON 34R 33L, THE FWD FACE OF THE FRAME IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME AND ASSOCIATED PARTS IAW DWG 5754671 AND SRM 53-4-1.

Part: SPLICE — CORRODED (BS 1350)

INSPECTION TYPE-C, AFT PIT FS 1350 LONG, 28L SPLICE FITTING CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4646163.

Part: SHEAR TIE — CORRODED (BS 1161)

INSPECTION TYPE-C, FS 1161 BTWN STR 27L-28L SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-C, FS 1040 TO 1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FRAME — CRACKED (BS 99)

INSPECTION TYPE-C, NOSE SECTION LT SIDE AT STA 99 FRAME IS CRACKED IN TWO PLACES UPPER AND LWR SECTION OF SPLICE. STOP DRILLED CRACK ON UPPER FLANGE AND REMOVED DAMAGE ON LWR FLANGE AND REPAIRED IAW DHC SK 707-600 AND REFERENCE TO EO DC8 5310- 10296.

Part: LONGERON — CRACKED (BS 1280-1300)

INSPECTION TYPE:C F/S 1280-1300 STR 31L IS CRACKED BTWN 5 FASTENERS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 5753744.

Part: DOUBLER — CORRODED (BS 1160-1120)

INSPECTION TYPE-C, STA 1160 TO 1220 BTWN STR 33R TO 34L. THE INTERNAL DOUBLER HAS MANY AREAS OF MODERATE CORROSION. REPAIRED AREA IAW 8110-3 APPROVED DHC SH 707-569.

Part: SKIN — CORRODED (BS 1650)

INSPECTION TYPE-C, STA 1650 BTWN STR 28L TO 32L THE INTERNAL SKIN IS CORRODED AND EXTENDS UNDER THE TEAR STRAP AT EACH BAY. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK707-590.

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE-C, FS 1260 TO 1280 STR 35R SPLICE FITTING HAS 4 INCH CRACK. REMOVED, FABRICATED, AND REPLACED FITTING IAW SRM 51-1-20D AND DWG 3759258.

Part: CARGO TRACK — CORRODED (CARGO COMPT)

INSPECTION TYPE:C NR 2 PIT, CARGO TRACK AFT DOOR RT SIDE HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0. AND DWG 5750726.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE-C, STA 1180 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1346-1354)

INSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CORROSION FROM SKIN, FOUND WITHIN LIMITS IAW SRM 53-2-0. FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5779914.

Part: CUSP — CORROSION (BS 240-260)

INSPECTION TYPE-C, FS 240 TO 260 RT CUSP UPPER SURFACE HAS SEVERE CORROSION. REPAIRED IAW SRM 53-2-5.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE-C, STA 300 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 320)

INSPECTION TYPE-C, STA 320 AT STR 26L, DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-C, FS 440 TO 460 STR 34L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE-C, STA 1200 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1346-1354)

INSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CORROSION FROM SKIN, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5779914 AND SRM 51-1-21.

Part: FITTING — CRACKED (WS 98)

INSPECTION TYPE-C, LT WING T/E, THE LWR REAR SPAR TO AUX SPAR TIE FITTING AT THE STA 98 FLAP HINGE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5642205.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-C, LT WING RIB AT STA.XOLDI 6.225 I/B SIDE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 372.75)

INSPECTION TYPE:C LT WING L/E RIB AT STA XFS 372.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 379)

INSPECTION TYPE:C LT WING L/E RIB AT STA XFS 379.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 360)

INSPECTION TYPE-C, LT WING L/E LWR RIB AT STA XFS 360.25 IS CRACKED AT AFT DOUBLER FSTR HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769530.

Part: STRINGER — CORRODED (BS 70)

INSPECTION TYPE-B CK, CORROSION FOUND AT STR 30R BETWEEN STR 25 TO 35 DOME NUT ATTACH POINTS FOR EXTERNAL AIR COND DOOR GRND HOOK UP. EXPOSED STRINGER AREAS WITH CORROSION. BLENDED 5 AERAS OF CORROSION PERFORMED THICKNESS TEST PER QC THICKNESS TESTER CL304. REPAIRED PER EO DC8-5310-9989.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, BATTERY VOLTAGE LOW IE.-LESS THAN 24 VOLTS ON BITE CHECK, WITH EMERGENCY LIGHTING EXTREMELY WEAK/UNUSABLE. AIRCRAFT BATTERY VOLTAGE WITHIN LIMITS. RELAMPED EMERGENCY LIGHTING BULB AND OPS CHECKED NORMAL.

Part: BATTERY PACK — DAMAGED (CABIN)

INSPECTION TYPE-N/A, CONNECTOR P1-1345 AT EMERGENCY LIGHT BATTERY PACK HAS DAMAGED PINS. REPLACED CONNECTOR P1-1345.

Part: TRIPLER — CRACKED (WS I6.225)

INSPECTION TYPE-SP, RT WING L/E AT STA XOLDI 6.225 THE LWR INTERNAL TRIPLER IS CRACKED. REMOVED CRACKED TRIPLER, FABRICATED, AND INSTALLED REPLACEMENT TRIPLER IAW SRM 57-3-3 AND 51-1-21.

Part: RIB — CRACKED (WS 520.168)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XS 520.168, INBD END OF THE STUB WING, IS BROKEN AT THE AFT UPPER END INBD AND OUTBD HALVES, AND ALONG THE LWR SIDE BETWEEN THE FASTENERS. THREE CRACKS TOTAL. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 391.5)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XFS 391.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-3-2 AND 57-2-0.

Part: RIB — CRACKED (WS 467.323)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XS467.323 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-SP, RT WING L/E BETWEEN NR 3 AND NR 4 ENG'S AT STA 6.225 XOLDI HAS A CRACKED RIB, INTERCOSTAL, AND ATTACH CLIP. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL AND CLIP IAW SRM 51-1-21, 51-1-20D, AND DWG 5769589. REPAIRED RIB IAW SRM 57-2-0.

Part: INTERCOSTAL — CRACKED (WS I6.225)

INSPECTION TYPE-SP, RT WING L/E INBD SIDE OF THE STA XOLDI 6.225 RIB, FWD OF THE PNEU DUCT THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21 AND DWG 5769589.

Part: RIB — CRACKED (WS 448.581)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XS 448.581 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-3-2 AND 57-2-0.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-SP, RT WING L/E, LWR SKIN AT THE NR 4 PYLON CUTOUT HAS A 6 INCH CRACK. REPAIRED IAW SRM 57-2-1A.

Part: RIB — CRACKED (WS 467.323)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XS467.323 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 454.976)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA 454.976 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-3-2 AND 57-2-0.

Part: RIB — CRACKED (WS 329)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XFS 329.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 347.75)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XFS 347.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-3-2 AND SRM 57-2-0.

Part: RIB — CRACKED (BS 461.372)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA 461.372 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XS442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE-SP, RT WING L/E RIB AT STA XFS 397.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: WINDOW — OUT OF ADJ (RT COCKPIT)

INSPECTION TYPE-N/A, 1ST OFFICERS CLEARVIEW WINDOW VERY HARD TO OPEN. ADJUSTED F/O'S CLEARVIEW WINDOW PER MM CH 56-10-03 ADJ/TEST.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS DID NOT FUNCTION DURING (ILLEGIBLE) CHECK. REPLACED EMERGENCY LIGHTING BATTERY PACK, OPS CKS GOOD.

Part: FRAME — CORRODED (BS 1540)

INSPECTION TYPE: C. AFT ACCESS COMPT FUSELAGE FRAME AND LONGERON 33L CORRODED STA 1540. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0, REMOVED GILLINER FOR ACCESS. REPAIRED FRAME SECTION IAW DC8 SRM 53-2-0 AND REO 02193. ALODINED AND PRIMED ALL PARTS IAW 51-1-8. INSTALLED CAP AND ANGLE SPLICES IAW SRM 51-1-20D. CLOSED GILLINER PANEL IAW SRM 51-3-0. SEALED REPAIR IAW 51-1-17.

Part: SKIN — CRACKED (C-4 DOOR)

INSPECTION TYPE: C. C-4 DOOR CUT-OUT CRACKED UPPER FWD CORNER. REPAIRED PER SRM 53-2-0 PG 149/150.

Part: LONGERON — CORRODED (BS 1600-1640)

INSPECTION TYPE: C. LONGERON NR 24L FROM STA 1600 - 1640 CORRODED. FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM'S 53-4-1 AND 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51-1-20D. PAINT TO BE ACCOMPLISHED ON UPS N/ 468048.

Part: SKIN — CRACKED (DOOR)

INSPECTION TYPE: C. DOOR CUT-OUT CRACKED FWD LOWER CORNER, .50 INCH. REPAIRED PER SRM 53-2-0 PG 139.

Part: ENGINE — MALFUNCTION (NR 1 ENGINE)

PILOT REPORTED NR 1 ENGINE SHUTDOWN DUE BANG AND N1, N2 AND F/F ALL CUT BACK. A/C ENGINE SHUTDOWN IAW QRH PROCEDURES. REPLACED NR 1 ENGINE PER TC 1001, 1002, 1003. OPS RUN AND LEAKS CHECK OK. PN CFM56-2-C1.

Part: LANDING GEAR — FAILED (RT MLG)

(SUPPLEMENTAL MRR) PILOT REPORTED RT MAIN LANDING GEAR COLLAPSED ON LANDING ROLL AT SDF. REPLACED RT MAIN GEAR. OPS CK GOOD PER T/C 2535.

Part: INSULATION — BINDING (PRESS BULKHEAD)

DURING TEST OPS AND TAKEOFF, THE GEAR LEVER WAS HARD TO RAISE INTO UP AND LOCKED POSITION, CYCLED GEAR AND LEVER MOVED OK INTO UP AND LOCKED. FOUND INSULATION ON FWD PRESSURE BULKHEAD FOULING CONTROL CABLES. INSTALLED INSULATION PROPERLY AND GEAR OPS CHECKED GOOD PER MM 32-30-00.

Part: BULKHEAD WEB — CRACKED (FS 980)

WHILE IN 'C' CHECK MAINTENANCE FOUND 1 INCH LONG CRACK ON PRESSURE BULKHEAD WEB AT FS 980, RBL 2.65. INSTALLED REPAIR IAW UPS EO DC8-53-1308.

Part: FITTING — CORROSION (FS 280)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON B/T FITTING LONGERON 33R-34R, FS 280. INSTALLED REPAIR IAW SRM 53-2-0.

Part: DOUBLER — CORROSION (FS 267-273)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION AT DOUBLER, FS 267 TO 273, LONGERON 35L. INSTALLED REPAIR IAW UPS EO DC8-5310-6602.

Part: BEAM — CRACKED (CARGO SLIDE DOOR)

WHILE IN 'C' CHECK MAINTENANCE FOUND CARGO SLIDE DOOR NR 5 BEAM INBOARD CHANNEL CRACKED IN TWO LOCATIONS. INSTALLED REPAIR IAW UPS EO DC8-5230-6564-A.

Part: DOUBLER — CORROSION (FS 320-405)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON INNER DOUBLER, FS 320-405, LONGERON 35L-34R. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: SHEAR TIE — CORROSION (FS 1240)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON SHEAR TIE, LONGERON 35L-36, FS 1240. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: JAMB DOUBLER — CRACKED (FWD CARGO DOOR)

WHILE IN 'C' CHECK MAINTENANCE FOUND EXTERNAL SKIN DOUBLER HAS SEVERAL CRACKS ON FORWARD CARGO DOOR JAMB CUTOUT. LOWER FWD CORNER. INSTALLED REPAIR IAW UPS EO DC8-5310-6566-B.

Part: WEBBING — CORROSION (FS 1180)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON WEBBING, FS 1180 LONGERON 34R-35R. INSTALLED REPAIR IAW UPS EO DC8-5310-6599-A.

Part: END FITTING — CORROSION (FS 1400)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON FS 1400, END FITTING, LONGERON 21L. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: BELTFRAME — CORROSION (FS 1360)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON BELTFRAME, FS 1360, LONGERON 34L-33R. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2.

Part: FITTING — CORROSION (FS 1153)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON B/T FITTING, FS 1153, LONGERONS 30L-31L. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1180)

WHILE IN 'C' CHECK MAINTENANCE FOUND MODERATE CORROSION ON B/T FITTING, FS 1180, LONGERON 35R-36. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2D.

Part: FITTING — CORROSION (FS 1153)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING, FS 1153, LONGERONS 27L-28L. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 110)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 25R SPLICE FITTING, FS 110. INSTALLED REPAIR IAW SRM 51-1-20D AND SRM 51-1-21.

Part: ANGLE — CORROSION (FS 810)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON FLOOR WEB ANGLE, LONGERON 21R, F.S. 810. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 380-400)

WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 35L, FS 380-400. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 1560)

DURING 'C' CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION ON LONGERON 31L, FS 1560. INSTALLED REPAIR IAW UPS EO DC8-5310-6606-A.

Part: FITTING — CRACKED (FS 610)

DURING 'C' CHECK, MAINTENANCE FOUND LONGERON SPLICE FITTINGS 2 EACH CRACKED AT FS 610, LONGERONS 31L AND 31R. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: FRAME — CORROSION (FS 1360-1340)

DURING 'C' CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION ON FRAME, FS 1360-1340, BELOW LONGERON 21R. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2.

Part: SKIN DOUBLER — CORROSION (FS 1600)

DURING 'C' CHECK, MAINTENANCE FOUND SKIN DOUBLER HEAVY CORROSION UNDER SHEAR TIE, FS 1600, LONGERON 28R. INSTALLED REPAIR IAW UPS EO DC8-53-1310 (MINOR).

Part: VANE — DELAMINATED (NR 2 TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 2 FLAP VANE DELAMINATED ON UPPER SURFACE. REPLACED VANE PER MM 27-51-14.

Part: VANE — DELAMINATED (NR 6 TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NB 6 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14.

Part: VANE — DELAMINATED (NR 5 TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NR 5 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14.

Part: RIB — CRACKED (WS 660 LE)

DURING 'C' CHECK MAINTENANCE FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STA XFS 660. REPAIRED RIB PER MM 57-00-00.

Part: SKIN DOUBLER — CRACKED (FS 12)

WHILE IN 'C' CHECK MAINTENANCE FOUND FUSELAGE SKIN DOUBLER HAS 1 INCH LONG CRACK. RT AND LT AFT HEAT EXCHANGER CUTOUT LOWER AFT CORNERS. INSTALLED REPAIR IAW UPS EO DC8-5330-4732D.

Part: LONGERON — CRACKED (FS 260-265)

WHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10.

Part: RIBS — CRACKED (LT WING LE)

WHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 9, 11, 12, 14, AND 16 UPPER RIBS CRACKED ON UPPER SURFACES. INSTALLED REPAIRS IAW MM 57-00-00, FIG. 801. (P/N 5769589, 5720123).

Part: LONGERON — CRACKED (FS 260-265)

WHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10.

Part: RIBS — CRACKED (LT WING LE)

WHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 17, 21, 24, AND 27 UPPER RIBS CRACKED IN UPPER SURFACES. INSTALLED REPAIRS IAW MM 27-00-00, FIG. 801. (P/N 5769589, 5720123).

Part: FITTING — CRACKED (FS 1152)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: SUPPORT FITTING — CORRODED (FS 680-687)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D.

Part: FRAME — CORROSION (FS 20)

WHILE IN 'C' CHECK, MAINTENANCE FOUND DURING A CORROSION BULGE INSPECTION, FRAME HEAVILY CORRODED ON OPEN UP AT FS 20, LONGERON 33R. INSTALLED REPAIR IAW SRM 53-2-0.