N836UP

Part: FUEL CONTROL — DEFECTIVE (LT ENGINE) · airframe 923 hrs · 751 cycles

LEFT POWER LEVER BINDS WHEN ADVANCED FWD. IN CRUISE POWER LEVERS ARE SPLIT BY ONE KNOB WIDTH. R & R THE LT ENG FUEL CONTROL UNIT. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RETURNED TO SERVICE.

Part: STOP FITTING — OUT OF ADJUST (ELEVATOR TRIM) · airframe 352 hrs · 301 cycles

ON DESCENT THROUGH ABOUT FL 270 THE YELLOW ELEC PITCH TRIM INDICATION ON PFD FOLLOWED BY RED PITCH TRIM ANNUNCIATOR LIGHT. CONTROLS WERE VERY HARD TO PUSH FWD. USED POWER TO ASSIST IN THE CONTROL OF THE ACFT. AN EMERGENCY WAS DECLARED AT FL 200 & DIVERTED. FOLLOWED THE CHECKLIST & A SUCCESSFUL FLAPS UP LANDING WAS MADE. TROUBLESHOT & FOUND THE LEFT TRIM CABLE STOP NOT CLEARING LIGHTENING HOLE. CABLE STOP WAS ADJUSTED. ELECTRIC AND MANUAL TRIM OPS CHECKS WERE MADE, NO DEFECTS NOTED. REPLACED THE LT & RT ELEVATOR TRIM ACTUATORS, ELEVATOR TRIM CABLE BULLET STOP FRAME WEB TRIMMED FOR CLEARANCE & ELEVATOR TRIM CABLES ADJUSTED. A SUCCESSFUL OPS CHECK FLIGHT WAS PERFORMED. ACFT WAS RETURNED TO SERVICE.

Part: KNOB — MALFUNCTIONED (RUDDER TRIM) · airframe 95 hrs · 83 cycles

DURING PREFLIGHT INSPECTION RUDDER TRIM DIFFICULT TO ROTATE & SKIPS UNITS MAKING POSITION INDICATION INACCURATE. MX DISASSEMBLED RUDDER TRIM TAB KNOB & POINTER ASSEMBLY, CLEANED, LUBED & RE-INDEXED TRIM INDICATOR ASSEMBLY. NO DEFECTS NOTICED. ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (TE FLAP)

RT INBD FLAP INBD WEB CRACKED. REMOVED ONE AREA OF CRACKED SKIN. D. RIEKE. 75838 5-8-03. REMOVED WEB. FABRICATED NEW WEB FROM 2024-T3 .040" PER SAMPLE. STARTED DRILLING NEW WEB. J. DUNLAP 26402 05-09-03. INSTALLED NEW WEB AND STIFFNERS IAW EO DC-8 5750-18733.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY LIGHT DISARM CHECK INOPERATIVE. REPLACED CONNECTOR PLUG P01-1345. SYSTEM CHECKS GOOD IAW M/M 33-50-01

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: ASV, EMERGENCY LIGHTS INOPERATIVE. REPAIRED OPEN AT P1-1345 PIN 11 AS REQUIRED REF WDW 33-50-01. SYSTEM OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS BATTERY DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY SYSTEM, OPS CHECKS NORMAL PER MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, LIGHTS OPS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:AS EMERGENCY LIGHTS ARE INOP IN TEST. REMOVED, REPLACED, AND TESTED EMERGENCY BATTERY PACK IAW MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:IN NO ILLUM OF EMERGENCY LIGHTS. REMOVED AND REPLACED BATTERY (EMERGENCY) PACK, OPS CHECK GOOD 33-50.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 1520 LBL 55 SEAT TRACK IS CRACKED. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 FWD ENTRY DOOR AFT TORQUE BOX HAS A CRACKED INTERCOSTAL STA 60-70 BETWEEN LONG 14L-15L. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5597646, AND SRM 51-1-20D, 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 1240 FRAME IS CORRODED BEYOND LIMITS LONG 35R-36. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 836-901, BY INSTALLING A REPAIR STRAP IAW DH SK 836-901.

Part: FITTING — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING STRINGER 64 SPLICE FITTING IS CRACKED AT APPROX XRS 510. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3644046 AND SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 55 RT SIDE FRAME IS CRACKED ABOVE FITTING AT CUSP. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 70-120 LONG 31R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT HORIZONTAL STAB T/E UPPER ANGLE IS CRACKED AT XE 29. REPAIRED ANGLE IAW SRM 55-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 SEAT TRACK STA 1020-1040 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 SEAT TRACK STA 1400-1540 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 12 FRAME AND WEB ARE CORRODED BEYOND LIMITS AT RBL 48. REPAIRED FRAME BY INSTALLING FILLER AND ANGLE DOUBLER IAW 8110-3 APPROVED DH SK 836-869, AND REPAIRED WEB IAW SR08530026.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 SEAT TRACK IS CORRODED BEYOND LIMITS STA 1130-1150 AT LBL 60. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A, AND DC8-53B-003-501.

Part: RIB — CRACKED (HORIZ STAB) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT HORIZONTAL STAB LOWER RIB IS CRACKED AT XFS 135. REPAIRED RIB IAW SRM 55-2-0 FIG 2.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT HORIZONTAL STAB LOWER FLANGE FITTING AT FRONT SPAR IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 354 AND XFS 379 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 491.193. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 834. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 610 LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D, 53-1-0.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 366.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: CLIP — CRACKED (LEFT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, LEFT WING L/E. INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED,FABRICATED,AND REPLACED CLIP I.A.W.DWG. 5769589,AND SRM. 51- 1-20D

Part: CLIP — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED CLIP IAW DWG 5769589, AND SRM 51-1-21.

Part: DOUBLER — CORRODED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E STALL WARNING DOUBLER IS CORRODED BEYOND LIMITS AT XFS 373. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21 APPROX SIZE 5 X 7 INCHES.

Part: FITTING — CRACKED (CARGO BAY) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, STA. 440-460 LONG. 31R SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20D

Part: ANGLE — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 472.099. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770170, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 297.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E INBOARD WRAP-AROUND DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (LEFT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, LEFT WING L/E. LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.25 REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-21,51-1-20D

Part: SPLICE — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 600-620 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 280 LONG 21R FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 404. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 NR 2 STUB WING VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 515.72. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 585. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RIGHT WING L/E.) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 653.75 AND XFS 660 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C2,3, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 766.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: DOUBLER — CORRODED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E LOWER INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 722.25 TO XFS 735 (PANEL 518C). REMOVED AND REPLACED DOUBLER IAW DWG 3641257, AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 R-2 DOOR UPPER AFT CORNER OF OPENING SKIN, INTERNAL DOUBLER, AND LONGERON 11R ARE CRACKED AT STA 1654. REPAIRED SKIN AND INTERNAL DOUBLER, AND LONGERON IAW 8110-3 APPROVED DH SK 936-267, AND DC8-5330-15557-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E INTERNAL WRAP AROUND DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CORRODED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS 341. CUT OUT CORRODED AREA, FABRICATED DOUBLER AND FILLER APPROX SIZE 6 X 2.5 INCH. REPAIRED SKIN IAW EO DC8-5720-7767-A.

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 747.5 TO XFS 760 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 628.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 578.75, XFS 585. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 847.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 753.75, XFS 760. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 635 AND XFS 647.5. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 130 LONG 31L FINGER DOUBLER IS CRACKED. TRIMMED OFF CRACKED FINGER ON FINGER DOUBLER IAW ENGINEERING RESPONSE AND SRM CHAPTER 51 GUIDELINES.

Part: RIB — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, LEFT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: SPLICE — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 210 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754220, AND SRM 51-1-20D.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 STA 1766 LONG 10R AFT SIDE OF AFT PRESSURE BULKHEAD HAS TWO SEAL ANGLES CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED ANGLES IAW DWG 5772638, AND SRM 51-1-20D, 51-3-0.

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5,XFS 728.75, XFS 735. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75, XFS 835. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING L/E.) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5 AND XFS 728.75 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: ANGLE — CRACKED (COCKPIT) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C2,3 STA -99 PILOTS WINDOW FRAME HAS A CRACKED ANGLE AT FWD LOWER CORNER AFT OF SPLICE. REMOVED, FABRICATED, AND REPLACED ANGLE IAW SRM 53-2-3 FIG 3, 53-1-0.

Part: SKIN — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9 REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 10

Part: RIB — CRACKED (RIGHT WING L/E) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 672.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: DOUBLER — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED NAT XFS 585. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 FUSELAGE SKIN IS CRACKED AT CANTED STA 1723.076 LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7.

Part: PANEL — CORRODED (LT AILERON) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT O/B AILERON I/B WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN. REMOVED AND REPLACED WEIGHT PANEL IAW DWG 5764617U51, AND REMOVED, FABRICATED, AND REPLACED SKIN IAW DWG 5763133, AND SRM 51-3-0.

Part: RIB — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 610. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 638. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: DOUBLER — CRACKED (RT WING) · airframe 94,650 hrs · 26,672 cycles

INSPECTION TYPE:C23 RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: THRESHOLD — CRACKED (EMERGENCY EXIT)

INSPECTION TYPE:N/A, FWD RT EMERGENCY EXIT DOOR AFT LWR HAS CRACK. *S/D* TRIMMED OUT DAMAGE AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 17 AND REO G07608.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DISARM CHECK INOP. REMOVED, REPLACED AND TESTED THE EMERGENCY BATTERY PACK IAW MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK.

Part: SLIDE — LOOSE (CABIN)

LOAD SUPERVISOR OPENED MAIN ENTERANCE DOOR AND SLIDE FELL OUT. REINSTALLED EVAC SLIDE IAW MM 25-60-01 PG 202-204.

Part: SKIN — PUNCTURED (HORIZONTAL STAB)

INSPECTION TYPE:N/A, PUNCTURE IN LT HORIZONTAL STABILIZER LEADING EDGE. *S/D* REMOVED DAMAGED SECTION OF L/E SKIN PER SRM 55-2-1 BPT 92716 PC 1565 0. FABRICATED AND DRILLED REPAIR DOUBLER PER SRM 55-2-1. BAT 92716 12-13-99. INSTALLED DOUBLER PER SRM 55-2-1.

Part: WEB — CRACKED (RT MLG WW)

INSPECTION TYPE:C1, CRACK 2.5 INCHES LONG STOP DRILL LOCATED BY RT MLG DOOR SWITCH. PERM REPAIRS AT NEXT C CHECK. FABRICATED AND INSTALLED NEW WEB AND ANGLE IAW DC8 SRM 51-3-0 & 51-1-21L. TERMINATED AND SECURED WIRING TO GEAR SWITCH AND INTERPHONE JACK. OPS CHECKED SWITCH IAW DC8 MM 32-60-0.

Part: FITTING — CRACKED (BS 640)

INSPECTION TYPE:C1, CRACKED FITTING STA 640 LONG 36. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 580)

INSPECTION TYPE:C1, HARDWARE CORRODED AT STA 580 AT CUSP AREA RT SIDE FORWARD CARGO PIT. SEAT TRACK AT FS 590 IS OUT OF LIMITS. REMOVED DAMAGED SECTION IAW DC8 SRM 51-3-0, MAT ID S2772660 IAW DC8-53B-003, PO NR 293505. MANUFACTURED SEAT TRACK AND SEAT TRACK SPLICE IAW DC8 5313-003. INSTALLED SEAT TRACK AND AIR GRILL IAW DC8 SRM 51-3-0.

Part: BULKHEAD ANGLE — CORRODED (BS 70)

INSPECTION TYPE:C1 CORROSION ON AND AROUND T-ANGLE AND FASTENERS AT STA 70 BULKHEAD, RBL 28. REMOVED BOLTS IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51- 1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED ANGLE P/N NR 2615487-1 PO NR 304895. REMOVED CORROSION AROUND L-ANGLE, WITHIN LIMITS. LOCATED, DRILLED AND DEBURRED ANGLE IAW DC8 SRM 51-1-24. INSTALLED ANGLE IAW DC8 SRM 51-3-0.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:C1 AFT PIT FITTING AT FS 1180 L29L-L30L CORRODED. REMOVED FITTING, DRILLED UP NEW FITTING IAW DC8 SRM 51-3-2. INSTALL ED FITTING IAW DC8 SRM 51-1-20D.

Part: FRAME — MISDRILLED (BS 1620)

INSPECTION TYPE:C1 L-2 DOOR JAMB FWD AFT FRAME AT L17L HAS MISDRILLED HOLE. REMOVED FASTENERS TRIMMED OUT DAMAGE AND FABBED REPAIR STRAP PER TIM CO REO 06748. INSTALLED REPAIR PER DC8 SRM 51-1-21 AND REO 06748.

Part: SKIN — CORRODED (BS 1720-1740)

INSPECTION TYPE:C1, RT FUSELAGE EXTERIOR SKIN SHOWS SIGNS OF BULGING AND PULLED RIVETS BETWEEN FS 1720-1740 AT L28R-L30R. REMOVED CORRODED SECTION OF SKIN. FABRICATED REPAIR DOUBLER, FINGER DOUBLER AND FILLER IAW DC8 SRM 53-2-1, FIG 7, 51-1-8 & 51-1-21.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C1 AFT PIT FS 1240 FITTING THAT CONNECTS INTERCOSTAL TO FRAME AT L35R IS CRACKED. REMOVE AND REPLACE FITTING IAW DC8 SRM 51-1-20D.

Part: FRAME — DAMAGED (BS 1614)

INSPECTION TYPE:C1 LT AFT SERVICE DOOR FWD TORQUE BOX FWD FRAME HAS DOUBLE DRILL HOLES SPLICE IN NEW FRAME SECTION PER TIMCO REO 06750. INSTALLED PER TIMC O REO 06750.

Part: LONGERON — CRACKED (BS 600)

INSPECTION TYPE:C1, STA 600 LONGERON 34R CRACKED 6 INCHES LONG, DOT F-758. FABRICATED LONGERON SECTION IAW REO 06771 FROM MACH SHOP, REC'D FABBED REPAIR SPLICE AND DRILLED UP NEW LONGERON, SPLICE AND STRAPS IAW DC8 S RM 51-1-2 AND REO 06771. INSTALLED REPAIR SPLICE AND STRAPS IAW DC8 SRM 51-1-20D. REINSTALLED FACTORY SPLICE IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 640)

INSPECTION TYPE:C1 STA 640 LONGERON 31R CORRODED, DOT F-744. REPAIRED IAW REO 06757.

Part: LONGERON — CORRODED (BS 560-580)

INSPECTION TYPE:C1 STA 560 TO STA 580 LONG 34R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION. FABBED REPAIR STRAPS, AND INSTALLED IAW DC8 SRM 51 -1-20D. REPAIR ACCOMPLISH IAW REO 06772 FIG 3.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C1 STA 1140 35R LONGERON FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-2.

Part: FITTING — CRACKED (BS 840)

INSPECTION TYPE:C1 FRAME FITTING AT STA 840 LEFT CRACKED P/N 3779978-2. REMOVED CRACKED FITTING, FABRICATED NEW FITTING ON TIMCO ROUTINE 197 126, 50015 AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C1 BATHTUB FITTING AT FS 860 L3L CRACKED. REMOVED LONG END FITTING STA 860 L3L RECEIVED NEW FITTING PN 3779659 -501 LOCATED DRILLED AND DEBURIED IAW DC8 SRM 51-1-24. INSTALLED FITTING AT 860 STA L3L IAW DC8 SRM 51-3-00.

Part: WEB — CRACKED (BS 45-55)

INSPECTION TYPE:C1, SHACKLEBOX AND FLOOR WEB ARE CRACKED AT STA 45-55, X=-20. SHACKLEBOX REMOVED, MAT ID FOR DOUBLER REPAIR 032 2024T3 IAW DC8 SRM 53-2-0 FIG 1B PO NR 297210 MAT ID FOR WEB .025 2024T3 IAW DC8 SRM 53-3-3 FIG 5. FABBED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0 FIG 1B & 51-1-21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C1, LONGERON 10R FS 680 BATHTUB FITTING IS CRACKED. REMOVED LONGERON FITTING, LOCATED AND DRILLED UP FITTING AND INSTALLED IAW DC8 SRM 51-1-24, 51-1-21, 51-1-20D & 51-3-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C1, LONGERON 7R, FS 680 BATHTUB FITTING IS CRACKED. REMOVED LONGERON FITTING, LOCATED AND DRILLED UP FITTING AND INSTALLED IAW DC8 SRM 51-1-24, 51-1-21, 51-1-20D, & 51-3-0.

Part: BLKHD STIFFENER — CORRODED (BS 8)

INSPECTION TYPE:C1, VERTICAL STIFFENER FWD FLANGE WAS CORRODED, AFT SIDE OF STA 8 BULKHEA D AT L28R. FABRICATED STIFFENER END REPAIR ANGLES IAW TIMCO REO 06773, HEAT TREAT PERFORMED IAW TPS-1003 REV A O CONDITION TO T6. DRILLED UP IAW DC8 SRM 51-1-24 & TIMCO REO-06773. INSTALLED STIFFENER END REPAIR ANGLES IAW TIMCO REO-06773.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C1 BATHTUB FITTING AT FS 860 L5L CRACKED. REMOVED OLD FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING P/N 37 79659-501 PER DC8 SRM 51-1-20D, 51-1-21, 51-3-0, AND 51-3-1.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C1 LONGERON 3R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779659-501N IAW DC8 SRM 51-1-20D.

Part: SKIN — MISDRILLED (BS 150)

INSPECTION TYPE:.C1, RT FUSELAGE, EXTERNAL SKIN HAD 3 EXTRA HOLES IN SKIN JUST UNDER RT SERVICE DOOR FS 150 DOT E618. REMOVED DAMAGE, FABBED TITANIUM DOUBLER, REPAIR DOUBLER, TRIPLER, LONGERON AND FILLERS IAW REO 06755. DRILLED NEW CUSP FITTING IAW DC8 SRM 51-1-24. INSTALLED TITANIUM DOUBLER, REPAIR DOUBLER, TRIPLER, LONGERON FILLERS, CUSP FITTING AND BUSHING IAW DC8 SRM 51-1-20D, 51-1-25 & REO 06755.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C1 LONGERON 4R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779659-501N IAW DC8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (BS 1766)

INSPECTION TYPE:C1, AFT PRESSURE BULKHEAD AT STA 1766 LONG 11R IS CRACKED. FABBED DOUBLERS -25.032 7075-T6 & -27.063 7075-T6 PER DWG NR SRO 85300 07. FABBED ANGLE (P/N 5772638-48.063) 7075-T6, FABBED FILLERS -19.090 7075-T6, -9.050 7075-T6 & -11.063 7075-T6 PER DWG SRM 8530007. INSTALLED DOUBLER, FILLERS AND ATTACH ANGLE PER DWG NR SRO 8530007 & DC8 SRM 51-1-20 & 51-1-21D.

Part: WEB — CRACKED (BS 55)

INSPECTION TYPE:C1, FLOOR WEB CRACKED AT SHACKLEBOX, STA 55, X=-40. REMOVED FLOORBOARD TO GAIN ACCESS TO REPAIR AREA. MAT ID FOR WEB .02 5 2024T3 IAW DC8 SRM 53-3-3 FIG 5 MAT ID FOR REPAIR DOUBLER .025 202 4T3 IAW DC8 SRM 53-2-0 FIG 1B. FABBED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21 & 53-2-0.

Part: FITTING — CRACKED (BS 860)

INSPECTION TYPE:C1 LONGERON 7R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779654-501N IAW DC8 SRM 51-1-20D.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING UPPER SIDE FUEL TANK ACCESS PANEL 505F CUTOUT CRACKED 2 PLACES. MAT ID FOR EXTERNAL DOUBLER 7075-T6.160 PO NR 287514, INTERNAL DOUBLER 7075-T6.063 PO#300912, AND FILLER 7075-T6.375 PO NR 254136, IAW DC8 SRM 5 7-2-1. FABBED DOUBLERS AND FILLER IAW DC8 SRM 57-2-1. CUT OUT DAMAGED AREA IAW DC8 SRM 57-2-1. INSTALLED ALL PARTS IAW DC8 SRM 57-2-1 AND 51-1-20D. LEAK CHECK TO PERFORMED ON UPS TASK CARD NR 8000.

Part: DOOR TRACK — CRACKED (BS 35)

INSPECTION TYPE:C1, AIR CONDITIONING COMPT DOOR FWD TRACK IS CRACKED. REMOVED RIVETS, REMOVED TRACK AND REPLACED TRACK WITH RIVETS IAW DC8 S RM 51-1-21.

Part: INTERCOSTAL — CORRODED (BS 50-55)

INSPECTION TYPE:C1, FLOOR STRUCTURE INTERCOSTAL UPPER FLANGE WAS CORRODED ON LOWER SIDE, STA 50-55, X=-50. REMOVED DAMAGED AREA IAW 53-2-0. FABBED AND INSTALLED ANGLES AND FITTINGS IAW REO 06768.

Part: INTERCOSTAL — CRACKED (BS 280)

INSPECTION TYPE:C1 INTERCOSTAL AT FS 280, LONGERON 11R IS BENT, CRACKED AND CORRODED. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL IAW DAC DWG 3704510. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D.

Part: SKIN — DENTED (RT TE FLAP)

INSPECTION TYPE:C1, RT I/B FLAP LOWER SKIN HAS 2 DENTS STA XRS 74 AND XRS 172. REMOVED DAMAGE FROM FLAP, FABBED AND INSTALLED DOUBLERS IAW DC8 SRM 57 2-1 & 51-1-21.

Part: SKIN — PUNCTURE (NR 1 SPOILER)

INSPECTION TYPE:C1 PUNCTURE, UNDERSIDE NR 1 SPOILER, DOT E972. MATERIAL ID FILLER AND DOUBLER 7075-T-6.016 PO NR 271715, FABBED FILLER AND DOUBLER IAW SRM 51-1-9A. BONDED FILLER AND DOUBLER IAW DC8 SRM 51-1- 9A. REINSTALLED SPOILER IAW DC8 MM 27-61-01.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE:C1 L24L AT STA 879 HAD CORROSION FWD AND AFT. REMOVED CORROSION FOUND FITTING OUT OF LIMITS. FABRICATED NEW FITTING AND REPAIR PARTS IAW DC8 SRM 57-2-1 FIG 3B & RFTS NR N836UP-36-20407. INSTALLED FITTING AND REPAIR PARTS IAW DC8 SRM 51-1-20D & 51-3-0.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE:C1 RT LONGERON 24 FITTING AT STA 879 HAS CORROSION FWD AND AFT (REMOVED FITTING AND FOUND 2 CRACKS). REMOVED FITTING, REMOVED CORROSION. REPAIRED CRACKS ON LONG 24 WITH REPAIR ANGLES IAW DC8 SRM 53-2-2 FIG 5.

Part: SKIN — DAMAGED (LT SERVICE DOOR)

INSPECTION TYPE:C1, LT AFT SERVICE DOOR INNER LOWER STRUCTURE HAD A DOUBLE DRILLED HOLE. DOUBLE DRILLED HOLE WENT THROUGH EXISTING REPAIR. REMOVED EXISTING REPAIR DOUBLER AND EXTEND NEW DOUBLER PAST DOUBLE DRILLED HOLES. EXISTING INNER SKIN REPAIR DID NOT MEET SRM REQUIREMENTS. FABBED REPAIR DOUBLER ON INNER SKIN AND INSTALLED WITH RIVETS IAW DC8 SRM 51-1-21, 52 -2-0, 52-3-1, 51-9-0 & 52-2-2.

Part: WEB — DOUBLE DRILLED (BS 160)

INSPECTION TYPE:C1, MISDRILLED HOLE FS 160 FWD LOWER CORNER OF TORQUE BOX AND FWD PART O F FWD RT SERVICE DOOR, DOTS E761, E764, E768. FABBED WEB AND REPAIR ANGLE IAW DAC DWG 561570D & FDC8 SRM 53-2-0 FIG 1B. HEAT TREATED ANGLE IAW TPS 1003 REV A. INSTALLED REPAIR ANGLE TO CORNER PAN IAW DC8 SRM 51-1-20D. WEB AND CORNER PAN TO BE INSTALLED ON AIRCRAFT ON UPS NR 001817.

Part: SEAT TRACK — GOUGED (BS 781)

INSPECTION TYPE:C1, STA 781 SEAT TRACK G GOUGED. BLENDED SCALLOPS AT DAMAGED AREA PER DC8 SRM 51-1-8. FOUND OUT OF LIMITS. CUT DAMAGED AREA AT G SEAT TRACK FROM STA 770 TO 810 PER UPS SRM ADDENDUM DC8-5320-8309. REPLACED DAMAGED SEAT TRACK IAW UPS DC8 SRM ADDENDUM DC8-5320-8309.

Part: FRAME — CORRODED (BS 1480)

INSPECTION TYPE:C1, MAIN CABIN STA 1480 L3R TO L4R FRAME FWD FACE CORRODED. REMOVED CORROSION, FRAME FOUND TO BE OUT OF LIMITS. FABBED SPLICES IAW DC8 SRM 53-2-0, HEAT TREAT FOR T-6 CONDITION. GEN AND REC'D RFTS NR 836UP-24-20191 W/REO 06760, MAT ID S2537716-1400 7075-0 EXT PO NR 28567 8. LOCATED, REAMED, INSTALLED FRAME SEGMENTS AND SPLICES IAW DC8 SRM 51-1-24, 51-1-20D AND REO 06760.

Part: FRAME — DAMAGED (BS 1580)

INSPECTION TYPE:C1 STA 1580 R/S 26 ABOVE CUSP FRAME AND GUSSETT HAS DRILL DAMAGE. REMOVED DAMAGED GUSSETT AND FASTENER IAW DC8 SRM 51-21-1. REMOVED DAMAGE FROM FRAME IAW REO 06735. FABBED AND INSTALLED NEW GUSSET AND REPAIR ANGLE IAW DAC DWG 9751061, REO 06735, AND DC8 SRM 51-1-20D AND 51-1-21.

Part: FRAME — GOUGED (BS 1660)

INSPECTION TYPE:C1, FRAME FACE GOUGED IN RADIUS AT STA 1660 LONG 4L. TRIMMED OUT DAMAGE AND REPAIRED IAW REO-06735.

Part: SEAT TRACK — CORRODED (BS 1270)

INSPECTION TYPE:C1, STA 1270 SEAT TRACK G HAS CORROSION DOWN CENTER. FABRICATED SPLICE CHANNEL IAW DC8 5320-8309 APP-B. DRILLED AND LOCATED SEAT TRACK SPLICES AND SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED SEAT TRACK SPLICES & SEAT TRACK IAW DC8 SRM 51-3-0.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION TYPE:C1, RT AFT DOOR HAS CRACKED FRAME AT UPPER FWD CORNER. OPENED INNER WEB AND REMOVED CRACKED DOOR BEAM. FABRICATED NEW DOOR BEAM (P/N 5772639-21) IAW DC8 SRM 51-1-21, INSTALLED IAW DC8 SRM 51-1-2 0D, 51-1-21 AND REINSTALLED INNER WEB IAW DC8 SRM 51-1-21.

Part: SEAT TRACK — GOUGED (BS 600)

INSPECTION TYPE:C1, STA 600 SEAT TRACK F SCALLOPS GOUGED BLENDED DAMAGED IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED OUT OF LIMITS SECTION STA 570-610 IAW DC8 SRM UPS ADDENDUM DC8-53B-003.

Part: FRAME — DAMAGED (BS 1580)

INSPECTION TYPE:C1, STA 1580 LONG, L19L TO L14L HAD DRILL DAMAGE. CLEANED UP DAMAGED AREA AND REPAIRED FRAME IAW TIMCO DWG DC8 53-0229, REO 06737 AND UPS COVER SHEET DC8 53-2711.

Part: FRAME — DAMAGED (BS 1600)

INSPECTION TYPE:C1 STA 1600 19 ABOVE CUSP, FRAME AS DRILL DAMAGE IN RADIUS OF FLANGE GEN RFTS N836UP-03-20183 ON 9-7-99, REC'D RFTS 9-8-99. MATERIAL VERIF ICATION 7075-0.071 PO NR 296823, FABBED FILLER AND SPLICES IAW DC8 SRM 53 -2-0; LOCATED, DRILLED AND TRIMMED FILLER AND SPLICES IAW DC8 SRM 53-2-0 . INSTALLED FILLER AND SPLICES IAW DC8 SRM 53-2-0, 51-1-20D.

Part: SEAT TRACK — GOUGED (BS 160)

INSPECTION TYPE:C1, STA 160 SEAT TRACK F SCALLOPS GOUGED IN TRACK OUT OF LIMITS. REMOVED DAMAGED TRACK, FABBED AND INSTALLED REPLACEMENT SECTION IAW DC8 SRM 53-2-3.

Part: BATTERY — DISCHARGED (COCKPIT)

COCKPIT EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW M/M 33-50-01, OP'S CK NORMAL OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS ARE ON CONTINUOUSLY IN THE ARM POSITION AND WILL NOT DISARM CHECK. REMOVED AND REPLACED EEL CIRCUT BREAKER REF 20-50-00, OPS CHECK GOOD W/REF TO MM 33-50-01.

Part: FITTING — CORRODED (BS 1160)

INSPECTION TYPE:C/CK, Z FITTING AT L34R L33R AT FUSELAGE STATION 1160 HAS EXTENSIVE CORROSION. REMOVED Z FITTING CUT NEW 2 FITTINGS AND FABBED REPAIR ANGLES IAW DC8 SRM 53 2 0. TRANSFER EXISTING HOLES TO NEW 2 FITTINGS IAW DC8 SRM 51 3 2. ALODINED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51 1 8. INSTALLED 2 FITTING AND REPAIR ANGLES IAW DC8 SRM 51 1 20D.

Part: LONGERON — CORRODED (BS 190-380)

INSPECTION TYPE:C/CK, LONGERON 35 LEFT STA 190 380 CORRODED. REMOVED L35L. FOUND TO BE CORRODED BEYOND LIMITS, RECEIVED NEW LONGERON PART 9754913 324 LOCATED AND DRILLED LONGERONS IAW DC8 SRM 51 3 2. INSTALLED WITH HI-LOKS IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (BS 1228)

INSPECTION TYPE:C/CK, Z FITTING STA L35R L34R FS 1228 IS CRACKED AND CORRODED. REMOVED OLD FITTING HOLES IN NEW FITTING IAW DC8 SRM 51 1 24. ALODINED AND PRIMED HOLES IAW DC8 SRM 51 1 8. INSTALLED NEW FITTING IAW DC 8 SRM 51 1 20D.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C/CK, Z FITTING CORRODED AT FUSELAGE STATION 280 34R- 35R. REMOVED OLD FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 1 20D. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: SPLICE — CRACKED (BS 1050)

INSPECTION TYPE:C/CK, STA 1050, L31R SPLICE CRACKED. REMOVED SPLICE IAW DC8 SRM 51 1 20D AND DC8 SRM 51 3 1, MATERIAL ID 3750257-1 FITTING IAW DAC DWG 5750322, ALODINED AND PRIMED MATING AR EA IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE:C/CK, Z FITTING CORRODED STA 340, LONGERON 35L TO 36. REMOVED OLD FITTING IAW DC8 SRM 51 1 20D. RECEIVED NEW PART PN 37558 2201N, LOCATED AND DRILLED NEW PART, IAW DC8 SRM 51 3 2 ALODINED AND PRIMED HOLE IN NEW PART IAW DC8 SR, 51 1 8, INSTALLED NEW PART IAW DC8 SRM 51 1 20D.

Part: FITTING — CORRODED (BS 270)

INSPECTION TYPE-C/CK, ZEE FITTING STA 270, LONGERON 33-34 RIGHT CORRODED. REMOVED FITTING, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 51-3-2, 51-1-20D, AND 51-1-8.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE-C/CK, ZEE FITTING CORRODED, STA 300, LONGERON 32-33 LEFT. REMOVED FITTING, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 450)

INSPECTION TYPE-C/CK, FUSELAGE STATION 450 LONGERON 31 LEFT TP 31 RIGHT FINGER DOUBLER CORRODED. REMOVED DOUBLER, FABBED NEW ONE IAW DAC DWG 5755271. INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE-C/CK, REMOVED AND REPLACED FWD INTERNAL SKIN DOUBLER. REMOVED DOUBLER, FABBED NEW ONE IAW DC8 SRM 51-1-24. NEW DOUBLER TO BE INSTALLED ON UPS NR 522669.

Part: FITTING — CORRODED (CENTER WING)

INSPECTION TYPE:C/CK CORROSION ON CENTER WING SPAR FITTING FUSELAGE STATION 855 INSIDE LEFT HAND WHEEL WELL BELOW UPPER CORNER. REMOVED CLIP, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 57 2 3, THIS CLIP INSTALLED WITH -3 DOUBLER AFTER CORROSION REMOVAL IAW DC8 SRM 51 1 8, 51 1 20D, AND 51 3 0.

Part: CLIP — CORRODED (BS 855)

INSPECTION TYPE-C, CORROSION ON CENTER WING SPAR FITTINGS FS 855 INSIDE LT W/W BELOW UPPER CORNER. REMOVED CLIP, DRILLED AND INSTALLED IAW DC8 SRM 57-2-3.

Part: LONGERON — CORRODED (BS 190-220)

INSPECTION TYPE:C/CK FWD LOWER CARGO, LONG 35 R CORRODED STA 190 TO 220. REMOVED I/B AND O/B SECTIONS OF LONGERON 35 RIGHT, LONGERON CORRODED BEYOND LIMITS IAW DC8 SRM 53 2 0. LOCATED DRILLED AND DEBURRED LONGERON IAW DC8 SSRM 51 1 24 AND INSTALLED IAW DC8 SRM, 51 1 20D.

Part: SKIN — CORRODED (BS 370)

INSPECTION TYPE:C/CK, FWD LOWER CARGO SKIN BULGED AND CORRODED AT STA 270 RIGHT OF L36. REMOVED LOWER BELLY SKIN STA 190 450 AND DOUBLERS DRILLED COUNTER SUNK AND INSTALLED NEW SKIN AND DOUBLERS IAW DC8 SMR 51 1 4, 51 1 20, 51 1 20D.

Part: FITTING — CORRODED (BS 1170)

INSPECTION TYPE-C/CK, ALC C-3 DOOR LOWER JAMB BACKUP FITTING CORRODED, STA 1170. REMOVED Z-FITTING, DRILLED AND INSTALLED IAW DC8 SRM 51-1-8, AND 51-1 20D, 2 NEW FITTING. REMOVED CORROSION FROM A THIRD FITTING, ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: LONGERON — CORRODED (BS 220-240)

INSPECTION TYPE:C/CK, FWD LOWER CARGO L36 CORRODED, STA 220 TO 240. REMOVED CORROSION, REMOVED LONGERON BOTH HALVES AND LOCATED AND DRILLED NEW LONGERON HALVES IAW DC8 SRM 51 1 8, 53 2 0, 51 1 24, AND INSTALLED IAW DC8 SRM 51 1 20D.

Part: LONGERON — CORRODED (BS 220-240)

INSPECTION TYPE-C/CK, FWD LOWER CARGO L36 CORRODED, STA 220 TO 240. REMOVED CORROSION, REMOVED LONGERON BOTH HALVES AND LOCATED AND DRILLED NEW LONGERON HALVES IAW DC8 SRM 51-18, 53-2-0, 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (WS 700)

INSPECTION TYPE-C/CK, CRACKS AT 2 SCREW HOLES, LEFT HAND LEADING EDGE AT XFS 700, BOTTOM OF LEFT WING. FABBED REPAIR DOUBLER AND INSTALLED WITH RIVETS IAW UPS EO 5720 4082.

Part: LIGHTS — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS ILLUMINATED IN FLIGHT WITH NO SWITCH ACTIVATION. *S/D* REMOVED AND REPLACED EMERG BATTERY PACK PER M/M 33-50-01, ON (P/N 5708458-503) (S/N 166), OFF (P/N 5708458-503) (S/N FTL 244).

Part: LINK ASSY LOCK — FAILED (NLG DOOR)

INSPECTION TYPE-C, GEAR NOT LATCHED LIGHT ILLUMINATED, CONFIRMED OPEN BY LOUD AIR NOISE. COMPLETED QRH DID NOT FIX PROBLEM. FOUND L-FWD NOSE GEAR DOOR HANGING OPEN DUE TO DEFECTIVE LOCK ON LINK ASSY. REMOVED AND REPLACED LINK PER MM 32-22-02. PERFORMED GEAR SWING ALL OPS CHECK NORMAL. (P/N 5-1036) (S/N 312) ON, (P/N 5-1036) (S/N 462) OFF.

Part: SKIN — CRACKED (LT WING LE)

INSPECTION TYPE-C, LT LEADING EDGE ATTACHMENT HOLE HAVE CRACKS IN NR 7, 8, 9, 10 AND 11. REPAIRED PER DRAWING NR J060232.

Part: SKIN — CRACKED (RT WING LE)

INSPECTION TYPE-C, RT LEADING EDGE ATTACHMENT HOLE HAVE CRACKS IN NR 1, 2, 4, 7, 8, 10 AND 11. REPAIRED PER DRAWING NR J060232.

Part: SKIN — CORRODED (BS 1766-1790)

INSPECTION TYPE-C, AFT FUSELAGE SKIN LT SIDE STA 1766 TO 1790 L10L AT LAP SEAM HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, MATERIAL LOSS EXCEED 20 PERCENT. REMOVED DAMAGE IAW DC8 SRM 53-2-1, MATERIAL ID FOR REPAIRS ARE IAW DC8 53-5-3 FIG 1 AND 53-21-1. FABD DOUBLERS AND FILLERS IAW SRM 51-1-8, INSTALLED REPAIRS WET WITH SEALER IAW 51-1-16, 51-1-17, 51-1-20D AND 51-1-20B.

Part: PANEL — CRACKED (CENTER WING)

INSPECTION TYPE-C, 506A RT WING CRACKED PNL LAND NR 4 MAIN. REMOVED CRACKED AREA OF PNL AND FABRICATED INTERNAL AND EXTERNAL DOUBLERS, FILLERS IAW SRM 57-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ALL REPAIR PARTS IAW DC8 SRM 51-1-20D AND 51-1-20A.

Part: BOOST PUMP — INOPERATIVE (NR 1 ENGINE)

CREW REPORTED NR 1 ENGINE FLAME-OUT AT FLT 370 (NO FUEL FLOW NOTED DURING RESTART ATTEMPT). INSPECTED INLET AND EXHAUST SECTIONS. ALSO, INSPECTED CHIP DETECTORS. RAN ENGINE AT IDLE AND 82 PERCENT N2. NO PROBLEMS DETECTED. ENGINE OK FOR CONTINUED SERVICE. NOTE: REMOVED AND REPLACED NR 1 ALT FUEL BOOST PUMP.

Part: SKIN — CRACKED (FUSELAGE)

WHILE ON GROUND, MAINTENANCE FOUND LT AFT SERVICE DOOR CUT OUT HAS AFT UPPER RADIUS CRACKED. REPAIRED IAW DC8-5330-4067A.

Part: BULKHEAD — CRACKED (BS 683)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BULKHEAD AT STA 683 BETWEEN STRINGERS 30R-31R. INSTALLED REPAIR PER SRM 53-2-5.

Part: SKIN — CRACKED (NLG WW CUTOUT)

WHILE IN 'B' CHECK, MAINTENANCE FOUND A CRACK IN FUS SKIN AFT LEFT CORNER OF NOSE WHEEL WELL CUT OUT. REPAIRED PER UPS EO DC8-5330-4154A.

Part: SKIN — CRACKED (LT ELEVATOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LEFT ELEVATOR TOP SKIN O/B OF NR 3 HINGE, 8 INCHES AFT OF T-CAP. REPLACED PER SRM 55-2-1.

Part: ANGLE — CRACKED (NR 1 PIT)

WHILE IN 'B' CHECK, MAINTENANCE FOUND A CRACK IN FWD VERTICAL 'V' ANGLE NR 1 PIT, LWR SECTION BETWEEN BOLT HOLES. REPAIRED PER UPS EO DC8-5310-6773A.

Part: BULKHEAD — CRACKED (BS 683)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BULKHEAD AT STA 683 BETWEEN STRINGERS 30L-31L. INSTALLED REPAIR UPS EO DC8-5310-6755A.

Part: BELTFRAME — CRACKED (BS 240)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BELTFRAME STA 240, LONGERON 34-35L. INSTALLED REPAIR PER SRM 53-2-0.

Part: LONGERON — CRACKED (BS 340)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LONGERON 21L FWD SIDE OF STA 340. INSTALLED REPAIR PER UPS EO DC8-5310-6682A.