N744UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

NO EMERGENCY LIGHTS ON PREFLIGHT CHECK, COCKPIT INSTRUMENT FLOODS AND COCKPIT DOME. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK NORMAL. REF DC8 MM 26-00.

Part: FLOORBEAM — CORRODED (FS 80 RBL 57) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 CORROSION ON FLOORBEAM LOWER T-CAP EXFOLIATED STA -80 RBL 54. REMOVED OUT OF LIMITS CORROSION AT STA -80 RBL 57 IAW SRM 51-2-1. FABRICATED AND INSTALLED REPAIR PARTS AT STA -80 RBL 57 IAW SRM 51-2-1 FIG 1, AND TR 51-130.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 AFTER REMOVAL OF CORROSION, FOUND CORROSION OUT OF LIMITS ON FRAME AT STA 1973, LT & RT. REMOVED FRAME SPLICE AT STA 1973 FWD OF TAIL NAV LIGHT IAW SRM 51-1-21. FABRICATED, AND INSTALLED REPAIR FRAME SPLICES AT STA 1973 LT & RT IAW SRM 51-1-4, 53-02-00 FIG 6, AND SRM 51-1-21.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 SUPPORT FITTING CRACKED AT STA 980 RBL 24 4 INCHES BELOW CABIN SEAT TRACK. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SPAR CAP — CRACKED (WING) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C3 POSSIBLE CRACK AT NR 4 ALT BETWEEN LWR FRT SPAR CAP FLANGE AND STRINGER 64 JUST OUTBOARD XRS428. REMOVED, FABRICATED AND INSTALLED SPAR CAP FLANGE IAW SRM 51-1-20D & DWG 3644046.

Part: STIFFENER — CRACKED (LT WING) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 RADIOGRAPHIC INSP DETECTED A CRACK ON THE LT WING AT STA XRS437.00 VERTICAL STIFFENER IN THE LEADING EDGE. REMOVED REPAIR FROM VERTICAL STIFFENER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER, AND REPAIR ANGLE AT LT WING STA XRS 437.00 VERTICAL STIFFENER IAW DWG 5770170-5, AND SRM'S 57-02-00 FIG 2, 51-1-4, AND 51-1-20D.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 LT HORIZ STAB L/E UPPER SKIN CRACKED AT STA XFS 60. CUT OUT DAMAGED AREA ON HORIZ STAB LT L/E UPPER SKIN AT STA XFS 60 IAW SRM 55-02-01-0 FIG 4. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER ON LT HORIZ STAB L/E UPPER SKIN STA XFS 60 IAW SRM 55-02-01-0 FIG 4.

Part: FITTING — CORRODED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON END FITTING AT STA 70 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 70 L35R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON LONGERON L35R STA 50-70. REMOVED LONGERON L35R AT STA 50-70 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON L35R AT STA 50-70 IAW DWG 3702969, AND SRM 51-1-21, AND 51-1-20D.

Part: WINDOW FRAME — CORRODED (FS 117) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 RIGHT & LEFT WINDOW FRAME Z-ANGLES (CENTER WINDSHIELD) ARE CORRODED AND PITTED. REPAIRED CENTER WINDSHIELD Z-ANGLE IAW SAA EA 008-5310-01-A0570 UPS EO DC8-5310-25945-A, BAC MSG 1-269510850, AND FAA FORM 8100-9.

Part: LONGERON SPLICE — CRACKED (FS 1040 L31L) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 C-PIT STA 1040 L31L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1040 L31L IAW SRM 51-01-20D, 51-03-02.

Part: PRESSURE PANEL — CORRODED (FS 80 LBL24) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 COCKPIT SUBFLOOR HORIZ PRESS PANEL STA -80 LBL 24 HAS EXFOLIATION CORROSION. REPAIRED COCKPIT SUBFLOOR HORIZ PRESS PANEL AT STA -80 LBL 24 IAW SAA EA 008-5330-01-A0608, UPS EO DC8-5330-26007-A, BAC SERVICE MSG 1-275991347, AND FAA FORM 8100-9. THIS REPAIR MUST BE REPLACED AT 24,000 CYCLES, WITH REPEAT INSPECTIONS AT 4,000 CYCLES AFTER A/C LEAVES HEAVY MAINT.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 LEFT HORIZ STAB LEADING EDGE VERY INBOARD UPPER T-ANGLE CRACKED. CUT OUT DAMAGED AREA ON INBOARD UPPER T-ANGLE ON LT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, RECEIVED, LOCATED, DRILLED UP AND INSTALLED T-ANGLE FITTING ON THE LEFT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, AND SRM 51-3-0.

Part: BOSS — CORRODED (RT MLG) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 RIGHT MAIN LANDING GEAR RETRACT PIN BOSS ID CORRODED. RIGHT MLG RETRACT PIN BORE BOSS CORROSION IS OUT OF LIMITS IAW EO DC8-3230-0450-O. RIGHT MLG TO BE REMOVED AND REPLACED ON NRC 949517 AND TC 9132-3.

Part: SPAR — CRACKED (WING) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 FOUND CRACK ON LOWER CENTER SPAR CHORD AND WEB JUST I/B OF XRS 255 NR 1 MAIN TANK. REPAIRED CRACKED SPAR CHORD AND WEB AT NR 1 MAIN TANK JUST I/B OF XRS 255 IAW SAA EA# 008-5710-01-A0595, UPS EO DC8-5710-25944-A, BAC SERV MSG NR 1-270145772, AND FAA FORM 8100-9 . THIS REPAIR IS TIME LIMITED PENDING A DAMAGE TOLERANCE ANALYSIS OF 24 MONTHS IN WHICH DTA IS INCORPORATED.

Part: FLOORBEAM — CRACKED (FS 240 LBL 36) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 FLOORBEAM VIEWED FROM A-PIT STA 240 LBL 36 HAS A 9 INCH CRACK. REPAIRED FLOORBEAM AT STA 240 LBL 36 IAW SAA EA008-5310-01-A00586 UPS RAA DC8-53-20605-A, BAC MSG 1-271080190, AND FAA FORM 8100-9.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C3 A-PIT FWD BULKHEAD STA 70 RBL 24 SUPPORT FRAME CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT IAW SRM 51-1-21, 51-1-20D AND DWG 5613064.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 HFEC INSP DETECTED A .156" CRACK ON THE UPPER FWD CORNER OF THE B-PIT DOOR JAMB. CUT OUT DAMGED AREA AT THE UPPER FWD B-PIT DOOR JAMB IAW SRM 53-2-0 FIG 20. FABRICATED AND INSTALLED FILLERS, DOUBLER AND TRIPLER AT THE UPPER FWD B-PIT DOOR JAMB CORNER IAW SRM 53-2-0 FIG 20. THIS REPAIR REQUIRES A UPS MPI AND DAMAGE TOLERENCE INSP INITIAL AT 12,000 CYCLES AND REPETITVE INSP AT EVERY 4,000 CYCLES IAW TR NR 543-186.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 L1 DOOR INTERCOSTAL CRACKED 1.75 INCH, UPPER AFT CORNER OF DOOR. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT STA 70 LBL 60 L1 DOOR AFT CORNER INTERCOSTAL IAW SRM 52-02-00-0, AND SRM 51-01-08.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 L1 DOOR INTERCOSTAL CRACKED .625 INCH UPPER FWD CORNER OF DOOR. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT L1 DOOR UPPER FWD CORNER STA 25 L11L IAW SRM 52-02-00-0 FIG 002 AND SRM 51-01-21D.

Part: SHEAR TIE — CRACKED (FS1795 L3R) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 60 COMPT CEILING SHEARTIE BROKEN AT EOP RT SIDE STA 1795 L3R. REMOVED CRACKED SHEARTIE AT STA 1795 L3R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT SHEARTIE AT STA 1795 L3R IAW DWG 5612148, AND SRM'S 51-03-02-0 FIG 55, AND 51-1-20D.

Part: FITTING — BROKEN (FS 1770 L10L) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 END FITTING BROKEN AT STA 1770, L10L. REMOVED AND REPLACED END FITTING AT STA 1770, L10L IAW SRM 51-1-20D AND SRM 51-3-0.

Part: FITTING — CORRODED (BS 1755-1766) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON FITTING AT BASE OF APB CENTERLINE BEAM, LT SIDE L36 STA 1755-1766. REMOVED FABRICATED AND REPLACED FITTING AT L36 STA 1755-1766 IAW SRM 51-1-20D AND DWG 5753522.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 SEAT TRACK SCALLOPS GOUGED AT STA 958 LBL 24 IN MAIN CABIN. CUT OUT DAMAGED AREA OF SEAT TRACK AT STA 958 LBL 24 IAW SRM 53-02-03 FIG 6D. INSTALLED SEAT TRACK PLUG REPAIR AT STA 958 LBL 24 IAW SRM 51-3-0.

Part: RIB — CRACKED (LT WING) · airframe 76,629 hrs · 50,136 cycles

INSPECTION TYPE:C2 LEFT WING UPPER LEADING EDGE RIB CRACKED AT XFS 659. STOP DRILLED CRACKED RIB AT WING STA XFS 659 IAW SRM 51-1-21, AND SRM 57-02-00. FABRICATED AND INSTALLED REPAIR DOUBLER AT WING STA XFS 659 IAW SRM 57-02-00, AND SRM 51-1-20D.

Part: SLIDE — BROKEN (COCKPIT)

EMERGENCY ESCAPE SLIDE FELL OUT OF CONTAINER. SLIDE LANYARD TANG BROKEN. REMOVED AND REPLACED EVAC SLIDE CONTAINER IAW 25-60-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT, DISARM CHECK LIGHT INTERMITTENT INOP. RELAMPED EMERGENCY EXIT LIGHT PER M/M 33-10-00. OPS CHECK GOOD.

Part: HOSE — DEFECTIVE (HYD SYSTEM)

ON CLIMBOUT HYDRAULIC QUANTITY DECREASED. AOM PROCEDURE WAS COMPLIED WITH AND RESERVOIR WAS NOT EMPTY. FOUND LT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE HOSE BROKEN. REPLACED WITH TEMPORARY HOSE REFERENCE GMM 3-24-1- D329494 ASSIGNED. R&R PRESS LINE WITH SERVICEABLE PERM LINE PER MM 20-12-02-2 LEACK CHEC K PER MM 29-00-00 & 32-32-04-5

Part: WHEEL — CORRODED (MLG)

CORROSION ON NR 5 MAIN LANDING GEAR AXLE - INNER WHEEL BEARING. CHROME W/SOME PITTING. R/R NR 5 MLG WHEEL & TIRE ASSY. IAW MM REF 32-40-01-2. BLENDED AREA APPLIED FR PRIMER TO BLENDED AREA; REINSPECT EVERY 70 DAYS PERM. REPAIR AT OR BEFORE C CK.

Part: GAUGE — UNSERVICEABLE (EVAC SLIDE)

INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE GAUGE IS UNREADABLE. VERIFY IF SLIDE PRESSURE IS SERVICEABLE PER TC 0231, STEP 1D SLIDE PRESSURE IS SERVICEABLE PER TC 231, 1D.

Part: STRUCTURE — PUNCTURED (FUSELAGE)

INSPECTION TYPE:N/A PINHOLE PUNCTURE PIT 33 STA 1240 LEFT SIDE. PERFORMED INTERIM REPAIR PER EO DC8-5320-8724 APPENDIX A.

Part: SKIN — CRACKED (NR 4 PYLON)

NR 4 PYLON O/B SKIN CRACKED APPROX 1 INCH LONG OB SIDE APPROX 6 INCHES AFT OF FWD BOX BULKHEAD. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5430-23086A. PERMANENT REPAIR WITHIN 10 FLT CYCLIES, D312151 ASSIGNED. ACCOMPLISHED PERMANENT REPAIR PER EO DC8-5430-23086B. THIS CLEARS D312151.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

BATHTUB FITTING CRACKED AT STA 1200 L34R-L35R. FITTING HAD BEEN PREVIOUSLY REPLACED. REMOVED AND RETAINED SPLICE PLATES FROM CRACKED FITTINGS REF SRM 51-1-20D. CUT REPLACEMENT FITTING, DRILLED, TREATED, AND PRIMED PER SRM 53-2-0 FIG2D. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 2D.

Part: WEB — CORRODED (CARGO BAY) · airframe 75,722 hrs · 49,419 cycles

TORQUE BOX WEB CORRODED BEYOND LIMITS AT STA 1200, LONG 36. REMOVED FASTENERS TO FOM REF SRM51-1-20D. REMOVED CORROSION REF SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL RANGE 0.125" - 0.088" REF NDT SPM 04-00-06. FABRICATED REPAIR DOUBLER FROM SHT7075T6-.160" REF SRM 53-2-0 FIG23, 53-2-0 FIG25 DWG9754945, 3753772. INSTALLED REPAIR REF SRM51-1-8, 51-1-21, 51-1-20D

Part: DOUBLER — CRACKED (RT LE AUX TANK) · airframe 75,722 hrs · 49,419 cycles

RT WING L/E INTERNAL DOUBLER (AUX TANK) CRACKED AT STA.182.502. FABRICATED REPAIR DOUBLER FROM SHT7075T6/0.125 AND INSTALLED SAME PER SAA SK744-520, SRM 51-1-8, 51-1-26, 51-1-20D.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

GUSSET CRACKED AT STA 460 ABOVE LONG 31 R. REMOVED CRACKED GUSSET REF SRM 51-1-21. FABRICATED REPLACEMENT GUSSET FROM SHT7075T6/.080 REF DWG 9758907. INSTALLED SAME REF SRM 51-1-8, AND 51-1-20D

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT RT AFT HEAT EXCHANGER CUT OUT LOWER AFT CORNER. REPAIRED PER EO DC8-5330-4732-D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

STA 70 FRAME CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED CORROSION, TREATED AND PRIMED SITE PER SRM51-1-8. FABRICATED REPAIR DOUBLER FROM SHT7075O-.080 PER EO DC8- 5310-11728/DWGDC8-53A-011. HEAT TREAT TO T6 PER DPS7.00 INSTALLED REF SRM 51-1-20D, 51-1-8, EOD C8-5310-11728.

Part: SHEAR TIE — CRACKED (CARGO BAY) · airframe 75,722 hrs · 49,419 cycles

CRACKED SHEAR TIE AT LONG 21L STA 460. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-1-20D, 51-9-0 FIG 68A, DWG3750891, AND DPS7.00-1.

Part: SHEAR TIE — CRACKED (CARGO BAY) · airframe 75,722 hrs · 49,419 cycles

SHEAR TIE CRACKED AT STA 440 LONG 21L. REMOVED, FABRICATED, AND INSTALLED. REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-9-0 FIG 88A, 51-1-20D DWG3750891, AND DPS7.00-1.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

LONG 31R SPLICE FITTING CRACKED AT STA 1050. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8, 51-1-22, 51-3-2.

Part: ATTACH FITTING — CRACKED (CARGO BAY) · airframe 75,722 hrs · 49,419 cycles

INSPECTION TYPE: C3, INTERCOSTAL FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35L. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8 NDT-SPM06-10-01.001.

Part: GUSSET — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

CRACKED GUSSET IN LT WING CENTER L/E NEAR XW371. REMOVED CRACKED GUSSET REF SRM 51-1-21. FAB REPLACEMENT FROM SHT 7075T6-.063 REF DWG5769589 AND SRM 51-1-8. INSTALLED GUSSET REF SRM 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LEFT WING CENTER L/E RIB CRACKED AT XW408. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG 1, 57-3-1 FIG 4, 51-1-8, 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

C3 LT WING CENTER L/E RIB CRACKED AT UPPER AFT END STA XW398. STOP DRILLED CRACK NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG2, 57-3-1, FIG4, 57-3-1 FIG2, 51-1-8.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

CRACKED RIB IN LT CENTER L/E NEAR STA XW322. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR FROM SHT7075T6, .040 AND .032 THICK, AND INSTALLED SAME REF SRM 51-1-8, 57-2-0, 57-3-1.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING CENTER L/E RIB CRACKED AT XW429 UPPER RIB. STOP DRILLED CRACK, NDT VERIFIED TERMINATION PER SPM 06-10-01.001. FABRICATED STACKED ANGLE REPAIR DOUBLERS FROM SHT7075T6/.040 AND .050 THICK REF SRM 57-3-1 FIG 4 ITEM C, 57-2-0 FIG2. INSTALLED PARTS REF SRM 51-1-20D, 51-1-8, 57-2-0.

Part: RIB — CRACKED (RT WING) · airframe 75,722 hrs · 49,419 cycles

RT WING O/B L/E RIB CRACKED NEAR XFS722.50. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE REPAIR ANGLE FROM SHT7075T6-.063 AND INSTALLED SAME REF SRM 57-3-3, 57-2-0 FIG2, 51-1-8, 51-1-21.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 75,722 hrs · 49,419 cycles

RT WING L/E INTERNAL DOUBLER CRACKED AT DRAN HOLE, STA XFS329. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6/.090 PER SRM 57-3-0 FIG 12. TREATED AND PRIMED REF SRM 51-1-8. REMOVED AND REPLACED PART PER SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

SPLICE FITTING CRACKED AT STA 1270, LONG 34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-8, 51-3-2, 51-1-20D.

Part: LONGERON — CRACKED (FUSLEAGE) · airframe 75,722 hrs · 49,419 cycles

LONGERON CRACKED AT STA 1742. CUT OUT CRACKED PORTION OF LONG AT SHEAR TIE. NDT VERIFIED ALL DAMAGE REMOVED REF SRM53-2-2 FIG 11 AND SPM06-10-01.001. FABRICATED FILLER AND REAPIR ANGLE FROM SHT7075T6/.063 AND S2645517 EXTRUSION AND INSTALLED SAME REF SRM 53-2-2 FIG11 51-1-20D.

Part: LONGERON — CRACKED (MAIN CABIN) · airframe 75,722 hrs · 49,419 cycles

LONG 15L CRACKED AT STA 1702. REMOVED LONG 15L FROM STA 1695-1707 REF SRM53-2-0FIG10. FAB LONG SECTION FROM S1616757 EXTRUSION AND 4 SPLICE STRAPS FROM SHT7075T6 .080" REF SRM 53-2-2 FIG10 AND 53-5-3. INSTALLED PARTS AND TWO REPAIR SPLICES PER SRM 51-1-20D, 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

INSPECTION TYPE: C3, LONG 15R CRACKED AT FRAME ATTACHMENT, STA 1755. CUT OUT LONG SECTION FROM STA 1750-1760, REMOVED END FITTING AT STA 1760 & SHEAR TIE AT 1755. FAB LONG SECTION FROM S1616757 EXTRUSION, & TWO SPLICE STRAPS FROM SHT7075T6/.080 REF SRM 53-2-2 FIG 10, 51-1-8, 53-5-3 ASSEMBLED REPAIR & REINSTALLED PARTS & REPAIR SPLICE FITTING REF SRM 53-2-2 FIG 10, 51-1-20D, 51-1-8, DPS4.707, NDT-SPM06-10-01.001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

INSPECTION TYPE: C3, LONGERON 16R CRACKED AT STA 1750 FRAME ATTACH FASTENERS. REMOVED END FITTING, ATTACH CLIP, AND LONGERON SECTION FROM STA 1750-1 TO 1760. FAB REPLACEMENT LONG SECTION FROM S1616757 EXTRUSION & 2 SPLICE STRAPS FROM SHT7075T6/.080 INSTALLED ALL PARTS & REPAIR SPLICE FITTING. ALL MAINT PER SRM 53-2-2 FIG 10, 53-5-3, 51-1-8, 51-1-20D, DWG 5644130, DPS4.707, NDT-SPM06-10-01.001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

LONG 9R CRACKED AT STA 1735 FRAME ATTACH. CUT OUT DAMAGE, NDT VERIFIED PER SPM 06-10-01.001. FABRICATED FILLER FROM SHT7075T6/.063 AND DOUBLER FROM S2645716 EXTRUSION PER SRM 53-2-2 FIG 11. INSTALLED PARTS REF SRM 51-1-8, 51-1-20D, 51-3-0.

Part: RIB — CRACKED (RT WING) · airframe 75,722 hrs · 49,419 cycles

RT WING L/E RIB CRACKED AT XFS828.75. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 PER SRM 57-2-0 FIG 2. INSTALLED REPAIR PER SRM 57-2-0 FIG 2, 51-1-8, 57-3-1, 51-1-21, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING CENTER L/E LOWER RIB CRACKED AT AFT END, STA XW408. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR DOUBLERS FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-3-1 FIG 4, 57-2-0, 57-3-1, 51-1-21, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 75,722 hrs · 49,419 cycles

C3 RT WING CENTER L/E RIB CRACKED AT AFT END, STA XFS347. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6 .040 AND .032 AND INSTALLED SAME REF SRM 57-3-1, 57-2-0, 51-1-8,

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING L/E RIB CRACKED AT LOWER AND UPPER ENDS, STA835. STOP DRILLED CRACKS. NDT VERIFIED BOTH REF SPM 06-10-01.001. FABRICATED UPPER REPAIR FROM 7075T6-.050 AND FABRICATED LOWER REPAIR FROM S25972423 EXTRUSION REF SRM57-3-1, 57-2-0. INSTALLED REPAIRS REF SRM 57-2-0, 51-1-8, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING L/E LOWER RIB CRACKED AT END, STA 753.75. STOP DRILLED CRACK, NDT VERIFIED PER SPM06-10-01.001. FABRICATED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D.

Part: DOOR FRAME — CRACKED (PLUG DOOR) · airframe 75,722 hrs · 49,419 cycles

INSPECTION TYPE:C3 RIGHT FWD OVERWING PLUG DOOR FRAME CRACKED AT FWD UPPER CORNER. STOP DRILLED CRACK, NDT VERIFIED PER NDT-SPM06-10-01.001. REMOVED ADJACENT DOUBLER PER SRM 51-1-20B. WELDED CRACK PER DPS10.225. NDT WELD PER DPS4.707, NO DEFECTS. TREAT AND PRIME PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING L/E RIB CRACKED AT LOWER AFT END, STA860. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FAB REPAIR ANGLE FROM S25972423 EXTRUSION. INSTALLED REPAIR PER SRM 57-2-0, 51-1-8, 51-1-21D, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING L/E RIB CRACKED AT STA 728 UPPER AFT END. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D.

Part: FITTING — CRACKED (LT WING) · airframe 75,722 hrs · 49,419 cycles

LT WING STA 419 T/E FLAP CANOE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D, 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

INTERCOSTAL TO FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,722 hrs · 49,419 cycles

INSPECTION TYPE:C3 LONGERON 16R AT FS 1728 IS CRACKED AT FRAME ATTACHMENTS, LENGTH OF CRACKS IS APPROX 1.5 INCH. REPAIRED LONGERON AT 16R STA1728 IAW DWG 5644130, DC-8 53-2-2 FIG 10, SRM 53-02-02-0, SRM 51-1-20D.

Part: LINE — LEAKING (HYD SYSTEM)

EMERGENCY LANDING FOR LOSS OF HYD QTY. REMOVED AND REPLACED BOGIE TRIM CYLINDER FLEX LINE, LT GEAR SERVICED HYD FLUID & OPERA TED ALL SYSTEMS CHECKS GOOD NO LEAKS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND RELAY UNIT PER MM 33-50-01.

Part: PANEL — CRACKED (NR 4 PYLON)

NR 4 PYLON SIDE HAS 3.5 INCH CRACK IN ACCESS PANEL 499E {FIBERGLASS PANEL} 8 INCHES AFT OF L/E OF PANEL VERTICAL CRACK FROM BOTTOM EDGE OF PANEL. PANEL REPAIRED PER REF SRM 51-1-19.

Part: ROD — CORRODED (RT MLG ACTUATOR)

RT MAIN LANDING GEAR RETRACT ACTUATOR HAS CORROSION ON ROD END, JAM NUT & LOCK TAB WASHER ROD END CONDITION UNKNOWN. REPAIR PER EO DC8-3230-3958-D PARTS ON ORDER, ACTUATOR AND ROD END ASSY. REMOVED AND REPLACED MLG ACTUATOR IAW MM 32-32-02.

Part: ENGINE — FLAMED OUT (NR 3)

NR 3 ENGINE FLAMED OUT IFSD AT 35000 FT N1 WINDMILLING AT 30 PERCENT N2 AT 15 PERCENT OIL PRESSURE = 1PSI, QUANTITY AND TEMP NORMAL TIME = 1235 TIME 1340 N1 = 14.5 PERCENT N2 = 0 OIL PRESSURE 0. PERFORMED T/S 71-00-00 PG 165-167, ADJUSTED GROUND AND FLIGHT IDLE IAW MM 73-20-01 PG 533. REF CFM MM 71-00-00 FAULT 51. PERFORMED ENGINE RUNS IAW 71-00-00, NO DEFECTS NOTED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, MAIN CABIN INTERIOR RT SIDE OVERWING HATCH UPPER AFT FITTING CRACKED. REMOVED AND REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, L1 DOOR CORNER UPPER AFT DOUBLER IS STEEL. REMOVED DOUBLER IAW DC8 SRM 51-1-21. ROUTED OUT CRACKS, REPERFORMED HFEC AND NO CRACKS WERE NOTED. FABRICATED FILLERS AND DOUBLERS IAW DC8 SRM 53-2-0 FIG 15. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DBLR/TRIPLER AND FILLERS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FWD PIT FS 340 RT FLOORBEAM END FITTING CRACKED. REMOVED AND REPLACED CRACK FITTING P/N 6754022-504A IAW DC8 SRM 51-1 -20D AND 51-3-0

Part: FITTING — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, AFT PIT FS 1160 RAMP PANEL SUPPORT FITTING CORRODED AT LONGERON 36 REMOVED SUPPORT LOCATED AND DRILLED NEW SUPPORT IAW DC8 SRM 51-1-24 INSTALLED SUPPORT IAW DC8 SRM 51-1-20D

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, L2 DOOR UPPER FWD CORNER HAS CRACK IN EXISTING DOULBER REPAIR. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER IAW DC8 SRM 52-2-0

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 HOLES FOR LOCK PINS WORN OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-3 HOLES FOUND TO BE ELONGATED BEYOND LIMITS OF DC8 SRM 53-2-3 REMOVED WORN SEAT TRACK IAW DC8 SRM 51-3-0 DRILLED NEW SEAT TRACK IAW DC8 SR M 51-1-24 INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FS 450 BETWEEN LONGERON 36 AND 35 RT HAS FOUND TO HAVE DAMAGE IN SKIN SPLICE DOUBLER. FABRICATED DOUBLER PN 5779911-7 IAW DAC DWG 5779911-7. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND FABRICATED FINGER DOUBLER IAW DAC DWG 5779911-9 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FINGER DOUBLER AND STRAP IAW DC8 SRM 51-1-21 AND 51-1-20D

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, AFT LOWER CARGO STA 1420 LONGERON 22 RT CORRODED AND CRACKED. CUTOUT DAMAGED AREA OF LONGERON, LOCATED DRILLED, & DEBURRED NEW SECT OF LONGERON & 2 EA SPLICE FITTING IAW DC8 SRM 53-2-2 FIG 4. ALODINED AND PR IMED IAW DC8 SRM 51-1-8. INSTALLED NEW SECT OF LONG & 2 EA SPLICES I AW DC8 SRM 53-2-2 FIG 4

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, CABIN INTERCOSTAL CRACKED AT FWD END FS 960 S-5 BLENDED AREA AND FOUND TO BE IN LIMITS IAW DC8 SRM 53-2-0 ALODINED A ND PRIMED IAW DC8 SRM 51-10-8 INSTALLED FASTNERS IAW DC8 SRM 51-1-21 D

Part: FRAME — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, AFT LOWER CARGO AT STA 1420 FRAME AT LONGERON 22 RT HAS ELONGATED HOLES. REMOVED OLD FRAME, LOCATED DRILLED, AND DEBURRED NEW FRAME IAW DC8 SR M 51-1-21 ALODINED & PRIMED IAW DC8 SRM 51-1-8 INSTALLED NEW FRAME IAW DC8 SRM 51-1-24

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, R1 DOOR JAMB LWR AFT CORNER HAS 2 CRACKS FOUND WITH NDT, REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 14

Part: GUSSET — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 759 STR 5R INTERCOSTAL GUSSET CRACKED. REMOVED AND REPLACED GUSSET IAW DC8 SRM 51-1-21

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 REPAIR DOUBLER 744-2R-07 STA 718 & 727 AND LONG 13R IS CAT D STAINLESS STEEL REPAIR WITH 2 ROWS OF FASTENERS BEYOND CUTOUT AND ALL CRITICAL ROW HIDDEN. REPAIRED AREA IAW REO G08803

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR 744-3L-05 STA 1748 TO 1754 AND LONGERON 14 LT TO LONGERON 15 LT, IS CAT B REPAIR, 9 INCHES TO REPAIR 744-3L-04 ONLY 2 ROWS BEYOND DAMAGE LOWER CRITICAL ROW SKIN HIDDEN, REPAIRED AREA IAW DC8 SRM 53-2-0, FIG 7, CLASS II

Part: DOUBLER — MISINSTALLED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-2R-04 DETERMINED TO BE CAT D, DUE TO LESS THAN 3 ROWS OF FASTNERS PAST DAMAGE FS 450-455 LONGERON 35 RT FABRICATED FILLER, DOUBELR, DINGERS IAW DC8 SRM 53-2-1 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1 -20D

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FUSELAGE AT STA 1745 ABOVE LONGERON 15 RT, SKIN CRACKED. PERFORMED HFEC IAW DAC SPM NDT MANUAL PT 6 51-00-01.003 TO VERIFY CRACK REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, FINGER DOUBLERS AND FILLER IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED REPAIR PART S IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIG 7, 51-1-21, AND 51-1-20D

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOORBEAM ATTACH ANGLE STA 1766, LBL 20 HAS CORROSION UNDER NUTPLATE ON VERTICAL LEG. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-21

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 VERTICAL STIFFENER, LBL 20, ON FWD FACE OF AFT PRESSURE BULKHEAD HAS CORROSION ON LOWER END AT FLOOR LEVEL REPAIRED IAW REO G08808

Part: DOUBLER — WORN (R2 DOOR) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 R2 DOOR FRAME AT FS 1650 AT L17R DOUBLER ON FRAME IS WORN AND CHAFFED AT RADIUS. REMOVED AND REPLACED DOUBLER IAW DAC DWG 5615700

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, BELLY SKIN AT STA 150 UNDER LOWER VHF ANTENNA IS EXFOLIATED, REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 5 1-1-8 PROCURED MATERIAL IAW DC8 SRM 53-2-1 FIG 7. CUT OUT DAMAGED AR EA IAW DC8 SRM 53-2-1 FIG 7. FABBED DOUBLER, FILLER AND 4 EA FINGER DOUBLERS IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED IAW DC8 SRM 51 -1-8. INSTALLED IAW DC8 SRM 53-2-1 FIG 7

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOOR SUPPORT ANGLE CORRODED AT FS 1766 24 LBL. CORROSION OUT OF LIMITS, FABBED NEW ANGLE IAW DAC DWG 5755032 INSTAL LED NEW ANGLE IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 LONGERON FITTING CRACK AT STA 1767 AT L17R ACCESS THRU DOOR 60 REMOVED AND REPLACE LONGERON END FITTING IAW DC8 SRM 51-1-20D & 51-1 -21

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 7 RT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT B S 851 L8R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 704 STR 17L INTERCOSTAL CRACKED. ROUTED OUT DAMAGE AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 H EAT TREATED TO BE IAW TPS-1003. FABRICATED, LOCATED, AND DRILLED IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 INSTALLED FA STENERS IAW DC8 SRM 51-1-21D

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOORBEAM AT FS 1723 BL16L HAS CORROSION UNDERNEATH LOWER FLANGE. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND TO BE OUT OF LIMITS IAW D C8 SRM 53-2-0 REMOVED FLOORBEAM IAW DC8 SRM 51-1-20D FABBED FLOORBEAM IAW DC8 DAC DWG 5755032 ALODINED AND PRIMED FLOORBEAM IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (STA 680) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 3 RT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT BS 678, L2L. REMOVED FITTING IAW DC8 SRM 51-1-20D, DRILLED NEW FITTING IAW DC8 SR M 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED AN D TIGHTENED PLI WASHER IAW DC8 SRM 51-1-23

Part: CHANNEL — CORRODED (FLOOR SUPPORT) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOOR SUPPORT CHANNEL CORRODED AT APPROX BL10L FS 1717 REMVOED CORROSION IAW DC8 SRM 51-1-8 AND FOUND TO BE OUT OF LIMITS I AW DC8S SRM 53-2-0 HEAT TREATED NEW CHANNEL FROM 0 TO T6 IAW TPS -10 03 FABBED CHANNEL IAW DC8 DAC DWG 5755032 ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, MAIN CABIN BATHTUB FITTING CRACKED AT BS 587 L10L REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, L9R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, LONGERON CRACK AT STA 1767 AT L17L ACCESS THRU DOOR 60. REMOVED & REPLACED LONGERON PN 5639327-43 IAW DC8 SRM 51-1-20D AND 5 1-1-21

Part: SKIN — DAMAGED (FS 1436) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-04, STA 1436 TO 1445 AND LONGERON 26 RT TO 27 RT IS CAT C STEEL WITH REPLACABLE BLIND FASTENERS AND ALL CRITICAL ROWS FASTENERS SKIN HIDDEN. REMOVED OLD DOUBLER & FILLER FOM. PREFORMED HFEC ON CUTOUT SKIN. NO CRACKS FOUND IAW NDT SPM 06-10-01-001. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. IN STALLED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 21

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, LONGERON CRACK AT STA 1767 L17R ACCESS THRU DOOR 60. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 FLOOR SUPPORT ANGLE CORRODED AT FS 1766 BL 18L REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED ANGLE IAW DC8 SRM 51-1-21 FAB, LOCATED AND DRILLED IAW DAC DWG 5 755032, ALODINE AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 REPAIR DOUBLER 744-1R-02 DETERMINED TO BE CATEGORY B DUE TO PROXIMITY TO 744-1R-01 REMOVED EXISTING DOUBLERS AND REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOOR SUPPORT ANGLE CORRODED AT FS 1766 LBL13. CORROSION OUT OF LIMITS, FABBED NEW ANGLE IAW DAC DWG 5755032 INSTAL LED NEW ANGLE IAW DC8 SRM 51-1-21D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT BS 681, L6R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 IN MAIN CABIN L4L END FITTING ON AFT SIDE OF BS 680 IS CRACKED REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR 744-3R-05, STA 1376-1384 AND LONGERON 24 - 26 RT IS CATEGORY D, DUE TO ONLY 2 ROWS OF FASTENER BEYOND CUTOUT AND AFT CRITICAL ROW FASTENER SKIN HIDDEN REMOVED OLD DOUBLER IAW DC8 SRM 51-1-21, REMOVED DAMAGED AREA, FABBED NEW DOUBLER, FINGER DOUBLERS AND FILLER IAW DC8S RM 53-2-1 FIG 7 S H 4 AND REO G08806 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21 AND 51-1-20D

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, FLOOR SUPPORT CORRODED AT BL0 FS 1723-1730 LT LOWER FLANGE. BLENDED CORROSION IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DC8 SRM 53-2- 0 MAD ID FLOOR SUPPORT PN S2652479, ALODINED & PRIMED IAW DC8 SRM 51 -1-8, INSTALLED IAW DC8 SRM 51-1-21D

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-2L-01 DETERMINED TO BE CATEGORY B WITH HIDDEN ROWS (ALSO DOUBLER IS STEEL) FS 415-423 LONG 20L-21L REMOVED EXISTING DOUBLER, CUTOUT DAMAGED SECTION OF SKIN IAW REO G08 800 FABRICATED REPAIR DOUBLER, TRIPLER, FILLER IAW REO G08800 ALODIN ED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW DOUBLER, TRIPLER, FILL ER IAW REO G08800

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-01 STA 1690-1697 AND LONGERON 26 - 28 RT IS CAT D, DUE TO DEFORMED FASTENER LESS THAN 3 ROWS OF FASTENERS BEYOND DAMAGED AND IS A STEEL REPAIR LESS THAN BASE SKIN. FABRICATED NEW REPAIR DOUBLER, FINGER DOUBLER, TEAR STRIP AND FILLER IAW DC8 SRM 53-2-1 FIG 7 SHEET 5 ALODINED & PRIMED IAW DC8 SRM 51-1- 8. INSTALLED REPAIR DOUBLER, FINGER DOUBLER, TEAR STRIP, FILLER, FIT TINGS AND PROCUCTION BOLTS IAW DC8 SRM 51-1-20D, 51-1-21, AND 51-3-0 .

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 10 LT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: SKIN — DAMAGED (FS 1714) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-02, STA 1714 - 1723 AND LONG 17 RT TO 18 RT IS CAT D ONLY 2 ROWS BEYOND DAMAGED. NO CUT-OUT (STOP-DRILLED) AND UPPER CRIT ICAL ROW HIDDEN SKIN REMOVED EXISTING REPAIR DOUBLER AND DAMAGED AREA IAW DC8 SRM 51-1-21 AND 53-2-1 FIG 7. REMOVED LONGERON 17 RT CAP INTERCOSTAL AND SHEAR TIE. FABRICATE REPAIR DOUBLER IAW DC8 SRM 53-2-1 FIG 7, ALODINED & PR9 IMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 53-2-1 FIG 7. REINSTALLED LONG 17 RT CAP INTERCOSTAL AND SHEAR TIE IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (STA) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 BATHTUB FITTING CRACKED AT BS 681, L8R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 IN MAIN CABIN L2L END FITTING ON AFT SIDE OF BS 680 IS CRACKED REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT BS 851 L9R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C 1, MAIN CABIN BATHTUB FITTING CRACKED AT BS 857 LONGERON 10 RT. REMOVED AND REPLACED FITTING AIW DC8 SRM 51-1-20D

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 LEFT MID GALLEY SERVICE DOOR LOWER FWD CORNER OF JAMB HAS A CRACK FOUND WITH HFEC. REPAIRED DOOR CORNER IAW DC8 SRM T/R 53-2-0 FIG 15A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN L8R CRACKED AT FS 280, 320, 340. REMOVED CRACKED LONG SECTION AT L8R FS 280-340, LOCATED AND DRILLED LONG AND SPLICE IAW DC8 SRM 51-1-247, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONG AND SPLICE IAW DC8 SR M 51-1-21

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 REPAIR DOUBLER 744-3L-03 STA 1715 TO 1720 AND LONG 17L IS CAT B DUE TO PROXIMITY 18 IN TO REPAIR 744-3L-04 AND NO CUTOUT STOP DRILLED ONLY UPPER CRITICAL ROW HIDDEN SKIN. REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN L 10 RT END FITTING CRACKED AT FS 680 REMOVED FITTING IAW DC8 SRM 51-1-20D DRILLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED PLI WASHER AND TIGHTENED PLI WASHER IAW DC8 SRM 51-1-23

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, REPAIR DOUBLER 744-3L-02 STA 1710 TO 1737 AND LONG 26 LT TO 28 LT IS CAT D, DUE TO NO FASTNER ROWS BELOW CUT-OUT AND SKIN CRITICAL ROWS HIDDEN. REMOVED EXISTING DOUBELR, FABRICATED NEW DOUBLER, SKIN DILLER, AND FINGER DOUBLERS AND INSTALLED IAW DC8 SRM 53-2-1 FIG 7. ALODINED AND PRIMED IAW DC8 SRM 51-1-8

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN L9R CRACKED AT FS 340 REMOVED CRACKED LONG SECT AT L9R FS 340, LOCATED AND DRILLED LONG AN D SPLICE (PART# DC9-53B-009-3) IAW DC8 SRM 51-1-24, ALODINED AND PRI MED IAW DC8 SRM 51-1-8, INSTALLED LONG AND SPLICE IAW DC8 SRM 51-1-2 1

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 MAIN CABIN L8R CRACKED AT FS 120. INSTALLED SPLICE FITTING AND LONGERON IAW DC8 SRM 51-1-20D AND 51-1- 21 AND DC8 SRM 53-2-2 REPLACE LONG SECTION IAW DAC DWG 5610949, ALOD INED AND PRIMED IAW DC8 SRM 51-1-8

Part: FITTING — CRACKED (DOOR WA7) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 LT AFT ENT DOOR FWD UPPER CORNER INNER FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 INSTALLED FITTING IAW DC8 SRM 51-1-20D

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 DOUBLER REPAIR 744-2R-03 STA 328 TO 338 LONG 32R CLASSIFIED AS REMOVED DOUBLER. FABBED DOUBLER AND FILLERS IAW DC8 SRM 53-2-0. ALOD INED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 S RM 53-2-0

Part: FITTING — CRACKED (FS 1170) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 AFT PIT STA 1170 BY LONG 33 RT FITTING CRACKED. REMOVED OLD FITTING. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLE D (2) NEW FITTINGS IAW DC8 SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 AFT PIT STA 1180 BY LONG 28 AND 27L FITTING IS CRACKED REMOVED CRACKED FITTING, RECIEVED NEW FITTING P/N 3755842-505N. FABB ED REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 5 1-1-8. INSTALLED IAW DC8 SRM 51-1-20D. SEALED IAW DC8 SRM 51-1-17 & 51-1-14

Part: FITTING — CRACKED (STA 1150) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 AFT PIT FITTING AT SKIN TO FWD END OF C-3 DOOR TORQUE BOX CRACKED, STA 1150 BETWEEN LONGERONS 34 R - 35 R. REMOVED TWO FITTING IAW DC8 SRM 51-1-20D FAB REPAIR DOUBLERS IAW DC8 SRM 53-2-0 ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 REPAIRS DOUBLER 744-1L-01, 744-1L-03, 744-1L-04 AT BS 36 TO BS 56 LONG 28L TO LONG 30L CAT C & D REPAIRS DUE TO FASTENERS SPACING AND MA TERIAL THICKNESS AND STAINLESS STEEL REPAIR REMOVED (4) DOUBLERS IAW DC8 SRM 51-3-2, MAT'L ID IAW DAC DWG# SRO B S300-20 DOUBLERS 2024-T3.071 PO# 389651, FILLER 2024-T3.063 PO# 3908 75, FABRICATED DOULBER & (4) FILLERS IAW REO G08798, ALODINE AND PRI MED IAW DC8 SRM 51-1-8, TRIMMED OUT DAMAGED AREA IAW REO G08798, INS TALLED DOUBLER & (4) FILLERS IAW DC8 SRM 51-1-20D

Part: FITTING — CORRODED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 AFT PIT STA 1220 BY LONG 33R FITTING HAS CORROSION INSIDE TORQUE BOX. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC87 SRM 53-2-0 REMOVED TWO FITTINGS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1 AFT PIT STA 1340 TO 1360 LONGERON SPLICE FITTING CRACKED AND CORRODE D BY LONG 32L. REMOVED CRACKED LONGERON FITTING IAW DC8 SRM 51-1-20D, LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 AIR COND/PRESS COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMAT IC DUCT STANDOFF ATTACH BRACKET. REMOVED FRAME SECTION FS 56 L24R IAW DC8 SRM 51-1-8, FAB NEW FRAME A ND SPLICES IAW DC8 SRM 53-3-1, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED FRAME AND SPLICES IAW DC8 SRM 51-1-21, HEAT TREAT FRAME AND SPICE TO 7075-T6 IAW TPS 1003-REV A

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE: C1, R-1 DOOR CORNER DOUBLER IS STEEL UPPER FWD. REMOVED STEEL DOUBLER IAW DC8 SRM 53-2-0 AND TRIMMED CRACK AREAS IAW DC8 SRM 53-2-0 FABBED FILLER AND 2 EA DOUBLERS IAW DC8 SRM 53-2-0 A LODINED & PRIMED IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D A ND 51-1-21 PREFORMED HF-TEST TO LOCATE CRACKS

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 AIR COND/PRESS COMPT AT FS 56 ABOVE L24L FRAME IS CRACKED REMOVED FRAME AT FS 56 L24L, FAB FRAME AND SPLICES IAW DC8 SRM 53-3- 1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FRAME AND SPLIC E IAW DC8 SRM 51-1-21, FRAME AND SPLICE HEAT TREATED TO 7075-T6 IAW TPS 1003 REV A

Part: SKIN — CRACKED (PAX DOOR) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1` L1 DOOR CORNER UPPER FWD DOUBLER IS STEEL, CUT OUT CRACKS IN SKIN IAW DC8 SRM 53-2-0 FIG 15 TR 53-129 AND REO G 08797 PERFORMED HFEC IAW DC8 SPM NDT MAN 06-10-01.001 FABBED -15 & - 17 DOUBLERS AND -19 FILLER IAW DC8 SRM 53-2-0 FIG 15 TR 53-129 AND REO G08797. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS & FILLERS IAW DC8 SRM 51-1-20D,53-2-0 FIG 15 TR 53-129 & REO G08797

Part: FITTING — CRACKED (FWD ACCESS BAY) · airframe 74,722 hrs · 48,614 cycles

INSPECTION TYPE:C1 FWD ACCESS COMP'T AT FS 660 ABOVE L35L-L35R COMP DOOR UPPER TRACK FI TTING IS CRACKED REMVOED & REPLACED FITTING IAW DC8 SRM 51-3-0

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY PACK, CHECKED WORKED OK.

Part: CONNECTOR — NOT SEATED (COCKPIT)

INSPECTION TYPE:N/A DURING PREFLIGHT FOUND EMERGENCY LIGHT DISARM ARM SWITCH LIGHT DID NOT WORK. FOUND CONNECTOR P1-1344 AT DIMMING BOX B5-60 NOT FULLY SEATED. SEATED CONNECTOR P1-1344 LIGHT OPS CK NORMAL REF WDM 33-50-01.

Part: CDU — MALFUNCTIONED (CARGO BAY)

INSPECTION TYPE:N/A DIVERSION TO PIT LOWER FWD CARGO SMOKE WARNING IN FLIGHT. NOTE: MX STATED SYSTEM TESTED OK ON GROUND. MX SMELLED CHEMICAL WHEN OPENING CARGO DOOR. HAZMAT TEAM ON SITE. PERFORMED TEST OF EACH FIRE DET PER MM 26-18-00 SYSTEM. COMPLETE BOW TS-1493 REV NO 998, T/S THE LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM. REMOVED AND REPLACED CDU GROUND OPS CHECKS GOOD PER MM 26-18-03.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A DURING FAULT ON NR 4 BUSS POWER FAIL LANDING GEAR FAULT ON EXTENSION THE GEAR HAD UNSAFE INDICATION ON ALL THREE GEARS AND GEAR WARNING HORN. PERFORMED LANDING GEAR CONTROL SYSTEM CHECK PER MM 32-31-00, NO FAULTS NOTED. SYSTEM CHECKS GOOD, OK TO CONTINUE.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHTS WOULD NOT COME ON. REMOVED EMERGENCY BATTERY PACK. LIGHTS OPS CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK VOLTAGE DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND RELAY UNIT IAW 33-50-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT LONGERON 29 RIGHT SPLICE FITTING CRACKED STA 1680. REMOVED AND REPLACED CRACKED FITTING PO 341342 (P/N 46413246502).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, SEAT TRACK FLANGE CORRODED BL 0 STA 1124. REPAIRED SEAT TRACK IAW REO G07703.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, FWD LONGERON 29R SPLICE FITTING CRACKED AT STA 1680. REMOVED AND REPLACED FITTING.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1200 FWD ATTACH FITTING CRACKED BETWEEN LONGERON 27 LT AND 28 LT. REMOVED CRACKED FITTING, FAB REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATE NEW FITTING AND REPAIR ANGLES AND DRILL EXISTING HOLES IAW DC8 SRM 51-1-24, INSTALL FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, CRACK IN SHEAR TIE FS 1360 BETWEEN LONGERON 32 TO 31 RIGHT. REMOVED DAMAGED SECTION OF SHEAR TIE, FABD NEW SHEAR TIE SECTION AND DOUBLER STRAP, ALODINED AND PRIMED, INSTALLED TIE SECTION AND DOUBLER STRAP.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK AT FS 15080, SEAT TRACK ''A'' HAS 3 DAMAGED SCALLOPS. CUT OUT TRACK IAW DC8 SRM 53 FIG 6D, ALODINED AND PRIMED DRILLED CHANNEL PLUGS TO FIT IAW DC8 SRM 51-1-24, 53-2-3 FIG 6D. INSTALLED IAW DC8 SRM 51-3-0, 53-2-3 FIG 6D.

Part: SEAT TRACK — WORN (CABIN) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, SEAT TRACK E HAS WORN SCALLOPS 2 PLACES AT APPROX FS 160. BLENDED SEAT TRACK AT FS 150. BLENDOUT IS WITHIN LIMITS IAW DC8 SRM 53-2-3 FIG 12. CUT OUT HOLE FOR PLUG AT FS 160 IAW DC8 SRM 53-2-3 FIG 6D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-3 FIG 6D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1200 FWD ATTACH FITTING CRACKED BETWEEN LONG 27 RT AND 28 LT. REMOVED CRACKED FITTING, FAB REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED, PRIMED, LOCATE NEW FITTING AND REPAIR ANGLE, DRILL EXISTING HOLES IAW DC8 SRM 51-1-8. INSTALL FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1100 FRAME CORRODED AROUND FASTENERS AT LONGERON 35 RT. REMOVED CORROSION FOUND OUT OF LIMITS. FAB REPAIR ANGLE IAW EO 5310-117 28 REV A. REMOVED INTERCOSTAL AND GUSSET STA 1100 - 1120 L35 RT, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER FILLER INTERCOSTAL AND GUSSET IAW DC8 SRM 51-1-20D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT PIT SMOKE BARRIER CEILING ATTACH ANGLE CORRODED. REMOVED CORRODED ANGLE, FABED NEW ANGLE IAW TIMCO DWG DWG-01252. ALODINED AND PRIMED INSTALLED ANGLE IAW 51-3-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1100 FRAME CORRODED AROUND FASTENERS AT LONG 35 RT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FAB REPAIR ANGLE FILLER IAW UPS EO 5310-11728, REMOVED INTERCOSTAL AND GUSSET STA 1100 - 1120, ALODINED AND PRIMED INSTALLED IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, CORROSION ON I/B AND O/B LEGS OF LONGERON 36 IN AREA AROUND FWD DME ANTENNA BETWEEN FS 8 & 25. REMOVED FWD DME ANTENNA AND SEPARATED WIRE BUNDLE FROM TEMP CONTROLLER AND HOUSING TO FOM. REMOVED SHOVEL FITTING, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED IAW 51-1-24, ALODINED AND PRIMED INSTALLED SHOVEL FITTING IAW 51-1-21, INSTALLED BME AND TEMP CONTROLLER IAW 53-20-00, DME SYS OPS CHECK GOOD IAW DC8 MM 34-21-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1055 - 1060 L35R SPLICE CRACKED. REMOVED INTERCOSTAL, 2 L-ANGLES TO GAIN ACCESS TO LONG SPLICE FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1 -24. INSTALLED INTERCOSTAL FITTING AND 2 L-ANGLES IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT CROSSLIDE DOOR 2 LOWER ''T'' BOLT FITTING CRACKED. REMOVED 2 T-BOLT FITTINGS IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED 2 NEW FITTINGS IAW DC8 SRM 51-1-24, INSTALLED 2 FITTINGS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT CARGO COMPT FS 1160 LONGERON 34RT ATTACH FITTING CRACKED AT LOWER FASTENER HOLE. REMOVED CRACKED FITTING, RECVD NEW FITTING (P/N 3755843-502N) MAT ID FOR REPAIR ANGLE 60-436 EXTRUSION .125 7075-T6 511 IAW DC8 SRM 53-2-0. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, FABD REPAIR ANGLES IAW DC8 SRM 53-2-0, ALODINED AND PRIMED, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, MAIN CABIN FS 1575 FRAME CRACKED JUST ABOVE LT CUSP. REPAIRED FRAME IAW REO G07671.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, CORROSION AROUND FASTENERS IN GUSSET ON LOWER LEG OF FLOOR FRAME AT FS 1340 APROX 20 INCHES I/B OF RIGHT CUSP. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED GUSSET, FAB NEW IAW DAC DWG 9754034, ALODINE AND PRIME INSTALLED IAW 51-1-20D.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, CORROSION AROUND FASTENERS IN GUSSET ON LOWER LEG OF FLOOR FRAME AT FS 1320 APPROX 20 INCHES I/B OF THE RIGHT CUSP. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED GUSSET, FAB NEW GUSSET IAW DAC DWG 9754034, ALODINE AND PRIME IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, LT LWR FUSELAGE STA 702 FILLET FAIRING ATTCH ANGLE IS CRACKED IN RADIUS. REPAIRED FILLET FAIRING ATTACH ANGLE IAW DC8 SRM 53-2-0 AND LONGERON 33 LT IAW TIMCO REO G07690 REV A.

Part: ANGLE — CRACKED (DOOR FRAME) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT PIT ''D'' DOOR JAMB ''L'' ANGLE CRACKED. FABED NEW DOOR JAMB ''L'' ANGLE IAW DAC DWG 3712791. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, RIGHT APB CRACKED STA 1766 APPROX L11R. FABED, LOCATED AND DRILLED -25 & -27 DOUBLERS -9 -19 & -11 FILLERS AND -29 ATTACH ANGLE IAW DC8 SRM 51-1-24 & REO G07688. ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (THRESHOLD) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2, AFT PIT ''D'' DOOR THRESHOLD SUPPORT CRACKED. REMOVED CRACKED SUPPORT ANGLE, FABED NEW SUPPORT ANGLE IAW DAC DWG 5703872. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 73,582 hrs · 47,807 cycles

INSPECTION TYPE:C2 LOG ITEM TRANSFERRED FROM LOG PAGE 5275611 ITEM 2 SEAT TRACK BROKEN MAIN CARGO DECK POSS 2-3 LEFT O/B CUT OUT DAMAGED IAW DC8 SRM 53-2-3 FIG 6D. ALODINED,PRIMED AND INSTALLED IAW DC8 SRM 51-3-0, 53-2-3 FIG 6D.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 ENGINE)

MX PREFLT, NR 2 ENG FIRE WARNING AND SHORT CIRCUIT TEST INOP. REMOVED AND REPLACED NR 2 FIRE DETECTOR CONTROL UNIT.

Part: OVERTEMP LIGHT — ILLUMINATED (FLIGHT DECK)

MAIN AIR OVERTEMP LIGHT ILLUM WITH MANIFOLD AIR TEMP IN NORMAL RANGE NO WARNING LIGHT. MONITORED LIGHT SUSPECT PRESS TO TEST. SWITCH LIGHT STILL ILLUM AFTER SHUTDOWN. RELAMPED MAN OVERTEMP LIGHT. RAN ALL ENG. NO OVERTEMP NOTED OPS CK OK.

Part: TRIM SERVO — FAILED (HORIZ STAB)

INSPECTION TYPE-N/A WHILE A/C WAS BEING LOADED, LOADERS COMPLAINED OF A STRANGE SMELL. MAINT WAS CALLED AND OBSERVED SMOKE IN A/C. A/C WAS EVACUATED AND THE FIRE DEPARTMENT WAS DISPATCHED. FOUND LONG TRIM SERVO UNIT 2 FROZEN EVIDENCE OF MOTOR BURNED UP. REMOVED AND REPLACED SERVO PER M/M 27-41-10 (P/N 300425-02) ON, (P/N 300425-01) OFF, OPS CHECK GOOD.

Part: FITTING — CORRODED (NR 1 PYLON)

INSPECTION TYPE-D, NR 1 PYLON THROUGH PANEL 197B FIRST RT VERTICAL STIFFENER LWR ATTACH FITTING CORRODED. REMOVED OLD FITTING, RCD NEW FITTING FROM MACHINE SHOP DRILLED HOLES AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: ANGLE — CORRODED (CARGO COMPT)

INSPECTION TYPE-D, CORROSION ON CUSP TO FRAME ANGLE, FWD OF FRAME 140 AT L21R. REMOVED CORRODED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SR M 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (BS 1766)

INSPECTION TYPE:D AT LONGERON 10L AT STA 1766 HAS A CRACK AT BULKHEAD. REMOVED STRAP FROM ACCESS. STOP DRILLED IAW DC8 SRM 53-7-5 FIG 9. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED STRAP IAW DC8 SRM 51-1-70D

Part: FRAME — CRACKED (BS 1717)

INSPECTION TYPE-D, AT LONGERON 11L STA 1717 CRACKED AT MAIN FRAME. REMOVED CRACKED SECTION FABRICATED NEW AND INSTALLED IAW DC8 SRM 53- 2-0, 51-1-20D, 51-1-8, 53-5-1.

Part: SKIN — CORROSION (TAIL CONE)

INSPECTION TYPE-D, REMOVED FWD SKIN ON RIGHT SIDE OF TAIL CONE DUE TO CORROSION. FAB NEW SKIN IAW DAC DWG 5644500, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.

Part: DOUBLER — CORROSION (BS 1540-1560)

INSPECTION TYPE-D, AFT ACC COMPARTMENT CORROSION O9N FINGER DOUBLER AT LONGERON 31L-32L FS 1540 TO 1560. FAB NEW SECTION OF FINGER DOUBLER IAW 53-4-1, FAB LONGERON SPLICE IAW REO-05809, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: LONGERON — CORRODED (BS 1540-1560)

INSPECTION TYPE:D AFT ACCY COMPARTMENT/CORROSION ON LONGERON INNER SURFACE LONGERON 2 5L FS 1540-1560. REMOVED CORR IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 S RM 53-2-0. REMOVED DAMAGED SECTION OF LONGERON DRILLED AND DEBURRED LONG END SPLICES IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SR M 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1700)

INSPECTION TYPE-D, FRAME CORRODED BETWEEN LONGERONS 35 LT TO 35 RT AT STA 1700. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-1-8. FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED ANGLE.

Part: INTERCOSTAL — CRACKED (BS 970)

INSPECTION TYPE-D, INTERCOSTAL BETWEEN MLG DOORS FS 970 CRACKED, WORN AND LOOSE BRACKETS. REMOVED INTERCOSTAL, DRILLED NEW INTERCOSTAL TO FIT IAW DC8 SRM 51-1 -24. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 978)

INSPECTION TYPE-D, CORROSION AROUND FASTENERS AT TOP OF LT CORNER OF MLG WHEEL WELL WEB ATTACH PLATES, STA 978. FOUND FITTING TO BE CRACKED. REMOVED AND REPLACED IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: ANGLE — CORRODED (BS 940)

INSPECTION TYPE:D CORRODED ANGLE AT RT END OF FRAME STA 940 AT AFT UPPER CAP. REMOVED AND REPLACED ANGLE FRAME STA 940 AT UPPER CAP.

Part: PAN — PUNCTURED (SERVICE DOOR)

INSPECTION TYPE:D RIGHT AFT SERVICE DOOR JAMB PUNCTURE IN LOWER AFT PAN. REMOVED DAMAGED SECTION OF PAN FABRICATED NEW SECTION. FABRICATED SPLICE ANGLES ALODINED PRIMED AND INSTALLED NEW PARTS.

Part: FLOORBEAM — CORROSION (BS 702.875)

INSPECTION TYPE:C, FS 702.875 AT RBL 62 TO 65 THE FLOORBEAM LOWER FLANGE AT FWD SIDE HAS EXFOLIATION, CORROSION BLENDED OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 53-10-0, 51-1-20D, AND DWG 5642500.

Part: FITTING — CRACKED (BS 781.5)

INSPECTION TYPE:C, MAIN CABIN FS 781.5 LBL 47 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D AND DWG 3641126.

Part: FRAME — CORRODED (BS 1240)

INSPECTION TYPE:C, FS 1240 AT LONG 35R FRAME LOWER FLANGE HAS HEAVY CORROSION, METAL IS SEPARATING. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW DHC SK-744-66, REF UPS ENRG FILE NR DC8-53-1825.

Part: FITTING — CORRODED (BS 290 33R)

INSPECTION TYPE:C, C-1 BACKUP LATCH FITTING CORRODED BEYOND LIMITS 33R AT FS 290 NR 2 FWD. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20.

Part: DOUBLER — CORRODED (BS 280-360)

INSPECTION TYPE:C, FS 280 TO 360 BTWN STR 35L AND 35R INTERNAL DOUBLER IS CORRODED ON BOTH SIDES. REMOVED AND FABRICATED DOUBLER IAW DWG 5759839.

Part: SHEAR TIE — CORRODED (BS 320)

INSPECTION TYPE:C, FS 320 BTWN STR 35R TO 36, SHEAR TIE FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 260-340)

INSPECTION TYPE:C, FS 260 TO 340 STR 36 IS CORRODED AND CUT AT FS 340. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION FROM FS 260 TO 360 IAW SRM 53-2-2, 51-1-8, AND DWG 9754913.

Part: DOUBLER — CORRODED (BS 450)

INSPECTION TYPE:C, F/S 450 BETWEEN STR 31L TO 31R SKIN BUTT INTERNAL FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER AND TRIPLER IAW SRM 51-1-11, 51-1-21, 51-1-8, AND DWG 5755271.

Part: LONGERON — CORRODED (BS 300-350)

INSPECTION TYPE:C, FS 300 TO 350, STR 35R HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-1-0 AND DWG 9754913.

Part: STRINGER — CRACKED (BS 1340-1350)

INSPECTION TYPE:C, FS 1340 TO 1350 , STR 35R HAS A 6 INCH CRACK. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER IAW SRM 51-1-20D, 51-1-8, 51-1-20D, AND DWG 5750322.

Part: STRINGER — CRACKED (BS 1340-1350)

INSPECTION TYPE:C, FS 1340 TO 1350 STR 36 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-0, 53-1-0, 51-1-20D.

Part: STRINGER — CRACKED (WS 502)

INSPECTION TYPE:C, RT WING (INTERNAL) AT STA XRS 502.00, STRINGER NR 53 IS CRACKED. REMOVED DAMAGED AREA OF STRINGER, FABRICATED AND INSTALLED REPLACEMENT SECTION AND SPLICES IAW SRM 57-2-2 FIG 3D AND 3E, 51-1-20D.

Part: FITTING — CRACKED (BS 822.5)

INSPECTION TYPE:C, FS 822.5 LT SIDE, BELOW THE FLOOR, AFT SIDE OF FRAME, THE FRAME TO INTERCOSTAL ATTACH CASTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-0, 51-1-21 AND DWG 4753360.

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 51-1-21, 51-1-20D, AND 53-4-1.

Part: SHEAR TIE — CORRODED (BS 1200)

INSPECTION TYPE:C, SHEAR TIE FITTING EXFOLIATED F/S 1200 BETWEEN LONG 33R AND 34R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0, 51-1-21, AND 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 281)

INSPECTION TYPE:C, F/S 281 AT STR 33R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2 SHT 2 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 1200)

INSPECTION TYPE:C, SHEAR TIE REPAIR FITTING CORRODED AFT SIDE F/S 1200 OTBD OF LONGERON 33R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE FITTING AND DOUBLER IAW SRM 53-2-0.

Part: FITTING — CRACKED (BS 702)

INSPECTION TYPE:C, FS 702.875 FRAME, RT LWR FITTING, JUST ABOVE THE CENTER WING, IS CRACKED IN THE OUTBD RADIUS APPROX 1 INCH LONG. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-0 AND 51-1-20D.

Part: SEAT TRACK — WORN (BS1572-1591)

INSPECTION TYPE:C, SEAT TRACK FROM FS 1572 TO 1591 RBL 46 WORN BEYOND LIMITS, 4 PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION FROM FS 1550 TO 1680 IAW SRM 53-2-3, 51-1-20D, 51-1-20.

Part: SHEAR TIE — CRACKED (BS 1229)

INSPECTION TYPE:C, F/S 1229 BETWEEN STR 33R TO 34R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: SEAT TRACK — CORROSION (COCKPIT)

INSPECTION TYPE:C, F/E'S FWD SEAT TRACK HAS ENLONGATED LOCK HOLES AND INTERGRANNULAR CORROSION AT 2 FASTENER HOLES. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-0.

Part: RIB — CRACKED (WS 773)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 773 THE L/E RIB IS CRACKED AT THE UPPER AFT END. REPAIRED IAW SRM 57-2-0.

Part: SHEAR TIE — CRACKED (BS 640)

INSPECTION TYPE:C, FS 640 BTWN STR 26L AND 27L SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED FORMER IAW SRM 53-2-0 FIG 2A.

Part: SHEAR TIE — CRACKED (BS 640)

INSPECTION TYPE:C, FS 640 BTWN STR 26R AND 27R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FORMER IAW SRM 53-2-0.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:C, A/C COMPT LONGERON 27R END FITTING CORRODED F/S 70. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-0, AND 53-1-0.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:C, A/C COMPT LONGERON 28R END FITTING CORRODED F/S 70. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21, 51-3-0, AND 51-1-0.

Part: LONGERON — CORRODED (BS 58-70)

INSPECTION TYPE:C, EXFOLIATED CORROSION IN LONGERON 36, FS 58 TO 70. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-0, 51-1-21, AND DWG 5613861.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE-N/A, NR 3 ENGINE HAD FLAME-OUT AT FL 330. RAN FLAME-OUT CHECKLIST AND RECOVERED ENGINE AT FL 280 IN DESCENT. *S/D* PERFORMED T/S TREE NR 139, PERFORMED ALL ASPECTS OF ADJ/TEST PER MM 71 -00-00, PERFORMED POWER ASSURANCE RUN AND ALL PMC ON AND OFF, CHECK VBV AND VSV RIG TRAVEL CHECK, ALL OPERATES NORMALLY PER MM 71-00-00, FIG 139 PG 169-173.

Part: HYD LINE — LOOSE (RT MLG WW)

LOSS OF HYDRAULIC FLUID IN-FLIGHT DOWN TO AUXILIARY LEVEL. (RAPID). FOUND IN RT WHEELWELL LINE ON BRAKE CONTROL VALVE, B-NUT CAME LOOSE. TIGHTENED B-NUT AND LEAK CHECK LINE. NO LEAKS NOTED.

Part: BLEED AIR LINE — OUT OF POSITION (ENGINE PYLON)

INSPECTION TYPE-N/A, AIR TURNBACK DUE TO NR 3 FIRE BELL INADVERTENTLY RINGING. NR 3 FIRE DETECT CIRCUIT WOULD NOT TEST IN FIRE TEST POSITION OR SHORT CIRCUIT TEST. REMOVED AND REPLACED PYLON LOOP PER MM 26-10-00, DUE TO HISTORY AND AGE. FOUND BLEED AIR LINE ADJ TO FIRE LOOP LOOSE AND RESULTING IN HOT AIR OVER LOOP. TIGHTENED SAME. REMOVED AND REPLACED 5 LOOP CONNECTORS PER EO DC8-2610-4683-D DUE TO AGE. RAN NR 3 FIRE WARNING TEST, NO DEFECTS.

Part: FLOAT SWITCH — INOPERATIVE (HYD SYST)

EMERGENCY HYD LEVEL LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED FLOAT SWITCH IAW MM 29-20-00.

Part: SKIN — CRACKED (WS 304)

WHILE IN FOR C-CHECK, MAINTENANCE LT WING LEADING EDGE LOWER SKIN CRACKED 1 INCH AT STA XFS 304. REPAIRED PER UPS EO DC8-5720-7598-A.

Part: TRAP FITTING — CRACKED (FS 879-940)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT MAIN LANDING GEAR WHEEL WELL TRAPEZOIDAL FITTING CRACKED. REPAIRED FITTING PER UPS EO DC8-5340-0748A.

Part: ANGLE — CRACKED (VERT STAB)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS 1 INCH LONG CRACK. REPAIRED PER UPS EO DC8-5310-7585-A.

Part: SKIN — CRACKED (NR 2 PYLON TE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 PYLON TRAILING EDGE SKIN CRACKED 1 INCH LONG ABOVE FWD DRAIN TUBE RT SIDE. REPAIRED PER UPS EO DC8-5420-4308-A.

Part: SKIN — DELAMINATION (NR 3 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 3 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER MM 27-61-01.

Part: LONGERON — CRACKED (FS 857-920)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L HAS 2 CRACKS AT FS 857 AND AT FS 902 TO 920. REPAIRED LONGERON PER SRM 53-2-2 FIG 5.

Part: VANE — DELAMINATED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 4 FLAP VANE DELAMINATED ON TOP CENTER SIDE. REPLACED VANE IAW M/M 27-51-14.

Part: VANE — DELAMINATED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 2 FLAP VANE DELAMINATED ON TOP SIDE AT I/B END. REPLACED VANE IAW M/M 27-51-14.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT AND RT FORWARD NOSE GEAR DOOR HINGE CUTOUTS HAVE .5 INCH CRACKS. REPAIRED SKIN IAW SRM 53-2-0, DC8-5330-4154B.

Part: VANE — DELAMINATED (RT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 3 FLAP VANE DELAMINATED ON TOP SIDE AT I/B END. REPLACED VANE IAW M/M 27-51-14.

Part: FRAME — CRACKED (BAGGAGE DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND D-BAG/BIN DOOR LOWER AFT CORNER FRAME HAS 2 INCH CRACK. REPAIRED IAW UPS DC8-5230-6603A.

Part: EEL BATTERIES — DISCHARGED (CABIN)

WHILE ON THE GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK ASSEMBLY. SUSPECT BATTERIES DEAD, REASON UNKNOWN. OPS GOOD AFTER REMOVED AND REPLACED.

Part: EEL BATTERY — DISCHARGED (CABIN)

WHILE ON GROUND MAINTENANCE FOUND EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK ASSY. SUSPECT BATTERIES DEAD, REASON UNKNOWN. OPS GOOD AFTER REMOVED AND REPLACED.

Part: DOOR LIGHT — ILLUMINATED (RT MLG)

PILOT REPORTED EXTENDED GEAR FOR EARLY DESCENT. GEAR RETRACTED DUE TO ATC. AFTER RETRACTION, RED 'DOOR NOT LATCHED' LIGHT REMAINED ILLUMINATED WITH RIGHT 'ALT GEAR DOOR' LIGHT ILLUMINATED. RECYCLED GEAR WITH SAME INDICATIONS. MAINTENANCE CHECKED RIGHT GEAR AND DOOR AREA. NO DEFECTS NOTED. TESTED RIGHT MAIN GEAR DOOR UPLATCH IAW MM 32-31-04, PAGE 503. CHECKS OK. LUBED GEAR. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (FLIGHT DECK EEL)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS FAILED OPS TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.