N709UP

Part: ENGINE — FLAMED OUT (NR 1)

INSPECTION TYPE:N/A NR 1 ENGINE FLAMED OUT DURING CLIMB THROUGH 210 ENGINE ANTI-ICE WAS ON LIGHT TURBULENCE COMPLETED FLAME-OUT CHECKLIST. SUCCESSFUL RESTART AT 6 T/S IAW MM 71-00-00 ALL PROCEDURES PERFORMED BY PHL MX, SECURED CDP PS 3 LINE AT THE MED. REPLACED FUEL FILTER NO DEBRIS FOUND IN ORIGINAL FILTER PERFORMED PWR ASSURANCE CHECK IAW 71-00-00 P538-547 ALL PARAMETERS GOOD PER FIG 516.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 L1 FWD ENTRY DOOR LWR AFT CORNER HAS CRACK INDICATION. ROUTED OUT CRACKS IN FUSELAGE SKIN & INNER DOUBLER IAW DC8 SRM 53-2-0 FIG 15.

Part: INTERCOSTAL — CRACKED (FUSLEAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1, L1 DOOR JAMB INTERCOSTAL IS CRACKED ON BOTH ENDS. FABBED NEW INTERCOSTAL IAW DAC DWG 5597646. INSTALLED DOOR PANS AND INTERCOSTAL IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. REMOVED STEEL DOUBLER RAIN GUTTER UPPER DOOR STOP GILLINER ATTACH ANGLE AND WEB FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REMOVED CRACK IAW DC 8 SRM 53-2-0 FIG 14. ALODINED & PRIMED IAW 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-20D. REINSTALLED DOOR STOP GILLINER ATTACH ANGLE AND WEB IAW 51-1-21, 51-3-0. PLUGGED HOLES & REINSTALLED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING I AW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.

Part: CLIP — CRACKED (WING) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 O/B SKATE ANGLE CLIP BETWEEN STRINGER 62 AND STRINGER 63 CRACKED NR 1 PYLON NR 1 ALT. REMOVED AND REPLACED CLIP IAW DC8 SRM 51-1-20D.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 REPAIR AT BS 25.5 TO 39.25, L21L TO L22L FALLS INTO THE D CAT PER UPS EO DC8-5330-12800 AND REQUIRED FURTHER EVAL BY ENGINEERING BY REPAIR GOUGED BEYOND LIMITS. REMOVE OLD DOUBLER, FABBED NEW REPAIR DOUBLERS AND FILLER PER 53-2-1 FIG 7, INSTALLED PER DC8 SRM 51-1-21 AND DC8 SRM 51-1-20D.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 CABIN FLOORBOARD STA 1480-1580 POS NR 7 HAS SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-9691C.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 FLOORBOARD STA 340-460 POS 7 SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-9691C.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 STA 240 LONG 9R CRACKED. CUT OUT DAMAGED SECTION OF LONG & FABBED NEW SECTION IAW DAC DWG 5755 649-509 & DC8 SRM 53-2-2. INSTALLED SPLICES & NEW LONGERON SECTION IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 STA 320 LONG 7R CRACKED. REMOVED CRACKED LONGERON FAB NEW LONG & SPLICES IAW DC8 SRM 53-2-2 AND DAC DWG 5755649. INSTALLED NEW LONGERON AND SPLICES IAW DC8 SRM 51-1-20D & 53-2-2.

Part: DOOR — DAMAGED (AIRSTART) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 PERMANENT REPAIR ON SECOND AIRSTART DOOR IAW EO DC8-5330-12800. REPAIRED AREA IAW UPS EO DC8-5330-0793 AND DAC DRWG 08530020.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 AFT PIT STA 1270 INSULATE PAD IS CRACKED AT TORQUE BOX. REMOVED ANGLE IAW DC8 SRM 51-1-21 & 51-1-20D AND INSTALLED ANGLE IAW DC8 SRM 51-1-120D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 AFT PIT IN TORQUE BOX STA 1220-1228 BETWEEN LONG 33R TO 32R IS CORRODED. REMOVED AND REPLACED CORRODED ANGLE IAW DC8 SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLE IAW DC8 SRM 563-2-0, INSTALLED Z-ANGLES & SPLICES IAW DC8 SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 BETWEEN L34R - L35R Z-FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLES IAW DC8 SRM 53-2-0, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 FRAME AT FS 720 AND BETWEEN L35L AND 36 IS CRACKED. REMOVED AND REPLACED DAMAGED FRAME SPLICES IAW DAC DWG 9753750.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 A/C COMPT AT FS 24 ABOVE LONG 35R FRAME IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS. FABBED REPAIR PART IAW DWG DC8-53A-0II. INSTALLED PART IAW DC8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R. REPAIRED AREA IAW REO G08569.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REMOVED CRACK IAW DC8 SRM 53- 2-0 FIG 14. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM L2 LOWER AFT CORNER. REMOVED DOUBLER, PERFORMED HFEC AND NO CRACKS NOTED. FABBED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW REO G08571. SEALED AREA IAW DC8 SRM 51-1-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,457 hrs · 50,203 cycles

INSPECTION TYPE:C1 FWD ACCESSORY COMPT AT FS 660 RBL 12 MAIN CABIN FLOOR INTERCOSTAL IS CRACKED. FABRICATED DOUBLER IAW DC8 SRM 53-2-0, INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A AT FL370 NR 3 ENG BEGAN TO ROLLBACK SLOWLY. NO RESPONSE TO THROTTLE. TURNED OFF PMC, NO HELP. ATTEMPTED RESTART AT FL330, NO RESTART. ATTEMPTED 2ND RESTART AT 17000 FT, NORMAL START. PERFORMED FUEL LINE NEGATIVE PRESSURE CHECK IAW MM 28-22-12, NO DEFECTS NOTED. BEGAN T/S OF NR 3 FLAME-OUT PER 71-00-00. REPLACED FUEL FILTER IAW 73-10-01 MM AS PRECAUTIONARY. NO DEFECTS NOTED IN FILTER. ACCOMPLISHED TROUBLESHOOTING OF ENG FLAME-OUT AS PER M/M.

Part: SUPPORT — CRACKED (FUSELAGE)

INSPECTION TYPE:B LT VERT MAIN SUPPORT ANGLE ON AFT SIDE OF AFT PRESS BULKHEAD IS CRACKED IN HALF ABOUT 1 INCH FROM TOP OF BULKHEAD (AS VIEWED FROM LT ACCESS HOLE IN CANTED BULKHEAD). *S/D* LT VERT SUPPORT ANGLE P/N 57735701 1 PREVIOUSLY REPAIRED IN 4-94 IAW UPS EO DC8 5310 5665A BY INSTALLING 53 503 REV DOUGLAS FAA APPROVAL MISC 1742/GLP AND DC8.

Part: SKIN — CRACKED (WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV BOTTOM SKIN OF NR 4 MAIN I/B SIDE OF NR 3 PYLON BY PUMP HOUSING LOWER SKIN CRACKED AT FASTENER HOLE STA XCW 172.000 STR 58. COUNTERBORED HOLE TO .630 .003, FABRICATED BUSHING FOR SKIN, INSTALLED COUNTERSUNK BUSHING IAW REO G08431.

Part: STRINGER — CRACKED (WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV FOUND CRACKED STRINGER IAW HFEC PER NDT SRM 06-10-01.003 AT STA APPROX 240.000 XLS STRINGER 58. REMOVED 80 INCHES OF STRINGER AND SPLICED IN NEW SECTION OF STRINGER IAW DC8 SRM 51-1-24, 57-2-2 AND 51-1-8.

Part: FITTING — CRACKED (LT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 AFT I/B STRINGER END FITTING IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (LT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 060101. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 5613423. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (RT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV RIGHT WING NR 3 ALT TANK STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 5613423. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (LT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 FWD I/B SIDE HAS A CRACKED STRINGER END FITTING. PERFORMED HFEC TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-001. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (LT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND RPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (RT WING) · airframe 76,204 hrs · 50,010 cycles

INSPECTION TYPE:SV RIGHT WING NR 3 MAIN TANK STRINGER 51 END FITTING ON I/B SIDE IS CRACKED. REMOVED STRINGER 51 END FITTING ON I/B SIDE IAW DC8 SRM 51-3-2. LOCATED DRILLED AND INSTALLED NEW END FITTING IAW DAC DWG 5613423.

Part: CONTROL COLUMN — LACK OF LUBE (COCKPIT)

INSPECTION TYPE:N/A DURING FLIGHT CONTROL CHECK ELEVATOR EXHIBITED NON-UNIFORM MOVEMENT WHICH RELEASED FROM FORWARD POSITION AS YOKE TRAVELED FROM ITS MOST FWD POSITION AFT STOP AFT IT STOPPED ITS TRAVEL FOR 1-2 SECONDS FROM CONTINUED TO NORMAL POSITION *S/D* LUBED CONTROL COLUMN AREA AND ELEVATOR CONTROL SYSTEM. PERFORMED INSPECTION/CHECK OF ELEVATOR AND TAB ASSY. OPS CHECKS GOOD.

Part: ENGINE — FLAMED OUT (NR 1)

NR 1 ENGINE FLAMEOUT IN CRUISE FLT THEN RESTARTED. ACCOMPLISHED TROUBLESHOOTING PROCEDURES: VISUAL INSP, ROTATION OF FAN, INSPECTED MAGNETIC CHIP DETECTORS, SUMPED FUEL TANK AND INSPECTED NR 1 ENGINE FUEL FILTER, NO CONTAMINATES NOTED. REF AMM 71-00-00 AND AMM 73-10-02

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY)

SMOKE DETECTOR INOP. DEF M213526 M213526 4/20 PIT 33 SMOKE DETECTOR 2ND FROM FRONT S/N 6631 FALSE WARNING REPLACED SMOKE DETER S/N OFF 6631 ON 3094 REPLACED CM, PRECAUTIONALY OPS. CHECK O.K.

Part: SEAL — BROKEN (FIRST AID KIT)

INSPECTION TYPE:IN, FIRST AID KIT SEAL BROKEN. REMOVED AND REPLACED FIRST AID KIT.

Part: ENGINE — FLAMED OUT (NR 1)

NR 1 ENGINE FLAMED OUT AT FL310 M80 CRUISE FLT WHEN ENGINEER OPENED NR 1 CROSSFEED THEN TURNED OFF NR 2 MAIN BOOST PUMP TO TRANSFER FUEL FROM NR 1 TO NR 2 MAIN CROSSFEEDS WERE OPENED AND START SWITCH TO ALL ENGINES BOTH, RESTARTED ENGINES ***SUPPLEMENTAL MRR*** SEE LOG PAGE 526934 FOR MAINT ACCOMPLISHED. C/W MN 71-00-00 ENGINE FLAMED OUT CK AT HIGH POWER WAS UP AND P167 SYS C KS NORMAL. NO FLAME OUT. COPIED WHAT FE STATES AND SYS CHECKS GOOD

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123, STA 690 LONG 34L TIE-END DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5755058 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 640 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 160 - 180 LONG 10R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5615700 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1140 - 1145 LONG 35L INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1890 LONG 30L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4652998 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (ACCESSORY BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 SHEAR TIE IS CORRODED BEYOND LIMITS BETWEEN LONG 34L AND 34R. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5750837 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 650 LONG 31L-31R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5779913 AND SRM 51-1-21, 51-1-20D.

Part: FITTING — CORRODED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1220 LONG 31R FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5711283 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 980 - 1000 LONG 23L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1200 LONG 27L FRAME STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 1690 - 1890 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STA 1766 LONGERON 33 LT. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5644130, AND SRM 51-1-21

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1135 - 1139 INTERCOSTAL TIE FITTING IS CRACKED AT LONG 35L. REMOVED AND REPLACED FITTING IAW DWG 3758496 AND SRM 51-1-20D.

Part: FITTING — CRACKED (TAIL SKID) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 1754, TAIL SKID FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3750865, AND SRM. 51-1-20D

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1792 LONG 34L IS CRACKED. REPAIRED IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1328 LONG 21R LOWER CUSP TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755584 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1040 - 1060 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (COCKPIT FLOOR) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA -52, LBL 50 FRAME TO FLOORBEAM ANGLE IS CRACKED. FWD. SIDE OF FRAME. REPAIRED I.A.W. SRM. 53-2-0 FIG. 1B

Part: ANGLE — CORRODED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1754 - 1766 LONG 36 T-ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5753522 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1288 LONG 21L LOWER CUSP TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755584 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 RIGHT FWD SERVICE DOOR HAS A CRACKED INTERCOSTAL BETWEEN LONGERONS 16R AND 17R AT STA 148. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5615700 AND SRM 51-1-21.

Part: FRAME — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 240 FRAME IS CRACKED LONG 36-35R. REPAIRED IAW DC8-53A-011.

Part: ANGLE — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 LEFT WING L/E UPPER ANGLE IS CRACKED AT XS195. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769859 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 330 LONG 33R T-BOLT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755172 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 140 - 160 LONG 36 IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 AND 53-4-1 FIG 29.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA.1040-1060 LONG 31L SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20D

Part: FRAME — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1287 FRAME IS CRACKED AT LONG 21L. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA. 25 LONG.21R CUSP ATTACH FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3758498,AND SSRM. 51-1-20D

Part: FRAME — CRACKED (A/C BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24R. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 857 LONG 7L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123, STA 680 LONG 11L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751626, AND SRM 51-1-20D.

Part: WEB — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 UPPER CUSP CRACKED STA 1120 AT LONG 21L. REPAIRED IAW SRM 53-2-5 FIG 15.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 440 -460 LONGERON 31 RT, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257, AND SRM. 51-1-20D

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1480 AT LONG 27L VERTICAL SUPPORT IS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123, STA 630 - 640 BETWEEN LONG 35L - 35R INTERNAL SKIN IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW 8110-3 DH SK 709-687.

Part: FRAME — CRACKED (ACM BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 55 FRAME IS CRACKED AT LONG 24L. REPAIRED IAW SRM 53-2-0 FIG 2 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA. 600 - 620 LONGERON 31 LT, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20D

Part: ANGLE — CORRODED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 340 - 346 ABOVE LONG 33R TORQUE BOX ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754020 AND SRM 51-1-20D.

Part: ANGLE — CORRODED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1324 LONG 21R HAS A ANGLE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753288 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 160 LONG 8R SHORT INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 56157000, AND SRM 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C, LT WING LE UPPER RIB CRACKED AT XILD .7095 REPAIRED I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, RT WING LE RIB IS CRACKED AT XS 535. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2

Part: LONGERON — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1260 - 1280 LONG 35R IS CRACKED. REPAIRED IAW 8110-3 APPROVED DH SK 709-732.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 822 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 857 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 781 LONG 20L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779970 AND SRM 51-1-20D.

Part: FRAME — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 160 FRAME IS CRACKED AT LONG 8R. REPAIRED IAW SRM 53-2-0 FIG 2B.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 781 LONG 20L FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 781 LONG 13R FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 717 LONG 13R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 781 LONG 19L FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 1766 LONGERON 15 LT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG 4772397, AND SRM. 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA. 920 LONG. 19R INTERCOSTAL ATTACH FITTING IS CRACKED REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 3779874,AND SRM. 51-1-20D

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 717, LONGERON 11 LT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG. 4750419, AND SRM. 51-1-20D

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 879 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, RT WING LE, UPPER RIB IS CRACKED AT XFS 328.750. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 600 - 620 LONGERON 31 RT, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG 3750257, AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA. 1766 LONGERON 15 RT, END FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 4772397,AND SRM. 51-1-20D

Part: DOUBLER — CRACKED (RT WING) · airframe 75,262 hrs · 49,358 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, LT WING LE, VERTICLE RIB IS CRACKED AT XW 240. REMOVED, FABRICATED, AND REPLACED RIB I.A.W. DWG. 9753294, AND SRM. 51- 1-21,51-1-20D

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 4R END FITTING IS CRACKED, FWD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 798 LONG 13R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751642 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 340 LONG 33R-35R S-PIT AFT DOOR FRAME IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754055 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 5L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1220 INSIDE TORQUE BOX BANANA FITTING IS CRACKED AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 920 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 834, LONGERON 13 RT FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3779874, AND SRM. 51-1-20D

Part: DOUBLER — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, LT WING LE, LOWER DOUBLER CRACKED OUTBOARD OF XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769891, AND SRM. 51-1-20D

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, RT WING LE, LOWER INTERNAL DOUBLER IS CRACKED AT XFS 201.250 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5718325, AND SRM. 51-1-20D,51-1-21

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1230 LONG 35L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758495 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 759 LONG 19R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1240 LONG 35L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 360.25 AND XS 442.185. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 7R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1230 TORQUE BOX AFT BANANA FITTING LONG 33R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1260 - 1280 LONG 36 SPLICE IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 680 LONG 8R END FITTING IS CRACKED AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, STA 822, LONGERON 11 RT. END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG.4750418, AND SRM. 51-1-20D

Part: FITTING — CRACKED (CARGO BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1260 - 1280 LONG 34L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 920 LONG 11R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

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

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 857 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 717 LONG 20R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE: C1, LT WING LE INTERNAL DOUBLER IS CRACKED AT XW 485 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-20D,51-1-21

Part: RIB — CRACKED (LT WING) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 LEFT WING L/E RIB IS CRACKED AT XFS 691.25. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 1746 LONG 4L-4R CANTED CENTER SUPPORT RIB IS CRACKED AT BOTH ENDS. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 56144140 AND SRM 51-1-20D.

Part: FITTING — CRACKED (A/C BAY) · airframe 75,262 hrs · 49,358 cycles

INSPECTION TYPE:C123 STA 8 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4612650, AND SRM 51-1-21 AND 51-1-20D.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (CABIN)

INSPECTION TYPE-N/A, EMERG EXIT LIGHTS WILL NOT DISARM. RESET EMER EXIT LIGHT CIRCUIT BREAKER, OPS CKS GOOD.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHTS DISARM CHECK SWITCH IS INTERMITTENT. TIGHTENED LOOSE TERMINAL ON EMERGENCY LIGHT SWITCH, OPS CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS DID NOT ILLUMINATE DURING PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK.

Part: WEB — CRACKED (BS 680)

INSPECTION TYPE-C, STA 680 RT LWR WEB FOUND TO BE CRACKED IN RADIUS. REMOVED AND REPLACED WEB SECTION IAW DWG 9753751 AND SRM 51-1-20D.

Part: FRAME — CORRODED (BS 680)

INSPECTION TYPE-C, STA 680 FRAME HAS CORROSION AT LONG 27 TO 28R. REMOVED, FABRICATED AND REPLACED FRAME SECTION IAW DWG 9753751 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 700-710)

INSPECTION TYPE-C, STA 700 TO 710, LONGERON 31R HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 709-591.

Part: SKIN — CRACKED (BS 1400)

INSPECTION TYPE-C, THE SKIN PANEL AT THE LOWER AFT CARGO COMP AFT DOOR JAMB IS CRACKED AT THE LOWER FWD CORNER. REPAIRED AREA IAW DC8-5330-10707-A AND REFERENCE TO DHC SK 709-145.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING NR 2 MAIN TANK AFT UPPER ACCESS PANEL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 36.

Part: BULKHEAD — CRACKED (BS 680)

INSPECTION TYPE-C, STA 680 BULKHEAD HAS MANY CRACKS ON EACH SIDE OF VERTICAL STIFFENERS IN FWD ACC COMP LBL 32 TO RBL 28. REPAIRED AREA IAW SRM 53-2-5 FIG 13.

Part: RIB — CRACKED (WS 484.895)

INSPECTION TYPE:C, LT WING L/E RIB AT STA XS484.895 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 572.5)

INSPECTION TYPE:C, LT WING L/E LWR SKIN IS CRACKED AT STA XFS572.500, JUST AFT OF THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 709.5)

INSPECTION TYPE:C, LT WING L/E SKIN AT STA XFS 709.500 HAS HEAVY CORROSION AND IS CRACKED AT THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 28.

Part: SKIN — CRACKED (WS 360.25 & 379)

INSPECTION TYPE:C, LT WING L/E UPPER SKIN AT STA XFS 360.250 AND XFS 379.000 IS CRACKED AT 2 FASTENERS. REPAIRED AREAS IAW DC8-5720-7767-A.

Part: SKIN — CRACKED (WS 258)

INSPECTION TYPE:C, LT WING L/E AY STA XW258.00 IS CRACKED AT A FASTENER HOLE. REPAIRED AREA IAW SRM 57-2-1.

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE)

INSPECTION TYPE-A, FOUND ESCAPE SLIDE BOTTLE PRESSURE BELOW MINIMUMS, GUAGE READ 2300 PSI. REMOVED AND REPLACED ESCAPE SLIDE PER MM 25-60-01.

Part: FRAME — CRACKED (LT WING)

INSPECTION TYPE-C/CK, LEFT WING CENTER LEADING EDGE SECTION FRAME CRACKE. REPAIRED IAW TIMCO REO 03083 AND DC8-57-0776.

Part: SKIN — DAMAGED (BS 260)

INSPECTION TYPE-C, EXT FUSE STA 260, L18 TO 22R, FASTENERS PULLING THROUGH AND SLIGHT BULGE ON SKIN. REPAIRED IAW TIMCO REO NR 03063, REV A AND DC8-53-1786.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C, R/W CTR L/E BOTTOM INBD AREA IS CRACKED ON BOTH SIDES OF DRAIN HOLE. REPAIRED IAW TIMCO REO NR 03051 AND DC8-57-0777.

Part: BULKHEAD — CORRODED (BS 1766)

INSPECTION TYPE-C, AFT PRESS BULKHEAD STA 1766 HAS CORROSION AROUND VHF 1 RUN G FEED THROUGH DISCOUNT COUPLING. REPAIRED IAW TIMCO REO NR 03035, REV A AND DC8-53-1787.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-C/CK, LEFT WING CENTER LEADING EDGE SECTION CRAKED 2 PLACES, BOTTOM LEADING EDGE BETWEEN ACCESS PANELS DOT E734 DC8-57-0778. CUT AND REMOVED DAMAGED SECTION OF THE 1 AND -27 DOUBLER AREA, FABBED -31 AND -27 AND EXTERNAL DOUBLER AND STRAPS FOR -31 DOUBLER IAW TIMCO REO 03077. FABBED REPAIR BUSHING IAW DAC DRAWING 47D9981. ROUTED OUT CRACKED AREA ON SKIN IAW DC8 SRM 51-1-5. INSTALLED BUSHING IAW DC8 SRM 51-1-25, INST -31 AND DOUBLER AND STRAPS IAW DC8-57-0778.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-C/CK, LEFT HAND LEADING EDGE WING SECTION OUTBOARD END OF SLOT DOOR CRACKED. REPAIRED IAW REO 03029 AND DC8-57-077.

Part: SPAR CAP — CRACKED (BS 857)

INSPECTION TYPE-C, LT MLG WHEEL WELL, WING REAR SPAR LOWER CAP AT FASTENER 6 INCHES OUTBOARD FROM KEEL BEAM STA 857 HAS A CRACK. REMOVED FASTENERS (10) ALONG REAR SPAR AFT SIDE, REAMED DAMAGED HOLE TO .375, CUTOUT CRACKED AREA, FABRICATED REPAIR STRAP, FILLER, SHIM AND BUSHING IAW REO-0289, REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED BUSHING, REPAIR STRAP, FILLER AND SHIM IAW REO-02989 AND SRM DC8 51-3-0. UPS EFN DC8-57-07-69.

Part: CIT SENSOR — INTERMITTENT (NR 1 ENGINE)

INSPECTION TYPE-N/A, NR 1 ENGINE FLAME-OUT AT FL280 W/LIGHT CHOP. ENGINE RESTARTED USING FLAME-OUT CHECKLIST PROCEDURES. PERFORMED FUEL FEED LINE NEG PRESS CH PER MM 28-22-12 SYST HELD PRESS FOUND NO LEAKS. REMOVED AND REPLACED CIT SENSOR IAW 73-20-0, OPS CHECKS GOOD ON GROUND. S/N ON WYG29523, S/N OFF WYG34034.

Part: ENGINE — FLAMED OUT (NR 1)

INSPECTION TYPE N/A, AT TOP OF DESCENT WITH BALANCED FUEL AT 390 NR 1 ENGINE FLAMED OUT. INITIATED FLAME-OUT CHKLIST. RESTART NORMAL WITH NO EXCESSIVE OR ERRATIC ENGINE INDICATIONS. ALL BOOST AND FEED PUMPS WERE ON AND WORKING. PERFORMED HIGH POWER ENGINE WITH SNAP DECELL TO GROUND IDLE AND FLIGHT IDLE. DID DECELL AND POWER RUN WITH OUT BOOST AND FEED PUMPS. TESTED BOOST AND NASH PUMP IAW 73-10-01. ALL PUMPS CHECKED GOOD, COULD NOT GET FLAME-OUT.

Part: EXC ROPE COVER — OUT OF ADJUST (COCKPIT)

MAINTENANCE REPORTED, CAPTAINS ESCAPE ROPE WILL NOT REMAIN SECURE IN STOWED POSITION. PERFORMED INTERIM REPAIR TO CAPT'S ESCAPE ROPE COVER AND DEFERRED PER EO DC8-2510-7055 A FINAL REPAIR REQUIRED PRIOR TO FIRST FLIGHT ON 3-4-96.

Part: SKIN — CRACKED (LT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 1 PYLON CUT OUT AT WING LEADING EDGE HAS A 4 INCH CRACK. REPAIRED PER SRM 57-2-1A, FIG. 1, AND UPS E.O. DC8-57-371.

Part: FRAME — CRACKED (NR 2 CARGO DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 BELLY DOOR HAS A 5.75 INCH LONG CRACK AT LOWER FRAME. REPAIRED FRAME PER U.P.S. E.O. DC8-5230-7357-A.

Part: LONGERON — CORRODED (FS 1540-1560)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R AT STATION 1540 - 1560. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2.

Part: LONGERON — CORRODED (BS 1540)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L AT STATION 1540. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2.

Part: SKIN — CRACKED (RT LE SLOT)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT WING OUTBOARD MID-SLOT PANEL. MAINTENANCE REPLACED THE SLOT PANEL PER MM 27-80-02.

Part: SKIN — CORRODED (FUSELAGE)

WHILE IN FOR B-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN APPROX 12 INCHES FWD OF E AND E COMPARTMENT RIGHT SIDE. REPAIRED IAW EO DC8-5330-7189.

Part: BULB — FAILED (GEAR INDICATION)

PILOT REPORTED, GEAR DOWN LT LANDING GEAR LIGHT NOT ILLUMINATED. CHANGED BULBS AND RECYCLED GEAR. COMMENT NOTED BY MAINTENANCE INPECTED AND CHECKED SWITCH, PLUG, AND SOCKET, OK. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: BEAM — CRACKED (AFT BLKHD)

(SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD TOP SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A.

Part: BEAM — CRACKED (AFT BLKHD)

(SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD BOTTOM SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A.