N806UP

Part: SWITCH — INTERMITTENT (MLG) · airframe 4,443 hrs · 3,684 cycles

LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE SELECTED UP. GEAR HANDLE SELECTED DOWN AND GEAR INDICATIONS 3 GREEN. GEAR RELAY CIRCUIT BREAKER POPPED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED DEFECTIVE LEFT GEAR SQUAT SWITCH. SUCCESSFUL OPERATIONAL CHECK FLIGHT PERFORMED. AIRCRAFT RETURNED TO SERVICE.

Part: BYPASS VALVE — INTERMITTENT (LT ENGINE) · airframe 2,904 hrs · 2,426 cycles

LEFT ENGINE HAD HIGH OIL TEMPERATURE DURING CRUISE. 97C AND CLIMBING. DESCENDED TO FL250, TEMPERATURE DECREASED FOR A FEW MINUTES AND BEGAN CLIMBING AGAIN. EMERGENCY DECLARED AND DIVERTED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT ENGINE OIL COOLER THERMOSTATIC BYPASS VALVE. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — FAILED (LEFT) · airframe 2,780 hrs · 2,318 cycles

LEFT BRAKE PEDAL AND LEFT BRAKE FAILED WHEN OPERATED FROM COPILOTS SIDE. MAINTENANCE REPLACED THE LEFT INBOARD AND OUTBOARD BRAKE ASSEMBLIES WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DEFECTIVE (NLG) · airframe 2,567 hrs · 2,112 cycles

NOSE GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. PERFORMED EMERGENCY GEAR EXTENSION AND GO AROUND FOR TOWER CONFIRMATION OF GEAR EXTENSION. LANDING WAS UNEVENTFUL. AIRCRAFT WAS FERRIED FROM THE BAHAMAS TO TAMPA FLORIDA FOR MAINTENANCE. MAINTENANCE REPLACED THE NOSE GEAR DRAG BRACE DOWNLOCK SWITCH. GEAR SWINGS PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 1,320 hrs · 1,101 cycles

GEAR EXTENSION, LT MAIN GEAR GREEN INDICATION DID NOT ILLUMINATE. A GO AROUND WAS INITIATED & CHECKLIST PROCEDURES FOLLOWED WITH NO HELP. AN EMER WAS DECLARED & LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY TO AN INOPERATIVE LT MAIN GEAR INDICATOR LIGHT BULB. BULB WAS REPLACED & OPERATIONAL CHECKED OK. ACFT WAS RTS.

Part: BLADDER — LEAKING (FUEL SYSTEM) · airframe 292 hrs · 264 cycles

FUEL LEAK FROM RT GEAR WELL AT 2 - 3 DROPS PER SECOND. FUEL BLADDER LEAKING. THIS ACFT HAD THE FUEL BLADDERS REPLACED.

Part: TRANSPONDER — MALFUNCTIONED (NR 1) · airframe 93 hrs · 85 cycles

AIRCRAFT DEPARTED, CREW SWITCHED THE NR 1 TRANSPONDER FREQUENCY FROM TOWER TO DEPARTURE & WAS NOTIFIED THAT THEIR TRANSPONDER SIGNAL WAS INTERMITTENT. CREW SWITCHED OVER TO THE NR 2 TRANSPONDER & DEPARTURE NOTIFIED THEM THAT THE NR 2 TRANSPONDER SIGNAL WAS NOT BEING RECEIVED. ACFT RETURNED. PERFORMED AN OPS TEST ON THE NR 1 & 2 TRANSPONDERS WITH NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE & AN CHECK FLIGHT WAS ACCOMPLISHED WITH NO DEFECTS NOTED. ACFT HAD SEVERAL SUCCESSFUL FLIGHTS SINCE THE RTS.

Part: SKIN — CORRODED (BS 70)

CORROSION RT LWR FUSE AFT OF THE E&E DOOR APPROX. STA 70. STARTED ECA FORM 011382. INSTALLED TIME LIMITED REPAIR IAW EO DC8-5330-29905A. ALL WORK PERFORMED ON ECA FORMS 011382 AND 011385. REPAIR DEFERRED FOR 24 MONTHS.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

ON PRE-DEPARTURE CK, EMERGENCY EXIT LIGHT CK FAILED. FOUND SW IN ON POSITION. REPLACED AND TESTED BATTERY PACK IAW 33-50-01-2 CKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2 PARA 4. OPS CHECK GOOD.

Part: LIGHT — INTERMITTENT (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INTERMITTENT ON OPS CHECK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MM 33-50-02-2. OPS CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-01-2 AND TESTED.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-02-2.

Part: SLIDE — UNSECURE (PAX DOOR)

ESCAPE SLIDE CAME LOOSE. RESECURED ESCAPE SLIDE TO FWD ENTRY DOOR B DC8 25-60.

Part: LIGHT — NO TEST (COCKPIT)

EMERGENCY LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY PER AMM 33-50-01. OPS CK NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND TESTED OK PER MM 33-50-01-2.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD PER MM 3-50-01-2.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 STA 219 LT FLAP FOUND O/B VERT DOUBLER AND LWR ATTACH ANGLE GOUGED OUT OF LIMITS. REMOVED DAMAGED DOUBLER AND ATTACH ANGLE AT LT FLAP STA 219 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT REPAIR WEB, STRAP AND REPAIR ANGLE IAW DWG 5655988, DC8-5350-7876-A, AND SRM 57-02-00 FIG 2.

Part: FITTING — CRACKED (WING) · airframe 73,559 hrs · 28,643 cycles

INSPECTION TYPE-C1-3 BOTH STRINGER END FITTINGS ON STRINGER 51 AT XRS 74 ARE CRACKED NR 2 MAIN TANK. REMOVED BOTH STRINGER END FITTINGS AT STR 51 XRS 74 NR 2 MAIN TANK IAW SRM 51-1-20D. LOCATED AND DRILLED UP, AND INSTALLED 2 END FITTINGS AT STR 51 AT STA XRS 74 NR 2 MAIN TANK IAW SRM 51-1-8, 51-3-2 AND SRM 51-1-20D.

Part: FITTING — CORRODED (FS 280 L33-34L) · airframe 73,553 hrs · 28,643 cycles

BATH TUB FITTING EXFOLIATED OUT OF LIMITS AT A-PIT TORQUE BOX STA 280 L33L-L34L. REMOVED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00, AND SRM 51-1-20D. DRILLED UP AND INSTALLED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00-0.

Part: SKIN — CORRODED (FS1350-1490 L31R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1-3 D-PIT BELLY SKIN REQUIRES REPLACEMENT DUE TO OUT OF LIMITS CORROSION AT L35R-36 STA 1490-1350. REMOVED AND REPLACED BELLY SKIN AT STA 1490-1350 L31L-L31R IAW SRM 51-1-20D, 51-1-21.

Part: ATTACH FITTING — CRACKED · airframe 735,532 hrs · 28,643 cycles

INSPECTION TYPE:C1/3 NR 1 MAIN TANK REAR SPAR ATTACH TEE FITTING AT XW-408 HAS A 4 INCH CRACK. REMOVED AND REPLACED ATTACH TEE FITTING AT XCW-408 NR1 MAIN TANK.

Part: SPLICE — CRACKED (FS1260-1280 L35L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1,3 LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L35L. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 60 HOLE APPROX STA 1800 LONGERON 24L END FITTING IS CRACKED. REMOVED DRILLED UP, AND INSTALLED END FITTING AT STA 1800 L24L IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS1270 L34R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 CRACKED LONGERON L34R FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 - 1350 L34R IAW SRM 51-1-20D.

Part: DRAG ANGLE — CRACKED (NR 2 PYLON IB) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1, 3 POSSIBLE CRACKS ON BULKHEAD FWD OF CENTER SPAR UPPER BOLT IB DRAG ANGLE. REMOVED, FABRICATED AND INSTALLED DRAG ANGLE IAW SRM 51-1-21, DWG 5615767 AND 51-1-20D.

Part: LONGERON — CRACKED (FS 905 L9L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 MAIN CABIN LONGERON END FITTING CRACKED AT STA 905 L9L. REMOVED AND REPLACED LONGERON END FITTING AT STA 905 L9L IAW SRM 51-1-20D, AND SRM 51-01-23-0.

Part: LONGERON SPLICE — CRACKED (FS 900-920 L1) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LONGERON SPLICE FITTING CRACKED AT STA 900 TO 920 L1. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 900 TO 920 LONGERON 1 IAW SRM 51-01-20D, AND SRM 51-01-20D.

Part: LONGERON — CRACKED (FS 1270 L35L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 CRACKED LONGERON L35L FS 1270 C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 L35L IAW SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FS 120 LBL20) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 9 SHEARED RIVETS ON FINGER DOUBLER IN COCKPIT SUBFLOOR, STA -130 LBL 20. REMOVED CORRODED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBL 20 IAW SRM 53-03-03 FIG 006 AND SRM 51-01-20D.

Part: LONGERON — CRACKED (FS 1270 L36) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 CRACKED LONGERON AT L36 FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON FROM STA 1270 - 1350 L36 IAW SRM 51-1-20D.

Part: SKIN — CORRODED (FS1660-1680 L31R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1 3 HEAVY CORROSION BETWEEN FUSE SKIN AND FINGER DOUBLER AT STA 1670 L31R IN AFT ACC COMPT. REPAIRED FUSELAGE SKIN FROM FS 1660 TO 1680 IAW SAA EA 008-5330-01- A0329 REV A AND UPS RA DC8-53-20579.

Part: SPLICE — CRACKED (FS 200-180 L31L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 L31L AT STA 200 TO STA 180 SPLICE IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 200-180 L31L IAW SRM 51-1-20D, AND SRM 51-03-02.

Part: FITTING — CRACKED (FS 270 L34R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1, 3 CRACKED BATHTUB FITTING AT FS 270 L34R IN A-PIT. REMOVED AND REPLACED BATHTUB FITTING. IAW SRM 51-1-20D

Part: LONGERON — CORRODED (BS 270 L33L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1,3 AT STA. 270 L33L IS BLOWN OUT. REMOVED WEB, BATHTUB FITTING AND LONGERON. FABRICATED AND INSTALLED LONGERON, SPLICE FITTING,BATHTUB FITTINGS AND REPAIR ANGLES. IAW SRM 51-1-20D, 51-1-21,53-02-00 FIG. 10,51-3-2,53-02-02, DWG 9754913

Part: DOUBLER — BROKEN (CARGO DOOR) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1/3 INTERNAL DOUBLER BROKEN AT 6:00 AND 12:00 POSITION UNDER EXTERIOR MAIN CARGO DOOR ACCESS PLATE FOR NR 4 LATCH FABRICATED AND INSTALLED -1 AND -2 INTERNAL DOUBLERS IAW SAA EA 008-5320-01-A0331 DTD.05 AUG 2006 MFG DRAWING NR 5772790-637 REV CW-00 AND SRM 51-3-0.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 73,553 hrs · 28,643 cycles

C1-3 FE'S FWD SEAT TRACK LOCK PINS HOLES WORN. REMOVED AND REPLACED FE'S FWD SEAT TRACK IAW SRM 51-03-00,51-01-22 AND SRM 51-03-00.

Part: SHEAR TIE — CRACKED (FS 1740 L14L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 MAIN CABIN STA 1740 L14L SHEAR TIE CRACKED. REMOVED SHEAR TIE AT STA 1740 L14L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIE AT STA 1740 L14L IAW SRM 51-03-02, 51-1-20D AND DWG 5772706.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 73,553 hrs · 28,643 cycles

C1-3 2ND OBSERVERS AFT SEAT TRACK LOCKPIN HOLES WORN. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-3-0 51-01-24.

Part: RIB — CRACKED (LT WING) · airframe 73,553 hrs · 28,643 cycles

LT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK ON RIB ANGLE IAW SRM 57-2-0 AT STA XFS 304. FABRICATED AND INSTALLED REPAIR ANGLES AT STA L/WING STA XFS304 IAW SRM 57-02-0, AND 51-01-20D.

Part: RIB — CRACKED (LT WING) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT CENTER WING L/E UPPER RIB CRACKED AT XFS 497. STOP DRILLED CRACKED RIB AT LT L/E WING STA XFS 497 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED DOUBLERS ON RIB AT LT L/E WING STA XFS 497 IAW SRM 57-03-03 FIG 5, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 35 L36) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C1,3 AIR CONDITIONING COMPT, L36 IS CORRODED AND CRACKED AT STA.35. REMOVED, FABRICATED AND INSTALLED LONGERON AT FS 35 L36.

Part: RIB — CRACKED (L/E SLAT) · airframe 80,092 hrs · 25,938 cycles

RT CENTER LE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D. SAT PREVIOUSLY SENT THIS WRITEUP WITH WRONG TAIL NR.

Part: RIB — CRACKED (LT WING) · airframe 73,553 hrs · 28,643 cycles

RT CENTER L/E UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK ON RIB AT LT L/E STA XFS 415 IAW SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E STA XFS 415 IAW SRM 57-03-03 FIG 5 AND SRM 57-02-00.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

FOUND LT CENTER LE UPPER RIB CRACKED AT XS454. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2 AND 51-1-20A.

Part: SPAR CAP — CRACKED (FS 857 LBL 36) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT MLG WHEEL WELL FRONT SPAR CAP STA 857 LBL 36 HAS A CRACK BETWEEN BOLTS. REPAIRED LT MLG WHEEL WELL FRONT SPAR CAP AT STA 857 LBL 36 IAW SAA EA NR 008-5710-01-A0299, UPS EO NR DC8-5710-24870, DOUGLAS DWG SRO 8570009.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1,3 LT WING CTR LE LWR IB CRACKED AT XFS 347. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 57-02-03 FIG 005 AND 51-1-20D.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

C1, 3 RT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS409. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-1-21, 57-02-00 FIG 2, 57-03-03 FIG 5.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

FOUND LT CTR LE UPPER RIB CRACKED AT XS 491. SET HOLE TERMINATED CRACK. FABRICATED AND INSTALLED 2. REPAIR DOUBLERS IAW SRM 57-02-00 FIG 002 SHT 2, 51-01-20D AND 51-1-15.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

LT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES 2 IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 73,553 hrs · 28,643 cycles

LEFT WING CENTER L/E RIB CRACKED AT XFS 328. STOP DRILLED CRACK AT LT WING L/E RIB AT STA XFS 328 IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E WING STA XFS 328 IAW SRM 57-03-03 FIG 5, AND SRM 57-02-00.

Part: FITTING — CRACKED (FS 65 L31L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LONGERON END FITTING CRACKED AT STA 65 L31L. REMOVED AND REPLACED LONGERON END FITTING AT STA 65 L31L IAW SRM 51-3-0, 51-1-21, AND SRM 51-3-2.

Part: LONGERON — CRACKED (FS 1750 L14R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 RT AFT MAIN CABIN FS 1750 L14R CRACKED AT CANTED FRAME REMOVED CRACKED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FI FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05-03-0.

Part: FITTING — CRACKED (FS 680 L6L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT MAIN CABIN FS 680 FWD LONG END FITTING 6L IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-03-00, 51-1-20D, AND SRM 51-02-23.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

C1,3 LT OB LEADING EDGE UPPER RIB CRACKED AT XFS 752. FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 21-1-20D AND 51-1-15.

Part: FITTING — CRACKED (BS 1690 L35L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE: C 1-3 MAIN CABIN STA.1690 LONGERON 35L END FITTING CRACKED REMOVED AND REPLACED LONGERON 35L END FITTING AT STA.1690 IAW SRM 51-1-21 AND SRM 51-1-20D.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

C1, 3 LT OB LEADING EDGE RIB CRACKED AT XFS 746 UPPER RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 51-01-20D AND 51-01-15.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT MLG WHEEL WELL STA 940 LBL 63 PRESSURE DECK SKIN IS CORRODED AND CRACKED. CUT OUT DAMAGED AREA IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW SAA EA 008-5320-01-A0300, UPS EO DC8-5330- 24740-A, DOUGLAS DWG 5645332 REV BU, BOEING MSG 1-212089989, BOEING ROD SKETCH 06-07-18-003, AND FAA FORM 8100-9.

Part: LONGERON — CRACKED (FS1766-1725 L14L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT AFT MAIN CABIN LONG 14L CRACKED AT CANTED FRAME INTERSECTION FS 1734. REMOVED CRACKED LONGERON AT STA 1766 - 1725 L14L IAW SRM 53-02-02-0 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION SPLICE AT STA 1766 - 1725 L14L IAW SRM 53-02-02-0 FIG 10, 53-05-03-0, AND DWG DC8-53B-009.

Part: LONGERON — CRACKED (BS 1736 13L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1 LT AFT MAIN CABIN LONGERON 13L CRACKED AT CANTED FRAME INTERSECTION STA 1736. REMOVED FABRICATED AND INSTALLED LONGERON SECTION AT STA 1729 - 1747 LONGERON 13L IAW SRM 53-02-02-0 FIG 10 SRM 51-01-21-0 AND DRAWING DC8 53B-0009.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

C1, 3 RT OB LEADING EDGE LWR RIB CRACKED AT XFS 734. FABRICATED AND INSTALLED STACK ANGLE REPAIR IAW SRM 57-02-00 AND 51-1-20D.

Part: LONGERON — CRACKED (FS 1734 L15L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 FS 1734 L15L CRACKED AT CANTED FRAME INTERSECTION. REMOVED LONGERON SECTION FROM STA 1748 - 1734 L15L IAW SRM 53-02-02-0 FIG 10. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1748-1734 IAW SRM 53-02-02-0 FIG 10, AND DWG DC8-53B-009.

Part: RIB — CRACKED (WING) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 RT CENTER LE UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK ON UPPER RIB AT XFS 297 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED DOUBLERS AT RT WING STA XFS 297 IAW SRM 57-02-00 FIG2, AND SRM 57-03-00 FIG 13.

Part: RIB — BROKEN (RT WING) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 RT CENTER L/E RIB BROKEN AT STA XW 408. REMOVED AND REPLACED RT CENTER L/E RIB AT STA XW 408 IAW SRM 51-03-00-0, 51-1-20D AND DWG 5769857.

Part: LONGERON — CRACKED (FS 1746 L16L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT AFT MAIN CABIN LONG 16L CRACKED AT CANTED FRAME INTERSECTION FS 1746. REMOVED LONGERON SPLICE SECTION AT STA 1766-1738 L16L IAW SRM 53-02-02-0 FIG 10. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1766-1738 L16L IAW SRM 53-02-02-0 FIG 10 51-01-20D-0, DWG DC8-53B-009.

Part: RIB — CRACKED (L/E SLAT) · airframe 80,092 hrs · 25,938 cycles

RT OB LE UPPER RIB CRACKED AT XFS 834. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (L/E SLAT) · airframe 73,553 hrs · 28,643 cycles

RT OB LE LWR RIB CRACKED AT XFS 796. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00 AND 51-1-21.

Part: ATTACH ANGLE — CRACKED (FS 1766 L6L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 MAIN CABIN FS 1766 LT UPPER AREA OF APB INTERCOSTAL ATTACH ANGLE CRACKED AT L6L. REMOVED, FABRICATED, AND INSTALLED ATTACH ANGLE CLIP AT FS 1766 APB L6L IAW SRM 51-1-21, 51-03-07, AND SRM 51-01-20D.

Part: SKIN — CRACKED (FS 1702 L14-17L) · airframe 73,559 hrs · 28,643 cycles

FUSELAGE SKIN WHERE VERTICAL ATTACHES FUSELAGE STA 1702 BETWEEN L14L-L17L CRACKED AT 2 FASTNERS. CUT OUT DAMAGED SKIN AT STA 1702 L14L-L17L IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED -1, -2 FILLERS, AND -3 DOUBLER IAW SAA EA NR 008-5320-01-A0334, UPS EO NR DC8-5330-24864-A, BAC MSG NR 1-216250620-2 DWG 5649327 REV F AND FAA FORM 8100-9.

Part: LONGERON — CRACKED (FS 1742 L17L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 AFT MAIN CABIN FS 1742 LONG 17L CRACKED IN RADIUS LWR INBOARDD FLANGE. REMOVED LONGERON SECTION AT STA 1745-1734 IAW SRM 53-02-02-0 FIG 10. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1745-1734 L17L IAW DWG DC8-53B-009, AND SRM 53-02-02-0 FIG 10, AND SRM 53-05-03.

Part: LONGERON — CRACKED (FS 1756 L13L) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 MAIN CABIN LT AFT AREA FS 1756 L13L IS CRACKED. REMOVED CRACKED LONGERON AT STA 1766 - 1747 L13L IAW SRM 53-02-02-0 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1766 - 1747 IAW SRM 53-02-02-0 FIG 10 AND DWG DC8-53B-009 REF S/O 7411676.

Part: BULKHEAD — CRACKED (FS 1766) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 LT AFT MAIN CABIN APB STA 1766 LBL 30 APROX 48 INCHES ABOVE FLOOR IS CRACKED. CUT OUT DAMAGED AREA AT FS 1766 LBL 30 IAW SAA EA 008-5305-01- A0305. FABRICATED AND INSTALLED REPAIR PARTS IAW SAA EA 008-5305-01- A0305, UPS EO DC8-5330-247787-A,BOEING MSG 1-212213339-7, AND FAA FORM 8100-9.

Part: BULKHEAD — CRACKED (BS 1766) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 AFT MAIN CABIN RT SIDE OF APB CRACKED AT RBL 30-33 AND FROM RBL 36-40 APPROX 60 INCHES ABOVE FLOOR LINE. CUT OUT CRACKED AREA IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -25 AND -27 DOUBLER, -9, -11 AND -19 FILLER IAW SRM 53-2-5 FIG 14A, 51-1-20D AND SRM 51-1-21.

Part: FITTING — CRACKED (FS 780) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 MAIN CABIN BOOT FITTING CRACKED AT STA 780 LT. REMOVED AND REPLACED BOOT FITTING AT STA 780 LT IAW SRM 51-01-20D 51-1-21, AND SRM 51-01-24.

Part: LONGERON — CRACKED (FS 1734 L15R) · airframe 73,553 hrs · 28,643 cycles

INSPECTION TYPE:C1-3 RT SIDE OF AFT MAIN CABIN FS 1734 L15R CRACKED AT CANTED FRAME INTERSECTION. REMOVED CRACKED LONGERON SECTION AT STA 1734 L15R IAW SRM 51-01-21-0 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1734 L15R IAW SRM 53-05-03-0, AND 53-02-02-0 FIG 10.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE: PFLT, BELLY SKIN BULGED/CRACKED AREA OF PIT 34 DOOR CUTOUT AT LONG 35R & LR 36. ACCCOMPLISH LFEC INSP OF AREA FOUND INDICATION OF 30 PERCENT DEFECT IN 3 AREAS (MARKED) PER ENGINEERING REQUEST ACCOMPLISHED ETLF 6-10-02 TO MAP AREA OF DEFECT INSTALLED A REPAIR DOUBLER AS PER EO DC8 5330-19859A THIS CLOSES D274572.

Part: REGULATOR — BYPASSING (OXYGEN SYS)

2ND OBSERVER O2 REGULATOR BY-PASSING AIR IN FLIGHT, LOST O2 EMERGENCY SYSTEM. FOUND FIRST OBSERVERS SUPPLY LINE TO REGULATOR LEAKING AT FITTING, DAMAGED. THIS FITTING WAS DAMAGED AT TEE FITTING BEHIND 2ND OBSERVERS REGULATOR. REMOVED AND REPLACED SUPPLY HOSE, OPS CHECK GOOD. LEAK CHECK GOOD.

Part: SEAT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A FE SEAT WILL NOT LOCK IN POSITION. R&R SEAT OPS CK GOOD W/REF TO MM 25-11-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 STA 680 AT LBL 63 CENTER WING BOX TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3642974, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1160 AT LONG 34R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 STA 320 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 29L AND 30L. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 STA. 8 TO -25 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW DWG 5612298, AND SRM 51-1-21, 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 STA -52 TO -67 FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT LBL 60. REMOVED FINGER DOUBLER, CUTOUT DAMAGE ON WEB, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW SR08530036.

Part: FITTING — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 STA 1660 FRAME TO CUSP FITTING IS CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4773161, AND SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FREEZE PLUG AND DOUBLER IAW SRM 57-2-1 FIG 10.

Part: SKIN — CRACKED (RT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FREEZE PLUGS IAW SRM 57-2-1 FIG 10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 MAIN CABIN FLOORBEAM IS CORRODED BEYOND LIMITS AT STA 920 AT RBL 65. CUTOUT CORRODED SECTION OF FLOORBEAM, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED FLOORBEAM SECTION IAW UPS ENGINEERING FILE NUMBER DC8-53-20237, AND SAA SK806-663.

Part: PAN — CRACKED (RUDDER) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LOWER RUDDER PANS ARE CRACKED AT 2ND AND 3RD HINGE FROM BOTTOM AT XE 77 AND XE 149. REMOVED, FABRICATED, AND REPLACED PANS IAW DWG 5656233, AND SRM 51-1-21, 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 R2 DOOR UPPER AFT CORNER SKIN IS CRACKED AT STA 1660 AT LONG 11R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRM 53-2-0 FIG 16.

Part: SKIN — CORRODED (LT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 366.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-2-0 FIG 7, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2- 1 FIG 38.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 CABIN FLOOR SEAT TRACK IS WORN AND BROKEN AT LBL 45 STA 1590-1600. REMOVED DAMAGED SEAT TRACK STA 1590 TO 1680 LBL 45, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A.

Part: RIB — CRACKED (LEFT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 616.25. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 15. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15, AND EO DC8-5320-17264-A, AND SAA SK 806-198.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE R1 DOOR LOWER AFT CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 14. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AROUND EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND TRIPLER IAW SRM 53-2-0 FIG 14.

Part: SKIN — CRACKED (LEFT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 BULKHEAD FWD OF RT WHEEL WELL STA 851 RBL 50 L ANGLE FITTING IS CRACKED. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER DC8 53-2-0 FIG 18. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT PREVIOUS CUTOUT, FABRICATED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18.

Part: SKIN — CORRODED (LEFT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION IB OF XFS 710. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 COMPLY WITH MPI P 13516;PERM REPAIR TO DENT STA -80 TO -74 ON LEFT SIDE ABOVE CUSP ANGLE. REMOVED INTERIN REPAIR, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: HYDRAULIC LINE — LEAKING (LT MLG)

INSPECTION TYPE:N/A ATB DUE TO HYDRAULIC FAILURE. WHILE MANUALLY PUMPING OPEN CARGO DOOR, NOTED HYD LEAK IN LT W/W. TRACED LEAK TO FLEX LINE ON DOWNLOCK BUNGEE, LEAKING JUST DOWNSTREAM OF FITTING ON BUNGEE. FOUND FLEX LINE LEAKING GOING TO LT GEAR DOWNLOCK REMOVED AND REPLACED SAME. LEAK CHECK GOOD. SERVICED HYD TO FULL. INSPECTED HIGH PRESS FILTERS OK REMOVED AND REPLACED LT AND RT HYD PUMP CAE DRAIN FILTERS IAW M/M 29-00-00 PG 218. OK FOR SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 72,748 hrs · 27,969 cycles

INSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGERS 9,10,12. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE AT XRS 74 STRINGERS 9,10,12, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS ENGINEERING FILE NUMBER DC8-57-20054, AND SAA SK 806-503.

Part: OXYGEN BOTTLE — LEAKING (COCKPIT)

INSPECTION TYPE:IN BOTH 02 SYS LEAKING. *S/D* REMOVED AND REPLACED BOTH CREW AND COURIER 02, LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, DURING BITE CHECK NO EMERGENCY EXIT LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY AND RELAY UNIT.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT TEST DURING PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT, EMERGENCY LIGHTS VERY DIM. DISARM LIGHT DOES NOT ILLUMINATE WHEN DISARMED. REMOVED AND REPLACED BATTERY PACK AND SECURED ELECTRICAL CONNECTOR. OPS CK OK.

Part: SKIN — CORRODED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL SKIN IS CORRODED BEYOND LIMITS AT XFS572.5 BELOW INTERNAL DOUBLER. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E LOWER ATTACH FLANGE FITTING IS CRACKED AT XFS 60. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1520 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 50. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 806-429.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1540 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 50. REPAIRED IAW 8110-3 APPROVED DH SK 806-428.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, VERTICAL STAB NR 3 RUDDER DAMPER ATTACH POINT FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3651256, AND SRM 51-3-0.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, MAIN CABIN FLOORBEAM AT STA 1560 LBL 50 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 806-427.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, VERTICAL STAB L/E FORMER IS CRACKED AT ZFS 171 LEFT SIDE. REPAIRED FORMER IAW SRM 55-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 416.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 341.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: TRIPLER — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING CENTER L/E UPPER TRIPLER IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED TRIPLER IAW DWG 5769891, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING STA XW 727 STRINGER 3 ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4614390, AND 8110-3 APPROVED DH SK 806-014, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 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 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 798 LBL 50 ANGLE IS CRACKED UPPER SIDE CENTER FUEL TANK. REMOVED AND REPLACED ANGLE IAW DWG 3643112, AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT NR 1 STUBWING UPPER RIB IS CRACKED AT XS 520. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT NR 2 STUB WING VERTICAL ANGLE IS CRACKED AT XS250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (CARGO BAY) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 200 LONG 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW 8110-3 APPROVED DH SK 806-078, AND SRM 51-1-20D, 51-1-21.

Part: TRIPLER — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER TRIPLER IS CRACKED AT XOLDI 6.225 AFT OF SLOT BOX. REMOVED, FABRICATED, AND REPLACED TRIPLER IAW DWG 5769891, AND SRM 51-1-20D.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 150. REPAIRED RIB IAW SRM 55-2-0 FIG 2.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL WRAP AROUND DOUBLER IS CRACKED AT XFS 710 I/B SIDE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769572, AND SRM 51-1-21.

Part: FITTING — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING AT XRS 90 HAS A CRACKED SPLICE FITTING AT STRINGER 16 TO FRONT SPAR. REMOVED, FABRICATED, AND REPLACED FITTING IAW DEG 3645275, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1200 LONG 27L DOOR STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 347.75, 354, 360.25, 410.25, 497.491. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E RIBS ARE CRACKED AT XFS 791.25 UPPER, AND XFS 776.25, 785, 791.25 LOWER. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT XS 435.789. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING LE FLAP) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 467.323. REMOVED, FABRICATED, AND REPLACED RIB ANGLE/DOUBLER IAW DWG 5770170, AND SRM SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E RIB IS CRACKED AT XFS 622.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 647.5, AND XFS 635. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E SMALL UPPER DOUBLER IS CRACKED AT XW 408. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.

Part: FITTING — CRACKED (CABIN) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1690 LONG 26L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324, AND SRM 51-1-21, AND 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E RIB IS CRACKED AT XFS 816.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 803.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1744 LONG 15L LOWER FLANGE IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.

Part: FITTING — DAMAGED (RIGHT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E PAN FITTING HAS ELONGATED HOLES AT XS 520. REMOVED AND REPLACED FITTING IAW DWG 5769857 AND SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LONGERON 31L SPLICE FITTING IS CRACKED AT STATION 1040 - 1060. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E RIB IS CRACKED AT XFS 797.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 1744 LONG 15R UPPER AND LOWER FLANGES ARE CRACKED AT FASTENER HOLES. REMOVED, FABRICATED, AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 1753 LONG 14L LOWER FLANGE IS CRACKED. REPAIRED IAW SRM 53-2-2 FIG 10.

Part: ANGLE — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-21, 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 70 FRAME TO CUSP FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3610130 AND DH SK 806-478 AND SRM 51-1-21, 51-3-0.

Part: WEB — CORRODED (COCKPIT FLOOR) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA -32 RBL 60 IN RIGHT NOSE TUNNEL HAS WEB AND DOUBLERS CORRODED BEYOND LIMITS. REPAIRED WEB AND DOUBLERS IAW SRO 08530026.

Part: RIB — CRACKED (RT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 300 LONG 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1-20D, 51-1-21, 53-2-0 FIG 1D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 1040 - 1060 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG3750257 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 450 AND 520 SEAT TRACK AT LBL 60 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A, 53-2-3 FIG 14.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 857 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750423 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 834 LONG 13L ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 759 INTERCOSTAL FITTING IS CRACKED FWD SIDE LONG 13L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 780 LONG 13L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, MAIN CABIN SEAT TRACK STA 1120 - 1140 BL 0 SCALLOPS ARE WORN BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 834 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 680 LONG 8L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-1-21, 51-1-23.

Part: SKIN — CRACKED (LT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 410.25-XOLDI 6.225. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 680 LONG 6L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-1-21, 51-1-23.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 320 LONG 11R INTERCOSTAL IS CRACKED. REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 23.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 1170 RT UPPER CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754918 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 335 - 341. REPAIRED SKIN IAW EO DC8-5720-7767-A APPX A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STATION 1210 RT UPPER CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 220 - 240 LONG 18R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4651908, 8110-3 APPROVED DH SK 806-498 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LEFT WING) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER SKIN IS CRACKED O/B OF XFS 710. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, STA 8 LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3642838 AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 71,296 hrs · 27,109 cycles

INSPECTION TYPE:C123, NR 1 PYLON INTERIOR RIGHT SIDE AFT OF TOMBSTONE FITTING HAS A ANGLE CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5756791 AND SRM 51-3-0.

Part: FRAME — CRACKED (A/C BAY) · airframe 71,296 hrs · 27,109 cycles

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

Part: FRAME — CRACKED (A/C BAY) · airframe 71,296 hrs · 27,109 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, ON PREFLIGHT EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK GOOD.

Part: PACK — FAILED (AIR DISTRIBUTION)

NR 1 BUS PWR FAIL LIGHT ILLUMINATED ON BLOCK IN. COCKPIT FILLED W/PACK SMOKE EVEN THOUGH PACK WAS OFF. COULD STILL HEAR FAN OPERATING AND COOLING DOORS OPEN. TROUBLESHOT SYSTEM PER MM 24-20-00. RECONNECTED NR 3 GENERATOR, RAN ENGINE, SYSTEM OPS CHECKS GOOD. SEE M180145.

Part: REGULATOR — INOP (RT COCKPIT)

CO-PILOTS OXYGEN DOES NOT SHUTOFF WHEN IN THE OFF POSITION. REMOVED AND REPLACED CO-PILOTS O2 REGULATOR ASSY, LEAK CHECK AND OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, DURING CREW PREFLIGHT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. LIGHTS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE ON BATTERY POWER. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK. OPS CHECK GOOD P/N ON 60-1223-5, S/N 356, P/N OFF 5708458-503, S/N 488.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, EMERG EXIT DISARMED LIGHT INOP. RELAMPED, OPS CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY BATTERY PACK.

Part: CLIP — CRACKED (CABIN)

INSPECTION TYPE C-CK, SEAT TRACK FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP FITTING IAW DC8 SRM 51-3-0. INSTALLED NEW FITTING SRM 51-3-0.

Part: CLIP — CRACKED (BS 759)

INSPECTION TYPE C-CK, MAIN CABIN STA 759 SEAT TRACK E ATTACH CLIP CRACKED. REMOVED 7 REPLACED ATTACH CLIP FITTING IAW DC8 SRM 51-1-2, 51-1-20D.

Part: CLIP — CRACKED (BS 781)

INSPECTION TYPE C-CK, SEAT TRACK E STA 781 XCW-29 FRAME ATTACH CLIP CRACKED. REMOVED AND REPLACED SEAT TRACK E IAW 51-1-20, DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1300)

INSPECTION TYPE C-CK, SEAT TRACK STA 1300 C TRACK HAS CORROSION. REMOVED DAMAGED AREA OF SEAT TRACK, SPLICED NEW TRACK IAW DC8 SRM 53-2-3.

Part: FRAME — CORRODED (BS 870)

INSPECTION TYPE C-CK, FRAME AT FS 870 LOWER LT SKIN PANEL HAS CORROSION AT RB ATTACHMENT. REMOVED DAMAGED SECTION OF FRAME, FORMED FRAME AND SPLICE IAW REO 0530 1 AND DC8 SRM 51-1-4. HEAT TREATED FRAME AND SPLICE, REMOVED INTERCOSTAL TO ALLOW ACCESS. FAB FRAME AND SPLICE IAW REO 05301. REINSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. FAB -59 ANGLE IAW REO 05301. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 865)

INSPECTION TYPE C-CK, FRAME SUPPORT ANGLE STA 865 HAS CORROSION IN LOWER LEG, DOUBLER HAS CORROSION OUTER AND INNER SKIN PANEL. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0 FOR MED INTERCOSTAL IAW DC8 SRM 51-1-4 AND DAC DWG 5616306. FAB DOUBLER IAW DC8 SRM 53-4-1, 51-1-24, FAB CLIP IAW DAC DWG 5616306, HEAT TREATED INTERCOSTAL FROM 2004-0 TO 2024T3, FAB INTERCOSTAL IAW DAC DWG 5616306. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW 51-1-20D AND 51-1-21A.

Part: FRAME — CORRODED (BS 857)

INSPECTION TYPE-C CK, LWR FRAME AT FS 857 LT HAS CORROSION AND CRACK ON RADIUS ON INTERCOSTAL (ABF SENSE ANTENNA SUPPORT ATTACHMENT ANGLE). REMOVED AND REPLACED INTERCOSTAL AND REPAIRED RIB WITH STACKED ANGLE REPAIR IAW REO-05372 DC8 SRM 53-2-0 FIG 1B. ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED EO A/C AFFECTED PARTS IAW DC8 SRM 51-3 -0, 51-1-21, 51-1-21D.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE-C CK, MAIN CABIN STA 759XC-46 AT TOP OF L/W TANK FLOORBEAM ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED FITTING.

Part: ANGLE — CORRODED (LAVATORY)

INSPECTION TYPE C-CK, LAV SEAT CONTAINER BOTTOM ATTACH ANGLES HAS CORROSION AND BARE METAL ON BOTTOM SIDE. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB ANGLES IAW DOUGLAS DWG DC-8- 380-001. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE-C CK, AFT CARGO UPPER FITTING AT FS 960 ABOVE LONGERON 24L HAS CRACK IN ATTACHMENT HOLE. REMOVED EXISTING FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE C-CK, UPPER FITTING AT FS 940 ABOVE LONGERON 24 HAS CRACK IN ATTACHMENT HOLES. REMOVED EXISTING FITTING AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON N/R 840692.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE C-CK, UPPER FITTING AT FS 920 ABOVE LONG 24L HAS CRACK. REMOVED EXISTING FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692.

Part: SPLICE — CORRODED (BS 1000)

INSPECTION TYPE C-CK, MAIN CABIN STA 1000 FLOORBOARD B SPLICE HAS CORROSION. REMOVED CORROSION FROM SPLICES IAW DC8 SRM 51-1-8. FOUND SPLICES TO BE OUT OF LIMITS MAT ID IAW DC8 SRM 53-7-3 7075-T6 .090 PO 263213. FABRICATED PARTS IAW DC8 SRM 53-7-3. ALODINED AND PRIMED IAW DC8 SRM 51-1- 8. REINSTALLED AT STA 1000 FLOORBOARD B.

Part: ANGLE — CORRODED (BS 857)

INSPECTION TYPE C-CK, LT MLG WHEEL WELL, STA 857 ANGLE ABOVE REAR SPAR HAS CORROSION ON FWD SIP AT JUST O/B OF I/B PRESSURE PANEL 48 IN LT OF C/L. REMOVED CORROSION WAS OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-8/ 51-1-20D/ 53-2-0.

Part: BRACKET — CRACKED (BS 857)

INSPECTION TYPE C-CK, LT MLG WHEEL WELL STA 857 ABOVE REAR SPAR, CORNER BRACKET HAS A VISIBLE CRACK THROUGH RADIUS AND FASTENER HOLES O/B SIDE OF I/B PRESSURE PANEL. REMOVED AND REPLACED BRACKET IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: CLIP — CRACKED (BS 759)

INSPECTION TYPE C-CK, MAIN CABIN STA 759 XCW-26 UNDER AFT SIDE SEAT TRACK E FITTING FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 375522-1) PO NR 267866 IAW DC8 SRM 51-3-2. INSTALLED NEW FITTING IAW SRM 51-1-2 & 51-1-20D.

Part: SEAT TRACK — CORROSION (BS 879-1080)

INSPECTION TYPE C-CK, MAIN CABIN STA 879 TO 1080 SEAT TRACK A HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED SECTION OF SEAT TRACK STA 590 TO 1030, DRILLED NEW SECTION IAW DC8 SRM 51-1-4. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SECTION OF TRACK IAW DC8 SRM 53-2-3 AND 51-3-0. REINSTALLED FLOOR PANELS IAW DC8 SRM 51-3-0.

Part: FLOORBEAM — CORRODED (BS 781)

INSPECTION TYPE C-CK, MAIN CABIN STA 781 SCW-29 AND -36 FLOORBEAM HAS CORROSION AROUND PLATE. REMOVED DAMAGED AREA IAW REO 05223, FABBED FILLER AND L-ANGLE IAW REO 0 5223. LOCATED AND DRILLED UP L-ANGLE AND FILLER IAW REO 05223. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER AND L-ANGLE IAW DC8 SRM 51-1-2 0D AND REO 05223.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE C-CK, MAIN CABIN STA 781 XCWX29 UNDER SEAT TRACK C FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 3773906-1), PO NR 267861 IAW DC8 SRM 51-3- 2. INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 & 51-1-20D.

Part: FLOORBEAM — CORROSION (BS 902)

INSPECTION TYPE C-CK, MAIN CABIN STA 902 FLOORBEAM AT XCW-39 CRACKED AND HAS CORROSION. BLENDED OUT CORROSION TO UPPER FWD FLANGE LWR SURFACE IAW DC8 SRM 53 -2-0 MAT ID 7075-T6 .125 REPAIR STRAP, FILLER 7075-T6 .090 PO 248989 , 263213. FAB REPAIR STRAP IAW REO 05238. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED REPAIR STRAP IAW REO 05238 AND SRM 51-1-11.

Part: FLOORBEAM — CORROSION (BS 822)

INSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-30 FLOORBEAM HAS CORROSION. REMOVED CORROSION AND DOCUMENTED REMAINING MAT THICK ON REO 05281, MAT ID .190 7075-T6 PO 234881 FOR FILLER AND 60-4139 L-ANGLE EXTRUSION 7075-T6 511 FOR REPAIR ANGLE. TRIMMED DAMAGE, FABBED FILLER FOR UPPER FLANGE AND FAB, DRILLED REPAIR ANGLE IAW REO 05231. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW REO 05231.

Part: FRAME — CORRODED (BS 781)

INSPECTION TYPE C-CK, MAIN CABIN STA 781 XCW0 FRAME HAS CORROSION AT SEAT TRACK ATTACH POINT. REMOVED BOLT STA 781 IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51-1-8. MAT REMOVED OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB FLOORBEAM REPAIR ANGLE, SUPPORT REPAIR ANGLE FILLER AND REPAIR STRAP IAW REO 05229 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED BOLTS IN SEAT TRACK IAW DC8 SRM 51-3-0.

Part: CLIP — CRACKED (BS 822)

INSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-29 UNDER SEAT TRACK E FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 373906-1) PO NR 267866 IAW DC8 SRM 51-3-2. INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 AND 51-1-20D.

Part: FLOORBEAM — CRACKED (BS 920)

INSPECTION TYPE C-CK, MAIN CABIN STA 920 FLOORBEAM AT SCW-40 CRACKED AND HAS CORROSION. CUT OUT DAMAGED AREA IAW REO 05244, FAB AND DRILLED REPAIR ANGLE, STRAP AND FILLER IAW REO 05244. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE STRAP AND FILLER IAW REO 05244 REV A AND DC8 SRM 51-1-20 AND 51-3-0.

Part: SEAT TRACK — CORRODED (CABIN)

INSPECTION TYPE-C CK, SEAT TRACK NR C AT POSITION NR 3 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW DC 8 SRM 51-3-0.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING IS CRACKED. REMOVED CRACKED FITTING HAD NEW ONE FABRICATED IAW DAC DWG 3724841 AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23.

Part: SPLICE — CORRODED (BS 1000)

INSPECTION TYPE C-CK, MAIN CABIN STA 1000 FLOORBOARD C SPLICES HAVE CORROSION. REMOVED CORROSION FROM SPLICES IAW DC8 SRM 51-1-8. FOUND SPLICES TO BE OUT OF LIMTIS IAW DC8 SRM 53-2-0 MAT ID IAW DC8 SRM 53-7-3 7075T6 .090 PO 263213. FAB PART IAW DC8 SRM 53-7-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-18. REINSTALLED SPLICE AT STA 1000 FLOORBOARD C.

Part: SPLICE — CORRODED (BS 580)

INSPECTION TYPE C-CK, MAIN CABIN STA 580 FLOORBOARD B SPLICES HAVE CORROSION. REMOVED SPLICES FROM FLOORBOARDS AND REMOVED CORROSION IAW DC8 SRM 51-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-0. FAB NEW SPLICES IAW DC8 SRM 53-7-0 AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-21 AND REINSTALLED SPLICES IAW DC8 SRM 51-3-0.

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE C-CK, STA 340 L31L Z FITTING HAS CORROSION EMITTING FROM FASTENER. REMOVED CORROSION FOUND TO BE OUT OF LIMITS DC8 SRM 51-1-8 AND 53-2-0. REMOVED FITTING, FABBED DOUBLERS, REINSTALLED FITTING IAW DC8 SRM 5 3-2-0. ALODINED, PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. FILLETED SEALED IAW DC8 SRM 51-1-16.

Part: FLOORBEAM — CORRODED (BS 920)

INSPECTION TYPE C-CK, FLOORBEAM UPPER FLANGE LOWER SURFACE HAS CORROSION STA 920 X=+59 D OT P788. REPAIRED FLOORBEAM IAW REO 05246.

Part: DOOR — CRACKED (CARGO COMPT)

INSPECTION TYPE-C CK, AFT LOWER CARGO DOOR HAS CRACK ON FORWARD UPPER AREA. STOP DRILLED CRACK, FAB DOUBLER, ALODINE, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-0, 52-4-1, 51-1-8, AND 51-1-11.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK JUST I/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D. FABBED FITTING IAW DAC CWG 3724841.

Part: FITTING — CRACKED (BS 320)

INSPECTION TYPE C-CK, STA 320 F/L/C AFT DOOR STOP FITTING CRACKED L29L AND RUBBER BUMPER MISSING. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STINGER 51 THE FWD SPLICE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED NEW FITTING IAW DAC DWG 3704841. INSTALLED FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23.

Part: SEAT TRACK — CORRODED (BS 130-220)

INSPECTION TYPE C-CK, MAIN CABIN STA 130 TO 220 SEAT TRACK B HAS CORROSION. REMOVED CORRODED SECTION OF TRACK B STA 50 TO 220. TRIMMED, LOCATED, DRILLED NEW SECTION IAW DC8 SRM 53-2-3 & 51-1-24. ALODINED AND PRIMED TRACK AND AREA IAW DC8 SRM 51-1-8. INSTALLED TRACK IAW DC8 RM 51-3-0.

Part: SEAT TRACK — CORROSION (BS 280-520)

INSPECTION TYPE C-CK, SEAT TRACK E HAS CORROSION STA 280 TO STA 520. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3 MAT ID IAW DC8 SRM 53-2-3 AND SPLICES IAW DC8 SRM 53-7-3. LOCATED, DRILLED NEW SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3 & 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK AND SPLICES IAW DC8 SRM 53 -2-3 AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 70-280)

INSPECTION TYPE C-CK, SEAT TRACK E HAS CORROSION STA 70 TO 280. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-3 FIG 12 AT FS 130 TO 270. REMOVED CORROSION AT FS 70 TO 80 IAW DC8 SRM 51-1-8 AND 53-2-3 FIG 12. ALODINED AND PRIMED IAW DC8 SRM 51. REMOVED TRACK FROM 130 TO 270 MAT ID 527726607075-T6 IAW DC8 SRM 53-2-3 AND 51-2-0. DRILLED AND INSTALLED IAW DC8 SRM 53-2-3, 51-3-0, 51-1-8, 51-1-14.

Part: STANCION — CORRODED (BS 440)

INSPECTION TYPE C-CK, FLC STA 440 LT SIDE STANCION CORRODED AROUND NUT PLATES. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC8 SRM 53-2-0.

Part: SEAT TRACK — CORRODED (BS 70-280)

INSPECTION TYPE C-CK, SEAT TRACK HAS CORROSION STA 70 TO STA 280. CORROSION OUT OF LIMITS ON TRACK F STA 85 IAW DC8 SRM 53-2-3. REMOVED DOUBLE SEAT TRACK MAT ID 54889485 7075-T6 IAW DC8 SRM 53-2-3 PO NR 10 8589. FAB SEAT TRACK IAW DC8 SRM 53-2-3. DRILLED SEAT TRACK IAW DC8 SRM 51-3-2. ALODINED AND PRIMED SEAT TRACK IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1400-1580)

INSPECTION TYPE C-CK, SEAT TRACK G HAS CORROSION AT STA 1400 TO 1580. REMOVED DAMAGED SEAT TRACK MATERIAL ID FOR NEW SEAT TRACK 2772660 EXTRUSION 7075T6 PO 158781. FAB AND DRILLED UP NEW SEAT TRACK AND SPLICE FITTING DC8 53B003-501 TAG 447216 IAW DC8 SRM 53-2-3. ALODINED IAW DC8 SRM 51-1-8. PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0.

Part: SPLICE — CORRODED (BS 759-1100)

INSPECTION TYPE-C CK, SEAT TRACK E CORRODED FS 759 TO 1100. REMOVED CORROSION IAW DC8 SRM 511-8, 53-2-3. FOUND AT FS 1040, OUT OF LIMITS CORROSION. REMOVED SEAT TRACK FROM 1030 TO 1050, FABBED, DRILLED, INSTALLED NEW SECTION IAW DC8 SRM 53-2-3 AND 51-1-8.

Part: SEAT TRACK — CORRODED (BS 50-260)

INSPECTION TYPE C-CK, MAIN CABIN STA 50 TO 260 SEAT TRACK A HAS CORROSION. REMOVED CORROSION IAW 1-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-3. DRILLED NEW SECTION OF SEAT TRACK IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SECTION OF TRACK IAW DC8 SRM 51-3-0 AND 53-2-3.

Part: SEAT TRACK — CORRODED (BS 800-1100)

INSPECTION TYPE-C CK, SEAT TRACK G HAS CORROSION AT STA 800 TO STA 1100 AS MARKED. REMOVED CORROSION ON SEAT TRACK IAW DC8 SRM 51-1-8 AND INSTALLED 3 SEAT TRACK PLUG ON STA 941, 917, 816 IAW DC8 SRM 53-2-3 FIG 6D. TREATED ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: SPLICE — CRACKED (BS 610)

INSPECTION TYPE C-CK, FLC LONG 31R STA 610 SPLICE CRACKED. REMOVED AND REPLACED (P/N 3750257-503N) LONGERON SPLICE FITTING ON LONGERON 31R AT STA 610 IAW DC8 SRM 51-1-20D.

Part: PLUG — CORRODED (BS 860-880)

INSPECTION TYPE-C CK, SEAT TRACK D BETWEEN STA 860 AND 880 HAS CORRODED SEAT TRACK PLUG ON BOTTOM SIDE. REMOVED AND REPLACED PLUG AND SPLICE IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1460-1580)

INSPECTION TYPE C-CK, SEAT TRACK F HAS CORROSION STA 1460 TO 1580. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED SECTION OF TRACK IAW DC8 SRM 51-3-0, MAT ID S4889185. DOUBLE SEAT TRACK 7075 T6 PO NR 108584 IAW DC8 SRM 53-2-3. FAB SEAT TRACK REPAIR IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 51-1-8. INSTALLED IAW DC8 SRM 53-2-3.

Part: FLOORBEAM — CORROSION (BS 798)

INSPECTION TYPE C-CK, SEAT TRACK D STA 798 FLOORBEAM HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW REO 05232.

Part: FLOORBEAM — CORRODED (BS 92)

INSPECTION TYPE C-CK, SEAT TRACK D STA 920 AT FWD MOUNT BOLT FLOORBEAM IS CRACKED. FABBED REPAIR STRAP IAW REO 05207, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. NO CRACK NOTED, PART WAS CORRODED.

Part: SEAT TRACK — CORRODED (BS 50-120)

INSPECTION TYPE C-CK, MAIN CABIN STA 50 TO 120 SEAT TRACK B CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REPLACED SEAT TRACK ON NR 840844.

Part: SUPPORT — CORRODED (BS 25)

INSPECTION TYPE C-CK, STA 25 FLOOR SUPPORT CORRODED CUSP TO CUSP. REMOVED DAMAGED FLOOR SUPPORT AT STA 25 CUSP TO CUSP, FAB NEW SUPPORT IAW DC8 53-3-2 AND DOUGLAS DWG 5888367. ALODINED AND PRIMED FLOOR SUPPORT IAW DC8 SRM 51-1-8. INSTALLED FLOOR SUPPORT IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-21A.

Part: LONGERON — CRACKED (BS 862)

INSPECTION TYPE C-CK, LT WHEEL WELL LONGERON 24 CRACKED APPROX 2 INCHES AT STA 862. REMOVED AND REPLACED LONGERON 24 IAW TIMCO WORK CARD 90453100.

Part: SPLICE — CORROSION (BS 70)

INSPECTION TYPE-C CK, LONG 33 RT END SPLICE TO FRAME CORRODED STA 70. REMOVED CORROSION IAW DC8 SRM 51-1-8. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: INTERCOSTAL — CRACKED (BS 90)

INSPECTION TYPE C-CK, STA 90 ABOVE L33R INTERCOSTAL CRACKED TOP FLANGE. REMOVED AND REPLACED INTERCOSTAL IAW DC8 SRM 51-1-21. FABRICATED INTERCOSTAL IAW DAC DWG 5750726. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FRAME — CRACKED (BS 1480)

INSPECTION TYPE C-CK, MAIN CABIN STA 1480 LONG 21R FRAME CRACKED. REMOVED GILLINER FOR ACCESS. REMOVED DAMAGED CLIP, FAB REPLACEMENT CLIP IAW DAC DWG 5773480. HEAT TREATED CLIP IAW TPS-1003, DRILLED DEBURNED CLIP, TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CLIP IAW DC8 SRM 51-1-20D & 51-1-9. REINSTALLED GILLINER IAW DC8 SRM 51-1-21D.

Part: DOOR — CRACKED (CARGO COMPT)

INSPECTION TYPE-B CK, NR 2 PIT DOOR, FWD UPPER CORNER CRACKED WHERE ROLLER SUPPORT BOLTS TO DOOR FRAME. REPAIRED PER DC8 52-02-0 PG 13.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATT PACK, OP'S CHECK OK. (S/N 335) ON, (S/N 255) OFF.

Part: FRAME — CORRODED (FS 1060)

INSPECTION TYPE-SV, AFT FUSELAGE SKIN REPLACEMENT AREA LEFT HAND FRAME AT FUSELAGE STATION 1060 CORROSION AROUND NUT PLATE AND LOWER FRAME SURFACE LONGERON 35 RIGHT. REPAIRED FRAME AT FS 1060 IAW TIMCO REO 03055, REMOVED CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0, FABRICATED REPAIR DOUBLER IAW REO 030 55, ALODINED AND PRIMED IAW DC8 SRM D51-1-8, INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-20D.

Part: FITTING — GOUGED (BS 1180)

INSPECTION TYPE-SV, SKIN REPLACEMENT AREA/GOUGES ON WEBBING AT BATHTUB FITTING FS 1180 LONGERON 35R TO 34R UPPER SURFACE. BLENDED DISCREPANT AREA ORIGINAL MATERIAL THICKNESS .127 REWORK .064 / OUT OF LIMITS IAW DC8 SRM 51-2-0. FABBED REPAIR DOUBLER IAW REO-03 056. TREATED AND PRIMED DISCREPANT AREA AND REPAIR DOUBLER IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-20D AND REO-03056.

Part: SKIN — CORRODED (BS 1200)

CORROSION FOUND IN BELLY SKIN AFT AT STA 1200. ALL DISCREPANCIES DEFERRED IAW GMM CHAP 3 AND FERRY PERMIT NR 9007 NO INTERIM ACTION REQUIRED AS PER CONCURRENCE FOR PERMIT. ENTERED AS D- 127570, ALL FERRY FLIGHT PROCEDURES HAVE BEEN C/W AND A/C IS IN SAFE OPS COND FOR FERRY FLT.

Part: FLOORBEAM — CORRODED (BS 640)

INSPECTION TYPE-C, FLOORBEAM UPPER CAP CORRODED FS 640 RBL 34. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED PER DHC SRM 51-1-20, AND DHC SK-806-215A REF ENRG FILE NR DC8-53-1739.

Part: FITTING — CRACKED (FS 280)

INSPECTION TYPE-C, C-1 CARGO COMPARTMENT FITTING CRACKED AT FS 280 BETWEEN LONG 27R AND 26R. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3754025, INSTALLED REPLACEMENT FITTING IAW DWG 3754025 AND SRM 51-1-20.

Part: SKIN — CORRODED (BS 520-540)

INSPECTION TYPE-C, SKIN CORRODED BELOW C2 DOOR, STA 520 TO 540, LONGERON 33R. CUT OUT DAMAGE AREA, INSTALLED REPAIR DOUBLER AT STA 520 TO 540, LONGERON 31R TO 35R, IAW SRM 51-1-20, 51-1-21 AND DHC SK-806-705 REF UPS E0 DC8-5330-9022-A.

Part: RIB — CRACKED (WS 257)

INSPECTION TYPE-C, LT WING L/E RIB HAS CRACK IN UPPER AFT END AT XW257. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 57-3-3 AND 51-1-21.

Part: FLOORBEAM — CRACKED (BS 1580)

INSPECTION TYPE-C, FLOORBEAM CRACKED AT FASTENER HOLE FS 1580 LBL 36. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK-806-586 REV C REF ENRG FILE NR DC8-53-1741.

Part: SKIN — CORRODED (BS 1224)

INSPECTION TYPE-C, RT FUSELAGE SKIN HAS CORROSION BETWEEN LONGERON 22R AND 23R AT FS 1224. REPAIRED IAW DHC SK-806-392 REV IR REF UPS ENRG FILE NR DC8-53-1738.

Part: FITTING — CORRODED (BS 922)

INSPECTION TYPE-C, CASTING ABOVE LONGERON 24 RT HAS EXFOLIATED CORROSION THOUGH WEB PART STA 922 ABOVE MLG UPLOCK. REMOVED FITTING, FABRICATED AND INSTALLED FITTING IAW SRM 53-2-0 FIG 8.

Part: SEAT TRACK — CORRODED (BS 1123-1133)

INSPECTION TYPE-C, SEAT TRACK HAS HEAVY CORROSION STA 1123 TO 1133 LBL 24. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK FROM STA 1030 TO 1170 IAW SRM 53-2-3, 53-7-3.

Part: SEAT TRACK — CORRODED (BS 450-590)

INSPECTION TYPE-C, MAIN CABIN BTWN STA, 495 TO 505 LBL 24 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPAIR SECTION OF SEAT TRACK STA 450 TO 590 IAW SRM 53-2-3 FIG 8.

Part: SEAT TRACK — CORRODED (BS 785-1030)

INSPECTION TYPE-C, SEAT TRACK HAS HEAVY CORROSION STA 785 TO 1030 LBL 24. REMOVED AND REPLACED DAMAGED SECTION IAW SRM 53-2-3 AND 53-7-3.

Part: SEAT TRACK — CORRODED (BS 1035-1136)

INSPECTION TYPE-C, SEAT TRACK CORRODED FROM STA 1035 TO 1136 LBL 44. REMOVED DAMAGED SEAT TRACK, FABRICATED REPAIR TRACK AND INSTALLED TRACK FROM STA 990 TO 1170, LBL 44 IAW SRM 51-1-20D AND 53-2-3.

Part: SEAT TRACK — CORRODED (BS 1484-1494)

INSPECTION TYPE-C, MAIN CABIN SEAT TRACK HAS HEAVY CORROSION STA 1484 TO 1494. REMOVED DAMAGED SEAT TRACK PER SRM 53-2-3, FABRICATED AND INSTALLED REPAIR SECTION BS 1470 TO 1590 PER SRM 53-2-3 AND 51-01-20.

Part: LONGERON — CORRODED (BS 880)

INSPECTION TYPE-C, LONG 24 LT HAS EXFOLIATION CORROSION ABOVE PREVIOUS REPAIR APPROX STA 880 TOP. REMOVED CORROSION AND REPLACED IAW DHC SK-806-479 REF ENRG FILE NR DC8-53-1743.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-C, LT AILERON TAB LOCK-OUT CYLINDER ACCESS PANEL LAND, MATING SURFACE HAS 2 CRACKS. CUT OUT DAMAGED AREA OF INNER DOUBLER, FABRICATED AND INSTALLED REPAIR IAW DHC SK-806-413 REF UPS ENRG FILE NR DC8-57-0752.

Part: SEAT TRACK — CORRODED (BS 360-420)

INSPECTION TYPE-C, HEAVY CORROSION AROUND RT AFT TRACK FASTENER HOLES STA 360 TO 420. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW DC8 SRM 51-1-20, 51-1-0, AND 51-3-0.

Part: BOOST PUMP SW — OUT OF POSITION (NR 3 ENGINE)

INSPECTION TYPE-N/A, NR 3 ENGINE FLAMED OUT AT 35,000 FT. BOOST PUMP SWITCH WAS OFF, RESTARTED AT 15,000 FT. PERFORMED NEG PRESS TEST ON NR 3 ENG FEED LINE PER MM 28-22-12. APPLIED NEG PRESS OF -5 PSI FOR 2 MINS, OBSERVED PRES HELD TO -4.6 PSI. FEED LINE CK FROM BOOST PUMP TO NASH PUMP, NO LK NOTED PER MM 28-22-12. ACCOMPLISHED FCD DC8-7200-0064A AND DC8-CFM56-2 MIN FUEL PRESS 18 PSI NO DISCREPANCY NOTED.

Part: PUMP SWTCH — OUT OF POSITION (NR 3 ENG BOOST)

INSPECTION TYPE-N/A, DURING CLIMB THROUGH FL350 NR 3 ENG N1 BEGAN TO FLUCTUATE +/- 3 PERCENT THEN GOT WORSE. SHUT OFF PMC TO STABILIZE, NO EFFECT. LOST THROTTLE CONTROL OF NR 3 ENG. PERFORMED INFLIGHT SHUTDOWN AND TURNED BACK TO SDF. SECOND OFFICER NOTED NR 3 BOOST/FEED SWITCH WAS IN OFF POSITION. RESTART AT FL190 WAS SUCCESSFUL, OPERATED NORMALLY. INSPECTED ENGINE VISUALLY FOR DEFECTS, NONE FOUND.

Part: GCU — MALFUNCTIONED (AC GEN SYST)

INSPECTION TYPE N/A, GEN UNPARALLEL LIGHT ILLUMINATED ON DECENT. AC LOAD AND FREQ WENT TO ZERO, STARTED GETTING AN ELECT BURNING SMELL, SO WE DISCONNECTED GENERATOR. REMOVED AND REPLACED VR AND GCU, RAN ENG AND OPS CHK GOOD. THIS CLEARS M-117170, (P/N 51508-000) (S/N 665ABC) ON, (P/N 51508-0000) (S/N 217ACB) OFF.

Part: ATTACH PIN — SHEARED (LT MLG)

INSPECTION TYPE-N/A, UPON GEAR EXTENSION THERE WAS A LOUD BANG AND YAW OF THE A/C TO THE RIGHT. ONLY THE LEFT GEAR EXTENDED AND AFTER ABOUT 10 SECONDS THE RIGHT MAIN AND NOSE GEAR EXTENDED. GEAR INDICATIONS WERE NORMAL, LATER FOUND LT MLG ATTACH PIN WAS SHEARED. REPLACED TORQUE TUBE, BUNGEE AND UPPER CYLINDER PER TASK CARD 2534 AND OHM 32-10-01 REPLACED ATTACH PIN.

Part: BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS INOP. REPAIRED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, SYSTEM CHECKS GOOD PER MM 33-50-01.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT DID NOT OPERATE. MAINTENANCE REPLACED THE BATTERY PACK AND LIGHT OPS GOOD. THE OFF (P/N 60-1223-3), (S/N 188) AND ON (P/N 5708458-503), (S/N FT002).

Part: WIRE — FAULTY (LANDING GEAR)

PILOT REPORTED, ON RETRACTION GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED, USED CHECK LIST AND RECYCLED GEAR. WHEN GEAR RETRACTED, THE DOOR NOT LATCHED AND THE GEAR NOT LATCHED WERE ILLUMINATED. ALSO, ALT GEAR DOOR INDICATOR INDICATED RIGHT GEAR DOOR. RECYCLED GEAR ONCE AGAIN, THE DOOR AND GEAR NOT LATCHED LIGHTS EXTINGUISHED. PERFORMED UP LATCH CHECK AND THE GEAR NOT LATCHED LT AND RT DOOR WARNING ILLUMINATED. PROCEEDED AT 230 KTS DUE TO ALT GEAR DOOR LIGHT ILLUMINATED. MAINTENANCE REPAIRED FAULTY WIRING.

Part: SKIN — CORRODED (FS 140)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 140 LONG 31R AFTER CORROSION REMOVAL, SKIN WAS FOUND TO BE BEYOND ALLOWABLE LIMITS PER SRM 53-2-0 ON NR 289954. CUT OUT DAMAGED AREA PER SRM 53-2-1, FABRICATED AND INSTALLED PARTS ACCORDING WITH SRM 53-2-1.

Part: ANGLE — CORROSION (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT STA 80 LBL 59 CHORD ANGLE HAS HEAVY CORROSION AT O/B END. CUT OUT DAMAGE, FABRICATED T-CHORD, REPAIR ANGLE AND INSTALLED PER UPS EO DC8 5310-7325A.

Part: PANEL — CORRODED (BS 960)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MAIN CABIN CENTER SECTION PRESSURE PANEL HAS EXFOLIATION CORROSION AT FS 960 RBL 69. REMOVED DAMAGED SECTION OF PAN IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR IAW UPS EO DC8 5310-7339A.

Part: FLOORBEAM — CORRODED (BS 850)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 850 LBL 50 FLOORBEAM HAD CORROSION IN FWD LWR CORNER, AFTER FASTENERS CORROSION AND DAMAGED CHORD WERE REMOVED. WEB WAS FOUND IN LIMITS AND PROTECTIVE TREATED CHORD WAS SUBMITTED TO ENG. REMOVED DAMAGED AREA, FABBED AND INSTALLED REPAIR PARTS PER UPS EO DC8 5310-7340A.

Part: FITTING — CRACKED (FS 1240)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 1240 LONG 35R AFT INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-10 AND 51-1-20D.

Part: PANEL — CORRODED (FS 880-900)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MAIN CABIN CENTER SECTION PRESSURE PANEL HAS EXFOLIATION CORROSION AT FS 880 TO 900. REMOVED DAMAGED SECTION IAW SRM 53-0-0. RADIUSED CORNER, INSTALLED REPAIR SPLICE IAW UPS EO DC8 5310-7338A.

Part: SPLICE — CRACKED (FS 200-220)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND SPLICE IS CRACKED ON STRINGER 31L BETWEEN FRAME 200 AND 220. REMOVED SPLICE AND INSTALLED NEW SPLICE IAW SRM 53-2-2 AND 51-1-10.

Part: FITTING — CRACKED (BS 960)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME FITTING B/S 960 IN RT WHEEL WELL ABOVE LONG 24R IS CORRODED AND CRACKED. REMOVED AND REPLACED FITTING AT B/S 960 IN RT WHEEL WELL PER SRM 53-2-0 FIG 8.

Part: BULKHEAD — CORRODED (BS 980)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT MLG WHEEL WELL AFT PRESSURE BULKHEAD, B/S 980 AT LONGERON 31R CORRODED BEYOND LIMITS. REPAIR BULKHEAD B/S 980 AT LONGERON 31R IAW DC8-5310-7307A.

Part: FRAME — CORRODED (BS 1040)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME B/S 1040 CORRODED AT LONGERON 34R. CUT OUT CORROSION DAMAGE, FABRICATED AND INSTALLED ANGLE AND FILLER IAW DC8-5310-7303A.

Part: SKIN — CRACKED (RT TE SLOT)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT INBOARD WING SLOT OUTBOARD END UPPER SURFACE. MAINTENANCE REMOVED THE ANGLE REPAIR, STOP DRILLED, REPAIRED AND REINSTALLED PER SRM 51-3-0, 57-2-0, AND 51-1-20.

Part: FITTING — CRACKED (BS 1220)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FITTING ACROSS THE FASTENER C-3 AFT AT DOOR OPENING LOWER AT STATION 1220. MAINTENANCE REMOVED AND REPLACED THE FITTING AND FASTENERS IAW SRM 51-1-20D.

Part: LE RIB — CRACKED (WS 520.168)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT UPPER END OF THE RIGHT WING LEADING EDGE RIB AT STATION XS520.168. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED AND INSTALLED THE ANGLE PER SRM 53-2-0.

Part: FITTING — CORRODED (BS 420)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN DECK FRAME 420 RIGHT FLOOR FITTING AT CUSP AROUND ATTACH BOLTS. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE FITTING PER SRM 51-1-20.

Part: DOUBLER — CORRODED (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 80 - 100 AT LONGERON 31R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE FINGER DOUBLER IAW SRM 51-1-20 AND 51-1-20D.

Part: CASTING — CORRODED (BS 560)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BOTH SIDES OF CASTING AT THE RIGHT CUSP AT STATION 560. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 5 1-1-20D.

Part: CASTING — CORRODED (BS 1460)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEAD ON THE LEFT CUSP AT STATION 1460 AFT TOP. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 51-1-20.

Part: LONGERON — CRACKED (BS 855-920)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN LONGERON 24R AT STATION 855 - 867 AND STA 919 - 920. MAINTENANCE REMOVED AND REPLACED THE LONGERON IAW SRM 51-1-20D AND 51-3-0.

Part: WEB — CORRODED (STA 367-380)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN DECK 21 RIGHT BETWEEN FRAME 360 - 380 AT STATION 367 - 380. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED PER SRM 53-01-0 AND 53-2-5.

Part: FITTING — CORRODED (BS 600)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT THE RIGHT CUSP AROUND BOLT HEADS AT STATION 600. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT WING FORWARD OF THE FORWARD SPAR WING TO BODY ANGLE AT STATION 640 - 680. MAINTENANCE REMOVED THE ANGLE, FABRICATED AND INSTALLED PER SRM 51-1-20D AND 51-3-0.

Part: DOUBLER — CORRODED (BS 960-980)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 960 - 980 AND RBL 62. MAINTENANCE FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-4-1, 51-1-8 AND 51-1-21.

Part: FITTING — CORRODED (BS 660)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT RIGHT CUSP AROUND BOLT HEADS AT STATION 660. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT RIGHT CUSP AROUND THE BOLT HEAD AT STATION 640. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: CASTING — CORRODED (BS 620)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEAD AT RIGHT CUSP, STATION 620. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 35)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE ANGLE STIFFENER ON THE LAVATORY FLOOR AT STATION 35 AND RBL 45. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE PART PER SRM 53-3-1, 53-3-3 AND 51-1-21.

Part: FITTING — CRACKED (BS 1140)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FITTING AT STATION 1140 AND LONGERON 33R. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20D AND 51-1-8.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TOP FORWARD CORNER OF THE RIGHT FORWARD SERVICE DOOR ON THE FUSELAGE SKIN. MAINTENANCE CUT OUT THE DAMAGED AREA PER UPS EO DC8-5330-7308-A.

Part: SKIN — CORRODED (WS 635-667)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD LEADING EDGE LOWER SKIN BETWEEN STATION XFS 635.0 - XFS 667.0. MAINTENANCE TRIMMED OUT THE CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 57-2-1.

Part: FUSELAGE — CORRODED (BS 1120)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 1120 BETWEEN LONGERON 33R AND 34R. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7306-A.

Part: SPLICE — CORRODED (BS 600)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER SPLICE 31L BETWEEN FRAME 600 - 620. MAINTENANCE REMOVED THE SPLICE, FABRICATED AND INSTALLED THE SPLICE IAW SRM 51-1-20 AND 53-4-1.

Part: FITTING — CORRODED (BS 420)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT LEFT CUSP AT STATION 420. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE FITTING IAW SRM 51-1-20, 53-1-0 AND 51-3-0.

Part: SKIN — CORRODED (WS 703.5)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE SCREW HEAD AT THE RIGHT HAND WING, OUTBOARD LEADING EDGE LOWER SKIN AT STATION XFS 703.5. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED THE FILLER AND DOUBLER AND INSTALLED PER SRM 57-2-1.

Part: WEB — CRACKED (BS 008)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 4 INCH CRACK IN THE WEB AT THE COURIER SUBFLOOR AT STATION 008 RBL 46. MAINTENANCE STOP DRILLED THE CRACK AND REPAIRED THE WEB PER SRM 53-3-3 AND 53-2-0.

Part: DOUBLER — CORRODED (BS 55)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD AIRCRAFT COMPARTMENT FINGER DOUBLER AT STATION 55 AND LONGERON 31R. MAINTENANCE REMOVED THE FINGER DOUBLER, FABRICATED AND INSTALLED THE FINGER DOUBLER IAW SRM 53-3-3 FIGURE 1 AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 1700)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE END FITTING AT STATION 1700 AND LONGERON 35R. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20 AND 53-1-0.

Part: LONGERON — CORRODED (BS 1645)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE LONGERON AT STATION 1645 TO 1700 AND LONGERON 35R. MAINTENANCE CUT OUT DAMAGED AREA, INSTALLED REPLACEMENT LONGERON PER SRM 53-2-2 AND FABRICATED REPAIR SPLICE AND INSTALLED PER SRM 53-1-22, 51-1-20D.

Part: FRAME — CORRODED (BS 1020)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT SIDE OF THE FRAME AT STATION 1020 AND STRINGER 33L. MAINTENANCE REMOVED THE CORROSION, FABRICATED AND INSTALLED THE REPAIR ANGLE PER SRM 53-2-0, FIGURE 2B AND 51-1-21.

Part: FITTING — CORRODED (BS 1691)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE END FITTING AT STATION 1691 AND LONGERON 36. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20.

Part: SPAR — CRACKED (WS 1)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE 3 O'CLOCK POSITION TOP VIEW LOOKING DOWN RIGHT HAND FRONT SPAR LOWER CAP FORWARD T-ANGLE, IN FURTHEST INBOARD HOLD AT STATION XFS 1.000, .020 DEEP. MAINTENANCE ENLARGED THE HOLE IAW SRM 57-2-6 FIGURE 4. HFEC INSPECTION AFTER REWORK CRACK NOTED. INSTALLED REPAIR IAW SRM 57-2-6 FIGURE 4.

Part: FITTING — CRACKED (BS 1690)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE ATTACH POINT TO FRAME AT STATION 1690 AND LONGERON 30R. MAINTENANCE REMOVED THE FITTING PER SRM 51-1-21 AND INSTALLED THE REPLACEMENT FITTING IAW SRM 51-1-21 AND 51-3-0.

Part: RIB — CORRODED (WS 297.5)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT UPPER END OF THE LEFT HAND WING LEADING EDGE RIB AT STATION 297.5. MAINTENANCE REPAIRED THE DAMAGED AREA IAW SRM 57-2-0.

Part: SPLICE — CRACKED (BS 1050)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SPLICE AT STATION 1050 AND LONGERON 31R. MAINTENANCE REMOVED AND REPLACED THE SPLICE FITTING PER SRM 51-1-20D, 51-3-0 AND 51-1-11.

Part: LE RIB — CRACKED (WS 822.5)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 822.5, AT THE AFT LOWER END. MAINTENANCE REMOVED THE FASTENERS AND STOP DRILLED THE CRACK PER MM 57-00-00 FIGURE 801. HFEC STOP DRILL CRACK TERMINATION. REPAIRED PER MM 57-00-00 FIGURE 801.

Part: INTERCOSTAL — CORRODED (BS 980)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A LARGE CRACK AFT END OF THE BULKHEAD TIE INTERCOSTAL AND CORROSION ON THE FORWARD END AT STATION 980 TO 1000 STRINGER 32L. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 960)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEVERAL FASTENERS ON THE FRAME AT STATION 960 AND STRINGER 22L. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 53-4-1.

Part: FRAME — CORRODED (BS 1020)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT SIDE OF THE FRAME AT STATION 1020 AND STRINGER 34R. MAINTENANCE REMOVED THE CORROSION, FABRICATED AND INSTALLED THE REPAIR ANGLE PER SRM 53-2-0 FIGURE 2B, 51-1-21.

Part: FITTING — CORRODED (BS 360)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEADS AT THE RIGHT HAND CUSP AT STATION 360. MAINTENANCE REMOVED THE OLD FITTING, DRILLED AND FASTENED THE NEW FITTING IAW SRM 51-1-20 AND 51-3-0.

Part: AUX SPAR CAP — CORRODED (FUSELAGE)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSON ON THE LEFT HAND LOWER AUX SPAR CAP AT OUTBOARD HOLES. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND LOWER AUX SPAR CAP IAW SRM 51-01-20.

Part: SEAT TRACK — CORRODED (NR 2 PIT DOOR)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER FORWARD CORNER OF THE NR 2 PIT DOOR ON THE RIGHT HAND SEAT TRACK. MAINTENANCE REMOVED THE CORRODED SECTION OF THE TRACK, FABRICATED REPLACEMENT AND INSTALLED SECTION OF TRACK PER SRM 51-3-0, 53-1-0, AND 51-3-0.

Part: DOOR FRAME — CORRODED (NR 2 PIT DOOR)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME LOWER FORWARD CORNER OF THE NR 2 PIT DOOR PLATE. MAINTENANCE REMOVED THE CORRODED WEB, FABRICATED AND INSTALLED A NEW WEB PER SRM 51-1-8.

Part: RIB — CRACKED (WS 729)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LEADING EDGE RIB AT THE AFT END OF THE LEFT HAND LEADING EDGE WING AT STA 729. MAINTENANCE STOP DRILLED THE CRACK AND REPAIRED THE RIB PER SRM 57-2-0 FIGURE 1, TREATED AND PRIMED PER SRM 51-8-1.

Part: RIB — CRACKED (WS 304)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE AFT END OF THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 304. MAINTENANCE STOP DRILLED THE CRACK, REPAIRED AND PRIMED PER SRM 57-2-0 FIGURE 1 AND 51-8-1.

Part: RIB — CRACKED (WS 385.25)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE LOWER SPANWISE INTERCOSTAL AT THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 385.25. MAINTENANCE REPAIRED THE RIB IAW SRM 51-2-0.

Part: FITTING — CRACKED (BS 1520)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FLOORBEAM TO SEAT TRACK SUPPORT FITTING AT STATION 1520, BL 0 AND WL 202. MAINTENANCE REMOVED AND REPLACED THE FITTING WITH HI-LOC PER SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1691)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND THE AFT FUSELAGE END FITTING WAS CRACKED AND CORRODED AT STATION 1691 AND LONGERON 28L. MAINTENANCE REMOVED THE FITTING PER SRM 51-1-20 AND INSTALLED THE NEW FITTING PER SRM 51-1-20 AND 51-3-0.

Part: DOUBLER — CORRODED (BS 180)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 180 AND LONGERON 31R. MAINTENANCE REMOVED THE DOUBLER, SPLICE ANGLES, FABRICATED THE REPLACEMENT DOUBLER AND INSTALLED PER SRM 53-4-1, 51-1-8, 51-1-20 AND 51-1-14.

Part: SEAT TRACK — CORRODED (CABIN)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN CABIN SEAT TRACK AT THE LAV AREA AT STATION RBL 59. MAINTENANCE REMOVED THE CORRODED SECTION OF THE SEAT TRACK, FABRICATED THE SECTION OF TRACK AND INSTALLED PER SRM 53-2-3, 53-7-3, FIGURE 3 AND SRM 53-2-3.

Part: RIB — CRACKED (WS 596.0)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT END OF THE UPPER LEADING EDGE RIB ON THE LEFT HAND WING LEADING EDGE AT STATION XFS 596.0. MAINTENANCE STOP DRILLED THE CRACK AND FABRICATED THE REPAIR PARTS IAW SRM 53-2-0 AND INSTALLED PARTS PER SRM 53-2-0 AND 51-1-21.

Part: FITTING — CORRODED (BS 960)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE FASTENERS AT THE END OF THE FRAME AT STATION 960 AND STRINGER 22R. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20.

Part: SKIN — CORRODED (BS 1690)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE SKIN AT STATION 1690 TO 1700 BETWEEN LONGERON 35L AND 36. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-2-1.

Part: FRAME — CORRODED (BS 1040)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME CAP AT STATION 1040 AND L36 AND L35L TO L35R. MAINTENANCE REMOVED THE CORROSION PER SRM 51-1-8, FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-8 AND 53-2-0.

Part: SPAR — CRACKED (WS 33.5)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE 7 O'CLOCK POSITION TOP VIEWING DOWN OF THE LEFT HAND FRONT SPAR, LOWER SPAR FORWARD T-ANGLE. FASTENERS HOLE AT STATION XFS 33.50L GREATER THAN .020 INCHES IN DEPTH. MAINTENANCE ENLARGED THE HOLE IAW SRM 57-2-6 FIGURE 4. HFEC INSPECTION AFTER REWORK REPAIR, NO CRACK NOTED. INSTALLED REPAIR IAW SRM 57-2-6.

Part: RIB — CRACKED (WS 785.0)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT LWR END. REPAIRED IAW MM 57-00-00.

Part: SHEAR TIE — CORRODED (BS 1340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND STA 1340 AT STR 31L, SHEAR TIE HAS HEAVY CORROSION. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-4-1 AND 51-1-21.

Part: RIB — CRACKED (WS 653.75)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 653.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.

Part: FITTING — CORRODED (BS 1340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT FLOORBEAM SUPPORT FITTING CORRODED ON INNER SERVICE AT FLOORBEAM ST 1340. REMOVED CORROSION PER SRM 51-1-8, FABRICATED, DRILLED AND INSTALLED DOUBLER PER SRM 53-2-0.

Part: RIB — CRACKED (WS 728.75)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 728.75 WAS CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-20-0.

Part: RIB — CRACKED (WS 766.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0.

Part: RIB — CRACKED (WS 766.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-00-00.

Part: RIB — CRACKED (WS 797.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 797.5 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.

Part: RIB — CRACKED (WS 785.0)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00 PG 801.

Part: RIB — CRACKED (WS 747.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD WING, STA XFS 747.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00 PG 801.

Part: RIB — CRACKED (WS 816.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 816.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.

Part: RIB — CRACKED (WS 791.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.

Part: RIB — CRACKED (WS 672.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E AT STA XFS 672.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00.

Part: WEB — CRACKED (FS 190-200)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND WEB CRACK AT ACCESS HOLE CLOSURE WEB BETWEEN FRAME STA 190 AND 200 AT LONG 16R. ROUTED CRACK THAT TERMINATED AT .25 STOP DRILL IAW SRM 53-2-0, INSTALLED DOUBLER IAW SRM 53-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS 778.75)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 778.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.

Part: RIB — CRACKED (WS 641.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 641.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.

Part: RIB — CRACKED (WS 810)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 810.0 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.

Part: ANGLE — CRACKED (BS 680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ACC COMPT STA 680 LBL 48 SEAT TRACK SUPPORT ANGLE WAS CRACKED. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 53-4-3 AND 51-1-20D.

Part: SEAT TRACKS — CORRODED (BS 1330/1370)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND STA 1370, BLO SEAT TRACK SPLICES AND BOTH SEAT TRACKS ARE CORRODED ON UNDERSIDE. ALSO, AT 6 STA 1330. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE. CLEANED AND TREATED LOWER ENDS OF SEAT TRACKS PER SRM 51-1-8.

Part: RIB — CRACKED (WS 660)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB STA XFS 660.0 WAS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.

Part: RIB — CRACKED (WS 566.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 566.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM 57-20-0.

Part: RIB — CRACKED (WS 610.0)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 610.0 WAS CRACKED AT THE AFT LWR END. REPAIRED PER SRM 57-2-0.

Part: RIB — CRACKED (WS 791.25)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0.

Part: ANGLE — CRACKED (BS 680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ACC COMPT STA 680 RBL 24 SEAT TRACK SUPPORT ANGLE WAS CRACKED. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 53-4-3 AND 51-1-20D.

Part: RIB — CRACKED (WS 760.0)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 760.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00.

Part: HYD PRESS IND — MALFUNCTIONED (COCKPIT)

WHILE EN ROUTE TO TPE, PILOT NOTED PRESSURE DROP TO 1000 PSI (HYD. SYS. PRESS.) ON UPLATCH CHECK. CYCLED GEAR; PRESSURE RETURNED TO NORMAL. SYSTEM LEAK CHECKED, NO EVIDENCE OF HYD. LEAK. ACCUMULATOR PRESSURE CHECKED SATIS. HYD QTY. CHECKED, SYSTEM FULL. HYD. SYS. PRESSURE CHECKED, SATIS.

Part: BEAM — CRACKED (AFT BULKHEAD)

DURING B-CHECK, MAINTENANCE FOUND NR 3 AND 4 'J' BEAM CRACKED AT AFT BULKHEAD. REPAIRED PER UPS EO DC8-5310-6715A.