N706UP

Part: ENGINE — FLAMED OUT (NR 4)

NR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL.

Part: A/C PACK — ODOR (BOTH)

ON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INSPECTED A/C FOR SPILLED FLUIDS IN CARGO AREA AND LOWER PITS. NONE FOUND. A/C OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD.

Part: LINK — BROKEN (NR 4 BRAKE)

NR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-290, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: LONGERON — CRACKED (AFT CABIN) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION, INSTALLED STRAPS AND SPLICE FITTING IAW SRM 53-2-2 FIG 10.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPAIR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING DOUBLER, CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2A.

Part: DOUBLER — CORRODED (ACCESSORY BAY) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17D, 51-1-20D, 51-1-21.

Part: SUPPORT FITTING — CRACKED (FLOORBEAM) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D, 53-1-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SECTION, FABRICATED, INSTALLED 2 SPLICES, ANGLES AND REPLACEMENT FRAME SECTION IAW SRM 53-2-0 FIG 2.

Part: SKIN — CRACKED (RUDDER) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,092 hrs · 46,218 cycles

INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKIN FILLER IAW SAA SK 706-550 AND DC8-5330-20148-A.

Part: RELIEF VALVE — STUCK (BOGIE UNLOCK)

DURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND BOGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT MAIN FEAR STUCK OPEN. REPLACED RELIEF VALVE POF 32-53-02. NO LEAKS DETECTED. HYD WAS SERVICED.

Part: SKIN — CORRODED (FUSELAGE)

FOUND EXTENSIVE CORROSION AT STATION 1746 SEVERAL RIVETS PULLED THROUGH SKIN. SKIN IS CRACKED AT L36 AND STA 1746. REMOVED FASTENERS IN CORRODED AREA FOUND L36 AFT OF STA 1746. REMOVED 9 X 6 SECTION OF SKIN REF SRM 53-02-011 NR 39550, REF ECA 56908 LOG PAGE 039299 PAGE 27.

Part: FITTING — CRACKED (LT WING TE FLAP)

LT INBOARD FLAP HINGE CRACKED (MARKED) LT WING STA 98. DEFERRED PER FERRY PERMIT 9020. REMOVED STA 98 BASED FTG & ATTACHING STRUCTURE. LOCATED & DRILLED NEW 5751182-505 BASE FTG IAW DAC DWG 5751172. INSTALLED BASE FTG IAW DAC DWG 5751172. INSTALLED CLOSURE PANELS & ATTACHING STRUCTURE IAW DC8 SRM 51-3-0. CHECK FLAP IAW DC8 MM 27-51-04. OPS CHECK GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (NR 3)

NR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD.

Part: ODOR — DETECTED (COCKPIT)

INSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUPLICATE ODOR. OK FOR CONTINUED SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D, 53-2-0 FIG 2D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LONG 35L BETWEEN STA 1650-1680, FABRICATED AND REPLACED LONGERON SECTION AND END FITTINGS IAW DWG 3647110, AND SRM 51-1-20D, 51-3-0.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACED DOUBLER IAW DWG 5649028, AND SRM 51-1-20D, 51- 1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D, 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5616306, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITTING HAVE INTERGRANULAR CORROSION AT STA 280 LONG 21L. REMOVED AND REPLACED FITTINGS IAW DWG 4773295 AND SRM 51-3-0, 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND SKIN IS CRACKED AT STA 60 BETWEEN LONG 20L AND 21L. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKIN IS CRACKED BETWEEN LONG 31R AND 32R. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG 22.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CRACKED AT LONG 22R APPROX. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW SRM 53-2-0 FIG 21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 STA 822 LONG 12R FRAME FITTING IS CRACKED AT EMERGENCY EXIT FRAME, AFT FITTING. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D, 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN, INTERNAL DOUBLER, AND LONG 11R ARE CRACKED AT STA 1654 AND LONG 11R. CUT OUT CRACKED AREA ON SKIN AND INTERNAL DOUBLER, STOPDRILLED CRACK ON LONG 11R. NDT VERIFIED NO CRACKS AT STOPDRILL AND CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, FILLER, AND STRAP IAW DC8-5330-16410-A, AND 8110-3 APPROVED DH SK 706-504.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT L-1 DOOR FWD UPPER CORNER STA 25 BETWEEN LONG 10L-11L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.

Part: RIB — CRACKED (LT WING) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 SKIN CRACKED STA 160 LONG 10R-11R. REMOVED EXISTING, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED REPAIR FILLER, AND DOUBLERS IAW SRM 53-2-0 FIG 14.

Part: RIB — CRACKED (LT WING) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 LT WING T/E UPPER RIB IS CRACKED AT XRS 247. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 BELLY SKIN BULGING APPROX 2 FT FWD TO THE RIGHT OF THE VHF ANTENNA, NO CORROSION FOUND. REMOVED FASTENER TO INSPECT AND REPLACED WITH BLIND. FOUND LONG 36 CORRODED BEYOND LIMITS STA 1260-1350. REMOVED AND REPLACED LONGERON SECTION IAW DWG 3758593, AND SRM 53-1-0, 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,093 hrs · 45,443 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER AFT CORNER STA 1660 BETWEEN LONG 20L-21L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED PREFLIGHT CHECK. REPLACED LIGHT BATTERY PACK, OPS CHECK NORMAL.

Part: HINGE FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE:N/A PIT34 LWR AFT BELLY CARGO DOOR UPPER FWD HINGE POINT STRUCTURE CRACKED. DOOR COMES OFF TRACK AND WILL NOT CLOSE. CLOSED DOOR AND TAPED HANDLE IN STOWED POSITION. REPAIRED IAW DC8 SRM 52-2-0 LOG PAGE 780026 AND 780028.

Part: FLAP — CRACKED (LT WING)

INSPECTION TYPE:PFLT LEFT WING INBOARD FLAP HAS A CRACK ON INBOARD TRAILING EDGE NEXT TO FUSELAGE AND BENT. REMOVED PREVIOUS SKIN REPAIR. REPAIRED IN REF SRM 57-20-0.

Part: TIRE — WORN (NLG)

INSPECTION TYPE:N/A BTB - REJECTED TAKEOFF AT80 KIAS DUE TO VIOLENT SHAKING AND THUMPING SOUNDS DURING TAKEOFF ROLL. SUSPECTED BLOWN NOSE TIRE. FOUND LEFT AND RIGHT NOSE TIRES WORN UNEVEN. SUSPECT OUT OF ROUND PER MM 32-50-00. REMOVED AND REPLACED LEFT AND RIGHT NOSE TIRES.

Part: PUMP — LEAKING (HYD SYSTEM)

INSPECTION TYPE:N/A HYD LOSS DOWN TO APPROX 6 GAL BYPASSED PUMPS. RAN LOSS OF HYD FLUID OR PRESS AND WAS ABLE TO CONFIGURE WITH GEAR AND FULL FLAPS - FLUID LEAKING AFTER LANDING RT SIDE R-R RUDDER STANDBY PUMP PN 57155A. OPS AND LEAK CHECKED OK. DURING ENG RUNS FOUND BOTH EDP LEAKING. REPLACING BOTH PUMPS.

Part: BUSS — OPEN (COCKPIT)

BTB-FOR SMOKE IN COCKPIT DUCT OVERHEAT LIGHT ON. SMOKE IN COCKPIT LEFT PACK TEMP GAUGE PEGGED FULL HOT. LEFT PACK WAS NEVER TURNED ON. SUSPECT LOSE OF NR 1 BUS OPENING LEFT PACK VALVE, RUN BOTH PACKS NO DEFECTS NOTED.

Part: RIB — CRACKED (RT WING)

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

Part: LONGERON — CRACKED (BS 1650)

INSPECTION TYPE:C123 STA 1650, LONGERON 33L HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (BS 1767-1780)

INSPECTION TYPE:C123, STA 1767-1780, STR 18L IS CRACKED UNDER THE END FITTING. REPAIRED AREA IAW SRM 53-2-2 FIG 10 AND FIG 11.

Part: FRAME — CRACKED (BS 55)

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

Part: STRINGER — CRACKED (BS 1767)

INSPECTION TYPE:C123 STA 1767, STR 18R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1767-1780)

INSPECTION TYPE:C123, STA 1767-1780, LONGERON 18R IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10 AND FIG 11.

Part: RIB — CRACKED (VERTICAL STAB)

INSPECTION TYPE:C123, LOWER VERTICLE STAB L/E RIB IS CRACKED RIGHT SIDE AT ZFS 111.00. REPAIRED IAW SRM 55-2-0 FIG 2.

Part: FLOORBEAM — CRACKED (BS 1200)

INSPECTION TYPE:C123, FLOORBEAM END FITTING IS CRACKED AT STA 1200 RBL54. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754923 AND SRM 51-1-20D.

Part: FINGER DOUBLER — CRACKED (BS 610)

INSPECTION TYPE:C123, STA 610 BTWN STR 31L-31R, THE FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5750365 AND SRM 51-1-20D.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:C123, RIGHT HORIZONTAL L/E RIB IS CRACKED AT XFS 135. REPAIRED IAW SRM 55-2-0 FIG 2.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,822 hrs · 44,559 cycles

INSPECTION TYPE:C123, KEEL BEAM HAS HEAVY CORROSION AT STA 780, 740, 670 - 680. REPAIRED AREA IAW 8110-3 APPROVED DH SK 706-039.

Part: SKIN — CORRODED (BS 690)

INSPECTION TYPE:C123, FUSELAGE SKIN HAS HEAVY CORROSION AT STA 690 BTWN STR 31L-31R. REPAIRED AREA IAW 8110-3 APPROVED DH SK 706-984.

Part: RIB — CRACKED (LE FLAP)

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

Part: RIB — CRACKED (WS 250)

INSPECTION TYPE:C123, RT WING L/E AT STA XS250.089, THE RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769859 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 520)

INSPECTION TYPE:C123, LEFT WING L/E AT STA XS520.168, THE UPPER RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769857 AND SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,822 hrs · 44,559 cycles

INSPECTION TYPE:C123, STA 1220 FRAME/SLIDE RAIL ABOVE STR 35L HAS HEAVY CORROSION ON UPPER FLANGE LWR SURFACE. REMOVED, FABRICATED AND REPLACED FRAME/RAIL IAW 8110-3 APPROVED DH SK 706-958 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 1748.5)

INSPECTION TYPE:C123 STA 1748.5 LONG 15L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG DC8-53B-009-39, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1748.5)

INSPECTION TYPE:C123 STA 1748.5, LONGERON 15R IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (BS 1754)

INSPECTION TYPE:C123 STA 1754, LONGERON 14L IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (BS 1048 - 1060)

INSPECTION TYPE:C123, STA 1040-1060 LONGERON 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C123, STA 1180 LONGERON 26L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854, AND SRM 51-1-21.

Part: RIB — CRACKED (LE FLAP)

INSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE:C123, STA 1200 BETWEEN LONGERON 27L-28L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755842, AND SRM 51-1-20D.

Part: SKIN — CRACKED (HORIZ STAB)

INSPECTION TYPE:C123, LEFT HORIZ STAB L/E AT STA FSX0, THE LOWER CAP IS CRACKED. REMOVED, FABRICATED AND REPLACED CAP IAW DWG565449.

Part: FITTING — CRACKED (BS 1150 STR 26L)

INSPECTION TYPE:C123, STA 1150 LONGERON 26L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854, AND SRM 51-1-21.

Part: FITTING — CRACKED (RT WING)

INSPECTION TYPE:C123 RIGHT WING L/E FITTING CRACKED AT XS 250.089. REMOVED AND REPLACED FITTING IAW DWG 5754705, AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (HORIZ STAB)

INSPECTION TYPE:C123 LEFT H-STAB L/E INBD SIDE ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED ANGLE IAW DWG 3701427, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LE FLAP)

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIBS CRACKED ST XFS 322.75,XFS 448.51, XFS454.976,XFS484.895. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LE FLAP)

INSPECTION TYPE:C123, RIGHT WING L/E ANGLE IS CRACKED AT INBOARD RIB NR 4 PYLON AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 600 - 620)

INSPECTION TYPE:C123, STA 600-620 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 440 - 460)

INSPECTION TYPE:C123, STA 440-460 LONGERON 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 600 - 620)

INSPECTION TYPE:C123, STA 600-620 LONGERON 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 485)

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 485. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-21, 51-1-21A.

Part: INTERCOSTAL — CRACKED (BS 360 - 380)

INSPECTION TYPE:C123, STA 360-380 INTERCOSTAL BETWEEN LONGERON 33L-34L. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21, 51-3-0.

Part: FITTING — CRACKED (BS 350)

INSPECTION TYPE:C123, STA 350 BETWEEN LONGERON 36AND 35L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 80 STR 3R)

INSPECTION TYPE:C123, STA 80 LONGERON 3R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680 STR 5R)

INSPECTION TYPE:C123, STA 680 LONGERON 5R END FITTING IS CRACKED AFT SIDE OF FRAME. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 220 -240)

INSPECTION TYPE:C123 STA 220-240 LONGERON 13R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5755292, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 902 - 920)

INSPECTION TYPE:C123, STA 902-920 LONGERON 6L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-21, 51-1-20D.

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE:C STRINGER SPLICE FITTING CRACKED FS 1260-1280 L-35L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 1160)

INSPECTION TYPE:C SHEAR TIE LWR FLANGE LWR SURFACE HAS MODERATE CORROSION F/S 1160 L-34R TO L-33R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: LONGERON — CRACKED (BS 1272)

INSPECTION TYPE-C, LONGERON 35R IS CRACKED AT STA 1272. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5750322 AND DWG 3758593.

Part: RIB — CRACKED (WS 297.5)

INSPECTION TYPE:C LT WING L/E RIB AT W/S XFS 297.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 240)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN AT STA XW240.00 IS CRACKED IN 2 PLACES, NEAR THE L/E AT THE FRONT SPAR. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE:C RT WING I/B SLOT O/B VERTICAL ANGLE CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND DWG 9753293.

Part: SKIN — CRACKED (WS 314-310)

INSPECTION TYPE:C RT WING L/E LWR SKIN CRACKED 2 PLCS XFS 304-310 7 FWD OF TE AND 5 FWD OF T/E. REPAIRED IAW DC8-5720-4087-B.

Part: ANGLE — CRACKED (WS 246.089)

INSPECTION TYPE:C, LT WING L/E I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM, (STA.XS246.089). REMOVED AND REPLACED ANGLE IAW DWG 9753293.

Part: WEIGHT — CORRODED (LT AILERON)

INSPECTION TYPE-C, LEFT I/B AILERON I/B BALANCE WEIGHT HAS MODERATE CORROSION. REMOVED AND REPLACED THE I/B AILERON IAW MM 27-11-01.

Part: FITTING — CORRODED (BS 8)

INSPECTION TYPE-C, LONGERON 36 END FITTING AT STA 8 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755865.

Part: DOUBLER — CRACKED (WS 78.5)

INSPECTION TYPE-C, RT WING FUEL TANK ACCESS PANEL LAND IS CRACKED AT THE AFT O/B CORNER (XCW 78.5). REPAIRED AREA IAW SRM 57-2-1 FIG 36.

Part: SKIN — CRACKED (WS 76)

INSPECTION TYPE:C RT WING UPPER SKIN CRACKED AT STA 76 STR 10 AFT ROW OF FASTENERS. REPAIRED IAW SRM 57-2-1.

Part: WEIGHT — CORRODED (RT AILERON)

INSPECTION TYPE-C, RT WING I/B AILERON BALANCE WEIGHT IS CORRODED. REMOVED AND REPLACED I/B AILERON IAW MM 27-11-01.

Part: SKIN — CRACKED (WS 360-385)

INSPECTION TYPE:C RT WING L/E UPPER SURFACE CRACKED IN 2 PLACES FWD OF TE XFS 360.25 AND 385.25. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C THE FUSELAGE SKIN IS CRACKED AT THE UPPER FWD CORNER OF THE D PIT DOOR CUTOUT. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CORRODED (BS 58)

INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN AT STA 58 AND LONGERON 34R IS CRACKED AND CORRODED. REMOVED AND REPLACED BELLY SKIN FROM STA -136 TO 70 IAW DC8-5330 -8942 C.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE N/A, EEL WILL NOT STAY ON. REMOVED AND REPLACED EMERG BATT PACK, OPS CHECK GOOD (P/N 5708458-503) ON, (S/N 2054) ON.

Part: SKIN — DENTED (BS 1890)

INSPECTION TYPE-N/A, FUSELAGE DENTED APPROX 3 INCH FWD OF STA 1890 BETWEEN STRINGER 36 AND 35 LEFT. *S/D* REPAIR ACCOMPLISHED AS PER SRM ADDIDUME DC8-5350-7876. DMI 143423

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY BATTERY WEAK. REPLACED EMERGENCY BATTERY PACK, OP CHKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-WKD, EMERGENCY EXIT LIGHTS FOUND INOPERATIVE DURING WEEKEND OPERATIONAL CHECK. REMOVED, REPLACED AND TESTED EMERGENCY BATTERY PACK IAW MM 33-50-02.

Part: SKIN — CORROSION (BS 1690-1890)

INSPECTION TYPE-C, REMOVED AND REPLACED BELLY SKIN AFT OF STA 1690. REMOVED AND REPLACED SKIN (P/N 5649329-75N2) IAW SRM 51-1-21 FROM STRINGER 28L TO 28R, BS 1690 TO 1890.

Part: FITTING — CRACKED (BS 834.5)

INSPECTION TYPE: C. HORIZONTAL FITTING CRACKED AT FWD SIDE OF FRAME 834.5 AT STR. 22R. REMOVED DAMAGED FITTING IAW SRM 51-1-20. FABRICATED FITTING AND INSTALLED AT FRAME IAW SRM 51-1-29D.

Part: FITTING — CRACKED (BS 822)

INSPECTION TYPE-C, HORIZONTAL FITTING AFT SIDE OF FRAME 822.5 AT STR 22L CRACKED. REMOVED DAMAGED FITTING IAW SRM 51-1-20, FABRICATED FITTING AND INSTALLED AT FRAME 822.5 OF STR 22L.

Part: INTERCOASTAL — CRACKED (BS 260)

INSPECTION TYPE: C. NR 1 PIT STA 260-270 AT STR 33L INTERCOASTAL BETWEEN FRAMES HAS A HOLE AND 2 CRACKS IN RADIUS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0.

Part: SHEAR TIE — CRACKED (BS 1640)

INSPECTION TYPE: C. SHEAR TIE AT STA 1040 BETWEEN STR 31-32 CRACKED AT RADIUS. REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-2-0 AND 51-1-20D.

Part: SKIN — CRACKED (WS 339.5)

INSPECTION TYPE: C. LT WING CENTER L/E UPPER SKIN AT STA 339.5 IS CRACKED AT A SCREW HOLE, .7 INCHES LONG ON BOTH SIDES OF HOLE. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-1.

Part: ANGLE — CRACKED (LT LE FLAP)

INSPECTION TYPE: C. LT WING L/E SLOT VANE ATTACH ANGLE I/B END IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM'S 51-1-21, 57-1-1, 51-1-4, 51-1-21, AND DOUGLAS DWG 5769891.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE: C. LT WING SECTION BETWEEN PYLONS AT CENTER AFT OF PART HAS L/E RIB SUPPORT ANGLE CRACKED ON LOWER AFT END. STOP DRILLED CRACK AND INSTALLED REPAIR IAW 57-2-0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE: C. FITTING AT STA 1090, STR 30R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM'S 51-3-0 AND 51-1-21.

Part: SKIN — CRACKED (BS 1741-1749)

INSPECTION TYPE-C, LT FUSELAGE SKIN BS 1746 LONGERON 16 WAS FOUND TO HAVE 3 CRACKS AFTER REMOVAL OF DOUBLERS. CUT OUT DAMAGED AREAS, INSTALLED FILLERS AND DOUBLERS IAW DHC SK 706 -117B REF, ENGINEERING FILE NR DC8-53-1736.

Part: SKIN — CRACKED (WS 258)

INSPECTION TYPE-C, LT WING CENTER L/E SKIN AT STA XW258 IS CRACKED AT ONE FASTENER HOLE THE CRACK IS APPROX 1 INCH LONG. STOP DRILLED CRACK AND REPAIRED PER SRM ADDENDUM EO DC8-5720-7767-A.

Part: DOUBLER — CRACKED (WS 435)

INSPECTION TYPE-C, RT WING L/E INTERNAL LOWER DOUBLER AND STRAP CRACKED AT RIB XFS435. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND STRAP AND INSTALLED IAW SRM 51-1-21.

Part: STRINGER — CORRODED (BS 1180-1190)

INSPECTION TYPE: C. STA 1180 TO 1190 HAS CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS DOUBLER, FILLER, AND SPLICE ANGLE AND INSTALLED IAW DHC SK706-731. REF UPS EFN FILE NR DC8-53-1735.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE: C. STA 1690 STR 25L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-21 51-1-20D.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE: C. FUSELAGE STA 1690 LONGERON 33R END FITTING EXFOLIATED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-21.

Part: LONGERON — CRACKED (BS 1675-1689)

INSPECTION TYPE: C. STR 24L FWD OF STA 1690 IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON STA 1675-1689, FABRICATED AND INSTALLED REPAIR SECTION IAW SRM 53-2-2, 53-4-1, AND 51-1-21.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE-C, STA 1690 STR 36 END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21.

Part: ATTACH FITTING — CRACKED (BS 1680)

INSPECTION TYPE: C. ATTACH FITTING AT STR 24L, F.S. 1690 CRACKED ON UPPER FLANGE FASTENER HOLE. REMOVED AND REPLACED ATTACH FITTING PER SRM'S 53-1-0, 51-1-21, 51-1-20 D.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED REPAIR PER DC8 SRM 57-2-0.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE: C. LT WING L/E SECTION BETWEEN PYLONS HAS LOWER L/E RIB CRACKED AT THE AFT END, BELOW AND AFT OF SLOT ACTUATOR. STOP DRILLED CRACK PER SRM 57-2-0 AND INSTALLED REPAIR IAW DC8 SRM 57-2-0.

Part: FITTING — BROKEN (BS 1690)

INSPECTION TYPE-C, FUSELAGE STA 1690 STR 34R 2ND FITTING FLANGE BROKEN OFF. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-21.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE: C. LT WING L/E SECTION BETWEEN PYLONS HAS UPPER L/E RIB CRACKED AT THE AFT END ABOVE SLOT ACTUATOR. STOP DRILLED CRACK AND INSTALLED REPAIR IAW DC8 SRM 57-2-0.

Part: LONGERON — CORRODED (BS 1765)

INSPECTION TYPE-C, FS 1765, LONG 34R IS CORRODED. REMOVED AND REPLACED STRINGER 34R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-1-21.

Part: LONGERON — CRACKED (BS 1691)

INSPECTION TYPE-C, FS 1691, LONG 30R IS CRACKED. REMOVED AND REPLACED STR 30R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-3-0.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE: C. LEFT WING L/E O/B SECTION HAS 1 EA LWR L/E RIB CRACKED INSIDE 2ND ACCESS PANEL O/B OF I/B END. STOP DRILLED CRACK . NDT VERIFIED CRACK TERMINATED. FABRICATED AND INSTALLED REPAIRS PER UPS SRM 57-2-0 FIG. 2 AND DC8 S.R.M. 06-00-00.

Part: SPLICE — CORRODED (BS 1690)

INSPECTION TYPE-C, AFT TEE CHORD SPLICE STA 1690 LBL 12 SEVERLY EXFOLIATED. REMOVED EXISTING SPLICE, FABRICATED REPLACEMENT SPLICE ANGLE IAW DWG 3642778, DRILLED AND INSTALLED IAW SRM 51-30-1.

Part: LONGERON — CORRODED (BS 1690)

INSPECTION TYPE-C, LONGERON 36 CORRODED AT STA 1690. REMOVED CORRODED SECTION OF LONGERON 36 FROM STA 1690 TO STA 1730 PER SRM 53-2-2. FABRICATED AND REPLACED LONGERON PER SRM 53-2-2 AND 51-3-0.

Part: RIB — CRACKED (LT WING LE)

INSPECTION TYPE: C. LT WING O.B. L/E SECTION HAS 6 L/E RIBS CRACKED AT AFT END. STOP DRILLED L/E RIBS, FABRICATED AND INSTALLED REPAIR PARTS PER SR M 57-2-0 AND 51-1-20D.

Part: ANGLE — CORRODED (BS 858/930)

INSPECTION TYPE-C, ANGLE HAS EXFOLIATION CORROSION AT RT MLG W/W TOP FWD STA 858 AND STA 930. REMOVED CORROSION, FLAP PEENED, INSTALLED FREEZE PLUG AND REPAIRED STRAP PER DHC SK-706-663, REF UPS ENGINEERING FILE NR DC8-53-1734, DPS 4.999-2, AND SRM 51-1-8, SRM 51-1-20.

Part: DOUBLER — CORRODED (BS 1610-1690)

INSPECTION TYPE-C, INTERNAL DOUBLER EXFOLIATED OUT OF LIMITS, VARIOUS AREAS FROM BS 1610 TO 1690 STRINGERS 25L TO 31L. REMOVED FASTENERS AND INTERNAL DOUBLER PER SRM 51-1-20. REMOVED CORROSION AND TREATED SKIN PER SRM 51-1-8. SKIN WITHIN LIMITS PER SRM 53-2-0 FIGURE 1F. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21.

Part: FITTING — CORRODED (CTR WING BOX)

INSPECTION TYPE-C, CENTER WING BOX UPPER SURFACE FWD RT CORNER FITTING HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 10.

Part: CLIP — CRACKED (BS 1338.23)

INSPECTION TYPE: C. FRAME CLIP CRACKED AT STA 1338.23, LT UPPER CUSP, AFT SIDE OF FRAME. STOP DRILLED CRACK PER SRM 53-2-0. FABRICATED FRAME CLIP ANGLE REPAIR AND INSTALLED FASTENERS PER SRM 53-2-0 AND SRM 53-20-10.

Part: DOUBLER — CORRODED (BS 350-370)

INSPECTION TYPE-C, NR 1 PIT STA 350 TO 370 BTWN STR 35L TO 35R ANTENNA DOUBLER HAS HEAVY CORROSION. REMOVED AND REPLACED DOUBLER IAW DOUGLAS DWG 5754129 AND SRM 51-1-20 D AND 51-1-20.

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE: C. UPPER LE RIB CRACKED 2.0 INCHES ON RT WING AT STA. XFS 442.2. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE: C. LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED IN TWO PLACES ABOVE THE PNEUMATIC DUCT. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 711)

INSPECTION TYPE: C. LT WING O/B L/E SKIN AT XFS 711 IS CRACKED AT A SCREW HOLE. CRACK IS APPROX .36 INCH LONG JUST BELOW L/E HFEC INSP. VERIFIED CRACK TERMINATES AT SCREW HOLE. FABRICATED AND INSTALLED REPAIR IAW UPS E.O. DC8-5720-7767-A.

Part: RIB — CRACKED (WS 448.581)

INSPECTION TYPE: C. LT WING L/E RIB AT STA XFS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, PER SRM 57-3-11 AND 51-1-21.

Part: STRINGER — CRACKED (WS 508)

INSPECTION TYPE-C, RT WING NR 4 ALT TANK AT STA XRS 508.00, WING STRINGER 54 IS CRACKED IN HALF. REMOVED DAMAGED SECTION OF STR 54 AND REPAIRED IAW DHC SK-706-686 REF ENGINEERING FILE NR DC8-57-0748.

Part: COALESCER BAG — CONTAMINATED (RT PACK)

INSPECTION TYPE-N/A, STRONG DIESEL FUEL SMELL COMING FROM RIGHT PACK. CREW FELT NAUSEA AND HEADACHES, ONE HAD TO USE OXYGEN. REPLACED RT A/C WATER COALESCER BAG. BOTH PACKS OP/C FOR SMELL, NO SMELL NOTED OP/CK GOOD.

Part: STANDBY PUMP — LEAKING (RUDDER)

INSPECTION TYPE-N/A, AT FL35 HYD SYS PRESS WENT TO ZERO, HYD QTY DROPPED TO JUST ABOVE THE X-POSITION AND THE RUDDER AND AILERON MANUAL CONTROL LIGHTS ILLUMINATED. HYD FAILURE CHKLIST ACCOMPLISHED. FLUID BEGAN TO DECREASE RAPIDLY WITH AUX PUMP ON. FOUND STANDBY RUDDER PUMP LEAKING FROM DRAIN LINE. REPLACED STANDBY RUDDER PUMP AND TAGGED, REMOVED PART HOLD FOR EVALUATION.

Part: DOOR FRAME — CRACKED (PAX DOOR)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FWD ENTRY DOOR AFT FRAME SEGMENT CRACKED ABOVE BAYONETTE. REPAIRED PER UPS EO.

Part: SKIN — CORRODED (BS 1240)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SKIN AT STATION 1240 AND LONGERON 36. MAINTENANCE REPAIRED THE SKIN PER UPS EO DC8-5330-7351-A.

Part: LONGERON — CORRODED (BS 1445-1460)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R AT STATION 1445 - 1460. MAINTENANCE REPAIRED THE LONGERON PER UPS EO DC8-5310-7352-A.

Part: SKIN PANEL — CORRODED (BS 1350)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE BELLY SKIN AT STATION 1350 - 1490. MAINTENANCE REPLACED THE SKIN PANEL PER SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CORRODED (BS 1360-1460)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 35R AT STATION 1360 - 1460. MAINTENANCE REPLACED THE LONGERON PER SRM 51-1-20D.

Part: SKIN — CORRODED (BS 35)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE SKIN AT STATION 35 AND LONGERON 31R. MAINTENANCE REPAIRED PER UPS EO DC8-5330-7343-A.

Part: SKIN — CRACKED (BS 1540)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FUSELAGE SKIN AT STATION 1540 AND LONGERON 33R - 34R. MAINTENANCE REPAIRED PER UPS EO DC8-53-1445.

Part: SKIN — CORRODED (BS 160)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE SKIN AT STATION 160 - 190 AND LONGERONS 34L - 35R. MAINTENANCE REPLACED THE BELLY SKIN PANEL PER SRM 51-1-20D, 51-1-21 AND 51-1-14.

Part: SKIN — CORRODED (BS 1155)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SKIN AT STATION 1155 AND LONGERON 33R. MAINTENANCE REPAIRED THE SKIN PER UPS EO DC8-5330-7345-A.

Part: LONGERON — CORRODED (BS 80)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34R AT STATION 80 - 187. MAINTENANCE REPLACED THE LONGERON PER SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 100-187)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 36 AND ON THE END FITTING AT STATION 100 - 187. MAINTENANCE REPLACED THE LONGERON AND END FITTING PER SRM 51-1-20D,

Part: FRAME — CORRODED (BS 120)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE BELT FRAME LOWER LIP AT STATION 120 AND LONGERON 35L - 35R. MAINTENANCE REPAIRED THE FRAME PER SRM 53-2-0.

Part: LONGERON — CRACKED (BS 857)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN LEFT HAND LONGERON 24, UPPER VERTICAL FLANGE AT STATION 857. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2.

Part: SKIN — CRACKED (NR 1 SPOILER)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK ON THE LOWER SURFACE OF THE LEFT HAND WING NR 1 SPOILER. MAINTENANCE REPAIRED THE SPOILER PER SRM 51-1-9.

Part: SHEAR TIE — CRACKED (BS 1440)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 2 INCH CRACK IN THE SHEAR TIE AT STATION 1440 AND LONGERON 33L TO 34L. MAINTENANCE REPAIRED THE SHEAR TIE PER SRM 53-2-0.

Part: SPLICE — CRACKED (BS 1490)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SPLICE STRAP AT STATION 1490 AND LONGERON 32L. MAINTENANCE REPLACED THE SPLICE PER SRM 51-1-21.