N811UP

Part: BATTERY PACK — DISCHARGED (COCKPIT)

FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AND OPS CK IAW MM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS ON AT POWER TRANSFER, WOULD NOT GO OUT. 09-07-07 RESET DC EMERGENCY BREAKER. SYTEM OPS CKS OK REF MM 33-50-00-0.

Part: STRUCTURE — TORN (CARGO BAY)

APPROX 1 INCH TEAR IN FLOOR OF PIT 33 APPROX 24 INCHES A/C LEFT OF CENTER & APPROX 36 INCHES FROM AFT BULKHEAD. C/W UPS EO DC8-5320-8724 APPROX A. D355594 ISSUED BY AMC. REPAIRED PIT 33 FLOOR PER EO DC8-5320-8724. PERMANENT REPAIR INSTALLED. D355594 CLEARED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS DISENGAGED. LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPS CHECK GOOD IAW MM 33-10-00.

Part: DOWNLOCK SWITCH — INOPERATIVE (LT MLG)

INSPECTION TYPE:N/A EMERGENCY DECLARED - LEFT MAIN GEAR LIGHTS DID NOT ILLUMINATE GREEN. REPLACED BULBS WITH KNOWN BULBS THAT WORKED BUT STILL COULD NOT GET GREEN LIGHTS TO ILLUMINATE. WITH THE FLAPS AT 35 DEG THE LANDING GEAR WARNING HORN DID NOT SOUND. T/S AND FOUND FAULTY DOWN SWITCH ASSY PER DC8 MM 32-60-00-1. REMOVED AND REPLACED FAULTY SWITCH. A/C READY FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A TWO EMERGENCY LIGHTS AT MAIN CREW ENTRY DOOR INOP. RELAMPED INOP EMERGENCY LIGHTS PER MM 33-01-00. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 EXTERIOR FUSELAGE SKIN CRACKED AT L30L STA 1690. REPAIRED FUSELAGE SKIN AT STA 1690 L30R - L28L IAW SAA EA 008-5330- 01-0750, UPS EO DC8-5330-26567-A, FAA FORM 8100-9, AND AMOC APPROVAL FOR AD 2007-02-02.

Part: FRAME SPLICE — CRACKED (FS 1690 L24L) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 L24L END FITTING CRACKED ON AFT SIDE OF STA 1690 FRAME SPLICE. REMOVED END FITTING AT STA 1690 L24L IAW SRM 51-1-21. DRILLED, REAMED AND INSTALLED END FITTING AT STA 1690 L24L IAW SRM 51-3-2 AND SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (FS 1790 LBL8) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 FLOORBEAM STA 1790 LBL 8 HAS DEEP GOUGE AND EXFOLIATED CORROSION. REMOVED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 51-3-0. FABRICATED AND INSTALLED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 53-7-3, AND SRM 51-3-0.

Part: FLOORBEAM — CORRODED (FS 1723) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 FLOORBEAM STA 1723 RBL 30 - RBL 15 HAS POPPED RIVETS AND EXFOLIATION CORROSION. REMOVED CORROSION AND REPAIRED FLOORBEAM AT STA 1723 RBL 30 - RBL 15 IAW SAA EA 008-5320-01-A0762, UPS RAA DC8-53-20617, AND FAA FORM 8100-9.

Part: DOUBLER — CORRODED (FS 220 L35L-L35R) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 HEAVY CORROSION ON INTERNAL DOUBLER AT FS 220 BETWEEN L35L AND L35R A-PIT. REMOVED CORROSION AND REPAIRED INTERNAL DOUBLER AT STA 220 BETWEEN LONGERONS 35L AND 35R IAW SAA EA 008-5310-01-A0747, UPS RAA DC8- 53-20613, AND FAA FORM 8100-9.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 L30R AT STA 1700 HAS CORROSION. CORROSION EXTENDS UNDER END FITTING. REMOVED EXFOLIATED AND CRACKED END FITTING AT STA 1700 L30R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SEGMENT AT STA 1700 L30R IAW SRM 53-02-002 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 1260 TO 1280 L34L. REMOVED LONGERON SPLICE FITTING AT STA 1260-1280 L34L IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED LONGERON SPLICE FITTING AT STA 1260-1280 L34L IAW SRM 51-3-2, AND SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 INTERCOSTAL UNDER SEAT TRACK STA 70-80 RBL 48 HAS CORROSION. REMOVED INTERCOSTAL AT STA 65-80 IAW SRM 51-1-20D. FABRICATED INTERCOSTAL AND INSTALLED AT STA 65-80 IAW DWG 4888755, AND SRM'S 51-3-2, AND 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FS960-980 RBL65) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 CENTER WING BOX SUBFLOOR FINGER DOUBLER CORRODED AT STA 960-980 RBL 65. REMOVED FINGER DOUBLER AT STA 960-980 RBL 65 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 960-980 RBL 65 IAW SRM 53-7-3, AND SRM 53-07-03-0.

Part: SHEAR TIE — CORRODED (FS 660 L35L-35R) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 SHEAR TIE CORRODED AT STA 660 L35R TO L35L. REMOVED SHEAR TIE AT STA 660 L35R-L35L IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 660 L35L-L35R IAW DWG 5616509, AND SRM'S 51-1-20D, AND 51-1-21.

Part: FINGER DOUBLER — CORRODED (FS 935 RBL65) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 SUBFLOOR FINGER DOUBLER HEAVY CORRODED AT STA 935 RBL 65. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 53-2-0 FIG 1F, 53-07-03 AND 51-3-02.

Part: SKIN — DAMAGED (RT WING) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 DEEP CREASED DENT 3 INCHES LONG ON LEADING EDGE O/B RIGHT WING. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-01-00 FIG 002H.

Part: RIB — CRACKED (LT WING) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 LEFT WING OUTBOARD LWR RIB CRACKED AT XFS 790. CRACK TERMINATES AT FASTENER HOLE PER HFEC INSP NDTSPM 06-10-01-001 FABRICATED AND INSTALLED REPAIR DOUBLERS AND ANGLES AT LEFT WING OUTBOARD LEADING EDGE STA XFS 790 IAW SRM 57-03-03 FIG 7, AND SRM 57-2-0.

Part: LONGERON — CORRODED (FS 662 L36) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 L36 HEAVILY CORRODED AT STA 662. REPAIRED LONGERON 36 AT STA 662 IAW SAA EA 008-5310-01-A0734, UPS EO DC8-5310-26461-A, AND FAA FORM 8100-9.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 HEAVY CORROSION AT BASE OF VERTICAL STIFFENER ON STA 8 BULKHEAD IN A/C COMP'T, LEFT SIDE, ABOVE L28. REMOVED, FABRICATED AND INSTALLED STIFFENER AND SPLICE REPAIR IAW SRM 51-1-21, 51-1-20D AND DWG 5615530.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 CRACK IN NLG WHEEL WELL CEILING (PRESSURE WEB) STA -13 LBL 2. REPAIRED PRESSURE WEB IN NLG WHEEL WELL CEILING AT STA -13 LBL 2 IAW SAA EA008-5330-01-A0745, UPS EO DC8-5330-26455-A, AND FAA FORM 8100-9.

Part: SKIN — CORRODED (FS 1710 L20L) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 BULGING SKIN ON EXTERNAL FUSELAGE AT STA 1710 L20L. CUT OUT DAMAGED AREA ON SKIN AT STA 1710 L20L IAW SRM 53-02-01-0 FIG 7. FABRICATED & INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER AT STA 1710 L20L IAW SRM 53-02-01-0 FIG 7.

Part: SPAR CAP — CRACKED (LWS 515) · airframe 80,006 hrs · 27,377 cycles

INSPECTION TYPE:C3 DURING WING FORWARD SPAR INSPECTION FOUND 1EA ATTACHMENT HOLE CRACKED. REPAIRED LEFT WING FRONT SPAR LWR CAP BETWEEN XFS 515 AND 526.76 IAW SAA EA 008-5710-01-A0733, UPS EO DC8-5710-26430-A, AND FAA FORM 8100-9.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

FOUND COCKPIT COURIER AREA AND ENTRY DOORS LIGHT INOP DURING PREFLIGHT BATTERY SAI EMERGENCY LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. FAILED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK REF MM 33-50-02-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01-2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

CREW ENTRY DOOR LIGHTS INOP. RELAMPED LIGHTS. OPS CK NORMAL.

Part: WIRE — BROKEN (ELECTRICAL)

NR 1 BUSS POWER FAILED IN FLIGHT. RESET ACCORDING TO CHECKLIST. FAILED SECOND TIME AND CONTINUED WITH FLIGHT. GPWS AND BUSS FAULT RELAY SWITCHES SAFETY WIRE BROKEN. REMOVED AND REPLACED NR 1 VOLTAGE REGULATOR AND GENERATOR CONTROL PANEL IAW MM 24-20-06-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY. OPS TEST GOOD. REF MM CH 33-50-01.

Part: BOOT — DISCONNECTED (WATER SEPARATOR) · airframe 79,709 hrs · 27,173 cycles

ATB - A/C WOULD NOT MAINTAIN PRESSURIZATION ABOVE FL 310. FLOWS ON BOTH SIDES WERE SET TO MAX PRESSURE CONTROL WAS TRIED IN BOTH AUTO AND MANUAL MODES. LT MANIFOLD TEMP READ 195 AND RIGHT TEMP WAS 235. MANIFOLD PRESSURE FOR BOTH SIDES. OPENED PNLS 697,91D AND 602B. FOUND RT BOOT AFT OF RT WATER SEP OFF REINSTALLED WATER SEP BOOT PER DC8 MM 20-11-00. LK CK GOOD PER DC8 MM 21-31-00. DURING OPS CK FOUND RT PK WILL NOT COOL AND NO WATER DRAINAGE FR WATER SEP DRAIN TUBE. REMOVED AND REPLACED 35DEG TEMP SENSOR IAW DC8 MM 21-55-06-4, OPS CK DUE. REMOVED 35DEG VLV, LK CK GOOD PER MM 21-55-04-4.

Part: SKIN — CORRODED (BS 8 L28R) · airframe 79,709 hrs · 27,173 cycles

INSPECTION TYPE:N/A COMPLY WITH DMI D-329976: FUSELAGE SKIN CORRODED AT STA 8 AND LONGERON 28R. REFERENCE UPS EO DC8 5330-24757-A DTD.7-25-06. REMOVED DAMAGED (CORRODED) AREA. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLERS, AND FINGER DOUBLERS AT STA 8 LONGERON 28R-29R IAW SAA EA 008-5330-01-A0330 DTD.08-03-06 AND UPS EO DC8 5330-24844-A DTD.08-03-06.

Part: SKIN — BULGED (FUSELAGE)

BULGED SKIN ON LOWER EXT SKIN AFT OF AC BAY. POPPED RIVETS. WILL FERRY (#9002) TO SAA FOR REPAIR. TRANS. TO NRC 123458 PLEASE VOID THIS ENTRY SEE UPS06847592 FOR CORRECTIVE ACTION COMPLETED BY SAT MAJOR MX.

Part: SKIN — GOUGED (FUSELAGE)

A/C CURRENTLY OOS DUE TO DENT AND CREASE FOUND FWD IN THE SKIN FWD OF THE CREW ENTRY DOOR. REPAIR UNDER EVALUATION. FOUND DENT & GOUGE IN FUSE SKIN FWD OF MAIN ENTRY DOOR 24 INCHES TO BE W/IN SRM REF 53-01-0 & 53-02-0 LIMITS. NO CRACKS NOTED IN FUSELAGE SKIN. VERIFIED NO CRACKS IN DENTED AREA. BLENDED GOUGE. TREATED & PAINTED AREA. ISSUED I328764 FOR DENT IN FUSE SKIN.

Part: SMOKE BARRIER — TORN

TEAR IN BOTTOM RIGHT CORNER OF SMOKE CURTAIN. BOTTOM OF SMOKE CURTAIN NOT ATTACHED TO FLOOR. REPAIR SMOKE CURTAIN IAW EO DC8-2550-1872B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A PHL LOAD SUP REPORTS HOLE IN PIT 33 FLOOR, APPROX 3 INCHES IN LENGTH LOC'D 24 INCHES AFT OF DOOR & SLIGHTLY LEFT OF CENTER. C/W DC8 LOWER CARGO COMPARTMENT PIT NR 33 FLOOR PANEL PERMANENT REPAIR PER EO DC8-5320-87224-A APPENDIX C. THIS CLEARS D326176. PLACARDS REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS FAILED TO OPERATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: SKIN — CORRODED (LONG) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE: C2 TEMP RIVET HEAD CENTER PIN MISSING, FASTENER HEAD LOW & SKIN BULGING AT APPROX STA 380 L/S BELOW L2 DOOR. UPON FURTHER INVESTIGATION FOUND CORROSION ON BACK SIDE OF SKIN AT STA 380 LONG 29L. REPAIRED IAW SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE: C2, INNER DENT CRACK IN O/B SKIN LEFT LOWER EMPENNAGE FS 1875 LONG 24L. REPAIRED IAW SRM 53-02-00.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE: C2, C-PIT FS 1150 INTERCOSTAL ATTACH FITTING CRACKED IN FWD RADIUS BETWEEN FASTENERS, BETWEEN LONGERONS 32R & 33R. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 79,103 hrs · 26,689 cycles

INSPECTION TYPE: C2, DURING COMPLIANCE OF EO DC8-5740-2937-E, FOUND CLIP CRACKED ON RT WING NR 3 MAIN TANK STRINGER 70. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING, REF SAA TRAVE LLER 0001, INSTALLED FITTING, REF SRM 51-1-20D, 51-1-21, DWG3755207.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE:C2 AFT PRESSURE BULKHEAD IS CRACKED APPROX 1 INCH AT LBL 35 AROUND LONGERON 12L AREA. NDT VERIFIED CRACK APPROX 1.5 INCH PER NDT SPM 06-10-01.001. REPAIRED AFT PRESSURE BULKHEAD IAW SRO DWG 8530007.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,103 hrs · 26,689 cycles

INSPECTION TYPE: C2, LONG 15R CRACKED AT STA 1746. DISASSEMBLED SPLICES AT STA 1726 & 1746. REMOVED SHEAR-TIES, FOUND STA 1746 ASSEMBLED WITHOUT STRAPS UNDER LONGERON. FAB LONG SECTIONS (EXTR S1616 757 & 2 STRAPS SHT7075T6-.080). TREATED, PRIMED, INSTALLED REPAIR PARTS REF SRM 53-2-0 FIG 10, DWG5649327, SRM 51-1-8, 51-1-20D. INSTALLED SHEAR TIES REF SRM 51-1-20D.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 79,103 hrs · 26,689 cycles

INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD CRACKED AT APPROX RBL 26 & L12R. REMOVED EXISTING DOUBLER AT SITE. CUT OUT DAMAGE, NDT VERIFIED. FAB 2EA -9 FILLERS -25 DOUBLER, -27 DOUBLER (7075T6-.063), -19 FILLER (SHT7075T6-.090), -11 FILLER (7075T6 -.063). TREAT, PRIME, INSTALL & SEALED ALL REF SRO8530007, SRM51-1-8, MM20-30-00, NDT/SPM06-10-01.001.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE:C2 C-PIT DOOR ENTRANCE FS 1220 L32R BANANA FITTING CRACKED .400 INCH LONG. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AT FS 1220 LONG 29R TO 33R.

Part: SKIN — CRACKED (ELEVATOR) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE:C2 RT ELEVATOR UPPER SKIN SURFACE I/B SIDE HAS A LIGHTENING STRIKE WITH .5 INCH CRACK STA XE 50. NDT VERIFIED .5 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK IAW SRM 55-2-1 FIG 10. NDT VERIFIED CRACK TERMINATES AT STOP DRILL PER NDT SPM 06-10-01.001. REPAIRED RT ELEVATOR PER SRM 55-2-1 FIG 10, CALCULATED WEIGHT/BALANCE PER SRM 51-04-08. NEW BALANCE WEIGHT IS -1445.4. INSTALLED NEW BALANCE DATA PLATE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,107 hrs · 26,689 cycles

INSPECTION TYPE: C2 LT L/E AT APPROX 660 HAS CORROSION AND FLAKING. REPAIRED LT L/E WING UPPER SKIN REPAIR AT XFS 710-824 IAW UPS EO DC8-57-20127, SAA SK 811-933.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,103 hrs · 26,689 cycles

INSPECTION TYPE:C2 EXT FUSELAGE SKIN CRACKED AT STA 1740 BETWEEN L16R & L17R. CUT OUT DAMAGE, NDT VERIFIED. FAB FILLER (SHT7075T6-.063), FINGER DOUBLER (SHT7075T6-.040), EXT DOUBLER (SHT7075T6-.071). INSTALLED SAME REF SRM 53-5-1 FIG 1, 53-2-1 FIG 7, NDT/SPM 06-10-01.001, 51-1-8.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD PER REF DC-8 MM CH 33.

Part: CABLE — BROKEN (LT AILERON)

AILERON BINDING ON RIGHT TURN. LEFT AILERON BUSSING CABLE BROKEN AT I/B OF AILERON. INSTALLED LEFT .125 INCH BUSS CABLE PER MM 27-13-22 UP TO STEP (H) ACCOMPLISHED REMAINING STOPS AND ADJUSTED PER MM 27-10-17-5.

Part: WINDOW FRAME — CORRODED (COCKPIT)

CAPTS WINDOW FRAME CORROSION. REMOVED CORROSION & APPLIED ZINC CHROMATE. LOWER CORNER IN SERVICEABLE CONDITION. OK TO CONTINUE.

Part: FITTING — CRACKED (CABIN)

CENTER ZEE FITTING STRUCTURE CRACKED. R&R CENTER WINDSHIELD LOWER CENTER CHANEL PER EO DC8-532019452A. PERMANENT TO BE INSTALLED AT NEXT C-CHECK PER ITEM 2 THIS SAME LOGPAGE.

Part: CONTROL PANEL — SMOKE (COCKPIT)

SMOKE IN FLIGHT DECK, ATB SMOKE COMING FROM BEHIND F/E PANEL. REMOVED 2 FUSES AND SMOKE DISSIPATED. FOUND 2 WIRES BROKEN OF P1-509 OF TI-19 REPAIRED AND REINSTALLED WIRES L120A20 & L94A-20. ALSO T/S PROBLEM TO DEFECTIVE TRANSFORMER TI-37.

Part: SKIN — CRACKED (LT WING) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, AFTER REMOVAL OF LEAKING FASTENERS FOUND EXTERNAL DOUBLER AND UPPER WING SKIN CRACKED AT FASTENER HOLE AT XRS 22 AT STRINGER 5. REMOVED DOUBLER, OVERSIZED FASTENER HOLE, NDT VERIFIED NO CRACKS AT HOLE, FABRICATED FREEZE PLUG BUSHINGS, DOUBLER AND INSTALLED IAW SAA SK 811-230, DC8-57-20070.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS AT STA 1580 AT LBL 5. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER IAW SRM 53-2-0 FIG 1G.

Part: FITTING — CRACKED (RT WING) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD SIDE AT XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.

Part: FITTING — CRACKED (LT WING) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, LT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD OF XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED AT XRS 74 INBOARD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.

Part: STRINGER CLIP — CRACKED (RIGHT WING) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, RIGHT WING STRINGER CLIP IS CRACKED AT STRINGER 73 AT XRS 50. REMOVED, FABRICATED, AND REPLACED CLIP IAW SAA SK 811-162.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STATION 280-300 LONGERON 28L IS CORRODED BEYOND LIMITS. REMOVED LONGERON 28L FROM STATION 265 TO 290, FABRICATED AND INSTALLED LONGERON SECTION, INSTALLED 2 LONGERON SPLICES AND REPLACED 2 BATHTUB FITTINGS IAW DWG 9754913 AND SRM 53-2-2 FIG 10, 53-2-0 FIG 2D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED AN INTERNAL DOUBLER REPAIR BETWEEN THE OUTER SKIN AND INTERNAL DOUBLER OF THE L-2 DOOR UPPER CORNER,THE SKIN HAS A CUTOUT APPROX 1.75 X .90. INTERNAL DOUBLER REPAIR IS CONDITION II, AT STA 1660 LONG 10L. REMOVED PREVIOUS REPAIR DOUBLER, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STATION 300 TO 320 LONG 13L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SAA SK 811-747 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C-1, LONGERON SPLICE FITTING CRACKED AT LONGERON 12L BETWEEN STA 300-320. REMOVED, FABRICATED AND REPLACED LONGERON SPLICE FITTING IAW SAA SK 811-748, UPS ENGINEERING FILE NUMBER DC8-53-20283, DWG 4613574 SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STA 1760 LONG 25L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICES IAW SRM 53-2-2 FIG 10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE:C1 INTERCOSTAL CRACKED ON BOTTOM SIDE AT STA 660 AT LONG 11L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5750540 AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, TRIPLER/DOUBLER REPAIR DOES NOT CONFORM TO THE SRM, AT L-2 DOOR LOWER FORWARD CORNER AT STA 1620 AT LONG 20L. REMOVED PREVIOUS REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC8-5310-7975-B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE:C1 MAIN CABIN FITTING IS CRACKED AT STA 680 FWD SIDE AT LONG 12R. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STATION 1720 LONG 14R IS CRACKED. REMOVED CRACKED LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND INSTALLED REPAIR SPLICES IAW SRM 53-2-2 FIG 10 AND 11.

Part: CLIP — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STA 200 FRAME FORMER IS CRACKED ON I/B END BETWEEN LONG 32L AND 33L. REMOVED CRACKED FORMER CLIP, FABRICATED AND INSTALLED FORMER REPAIR CLIP IAW SRM 53-2-0 FIG 2A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, FUSELAGE SKIN IS CRACKED AT STA 1734 ABOVE LONG 16L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, STA 80 LONG 22L EXTERNAL DOUBLER HAS SEVERAL LOOSE CHERRY LOCK RIVETS. REMOVED DOUBLER AND FOUND BLIND FASTENERS UNDER DOUBLER WITH NO PITCH TO REPAIR DOUBLER HOLES, SHEAR TIE DRILLED THRU RADIUS, REMOVED DAMAGED SHEAR TIE, CUT OUT DAMAGED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED SHEAR TIE, DOUBLER, FILLER, AND FINGER DOUBLER IAW DWG 5610088 AND SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, REMOVE STEEL DOUBLER AT UPPER FWD CORNER OF THE L-1 FWD ENTRY DOOR AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, 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 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, EXTERNAL FUSELAGE SKIN IS CRACKED AND CORRODED AT FASTENER HOLE AT STA 445 LONG 31L. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: CLIP — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE:C1 CLIP IS CRACKED AT STA 80 ABOVE LONG 30L. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5613064 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,322 hrs · 26,030 cycles

INSPECTION TYPE: C1, CRACKED FITTING BETWEEN STA 660 AND 680 AT LONGERON 11R IN MAIN CABIN. REMOVED AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:AS UPON BLOCK IN, CHECKED EMERGENCY EXIT LIGHTS. EMERGENCY EXIT LIGHTS INOP. R&R EMERGENCY BATTERY PACK ASSY. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ENTRY DOOR)

INSPECTION TYPE:N/A, LIGHT INOP IN EMERGENCY LIGHT ASSY AT ENTRY DOOR. RELAMPED AS REQ, EMERGENCY LIGHTS CK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1140 RT FWD SIDE LONG 34R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, LT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1040 - 1060 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1240 LONG 35L INTERCOSTAL FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758495, AND SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1240 - 1260 LONG 33R INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 9754949, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1766 LONG 17R LONG FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1308 LONG 33L IS CORRODED BEYOND LIMITS ON OUTBOARD UPPER FLANGE. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 811-942.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE, C2, 3, STA 585 - 595 LBL 60 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3 STA 1220 BANANA FITTING IS CORRODED BEYOND LIMITS AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1227 LONG 35R INTERCOSTAL FITTING AFT SIDE OF FRAME IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570, AND SRM 51-1-20D.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE C2, 3, STA 70 SEAT TRACK SCALLOP IS BROKEN AT LBL 48. REPAIRED SEAT TRACK.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 257 AND 230 AT LBL 60 SEAT TRACK IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED, REPLACED SEAT TRACK IAW DWG 9753289 AND SRM 51-3-0.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE, C2, 3, STA 270 LBL 48 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE C2, 3, STA 1580 RBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SEAT TRACK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE, C2, 3, STA 280 AT LONG 33R INTERCOSTAL, FRAME, AND INTERCOSTAL ATTACH FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTINGS. REPAIRED FRAME AND INTERCOSTAL.

Part: SHEAR TIE — CRACKED (FWD CARGO BAY) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3, STA 360 SHEAR TIE IS CRACKED BETWEEN LONG 31L TO 32L. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE C2, 3, STA 415 LOWER FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE, C2, 3, STA 345 LONG 27L AND BATHTUB FITTING ARE CORRODED BEYOND LIMITS. REPAIRED LONGERON AND REPLACED BATHTUB FITTINGS.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIBS ARE CRACKED AT XFS 647.5, 672.5, 685, AND 697.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2/3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 310.25 AND XFS 335.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 816.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE C2, 3, STA -60 CUSP TO FRAME TFITTING IS CORRODED BEYOND LIMITS AT LBL 60. REMOVED, FABRICATED, AND REPLACED FITTING.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 747.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 785. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2/3, LEFT WING CENTER L/E LOWER RIB IS CRACKED AT XW 461.372. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 597.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XS 491.193, XS 503.789. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (LT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 728.75 AND XFS 747.5. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 811-335.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3 VERTICAL STAB LT SKATE ANGLE IS CORRODED BEYOND LIMITS AT STA 1766. REPAIRED ANGLE IAW SRM 53-2-5 FIG 16A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2,3 STA 950 LOWER KEEL BETWEEN GEAR DOORS DOOR SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 4645535, AND SRM 51-1-20D.

Part: SKIN — CORRODED (LT WING) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 591.25 AND XFS 597.5. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 811-336.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1766 AFT OF BULKHEAD LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,097 hrs · 25,230 cycles

INSPECTION TYPE:C2, 3, STA 1766 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:C, EMERGENCY EXIT LIGHTS DO NOT COME ON WITH BISE CHECK. REPLACED BATTERY PACK, OPS CK PER PREDEPARTURE CK OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACKS, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK OK

Part: GIRT BAR — DAMAGED (CABIN)

EVAC SLIDE GIRT BAR WOULD NOT ENGAGE IN FLOOR LOCKS. REMOVED SLIDE AND DEFERRED PER MEL.

Part: INDICATOR — FAILED (EADI)

AT CRUISE ALTITUDE, SMOKE IN THE COCKPIT:F/O EADI WENT BLANK, FOLLOWED BY SMOKE FROM UNDER THE GLARESHIELD. PULLED THE ATT REF Z(F/O)CB AND RT EFIS MASTER. SMOKE PERSISTED INTERMITTENTLY. EMERGENCY DESCENT TO AIA. FOUND THE F/O EADI SHORTED OUT. REMOVED AND REPLACD THE F/O EADI IND OPS SYS PER MM 34-23-01. OPS GOOD. RAN ALL ENG'S AND PACKS OPS GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. CHARGED BATTERY, OPS OK.

Part: BATTERY PACK — DEAD (RADIO RACK)

EMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHT SWITCH LEFT ON TURNED SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 1700)

INSPECTION TYPE-C1, STA 1700 FLOORBEAM IS CORRODED OUT OF LIMITS AT LBL 24. REPAIRED AREA IAW DHC SK 811-528.

Part: FLOORBEAM — CORRODED (BS 1700)

INSPECTION TYPE-C1, STA 1700 AT RBL 24, THE FLOORBEAM FLANGE HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 811-080.

Part: FITTING — CRACKED (BS 1228)

INSPECTION TYPE-C1, STA 1228 AT STR 29R TO 33R, THE SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1260-1280)

INSPECTION TYPE-C1, LONGERON 34L BTWEEN STA 1260 TO 1280 IS CRACKED. REPAIRED AREA IAW DHC SK 811-775.

Part: FRAME — CORRODED (BS 1700)

INSPECTION TYPE-C1, STA 1700 FRAME AT STR 36 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: DOUBLER — CRACKED (NR 2 FUEL TANK)

INSPECTION TYPE-C1, NR 2 MAIN TANK I/B AFT ACCESS PANEL INTERNAL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-2 FIG 36.

Part: LONGERON — CORRODED (BS 500)

INSPECTION TYPE-C1, LONGERON 31L AT STA 500 HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 811-817.

Part: SEAT TRACK — CORRODED (BS 55-70)

INSPECTION TYPE-C1, FS 55 TO 70, RBL 45, THE DOUBLE TRACK IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FS 55 TO 130, RBL 45 IAW SRM 51-1-3.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE-C1, FS 759, RBL 24, THE FLOORBEAM SPLICE/ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 903)

INSPECTION TYPE-C1, FS 903, LBL 68, THE CUSP SPLICE FITTING HAS HEAVY EXFOLIATION CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 575.75)

INSPECTION TYPE-C1, LT WING L/E RIB AT FS 575.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE-C1, FS 920, RBL 68, THE VERTICAL FITTING HAS A 6 INCH CRACK. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 960)

INSPECTION TYPE-C1, FS 960 AT BL 0, THE VERTICAL FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE-C1, STA 1220 AT STR 32L, THE STR END FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753569 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1691)

INSPECTION TYPE-C1, FS 1691 AT LONG 22R THE LONG END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 822.5)

INSPECTION TYPE-C1, FS 822.5 FLOORBEAM AT LBL 24, THE AFT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FRAME — CRACKED (BS 1680)

INSPECTION TYPE-C1, STA 1680 AT STR 21L, THE FRAME HAS A 2.5 INCH CRACK. REMOVED, FABRICATED AND REPLACED FRAME IAW DWG 5640243 AND SRM 51 1-20D.

Part: FITTING — CRACKED (BS 71)

INSPECTION TYPE-C1, LONGERON END FITTING AT FS 71, AND LONG 32R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-C1, LT WING RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 761)

INSPECTION TYPE-C1, LT WING L/E SKIN AT XW 761, IS CRACKED BETWEEN 2 FASTENERS. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (WS 711)

INSPECTION TYPE-C1, LT WING L/E SKIN AT FS 711 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1, FIG 24.

Part: WEB — CRACKED (LT TE FLAP)

INSPECTION TYPE-C1, LEFT I/B FLAP, I/B WEB IS CRACKED AT THE AFT LWR CORNER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 75)

INSPECTION TYPE-C1, LT WING UPPER SKIN AT XRS 75, JUST FWD OF THE CENTER SPAR IS CRACKED. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1, FIG 10.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C1, THE INTERCOSTAL END FITTING AT LONG 19L AND 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C1, THE EXTERNAL REPAIR DOUBLER AT THE NR 1 PYLON CUTOUT IS CRACKED AND THE SKIN IS CRACKED PAST THE STOP DRILL HOLE. REMOVED OLD REPAIR DOUBLER, STOP DRILLED CRACK AND FABRICATED A NEW REPAIR DOUBLER AND INSTALLED IAW SRM 57-2-1.

Part: DOUBLER — CRACKED (WS 6.225)

INSPECTION TYPE-C1, RT WING L/E LWR INTERNAL DOUBLER, JUST O/B OF THE XOLDI 6.225 RIB IS CRACKED AT THE T/E. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5669891 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 240)

INSPECTION TYPE-C1, LONG 25R END FITTING AT FS 240 HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (BS 80-120)

INSPECTION TYPE-C1, LONG 31R FINGER DOUBLER FROM FS 80 TO 120 IS CRACKED AND PULLING LOOSE. REMOVED, FABRICATED AND REPLACED THE FINGER DOUBLER IAW DWG 5779934 AND SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (WS 560)

INSPECTION TYPE-C1, RT WING UPPER L/E SKIN AT FS 560.0 IS CRACKED BETWEEN 2 FASTENERS. THE CRACK TERMINATES AT THE FASTENER HOLES. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 711)

INSPECTION TYPE-C1, RT WING L/E AT FS 711.0, THE SKIN HAS A CRACK AT 1 SCREW COUNTERSINK. STOP DRILLED THE CRACK AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 710)

INSPECTION TYPE-C1, LT WING L/E SKIN AT FS 710.0 IS CRACKED BETWEEN FASTENERS. STOP DRILLED THE CRACK AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 772.5)

INSPECTION TYPE-C1, RT WING L/E AT XFS 772.5, THE SKIN IS CRACKED BETWEEN 2 FASTENER HOLES. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP ON BISE CHECK. REMOVED AND REPLACED BATTERY PACK, OPS CK GOOD PER M/M 33-50-00.

Part: BATTERIES — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, DURING BIT TEST EMERG LIGHTS AND OTHER LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY, OPS CKS GOOD PER MM 33-50-0 OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT IS INOP AT ENTER DOOR. RELAMPED, OPS CK'ED W/REF TO 33-50-00.

Part: ANGLE — CRACKED (BS 640)

DURING C CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED F/S 640 BETWEEN LONGERON 26 AND 27 RT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE, DRILLED, PRIMED AND INSTALLED NEW ANGLE IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21

Part: FITTING — CRACKED (BS 350)

DURING C-CHECK INSPECTION, FOUND FITTING CRACKED AT LONG 36 FS 350. REMOVED CRACKED FITTING, CUT NEW FITTING, FABRICATED SPLICES, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D.

Part: ANGLE — CRACKED (BS 640)

DURING C-CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED FS 640 BETWEEN LONGERON 26 AND 27 LT. REMOVED CRACKED ANGLE, FABRICATED NEW REPAIR ANGLE IAW DC8 SRM 53-2-0, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D AND 53-2-0.

Part: SKIN — CRACKED (LT TE FLAP)

DURING C CHECK INSPECTION, FOUND TWO CRACKS AT EDGE OF FLAP SKIN OTBD OF EXHAUST GATE LT WING APPROX STA XRS 325. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1 FIG 20 PG 25, 51-1-8, 51-1-21.

Part: FITTING — CRACKED (BS 940)

DURING C-CHECK INSPECTION, FOUND FRAME FITTING CRACKED AND CORRODED FS 940 ABOVE LONGERON 24 RT. REMOVED DAMAGED FITTING, CUT NEW FITTING, DRILLED NEW FITTING, SPLICES AND INSTALLED IAW DC8 SRM 53-2-0 FIG 8, 51-1-8, 51-1-21, 51-1-20D.

Part: ANGLE — CORRODED (BS 781.5)

DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM ATTACH ANGLE CORRODED STA 781.5 AT BL 68 LT. REMOVED FLOOR SUPPORT BEAM LOWER ATTACH ANGLE, DRILLED NEW ATTACH ANGLE AND INSTALLED IAW DC8 SRM 53-2-0 PG 1 PAR 3, 51-1-20, 51-1-8.

Part: STIFFENER — CRACKED (BS 940)

DURING C CHECK INSPECTION, FOUND STIFFENER CRACKED OUTBOARD SIDE OF RT MAIN WHEEL WELL FWD OF FLAP DRUM AT STA 940. REMOVED CRACKED STIFFENER, FABRICATED NEW STIFFENER, DRILLED, TREAT, PRIMED AND INSTALLED NEW STIFFENER IAW DC8 SRM 53-2-0, 51-1-21.

Part: FITTING — CRACKED (RT WING)

DURING C CHECK INSPECTION, FOUND RT WING OTBD FLAP STA XF 408 (INBD) FLAP HINGE SUPPORT FITTING CRACKED. CRACK IS OUT OF SRM LIMITS. REMOVED SUPPORT FITTING AT STA 408, LOCATED, DRILLED AND INSTALLED NEW SUPPORT FITTING IAW DC8 SRM 57-1-0, 51-3-0.

Part: TAIL CONE — CRACKED (TAIL CONE)

INSPECTION TYPE DLY, 6 TO 8 INCH CRACK IN TAIL CONE BEHIND LEFT ELEVATOR. REPAIRED CRACK IN TAIL CONE PER EO DC-8-5350-7876-A.

Part: SKIN — CORRODED (LT HORIZ STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB L/E SKIN AT ATTACHING SCREW HOLES HAS HEAVY CORROSION AT STA XFS 125 AND XFS 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1.

Part: FITTING — CORRODED (LT HORIZ STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB FITTING HAS CORROSION DAMAGE AT NR 4 STR, STA XFS 135 BOTTOM INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D.

Part: BOLTS — CORRODED (FS 145-255)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01.

Part: BLKHD DOUBLER — CORRODED (FS 980)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD.

Part: DOUBLER — CORRODED (FS 50-67)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FINGER DOUBLER FS 50 TO 67 LONGERON 21L. REPLACED FINGER DOUBLER PER SRM 51-1-21.

Part: FITTING — CORRODED (FS 145)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR JAMB HAS HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0.

Part: DOUBLER — CORRODED (FS 8-80)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER FROM FS 08 TO 80 HAS CORROSION OUT OF LIMITS, RBL 40. REPLACED DOUBLER PER SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 32-52)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER AT FS 32 TO 52, RBL 15 HAS HEAVY CORROSION. REPLACED DOUBLER ON TASK CARD 424338.

Part: FLOOR BEAM — CORRODED (FS 12)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 12 RBL 50. REPAIRED PER UPS EO DC8-53-1582.

Part: FITTING — CORRODED (FS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON END FITTING HEAVY CORROSION AT FS 70, LONGERON 30R. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, FS 70, LONGERON 28R, CORROSION BEYOND LIMITS. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1350)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31L CRACKED AT FS 1350. REPAIRED PER UPS EO DC8-53-1600.

Part: FITTING — CRACKED (BS 100 R)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON END FITTING AT LONGERON 27R, FS 100, HEAVY CORROSION AND CRACKED. REPLACED FITTING PER SRM 51-1-21.

Part: SPAR — CRACKED (LT WING)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED NR 2 PYLON AREA WING FRONT SPAR AT STR 69, STRAP HAS A .50 INCH LONG CRACK. REPAIRED PER UPS E.O. DC8-57-0648.

Part: WEB — CORRODED (FS 1210)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON DOOR WEB FS 1210 I/B SIDE OF LONG 33R. REPLACED WEB PER SRM 53-2-0.

Part: STIFFENER — CRACKED (FS 1737)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT STIFFENER TO BOLT FRAME STA 1737 CRACKED LONGERON 22R. REPLACED STIFFENER PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 1140)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 1140 BOLT FRAME FWD LOWER FLANGE, LONGERON 36 TO 35L.

Part: FLOOR BEAM — CORRODED (FS 55)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 55 RBL 50. REPAIRED PER UPS EO DC8-53-1583.

Part: FITTING — CRACKED (FS 759)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL ATTACH FITTING IS CRACKED AT FS 759 RBL 48. REPLACED FITTING PER SRM 51-1-21.

Part: FLOOR BEAM — CORRODED (FS 35)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 35 RBL 50. REPAIRED PER UPS EO DC8-53-1586.

Part: WEB — CRACKED (FS 55)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CABIN SUBFLOOR WEB HAS A 4 INCH CRACK AT FS 55 LBL 6. REPLACED WEB SECTION PER SRM 51-1-21.

Part: FITTING — CRACKED (FS 680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM SUPPORT FITTING IS CRACKED AT FS 689 RBL 26. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ENTRY DOOR LOWER FWD CORNER FUSELAGE SKIN CUTOUT AND DOUBLER HAVE A 4 INCH LONG CRACK. REPAIRED PER UPS EO.

Part: FRAME — CORRODED (FS 1060)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME UPPER FLANGE HEAVY CORROSION AT FS 1060 ABOVE LONG 36. REPAIRED FRAME PER SRM 53-4-1 AND 53-2-1.

Part: FITTING — CORRODED (FS 1220)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING, FS 1220 LONGERON 33R. REPLACED FITTING PER SRM 53-2-0.

Part: DOUBLER — CORRODED (FS 25-90)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED COCKPIT SUBFLOOR DOUBLER AT FS 25 TO 90 HAS CORROSION DAMAGE LONGERON 22R. REPAIRED PER UPS EO DC8-5310-8040-A.

Part: LONGERON — CORRODED (FS 1270)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 31L, FS 1270. REPAIRED PER UPS EO DC8-53-1574.

Part: DOUBLER — CORRODED (FS 930)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 6 SHEARED FASTENERS DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER, FS 930 BL 0. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 912)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 1 SHEARED FASTENER DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER FS 912 RBL 1. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CORRODED (FS 1200)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING, FS 1200 LONGERON 23R. REPLACED FITTING PER SRM 53-2-0.

Part: SHEARTIE — CRACKED (BS 55)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEARTIE CRACKED AT F.S. 55, BETWEEN LONGERONS 28L-30L. REPLACED SHEARTIE SECTION PER SRM 53-2-0.

Part: BLKHD LWR CAP — CRACKED (NR 3 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 3 PYLON I/B SUPPORT BULKHEAD FWD LOWER CAP HAS A 17 INCH LONG CRACK. REPAIRED PER UPS EO DC8-57-0647.

Part: DOUBLER — CORRODED (FS 875)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 2 SHEARED FASTENERS DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER FS 875 LBL 1. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 90)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED COCKPIT SUBFLOOR DOUBLER AT FS 90 HAS CORROSION DAMAGE RBL 35. REPAIRED PER UPS EO DC8-5310-8040-A.

Part: SHEARTIE — CRACKED (BS 35)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEARTIE CRACKED AT F.S. 35 BETWEEN LONGERONS 28L-30L. REPLACED SHEARTIE SECTION PER SRM 51-1-20D.

Part: SKIN — CORRODED (FS 1395-1445)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EXTERNAL SKIN FS 1395 TO 1445, LONGERON 33R TO 35L HAS MODERATE CORROSION UNDER SCUFF PLATE. REPLACED SKIN SECTON PER SRM 51-1-21, AND 51-1-20D.

Part: LONGERON — CORRODED (BS 50-150)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 80-150, LONGERONS 28R, HEAVY CORROSION AROUND FASTENER HOLES. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 360)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION AT FRAME FITTING, LONGERON 21R FS 360. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 445)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 21L, FS 445. REPAIRED PER UPS EO DC8-53-1574.

Part: SHEAR TIE — CORRODED (BS 100)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON SHEAR TIE BOLT FRAME STA 100 LONGERON 21R. REPLACED SHEAR TIE PER SRM 51-1-20D.

Part: ANGLE — CORRODED (FS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CHORD ANGLE AT FS 70 BETWEEN LONGERONS 31R TO 32R. WILL BE REPAIRED ON TASK CARD NR 423121 PENDING APPROVAL.

Part: LONGERON — CORRODED (BS 1735)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 26R, FS 1735. REPAIRED PER UPS E.O.

Part: FLOOR BEAM — CORRODED (BS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FLOOR BEAM, FS 1680, RBL 35. REPAIRED PER UPS E.O. DC8-53-1588.

Part: DOUBLER — CORRODED (FS 1350)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON DOUBLER O/B OF LONG FS 1350. REPLACED DOUBLER SECTION PER SRM 51-1-21.

Part: ANGLE — CORRODED (FS 1340)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ANGLE AT LONGERON 31L, FS 1340. REPLACED ANGLE PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 1400-1420)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 34R, FS 1400 TO 1420 AT FRAME. REPLACED FRAME SECTION PER SRM 51-1-20D.

Part: SUPPORT — CRACKED (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME SUPPORT ANGLE CRACKED AT F.S. 80, LONGERON 33R. REPAIRED PER UPS EO.

Part: FITTING — CORRODED (FS 1260-1280)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION AND CRACK AT FITTING, FS 1260 TO 1280, LONGERON 33R. REPLACED FITTING PER SRM 51-1-8 AND 51-1-20D.

Part: ANGLE — CRACKED (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME SUPPORT ANGLE CRACKED AT F.S. 80, LONGERON 33L. REPAIRED ANGLE PER DPS 10.225.

Part: SKIN — CRACKED (FS 120)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR FWD UPPER CORNER OF CUTOUT HAS CRACKED FUSELAGE SKIN. REPAIRED PER UPS EO DC8-5330-7812A.

Part: FRAME — CORRODED (FS 180)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 180, FWD SIDE OF BOLT FRAME, LONGERON 33R AND 33L. REPAIRED PER SRM 53-2-0 FIG 2.

Part: FITTING — CORRODED (FS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 27R, END FITTING AFT SIDE OF FS 70. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CORRODED (FS 1766)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EXTERIOR FUSELAGE SKIN HEAVY CORROSION AT FS 1766, LONG 28R. REPAIRED PER UPS EO DC8-53-1571.

Part: ANGLE — CORRODED (BS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CHORD ANGLE, FS 70, BETWEEN LONGERONS 29R-30R. WILL BE REPAIRED ON TASK CARD 423121.

Part: SHEAR TIE — CORRODED (FS 1140)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME SHEAR TIE, FS 1140 LONG 36. REPLACED SHEAR TIE PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 1060)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME FS 1060, LONG 36. REPLACED FRAME UPPER SECTION PER SRM 51-1-20D PER SRM 53-2-0.

Part: ANGLE — CORRODED (BS 980-1000)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION FS 980-1000, SUPPORT ANGLE AT LONGERON 27R INBOARD AND OUTBOARD SURFACES. REPLACED ANGLE PER SRM 51-3-0.

Part: WEB — CORRODED (BS 1260-1280)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED RT TUNNEL WEB HAS MODERATE CORROSION AT FS 1260-1280 INBOARD OF LONGERON 21R. REPAIRED WEB PER SRM 53-2-0, FIG 1D.

Part: GUSSET — CORRODED (BS 180)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AT BAY BIN RT TUNNEL, FS 180, GUSSET HAS HEAVY CORROSION BETWEEN VERTICAL BRACE. REPLACED GUSSET PER SRM 51-20D.

Part: GUSSET — CORRODED (BS 100)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, A BAY BIN RT TUNNEL, FS 100, VERTICAL SUPPORT GUSSET HAS HEAVY CORROSION. REPLACED GUSSET PER SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FS 1080)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1080 SHEAR TIE STRAP SHEARED ABOVE LONG 31L. REPLACED SHEAR TIE PER SRM 51-1-4 AND 51-1-8B.

Part: LONGERON — CORRODED (FS 100-120)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 30R, HEAVY CORROSION FS 100 TO 120. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 70 BOLT FRAME AFT SIDE ON LONGERON 29R TO 26R. REPAIRED PER UPS EO DC8-53-1591.

Part: ANGLE — CORRODED (FS 120)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME ANGLE AT FS 120, LONG 27R, HEAVY CORROSION. REPLACED ANGLE PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 520)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONG 36, FS 520 BOLT FRAME. REPLACED FRAME PER SRM 53-2-0.

Part: ATTACH ANGLE — CRACKED (FS 1766)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS A 1 INCH CRACK ON AFT END. REPAIRED PER UPS EO.

Part: ANGLE — CORROSION (VERT STAB)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON VERTICAL STABILIZER TO FUSELAGE RT ATTACH ANGLE. REPAIRED ANGLE PER SRM 53-2-5, FIG. 16A.

Part: DOUBLER — CRACKED (BS 67)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUSELAGE SKIN DOUBLER CRACKED AT LOWER FORWARD CORNER OF LT PRIMARY HEAT EXCHANGER. REPAIRED PER UPS E.O.

Part: DOUBLER — CRACKED (FS 67)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUSELAGE SEAM DOUBLER CRACKED LOWER FWD CORNER OF RT PRIMARY HEAT EXCHANGER. REPAIRED PER UPS EO.

Part: CONTROL TAB — DELAMINATED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LEFT I/B AILERON CONTROL TAB DELAMINATED I/B AFT EDGE, TOP AND BOTTOM SIDE. REPLACED TAB PER MM 27-13-01.

Part: DOUBLER — CORRODED (BS 50-70)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BULGE UNDER LAV. SERVICE DR. REPLACED DOUBLER PER SRM 51-1-21.

Part: SKIN — CRACKED (FS 21.92)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 2 CRACK'S IN FUSELAGE SKIN, FS 21.92 LONGERONS 31 LT AND RT. REPAIRED SKIN PER UPS EO.

Part: SKIN — DELAMINATED (LT SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING SPOILER DELAMINATED TOP AFT O/B EDGE. REPLACED SPOILER ASSY REP MM 27-61-01.

Part: SKIN — CORRODED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SKIN BULGED AROUND AIR CONDITIONING DR. CUTOUTS LONGERON CORNERS. REPLACED DOUBLER PER SRM 51-1-20D AND SRM 51-1-21.

Part: SKIN — CORRODED (RT TE SLAT)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B SLAT UPPER SURFACE PITTED AND MODERATE CORROSION. REPLACED SLAT PANEL PER SRM 51-3-0.

Part: UPLATCH LIGHT — DEFECTIVE (LANDING GEAR)

CREW REPORTED DURING UPLATCH CHECK OBTAINED GEAR NOT LATCHED LIGHT. PERFORMED CHECKLIST AND CONTINUED FLIGHT. ACCOMPLISHED E.O. DC8-3230-7910, A/C O.K. TO CONTINUE PER D-105486 BY MMOC FOR ONE FLIGHT ONLY TO SDF.

Part: SLIDE — LOW PRESSURE (ESCAPE SLIDE)

MAINT REPORTED, ESCAPE SLIDE PRESSURE BELOW LIMITS AND DUE 12/95. REMOVED AND REPLACED SLIDE PER M/M 25-60-01, CHECKS OK.

Part: AIR DISRT — ODOR (COCKPIT)

WHILE ON GROUND, CREW REPORTED STRONG SMOKE SMELL IN COCKPIT AFTER SELECTING GROUND POWER. FOUND PACK SWITCH IN THE ON POS W/O AIR FLOW. CYCLED POWER NUMEROUS TIMES, NO UNUSUAL ODORS IN FLIGHT DECK.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD. THE OFF AND ON (P/N 5708458-503), S/N ON FTL 182 AND S/N ON FTL 231.

Part: EEL METER — MALFUNCTIONED (CABIN)

WHILE ON THE GROUND, MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY PACK METER SHOWING ON, WHEN EMERGENCY LIGHTS WERE OFF. A/C BATTERY PACK METER NEEDS TO BE DEACTIVATED AND PLACARDED. MAINTENANCE DEACTIVED THE METER PER WDM 33-50-01, OK TO CONTINUE SERVICE. INSTALLED DEACTIVED STICKER PER 34-21-04, EFIS WDM FOR FURTHER INFO.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMER EXIT LIGHTS INOP ON PREFLIGHT. REMOVED AND REPLACED EMER BATTERY PACK.