N809UP

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY LIGHTS STAY ON IN THE ARMED POSITION. FOUND EMERGENCY EXIT LIGHT CONTROL C/B OPENED, RE-SET C/B AND PERFORMED EMERGENCY LIGHTING OPS TEST PER AMM 33-50-01-2. OPS CHECK GOOD.

Part: BATTERY — MALFUNCTIONED (FIRE DETECTORS)

DURING FINAL APPROACH LOW CARGO COMPT FIRE LIGHT CAME ON AS SOON AS PACKS WERE TURNED OFF IT WENT AWAY. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYS T/S MM 26-18-00-1. REMOVED AND REPLACED BATTERIES ON DETECTORS FA1326, AC3305, AD6652, AD7666 SYS OK LIGHT INDICATED.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01.

Part: SPAR — CRACKED (CENTER TANK) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 POSSIBLE CRACK ON LOWER SURFACE SKIN AFT CTR SPAR RT CTR AUX TANK. NDT VERIFIED 2 INCH CRACK AT RT CTR AUX TANK AFT CTR SPAR. REMOVED CRACKED SECTION OF CTR SPAR, FABRICATED REPLACEMENT SECTION OF CTR SPAR AND REPAIR PARTS, AND INSTALLED IAW SAA SK 809-851262.

Part: PRESSURE PANEL — CORRODED (FS -67 RBL 60) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 FOUND EXFOLIATION CORROSION AND CRACKS ON COCK PIT SUBFLOOR AT STA -67 RBL 60 INSIDE RIGHT NOSE TUNNEL. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DWG SRO8530 026 AND DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS1230 L34-35R) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 -C- PIT STA 1230 BETWEEN L34R TO L35R FITTING CRACKED AROUND FASTENERS . REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SR M 51-1-20D.

Part: FITTING — CRACKED (FS 1240 L35R) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 -C- PIT STA 1240 L35R FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS1180 L27L) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 -C- PIT CROSS SLIDE DOOR BANANA FITTING CRACKED AT BUMPER STOPS AT L27L STA 1180. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CORRODED (FS1200 L29L-L28L) · airframe 77,280 hrs · 27,172 cycles

"C" PIT BATHTUB FITTING CORRODED AT STA 1200 BETWEEN L29L AND L28L. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D.

Part: SEAL — CORRODED (STA 20 RBL 60) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 HEAVY CORROSION AROUND EXTERNAL POWER CABLE PRESSURE SEAL BELOW EPC RA CK STA 20 RBL 60. REMOVED, FABRICATED, AND INSTALLED PRESSURE SEAL DOUBLER IAW DWG 56122 78 AND DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS 348 L31R) · airframe 77,280 hrs · 27,172 cycles

A PIT STA 348 L31R ZEE FITTING CRACKED 3 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: STIFFENER — CORRODED (FS -109 LBL36) · airframe 77,280 hrs · 27,172 cycles

HEAVY CORROSION ON BASE OF DIAGONAL STIFFENER IN COCKPIT SUB FLOOR BELOW PILOTS LT RUDDER PEDAL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT GUSSET IAW DWG 5597992 AND SRM 51-1-20D.

Part: FITTING — CRACKED (STA 280 L29R) · airframe 77,280 hrs · 27,172 cycles

"A" PIT STA 280 L29R ZEE FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED "Z" FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS 834 L18R) · airframe 77,280 hrs · 27,172 cycles

MAIN CABIN STA 834 L18R FRAME TO INTERCOSTAL FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FRAME — CRACKED (FS 1700 L20L) · airframe 77,280 hrs · 27,172 cycles

MAIN CABIN FRAME CRACKED 1" LONG AT STA 1700 L20L. TRIMMED OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5310 -11728-B AND DWG DC8-53A-011-A.

Part: FINGER DOUBLER — CORRODED (FS879-902 LBL65) · airframe 77,280 hrs · 27,172 cycles

CENTER WING BOX AT STA 879 TO 902 LBL 65 FINGER DOUBLER HAS SEVERAL SHEARED FASTENER HEADS AND HEAVY CORROSION UNDER THE FINGER DOUBLER. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. AREA UNDER FINGER DOUBLER FOUND IN LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-7-3 FIG 4 AND 51-1-20D.

Part: FITTING — CRACKED (FS 902 L5R) · airframe 77,280 hrs · 27,172 cycles

STA 902 L5R LONGERON FITTING CRACKED 2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FS 700 L18L) · airframe 77,280 hrs · 27,172 cycles

STA 700 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED APPROX 3" LONG. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (STA 310 L18L) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE: C1, MAIN CABIN LONGERON SPLICE FITTING HAS 4 INCH CRACK STA 310 L18L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SAA SK 809- 850545 AND UPS ENGINEERING FILE NUMBER DC8-53-20487.

Part: FITTING — CRACKED (FS 1160 L19R) · airframe 77,280 hrs · 27,172 cycles

STA 1160 L19R FITTING CRACKED 1" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1220 L20R) · airframe 77,280 hrs · 27,172 cycles

MAIN CABIN STA 1220 L20R FRAME ATTACH FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: SKIN — CRACKED (XCW 98) · airframe 77,280 hrs · 27,172 cycles

R/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10.

Part: SKIN — CRACKED (FS 1746 L15L) · airframe 77,280 hrs · 27,172 cycles

FUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15L. CUT OUT DAMAGED SECTION OF SKIN AT STA 1746 AND L15L. FABRICATED, AND IN STALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FS 1746 L15R) · airframe 77,280 hrs · 27,172 cycles

FUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15R. REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 77,280 hrs · 27,172 cycles

FE'S AFT SEAT TRACK STOP HOLES WORN AND HEAVY CORROSION AROUND COUNTER SUNK ATTACH SCREWS. REMOVED AND REPLACED FE'S AFT SEAT TRACK IAW DC-8 SRM 51-1-21, 51-3-2, AND 51-3-0.

Part: PRESSURE PANEL — CORRODED (BS 979 LBL 40) · airframe 77,280 hrs · 27,172 cycles

INSPECTION TYPE:C1 LEFT W/W SKIN HEAVILY CORRODED INSIDE HAT CHANNEL STA 979 LBL 40. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310 -22753-A AND SAA SK 809-850352.

Part: ENGINE — FLAMED OUT (NR 4)

NR 4 ENGINE FLAME OUT IN CRUISE FLT ENROUTE TO PHL. RESTART UNSUCCESSFUL. FUEL PRESSURE ON S/O PANEL DROPPED FROM 35 PSI TO 20 OIL TEMP & QTY NORMAL OIL PRESS DROPPED TO 18 PSI AFTER FLAMEOUT. R&R NR 4 ENGINE, MAIN ENGINE CONTROL (MEC) IAW MM 73-20-01-4. PERFORMED MEC ADJ AND TEST IAW 73-30-01-5. LEAK CK AND ENG RUN CHECK GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (ENTRY DOOR)

INSPECTION TYPE: N/A ONE EMERGENCY LIGHT INOPERATIVE AT CREW ENTRY DOOR. RELAMPED. OPS CK OKAY.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 260-280 IS CRACKED AT LONG. 33R REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG.5750726,AND SRM. 51-1-20D.

Part: WEB — CRACKED (RUDDER) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, WEB IN RUDDER LE AT FORWARD SPAR IS CRACKED AT XR 160 REMOVED WEB SECTION,FABRICATED AND INSTALLED REPLACEMENT WEB SECTION IAW SRM. 55-2-4 FIG. 1

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, STATION 55 BELTFRAME IS CRACKED AND CORRODED BETWEEN LONG. 35L TO 35R. REMOVED DAMAGED AREA,FABRICATED AND INSTALLED REPAIR J-ANGLES I.A.W. DC8-53A-011,AND SRM 51-1-20D

Part: FITTING — CRACKED (LOWER CARGO) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, STATION 300 LONG. 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3754041,SRM.53-2-0 FIG. 1B, DWG. 9751879.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, LONG. 32L SPLICE FITTING IS CRACKED AT STA. 610. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT LBL 26 AND 36, 67 ABOVE CABIN FLOOR CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLERS AND FILLERS I.A.W. DWG. SRO08530007

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, STATION 1240 LONG. 30R IS CRACKED REMOVED LONGERON SECTION STATION 1230-1250,FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-4-1 FIG.4,53-2-2 FIG. 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, FLOORBEAM FITTING IS CRACKED AT STA. 340 RBL. 58 REMOVED AND REPLACED FITTING IAW DWG. 9754022,AND SRM. 51-1-20D

Part: INTERCOSTAL — CRACKED (COCKPIT SUBFLOOR) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, COCKPIT SUBFLOOR INTERCOSTAL UPPER FLANGE IS CRACKED AT STA.-21 LBL 12. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 53-2-0 FIG. 1B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,467 hrs · 26,509 cycles

INSPECTION TYPE: C2, STATION 1320 LONGERON 31 RT AND FRAME ARE CORRODED BEYOND LIMITS, REMOVED,FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA. 1230 TO 1320 I.A.W. SRM. 53-4-1 FIG. 43A,AND REMOVED CORRODED AREA ON FRAME,FABRICATED AND INSTALLED FILLER AND DOUBLER I.A.W. SRM. 53-2-0 FIG.2

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, STA. 1720 AND 1740 LONG. 15R IS CRACKED AT FRAME ATTACH BOLTS. REMOVED DAMAGED LONGERON SECTION STA. 1720-1760, FABRICATED AND INSTALLED SECTION IAW SRM. 53-2-2 FIG. 10.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, AFT SIDE STATION 70 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONGERON 29L AND 30L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED ANGLE REPAIR AND DOUBLERS I.A.W. SRM. 53-2-5 FIG. 8C-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 80-100 AT LONGERON 28 RT IS CORRODED BEYOND LIMITS REMOVED,FABRICATED AND REPLACED INTERCOSTAL IAW SRM. 53-3-2 FIG. 5 AND 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT STA 1766 AT RBL 26 AND 36. CUTOUT DAMAGED AREAS AT RBL 26 AND 36,NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRO8530007.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, LONGERON 28R IS CORRODED BEYOND LIMITS AT SPLICE FITTING AT STA. 450. REMOVED,FABRICATED AND REPLACED LONGERON SECTIONS BETWEEN STA.430 AND 470,AND REPLACED LONGERON SPLICES I.A.W. SRM. 53-2-2 FIG.8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, FLOOR SUPPORT FITTING IS CRACKED AT STA. 120 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 5758571,AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, LONG. 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA. 1140 AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM. 51-1-20D.

Part: FRAME — CRACKED (AC BAY) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, BELT FRAME IC CRACKED AT STA. 55 LONG. 24L TO 25L CUTOUT DAMAGE, FABRICATED AND INSTALLED FILLER AND ANGLE DOUBLER I.A.W. SRM. 53-2-0 FIG. 2.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, LT HORIZONTAL STAB O/B TIP INTERNAL REAR SPAR ANGLE FITTING IS CRACKED AT XE 312.5 REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 5640789 AND SRM 51-1-20D,51-3-0,AND DWG. 4651609

Part: FITTING — CRACKED (SUBFLOOR) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 700 LBL. 24. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755222,AND SRM. 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT PRIMARY HEAT EXCHANGER CUTOUT HAS A CRACK ON SKIN AT LOWER AFT CORNER STATION -12 AT LONG. 27R. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-5330-4732-D APPX. A.

Part: SKIN — CRACKED (RT WING LE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT WING L/E SKIN IS CRACKED AT LOWER SURFACE XFS 304. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX C.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, 2 EACH CRACKED SEAT TRACK FITTINGS ,B-PIT CEILING STA. 420,RBL 24. REMOVED DAMAGED SEAT TRACK SECTION BETWEEN STA. 300 TO 490 RBL 24-31 FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM. 53-2-3 FIG. 8A,AND REPLACED FITTINGS IAW SRM. 53-2-3 FIG. 8A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, LEFT HORIZONTAL STAB. LE. RIB IS CRACKED AT XFS 47.5 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, 1 EA LIGHTNING STRIKE IS OUT OF LIMITS AT STA -95 4 INCHES ABOVE LONG 20L. 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 — NICKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, DEEP NICKS ON FUSELAGE SKIN AT STATION 520 LONGERON 25R, BLENDED OUT NICKS, FOUND OUT OF LIMITS, NDT VERIFIED NO CRACKS AT BLENDOUT AREAS. FABRICATED AND INSTALLED REPAIR DOUBLERS AT B-PIT UPPER FORWARD DOOR CORNER I.A.W. SRM. 53-2-0 FIG. 20,53-2-0 FIG. 1F.

Part: RIB — CRACKED (RIGHT WING LE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT STAB LE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT HORIZONTAL STAB. LEADING EDGE RIB IS CRACKED AT XFS 116.25 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2

Part: SKIN — CORRODED (RT WING LE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, RT WING LE UPPER SURFACE HAS 6 CRACKED FASTENER HOLES BETWEEN XFS 597.5 TO XFS 628.75. BLENDED OUT CORRODED AREAS, CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLER AND FILLERS I.A.W SRM. 57-2-1 FIG. 3B,57-3-0 FIG. 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,467 hrs · 26,519 cycles

INSPECTION TYPE: C2, WHILE ACCOMPLISHING WORK TASK AND REMOVAL OF SHUTTER BOX ON NR 687218. FOUND LOWER AFT SKIN CUT OUT CRACKED. C/W EO DC-8-5330-4732D, HFEC IAW NDBDM 06-10-01.0001, NO CRACKS AROUND CUT OUT,FABBED FILLER AND DOUBLER FROM 2024T3 .100 TREATED AND PRIMED PARTS AND SKIN, INSTALLED COUNTERSINK WASHERS IAW EO DC8 5330-4732D,INSTALLED REPAIR PARTS IAW EO DC8-5330-4732D.

Part: DOOR — CRACKED (AIR START)

LT FUSELAGE SECONDARY AIR START DOOR CRACKED. REPAIRED PER EO DC8-5330-18680-A

Part: ENGINE — FLAMED OUT (NR 2)

INSPECTION TYPE:N/A NR 2 ENG FLAMEOUT ON DESCENT ANTI-ICE 'ON' ING OVERRIDE FLT 15000 - 16000 FT. T/S PER 71-00-00 CFM MANUAL, COMPLIED WITH ALL STEPS FOR ENG FLAME-OUT PER MM 71-00-00 PG 101, 102 & 103. NO DEFECTS NOTED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26L-27L. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A AND 2B.

Part: SKIN — CRACKED (T/E FLAP) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RT EXHAUST GATE IS CRACKED AT IB T/E. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA -99 LT CUSP STIFFENER IS CORRODED BEYOND LIMITS. REPAIRED STIFFENER IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 742 RBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND DWG 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1770 LONG 17L IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649327, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1770 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D, AND 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG S1616757, AND SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1770 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397, AND SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 798 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 60. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 809-212.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 822 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1260-1280 LONG 35R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-818.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 680-700 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG4750521, AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 797.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 320 BANANA FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED FITTING IAW DWG 3754041, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 680-700 LONG 7L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1260-1280 LONG 34R IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 809-819.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 822 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LT WING FUEL PANEL 505F INTERNAL DOUBLER IS CRACKED AT XRS 12 AT STRINGER 5-6 AREA ON WING. REPAIRED DOUBLER IAW SRM 57-2-1 FIG 36.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 680 WING BOX TO FRAME SUPPORT FITTING IS CRACKED BELOW LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 3642974, AND SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1735 LONG 15L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.

Part: PAN — CORRODED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RT WING IB SLOT PAN HAS INTERGRANULAR CORROSION AT XS 250. REMOVED AND REPLACED PAN IAW DWG 5769859, AND SRM 51-1-21, 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 680-700 LONG 8L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 660-680 LONG 11L END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 440-460 LONG 17L, SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3887799, AND SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 35 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RT WING L/E UPPER RIB CAP IS CRACKED AT XS 467. REMOVED,FABRICATED,AND REPLACED RIB CAP IAW SRM 57-3-3 FIG 4, 51-1-21, 51-1-20D, 57-1-0.

Part: SKIN — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER SKIN IS CRACKED AT XFS 841.25. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 603. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING OB SLOT VANE INTERNAL DOUBLER IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769933, AND SRM 51-1-21,51-1-21A.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 791.25,XFS 797.5, XFS 803.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1710 RBL 10, MAIN CABIN FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT IAW DWG 5755032.

Part: SKIN — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 329. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING CENTER L/E. UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED 2 PLACES AT XW 485. REPAIRED SKIN IAW DC8-5720-7767-A, AND SRM 57-2-1 FIG 2H.

Part: SKIN — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 710. REPAIRED SKIN IAW DC8-5720-7767-A.

Part: DOUBLER — BROKEN (RT WING SPAR) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING LOWER FRONT SPAR HAS DOUBLER BROKEN AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14A, AND DWG 5802736.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LT HORIZ STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RT HORIZ STAB L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E NR 3 STUBWING LOWER DOUBLER IS CRACKED AT OPENING ABOVE PYLON CUTOUT. REMOVED, FABRICATED, AND REPLACED REPAIR DOUBLER IAW SRM 57-2-1A.

Part: SKIN — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED AT XFS 878. REPAIRED SKIN IAW SRM 57-2-1 FIG 2B.

Part: RIB — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 615. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 410.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 STA 1160 LONG 19R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT 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: SPAR CAP — CRACKED (RT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT WING REAR SPAR LOWER CAP IS CRACKED AT XCW 0. REPAIRED SPAR IAW 8110-3 APPROVED DK SK 809-649.

Part: RIB — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XRS 162. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 RIGHT MLG WHEEL WELL IB. BULKHEAD SUPPORT WEB IS CRACKED STA 879 RBL 4. REPAIRED WEB IAW SRM 53-2-0 FIG 1B.

Part: SKIN — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 635. REPAIRED SKIN IAW DC8-5720-4087-B.

Part: SKIN — DAMAGED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E UPPER SKIN HAS SCREWS PULLING THRU SKIN AT XFS 883. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: FITTING — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING T/E SUPPORT FITTING IS CRACKED OUTBOARD SIDE OF FLAP HINGE 410 CANOE FITTING. REMOVED AND REPLACED FITTING IAW DWG 4649597, AND SRM 51-1-20D, 51-3-0.

Part: SKIN — CRACKED (LT WING) · airframe 75,309 hrs · 25,673 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E. LOWER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW DC8-5720-4087-B.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT DISARM LIGHT DID NOT COME ON WHEN TURNED OFF. RELAMPED OP CHECK GOOD PER DC8 MM 33-50-02

Part: STOP FITTING — MISSING (EMERGENCY EXIT)

INSPECTION TYPE:PFLT BOTH OVERWING EXIT DOORS MISSING STOP FITTING ASSY/WILL NOT LATCH RESEATED IN SILL AND LATCHED INTO PLACE. M/M 52-20-00

Part: LIFE VEST — TORN (CABIN)

INSPECTION TYPE:PFLT, 2ND COURIER SEAT LIFE VEST BAG TORN. INSTALLED NEW LIFE VEST.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT BATTERY DEAD EMERGENCY LIGHT SWITCH INADVERTANTLY LEFT ON WITH A/C POWER OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS NORMAL.

Part: SWITCH — FAILED (MLG)

WHEN GEAR HANDLE SELECTED TO DOWN POSITION LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE. GEAR NOT LATCHED RED LIGHT ILLUMINATED. CYCLED GEAR WITHOUT IMPROVMENT, AFTER THIRD CYCLE 3 GEAR INDICATION, AND GEAR UNLATCHED LIGHT OUT. CYCLED GEAR, COULD NOT DUPLICATE PROBLEM. VISUALLY INSPECTED GEAR FOR DEFECTS, NONE FOUND. GREASED GEAR AND REPLACED DOWN LOCKSWITCH AS PRECAUTION.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK ASSY PER MM 33-50-01.

Part: SMOKE DETECTOR — INOP (CARGO COMP)

NR 6 CARGO SMOKE DETECTOR IS INOP. REPLACED NR 6 SMOKE DETECTOR TEST LAMP WITH PRO PER CM327AS15 LAMP TESTS GOOD.

Part: SMOKE DETECTOR — INOP (NR 6)

INSPECTION TYPE:N/A, NR 6 SMOKE DETECTOR WILL NOT TEST. DEFERRED IAW MEL 26-10-1, PLACARD INSTALLED.

Part: WEB — CRACKED (LT TE FLAP)

INSPECTION TYPE:C2, LT WING, I/B FLAP, I/B SIDE, CLOSE OUT WEB CRACKED SEVERAL PLACES. FABRICATED AND INSTALLED NEW WEB, DOUBLER AND STIFFENERS IAW REO 06611 AND DC8 SRM 51-1-21 & 51-1-14.

Part: SKIN — CORRODED (HORIZ STAB)

INSPECTION TYPE:C2, RT HORZ STAB O/B LEADING EDGE, I/B END, HAS CORROSION AROUND SCREW HOLES. FABBED AND INSTALLED REPAIR FILLED AND DOUBLER IAW DC8 SRM 51-1-21, 51-2 -0, & REO 06610.

Part: FLOOR — CORRODED (BS 1300)

INSPECTION TYPE:C-2 CORROSION ON MAIN CABIN FLOORBOARD SPLICES (3) STA 1040 X10 TO X17. FABRICATED AND INSTALLED NEW SPLICE IAW DC8 SRM 51-3-0. MAT ID 7075-T 6 .063 PO NR 289791 IAW DC8 SRM 53-7-3, DAC DWG 289791.

Part: FLOOR — CORRODED (BS 580-660)

INSPECTION TYPE:C3 FLOOR BOARD F88 TO F90 HAS LARGE DOUBLER BULBED BY CORROSION AND EX FOLIATION SHOWING ON UNDERSIDE OF PLANK FABBED AND INSTALLED NEW SECTION AND SPLICES IAW DC8 SRM 53-2-3 FIG 9 AND 51-3-0.

Part: SKIN — CRACKED (WS 889)

INSPECTION TYPE:C2, LEFT WING O/B LEADING EDGE, OUTBOARD END TOP SIDE SKIN IS CRACKED STA 889. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1 & 51-1-21.

Part: RIB — CRACKED (RUDDER)

INSPECTION TYPE:C2, LEADING EDGE RUDDER RIB CRACKED. FABRICATED AND INSTALLED NEW RIB IAW DC8 SRM 51-1-24, 51-1-22 & 51-1- 21.

Part: WEB — CRACKED (RUDDER)

INSPECTION TYPE:C2, RUDDER CTR DAMPER LOWER CLOSEOUT WEB WAS CRACKED. FABBED, INSTALLED AND HEAT TREATED NEW WEB IAW DAC DWG 5656229 AND DC 8 SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 680)

INSPECTION TYPE:C-2 FLOORBEAM CORRODED UNDERSIDE AT FS 680 BL 33L TO BL 36L. REPAIRED IAW REO-06602.

Part: SEAT TRACK — GOUGED (BS 255)

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK I IS GOUGED AT STA 255. FABRICATED AND INSTALLED PLUG AND CHANNEL IAW DC8 SRM 53-2-3 AND 51-3-0.

Part: SEAT TRACK — CORRODED (BS 270)

INSPECTION TYPE:C2, MAIN CABIN SEAT TRACK WAS GOUGED AND CORRODED AT STA 270. REMOVED AND INSTALLED NEW PLUG (P/N DC8 53B-007-004) IAW DC8 SRM 53-2- 3, UPS PARTS TAG NR 942460 (S/N 00290311).

Part: SEAT TRACK — CRACKED (BS 1400)

INSPECTION TYPE:C2 STA 1400 TRACK I SCALLOPS GOUGED. FABRICATED AND INSTALLED NEW SECTION OF CARGO TRACK IAW 51-1-20D, 51-3-0, 53-2-3. MAT ID FOR NEW SECTION OF CARGO TRACK S2772660-13500N, SPO429308.

Part: SEAT TRACK — GOUGED (BS 300)

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK I IS GOUGED AT STA 300. BLENDED GOUGED AREA, FOUND TO EXCEED LIMITS IAW DC8 SRM 53-2-3. REPAIRED IAW DC8 SRM 53-2-3. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0 AND 53-2-3.

Part: WEB — CRACKED (BS 857)

INSPECTION TYPE:C2, FS 857 LOWER WEB HAS CRACK AT NUT PLATE ON LOWER LEFT ACCESS PANEL. FABBED REPAIR IAW DC8 SRM 53-2-0. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-8.

Part: SUPPORT — CORRODED (BS 1160)

INSPECTION TYPE:C2, C-PIT STA 1160 FLOORBEAM SUPPORT EXFOLIATED L27L. FABRICATED AND INSTALLED NEW FLOORBEAM SUPPORT AND SHIM IAW REO NR 06609 AND DC8 SRM 51-1-20D.

Part: FUSELAGE — CORRODED (FS1300)

INSPECTION TYPE:C2 AFT CARGO PIT STA 1300 6 EA FLOORBOARD SPLICES CORRODED X-38 TO X-20 FABBED AND INSTALLED NEW SPLICES IAW DC8 SRM 58-1-20 AND DC8 SRM 53-2-3.

Part: WEB — CRACKED (BS 857)

INSPECTION TYPE:C2, FS 857 LOWER WEB HAS CRACK AT NUT PLATE ON LOWER RIGHT ACCESS PANEL. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND FILLER ALODINED AND PRIMED AREA.

Part: DOOR TRACK — CORRODED (BS 1200-1210)

INSPECTION TYPE:C2, AFT CARGO PIT CORROSION ON I/B AND O/B FACES OF INTERCOSTAL IN 'C' PIT DOOR TORQUE OBX STA 1200-1210 L29R. FABRICATED AND INSTALLED DOOR TRACK IAW DC8 SRM 51-3-8 DAC DWG 9754947.

Part: FRAME — CORRODED (BS 1260)

INSPECTION TYPE:C2, AFT CARGO PIT CORROSION EMINATING FROM JOINT AT INTERCOSTAL ATTACH CLIP AND FRAME, STA 1260 LONG 35R. REMOVED LITE CORROSION, ALODINED AND PRIMED IAW DC8-SRM 51-1-8.

Part: HINGE — CRACKED (LT TE FLAP)

INSPECTION TYPE:C2, LT OUTBOARD FLAP 339 FLAP HINGE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FLAP HINGE FITTING SUPPORT IAW S/B 27-249.

Part: DOUBLER — CRACKED (CARGO DOOR)

INSPECTION TYPE:C2 D CARGO PIT DOOR EXTERIOR SKIN HAS .75 INCH VISIBLE CRACK 12 INCHES ABOVE LOWER AFT CORNER. FABBED AND INSTALLED DOUBLER IAW DC8 SRM 52-2-0, 51-1-21, 51-1-20 & 51-1-15.

Part: SUPPORT — CORRODED (BS 1020)

INSPECTION TYPE:C2 C CARGO PIT RT TUNNEL STA 1120 FLOORBEAM SUPPORT CORRODED AT NUTPLATE 6 ABOVE LONG 27R. FABRICATED AND INSTALLED NEW STRUT IAW DC8 SRM 51-3-2 AND 51-1-20.

Part: SEAT TRACK — CORRODED (BS 1000)

INSPECTION TYPE:C2, CARGO PIT CORROSION ON BOTTOM SIDE OF MAIN CABIN FLOORBOARD AND SEAT TRACK STA 1000-1100 X3 TO -3. FABRICATED AND INSTALLED FLOOR PANELS IAW DC8 SRM 51-1-8 & 51-3-0, 53- 2-3 AND ADDENDUM DC8-53B-003.

Part: SHEAR TIE — CRACKED (BS 1160)

INSPECTION TYPE:C2, SHEAR THE CRACKED STA 1160 LONG 26L-27L INSIDE C-PIT DOOR TORQUE BOX. FABRICATED AND INSTALLED NEW SHEAR TIE SECTION IAW DAC DWG NR 9754002 & DC8 SRM 51-1-20D, 53-2-0 FIG 2B.

Part: ANGLE — CORRODED (BS 1160)

INSPECTION TYPE:C2, C-PIT GILLINER SUPPORT ANGLE CORRODED STA 1160 LONG 26L-27L. FABRICATED AND INSTALLED WEB, DOUBLER, FILLER IAW DC8 SRM 51-1-20D, 51 -1-21 DAC DWG 9751879 AND EO DC8 5350-7876.

Part: STANTION — CORRODED (BS 1180)

INSPECTION TYPE:C2, LT FLOORBEAM SUPPORT STA 1180 CORRODED 12 INCHES ABOVE LONG 27L. REMOVED STANTION, LOCATED DRILLED AND DEBURRED NEW STANTION. INSTALL ED NEW STANTION IAW UPS DC8 SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING)

INSPECTION TYPE:C2 R/W L/E DOUBLER CRACKED JUST ABOVE NR 4 PYLON. FABRICATED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-1A AND 51-1-20D.

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE:C2, MAIN CARGO DOOR FTG CRACKED UPPER FWD CORNER NEAR ACTUATOR. INSTALLED NEW FITTING, ACTUATOR SUPPORT AND CORNER FITTING IAW UPS DC8 SRM 51-1-21 & 51-3-0, UPS DCI M/M 52-36-03 & 52-36-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK IAW M/M 33-50-01, OPS CHK GOOD. (P/N 5708458-503), (S/N 1132) ON, (P/N 10382) OFF.

Part: FITTING — CORRODED (BS 1228)

INSPECTION TYPE-D, C-3 DOOR AFT TORQUE BOX SUPPORT FITTING AT FS 1228 BTWN LONG 32R AND 33R HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-01-20.

Part: WEB — CRACKED (BS 50-130)

INSPECTION TYPE-D, FS 50 TO 130 RBL 44 FLOOR WEB CORRODED AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-20D, 51-1-21, AND DWG 9753289.

Part: BRACKET — CRACKED (LT ELEVATOR)

INSPECTION TYPE-D, LT ELEV CONTROL TAB MOUNT 2ND FROM INBD IS CRACKED. REMOVED AND REPLACED BRACKET ASSY IAW SRM 51-1-21.

Part: FLOORBEAM — CRACKED (BS 1500)

INSPECTION TYPE:D N/R/C 620816 WRITTEN TO REMOVE FLOOR PANELS FROM FS 980 TO 1540 FOR ADDITIONAL INSPECTION OF FLOORBEAMS, DUE TO EXCESSIVE CORROSION IN AREA. FLOORBEAM CORRODED AND CRACKED FS 1500 LBL 48. REPAIRED FLOORBEAM IAW DHC SK-809-900.

Part: FLOORBEAM — CORROSION (BS 1180)

INSPECTION TYPE-D, FS 1180 LBL 24 FLOORBEAM CORROSION BEYOND LIMITS. REPAIRED IAW DHC SK-809-891.

Part: SKIN — CORRODED (HORZ STAB)

INSPECTION TYPE-D, RT HORZ STAB L/E O/B SECTION CORROSION REMOVAL BETWEEN SKIN OUT OF LIMITS, REF NR 621494. REPAIRED L/E SKIN IAW SRM 55-3-0, 55-2-0, 53-2-0, 55-3-1, AND 51-1-21.

Part: PRESURE PANEL — CORRODED (BS 10-25)

INSPECTION TYPE-D, COMPLY WITH DHC SK-809-038 COCKPIT SUBFLOOR AT FS -25 TO -10 BL-0 TO RBL-16 PRESURE PANEL FOR CABLE FEED THRU IS BULDGING AND HAS NUMEROUS RIVETS SHEARED. REPAIRED IAW DHC SK-809-038.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-D, FLOORBEAM SUPPORT TORQUE BOX FITTING CRACKED FS 1160 AT STR 27R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-0, 51-1-20D, AND DWG 3754025.

Part: FLOORBEAM — CORRODED (BS 640)

INSPECTION TYPE-D, FS 640 AT RBL 35 CABIN FLOORBEAM CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK 809-358.

Part: STIFFENER — CORRODED (BS 867)

INSPECTION TYPE:D F/S 867 LBL 16-30 STIFFENER CORROSION REMOVAL OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW SRM 51-1-21, 51-1-20D, AND DWG 5645332.

Part: FLOORBEAM — CORROSION (FS 460)

INSPECTION TYPE:D CORROSION ON FLOORBEAM AT F/S 460 RBL 24-26 WENT OUT OF LIMITS. REPAIRED IAW DHC SK 809-479.

Part: STIFFENER — CORRODED (LT MLG WW)

INSPECTION TYPE-D, CORROSION OUT OF LIMITS ON REAR MAIN SPAR STIFFENER LT W/W FWD O/B TOP AT BONDING POINT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 51-1-20D AND DWG 3642949.

Part: FITTING — CRACKED (BS 130)

INSPECTION TYPE-D, FS 130 LONG 21L FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1540)

INSPECTION TYPE:D F/S 1540 STR 25R HAS SEVERE CORROSION, AT TOP FRAME MOUNT BOLT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2, 51-1-21, 51-1-20D.

Part: LONGERON — CORRODED (BS 1540)

INSPECTION TYPE-D, FS 1540 STR 29R HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 53-2-2 AND 51-1-21.

Part: FLOORBEAM — CORRODED (BS 260)

INSPECTION TYPE:D FLOORBEAM F/S 260 RBL 27 CORROSION REMOVAL OUT OF LIMITS ON FWD FLANGE. REPAIRED IAW DHC SK 809-788.

Part: MEMBRANE — CRACKED (BS 55)

INSPECTION TYPE:D SUBFLOOR MEMBRANE CRACKED AT F/S 55 RBL 29. REPAIRED IAW SRM 53-2-0, 51-1-21, AND 53-3-1.

Part: STRINGER — CORRODED (BS 1540)

INSPECTION TYPE:D F/S 1540 STR 26R HAS SEVERE CORROSION AT FRAME ATTACH BOLT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 51-1-21 AND 53-2-2.

Part: DOUBLER — CRACKED (BS 1510)

INSPECTION TYPE-D, FS 1510 FINGER DOUBLER BTWN STR 21R TO 31R IS CORRODED AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5779936.

Part: SPLICE — CORRODED (BS 1540)

INSPECTION TYPE-D, FS 1540 STR 24R HAS SEVERE CORROSION AT FRAME ATTACH BOLT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 53-2-2, 51-1-20D.

Part: LONGERON — CORRODED (BS 1050-1060)

INSPECTION TYPE-D, LONG 36 FS 1050 TO 1060 HAS CORROSION OUT OF LIMITS AFT CARGO PIT. REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 AND 51-1-20D.

Part: ANGLE — CRACKED (BS 25)

INSPECTION TYPE:D F/S 25 ANGLE (FWD ENTRY DOOR PAN TO SKIN ANGLE) CRACKED ABOUT 8 LONG IN RADIUS LOCATED AT CUSP LINE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20, AND DWG 5597646-89.

Part: SEAT TRACK — CORROSION (BS 560-580)

INSPECTION TYPE:D F/S 560-580 RBL 59, SEAT TRACK HAS MODERATE CORROSION TO HEAVY CORROSION BOTTOM SIDE OF BOTH LT AND RT UPPER FLANGES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3 AND 51-1-20D.

Part: SKIN — CORRODED (BS 1340-1700)

INSPECTION TYPE-D, SKIN BULDGING AT EACH STA FROM FS 1340 TO 1700 STR 36 TO BELOW 21R. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-1-21, 51-1-20D, 51-3-0.

Part: FLOORBEAM — CORRODED (BS 1360)

INSPECTION TYPE-D, CORROSION ON FLOORBEAM F/S 1360 LBL 44. REPAIRED IAW DHC SK-809-741.

Part: FLOORBEAM — CORRODED (BS 1380)

INSPECTION TYPE-D, FLOORBEAM DAMAGED DUE TO CORROSION FS 1380 LBL44. REPAIRED IAW DHC SK-809-800.

Part: SUPPORT — CORRODED (BS 12)

INSPECTION TYPE:D FLOOR SUPPORT AT RBL 7-27 CORRODED BEYOND LIMITS F/S 12 AFT OF EPC RACK. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW 51-1-20D AND DWG 5755032.

Part: SKIN — CORRODED (BS 1350-1390)

INSPECTION TYPE-D, CORROSION ON SKIN BETWEEN FS 1350 TO 1390 LONG 25 TO 28R. REPAIRED SKIN IAW DHC SK-809-374.

Part: ANGLE — CRACKED (BS 86)

INSPECTION TYPE-D, COCKPIT SUBFLOOR AT FS 86 LBL 59 VERTICAL ANGLE IS CRACKED IN TWO PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20D AND DWG 5613781 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE-D, LONGERON 30L FITTING AT STA 1690 IS CRACKED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FRAME — CORRODED (BS 70)

INSPECTION TYPE-D, CORROSION ON FWD CHORD FS 70 OUT OF LIMITS FROM BETWEEN L-29R AND 30R L-33R AND 34R. REPLACED FRAME CAP IAW SRM 51-1-20D AND 53-2-5.

Part: DOUBLER — CRACKED (BS 857)

INSPECTION TYPE-D, FINGER DOUBLER CRACKED FS 857 BL 0. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-2, 51-1-20.

Part: FITTING — CORRODED (BS 902)

INSPECTION TYPE-D, FRAME TIE FITTING CORRODED OUT OF LIMITS FS 902 ABOVE L-24R INSIDE W/W. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 57-2-0, 51-1-21, AND 51-1-20.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE-D, FS 960 ABOVE L24R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 AND 51-1-21.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-D, FS 940 ABOVE LONG 24R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 AND 51-1-21.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE-D, FS 879 ABOVE L-24L FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE-D, FS 920 ABOVE L-24L, FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-1-20D.

Part: FITTING — CRACKED (BS 960)

INSPECTION TYPE-D, FS 960 L-24L FITTING IS CRACKED ABOVE LONGERON. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 1730)

INSPECTION TYPE:D CORROSION FOUND TO BE OUT OF LIMITS ON SHEAR TIE F/S 1730 LONG 26R- 28R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-1-10 AND 53-5-3.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-D, FS 940 ABOVE L-24L, FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-1-20D.

Part: FLOORBEAM — CRACKED (BS 60)

INSPECTION TYPE-D, FLOOR SUPPORT CRACKED AND CORRODED FS 60 RBL 45. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT IAW SRM 51-1-20D, 53-2-2, 53-7-0, AND DWG 5890314-2.

Part: WEB — CORRODED (BS 55-70)

INSPECTION TYPE:D AFTER CORROSION REMOVAL WEB FOUND TO BE CRACKED AT F/S 55-70 RT AT UPPER CUSP. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT WEB IAW SRM 53-2-0, 51-1-21, 51-1-20D, AND 53-3-1.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D LONGERON 27R F/S 70 LONGERON END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D.

Part: SKIN — DAMAGED (BS 1400)

INSPECTION TYPE-D, FUSELAGE SKIN DENTED AND DAMAGED FS 1400 L-30R TO 32R ON FWD EDGE OF C-4 CARGO DOOR CUTOUT. REPAIRED IAW DHC SK-809-371 REF UPS EO DC8-5330-9486-A.

Part: INTERCOSTAL — CRACKED (BS 280-300)

INSPECTION TYPE:D INTERCOSTAL CRACKED F/S 280-300 L-11L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-10 AND DWG 5610118.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE:D LONGERON 27R F/S 70 LONGERON TO BULKHEAD FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 781.5)

INSPECTION TYPE-D, CORROSION FOUND TO BE OUT OF LIMITS ON SEAT TRACK BL 0 FS 781.5. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 53-2-3, 51-3-0, AND DWG 5750864.

Part: WEB — CORRODED (BS 1160)

INSPECTION TYPE-D, CORROSION REMOVAL ON N/R 620814 MATERIAL LOSS IS BEYOND LIMITS OF SRM 53-2-0 FIG 1F AT FS 1160 LONG 32R 1 INCH DIAMETER AREA ON TORQE BOX WEB. REPAIRED IAW SRM DC8-5350-7876-A.

Part: FRAME — CORRODED (BS 1730)

INSPECTION TYPE-D, CORROSION OUT OF LIMITS ON FRAME FS 1730 LONG 28R TO 24R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF FRAME IAW SRM 53-2-0, 51-1-21, AND 51-1-20D.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:D F/S 1220 L33R TO 34R TORQE BOX FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CORRODED (BS 280)

INSPECTION TYPE-D, CORROSION OUT OF LIMITS ON FLOORBEAM SUPPORT UPPER SPLICE AT FS 280 RT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 53-2-0 AND 51-1-20D.

Part: SHEAR TIE — CORROSION (BS 1220)

INSPECTION TYPE-D, SHEAR TIE FITTING BTWN LONG 35R TO 36 AT FS 1220 LWR SURFACE OF LWR FLANGE HAS MODERATE CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-1-20D, 53-2-0.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED ABOVE THE PNEU DUCT. THE CRACK IS APPROX 1 LONG. REPAIRED IAW SRM 57-2-0 AND 57-3-3.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING CENTER L/E, OTBD END, THE OUTB SLOT, OUTBD CLOSURE RIB IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-1-0, 51-3-0.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:D C-3 DOOR AFT TORQUE BOX SUPPORT FITTING AT FS 1220 BTWN LONG 33R AND 34R HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (BS 8)

INSPECTION TYPE-D, INTERCOSTAL JUST UNDER LONG 29L AT FS 8 NOSE LANDING GEAR W/W TUNNEL HAS MODERATE CORROSION. ALSO, FS 8 TO LONG CLIP CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL SPLICE CHANNEL AND INTERCOSTAL STIFFENER IAW SRM 51-1-21, 51-1-20D, 53-3-3.

Part: DOUBLER — CORRODED (BS 900)

INSPECTION TYPE-D, DOUBLER STRAP CORRODED AROUND AND BEHIND FASTENER APPROX FS 900 RT W/W TOP O/B. REMOVED CORROSION, BLENDED, PEENDED AREA, AND TREATED AREA IAW SRM 51-1-20D, 51-3-0, 51-1-4A, 51-1-8, DPS999-2, AND COMPLIED WITH DHC SK 809-289.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING L/E AT NR 4 PYLON I/B SIDE SLOT ISLAND MOUNT ANGLE ABOVE PYLON IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21, AND DWG 9753293.

Part: SKIN — CORRODED (WS 393)

INSPECTION TYPE-D, LT WING UPPER L/E SKIN XRS 393 AT THE INBD END OF THE O/B SLOT HAS CORR OUT OF LIMITS. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:D RT WING L/E SECTION BETWEEN PYLONS, 3EA L/E RIBS ARE CRACKED AT THE UPPER AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 466.651)

INSPECTION TYPE:D, RT WING L/E AT STA XS 466.651. THE L/E LWR RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:D F/S 1140 ABOVE STR 35L - TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 246)

INSPECTION TYPE-D, RT WING L/E AT STA XS246.519 TO XS250.089 VERTICAL STIFFENER IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW SRM 51-1-21 AND DWG 9753293.

Part: FRAME — CRACKED (BS 1160)

INSPECTION TYPE:D, F/S 1160 FRAME ABOVE STR-32R IS CRACKED ON LWR END. REMOVED AND REPLACED FRAME ASSY IAW SRM 51-1-20.

Part: FITTING — CRACKED (BS 1141)

INSPECTION TYPE-D, FS 1141 AT STR 33R TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4758514.

Part: CARGO TRACK — CORRODED (BS 1376)

INSPECTION TYPE-D, FS 1376 ABOVE STR 33R CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-1-21 AND 51-3-0.

Part: INTERCOSTAL — CORRODED (BS 1240-1260)

INSPECTION TYPE-D, FS 1240 TO 1260 ABOVE STR 33R INTERCOSTAL HAS LITE AND HEAVY CORROSION I/B SIDE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 51-1-20D, 53-2-0, 51-2-0, AND 51-1-21.

Part: FRAME — CRACKED (BS 1220)

INSPECTION TYPE:D, F/S 1220 FRAME AT STR 29R HAS A 4 CRACK. REMOVED AND REPLACED FRAME IAW SRM 51-3-0.

Part: SUPPORT — CORRODED (BS 120)

INSPECTION TYPE-D, THE FLOOR SUPPORT AT FS 120, RT SIDE, THE INBD FLANGE AT THE BOTTOM NUT PLATE HAS HEAVY EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (WS 455)

INSPECTION TYPE-D, RT WING L/E SECTION BTWN PYLONS AT STA XS454.976 INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21.

Part: FLOORBEAM — CORROSION (BS 1460)

INSPECTION TYPE-D, FS 1460 LBL 24 ON NR 4 PIT CEILING, FLOORBEAM TANG HAS HEAVY CORROSION, METAL IS SEPARATING. REPAIRED IAW DHC SK 809-737 AND SRM 51-1-30.

Part: FITTING — CRACKED (BS 1360)

INSPECTION TYPE-D, F/S 1360 AT LT CUSP LWR SURFACE, FLOORBEAM TO FRAME TO SKIN TIE FITTING HAS LARGE CRACK DUE TO CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 51-3-0, AND DWG 3773479.

Part: ANGLE — CORRODED (BS 340-350)

INSPECTION TYPE-D, C-1 DOOR TORQUE BOX UPPER WEB SUPPORT ANGLE AT LONG 27R BTWN FS 340 TO 350 HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20D AND DWG 9754020.

Part: FLOORBEAM — CORRODED (BS 1160)

INSPECTION TYPE:D F/S 1160 AT LBL 44 ON NR 3 PIT CEILING, FLOORBEAM TANGS HAVE SEVERE CORROSION (METAL IS SEPARATING). REPAIRED IAW DHC SK 809-807.

Part: SUPPORT — CORRODED (BS 1580)

INSPECTION TYPE-D, CORROSION ON FWD SIDE OF FLOORBEAM SUPPORT FS 1580 AT STR 27R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT IAW 51-1-20D AND DWG 3773158.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE-D, CRACKED SPLICE FITTING UNDER SEAT TRACK RBL 24 FS 759. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 3755222.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 7L BETWEEN FS 300 TO 320 SPLICE FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4646163.

Part: FITTING — CRACKED (BS 679)

INSPECTION TYPE-D, FS 679 AT STR 13R END FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21D AND DWG 4750421.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 11L SPLICE FITTING BETWEEN FS 300 TO 320 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-0, 51-1-20D, AND REF SEO 5751702-001A ENRG INSTRUCTIONS.

Part: RIB — CRACKED (HORIZ STAB)

INSPECTION TYPE:D, LT INBD HORIZ STAB L/E HAS CRACKED RIB AT STA XFS 147.5 (LOWER) SIDE. (OFF A/C PAR ). REPAIRED IAW SRM 55-2-0.

Part: FITTING — CRACK (BS 759)

INSPECTION TYPE:D CRACK IN FITTING AT F/S 759 RBL 51 AT THE BEAM SUPPORT WEB. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 53-1-0, 51-1-20, DWG 3641125, AND DHC SK-809-663.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 8L SPLICE FITTING BETWEEN FS 300 TO 320 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 51-1-21, AND DWG 4646163.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE:D LONG 4-L SPLICE FITTING CRACKED BETWEEN F/S 300-320. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, 51-1-20D, AND DWG 2646348.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 10L BETWEEN FS 300 TO 320 SPLICE FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4646163.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 20L SPLICE FITTING BTWN FS 300 TO 320 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 53-1-0, AND 51-1-0.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 19L SPLICE FITTING BETWEEN FS 300 TO 320 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-0, 51-1-20D, 51-1-11, AND SEO NR 5751702-001A.

Part: SPLICE — CRACKED (BS 300-320)

INSPECTION TYPE-D, LONG 13L SPLICE FITTING BTWN FS 300 TO 320. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 51-1-20D, 53-1-0, 51-1-0, AND DWG 5779931.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:D, F/S 280 AT STR 27R, FLOORBEAM SUPPORT FITTING IS CRACKED AT BASE. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:D F/S 1160 AT STR 27R - FLOORBEAM SUPPORT FITTING IS CRACKED AT BOTTOM. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 100)

INSPECTION TYPE:D, F/S 100 FRAME END FITTING AT RT CUSP UPPER SURFACE HAS MODERATE CORROSION ON ALL SIDES. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 585-595)

INSPECTION TYPE-D, FS 585 TO 595 RBL 59 THE SEAT TRACK HAS MODERATE CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-2-3, 51-3-0, 51-1-21 AND DWG 2772660.

Part: SEAT TRACK — CORRODED (BS 240)

INSPECTION TYPE:D F/S 240 RBL 24, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW SRM 53-2-3 AND 53-7-3.

Part: DOUBLER — CRACKED (LT INBD AILERON)

INSPECTION TYPE-D, LT INBD AILERON INTERNAL DOUBLER AT ACCESS PANEL 541 IS CRACKED. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (LT AILERON)

INSPECTION TYPE-D, THE LT INBD AILERON T/E, OTBD END IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT T/E IAW SRM 51-1-21, 53-1-0, 51-1-9A, AND 57-2-1.

Part: SEAT TRACK — CORRODED (BS 326)

INSPECTION TYPE-D, FS 326 RBL 44 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 53-2-3, 51-3-0, AND DWG 5750872.

Part: FITTING — CORRODED (BS 870-902)

INSPECTION TYPE-D, RT LONG 24 HAS CORROSION ON, UNDER, AND AROUND FASTENERS AND PREVIOUS REPAIRS. REMOVED AND REPLACED LONG 24 FITTING IAW SRM 51-1-21.

Part: TRIPLER — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING L/E, JUST INBD OF THE STA XOLDI 6.225 RIB, THE UPPER SLOT DOOR AFT TRIPLER IS CRACKED IN TWO. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRIPLER IAW 51-1-21, 51-9-0, AND DWG 5770409.

Part: WING — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING L/E O/B SECTION AT SKIN BUTT HAS 2 CRACKS IN SKIN AND MODERATE CORROSION. REPAIRED IAW SRM 51-1-21 AND 57-2-1.

Part: RIB — CRACKED (WS 835)

INSPECTION TYPE:D LT WING L/E RIB AT XFS 835.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 868)

INSPECTION TYPE:D, RT WING L/E O/B SECTION AT STA XFS 868.00. THE L/E SKIN IS CRACKED AND FLAKING. REPAIRED IAW DC8-5720-7767-A.

Part: ANGLE — CRACKED (WS 250)

INSPECTION TYPE-D, LT WING L/E AT THE AFT OTBD CORNER OF THE INBD SLOT STA XS250.089 AFT SIDE BOTTOM, THE RIB TO SLOT AFT WEB ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 57-3-2, AND 51-1-20D.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING LWR L/E SKIN AT THE NR 2 PYLON CUTOUT, INTERNAL AND EXTERNAL REPAIR DOUBLERS ARE CRACKED. FABRICATED AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 57-2-1.

Part: FITTING — CORROSION (BS 920)

INSPECTION TYPE-D, CASTING HAS EXFOLIATION CORROSION FS 920 RT ABOVE LONG 24 RT W/W O/B TOP CENTER. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: SKIN — CORRODED (NR 3 SPOILER)

INSPECTION TYPE:D THE LT NR 3 SPOILER LWR SKIN HAS MODERATE CORROSION, THE CENTER OTBD HINGE TRIPLER IS DELAMINATED AT THE AFT END, AND THE DOUBLER AND TRIPLER EDGE SEALANT IS MISSING. REMOVED AND REPLACED SPOILER ON N/R/C 619538.

Part: FITTING — CORRODED (BS 870-905)

INSPECTION TYPE-D, LT LONG 24 HAS CORROSION UNDER 902 FITTING AND UNDER DOUBLER, FROM F/S 870 TO 905 LT TOP. CORROSION IN LIMITS, REMOVED AND REPLACED CRACKED L-24 FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: WEB — CRACKED (BS 1660)

INSPECTION TYPE:D, RT AFT SERVICE DOOR CUTOUT F/S 1660 ( INTERIOR ) UPPER AFT CORNER TORQUE BOX WEB HAS 2.5 CRACK. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CORRODED (BS 1280)

INSPECTION TYPE-D, FUSELAGE SKIN AND INTERNAL DOUBLER CORRODED UNDER ANTENNA FS 1280 LONGERON 36. REMOVED AND REPLACED FUSELAGE SKIN WITH INTERNAL DOUBLER FROM FS 1050 TO 1350 STR 31L TO 31R IAW SRM 51-1-21, 51-1-20D, AND DWG 5750322.

Part: SKIN — CORRODED (BS 70)

INSPECTION TYPE-D, BULGING CORROSION FS 70 SKIN SPLICE BETWEEN STR 34L AND 36. REMOVED AND REPLACED SKIN FROM FS 70 TO 121 IAW EO DC8-5330-8942-B.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-D, LONGERON 31R END FITTINGS FWD OF FS 70 HAVE MODERATE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-1-21, AND 51-3-0.

Part: FITTING — CRACKED (BS 1178)

INSPECTION TYPE-D, FS 1178 AT RT CUSP UPPER SURFACE FRAME END FITTING IS CRACKED BETWEEN HI-LOKS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: LIGHT — BROKEN (DOOR MAIN ENT)

MAINTENANCE REPORTED, RADIO ACTIVE EXIT SIGN ON FWD ENTRANCE DOOR IS BROKEN.

Part: SKIN — CRACKED (LEFT)

MAINT REPORTED, CRACK AT BOX ROOT AREA LT WING. STOP PER EO DC8-5750-7635C.

Part: FLOOR BEAM — CORRODED (BS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FLOOR BEAM HEAVY CORROSION AT FS 1580, LBL 50. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7529A.

Part: SKIN — CORRODED (BS 55)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FLOOR BEAM HEAVY CORROSION AT FS 1580, LBL 50. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7529A.

Part: SKIN — CORRODED (BS 1140-1150)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN HAS HEAVY CORROSION ON FS 1140-1150, LONGERON 33R. MAINTENANCE REPAIRED IAW UPS E.O. DC8-5330-7525A.

Part: LONGERON — CORRODED (BS 280-300)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 35L, FS 280-300 AND ON LONGERON 33L, FS 320. MAINTENANCE REPLACED LONGERON SECTION FS 190-390 PER SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LOWER SIDE OF THE FRAME AT THE STRINGER CUT-OUT. MAINTENANCE REPAIRED THE FRAME IAW SRM 54-10-03.

Part: LONGERON — CORRODED (BS 1540)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON LONGERON 31R, FS 1540. MAINTENANCE REPAIRED PER UPS E.O. DC8-5310-7527A.

Part: SHEAR TIE — CRACKED (BS 1640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SHEAR TIE AT 2 PLACES AT STATION 1640L BETWEEN STRINGERS 50 AND 51L. MAINTENANCE REMOVED THE DAMAGED PART FROM SHEAR TIE AND REPAIRED SHEAR TIE ACCORDING TO SRM 53-10-04.

Part: LONGERON — CORRODED (BS 1340-1460)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY INTERGRANULAR CORROSION ON LONGERON 31R, FS 1340 TO FS 1360. MAINTENANCE REPAIRED PER UPS E.O. DC8-5310-7520-D.

Part: FRAME — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RADIUS OF THE LOWER SIDE OF THE FRAME. MAINTENANCE REPAIRED THE FRAME IAW SRM 51-30-02/05.

Part: BLKHD WEB — DAMAGED (BS 2160)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HOLE DAMAGE IN THE AFT BULKHEAD AT STATION 2160 AND LBL 45. MAINTENANCE REMOVED THE DAMAGED PART FROM THE WEB AND REPAIRED THE WEB ACCORDING TO SRM 51-40-02.

Part: SKIN — CRACKED (BS 1350-1450)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN HAS CRACK DAMAGE AT FS 1350-1450, LONGERON 31R. MAINTENANCE REPAIRED IAW UPS E.O. DC8-5330-7546A.

Part: DOUBLER — CORRODED (FS 70)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FINGER DOUBLER, LONGERON 31R, FS 70-8. MAINTENANCE REPLACED DOUBLER PER SRM 51-1-21 AND 51-1-20D.

Part: BELT FRAME — CORRODED (BS 1400)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME FS 1400 BETWEEN LONGERONS 36-32R. MAINTENANCE REPAIRED IAW UPS EO DC8-5310-7537A.

Part: FITTING — CORRODED (BS 1140)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME AND FITTING HAS HEAVY CORROSION ON FS 1140, LONGERON 21R. MAINTENANCE REPLACED THE FITTING IAW SRM 51-3-0.

Part: FRAME — CORRODED (BS 1420)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FRAME FS 1420 BETWEEN LONGERONS 33R-34R. MAINTENANCE REPLACED A SECTION OF FRAME IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 450)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FINGER DOUBLER HEAVY CORROSION AT FS 450 BETWEEN LONGERONS 32L-32R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21.

Part: WEBBING — CORRODED (BS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE WEBBING CORRODED AT FS 1580-LBL 50. MAINTENANCE REPAIRED IAW SRM 53-2-0.

Part: SHEAR TIE — CORRODED (BS 1000)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND SHEAR TIE HAS HEAVY CORROSION AT FS 1000, LONGERON 30R-31R. MAINTENANCE REPLACED THE SHEAR TIE PER SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 1355 LON 35R)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AND CRACKS LONGERON 35R, FS 1355-1420. MAINTENANCE REPLACED LONGERON SECTION FS 1360-1460 IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME END FITTING HAS HEAVY CORROSION AT FS 80, LONGERON 21R. MAINTENANCE REPLACED THE FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (BS 280/300)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION IN 3 EACH B/T FITTINGS, FS 300, LONGERON 34R-33R AND LONGERON 34L-35L, AND FS 280, LONGERON 32L-33L. MAINTENANCE REPLACED THE FITTINGS PER SRM 53-2-0, FIGURE D.

Part: SPLICE — CORRODED (BS 1340-1360)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT 2 EACH LONGERON SPLICE FITTINGS FS 1340-1360, LONGERON 29L AND, FS 1400, LONGERON 35L-34R. MAINTENANCE REPLACED THE FITTINGS IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 280/300)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING SPLICES FS 280, LONGERON 34L-35L, FS 300, LONGERON 354-34R. MAINTENANCE REPLACED THE FITTINGS IAW SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 395)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FRAME ATTACH ANGLE AT FS 395, LONGERON 21L. MAINTENANCE REPLACED THE ANGLE IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 1535-1545)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION FINGER DOUBLER LONGERON 31R, FS 1535-1545. MAINTENANCE REPLACED THE DOUBLER IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1360-1480)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 32L BETWEEN FS 1360 TO 1480. MAINTENANCE REPAIRED LONGERON IAW SRM 53-2-2 AND 51-1-20D.

Part: ANGLE — CORRODED (BS 320)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON I/B LOWER ANGLE INNER WEB FS 320, LONGERON 28L. MAINTENANCE REPAIRED ANGLE IAW SRM 52-2-2 AND 51-1-20D.

Part: LONGERON — CORRODED (BS 284-300)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INBOARD END OF LONGERON 34R AT FS 300 TO 284. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A X-SLIDE DOOR CUTOUT CENTER DOUBLER HAS HEAVY CORROSION BULGES. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CORRODED (BS 1420)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FUSE EXT BELLY SKIN, FS 1420. MAINTENANCE REPLACED SKIN SECTION IAW SRM 51-1-21 AND 51-1-20D.

Part: ANGLE — CORRODED (BS 885-902)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION OUT OF LIMITS ON L-ANGLE, LONGERON 24 STA 885 TO 902. MAINTENANCE REPLACED ANGLE IAW SRM 51-1-20D.

Part: ANGLE — CORRODED (FS-895)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION OUT OF LIMITS ON L-ANGLES, FS 895 LONGERON 24L. MAINTENANCE REPLACED THE ANGLE IAW SRM 51-1-20D.

Part: FITTING — CORRODED (FS 28)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT B/T FITTING LONGERON 34R TO 35R, FS 28. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1420-1490)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 36 CRACKED AND HEAVILY CORRODED AT STA 1420 TO 1490. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 200-450)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER AT FS 200 TO 450, LONGERON 31L. MAINTENANCE RPELACED DOUBLER IAW SRM 51-1-21 AND 51-4-20D.

Part: LONGERON — CORRODED (BS 1350-1450)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 34R, FS 1350 TO 1450. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D.

Part: SKIN — CORRODED (BS 190-450)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGES AT BELLY SKIN FS 190 TO 450. MAINTENANCE REPLACED THE SKIN IAW SRM 51-1-20D.

Part: SHEAR TIES — CRACKED (BS 1420)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME SHEAR TIE CRACKED AT FS 1420, LONGERON 3XR. MAINTENANCE REPLACED TIE IAW SRM 51-1-20D.

Part: SPAR — CRACKED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING INBOARD FLAP REAR SPAR CRACKED FROM STA XW 59.5 TO XW 63.6. MAINTENANCE REPAIRED IAW UPS EO DC8-5710-7526A.

Part: SKIN — CORRODED (BS 1766)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND SKIN BULGED ON FS 1766, LONGERON 32R. MAINTENANCE REPAIRED SKIN IAW UPS EO DC8-5330-7522A.

Part: FITTING — CRACKED (BAG SLIDING DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BANANA FITTING CRACKED ON FWD SIDE OF B/B X-SLIDING DOOR, LONGERON 33R. MAINTENANCE REPLACED FITTING IAW SRM 51-1-20D.

Part: TAB — DELAMINATED (RUDDER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RUDDER TAB DELAMINATED ON UPPER FORWARD SECTION. MAINTENANCE REPLACED TAB PER MM 27-21-02.

Part: LONGERON — CORRODED (BS 1690)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERONS 28L AND 28R HAVE HEAVY CORROSION AT FS 1690. MAINTENANCE REPAIRED IAW SRM 53-2-2.

Part: SKIN — CORRODED (BS 1650-1690)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION IN FUSELAGE EXTERNAL SKIN AND INNER DOUBLER AT FS 1650 TO 1690, LONGERON 29R TO 32R. MAINTENANCE REPLACED THE SKI AND INNER DOUBLER PER SRM 51-1-21.

Part: LONGERON — CRACKED (BS 879)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L CRACKED AT LOWER SURFACE, FS 879. MAINTENANCE REPAIRED THE LONGERON IAW SRM 53-2-2 FIGURE 9.

Part: LONGERON — CRACKED (BS 280)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 34L CRACKED ON THE OUTBOARD SIDE, FS 280. MAINTENANCE REPLACED THE LONGERON SECTION IAW SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME CRACKED AT FS 1580, 3 INCHES ABOVE LONGERON 21R. MAINTENANCE REPAIRED THE FRAME IAW SRM 53-2-0.

Part: FITTING — CORRODED (FS 1685)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 26R AT FS 1685. MAINTENANCE REPAIRED IAW SRM 53-2-2 AND 51-1-22.

Part: PANEL — DELAMINATED (NR 1 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 1 SPOILER PANEL DELAMINATED AT INBOARD END. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: VANE — DELAMINATED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 2 FLAP VANE DELAMINATED AT UPPER OUTBOARD END. REPLACED FLAP VANE ASSY PER MM 27-51-14.

Part: VANE — DELAMINATED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 5 FLAP VANE DELAMINATED AT LOWER OUTBOARD END. REPLACED VANE ASSY PER MM 27-51-14.

Part: LONGERON — CORRODED (BS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 36 AND END FITTING, FS 1615. MAINTENANCE REPLACED THE FITTING AND REPAIRED LONGERON IAW SRM 53-2-2 AND 51-1-20.

Part: LONGERON — CORRODED (BS 1490-1620)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON LONGERON 36, 34 LT AND RT, 35 LT AND RT, AT FS 1490 TO 1620. MAINTENANCE REPLACED ALL 5 LONGERON SECTIONS IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 700)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND END FITTING CRACKED AT FS 700, LONGERON 21L. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20B.

Part: SKIN — CRACKED (BS 273)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FORWARD BELLY SKIN HAS A 2 INCH CRACK AT FS 273, LONGERON 33R. MAINTENANCE REPLACED BELLY SKIN IAW SRM 51-1-20D.

Part: SKIN — CRACKED (FS 1340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN CRACKED AFT UPPER RADIUS LT AFT ENTRY DOOR. REPAIRED PER UPS EO DC8-5310-7470-A.

Part: LONGERON — CRACKED (FS 1656)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 29R, 324 AND 33R CRACKED AT FS 1656. REPAIRED LONGERONS PER SRM 53-2-2 FIGURES 2 TO 6.

Part: SKIN — CRACKED (FS 1346)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN CRACKED FWD UPPER RADIUS RT FWD SERVICE DOOR. REPAIRED PER UPS EO DC8-5310-7471-A.

Part: SPLICE — CRACKED (FS 210)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON SPLICE AT FS 210, LONGERON 30R CRACKED. REPLACED SPLICE PER SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1540/1580)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 33L CRACKED AT FS 1540 AND FS 1580, LONGERON 33R. REPAIRED LONGERONS PER SRM 53-2-2.

Part: FITTING — CRACKED (FS 1680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 28L FITTING CRACKED AT FS 1680, FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1490-1660)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND EXFOLIATION CORROSION AND CRACK, LONGERON 33R BETWEEN FS 1490 TO 1660. MAINTENANCE REPAIRED IAW SRM 53-2-2.

Part: DOUBLERS — CORRODED (BS 1620-1690)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 INTERNAL DOUBLERS CORRODED AT FS 1620 TO 1690, LONGERONS 21L TO 21FL. MAINTENANCE REPLACED THE DOUBLERS IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 55)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 36 END FITTING CRACKED AT FS 55. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20D.