N708UP

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

ONE EMERGENCY EXIT LIGHT IN COCKPIT INOP. RELAMPED COCKPIT DOME LIGHT IAW DC8 MM 33-50-02-2. OPS CHECK GOOD.

Part: SLIDE — DISLODGED (PAX DOOR)

ENTRY DOOR OPENED FROM OUTSIDE A/C BY LOAD SUP. SLIDE FELL OUT OF PACK, DID NOT INFLATE. REINSTALLED SLIDE AS REQUIRED IAW MM 25-60-01-2

Part: LIGHT — SMOKE (COCKPIT)

HAD LIGHT ODOR OF SMOKE IN COCKPIT. F/E PANEL LIGHTS WENT OUT. APPEARS TO BE A 5 AMP FUSE HAS BLOWN ON F/E PANEL DID NOT REPLACE IN FLIGHT. REMOVED AND REPLACED F/E PANEL LIGHT. FUSE 5 IAW MM 33-13-00-5. OPS CHKS GOOD.

Part: SLIDE — OUT OF POSITION

INSPECTION TYPE:N/A ESCAPE SLIDE NOT PROPERLY STOWED. REPACK ESCAPE SLIDE, OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WOULD NOT COME ON WHEN PERFORMING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT AND TESTED IAW 33-50-01-2. TESTS OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WON'T TEST. FOUND ON PRE-DEPARTURE CK. REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT WITH REF TO M/M 33- 50-01-2. GROUND CKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 70 L32R FWD SIDE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20 D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 FITTING CRACKED AT RT STA 70 L30R. REMOVED AND REPLACED FITTING IAW SRM 51-3-0,51-1-20D AND 51-3-2.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 C-PIT STA 1160 INSIDE OF DOOR, SPYDER FITTING IS CRACKED AT THE BOLT. REMOVED CRACKED SPYDER FITTING AT STA 1160 IAW SRM 51-1-21, FABRICATED AND INSTALLED SPYDER FITTING AT STA 1160 INSIDE OF DOOR IAW SRM 51-3-0, 51-1-21, AND DWG 3754025

Part: STRINGER SPLICE — CRACKED (FS 440-460 L36) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 STA 440 TO STA 460 L36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L36 IAW SRM 51-1-20D, AND SRM 51-03-02-0.

Part: FINGER DOUBLER — CORRODED (FS 440-460) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 STA 440-460 L34L-L34R FUSELAGE DOUBLER AND FINGER DOUBLER HAVE CORROSION. REMOVED FUSELAGE SKIN DOUBLER AND FINGER DOUBLER AT STA 440-460 L34L-L34R IAW SRM 53-2-0. FABRICATED AND INSTALLED SKIN DOUBLER AND FINGER DOUBLER AT STA 440-46- L34L-L34R IAW SRM 53-2-0, 51-1-21 AND DWG 5755271.

Part: LONGERON SPLICE — CORRODED (FS 1690 L36) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 L36 AFT FITTING AND LONGERON AT STA 1690 HAVE CORROSION. FOUND CORROSION OUT OF LIMITS AT STA 1690 L36 SPLICE FITTING IAW SRM 51-20-00. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1690 L36 IAW SRM 51-1-20D, AND SRM 53-02-02-00.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 AFTER SKIN REMOVAL A/C BAY FOUND INTERNAL DOUBLER CORROSION OUT OF LIMITS STA 8-70 BETWEEN L30L-32L. REMOVED INTERNAL DOUBLER FROM STA 8-70 L30L-32L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA 8-70 L30L-32L IAW SRM 53-03-01 FIG 001, AND SRM 51-1-20D.

Part: RIB — CRACKED (RWS 772) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS772. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RWS 659) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS659. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RWS 734) · airframe 73,134 hrs · 48,951 cycles

RT WING OB LE LWR RIB CRACKED AT XFS 734. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 51-1-20D,51-1-21.

Part: DOUBLER — CRACKED (RWS 597) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 597. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21,51-1-20D AND DWG 5769600.

Part: DOUBLER — CRACKED (RWS 566) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS566. REMOVED, FABRICATED AND INSTALLED INNER DOUBLER AND FILLER IAW DWG 5769600, SRM 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RWS 653) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS 653. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RWS 824) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING OB LE UPPER RIB CRACKED AT XFS 824. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-21, 51-01-20D.

Part: SKIN — CORRODED (FS 1350-1490) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 AFTER REMOVAL OF CORROSION AT LWR D-PIT DOOR, SKIN, FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED D-PIT SKIN FROM 1350-1490 L31L-L31R IAW SRM 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE-C3 RT CENTER L/E UPPER RIB CRACKED AT XFS 366. STOPDRILLED CRACK AT RT L/E CENTER UPPER RIB AT XFS 366 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT RT L/E CENTER UPPER RIB AT STA XFS 366 IAW SRM 57-02-00 FIG 002 AND SRM 57-03-01.

Part: RIB — CRACKED (RWS 379) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 379. CRACK TERMINATES AT FASTENER HOLE. FABRICATED REPAIR ANGLES AND INSTALLED IAW DC-8 SRM 57-02-00-0 AND 51-01-20D.

Part: RIB — CRACKED (RWS 304) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.

Part: RIB — CRACKED (RWS 334) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.

Part: RIB — CRACKED (RWS 454) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:3C RT WING CENTER LE UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.

Part: RIB — CRACKED (RWS 460) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002, 51-01-21, AND 51-01-20D.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 NR 1 PYLON INBD SIDE FOUND CRACK AT APPROX STA YN 321. STOP DRILLED CRACK. CRACK TERMINATES AT STOP DRILL EO DC8-5740-0716.

Part: CUSP WEB — CORRODED (FS1250-1290 L21L) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 UPPER CUSP FROM STA 1260 TO 1290 EXFOLIATED CORROSION ON UPPER CUSP AND CRACKED LT SIDE. REMOVED DAMAGED CUSP AT STA 1260-1290 IAW SRM 51-3-0 AND SRM 51-1-8. REPAIRED DAMAGED CUSP AT STA 1250-1290 IAW SAA EA NR 008-5300-01-A0455 REV B, UPS RAA NR DC8-53-20592-B, FAA FORM 8100-9, BOEING SRID 1-231694214, AND SRM 53-2-5 FIG 1F TR# 53-180.

Part: FITTING — CRACKED (BS 742) · airframe 73,134 hrs · 48,951 cycles

INSPECTION TYPE:C3 AT STA 742.2 FRAME FITTING IS CRACKED ON AFT UPPER SIDE OF CUSP. REMOVED AND REPLACED FRAME FITTING IAW DC-8 SRM 51-01-20D AND 51-01-21.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: N/A EMERG LIGHTING BATT PACK PWR LOW. EMERG LIGHTING BATT PACK REPLACED IAW MM 33-50-01-2.

Part: TRIM TAB — CRACKED (RT ELEVATOR)

INSPECTION TYPE:N/A RT ELEV TRIM TAB CRACKED/DAMAGED ABOUT 1' OB OF PREVIOUS REPAIR. REMOVED RT ELEV GEAR TAB REF MM 27-30-03-2. OK TO INSTALL. TRIMMED OTBD EDGE OF RT ELEVATOR GEARED TRIM TAB PER EO DC8-5520-23895A AND INSTALLED TRIM TAB IAW MM 27-30-03. OPS CHECKS GOOD.

Part: DOUBLER — DELAMINATED (FUSELAGE)

UNDER BELLY PANELS (4EA) DELAMINATED ON PREVIOUS REPAIR. LT WING TO BODY LOWER FILLET PANEL DELAMINATED. D303878 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED D303879 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER 33-50-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,509 hrs · 48,466 cycles

INSPECTION TYPE:SP COMPLY WITH D 301309 REGARDING FUSELAGE SKIN CORROSION AT E/E DOOR STA 35. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330- 22128-A AND SAA SK 708-911.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN DAMAGE RT JUST OUTBOARD OF FWD EQUIPMENT CENTER DOOR MARKED. REMOVED DAMAGED SKIN IN CORRODED AREA DIM APPX 2.9 X 2.5 INCHES. REMOVED ADDITIONAL DAMAGED SKIN APPROX 10 X 9 INCHES TOTAL UNABLE TO CLEAN UP ALL OF UNDERLYING CORROSION AT THIS TIME ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-22107-A. PERMANENT REPAIR WITHIN 1 NON REV FLT. DEFERRED D301409.

Part: ENGINE — FLAMED OUT (NR 2)

NR 2 ENGINE FLAMED OUT IN FLIGHT. A/C IS OOS. PERFORMED STEP 4 UP TO FUEL FILTER REPLACEMENT ON FIGURE 139 SHEET 1 OF MM 71 00 00. TS (558010) PERFORMED ENG MAINT RUN PER MM 71-00-00-1, NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS FAIL PRELIGHT TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50, OPS CK GOOD.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25043-17-7PH .080. HEAT TREATED PER AMS 2759 & SRM 51-1-6. INSTALLED ANGLE PER SRM 53-2-5 FIG 16A, 51-1-20D, 51-1-15, SAA SK-708-048.

Part: FITTING — CORRODED (CARGO BAY) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, BATHTUB FITTING CORRODED AT STA 340 BETWEEN L35R & L34R. REMOVED BATHTUB FITTING PER SRM 51-1-20D. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING & REPAIR ANGLES PER SRM 51-1-20D, 53-2-0 FIG 2D.

Part: FITTING — CRACKED (AFT FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C, STATION 1776 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPAIRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DATED 09/08/04 & 8110-3 DATED 08/25/04.

Part: FITTING — CRACKED (CARGO BAY) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, FS 450 L31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31L.

Part: FITTING — CORRODED (CARGO BAY) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE:C2 A-PIT FS 300 BATHTUB FITTING BETWEEN L34L & L33L HAS HEAVY CORROSION. REMOVED BATHTUB FITTING. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2B. INSTALLED NEW FITTING AND REPAIR ANGLES PER SRM 53-2-0 FIG 2B, 51-1-20D.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C, LEFT HORIZONTAL STAB L/E UPPER RIB CRACKED AT XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 55-2-0 FIG 2.

Part: FITTING — CRACKED (TE FLAP HINGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C1, RT FLAP HINGE 3 FITTING HAS APPROX 6-8 IN LONG CRACK BETWEEN TRACK LANDS. REMOVED FLAP HINGE 3 FITTING. IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. FABED IAW SAA SK 708-840-2 FITTING SAME MFG P/N 5642342-2, FLAP LINK SUPPORT FITTING FROM 7050-T7451, AMS 4050,6.0 IN MAX THICKNESS. INSTALLED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, STATION 70 LONGERON 35R AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 70 AND 90, INSTALLED SPLICE AND REPLACED END FITTING IAW SRM 53-2-2 FIG 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C, EXTERNAL FUSELAGE EXISTING REPAIR DOUBLER AT STA 70 L36 REQUIRES REMOVAL, ASSESSMENT, AND REPAIR IAW SRM 53-2-1 FIG 7 REF EO DC8-5330-12800 REPAIR 708-2R-01. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, EXT DOUBLER, AND INTERNAL FINGER DOUBLERS PER SRM 53-2-1 FIG 7.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, STATION 1280 LONG 35R FWD UPPER FLANGE OF FRAME HAS A HOLE AT RADIUS. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AND FILLER IAW EO DC8-5310-11728-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,252 hrs · 48,264 cycles

INSPECTION TYPE: C2, FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 120-160 UNDER ADF ANTENNA MOUNTING LOCATION AT LONG 36. REMOVED EXISTING DOUBLER AT NR 1 ADF ANTENNA, CUT OUT DAMAGE AT NR 2 ADF ANTENNA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER BETWEEN STATION 105 AND 170 BETWEEN LONGERON 34L AND 35R IAW SRM 53-2-1 FIG 7.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CKS OK.

Part: STRINGER CLIP — CRACKED (RT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 RIGHT WING STA XRS 289 LOWER STRINGER CLIP IS CRACKED AT STRINGER 61. REMOVED, FABRICATED, AND INSTALLED CLIP IAW DWG 4614391, SAA SK 708-435, UPS ENGINEERING FILE NUMBER DC8-57-20058, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1180 FWD SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R TO 34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2G.

Part: TRIPLER — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT WING CENTER L/E LOWER INTERNAL TRIPLER IS CRACKED AT STA XOLDI 6.225. REMOVED INTERNAL DOUBLER AND TRIPLER AT WING STA XOLDI 6.225 IAW SRM 51-1-21, FABRICATED REPAIR DOUBLER AND TRIPLER IAW DC8 DRAWING 5769589. INSTALLED REPAIR DOUBLER AND TRIPLER AT STA XOLDI 6.225 IAW SRM 51-1-20D, AND SRM 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XS 484.895. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 A-PIT DOOR LWR PAN UNDER AFT STOP FITTING IS CRACKED STA 360.000 LONG 26R. REMOVED CRACKED LWR PAN IAW 52-4-1, NDT HFEC INSPECTED, NO CRACKS NOTED AROUND CUT OUT. FABRICATED PAN SEGMENT AND REPAIR ANGLES IAW SRM 52-4-1, INSTALLED PAN SEGMENT AND REPAIR ANGLES.

Part: ANGLE — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 250. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1240 INTERCOSTAL ABOVE LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT WING CENTER L/E INTERNAL CIRCUMFERENCE DOUBLER IS CRACKED ON LOWER SECTION AT XFS 348. CUTOUT CRACKED SECTION OF INTERNAL DOUBLER, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER SECTION AND SPLICE IAW UPS ENGINEERING FILE NUMBER DC8-57-20055 AND SAA SK 708-162.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1400 LONG 30L EXTERNAL DOUBLER, CLASSIFIED CATERGORY D, IAW DC8-5330. REMOVED EXTERNAL DOUBLER AT STA 1400 LONG 30L. FABRICATED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 53-2-1 FIG 7, INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 51-1-20D AND SRM 51-1-21.

Part: PAN — CRACKED (CARGO DOOR) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 A-PIT DOOR FWD LOWER STOP ON DOOR AND DOOR PAN UNDER FITTING ARE CRACKED AT STA 320 AT LONG 32R. REMOVED AND REPLACED STOP FITTING, REMOVED, FABRICATED AND REPLACED LOWER PAN SECTION IAW SRM 52-4-2 AND 52-2-0 FIG 2.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 A-PIT CARGO DOOR FWD AND AFT ANGLES UNDER SEAL AREA AT STA 280 AND 340 ARE CRACKED ON DOOR. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5754260, AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 8.000, LONG 33L DOUBLER INSTALLED, CLASSIFIED CATEGORY D. REMOVED DOUBLER, STOP DRILLED CRACK NDT HFEC INSPECTED, CRACK TERMINATES AT STOP DRILL. CUT OUT DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER IAW SK 708-078, INSTALLED FILLER AND REPAIR DOUBLER IAW SAA SK708-078, AND EO DC8-53-20245.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 STA 8.0, LONG 33R DOUBLER, CLASSIFIED CATEGORY D. REMOVED DOUBLER, CUT OUT DAMAGED AREA NDT HFEC INSPECTED NO CRACKS NOTED. FABRICTAED FILLER AND DOUBLER IAW SAA SK 708-080. INSTALLED FILLER AND DOUBLER IAW EO DC8-5330-12800-C, AND SAA SK 708-080.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1460 LONG 30L EXTERNAL DOUBLER. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-2-1 FIG 7.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1772 LONG 17R AND END FITTING ARE CRACKED. REMOVED LONGERON 17R AND END FITTING, FABRICATED LONGERON SECTION AND REPLACED END FITTING, AND INSTALLED END FITTING AND LONGERON SECTION IAW DWG 4772397 AND 5649327, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 LONG 17L AND END FITTING CRACKED AT STA 1772. REMOVED LONG AND END FITTING, FABRICATED LONGERON SLICE AND DRILLED UP NEW END FITTING IAW DRAWING 5649327 AND SRM 51-1-24, INSTALLED REPAIR PARTS IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 C-BAG BIN, BATHTUB FITTING CRACKED AT STA 1200, LONG-28L. REMOVED BATH TUB FITTING, FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2D. INSTALLED REPAIR DOUBLER INSTALLED NEW FITTING IAW SRM 53-2-0 FIG2D, AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 LIGHT CORROSION BETWEEN LONG 35L AND 35R STA 260 EXTENDING UNDER SHEAR TIES. CORROSION OUT OF LIMITS ON SHEAR TIE AT STA 260, LONG 35L. REMOVED SHEAR TIE IAW SRM 51-1-20. FABRICATED SHEAR TIE IAW SRM 53-4-1, INSTALLED SHEAR TIE IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1230 LONG 33R INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 AFT SIDE STA 1240 FRAME INTERCOSTAL TO FRAME FITTING IS CRACKED AT LONG 33R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LONG 34L IS CRACKED AND CORRODED BEYOND LIMITS STA 1746 LONG 34L. REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CORRODED AND CRACKED STA 1690 TO 1766 AT LONG 28R. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5644130, AND SRM 51-1-21, 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1240 AFT INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1230 LONG 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1745 BETWEEN LONG 35R AND 35L FWD BACKUP FITTING FOR TAILSKID SHOCK ABSORBER IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750865, AND SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C2 STA 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 32R-33R INSIDE TORQUE BOX. REMOVED AND REPLACED FITTING IAW DWG 3755840, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1140 LONG 35R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758496, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1746 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5649329, AND SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 C BAG BIN, BATH TUB FITTING CRACKED AT STA 1160 LONG 34R, INSIDE TORQUE BOX. REMOVED CRACKED BATH TUB FITTING IAW 53-2-0. FABRICATED REPAIR ANGLES AND FABRICATED REPAIR PARTS IAW SRM 53-2-0 FIG 2D, INSTALLED REPAIR ANGLES AND BATH TUB FITTING AT STA 1160 LONG 34R IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CRACKED AND CORRODED STA 1690 TO 1766 AT LONG 28L. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5644130, AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING CRACKED LONG 28L. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26R TO 27R. TRIMMED SHEAR TIE IAW SRM 53-2-0 FIG 2A, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-2-0 FIG 2A, AND 53-4-1 FIG 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 FRAME AT STA -12 IN LT NOSE TUNNEL IS GOUGED AND CRACKED AT LBL 24 AFT SIDE. REMOVED FRAME, FABRICATED AND INSTALLED FRAME IAW DWG 5613861, AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26L TO 27L. REMOVED SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW SRM 52-2-0 FIG 2A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 683 FWD SIDE LOWER BULKHEAD FRAME IS CRACKED BETWEEN LONG 28R TO 29R. REMOVED, FABRICATED AND REPLACED FRAME SECTION IAW DWG 9753751, AND SRM 51-1-20D, 53-2-5, 51-3-0.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 C-PIT DOOR SKIN IS CRACKED AND GOUGED NEAR LOWER FWD CORNER APPROX STA 1180 AT LONG 32R. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-2-0 FIG 4, 52-4-1.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT CENTER SERVICE DOOR BEAM SEGMENT ON DOOR IS CRACKED AT APPROX STA 1295 AT LONG 16L, 3RD LIGHTENING HOLE FROM TOP. CUT INTERCOSTAL/BEAM, FABRICATED AND INSTALLED BEAM SECTION IAW SRM 52-2-0 FIG 2, 52-40-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 KEEL BEAM FITTING 2ND FROM FRONT IS CRACKED BETWEEN WHEEL WELLS STA 902 APPROX LBL4 TO RBL 4. REMOVED AND REPLACED FITTING IAW DWG 4775262-1, AND SRM 51-1-20D, 51-3-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1660 LONG 24L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-4-1 FIG 43, AND 53-2-2 FIG 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 RT T-1 DOOR AFT LOWER CORNER HAS A DOUBLER AT STA 440.000. REMOVED DOUBLER, NDT HFEC NO CRACK NOTED AROUND CUTOUT. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW EO DC8-5330-17436-A AND SK-708-650. INSTALLED DOUBLER, TRIPLER, AND FILLER AT RT STA 440.0 IAW SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 822 LONG 22L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D.

Part: SKIN — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LT WING L/E LOWER SKIN IS CRACKED AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087 APPROX C.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 960-980 AT RBL 63. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5646674, AND SRM 51-1-21.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 850 LONG 7R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 1220 LONG 19R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4750418, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 857 LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 850 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 850 LONG 9R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C-1 LONG 10R END FITTING CRACKED AT STA 675. REMOVED CRACKED END FITTING AT LONG 10R, STA 675 IAW SRM 51-1-20 REPLACED IAW SRM 51-1-21 AND 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 700 LONG 18R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 857 LONG 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 4750422, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 781 FWD SIDE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 850 LONG 10R FWD SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND UPS ENGINEERING FILE NUMBER DC8-53-20246, SAA SK 708-514, SRM 51-1-20D, 51-3-0, 53-2-1 FIG 7.

Part: SKIN — CRACKED (RT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 AFT LOWER FUSELAGE SKIN IS CRACKED AT STA 1800 LONG 33. REMOVED AND REPLACED SKIN BETWEEN STA 1690 TO 1890 LONG 28L TO 28R IAW DWG 5649329, SRM 51-1-21, 51-1-20D, 53-1-0.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD ATTACH FITTING LONG 24R. CUT OUT DAMAGED FRAME IAW SRM 53-2-0 FIG 2. FABRICATED FRAME AND ANGLE REPAIR IAW SRM 53-2-0 FIG2, INSTALLED FRAME ANGLE DOUBLER IAW SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD BRACKET LONG 24L. CUT OUT DAMAGED AREA, REMOVED CRACKED SHEAR TIE AT STA 55 LONG 24L. FABRICATED AND INSTALLED FRAME REPAIR SECTION AND SHEAR TIE IAW SRM 53-2-0, SRM 53-2-0 FIG 2, AND SRM 53-3-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LWR AFT CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG18 AT STA 1660 LONG 21L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACK AT CUT OUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18 AT LONG 21L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC8-5330-17427-A, SRM 53-2-0 FIG 18, AND SAA SK 708-146.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 EXTERIOR SKIN BULGING STA 190 BETWEEN LONG 35L TO 35R, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5779925 AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 REMOVED DOUBLER ON R1 DOOR FWD UPPER CORNER AND REPAIR PER SRM 53-2-0 FIG 14 AT STA 160 LONG 10R. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

INSPECTION TYPE:N/A REPEAT ITEM (2) - DURING FLIGHT AMBER MX LIGHT ILLUMINATED. TECH RECOMENDS: REVIEW MX HISTORY. DURING SMOKE DETECTOR TEST MX INDICATES ON TWO OCCASIONS THAT SDU FB7739 IS FAULTED. REPLACED BATTERIES, NO HELP. REMOVE AND REPLACE SAID SDU. REPLACED LWR SMOKE DETECTOR FB 7739 PER MM 26-18-00. OPS CHECK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,399 hrs · 47,562 cycles

INSPECTION TYPE:C1 STA 908 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND SRM 51-1-20D, 51-1-21, 51-3-0.

Part: LIFE RAFT — MISSING (CABIN)

INSPECTION TYPE:IN A/C NEEDS TWO SIX MAN LIFE RAFTS FOR OVERWATER FLIGHT. INSTALLED TWO SIX MAN LIFE RAFTS PART 600-107RU SER D112M & F41M.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:DURING PREFLIGHT, CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE . APPX 6 IN. FWD OF OVERPRESS SAFETY VALVE. CRACK LENGTH IS .750 IN. THE UPPER DIRECTION & .500 IN. THE LOWER DIRECTION. REMOVED DAMAGED SKIN AT STA 1480, FABRCATED, DRILLED & FINISHED REPAIR. DFRL D206716 CLEARED ON LP 462587.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE APPROX 6 FT FWD OF OVERPRESS SAFETY VALVE CRACK LENGTH IS 3/4 INCH IN THE UPPER DIRECTION AND 1/2 INCH IN THE LOWER DIRECTION ALL.FERRY. FLIGHT.PROCEDURES.HAVE.BEEN.ACCOMPLISHED.AND.ACFT. IS.IN.SAFE.OPERATING.CONDITION.FOR.FERRY.FLIGHT..UPS AUTHORIZATION.J.WRIGHT.-.MGR.AMC

Part: ANGLE — CRACKED (CARGO BAY) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, C3 PIT CROSS SLIDE DOOR LWR SUPPORT ANGLE CRACKED. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW DC8 SRM 51-1-24, INSTALLED NEW SUPPORT ANGLE IAW DC8 SRM 51-3-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, AFT ACCESSORY COMPARTMENT FS 1600 AT L34L LONGERON EXFOLIATED UNDER FRAME. REMOVED DAMAGE SECTION OF LONGERON, LONGERON SPLICE AND LONGERON END FITTING IAW DC8 SRM 51-3-2. LOCATE NEW SECTION OF LONGERON, DRILL EXISTING HOLES, ALODINE AND PRIME IAW 51-1-24 & 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, LWR SKIN BETWEEN STA 360 TO 380 ANT MOUNTING PLATE CORRODED. FABBED MOUNTING PLATE IAW DAC DWG 3778019 AND SRM 51-1-21, OK TO ALODINE AND PRIME.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, REMOVE EXISTING DOUBLER FROM FWD SIDE OF LT AFT PRESSURE BULKHEAD AND INSTALL DOUBLERS IAW DAC DWG SR08530007. REPAIRED AREA BY INSTALLATION OF REPAIR DOUBLERS IAW DAC DWG SR08530 07 AND REO G07477.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, AFT PIT FS 1100 CORROSION UNDER NUT PLATE ON UPPER FRAME FLANGE LOWER SURFACE BETWEEN L36 AND L35L. REMOVED CORROSION MATERIAL, FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW UPS EO DC8 5310-11728B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, FWD PIT FS 180 LONG 36 SKIN HAS CRACK AT FASTENER HOLE. REMOVED CIRCULAR SECTION OF DAMAGED PLATING IAW DC8 SRM 53-2-1, FABBED EXTERNAL DOUBLER, FILLER, AND INTERNAL DOUBLERS IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED EXTERNAL DOUBLER, FILLER & INTERNAL DOUBLER IAW DC8 SRM 53-2-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, INTERCOSTAL CRACKED ON AFT SIDE OF LT AFT ENTRY DOOR JAMB AT L9L. REMOVED INTERCOSTAL, FAB NEW INTERCOSTAL FROM 7075-T6 .050 IAW DAC DWG 9251058, ALODINED AND PRIMED IAW 51-1-8, INSTALLED IAW 51-1-21, 51-3-0, 51-1-20D.

Part: FITTING — CRACKED (CENTER WING) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, WING CENTER SECTION LONGERON 34R AFT ATTACH FITTING HAS 4 INCH LONG CRACK AT STA 776.0. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-3-2.

Part: SKIN — CRACKED (LT WING LE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, LT WING CENTER L/E UPPER EXTERIOR SKIN IS CRACKED JUST I/B OF SLOT PANEL. FABBED DOUBLER IAW UPS EO DC8-5720-7767, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-20D & 51-1-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, AFT PIT STA 1080 L35R INTERCOSTAL EXFOLIATED. REMOVED CORRODED INTERCOSTAL, FAB INTERCOSTAL IAW DAC DWG 9758507, ALODINE AND PRIME IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: STIFFENER — CORRODED (VERTICAL STAB) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, VERTICAL STAB TOP STA ZY284 T/E WEB STIFFENER L-ANGLE HAS CORROSION FWD SIDE OF WEB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. MAT ID PO 331530 S1646835 PER DC8 DRWG 5611400. FAB STIFFENER IAW DC8 DRWG 5611400. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: MOUNT — DAMAGED (LT WING) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, SEVERAL TANK MOUNTING BOLT HOLES ARE ELONGATED ALONG THE UPPER FWD MOST O/B END OF THE LEFT WING L/E TANK. MATL ID 2024-0 .090 PO NR 328799 IAW DC8 SRM 57-2-1. FABBED REPAIR DOUBLER IAW DC8-5720-7767 HEAT TREATED IAW TPS-1003 REV A DRILLED REPAIR DOUBLER IAW 51-1-24 COUNTERSUNK IAW DC8 SRM 51-1-22. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW 51-1-20D & 51-1-21. LEAK CK NOT REQUIRED ON 71 SERIES A/C TANK IS DEACTIVATED.

Part: FLOORBEAM — CRACKED (CARGO BAY) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, FWD LWR CARGO PIT AT FS 340, FLOORBEAM AT RBL 40 IS CRACKED. REPAIRED PER TIMCO REO G07463, ALODINED AND PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-3-0, TIMCO REO-G07463.

Part: RIB — CRACKED (LT WING) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. LT WING CENTER L/E UPPER RIB CRACKED AT STA XFS 518 STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, SPLICE FITTING IS CRACKED. REMOVED CRACKED SPLICE FITTING. RECEIVED NEW FITTING. LOCATED, DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-1-24B. INSTALLED FITTING IAW DC8 SRM 51-1-24.

Part: WEB — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, CORROSION ON MEMBRANE AND CUSP UNDER SIDE RT STA 37 SPLICED IN NEW SECTION OF CUSP IAW REO-G07444.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, LONG AND SPLICE FITTING ARE CORRODED. REMOVED A OLD FITTING. RECEIVED NEW FITTING IAW P/N 379919-501U. LOCATED, DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, LWR FUSELAGE SKIN AT STA 120 ANTENNA MOUNTING AREA HAS CRACKED HOLE. FABBED REPAIR IAW DC8 SRM 53-2-1 FIG 7, ALODINED AND PRIMED REPAIR PER DC8 SRM 51-1-8, INSTALLED REPAIR PER DC8 SRM 51-1-21 AND DC8 SRM 51-1- 20D.

Part: ATTACH ANGLE — CORRODED (CARGO BAY) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, FWD LWR CARGO PIT AT FS 300 - 320 LONG 35 FITTING ATTACH ANGLE CORRODED IN DOORWAY. REMOVED ZEE FITTING AT FS 320 LONGERON SECTION FS 310 - 330 L35R IAW DC8 SRM 51-1-24, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED ZEE ANGLE REPAIR, LONGERON, AND SPLICES IAW DC8 SRM 53-2-0 FIG 20 & 53- 2-2. ALODINED AND PRIMED IAW 51-1-8, INSTALLED IAW 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. LONGERON IS CORRODED UNDER SPLICE FITTING. REMOVED SPLICE FITTING TO ACCESS TO CORROSION. FOUND TO BE OUT OF LIMITS IAW DC8 53-2-0. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-2. FABRICATED NEW SECTION & INSTALLED NEW SECTION & SPLICES.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D, 51-1-24.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. FWD LWR CARGO PIT AT BS 180 - 200, LONGERON 36 IS CORRODED ON BOTH SIDES. REMOVED CORROSION IAW DC8 SRM 51-1-8 WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. FLCP AT FS 260 FRAME HAS CORROSION & BAREMETAL FROM LONGERON 35LT - 33 RT. REMOVED CORROSION IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (A/C BAY) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE:C123, AIR COND COMPT RT SIDE L31 FITTING TO FS 70 CRACKED. REMOVED CRACKED FITTING RT L31 FS 70 IAW DC8 SRM 51-1-20D, LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. RT AFT SERVICE DOOR, AFT DOOR FRAME WEB CRACKED AT LIGHTNING HOLE FOR DOOR WARNING SWITCH. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.

Part: RIB — CRACKED (LT WING) · airframe 70,116 hrs · 46,622 cycles

INSPECTION TYPE: C123. LT WING, CENTER L/E UPPER RIB CRACKED AT STA XFS 404 . STOP DRILLED CRACK IAW DC8 SRM 57-3-3. FAB REPAIR ANGLE FROM MAT .0 71 EXT. 7075 T6 PO NR 316089 IAW DC8 SRM 57-3-3. ALODINED, PRIMED & I NSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-21, & 57-3-3.

Part: #4 PYLON — LEAKING (R/W #4 PYLONG)

INSPECTION TYPE:SV FUEL LEAKING AT NR 4 PYLON AREA FROM FWD SPAR TO REAR SPAR, LOWER SURFACE OF WING. REMOVED I/B AND O/B SKATE ANGLES, T-DOUBLERS, L/E SKIN PANEL, INTERNAL FITTINGS LOCATED AT CANT BLKHDS STA 495 AND 508. INJECTED FRONT SPAR, CTR SPAR AND STRINGERS IAW DC8 51-1-12. REINSTALL I/B AND O/B SKATE ANGLES AND DRAG ANGLES AND LEADING EDGE SKIN DOUBLER AND T DOUBLER IAW DC 8 SRM 51-1-20D AND REO 06862 REV A.

Part: STRAP — BROKEN (CABIN)

INSPECTION TYPE:N/A, RT ESCAPE TAPE RESTRAINING STRAP BROKEN. REMOVED AND REPLACED STRAP.

Part: LIGHT — INOPERATIVE (PASSENGER DOOR)

INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERG EXIT LIGHT HAS ONE BULB INOP. REMOVED AND REPLACED ASSY PER DC8 MM 33-50-02P201, OPS CK GOOD.

Part: FAIRING — CRACKED (LT TE FLAP)

10 INCH CRACK; LEFT INBOARD FLAP SURFBOARD FAIRING D/D 174412. REMOVED AND FABRICATED PLATING AND INSTALLED PLATING PER SRM 57-7-1 PAGE 2. THIS CLEARS DEFFERAL 174412.

Part: CONTROL CABLE — OUT OF ADJ (LANDING GEAR)

INSPECTION TYPE-N/A, ON TAKEOFF GEAR HANDLE REMAINED JAMMED WITH GEAR DOWN. PERFORMED GEAR HANDLE JAMMED CHECKLIST PER ADM. CONTINUED FLIGHT TO SDF WITH GEAR DOWN. ADJUSTED ANTI-RETRACTION LATCH CABLE PER MM 33-31-00, OPS CHECK GOOD.

Part: SKIN — CORRODED (WS 76.25)

INSPECTION TYPE-C, RT WING L/E LOWER SKIN AT WS XFS 76.25 HAS CORROSION BLEND OUT OF LIMITS. REPAIRED IAW DHC SK 708-746.

Part: SKIN — CRACKED (WS 336)

INSPECTION TYPE:C, RT WING L/E LWR SKIN AT STA XFS336.0 IS CRACKED AT THE DRAIN HOLE. REPAIRED AREA IAW DC8-5720-4087-B AND SRM 57-3-3 FIG 5.

Part: DOUBLER — CORRODED (BS 25-55)

INSPECTION TYPE-C, SKIN DOUBLER HAS HEAVY CORROSION BEYOND LIMITS AT FS 25 TO 55 L-30R. REPAIRED IAW DHC SK 708-708.

Part: FITTING — CORRODED (BS 100)

INSPECTION TYPE:C, STA 100, LONG 36 END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4647657 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1270)

INSPECTION TYPE-C, LONGERON 35R AT FS 1270 IS CRACKED. REPAIRED IAW DHC SK 708-689.

Part: LONGERON — CRACKED (BS 1270)

INSPECTION TYPE-C, LONGERON 36 AT FS 1270 HAS 8 INCH CRACK. REPAIRED IAW DHC SK 708-690.

Part: LONGERON — CRACKED (BS 220)

INSPECTION TYPE-C, LONGERON 35L AT FS 220 IS CRACKED. REPAIRED IAW SRM 53-2-2.

Part: SHEAR TIE — CRACKED (BS 1200)

INSPECTION TYPE-C, SHEAR TIE FITTING BETWEEN L 32L TO 33L FS 1200 CRACKED. REMOVED AND REPLACED IAW SRM 53-2-0.

Part: FITTING — CORRODED (BS 1560)

INSPECTION TYPE-C, RT UPPER CUSP TO FRAME FITTING HAS MODERATE CORROSION ON FWD SURFACE AT FS 1560. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE-C, TORQUE BOX FS 1220 L-33R FITTING CORRODED. REMOVED, FABRICATED AND REPLACED FITTING IAW DHC SK 708-559.

Part: SKIN — CORRODED (BS 1265)

INSPECTION TYPE-C, BELLY SKIN FS 1265 L 35L TO 35R HAS HEAVY CORROSION. REPAIRED IAW DHC SK-708-563.

Part: FITTING — CRACKED (BS 154 L)

INSPECTION TYPE-C, FS 154 RT SIDE THE FRAME TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1- 20D AND DWG 2649943.

Part: LONGERON — CORRODED (BS 35-55)

INSPECTION TYPE-C, LONG 30R CORRODED FS 35 TO 55. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 3648667.

Part: FITTING — CRACKED (BS 1324)

INSPECTION TYPE-C, FS 1324, RT SIDE, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: STRAP — CORRODED (VERT STAB)

INSPECTION TYPE-C, MODERATE CORROSION ON THE LT SIDE OF THE VERTICAL STAB TO EMP BASE STRIP. REPAIRED IAW SRM 53-2-5.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE:C, LT WING L/E AT STA XFS760.00, THE L/E RIB IS CRACKED AT THE AFT END, STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 803.75)

INSPECTION TYPE:C, LT WING L/E AT STA XFS803.750, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 572.5)

INSPECTION TYPE-C ,LT WING LE RIB UPPER ARM CRACKED BY AFT FASTENER AT WS XFS 572.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 703.75)

INSPECTION TYPE:C, LT WING L/E AT STA XFS703.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE:C, LT WING L/E AT STA XFS810.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: JAMB — CRACKED (SERVICE DOORWAY)

INSPECTION TYPE-C, RT AFT SERVICE DOOR HAS TWO CRACKS IN AFT UPPER DOOR JAMB CORNER, ON THE INNER DOUBLER 2.5 EMANATING FROM EDGE. REPAIRED IAW SRM 52-2-0.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE:C, LT WING L/E AT STA XFS797.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT AILERON)

RT I/B AILERON INTERNAL DOUBLER IS CRACKED AT ACCESS PNL NR 541. REPAIRED IAW DHC SK 708-207.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE-C, LT WING UPPER SURFACE WS XRS 74 STR 15 SKIN IS CRACKED. REPAIRED IAW SRM 57-2-1.

Part: RIB — CRACKED (LT TE FLAP)

INSPECTION TYPE:C LT WING T/E AT FLAP STA 3.00, THE T/E RIB IS CRACKED BEHIND NR 1 SPOILER I/B HINGE. STOP DRILLED CRACK AND REPAIRED IAW SRM57-2-0 FIG 2.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE:C, RT WING L/E UPPER RIB AT STA XFS304.00 IS CRACKED AT THE FWD END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: TRIPLER — CRACKED (WS 6.225)

INSPECTION TYPE:C, RT WING L/E LWR SKIN, THE INTERNAL TRIPLER AT THE I/B END OF THE O/ B SLOT IS CRACKED AT STA XOLDI 6.225. REMOVED, FABRICATED AND REPLACED TRIPLER IAW DWG 5769891 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (WS 347-385)

INSPECTION TYPE-C, RT WING L/E LWR SKIN INTERNAL DOUBLER WS XFS347.75 TO 354.0 AND 379.0 TO 385.25 HAS HEAVY EXFOLIATION CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG NR 5641253 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE-C, RT WING L/E LWR RIB AT WS XOLDI 6.225 IS CRACKED AT THE FWD END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769891.

Part: SKIN — CRACKED (WS 598)

INSPECTION TYPE-C, RT WING L/E LWR SKIN AT WS XFS 598 IS CRACKED. REPAIRED IAW DC8-5720-4087-B.

Part: TRACK — CORRODED (BS 1400-1540)

INSPECTION TYPE:C, CARGO TRACK AT STA 1400-1540 ABOVE STR 33R HAS CORROSION AND CRACK. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5750726 AND SRM 51-3-1.

Part: CLAMP — BROKEN (NR 2 ENGINE)

NR 2 ENGINE FIRE WARNING CAME ON, THROTTLE BACK WARNING WENT OUT. FOUND NR 2 ENG HIGH STAGE VALVE CLAMP FAILED. NR 2 ENGINE INBD THRUST REVERSER DAMAGED. REMOVED AND REPLACED NR 2 ENG INBD THRUST REVERSER IAW MM 78-30-00 PN ON CFM56BRO2BRH.

Part: EXTRUSION — CRACKED (RT WING)

INSPECTION C-CHECK, RT WING LE OUTBOARD, OUTBOARD SIDE UNDER SLOTED DOOR EXTRUSION, CRACKED. FABRICATED REPAIR DOUBLER SHIM. REPLACEMENT ANGLE IAW REO 02750. ALODINED AND PRIMED IAW DC8 SRM 51-1-8D. INSTALLED REPAIR DOUBLER AND SHIM IAW REO 02750 AND INSTALLED REPLACEMENT ANGLE IAW REO 02750.

Part: FITTING — CRACKED (WS 410)

INSPECTION C-CHECK, FLAP ATTACHED BOLTS AT STA 410.01 MAIN LEFT WING INBOARD AND OUTBOARD LEAKING. REMOVED FLAPS HINGE FITTING AND STRUCTURE TO ACCESS REPAIR AREA, CRACKED INNER AND OUTER VERTICAL STIFFENERS. REMOVED CRACKED LOWER BULKHEAD CAP FITTING, REAMED OUTBOARD FLAP ATTACH HOLE TO .798 THROUGH SPAR WEB AND LOWER SPAR TO REMOVE CRACKED REAMED INBOARD FLAPS ATTACHED HOLE TO .747 THROUGH SPAR WEB AND LOWER SPAR TO REMOVE CRACKS IAW REO 02733.

Part: FITTING — CRACKED (BS 1160)

INSPECTION C-CHECK, AFT PIT X SLIDE DOOR FWD TORQUE BOX HAS CRACKED Z FITTING, STA 1160 BETWEEN LONG 35R AND L34R. REMOVED Z FITTING, FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED Z FITTING AND REPAIRED ANGLES IAW DC8 SRM D53-2-0 AND DC8 SRM 51-1-21.

Part: LONGERON — CORRODED (BS 1150-1160)

INSPECTION C-CHECK, LONG 29L CORRODED AT AFT PIT SLIDE DOOR FWD TORQUE BOX, STA 1150-1160. REMOVED DAMAGED LONG SECTION IAW DC8 SRM S53-2-2D. CUT EXTERNAL SKIN TO ACCESS LONGERON IAW DC8 SRM D53-2-1 FIG 7. FABRICATED NEW SKIN DOUBLER AND FILLER PER DC8 SRM D53-2-1D FIG 7. FABRICATED SPLICES AND LONG SECTION PER DC8 SRM D53-2-2D. ALOINDED AND PRIMED ALL PARTS IAW DC8 SRM D51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-20D AND 51.

Part: FITTING — CRACKED (BS 1220)

INSPECTION C-CHECK, AFT LOWER FS 1220 Z FITTING CRACKED APPROX 2.75 AT LONGERON 34R. REMOVED CRACKED Z FITTING, FABRICATED NEW Z FITTING AND SPLICED PIECES IAW DC8 SRM 53-2 FIG 2G. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION C-CHECK, AFT LOWER CARGO, FS 1220, Z FITTING ON TORQUE BOX CRACKED APPROX 2.375 INCHES, BETWEEN LONG 32R AND 34R. REMOVED LONG SECTION ON LONG 32R AT FS 1220 TO ACCESS FITTING. ALODINED AND PRIMED ENDS OF CUT LONG IAW DC8 SRM 51-1-8. DRILLED AND INSTALLED FITTING IAW DC8 SRM D51-1-24 AND 51-1-20D AND REO 02711. INSTALLED LONG SECTION 32R IAW REO 02711.

Part: FRAME — CORRODED (BS 1600)

INSPECTION TYPE-C/CK, STA 1600 FRAME CORRODED AND SPLICE FITTING CORRODED BETWEEN LONG 33L AND 33R. REMOVED FASTENERS, CORROSION, DAMAGED FRAME SECTION, FABRICATED NEW FRAME SECTION AND SPLICES, ALODINED AND PRIMED PARTS, INSTALLED NEW FRAME SECTION AND SPLICES ALL IAW DC8 SRM D51 1 20D 51-1-8D AND 53-2-0 AND 53-4-1D AND 51-1-1.

Part: SKIN — CRACKED (BS 1700)

INSPECTION C-CHECK, AFT FUSELAGE SKIN CRACKED APPROX 3 INCHES LONG, STA 1700 L17R. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 FIG 7. ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED AND SEALED REPAIR PARTS IAW DC8 SRM D51-1-21, 5-1-1-20D.

Part: SKIN — CRACKED (BS 1734)

INSPECTION C-CHECK, AFT 6 FUSELAGE SKIN CRACKED APPROX 1.5 INCHES LONG, STA 1734, L17L. FABRICATED FILLER PLATE, SKIN DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1D. ALODINED AND PRIMED PART AND SKIN IAW DC8 SRM 51-1-8. INSTALLED REPAIRED PARTS IAW DC8 SRM 53-2-1.

Part: CATALYTIC CONV — CLOGGED (LT/RT PACK)

INSPECTION TYPE-N/A, STRONG FUMES EYE BURNING/SMELL IN COCKPIT WHEN LEFT OR RIGHT PACK TURNED ON. TURNED BOTH PACKS OFF ONE AT A TIME AND RETURNED TO RFD. THE SMELL WAS VERY STRONG. UPON AIR TURNBACK, FOUND BOTH OZONE CATALYTIC CONVERTERS TO BE CLOGGED. DEFERRED BOTH THE LEFT AND RIGHT CATALYTIC CONVERTERS PER MMOC FOR A FERRY FLIGHT TO GSO. SEE LOG PAGE 803461 ITEM 3, CONTROL NR D122984 ASSIGNED. ALL REQUIREMENTS FOR FERRY PERMIT NR 9001 HAVE BEEN ACCOMPLISHED.

Part: COALESCER BAG — CONTAMINATED (LT/ RT PACKS)

INSPECTION TYPE-N/A, BOTH LEFT AND RIGHT PACK PRODUCING DIESEL SMELL AND CAUSING EYE BURNING AND HEADACHE. SECURED RT PACK TO CONTINUE FLIGHT. SMELL VERY BAD WITH ANTI-ICE ON, SMELLS LIKE EXHAUST GAS. SUSPECT GROUND EQUIPMENT CONTAMINATION, FOUND WATER SEPARATOR BAGS CONTAMINATED. REMOVED AND REPLACED LEFT AND RIGHT SEPARATOR BAGS PER M/M 21-20, RAN ENGINES AND OPS CHECKED GOOD WITH NO ODORS DETECTED.

Part: HOSE ASSY — LEAKING (LT MLG)

LEFT MLG BOGIE TRIM EXTEND HOSE REPLACED, LINE SECURED. THE FLEX LINE IS LONGER AND NEEDS REPLACING.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND IN BWI, MAINTENANCE FOUND EMER LIGHTS DEAD. REMOVED AND REPLACED EMER BATTERY PACK, OPS CK NORMAL.

Part: SKIN — DAMAGED (RUDDER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RUDDER SKIN RT SIDE STA 2283 DAMAGED. REPAIRED IAW SRM 55-2-0, 51-1-21A.

Part: FLANGE — CRACKED (BS 258)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO HORIZ FLANGE CRACKED AT STA 258, LONG 35L. REPAIRED IAW SRM 53-2-2.

Part: DOUBLER — DAMAGED (BS 1406-1324)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND INNER DOUBLER FROM PREVIOUS REPAIR AT STA 1306 TO 1324 BETWEEN LONGS 24L TO 25L DAMAGED. REPAIRED IAW SRM 51-1-8.

Part: RIB — CRACKED (WS 416.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING RIB CHAFED AT STA SFX 416.5. REPAIRED IAW SRM 51-2-0, 57-2-0.

Part: FITTING — CORRODED (BS 1350)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 26L AT FS 1350. REPAIRED IAW SRM 51-1-20D, 53-4-1, 53-1-0.

Part: LONGERON — CRACKED (BS 193)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO LT LOWER FLANGE OF LONGERON 35R AT STA 193. REPAIRED IAW SRM 53-2-2.

Part: INTERCOSTAL — CRACKED (BS 80)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON BOTTOM END OF COCKPIT SUB FLOOR AT STA 80 LBL 56, VERTICAL INTERCOSTAL. REPAIRED IAW SRM 53-3-1, 51-1-20D.

Part: FITTING — CORRODED (BS 1010)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CARGO COMPARTMENT NR 3 PIT, RT STA 1010 SUP EXTRUSION LONGERON 21. REPAIRED IAW SRM 55-2-5, 51-1-20D, 53-2-0.

Part: SKIN — CORRODED (BS 400)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SKIN IN FWD LOWER CARGO STA 400 BETWEEN LONGS 36 AND 35L. REPAIRED IAW SRM 53-2-1.

Part: SKIN — CORRODED (BS 218-222)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO INNER SKIN/DOUBLER CORRODED STA 218 TO 222, LONGS 36 AND 35L. REPAIRED IAW SRM 51-2-2, 53-2-0.

Part: SPLICE FITTING — CORRODED (BS 1350)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 25L SPLICE FITTING AT STA 1350 CORRODED. REPAIRED IAW SRM 53-4-1, 51-1-20D.

Part: DOUBLER — CORRODED (BS 1399)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON AFT LOWER CARGO SKIN UNDER FINGER DOUBLER AT STA 1399 BETWEEN LONGS 30L TO 31L. REPAIRED IAW SRM 53-3-1, 51-1-8, 51-1-20, 51-1-11.

Part: FITTING — CRACKED (BS 822)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON TIE FITTING HAS LARGE CRACK AT STA 822, LONG 21R. REPAIRED IAW SRM 51-1-20.

Part: ANGLE — CRACKED (LT MLG WW)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK AROUND RADIUS OF ANGLE LT W/W O/B AFT FORWARD OF FLAP. REPAIRED IAW SRM 53-2-0, 51-1-21, 51-1-20D.

Part: FRAME — CRACKED (BS 1879-1890)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKS ON FRAMES INSIDE ACCESS DOOR NR 62 STA 1870 TO 1890. REPAIRED IAW SRM 53-2-0, 53-2-5.

Part: INTERCOSTAL — CORRODED (BS 1000-1020)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND INTERCOSTAL BELOW WINDOW PLUG LT SIDE STA 1000 TO 1020 CORRODED. REPAIRED IAW SRM 53-4-1, 51-1-21.

Part: SPAR — CORRODED (LT WING)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT WING LOWER AFT SPAR CAP. REPAIRED IAW SRM 57-10-0, 51-1-20D.

Part: LE RIB — CRACKED (WS 677)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER L/E RIB CRACKED AT STA XFS 677.0. REPAIRED IAW M/M 57-00-00.

Part: LE RIB — CRACKED (WS 316.5)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 316.5 CRACKED. REPAIRED IAW SRM 57-00-00.

Part: LE RIB — CRACKED (WS 803.75)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 803.75 CRACKED. REPAIRED IAW SRM 57-00-00, 51-1-21.

Part: LE RIB — CRACKED (WS 747.5)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 747.50 CRACKED. REPAIRED IAW SRM 57-00-00, 51-1-21.

Part: LE RIB — CRACKED (WS 607)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 607.0. REPAIRED IAW M/M 57-00-00.

Part: SKIN — DAMAGED (LT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND LT I/B AILERON, O/B END TOP SKIN DAMAGED. REPAIRED IAW SRM 51-1-21, 51-1-8.

Part: INTERCOSTAL — CRACKED (WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND RT L/E O/B OF AUX TANK, UPPER INTERCOSTAL ANGLE CRACKED. INSTALLED FABRICATED PARTS IAW SRM 51-1-21, 51-1-30.

Part: LE RIB — CRACKED (WS 778.25)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 778.25 CRACKED. REPAIRED IAW SRM 51-1-21.

Part: LE RIB — CRACKED (WS 847.5)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 847.50 CRACKED. REPAIRED IAW SRM 51-01-8, 51-1-21.

Part: LE RIB — CRACKED (WS 795.5)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER RIB AT STA. XFS 795.5 CRACKED. REPAIRED IAW SRM 51-1-20, 51-1-21.

Part: LE RIB — CRACKED (WS 593)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 593.0. REPAIRED IAW M/M 57-00-00.

Part: INTERCOSTAL — CRACKED (FS 88)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON VERTICAL INTERCOSTAL AT BOTTOM END OF COCKPIT SUB FLOOR AT STA. 80, RBL 56. REPAIRED IAW SRM 51-1-20, 51-3-1.

Part: TE SKIN — CRACKED (RT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND LT O/B AILERON T/E HAS SMALL CRACK EXTENDING TO FASTENER HOLE. REPAIRED IAW SRM 57-8-1, 51-1-21.

Part: LE RIB — CRACKED (WS 770)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 770.0. REPAIRED IAW M/M 57-00-00.

Part: TE SKIN — CRACKED (RT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND RT O/B AILERON T/E HAS CRACK. REPAIRED IAW SRM 57-8-1, 51-1-21.

Part: LE RIB — CRACKED (WS 784)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER RIB AT STA. XFS 784.00 CRACKED. REPAIRED IAW SRM 57-00-00, 51-01-8.

Part: LE RIB — CRACKED (WS 727)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 727.0. REPAIRED IAW M/M 57-00-00.

Part: LE RIB — CRACKED (WS 770)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 777.0. REPAIRED IAW M/M 57-00-00.

Part: LE RIB — CRACKED (WS 720)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 720.0. REPAIRED IAW M/M 57-00-00.

Part: LE RIB — CRACKED (WS 734)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 734.0. REPAIRED IAW M/M 57-00-00.

Part: RIB — CRACKED (WS 748)

WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 748.0. REPAIRED IAW M/M 57-00-00.

Part: SKIN — CRACKED (SERV DOOR CUTOUT)

WHILE IN B-CHECK, MAINTENANCE FOUND CRACKS ON LT AFT SERVICE DOOR, AFT UPPER CORNER OF FUSELAGE CUT OUT EXTENDING FROM TWO RIVETS. INSTALLED REPAIR PER UPS EO DC8-5330-4067A.

Part: PROX SWITCH — MALFUNCTION (RT MLG DOOR)

PILOT REPORTED DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH CHECK LIST AND CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED RT MLG DOOR PROX SWITCH WITH SERVICEABLE UNIT. PERFORMED OPS CHECK OK.