N702UP

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV WEB CRACK FWD CARGO DOOR JAMB AT STA 1400. REPAIRED 53-02-00 FIG 23.

Part: ELEVATOR — OUT OF BALANCE (RIGHT) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV RIGHT ELEVATOR REQUIRES WEIGHT AND BALANCE. ACCOMPLISHED IAW 27-30-01-4.

Part: STRUCTURE — UNKNOWN (LT WING) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV LT WING CENTER L/E LOWER OUTBOARD EDGE IS TRIMMED OUT AT ATTACHED FASTENER HOLES. REPAIR AS PER UPS EO DC8 5720 31291.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV STA 526.7 LT WING LOWER OUTBOARD EDGE IS TRIMMED OUT AT ATTACH FASTENER HOLES. REPAIR IAW UPS EO DC8 5720 31291.

Part: STRUCTURE — MISREPAIRED (LT WING) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV LEFT WING STA XRS 431 HAS A DOUBLER THAT IS WRONG THICKNESS. REPAIRED DOUBLER IAW 57-2-1 FIG 2Q.

Part: DOUBLER — DAMAGED (LT AILERON) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV LT AILERON STA 454 HAS A REPAIR DOUBLER WITH EDGE DAMAGE. REPAIRED AS PER UPS EO DC8 5710-31295A.

Part: STRUCTURE — UNKNOWN (LT WING) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV LEFT WING CENTER L/E HAS A STEEL DOUBLER INSTALLED. REPLACED DOUBLER UPS EO DC8 5710-31296-A.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV FLOOR WEB AT STA 620-640 LBL 45 HAS SMALL PUNCTURE. INSTALLED DOUBLER SRM 53-02-00.

Part: SKIN — MISREPAIRED (RT WING) · airframe 68,946 hrs · 26,297 cycles

INSPECTION TYPE:SV SURVEY SEQUENCE 702-W4-15, RT LEADING EDGE ACCESS PNL DOUBLER LOCATION 477.750 NOT IN COMPLIANCE WITH SRM (NO SRM REPAIR). VERIFIED DOUBLER MEETS SRM 57-02-00 FIG 2A & TR 57-84.

Part: SKIN — TORN (PAX DOOR) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV LT FORWARD DOOR MAIN ENTRY INTERIOR SKIN TORN IN FORWARD CORNER. REPAIRED 51-09-00-0 AND DRW 5615403

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV SURVEY SEQ NUMBER 702-S2-08 RT HORIZONTAL STAB UPPER SKIN DOUBLER REPAIR UNABLE TO VALIDATE PER SRM. REPAIRED AS PER UPS EO DC8 5510 31277A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT BS 850 L21R DOES NOT MEET SRM CRITERIA. REPAIRED UPS EO 5320-31273A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV DOUBLER DOES NOT MEET SRM REQUIREMENTS FS 184 L10R. REPAIRED AS PER UPS EO 5320 31298A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV SURVEY ESQ NUMBER 702-F1-61 DOES NOT MEET SRM REQUIREMENTS FS 1469. REPAIRED AS PER 53-02-01 FIG 7 AND TR 53-203 FIG 7 SHEET 24.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV SURVEY SEQUENCE NUMBER 702-F1-46 DOES NOT MEET SRM CRITERIA. REPAIRED IAW DC8 SRM 53-2-1 FIG 7.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION REPAIR AT BS 702-BS 688N L16R AND L17R REPAIR DOES INCORPORATE FASTENER ROW AFT OF REPAIR. REPAIR IS IAW 53-02-00 FIG 22A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT STA BS 8 L32R L33.5R HAS ONLY 2 ROWS OF RIVETS SRM CALLS FOR 3. REPAIRED AS IAW 53-2-1 FIG 7.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV DOUBLER AT STA 608 DOES NOT MEET SRM GUIDELINE. REPAIRED PER UPS EO DC8 5320 31276.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR DOUBLER AT STA 951 RT DOES NOT MEET SRM GUIDELINES. REPAIRED AS PER UPS EO DC8 5320 31274A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV FLUSH SKIN REPAIR AT STA FS 46.5 DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER EO DC8 5320 31350 A.

Part: SKIN — MISREPAIRED (BS 40) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV BS 40 FWD PASSENGER DOOR EXTERNAL SKIN REPAIR AROUND DOOR HANDLE DOES NOT MEET SRM CRITIA 702-F1-20. REPAIRED IAW 52-03000 FIG 1.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EXTERNAL SKIN DOUBLER FS 191.5 DOES NOT MEET SRM GUIDELINES. REPAIRED PER UPS EO DC8 5320 31294A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EXTERNAL SKIN AT STA FS 380 DOES NOT MEET SRM REQUIREMENTS. REPAIR PER UPS EO DC8 5330 31348A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EXTERNAL SKIN REPAIR AT BS 383 L11L DOES NOT MEET SRM REQUIREMENTS. REPAIRED AS PER UPS EO DC8 5100 30540.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV FUSELAGE SKIN REPAIR AT BS 55- BS61 L25R-L26R DOES NOT MEET SRM CRITERIA REF UPS EO REPAIR EVAL SURVEY SEQ 702-F1-11. REPAIRED DC SRM 53-203 AND SRM 53-2-0 FIG 7 SHT 5.

Part: STRUCTURE — MISREPAIRED (X312) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR DOUBLER AT STA X312.5 DOES NOT MEET SRM GUIDELINES. REMOVED AND REPLACED TIP AS PER SRM 51-01-21A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT BS 50-56 L28L -L29L DOES MATCH SRM 53-02-00 FIG 13. REPAIR TO 53-2-00 FIG 13.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT BS 99 TO 104 L31L-L33R HAS ONLY 2 ROWS OF FASTENERS. REPAIRED AS IAW 53-2-0 FIG 10.

Part: SKIN — MISREPAIRED (ELEVATOR) · airframe 68,946 hrs · 26,297 cycles

INSPECTION TYPE:SV SURVEY SEQ NO 702-S2-11 RT ELEV TIP EXT DOUBLER AT 312.500 FASTENER SPACING AND EDGE DISTANCE OUT OF LIMIT REF STEP 1, 2 APPEN-D. VERIFIED THE REPAIR IS IN THE INTENT AND GUIDELINES IAW DC8 SRM 51-1-21, TR 51-134 FIG 33.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT STA BS 35 TO 42 L28L L29L DOES NOT MATCH REPAIR IN SRM 53-2-00 FIG 13. REPAIRED TO SRM 53-02-00 FIG 13.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV REPAIR AT BS 50-55 L29L L30L DOES NOT MATCH SRM REPAIR 53-02-00 FIG 13. REPAIR PER 53-02-00 FIG 13.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 7021997113 NRC 750487 RIGHT CUSP MEMBRANE AT CARGO TRACK CRACKED FS 1430 TO FS 1580. REPAIRED IAW 53-2-0 FIG 25.

Part: WEB — CRACKED (FUSELAGE)

INSPECTION TYPE:SV EVALUATION AND DISPOITION OF REPAIR EFN 70219961004 ORIGINAL NON ROUTINE 445615 FLOOR WEB REPAIR CRACKED LEFT CORNER. REPAIRED 53-02-00 FIG 25.

Part: RIB — CRACKED · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION OF N/R288527 RIB CRACKED AT TOP AFT END AT XFS 185. REPAIRED 55-02-00 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:S/V EVALUATE REPAIR EFN 70219911007 ORIGINAL NRC 289089 HEAVY CORROSION ON FWD SIDE OF CANTED BELT FRAME STA 1723 L35 L35R. REPAIR FOUND TO BE VALID DWG 5772706.

Part: WEB — DAMAGED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70219961032 ORIGINAL N/R 445992 WEB NEEDS TO BE CUT AND REMOVED BETWEEN FS 1190 AND 1210. PREVIOUSLY REPAIRED SRM 53-02-00.

Part: RIB — MISREPAIRED (HORIZ STAB) · airframe 689,642 hrs · 6,297 cycles

INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 70219911047 ORIGINAL NR 288533 RIB CRACKED AT LOWER AFT END AT XFS 53. EVALUATED REPAIR FOUND ADDED FASTENERS TO BE INCORRECT, REPLACED FASTENERS TO CONFORM WITH DC8 SRM 55-02-00-0 PG 2 ITEM 6 USING HL326 HI-LOKS.

Part: RIB — MISREPAIRED (HORIZ STAB) · airframe 689,642 hrs · 6,297 cycles

INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 70219911048 ORIGINAL NR 288532 RIB CRACKED AT LOWER END AT XFS 47. EVALUATED REPAIR FOUND FASTENERS ADDED. FASTENERS TO BE INCORRECT REPLACED WITH HL 926 IAW DC8 SRM 55-02-00-0 FIG 2 ITEM 6.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION REPAIR EFN 70219971243 ORIGINAL NRC 750796 CUSP MEMBRANE CRACKED AT TRACK G FS 1470. PREVIOUSLY REPAIRED IAW 53-02-00 FIG 025.

Part: STIFFENER — CRACKED (RT WING) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70220061052 ORIGINAL NR 902713 CRACKED STIFFENER IN 2ND L/E LEADING EDGE ACCESS HOLE OUTBOARD OF NR 3 PYLON. REPAIRED BY 57-02-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70219971129 ORIGINAL 750504 CUSP MEMBRANE AT FS 1580 LATERAL LOCATION ID AS CARGO TRACK C. REPAIRED PREVIOUSLY SRM 53-02-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION REPAIR EFN 70220001109 ORIGINAL NRC 042313 CORROSION ON FLOOR BLANK FS 160 TO 180. INSPECTED PREVIOUSLY REPAIR AND REMOVED CORROSION 53-2-03 FIG 9.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70219901052 ORIGINAL NRC 158580 CORRODED PATCH ON C-CROSS DOOR AT FS 1182, L33R. SPLICE MEETS DOUGLAS DRAWING BSH4868.

Part: WEB — CRACKED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70219901008 ORIGINAL NRC 158466 LOWER FLOOR WEB CRACKED. REPAIRED IAW 53-2-0 FIG 25.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION REPAIR EFN 70219961018. REPAIRED 53-02-03 FIG 8A.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION OF REPAIR EFN 70220081026 N/R 123643 REPAIR DOUBLER IS GOUGED IN C PIT TORQUE BOX AT FS 1190 L33R. REPAIR PREVIOUSLY DC8 SRM 53-02-00 FIG 001B.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70220081043 ORIGINAL NR 123529 DAMAGE COUNTERSINKS ON INBOARD AFT CORNER OF LEFT ELEVATOR. REPAIR IAW 55-02-00 FIG 002.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE REPAIR EFN 7021991074 ORIGINAL NRC 289037 LEFT AFT EMERGENCY DOOR CRACKED ON FRAME FLANGE RADIUS FORWARD CORNER. REPAIRED SRM 52-02-00 FIG 002.

Part: CUSP WEB — DAMAGED (FS 260) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 7021991231 NRC 751026 CUSP MEMBRANE TRACK 1 BETWEEN FS26 0 AND FS360. REPAIRED IAW 53-2-00 FIG 25.

Part: STRUCTURE — DAMAGED (WING) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 7022004 ORIGINAL NRC 750568. REPAIRED PER SRM 57-02-00.

Part: RIB — CRACKED (WING) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE AND DISPOSITION EFN 70219911059 ORIGINAL NRC 188671 RIB CRACKED AT OUTBOARD FORWARD CORNER OF ACCESS PANEL 522B. REPAIRED IAW 57-02-00 PG 1 FIG 002.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,964 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATION AND DISPOSITION REPAIR EFN 70219971240 ORIGINAL NR 750802 CUSP MEMBRANE AT TRACK I AND AT A FUSELAGE STATION NOT DEFINED ON THE NON-ROUTINE IT MAY BE A REPAIR LOCATED BETWEEN THE REPAIR AT FS 1050 AND 1250. INSTALLED DOUBLER IAW DC8 SRM 53-02-00 FIG 25.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV EVALUATE EFN 70219911038 SEAT TRACK FS 160. REPAIRED SRM 53-02-03 FIG 008A.

Part: RUB STRIP — CORRODED (FUSELAGE) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV LT FILLER LOWER RUB STRIPS CORRODED. REPAIRED IAW SRM 51-1-11.

Part: SUPPORT ANGLE — CRACKED (FILLET FAIRING) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV RT UPPER WING TO FUSELAGE FILLET FAIRING 292B SUPPORT ANGLE CRACKED. REPAIRED DWG 5769482 SRM 51-1-08.

Part: REPAIR — CRACKED (CARGO DOOR) · airframe 689,467 hrs · 26,297 cycles

INSPECTION TYPE:SV PERMANENT REPAIR TO PIT 32 DOOR INNER PAN CRACKED. REPAIRED 52-02-00.

Part: PANEL — FAILED (ELECTRICAL)

FL340 - LIGHTS FLICKERED AND NR 1, 3, 4 GEN UNPARALELLED LIGHTS CAME ON. VOLTS & FREQS OK ON 1-3-4. NR 2 VOLTS & FREQS AT 50 VOLTS & 385 CYS. CHECK LIST ACCOMPLISHED; GOT EVERYTHING BACK W/GEN PARALLELED. LATER SAME SENERIO, BUT NOTHING CAME BACK. LIGHT ELECTRIC BURN ODOR. NR 2 VRP/GCP C/B POPPED & BURNING SMELL COMING FROM IT. REPLACED NR 2 VOLTAGE REG & GEN CONTROL PANEL. R&R NR 2 BTB; R & R BUSS PROTECTION PANEL. GROUND RUN ALL ENGINES, PERFORMED ADJUSTMENT TEST PER MM 24-20-03-4, 24-20-00-2, 24-20-07-2.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY BATTERY ASSY PER MM 25-00-00. OPS CHECK GOOD.

Part: GAUGE — UNSERVICEABLE (ESCAPE SLIDE)

ESCAPE SLIDE TO BE REPACKED. PRESSURE GAUGE IS UNREADABLE. REPACKED ESCAPE SLIDE PER DC8 MM 25-60-01-2. OK FOR SERVICE.

Part: SLIDE — DISLODGED

GROUND PERSONNEL OPENED DOOR WITH GIRT BAR IN PLACE. SLIDE FELL OUT OF CONTAINER. REINSTALLED ESCAPE SLIDE PER MM 25-60-01-2.

Part: PANEL — DELAMINATED (RT WING) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 RIGHT WING O/B TRAILING EDGE PANEL UPPER FWD. SURFACE IS DELAMINATED. REPAIRED RIGHT WING O/B TRAILING PANEL SURFACE IAW DWG 5644654 AND SRM 51-1-9A.

Part: FRAME — CRACKED (BS 980 L36) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 POSSIBLE CRACK ON STA 980 FRAME IN C-PIT AT L36. REMOVED CRACKED L ANGLE AT STA 980, DRILLED UP NEW L ANGLE AND INSTALLED AT STA 980 AT L36.

Part: SKIN — CRACKED (LT WING) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 LOWER SKIN HAS CRACK RUNNING OFF RIVET NR 1 PYLON STUB WING. REPAIRED LT OUTBD STUB WING LOWER SKIN REF SRM 57-02-01A-0 FIG 002.

Part: FLAP TRACK — DAMAGED (LT WING TE FLAP) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 LT WING FLAP STA XW 340 FLAP TRACKS MISSING CHROME. REMOVED AND REPLACED L/WING FLAP TRACKS AT STA XW 340 IAW DC8 AMM 27-51-03-2.

Part: FLOOR PANEL — CORRODED (FS 340) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CABIN, FLOOR PNL F27 HAS CORROSION BOTH SIDES AND POPPED RIVETS IN U CHANNEL. REMOVED TOP SKIN OF FLOOR PNL F27 IAW SRM 53-20-00 FIG 1F. FABRICATED AND INSTALLED REPAIR SKIN AND HAT CHANNELS ON FLOOR PANEL F27 IAW DWG 9758942, AND SRM 51-3-2.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CABIN FLOOR PNL F212 CRACKED. REPAIRED CABIN FLOOR PNL. PER SRM 51-1-19.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT FLOOR PNL 676C HAS CRACKS AT RIVETS. REMOVED TOP SKIN OF COCKPIT FLOOR PNL 676C IAW SRM 51-1-20D. FABRICATED AND INSTALLED TOP SKIN ON FLOOR PNL 676C IAW SRM 53-7-3 FIG 001.

Part: SKIN — DAMAGED (LWS 501) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 LT WING OUTBD SLOT LWR ACCESS PNL HAS DOUBLE DRILLED HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT WING OUTBD SLOT LWR ACCESS PNL IAW SRM 57-02-00 FIG 002A AND DWG 5769928.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT FLOOR PNL 682A HAS AREAS OF CORROSION OUT OF LIMITS. REMOVED TOP SKIN OF FLOOR PNL 682A IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT SKIN ON FLOOR PNL 682A IAW DWG 5619357, AND SRM 52-2-O FIG 001F.

Part: PANEL — CORRODED (FS 920) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 KEEL BEAM PNL BETWEEN WHEEL WELLS BULGED AT FASTENER HOLE. FABRICATED REPAIR KEEL BEAM PNL AND INSTALLED BETWEEN WHEEL WELLS IAW DWG 561606, AND SRM 51-09-22, SRM 51-01-22.

Part: SEAL — BROKEN (CARGO DOOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 APPROX 3 INCHES OF SEAL BACK-UP STRUCTURE MISSING AT LOWER AFT CORNER OF C-PIT DOOR. REPAIRED C-PIT DOOR LOWER AFT CORNER IAW DWG. 5754260 AND SRM 52-02 -00 FIG 002.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 C-PIT DOOR EXTERIOR SKIN DAMAGED AT LOWER AFT CORNER. REPAIRED C-PIT DOOR EXTERIOR SKIN LOWER AFT CORNER REF SRM 52-02-00-0 FIG 002 AND FIG 006.

Part: FITTING — CRACKED (FS 280 L21L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 FITTING L21L STA 280 IS CRACKED. REMOVED L21L END FITTING AT STA 280 IAW SRM 51-03-00-0. FABRICATED AND INSTALLED END FITTING AT L21L STA 280 IAW DWG 3773073, AND SRM 51-01-20D.

Part: SKIN — CORRODED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CORROSION UNDER BONDED SKIN RT SIDE OF RUDDER ABOVE ISOLATION BELT. RUDDER REPLACED ON N/R 123801.

Part: SKIN — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 1" CRACK BELOW RUDDER TAB ON RT SIDE OF RUDDER. RUDDER REPLACED ON N/R 123801.

Part: STIFFENER — BROKEN (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 STIFFENER BROKEN ON RUDDER LOWER SIDE. RUDDER REPLACED ON N/R 123801.

Part: RIB — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 9TH RIB FROM BOTTOM OF RUDDER IS CRACKED ON LT SIDE AT FRONT SPAR. RUDDER REPLACED ON N/R 123801.

Part: SKIN — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 EDGE CRACK ON RT UPPER RADIUS OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801.

Part: SKIN — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 EDGE CRACK ON RT SIDE OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801.

Part: SKIN — DENTED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CREASED DENT ON LT UPPER SKIN OF RUDDER. RUDDER REPLACED ON N/R 123801.

Part: RIB — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 NR 5 RIB FROM BOTTOM OF RUDDER IS CRACKED THROUGH PREVIOUS REPAIR AT RT SIDE AT FRONT SPAR. RUDDER REPLACED ON N/R 123801.

Part: FRAME — CORRODED (TAILCONE) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 TAIL CONE FRAME FWD OF LOWER NAV LIGHT CUTOUT HAS CORROSION. REPAIRED TAIL CONE FRAME FWD OF NAV LIGHT IAW RAA DC8-53-20678 AND EA 008-5710-01-A1261.

Part: FRAME — CUT (FS 560 L21L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CUTOUT IN FRAME AT FS 560 BETWEEN L21+20L-MAIN CABIN FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-02-00,51-01-08, AND DWG DC8-53A-011.

Part: SKIN — CORRODED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 POPPED FASTENER HEADS AND HEAVY CORROSION ON LT RUDDER SKIN FWD OF TAB. RUDDER REPLACED ON N/R 123801.

Part: STRUCTURE — GOUGED (FS 1190) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 C-PIT TORQUE BOX REPAIR DOUBLER GOUGED, STA 1190 L35R. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AT C-PIT TORQUE BOX FS 1190 AND L35R REF SRM 53-02-00 AND 51-1-8.

Part: BRACKET — MISSING (FS 1260 L33R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 BRACKET MISSING BETWEEN STA 1260 FRAME AND INTERCOSTALS AT L33R. INSTALLED BRACKET AT FRAME 1260 L33R IAW SRM 51-1-20D, AND SRM 51-03-02.

Part: WEB — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 LARGE CRACK ON LOWER WEB OF RUDDER. RUDDER REPLACED ON N/R 123737.

Part: RIB — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 17TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801.

Part: TORQUE BOX — GOUGED (FS 1190 L33R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 REPAIR DOUBLER IN C-PIT TORQUE BOX, STA 1190 L33R IS GOUGED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER IN C-PIT TORQUE BOX STA 1190 L33R IAW SRM 51-01-20D, AND DWG 3753772.

Part: INTERCOSTAL — TORN (FS1276 L33R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 LARGE HOLE TORN IN TOP OF INTERCOSTAL AT STA 1276 AND L33R. FABRICATED AND REPLACED INTERCOSTAL AT FS 1276 AND L33R REF DWG 9754949 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 HEAVY CORROSION INSIDE L33L AT STA 1414. REPAIRED LONG 33L AT SAT 1414 IAW EO DC8-5320-28559-A AND EA 008-5320- 1-A1264.

Part: RIB — CRACKED (RUDDER) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 16TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801.

Part: DOOR FRAME — GOUGED (OVERWING EXIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 OUTER FRAME GOUGED IN 3 PLACES LT SIDE OF LT OVERWING EXIT DOOR, BLENDED OUT GOUGES, WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW 52-2-0, 51-1-20D, 51-1-8,52-2-0 FIG 6.

Part: WEB — CRACKED (WING) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 NR 1 MAIN WEB CRACK BETWEEN XRS 255 AND XRS 250. REPAIRED NR 1 MAIN WEB CRACK BETWEEN XRS 255 AND XRS 250 IAW EO DC8-5710 -28478-B AND EA 008-5710-01-A1261.

Part: LONGERON SPLICE — CRACKED (FS 1050 L31L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 L31L SPLICE FITTING CRACKED AT STA 1050. REPLACED SPLICE FITTING AT FS 1050 AND L31L REF, SRM 51-1-20D AND SRM 51-1-24.

Part: FLOOR PANEL — WORN (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT FLOOR PANEL 676F 6 EA HAT CHANNELS ARE WORN, DAMAGED AND SKIN HAS ENLONGATED SCREW HOLES. REPAIRED COCKPIT FLOOR PNL 676F IAW SRM 51-01-21, SRM 53-07-00 FIG 049B SHT 1, SRM 51-01-24 AND SRM 51-01-08.

Part: DOOR — DAMAGED (FS 960 LBL 60) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 L/MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT MLG DOOR SWITCH MOUNT FRAME IAW EO DC8-3260-16914-A.

Part: STIFFENER — CRACKED (BS 980) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 AREA OF CORROSION AND POSSIBLE CRACK ON AFT SIDE OF STA 980 BULKHEAD AT LT STIFFENER, BOTTOM C-PIT. REMOVED CORROSION AT 980 BULKHEAD LT VERTICAL STIFFENER. REMOVED STIFFENER AT 980 BULKHEAD. DRILLED UP REPLACEMENT STIFFENER AND INSTALLED AT 98 0 BULKHEAD IAW SRM 51-1-24,51-1-8,51-1-20D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT STA -38 RBL 14, SUBFLOOR FINGER DOUBLER BULGING. REPAIRED COCKPIT SUBFLOOR AT STA -38 RBL 14 IAW EA 008-5320-01- A1265.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 RT ELEVATOR NR 5 HINGE CUTOUT IS CRACKED THROUGH FASTENER HOLE ON UPPER SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT ELEVATOR NR 5 HINGE CUTOUT IAW SRM 55-04-01, AND SRM 51-1-21.

Part: STRUCTURE — CRACKED (OVERWING DOOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 POSSIBLE CRACK LOWER AFT CORNER OF LT OVERWING EXIT DOOR. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-02-00 FIG 02, 51-1-24, 51-1-20D AND DWG 5758037.

Part: FITTING — DAMAGED (FS 960 RBL 60) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 RT MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT MLG DOOR MOUNT SWITCH FITTING IAW EO DC8-3260-16914-A.

Part: FRAME — DAMAGED (FS 1100 L33R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 DOUBLE DRILLED HOLES IN GUSSET AT STA 1100 FRAME L33R. REMOVED GUSSET AT STA 1100 L33R IAW SRM 51-01-21D. FABRICATED AND INSTALLED REPAIR GUSSET IAW DWG 9754949, AND SRM 51-01-21D.

Part: FITTING — CORRODED (FS 340 L35R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 A-PIT, CORROSION AND BARE METAL ON BATHTUB FITTING STA 340 AND L35R. REPLACED CORRODED BATHTUB FITTING AT STA 340 AND L35R IAW SRM 53-02 -00 FIG 002 AND DWG 3755822.

Part: FITTING — CRACKED (WING) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 NR 4 ALT5-65 TO FRONT SPAR FITTING CRACKED. REPAIRED FWD SPAR FITTING BY FABRICATION AND INSTALLATION IAW SRM 51-01-20D, SRM 51-03-02, SRM 51-01-08 AND SRM 51-01-12.

Part: WEB — CRACKED (BS 1324 L21L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 WEB BROKEN ON AFT LOWER CORNER OF LT AFT ENTRY DOOR TORQUE BOX. REPAIRED LT AFT ENTRY DOOR TORQUE BOX WEB IAW DWG 9751060, SRM 53- 02-00 FIG 23, SRM 51-01-08, SRM 51-01-21 AND SRM 51-01-21D AT STA 1324 AND L21L.

Part: CHANNEL — DAMAGED (FS 1766 LBL 8) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 MAIN CABIN "U" CHANNEL HAS HOLE IN RADIUS STA 1766 LBL 8. REMOVED, FABRICATED AND INSTALLED "U" CHANNEL AT STA 1766 LBL 8 IAW SRM 51-01-21D, AND DWG 5755032.

Part: WEB — CRACKED (BS 70 L21L) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 MAIN CABIN L-1 DOOR TORQUE BOX WEB GOUGED AND CRACKED STA 70 ABOVE L21L. REPAIRED MAIN CABIN L-1 DOOR TORQUE BOX WEB AT STA70 ABOVE L21L IAW SRM 53-02-00-0 FIG 001D AND DWG 5597646.

Part: SEAT TRACK — CRACKED (FS320 LBL55) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK HAS LUG MISSING, LUG CRACKED AND TRACK GOUGED, STA 320 LBL55. REPAIRED MAIN CABIN SEAT TRACK AT STA 320 AND LBL 55 REF SRM 53-02-03- 0 FIG 006D AND SRM 51-3-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CRACKED LOWER RIB ON HORIZ STAB RT LEADING EDGE. STOP DRILLED CRACK ON RT HORIZ STAB LEADING EDGE IAW SRM 55-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 55-02-00-0 FIG 002.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 RT ELEVATOR GEAR TAB IS DELAMINATED. REMOVED AND REPLACED RT ELEVATOR GEAR TAB IAW DC8 AMM 27-30-03-2.

Part: SKIN — CANNING (RT ELEVATOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 O/B UPPER SKIN IS OIL CANNED ON RT ELEVATOR. REPAIRED RT ELEVATOR O/B UPPER SKIN REF DWG 5654970 AND SRM 55-02-01 FIG 008.

Part: CUSP WEB — CRACKED (FS 275 L21R) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 MAIN CABIN, L21R HAS HEAVY INTERGRANULAR CORROSION AND A 4 INCH CRACK INSIDE TORQUE BOX STA 275. REPAIRED L21R CUSP CRACK AND CORROSION AT STA 210, 235 AND 275 IAW SRM 53-02-00 FIG 002, SRM 53-02-05 FIG 15 AND DWG 9755808.

Part: INTERCOSTAL — GOUGED (LT ELEVATOR) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 DAMAGED COUNTERSINK ON INBD AFT CORNER OF LT ELEVATOR. LT ELEVATOR INBD INTERCOSTAL AFT CORNER DAMAGED COUNTERSINK REPAIRED IAW SRM 55-02-00-0 FIG 002, SRM 55-04-01-00 FIG 002, SRM 51-01-21 AND SRM 51-01-21A.

Part: KEELBEAM — CRACKED (FS 870 RBL 12) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 RT WHEEL WELL KEEL BEAM WEB CRACKED STA 870, 2ND ACCESS HOLE AFT. STOP DRILLED END OF CRACK ON WEB AT STA 870 IAW SRM 53-02-00 FIG 23. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT WHEEL WELL KEEL BEAM WEB AT STA 870 IAW SRM 53-02-00 FIG 23.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT STA -52 SEAT TRACK IS WORN AND LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED F/E'S FWD SEAT TRACK AT STA -52 IAW SRM 51-03-00, AND DC8 AMM 25-11-02-0 FIG 002.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CAPT, AFT INBD SEAT TRACK LOCK PIN HOLES ARE WORN. REMOVED AND REPLACED CAPT AFT INBD SEAT TRACK IAW EO DC8-5340-18315 -B.

Part: DOUBLER — CRACKED (RWS 467) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 R/WING, OUTBD STUB WING HAS DOUBLER AT LWR SURFACE WITH 2" CRACK. REMOVED CRACK DOUBLER AT R/WING OUTBD STUB WING IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/WING OUTBD STUB WING STA XW 467.000 IAW SRM 57-02-01A-0 FIG 001.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CAPT'S FWD I/B SEAT TRACK IS WORN. REMOVED AND REPLACED CAPT'S FWD SEAT TRACKS REF, EO DC8-5340-18315 APPX B.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 F/O'S AFT INBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED F/O'S INBD SEAT TRACK IAW EO DC8-5340-18315-B.

Part: INTERCOSTAL — CRACKED (FS 8 RBL 54) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 INTERCOSTAL BROKEN IN MAIN CABIN SUBFLOOR, STA 8 RBL 54 AT MAIN A/C DUCT. STOP DRILLED CRACK ON INTERCOSTAL AT MAIN CABIN STA 8 RBL 54. FABRICATED AND INSTALLED REPAIR DOUBLER ON INTERCOSTAL AT MAIN CABIN STA 8 RBL 54 IAW SRM 53-02-00, 53-02-00 FIG 001B, AND DWG 5888479.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 CAPT, AFT OUTBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED CAPT, AFT OUTBD SEAT TRACK IAW EO DC8-5340- 18315-B.

Part: SEAT TRACK — WORN (BS -38) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 COCKPIT STA -38 SEAT TRACK IS WORN AND LOCK PIN HOLES ARE WORN. REMOVED AND REPLACED F/E AFT SEAT TRACK IAW SRM 51-03-00, 51-01-24.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 1ST OFFICERS AFT OUTBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED 1ST OFFICERS AFT OUTBD SEAT TRACK IAW EO DC8- 5340-1815-B.

Part: SKIN — CRACKED (LT TE FLAP) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 2 DENTS ON LOWER SKIN LT I/B FLAP POSSIBLE CRACKS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-02-01.

Part: RIB — CRACKED (LT WING FLAP) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 PNL - 551 SUPPORT FRAME CRACKED AT O/B END OF LT I/B FLAP. REPAIRED LT I/B FLAP O/B RIB (PNL 551 LANDING) IAW SRM 57-02-00, SRM 57-07-01-0, AND SRM 51-01-21-0.

Part: DRIVE ASSY — CRACKED (TE FLAPS) · airframe 68,725 hrs · 26,121 cycles

INSPECTION TYPE:C2 ULTRASONIC INSPECTION, DETECTED A RADIAL CRACK ON THE INBD LUG OF THE LT WING FLAP DRIVE LINK AT STA XW 97 AT POINT "J". REMOVED AND REPLACED LT WING FLAP DRIVE LINK AT STA XW 97 IAW DC8- AMM 27-51-04-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A ON COCKPIT PREFLIGHT EMERGENCY EXIT LIGHTS WHEN ARMED WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD.

Part: LINE — LEAKING (HYDRAULIC SYS)

DURING CLIMB, LOST MAIN SYS HYD PRES AND QTY TO AUX POS. RAN "LOSS OF HYD FLUID OR PRES" CK LIST. LANDED W/FULL FLAPS ON AUX PUMP. FOUND NR 3 ENG PRESS LINE CHAFED THROUGH. REMOVED AND REPLACED LINE AND CLAMP LEAK CK GOOD REF LP 625876/ITEM 2/3.

Part: STRUCTURE — MISSING (COCKPIT)

PILOT'S SIDE WINDOW BOLT POSITION NR 58 PER MM 56-10-02-2 HAS NO FRAME STRUCTURE BEHIND IT. BOLT ALSO WAS LEFT OUT OF TORQUE SEQUENCE STEP 10 AND 11 DUE TO NO STRUCTURE. DEFERRED CAPTS SIDE WINDSHIELD UPPER OUTBOARD DEFLECTOR AS MISSING PER EO DC8-5610-24395-B STEP 6A(3). TORQUED BOLT AND NUT. REF TO AMM 56-10-02-2. CONTROL NR D326104 ASSIGNED. PERMANENT REPAIR DUE IN 30 DAYS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT OVER MAIN ENTRY DOOR HAS BULBS INOP. RELAMPED. OPS CK'S GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHTS INOP. TRANSFERRED TO UPS NRC 814597. R&R EMERG BATT PACK IAW MM 33-50-01-2. OPS CK FAILED. OPENED EMER LT BATT ACCESS PNL. REPAIRED 2 BROKEN WIRES AT CONNECTOR. OPS CK FAILED R&R BATT PACK IAW MM 33-50-01-2. OPS CK GOOD. CLOSED ACCESS PNL IAW SRM 51-3-0.

Part: CLIP — BROKEN (FS 1195 L33R-34R) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1, T-BOLT BACKUP FITTING REPAIR BROKEN AT C-PIT DOOR JAMB, STA 1195 BETWEEN L33R AND L34R. REMOVED AND REPLACED BACKUP FITTING REPAIR CLIP IAW SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 EXFOLIATION CORROSION UNDER FRAME 1000 ABOVE L36 AT SITE OF REMOVED NUTPLATE. REPAIRED FRAME AT STA 1000 L36 IAW EO DC-8 5310-11728-B.

Part: SKIN — CORRODED (FS1690-1751 LBL3) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1, CORROSION ON LOWER SKIN IN MULTIPLE AREAS AROUND 62 HOLE ENTRANCE INTERIOR, ESPECIALLY IN CORNERS OF EVERY RIB AROUND DOOR. REPAIRED LOWER SKIN AND RIBS AT 62 HOLE DOOR STA 1690 RBL30 TO LBL30 TO STA 1751 RBL12 TO LBL12 IAW SRM 51-1-8, 53-2-0 FIG 1F, 51-1-4, 53-5-1, DWG 570465 AND EO DC8-5350-7876-A.

Part: SKIN — CRACKED (FS 1746 L16L) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT STA 1746 L16L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01-0 FIG 007, 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (BS 1726 L16R) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT STA 1726 L16R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1240 L19L) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 CRACK ON LONGERON 19L ATTACH BRACE AT STA 1240. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (LBL 24 FS 680) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 LBL 24 AT STA 680 HAS CORROSION UNDER SEAT TRACK AS VEIWED FROM LOWER ACCY COMPT. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-1-21, 51-3-0,5 AND 53-02-03.

Part: FITTING — CRACKED (FS1690-1700 L28R) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 L28R END FITTING CRACKED AT STA 1690-1700. REMOVED AND RPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: WEB — CORRODED (L33R FS 1190) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 HEAVY CORROSION ON C-PIT TORQUE BOX WEB ALONG L33R AT STA 1190. FABRICATED AND INSTALLED DOUBLER IAW DWG 3753772 AND SRM TEMP REV. 53-166 (53-2-0 FIG 25).

Part: FITTING — CRACKED (FS 680 L7R) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING HAS A 3 INCH CRACK STA 680 L-7R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 680 L8R) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING HAS A 4" CRACK, STA 680 L8R. REMOVED END FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END FITTING AT STA 680 L8R IAW SRM 51-01-20D.

Part: FITTING — CORRODED (FS974 LBL66) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 HEAVY CORROSION ON FITTING IN OB UPPER AFT CORNER OF LT W/W STA 974 LBL66. REMOVED, FABRICATED AND INSTALLED FITTING IAW 51-1-20D, DWG 2647420,

Part: SPAR CAP — CRACKED (LT WING) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1, NDT FOUND CRACK APPROX 8" LONG ON LT LOWER SPAR CAP AT BL 47-55 ON HORIZONTAL LEG STA 857. REPAIRED LT LWR SPAR CAP STA 857 BL47-55 IAW SRO 8530009 AND EA 008-5710-01-A0039.

Part: RIB — WORN (NR 1 PYLON) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 5TH RIB ON NR 1 PYLON WORN" CHECK LIMITS". BLENDED OUT WORN AREA. FABRICATED AND INSTALLED REPAIR STRAP IAW DC-8 SRM 54-3-1 FIG 3, 51-1-8,51-1-21 AND 51-1-20D.

Part: DOOR SEAL — CRACKED (EMERGENCY EXIT) · airframe 67,854 hrs · 25,446 cycles

INSPECTION TYPE:C1 LT AFT EMERGENCY EXIT AFT SEAL CRACKED AT 2 PLACES 6" BELOW UPPER CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-02 -00 FIG 009A AND DWG 5755980.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ON PREFLIGHT, FOUND EMERGENCY EXIT LTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CKS GOOD.

Part: HYDRAULIC SYSTEM — LEAKING

ATB - HYDRAULIC FLUID LOSS, EMERGENCY DECLARED. FOUND LEFT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE LINE LEAKING/ DAMAGED. R/R LINE PER MM 30-12-2. SVCD HYD SYSTEM PER MM 12-30-01-3 LEAK CK O.K.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,854 hrs · 25,446 cycles

HEAVY CORROSION ON AFT SIDE OF FITTING BETWEEN LT W/W CIELING AND L24L AT STA 920. REMOVED AND REPLACED FITTING AND REPAIR SPLICE IAW SRM 53-2-0 FIG 008 AND 51-03-01.

Part: STRUCTURE — CORRODED (RT MLG WW)

CORROSION IN RIGHT MLG WHEEL WELL. REMOVED CORROSION FROM RMLG W/2 PANEL. UT AREA FOUND MIN MATERIAL TO BE .048" THICK. PERFORMED HFEC INSP NO CRACKS FOUND. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-20826. DEFERRAL D285269 ASSIGNED AWAITING CLOSING LP AND CLOSING DEFERRAL.

Part: SKIN — CRACKED (RUDDER) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE:C3 RUDDER L/E SKIN IS CRACKED ON LT SIDE AT ZR 289.343. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK. FABRICATED AND INSTALLED DOUBLER AND SHIMS IAW SRM 55-2-1 FIG 5.

Part: CLIP — CRACKED (NR 1 FUEL TANK) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 61 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED AT NR 1 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED SLIP IAW DWG 5804007 AND SRM 51-1-20D.

Part: CLIP — CRACKED (NR 1 FUEL TANK) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED, APPROX STATION XW 485. REMOVED, FABRICATED AND INSTALLED CLIP IAW DWG 5804007 AND SRM 51-1-20D.

Part: CLIP — CRACKED (NR 4 FUEL TANK) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE AT NR 4 PYLON IS CRACKED IN NR 4 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5804007 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (AFT CABIN) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, STATION 1726 AND 1746 AND LONG 15L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: SHEAR TIE — CRACKED (TAIL COMP'T) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, SHEAR TIE CRACKED AT STA 1766 BETWEEN LONGERONS 9R AND 10R. STOP DRILLED CRACK AND INSPECTED PER NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR PER DAC DWG 5772706, AND DC8 SRM 53-2-0 FIG 1B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, STATION 1766 LONG 17L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21, 53-5-1 FIG 7.

Part: STRINGER — CRACKED (NR 4 FUEL TANK) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, STRINGER 59 IS CRACKED OUTBOARD OF XRS 428 INSIDE 505B NR 4 ALT TANK. REMOVED, FABRICATED AND REPLACED FITTING IAW UPS ENGINEERING FILE NUMBER DC8-57-20103.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, LONGERON 36 IS CORRODED BEYOND LIMITS BETWEEN STATION 120 - 160. CUT OUT LONGERON SECTION BETWEEN STATION 120 - 205, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, STATION 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.

Part: LONGERON — CRACKED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, STATION 1240 LONGERON 34R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND SPLICES BETWEEN STATION 1210 TO 1270 IAW UPD ENGINEERING FILE NUMBER DC8-53-20384, AND SAA SK 702-146.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, EXTERIOR FUSELAGE, 4 DENTS IN SKIN OVER BELLFRAMES, AND GOUGES BETWEEN LONG 21L - 24L, FOUND SHEAR TIE CRACKED AT STA 100 BETWEEN LONG 23L AND 24L. CUT OUT DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE SECTION AND DOUBLER IAW SRM 53-2-0 FIG 2B.

Part: SKIN — CORRODED (RT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, INTERGRANULAR CORROSION ON RT WING L/E UPPER SKIN AT AFT END AT XFS 347. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8-5720-7767-A.

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, STA 1228 LONG 34L - 35L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, A-PIT DOOR STOP BACK-UP FITTING CRACKED AT STA 320 L27L. REMOVED AND REPLACED FITTING REF DC8 SRM 51-1-20D AND SRM 51-3-0.

Part: SUPPORT FITTING — CRACKED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, INTERCOSTAL SUPPORT FITTING IS CRACKED AT STATION 1140 LONG 33R INBOARD. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING LE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, LEFT WING NR 2 STUB WING UPPER RIB IS CRACKED AT XS 250.089. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, LONGERON 34R IS CRACKED BETWEEN STATION 1270-1290. REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (RT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE:C3 RT WING L/E UPPER RIB IS CRACKED AT XFS 448. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, RT WING LE UPPER RIB IS CRACKED AT XFS 291. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG. 2

Part: LONGERON — CORRODED (AFT LOWER CARGO) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, LONGERON 33R CORRODED AT STA 1480. CUT OUT CORRODED SECTION OF LONGERON 33R FROM STA 1470 TO 1490. FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, FWD SIDE STATION 70 LONGERON 30R IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 3648667 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, RT WING LE UPPER RIB IS CRACKED AT XFS 316.5 STOP DRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 57-2-0 FIG. 2

Part: LONGERON — CRACKED (AFT CABIN) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, LONGERON STATION 1726 AND 1746 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (LT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 766.25, XFS 797.5. STOPDDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIBS ARE CRACKED AT XFS 635, XFS 641.25, XFS 647.5, XFS 653.75, XFS 660. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE:C3 RT WING L/E UPPER RIB IS CRACKED AT XFS 841. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE:C3 LT WING L/E HAS UPPER RIBS CRACKED AT XFS 835, XFS 822.5, XFS 803.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LH WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 448.581. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CORRODED (LEFT WING LE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, LT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 622.75 TO XFS 610, LOWER INTERNAL DOUBLER AT PANEL OPENING. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-21.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, LT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. 5769600 AND SRM. 51-1-21,51-1-20D,57-3-0 FIG. 2D.

Part: RIB — CRACKED (LT WING LE) · airframe 66,981 hrs · 24,724 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 685. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, FLOORBEAM IS CORRODED BEYOND LIMITS AT STATION 822 AT LBL 24 UPPER CAP. REMOVED, FABRICATED AND REPLACED FLOORBEAM IAW DWG 3773442 AND SRM 51-3-0, 51-1-20D.

Part: BATTERY — INOPERATIVE (FIRE DETECTION)

THE LOWER COMPARTMENT FIRE LIGHT CAME ON FOR THE FORWARD A COMPARTMENT. THE FIRE WARNING LIGHT WENT OUT & CHANGED TO A MAINT LIGHT. THE LOWER COMPARTMENT LIGHT WAS ON LESS THAN 20 SEC BEFORE IT CHANGED TO MAINT LIGHT. PERFORMED T/S TO THE LOWER CARGO FIRE WARNING SYS FOUND CCU FAULTY BUT DID NOT FIX PROBLEM. WITH FWD A BELLY 31 STILL SHOWS INOPERATIVE BATTERY FA 12560 SHOWS LOW DEFERRED PIT 31.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD.

Part: WINDOW — STUCK (COCKPIT)

UNABLE TO OPEN CAPTAIN`S SLIDING WINDOW. RIGGED UPLOCK BAR OF CAPT SLIDING WINDOW 56-10-03.

Part: WINDOW — STUCK (COCKPIT)

INSPECTION TYPE:PFLT CAPT'S SLIDE WINDOW WILL NOT OPEN. CYCLE LOCK AND OPS, CHECK NORMAL.

Part: SHEAR TIE — CRACKED (AFT FUSELAGE) · airframe 66,981 hrs · 24,729 cycles

INSPECTION TYPE: C3, STA 1766 AFT SIDE SHEAR TIE IS CRACKED AT LOWER END BETWEEN LONGERON 9L AND 10L. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, A/C FAILS STANDBY POWER CHECK (NO EMERGENCY LIGHTS). REPLACED EMERGENCY BATTERY PACK, EMERGENCY LIGHTS OPS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 798 LBL 49 FLOORBEAM WEB ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 3643112 AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1350 LONG 34R. CUT OUT CRACK, NDT VERIFIED NO CRACK AT CUT OUT AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1470 AT LONG 34R SKIN IS CRACKED. CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUT OUT. FABRICATED REPAIR AND INSTALLED IAW SRM 53-2-1 FIG 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA -80 FLOORBEAM AND PRESSURE WEB ARE CORRODED BEYOND LIMITS AT LBL 47-59 APPROX. FABRICATED AND INSTALLED WEB AND FINGER DOUBLERS IAW SRO 8530026, FABRICATED AND INSTALLED FLOORBEAM SPLICE REPAIR IAW 8110-3 DH SK 702-953.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 200-220 LONG 31L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW 8110-3 APPROVED DH SK 702-811.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STATION 1200 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STATION 1180 LONG 34R-35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5649327 AND SRM 51-1-20D, 51-3-0, 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1230 BETWEEN LONG 27L-28L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D, 51-3-0.

Part: WEB — CRACKED (RUDDER) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 RUDDER NR 2 HINGE CUT OUT LOWER WEB IS CRACKED AT ZR 161 APPROX. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5656229 AND SRM 51-1-21.

Part: LONGERON — CRACKED (FUSLEAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1260-1280 LONG 34R IS CRACKED. REMOVED LONGERON, FABRICATED LONGERON REPAIR AND SPLICES AND INSTALLED IAW 8110-3 APPROVED DH SK 702-586.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1860 LONG 3R CLIP/SHEAR TIE IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-0 FIG 1B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1230 BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 987 LONG 23L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 FLOORBEAM ATTACH FITTING IS CRACKED AT STA, 742 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 1230 BETWEEN LONG 36 TO 35L. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 1395 - 1447 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON SEGMENT IAW DWG 3646937 AND SRM 53-1-0, 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 LONG 24L IS CRACKED PAST STOP DRILL STA 857-879. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-2 FIG 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 LT WHEEL FWD BULKHEAD LOWER WING CHORD STA 857 AT XCW 0 CRACK. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS IAW 8110-3 APPROVED DH SK 702-461.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN IS CRACKED AT STA 1660 LONG 11R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER FWD CORNER STA 1620 AT LONG 20L. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 18.

Part: SKIN — CORRODED (LT WING) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 347.5 AND XFS 366.5. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STATION 683 BULKHEAD IS CRACKED AT RBL 5 AND RBL 12 AT WEB AT LOWER WING SPAR. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUT OUT. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-5 FIG 13.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STATION 1766 AT LONG 2L FUSELAGE TO VERTICAL STAB ANGLE IS CRACKED AND CORRODED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-5 FIG 16A.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 70 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R TO 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-5 FIG 8C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,998 hrs · 23,992 cycles

INSPECTION TYPE:C2 STA 55 FRAME IS CRACKED AT ROD ATTACH POINT LONG 23R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FRAME AND SEGMENT IAW SRM 53-2-0 FIG 2.

Part: STRUCTURE — CRACKED (LT WING)

MX INSP-CRACK IN WING STRUCTURE JUST AFT OF LEFT MLG STRUT, MRR FILED AS OPEN.

Part: STRUCTURE — CRACKED (LT WING)

CRACK IN WING STRUCTURE AFT OF LEFT MLG REF DC8-5720-14401-A D213157 COMPLETE AT NEXT C CHECK UPS01835548 VOIDED DUE TO DUPLICATION OF MRR

Part: SLIDE — INOPERATIVE (PAX DOOR)

INSPECTION TYPE:N/A ESCAPE SLIDE INOP REFERENCE M205259 ***SUPPLEMENTAL MRR*** R/R EVACUATION SLIDE & CONTAINER PER M/M 25-62-00. OPS CK NORMAL IN GERT BAR. THIS CLEARS M 205259. PLACARD REMOVED.

Part: CIRCUIT BREAKER — DAMAGED (EMERGENCY LIGHT)

INSPECTION TYPE:A CK EMERGENCY EXIT LIGHTING CIRCUIT BREAKER (5A) DAMAGED. REPLACED C/B B1-115 - REF WDM 33-50-01, PG 1,SH 1, SYS OPS CK NORMAL IAW M/M 33-50-01.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

INSPECTION TYPE:N/A, ON TOP OF DESCENT MAIN CARGO SMOKE LIGHT ILLUMINATED, LIGHT REMAINED ON AT ALL SEVEN POSITIONS. CARGO SMOKE LIGHT REMAINED ON FOR 30 MINUTES, UNTIL PARKING WHEN LIGHT WENT OUT. DID NOT SEE OR SMELL ANY SMOKE OR FUMES. REMOVED AND REPALCED #4 SMOKE DETECTOR ASSY ALSO RELAMPED ALL OTHER DETECTORS WITH CORRECT LAMPS. SYS OPS CK NORMAL IAW MM DC8 26-10-05. S/N ON: 32007, S/N OFF: 34371.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1 LT WING L/E LWR SKIN INTERNAL DOUBLER AT XOLDI 6.225 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769891 AND SRM 51-1-20D 51-1-21.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C1 STA 280 AT LONGERON 36, THE BATHTUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 347)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 347.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (WS 347,354,391.5)

INSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 347.75, 354, AND 391.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 635 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACKED AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FLOORBEAM — CORRODED (BS 980)

INSPECTION TYPE:C1 CABIN FLOORBEAM AT FS 980, LBL 54, UPPER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK702-314.

Part: RIB — CRACKED (WS 336)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 336 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 1270)

INSPECTION TYPE:C1 LONGERON 34R SPLICE FITTING AT FS 1270 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 1270)

INSPECTION TYPE:C1 THE LONGERON 36 SPLICE FITTING AT FS 1270 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 1050)

INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT FS 1050 AND LONGERON 31R. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1050)

INSPECTION TYPE:C1 THE LONGERON SPLICE FITTING AT FS 1050, LONGERON 31L IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FRAME — CRACKED (BS 1680)

INSPECTION TYPE:C1 STA 1680 AT RT CUSP LWR SURFACE, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: WEB — DAMAGED (BS 1160)

INSPECTION TYPE:C1 FS 1160 AT LONGERON 28R, THE PRESSURE WEB LIGHTENING HOLE COVER HAS 4 OPEN HOLES. REPAIRED WEB IAW DH SK702-183.

Part: SKIN — CRACKED (WS 597.5)

INSPECTION TYPE:C1 LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5740-4087.

Part: WEIGHT — CORRODED (AILERON)

INSPECTION TYPE:C1 THE RT OTBD AILERON INBD BALANCE WEIGHT HAS MODERATE CORROSION ON AND UNDER THE WEIGHT. REMOVED AND REPLACED THE RT OTBD AILERON IAW M/M 27-10-02.

Part: FITTING — CRACKED (BS 1260)

INSPECTION TYPE:C1 LONGERON 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 1260. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 360.2 - 366.5)

INSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 360.25 AND 366.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.

Part: LONGERON — CRACKED (BS 920 & 940)

INSPECTION TYPE:C1 LONGERONG 24L IS CRACKED BETWEEN FS 920 AND 940. STOP DRILLED CRACK AND REPAIRED THE LONGERON IAW SRM 53-2-2, FIG 5.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE:C1 FS 1200 AT LONGERON 17R THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C1 LONGERON 11L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 742. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 598)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XFS 598 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-4087.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1 FS 857 AT LONGERON 19R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DH SK702-997 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 467.232)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C1 FS 1230 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 440 - 460)

INSPECTION TYPE:C1 FS 440 TO 460 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING L/E RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: SHEAR TIE — CRACKED (BS 640)

INSPECTION TYPE:C1 THE SHEAR TIE AT FS 640 BETWEEN LONGERON 26R AND 27R IS CRACKED. CUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0, FIG 2B.

Part: RIB — CRACKED (WS 597.5)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 597.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: SKIN — CRACKED (WS 310.25)

INSPECTION TYPE:C1 LT WING L/E LWR SKIN IS CRACKED AT THE FASTENER HOLE AT XFS 310.25. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5740-4087.

Part: RIB — CRACKED (WS 379)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C1 FS 280, ABOVE LONGERON 27R, THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 227.335)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 759 STR 18R. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C1 STA 280 ABOVE STR 27R, THE BACK-UP FITTING FOR THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 429)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN, INTERNAL DOUBLER AT XS 429 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769891 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 467.2)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 902 STR 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4750423 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 640 - 660)

INSPECTION TYPE:C1, STA 640-660 STR 1 SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3750271 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE:C1 FS 742 AT LONGERON 12L, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CRACKED (BS 640 - 660)

INSPECTION TYPE:C1 SAT 640-660 LONGERON 1 IS CRACKED. FABRICATED AND REPLACED LONGERON 1 FROM STA 640-680 IAW DWG 63779657 AND SRM 53-4-1 FIG 41.

Part: RIB — CRACKED (WS 297 - 304)

INSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 297 AND 304 ARE CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1 FS 857 AT LONGERON 18L, THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 600 - 620)

INSPECTION TYPE:C1 FS 600 TO 620 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: ACCESS PANEL — CORRODED (RT WING)

INSPECTION TYPE:C1 RT WING L/E AT THE ACCESS PANEL 518A INTERNAL DOUBLER HAS HEAVY EXFOLIATION CORROSION UNDER THE NUTPLATE CHANNEL. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IWA DWG 3641257 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C1 FS 781 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE:C1 STA 879 AT STR 24R, SUPPORT FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3641004 AND SRM 53-2-0 FIG 8.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE:C1 LT W/W FITTING AT FS 879 ABOVE LONGERON 24 HAS HEAVY CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0, FIG 8.

Part: SKIN — CRACKED (WS 310.25)

INSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 310.25 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1, FIG 38.

Part: FITTING — CRACKED (BS 683)

INSPECTION TYPE:C1 FS 683 AT RBL 24, THE FLOOR SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: BUS PANEL — SMOKED (COCKPIT)

INSPECTION TYPE:N/A, WHEN GEN RELAY NR 1 CLOSED ON STARTUP, PASSING 45 PERCENT N2, NR 1 BUS PWR FAIL LIGHT ILLUMINATES WITH SMOKE AND ELECTRICAL BURNING SMELL IN COCKPIT BTB (AC VOLTS AND FREQS NORMAL, NO A/C LOAD) 5/18/99 0420Z. REMOVED AND REPLACED BUS PROTECTION PANEL (S/N 584) ON, (S/N 815) OFF, (P/N 50130-003 R7R GEN RELAY (P/N 50137-002) (S/N 4662ML) ON, (S/N 3926ML) OFF. REMOVED AND REPLACED REG AND CONTROL PANEL (P/N 51508-000) (S/N 1070BC) ON. RUN ALL ENG, ALL GEN CKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP, BATTERY VOLTAGE 22V ON BISE CK. REMOVED AND REPLACED EMERGENCY BATTERY PACK, PER MM-33-50-01, OPS CK NORMAL P/N OFF 60-1223-5, P/N ON 5708458-503, P/N OFF 230 S/N ON 187.

Part: ENGINE — FLAMED OUT (NR 4)

INSPECTION TYPE-N/A AT FL 310, SET UP SUCTION FEED OFF OF NR 4 ALT TANK FUEL PRESSURE WAS INTIALLY AT 30 PSI THEN PRESSURE FLUCTUATED FROM 30 PSI TO 0 PSI. FUEL PRESSURE STAYED AT 0 PSI AND THEN NR 4 ENG FLAMED OUT. ENGINE RESTARTED, OTHER INDICATIONS NORMAL. RAN NR 4 ENG PER MM 71-00-00 AND CHK'D FOR LEAKS AND OPS CK ENGINE DRIVER PUMP PER 73-10-01. SYS TEST NORMAL WITHIN PARAMETER.

Part: BATTERIES — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER LIGHTS ARE DEAD. EMER LIGHT BATTERIES CHARGED ON GROUND POWER FOR 6 HRS, OPS CHECKED OK.

Part: AMPLIFIER — FAILED (CARGO COMPT)

INSPECTION TYPE-N/A, FL 350 CARGO SMOKE LIGHT ILLUMINATED AND SHOWED SMOKE IN ALL POSITIONS. COMPLETED QRH. REMOVED AND REPLACED FIRE DETECTION SYSTEM CONTROL AMPLIFIER (P/N 30-303A) (S/N 9056) OFF, (P/N 30-326-4) (S/N 43852) ON OPS CHECKS GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

AT FL 350 MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED IN ALL POSITIONS, LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER; SYSTEM OPS CHECKED NORMAL IAW DC8 MM 26-00-00.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

INSPECTION TYPE-N/A, FL 350 CARGO SMOKE LIGHT ILLUMINATED ALL POSITIONS INCLUDING NORMAL AND OFF / COMPLIED WITH AOM EXCEPT FOR FIRE BOTTLES. REMOVED AND REPLACED NR 3, 4, 6 SMOKE DETECTORS AND AMPLIFIER. FERRIED TO SDF FOR FWD ENTRY DOOR REPAIR. SMOKE DETECTOR SYSTEM TO BE RETESTED AT SDF.

Part: LONGERON — CRACKED (BS 1740)

INSPECTION TYPE-C, LONG 21L AT FS 1740 IS CRACKED. REMOVED DAMGED LONGERON SECTION AND FABBED NEW ONE IAW DC8 SRM 53-2-2. SPLICES FABBED IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONG AND SPLICES IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74.9)

INSPECTION TYPE-C, CRACK IN FITTING AT XRS 74.9, 1ST FITTING AFT OF FWD SPAR AT BLKH TO FWD SPAR ATTACH. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 140)

INSPECTION TYPE-C, STA 140L 20R END OF LONGERON IS CRACKED. REPAIRED L20R END FITTING IAW DC8 SRM 53-2-2.

Part: LONGERON — CORRODED (BS 140)

INSPECTION TYPE-C, STA 140 L20R END OF LONGERON CRACKED. FABRICATED SPLICE IAW DC8 SRM 53-4-1. DRILLED SPLICE IAW DC8 SRM 53-2-2. ALODINED, PRIMED, INSTALLED SPLICE IAW DC8 SRM 51-1-8, 53-2-2 AND 51-1-20D.

Part: FITTING — CRACKED (BS 1600)

INSPECTION TYPE-C/CK, AFT FUSELAGE STATION 1600 BEAM END FITTING CRACKED. REMOVED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 1660)

INSPECTION TYPE-C/CK, FUSELAGE STATION 1660 FLOORBEAM IS CORRODED. REMOVED CORRODED SECTION OF BEAM IAW REO 03846, FABBED REPAIR ANGLE IAW REO 03846. INSTALLED, ALODINED AND PRIMED IAW REO 03846 AND DC8 SRM 51-3-0 AND 51-1-20D AND 51-1-8.

Part: FITTING — CRACKED (BS 1600)

INSPECTION TYPE-C, FS 1600 BEAM END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 1660)

INSPECTION TYPE:C/CK, FS 1660 FLOORBEAM IS CORRODED. REMOVED CORRODED SECTION OF BEAM IAW REO 03846. FABBED REPAIR ANGLE IAW REO 03846 INSTALLED ALODINED AND PRIMED IAW REO 03846 DC8 SRM 51-3-0 AND 51-1-20D AND 51-1-8.

Part: FITTING — CRACKED (BS 1600)

INSPECTION TYPE:C/CK, AFT FUSELAGE STATION 1600 BEAM END FITTING CRACKED. REMOVED FITTING DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: JAMB — CORRODED (CARGO DOORWAY)

INSPECTION TYPE-C, R-1 DOOR JAMB, LOWER FWD AND AFT PANS CORRODED. REMOVED PANS, FABBED -3 AND -5 SEGMENTS IAW DAC DWG NR 5615700. ALODINED PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D.

Part: ANGLE — CORRODED (CARGO DOORWAY)

INSPECTION TYPE-C, R1 DOOR JAMB CUSP ANGLE CORRODED. REMOVED CORR ANGLE,TRIMMED AND DRILLED NEW ONE IAW DC8 SRM 51-1-24 AND DAC DWG 5615700. ALODINED, PRIMED, INSTALLED IAW DC8 SRM 51-1-8, 51-1-21 AND 51-1-20D AND 51-3-0.

Part: SHEAR TIE — CRACKED (BS 710)

INSPECTION TYPE-C, BOTTOM FUSELAGE APPROX STA 710, RT KEEL AREA, SHEAR TIE CRACKED. FABBED SHEAR TIE IAW DC8 SRM 53-2-0 AND 51-1-4. HEAT TREAT IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FLOOR WEB — CORRODED (CARGO COMPT)

INSPECTION TYPE:C/CK, FLOOR WEB CORRODED AT FS 70 AFT OF FWD ACCY COMPT AFT BULKHEAD AT FLOOR LINE TOP OF RIGHT FWD LOWER CARGO COMPT STRUT. REMOVED CORROSION IAW DC8 SRM 51-1-8 FABRICATED REPAIR DOUBLER AND FILLER IAW REO 03853 IR INSTALLED IAW REO 03853 IR.

Part: WEB — CORRODED (BS 70)

INSPECTION TYPE-C/CK, FLOOR WEB CORRODED AT FUSELAGE STATION 70 AFT OF FWD ACCY COMPT AFT BULKHEAD AT FLOOR LINE TOP OF RIGHT HAND FWD LOWER CARGO COMPT STRUT. REMOVED CORROSION IAW DC8 SRM 51-1-8, FABRICATED REPAIR DOUBLER AND FILLER IAW REO 03853 IR. INSTALLED REPAIR IAW REO 03853 IR.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE-C, FS 300, L28L, HAS CRACKED Z-FITTING. REPLACED Z-FITTING, FABBED REPAIR ANGLES IAW DC8 SRM 53-2-0, LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE-C/CK, FS 300 LONGERON 28 LEFT HAND HAS CRACKED Z-FITTING. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-24, FABBED REPAIR ANGLES IAW DC8 SRM 53-2-0, INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-24, INSTALLED FITTING AND ANGLES IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1140)

INSPECTION TYPE-C/CK, CORROSION ON FWD LOWER FLANGE OF FRAME FUSELAGE STATION 1140 BETWEEN LONGERON 33 RIGHT TO 33 LEFT. REMOVED CORROSION OUT OF LIMITS, RECEIVED REO 03814. REMOVED CAP, FABRICATED NEW CAPS AND GUSSETS IAW TIMCO REO 03814. ALODINED AND PRIMED NEW CAP AND GUSSET IAW3 DC8 SRM 51-1-8. INSTALLED NEW CAPS AND GUSSETS IAW TIMCO REO 03814 DC8 SRM 51-1-20D AND 51-1-21.

Part: SKIN — CORRODED (BS 1690-1790)

INSPECTION TYPE-C/CK, EMPENNAGE SKIN CORRODED JUST FWD OF TAIL SKID. REMOVED AND REPLACED LONGERON 36 STA 1690 TO 1790 IAW DC8 SRM 81-3-0, HOLES ON LONGERON TO BE PICKED UP AND DRILLED ON UPS NR 75 1718 INCLUDE SKIN INSTALLTION.

Part: TRACK — DAMAGED (BS 500)

INSPECTION TYPE-C, STA 500 TRACK E DAMAGED. INSTALLED REPAIR BUSHING PER REO 03816.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE-C, CORNER FITTING CRACKED INSIDE NR 3 ALT TANK AT STA 74, LOWER FRONT SPAR. FITTING FABBED AND TREATED ON TIMCO OPS. 50043. INSTALLED FITTING IAW DC8 SRM 51-1-20D. LK CKECK TO BE PERFORMED ON TC NR 1000-03.

Part: FRAME — CORRODED (BS 1140)

INSPECTION TYPE:C/CK, CORROSION ON FWD LOWER FLANGE OF FRAME FS 1140 BETWEEN LONGERON 33 RT TO 33 LEFT 6. REMOVED CORROSION OUT OF LIMITS RECEIVED REO 03814. REMOVED CAP FABRICATED NEW CAPS AND GUSSETS IAW TIMCO REO 03814 ALODINED NEW CAP AND GUSSET IAW DC8 SRM 51-1-8. INSTALLED NEW CAPS AND GUSSETS IAW TI MCO REO 03814 DC8 SRM 51-1-20D AND 51-1-21.

Part: SEAT TRACK — BROKEN (BS 510)

INSPECTION TYPE-C/CK, MAIN CARGO STATION 510 TRACK D FLOOR TRACK PIECE BROKEN. REMOVED BROKEN SECTION STA 420 TO 650, FABBED NEW SECTION AND INSTALLED IAW UPS EO DC8 5320 5167C AND DC8 SRM 51-1-8 AND 53-2-3.

Part: FITTING — CORRODED (FUSELAGE)

INSPECTION TYPE-C/CK, FUSELAGE STATION L29L HAS CORRODED Z-FITTING AND FASTENERS FLC. REMOVED FASTENERS AREA IN Z-FITTING FOUND TO BE CRACKED. REMOVED FITTING, FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. DRILLED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRMN 51-1-20D.

Part: FITTING — CRACKED (LT WING)

INSPECTION TYPE-C/CK, CRACK IN STRINGER ATTACH FITTING XRS 600 SECOND STRINGER AFT OF C-SPAR. REMOVED CRACK STRINGER END FITTING NEW FITTING FABBED ON TIMCO PRINTED OPERATION 50016, DRILLED AND INSTALLED FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D AND 51-3-0, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE-C/CK, FUSELAGE STATION 280 LONGERON 29 LEFT HAS CORRODED Z-FITTING. REMOVED CORRODED Z-FITTING CUT NEW FITTING IAW DC8 SRM 53-2-0 FIG 2D, FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED BARE METAL IAW DC8 SRM 51-1-8, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE-C/CK, FUSELAGE STATION 280 L29L HAS CORRODED Z-FITTING. REMOVED CORRODED Z-FITTING CUT NEW FITTING IAW DC8 SRM 53-2-0 FIG 2 D FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED BARE METAL IAW DC8 SRM 51-1-8, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (BS 320)

INSPECTION TYPE-C/CK, FS 320 L29L HAS CORRODED Z-FITTING AND FASTENERS FLC. REMOVED FASTENERS AREA IN Z-FITTING FOUND TO BE CRACKED. REMOVED FITTING, FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 DRILLED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 86)

INSPECTION TYPE-C, STATION XRS 86.0 STRINGER ATTACH FITTING CRACKED 6 INCHES FWD OF R-SPAR, AFT SIDE OF 1ST STR (NR 2 I/B ALT). REMOVED AND INSTALLED NEW FITTING (FABRICATED ON OPS 50040) IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORROSION (BS 1190-1250)

INSPECTION TYPE-C/CK, FS 1020 TO 1040 CARGO TRACK D HAS CORROSION. REMOVED SEAT TRACK STA 1190 1250 FABRICATED NEW SEAT TRACK IAW DC8 SRM 51-1-24. ALODINED AND PRIMED TRACK AND INSTALLED IAW DC8 SRM 51-3-0, DRILLED SPLICES AND INSTALLED IAW DC8 SRM 51-3-2 AND UPS EO DC8 5320 5167C.

Part: SEAT TRACK — DAMAGED (BS 1620)

INSPECTION TYPE-C/CK, FS 1135 CARGO TRACK F AND G HAS SEAT TRACK DAMAGE. REMOVED OLD SEAT TRACK AT FS 1620 RIGHT HAND TRACK F, FABBED NEW TRACK SECTION FROM EXTRUSION PO 081001051, TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW TRACK FROM FS RIGHT HAND 1620 FS RIGHT HAND 1700 IAW DC8 SRM 51-3-0.

Part: FLOORBEAM — CORRODED (BS 1720)

INSPECTION TYPE-C/CK, CORROSION ON UNDER SIDE OF FLOORBEAM FWD UPPER FLANGE AT STA 1720 BETWEEN L29L TO L29R. REMOVED FLOORBEAM AT FS 1720, FABBED NEW FLOORBEAM FROM 1706317 T EXTRUSION .090 7075 T6 IAW DC8 SRM 53-7-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FLOORBEAM IAW DC8 SRM 51-1-20D.

Part: WEB — CORRODED (BS 1720-1740)

INSPECTION TYPE-C/CK, CORROSION ON WEBBING BETWEEN FS 1720 TO 1740 OUTBOARD END THAT ATTACHED TO FLOOR SUPPORT AT AFT SIDE 1720 ABOVE L35R. REMOVED WEB FABBED NEW WEB IAW DC8 SRM 53-7-1, PRIMED AND ALODINED IAW DC8 SRM 51-1-8, INSTALLED WEB IAW DC8 SRM 51-1-21 AND 51-1-20D AN BD 51-3-0.

Part: SEAT TRACK — CORRODED (BS 980-1705)

INSPECTION TYPE-C/CK, CORROSION ON SEAT TRACK FROM FUSELAGE STATION 980 TO 1705, UNDERSIDE AND AT NUT CLIP HOLES. REMOVED CORROSION FROM STA 980 TO 1270 AND 129 TO 1350. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FOUND CORROSION FROM STA 1350 TO 1700 TO BE OUT OF LIMITS. REMOVED SEAT TRACK FROM FUSELAGE STATION 1350 TO 1700 AND REPLACED IAW UPS EO 5320 5167C.

Part: SUPPORT — CORRODED (BS 1740-1760)

INSPECTION TYPE-C, FLOOR SUPPORT ANGLE AND WEB BETWEEN FS 1740 TO 1760 HAS CORROSION ON UPPER AND LOWER SURFACES. REMOVED CORRODED SUBSTRUCTURE AND SUPPORT IAW DAC DWG 5755038, FABRICATED REPLACEMENT HAT SECTIONS, SUBSTRUCTURE AND SUPPORT IAW DAC DWG 5755038. ALODINED PARTS IAW DC8 SRM 51-1-8. INSTALLED PARTS IAW DC 8 SRM'S 51-1-20D AND 51-1-21.

Part: ANGLE — CRACKED (BS 1740)

INSPECTION TYPE-C, FLOOR SUPPORT ANGLE AT FS 1740 HAS CORROSION ON BOTTOM FLANGE. REMOVED CORROSION, FABBED HAT SECTIONS, STIFFENERS AND SUPPORTS IAW DC8 SRM 51-3-0 AND DAC DWG 5755032. ALODINED, PRIMED AND INSTALLED COMPONENTS IAW DC8 SRM 51-1-8, 51-1-20D AND DAC DWG 5755032.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE-C, STRINGER END FITTING CRACKED AT STA XRS 74 ON LOWER AFT STRINGER IN SIDE NR 3 MAIN TANK. REMOVED CRACKED FITTING, NEW FITTING FABBED ON OP 50015, S/O NR 197067. INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (WS 74)

INSPECTION TYPE-C, UPPER CORNER FITTING CRACKED ON AFT SIDE OF CENTER SPAR, AT STA XRS 74 INSIDE NR 3 TANK. REMOVED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. FITTING FABBED ON TIMCO SO 197067, O PS 50042.

Part: SKIN — CORRODED (BS 55)

INSPECTION TYPE-C, STA 55 RBL 30 SUBFLOOR SKIN BULGED/CRACKED. REMOVED THREE INTERCOSTALS AND FOUR FITTINGS IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8. LOCATED AND DRILLED 3 INTERCOSTALS AND 4 FITTINGS IAW DC8 SRM 51-1-24. REPAIRED FLOORBEAM IAW REO 03777. REMOVED AND REPLACED CUSP FITTING IAW DC8 SRM 51-1-24, 51-1-20D AND 51-3 -0.

Part: SEAT TRACK — CORRODED (BS 980-1705)

INSPECTION TYPE:C/CK, CORROSION ON SEAT TRACK FROM FS 980 1705 UNDERSIDE AND AT NUT CLIP HOLES. REMOVED CORROSION FROM STA 980 1270 AND 1290 TO 1350 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FOUND CORROSION FROM STA 1350 TO 1700 TO BE OUT OF LIMITS. REMOVED SEAT TRACK FROM FS 1350 TO 1700 AND REPLACED IAW UPS EO DC8 5320 5167C.

Part: SEAT TRACK — CORROSION (BS 1190-1250)

INSPECTION TYPE-C/CK, FUSELAGE STATION 1020 TO 1040 CARGO TRACK D HAS CORROSION. REMOVED SEAT TRACK STA 1190 TO 1250, FABRICATED NEW SEAT TRACK IAW DC8 SRM 51-1-24, ALODINED AND PRIMED TRACK AND INSTALLED IAW DC8 SRM 51-3-0, DRILLED SPLICES AND INSTALLED IAW DC8 SRM 51-3-2 AND UPS EO DC 8 5320 5167 C.

Part: SPAR — CRACKED (WS 120)

INSPECTION TYPE-C, L/W LOWER AFT SPAR CRACKED AT STA XW 120. REMOVED 4 HYDRAULIC LINES FOM. REMOVED 2 AUX SPAR FITTINGS, INSTALLED 05, -7 AND -3 FITTINGS AND FILLER IAW DC8 SRM 57-2-6 AND REO 03831 REV A, DC8 SRM 51-1-20A, 51-3-0. REINSTALLED HYD LINES IAW DC 8 MM 20-18-0. LEAK CHECKED GOOD.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-C/CK, INT STA 1140 L 18R CRACK IN FITTING COMMON RADIUS. REMOVED FITTING IAW 3 DC8 SRM 51-1-20D, FABBED NEW FITTING IAW DAC D WG 4750418, DRILLED FITTING IAW DC8 SRM 51-3-2 AND INSTALLED IT DC8 SRM 51-1-20D.

Part: BUKLKHEAD ANGLE — CORRODED (BS 1766)

INSPECTION TYPE-C, THE FWD FACE OF BULKHEAD STA 1766, RT SIDE ATTACHED ANGLE IS CORRODED AT BOTTOM OF BULKHEAD. FABRICATED REPAIR PARTS IAW REO- 03836, TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS PER REO-3836, DC8 SRM 51-1-2 0D AND 51-1-21.

Part: SEAT TRACK — CRACKED (BS 160)

INSPECTION TYPE-C/CK, FWD LOWER CARGO COMPT LEFT HAND TUNNEL AT STA 160, SEAT TRACK BROKEN IN HALF. REMOVED FLOOR TRACK IAW DC8 SRM 51-3-0 AND DC8 5320-5167. FABBED SEAT TRACK IAW DC8 5320 5167 AND INSTALLED WITH SPLICES.

Part: SEAT TRACK — BROKEN (BS 160)

INSPECTION TYPE-C/CK, FWD LOWER CARGO COMPT LEFT HAND TUNNEL AT STA 160 SEAT TRACK BROKEN IN HALF. REMOVED FLOOR TRACK IAW DC8 SRM 51-3-0 AND DC8 5320 5167, FABBED SEAT TRACK IAW DC8 5320 5167 AND INSTALLED WITH SPLICES.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE-C/CK, CENTER FUSELAGE LONGERON TO FRAME ATTACH FITTING CRACKED AT STA 902 LONGERON 19 RIGHT. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATION OF NEW FITTING DONE ON AWR 197067.33 OP NR 50025. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE-C, CTR FUS LONG TO FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: FITTING — CRACKED (BS 905)

INSPECTION TYPE:C/CK CENTER FUSELAGE STATION TO FRAME ATTACH FITTING CRACKED AT STA 902 LONGERON 19 RIGHT. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED OF NEW FITTING DONE ON AWR 197067.33 OPS 50025 LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE-C, CTR FUS LONG TO FRAME ATTACH FITTING CRACKED AT STA 902 L19R. REMOVED FITTING, FABBED NEW ONE ON OPS 50025. DRILLED AND INSTALLED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: FITTING — CRACKED (BS 950)

INSPECTION TYPE-C, CTR FUS FITTING, STA 905, L2R, CRACKED. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1- 20D.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERG LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY BATTERY PACK BAD, NO TEST ON EMERGENCY LIGHT SWITCH. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL IAW 33-50-01.

Part: LONGERON — CRACKED (FS 882)

INSPECTION TYPE 'B', CRACK BEYOND STOP DRILL .5 INCH LONG AT LONGERON 24R FS 882. REPAIRED PER SRM 53-2-2.

Part: FITTING — CRACKED (FS 1200)

INSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 33R TO 34R FWD SIDE. REPLACED FITTING PER SRM 53-2-0.

Part: FITTING — CRACKED (FS 1200)

INSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 28L AFT SIDE. REPLACED FITTING PER SRM 53-2-0.

Part: SLIDE — LOW PRESSURE (MAIN ENTRY)

FWD ENTRY DOOR SLIDE HAS LOW PRESSURE. REPLACED ESCAPE SLIDE ASSY PER MM 25-62-00.

Part: FITTING — CORRODED (AFT BLKHD)

WHILE IN FOR B-CHECK, FOUND FITTING ON STRINGER 32R AT AFT BULKHEAD OF AIRCON COMP IS CORRODED. REMOVED AND REPLACED FITTING.

Part: FITTING — CORRODED (BS 8)

WHILE IN FOR B-CHECK, MAINTENANCE REPORTED LONGERON 34R ATTACH FITTING AT STA 8.00 CRACKED, EVIDENCE OF CORROSION. WILL REPAIR/REPLACE FITTING PER UPS E.O. DC8 SRM.

Part: STRIKER PLATE — BROKEN (RT MLG)

PILOT REPORTED, RIGHT MAIN GEAR ALTERNATE DOOR LIGHT ILLUMINATED AND STAYED ON IN FLIGHT. PERFORMED SECOND UPLATCH CHECK SUCCESSFULLY WITH NO MAIN GEAR DOOR NOT LATCHED ILLUMINATING, APPEARS TO BE ALT SWITCH. FOUND RT SWITCH STRIKER PLATE BROKEN ON RT MAIN GEAR DOOR. REPLACED STRIKER, A/C OK FOR SERVICE.