N315FE

Part: SLIDE — UNKNOWN (L1 DOOR) · airframe 66,750 hrs · 23,419 cycles

RECEIVED CALL FROM RAMP THAT L-1 DOOR WAS ARMED. UPON ENTRY FROM MEC BAY FOUND SLIDE ON FLOOR NOT DEPLOYED. L-1 MAIN ENTRY SLIDE/RAFT REMOVED-EXTENDED OVERWATER OPS REQUIRES TWO SLIDES AND/OR RAFTS. L-1 MAIN ENTRY SLIDE/RAFT REMOVED-EXTENDED OVERWATER OPS REQUIRES TWO SLIDES AND/OR RAFTS. INSTALLED NEW L1 SLIDE/CONTAINER ASSY, REF AMM 25-61-01-2. SLIDE ASSY CHECKS GOOD.

Part: SKIN — CRACKED (ZONE 500) · airframe 65,990 hrs · 23,035 cycles

L/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED A PERMANENT REPAIR IN ACCORDANCE TO SRM VOLUME I CHAPETER 57-00-01 FIGURE 4 (SHEET 2).

Part: SKIN — CRACKED (LT WING) · airframe 65,990 hrs · 23,035 cycles

L/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED A PERMANENT REPAIR IN ACCORDANCE TO SRM VOLUME I CHAPETER 57-00-01 FIGURE 4 (SHEET 2).

Part: SKIN — GOUGED (RT WING TIP) · airframe 65,990 hrs · 23,035 cycles

DEEP GOUGE FOUND ON WING TIP L/E PANEL REPAIR PER E.A. 8-5720-T0352117

Part: SUPPORT BRACKET — WORN (RT WING TE FLAP) · corrosion level 2 · airframe 65,990 hrs · 23,035 cycles

R/H I/B FLAP ACTUATOR SUPPORT BRACKET LOWER END HAS LOOSE HI LOKS BRACKET. REFER TO N/R 797 FOR ANB7394-502 BUSHING REPAIR PER EA T 8-5340-T0352193 P1. RH INBD FLAP, INBD ACTUATOR SUPPORT FITTING ANB7252-502 BUSHING REPAIR PERFORMED PER EA # 8-5340-T0352132. ACCESS TO AND REMOVAL OF FITTING ANB7252-502 PERFORMED IAW SRM 51-31-01, 51-32-01, 51-33-01 VOLII. AFTER BUSHING REPAIR ON ANB7394-502 AND ANB7252-502, ALL PARTS INSTALLED ER DOUGLAS DRWG ANB7393. NOTE, ATTACHMENT FASTENERS FOR ANB7252-502 ON DRWG ANB7393 CALLS FOR HL114 BUT PER SB53-170 SUSTITUTE TO HLT622.

Part: CAP — CORRODED (BS 1368) · airframe 65,990 hrs · 23,035 cycles

CTR W/W CAP P/N AYB7080-7 REQ TO BE FABRICATED FABRICATED NEW CAP SECTIONS A AND B OF AYB7080-7 REF. E.A 8-5310- T0352380 "FUSELAGE-MAINFRAME-BLKHD INST'L AFT PRESS STATION 1368"

Part: SEAT TRACK — CORRODED (BS 1089-1229) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK- SEAT TRACK- CORROSION FOUND FROM STATION 1089 TO STATION 1229, RBL9. REPAIRED DAMAGED SEAT TRACK FROM STATION 1089 TO STATION 1229, RBL9 PER SRM 53- 70-00 FIG. 1 VOL. 1 AND FEDEX DWG SR10-53-002.

Part: FLOORBEAM — CORRODED (BS 1741) · airframe 65,990 hrs · 23,035 cycles

MAIN CAGO DECK AT STA1741 L/H SIDE FLOOR BOAED SUPPORTS AGAINTS WALL HAS CORROSION REMOVED AND REPLACED FLOOR SIPPORT AT STATION 1741, LBL 80 TO 108 PER DAC DWG AFA3853, INSTALLED FLOOR SUPPORT AFA3853-10 PER SRM 51-35-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1501) · airframe 65,990 hrs · 23,035 cycles

MAIN CARGO DECK AT APPROX STA 1501 LBL 9 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #7 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AND SRM 51-31-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1481) · airframe 65,990 hrs · 23,035 cycles

MAIN CARGO DECK AT APPROX STA 1481 RBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #4 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AND SRM 51-31-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1741) · airframe 65,990 hrs · 23,035 cycles

UPPER CARGO, SEAT TRACK APROX STATION 1741 RBL 100 SHOW SIGNS OF CORROSION AROUND SEVERAL NUT PLATES (VIEWED FROM CTR CARGO) REMOVED AND REPLACED FLOOR SIPPORT AT STATION 1741, RBL -80 TO RBL -108 PER DAC DWG AFA3853, INSTALLED FLOOR SUPPORT AFA3853-10 PER SRM 51-35-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1381) · airframe 65,990 hrs · 23,035 cycles

MAIN CARGO DECK AT APPROX STA 1381 LBL 9 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #6 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AND SRM 51-31-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1361) · airframe 65,990 hrs · 23,035 cycles

MAIN CARGO DECK AT APPROX STA 1361 LBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #8 REMOVED AND REPLACED CORRODED FLOOR SUPPORT AEA0394-1 REF DAC DWG NEA6018 AND SRM 51-31-01 VOL. 2.

Part: FLOORBEAM — CORRODED (BS 1741) · airframe 65,990 hrs · 23,035 cycles

UPPER CARGO- APROX STATION 1741 RBL 118, FLOOR BOARD SUPPORT SHOWS SIGNS OF CORROSION (VIEWED FROM CTR CARGO) REMOVED AND REPLACED FLOOR SIPPORT AT STATION 1741, RBL -80 TO RBL -108 PER DAC DWG AFA3853, INSTALLED FLOOR SUPPORT AFA3853-10 PER SRM 51-35-01 VOL. 2.

Part: FLOOR SUPPORT — CORRODED (BS 1361) · airframe 65,990 hrs · 23,035 cycles

MAIN CARGO DECK AT APPROX STA 1361 RBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #3 REMOVED AND REPLACED CORRODED FLOOR SUPPORT AEA0394-1 REF DAC DWG NEA6018 AND SRM 51-31-01 VOL. 2.

Part: ACCESS PANEL — CORRODED (MLG WW) · airframe 65,990 hrs · 23,035 cycles

CENTER WHEEL WELL - LOWER AUX TANK ACCESS PANEL LOWER LANDING (AIRCRAFT SIDE) HAS COROSSION IN NUMEROUS AREAS. (AREAS MARKED) REMOVED CORRODED LOWER CAP AYB7080-7 AND INSTALLED NEW AYB7080-7 SECTIONS A AND B REFERENCE EA. 8-5310-T0352380 "FUSELAGE-MAINFRAME-BUKHD INST'L AFT PRESS. STATION 1368."

Part: FRAME — GOUGED (BS 469) · airframe 65,990 hrs · 23,035 cycles

AVIONICS COMPARTMENT, NO. 1 RAM AIR DUCT RED COUPLING/BOOT, LOWER BOLT IS CONTACTING AND GOUGING AIRCRAFT FRAME. MARKED WITH DOT #20. LOCATED AFT OF THE MAIN AVIONICS RACK, FORWARD AND LEFT OF REFRIGERATOR DOOR. REPAIRED DAMAGED PER E.A. # : 8-5310-T0352200, FUSEALAGE- MAIN FRAME- WEAR DAMGED ON FRAME FROM AIR BOOT FASTENER HEAD.

Part: FLOORBEAM — CORRODED (BS 1750) · airframe 65,990 hrs · 23,035 cycles

LOWER CTR CARGO PIT AT DOOR ENTRY STA. 1750 CEILING FLOOR BEAM HAS CORROSION ON LOWER LEG OF I-BEAM REMOVED & REPLACED CEILING FLOOR I-BEAM LOWER LEG AFA7509-5, REF. DAC DWG 7509 & MD10 SRM 51-31-01, VOL 2, PG 23

Part: SPAR — CRACKED (RT WING) · airframe 65,990 hrs · 23,035 cycles

R/H WING REAR SPAR LOWER SURFACE, FILLER STRIP CRACKED AT STA XORS 408. MARKED DOT #1. REMOVED CRACKED FILER STRIP SILL FROM I/B END TO NEW CUT LOCATION BETWEEN ORIGINAL CRACK AND NEXT FASTENER O/B. FABRICATED AND INSTALLED NEW SECTION OF ARC7008-2 SILL. REFERENCE E.A. 8-5710-T0352034 "WING STRUCTURE-RH LOWER SILL AT APAR XORS419"

Part: DOUBLER — CRACKED (LT WING LE) · airframe 65,990 hrs · 23,035 cycles

LH WING LEADING EDGE INTERNAL AT APPROX XORS 568 - INNER BEADED DOUBLER HAS SIX (6) CRACKS. DAMAGED CONFIRMED USING NDT HFEC. REPAIRED CRACKED ,(6)PLACES,INNER BEADED DOUBLER WITH ADDITIONAL DOUBLER. DC-10 SRM 57-10-00 VOL I FIG.71 PG.222

Part: BULKHEAD WEB — CORRODED (BS 1521) · corrosion level 2 · airframe 65,990 hrs · 23,035 cycles

INSIDE CLG WW, AFT BULKHEAD STA 1521, L/H SIDE, ATTACHING HORIZONTAL CHANNEL SECTION IS CORRODED THROUGH. POSSIBLE CORROSION ON AREA OF BULKHEAD COVERED UP BY CHANNEL. (MKD) REFER EA T 8-5315-T0352087, AND N/R 253 WORK ORDER 76085. REMOVED, FABRICATED AND REINSTALLED NEW CHANNEL. REF DAC DRAWING AEA7055. VERIFIED CORROSION ON BULKHEAD Y=STA1521 WAS REMOVED AND REPAIRED IAW EA# T 8- 5315-T0352087.

Part: SEAT TRACK — WORN (BS 635-659) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK: APPROX STA 635, RBL 8, SEAT TRACK LOBE WORN (IS CRESCENT SHAPED). (MARKED AND DOT 64) REPAIRED DAMAGED SEAT TRACK FROM STATION 635 TO STATION 659, RBL8 PER SRM 53- 70-00 FIG. 1 VOL. 1 AND FEDEX DWG SR10-53-002.

Part: SEAT TRACK — WORN (BS 795-828) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK: APPROX STA 795, RBL 28, SEAT TRACK LOBE WORN BEYOND LIMITS (MARKED AND DOT 62) REPLACED DAMAGED SECTION OF SEAT TRACK AT STA 795, RBL 28, REF SRM 53-70-00,FIG 1, VOL 1.

Part: SEAT TRACK — WORN (BS 1821) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1821, LBL 47 IS WORN. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1811 TO STA. 1831, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG

Part: SEAT TRACK — CORRODED (BS 1180-1190) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1180-1190, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1190 TO STA. 1190, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG

Part: SEAT TRACK — CORRODED (BS 1200-1210) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1200-1210, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1200 TO STA. 1210, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG

Part: SEAT TRACK — WORN (BS 1721-1741) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1721, LBL 47 IS WORN. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1721 TO STA. 1741, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG.

Part: SEAT TRACK — CORRODED (BS 1100-1129) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1100-1129, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1100 TO STA. 1129, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG

Part: SEAT TRACK — CORRODED (BS 1125-1140) · airframe 65,990 hrs · 23,035 cycles

MAIN DECK - SEAT TRACK - AT STA 1125-1140, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1125 TO STA. 1140, LBL 47, PER SRM 53-70-00 FIG. 1 VOL. 1, AND SRM 51-31-01 VOL. 2 ALSO SR10-53-002 DWG

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,261 hrs · 22,166 cycles

EMERGENCY LIGHT TEST. EMER LT BAT 1 LO ALERT. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY WITH CPN 3300197 S/N 1027 IAW AMM 33-51-01-4-1. OPS CHECKS NORMAL IAW AMM 33-51-01-5.

Part: CONNECTOR — DAMAGED (EVAC SLIDE) · airframe 63,952 hrs · 22,013 cycles

L1 DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM INOP. FOUND BATTERY SOLDER CONNECTION TO BE DISCONNECTED. RE-SOLDERED CONNECTION SLIDE LIGHT OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 63,054 hrs · 21,535 cycles

DURING PREFLIGHT, DISCOVERED THE R1 DOOR SLIDE BOTTLE PRESSURE NOT IN THE GREEN BAND. SERVICED THE BOTTLE IAW AMM 52-11-07-2

Part: WIRE — BROKEN (CONNECTOR) · airframe 62,980 hrs · 21,496 cycles

LEVEL 1 BRAKE DIFFERENTAL TEMP AT 30 MINUTES INTO FLIGHT FL380 SAT -56 BRAKE TEMP WHEEL 6 FLUCTUATING RAPIDLY BTWN 330-375. AT 40 MIN INTO FLIGHT LVL 2 BRAKE OVERHEAT ILLUMINATED MAX TEMP 575. COMPLIED W/QRH TEMP SUBSIDED TO APPROX 370 AND FLUCTATED THERE WITH LVL 1 BRAKE DIFF TEMP PERSISTING UNTIL 2:20 INTO FLIGHT. NO. 6 BRAKE TEMP HELD AT 300 ALL OTHER BRAKE TEMPS MATCHED AT -15 DEG THROUGHOUT. FOUND WIRE BROKEN ON THE NR 6 BRAKE TEMP SENSOR CONNECTOR. REPAIRED THE CONNECTOR IAW SWPM 20-31-00. BRAKE INDICATION READS NORMAL.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 62,922 hrs · 21,469 cycles

LEFT WING OTBD FLAP UPPER SURFACE SKIN XOF 563, HAS A 2.25 INCH CRACK. CONFIRMED BY HFEC. INSTALLED A FILLER AND DOUBLER IAW SRM 57-20-01, FIG 4, SHEET 2, VOL 1, AND SRM 51-35-02.

Part: FLOOR SUPPORT — CORRODED (BS 715) · corrosion level 2 · airframe 62,922 hrs · 21,469 cycles

FLOOR SUPPORT AT BS 715 RBL 63 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01 VOL II

Part: ROLLER TRAY — CORRODED (BS 959-1099) · airframe 62,922 hrs · 21,469 cycles

FWD CARGO BAY, BS 959 - 1099 ROLLER TRAY CORRODED AT THE LOCKS AND ROLLER AREAS. MAJOR REPAIR. REPAIRED IAW SRM 51-31-01, VOL.2, AND DWG NDJ6230.

Part: FLOOR SUPPORT — CORRODED (BS 715) · corrosion level 2 · airframe 62,922 hrs · 21,469 cycles

MAIN CARGO FLOOR SUPPORT AT BS 715, RBL 63 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01, VOL II

Part: CARGO TRACK — WORN (BS 1640) · airframe 62,922 hrs · 21,469 cycles

MAIN CARGO BAY, BS 1640, RBL 47.50, CARGO TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-70-00, FIG 1 VOL. 1, SHEET 1, AND SRM 51-31-01, VOL II.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK LBL 75.25 NEAR STA 740 SEAT TRACK WORN. REPAIRED DAMAGE SEAT TRACK AT LBL75.25 STA 740 REFERENCE SRM 53-70-00 FIGURE 2A PAGE II VOL I.

Part: SKIN — GOUGED (BS 2139) · airframe 62,922 hrs · 21,469 cycles

TWO GOUGES IN SKIN UNDER HORIZONTAL STABILIZER, BS 2139. BLENDED GOUGES AND INSTALLED A REPAIR DOUBLER IAW SRM 53-20-00, FIG 22, VOL 1.

Part: SEAT TRACK — WORN (BS 791) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK STA791 RBL47.50 WORN BEYOND LIMITS REPAIRED SEAT TRACK @ STA791 RBL47.50 PER SR10-53-501

Part: SEAT TRACK — WORN (BS 1240) · airframe 62,922 hrs · 21,469 cycles

MAIN CABIN APPRO. STA. 1240 X-= 47.50, SEAT TRACK UPPER SURFACE , NICKED /GOUGED PAINT PEELNG REMOVED AND REPLACED SEAT TRACK REF. SRM 53-70-00 FIG 1 VOL 1 AND 51-31-01 VOLI

Part: SEAT TRACK — DAMAGED (BS 1375) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK LBL 47.50 NEAR STA. 1375 DAMAGED REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1

Part: SEAT TRACK — DAMAGED (BS 1380) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK LBL 47.50 NEAR STA 1380 DAMAGED REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1

Part: SEAT TRACK — DAMAGED (BS 1638-1650) · airframe 62,922 hrs · 21,469 cycles

UPPER MAIN DECK SEAT TRACK RBL 27.50 NEAR BS 1635 TO 1650 DAMAGED. REPLACED THE SEAT TRACK SECTION IAW SRM 53-70-00, FIG 1, VOL 1. MAJOR REPAIR.,

Part: SEAT TRACK — DAMAGED (BS 1365) · airframe 62,922 hrs · 21,469 cycles

MAIN DEACK SEAT TRACK LBL 47.50 NEAR STA. 1365 DMAGED REMOVED AND REPLACED DMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL. 1

Part: NONE — NONE (NONE) · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: LOWER FUSELAGE SKIN, STA. 1781, LONG. 41R, AFT LOWER SIDE OF CENTER CARGO DOOR JAMB, HAS AN EXISTING REPAIR DOUBLER. DOT 17. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-50-00 FIG. 26 SH.3 VOL.1. REF. E.A. 8-5100-T0336013 "REPAIR CATALOG MD10 REPAIR ID" ATTACHMENT A-1 #17.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,922 hrs · 21,469 cycles

RIGHT WING LE INTERNAL SKIN AT XORS 695 BEADED DOUBLER HAS TWO CRACKS, 1.25 INCH AND .75 INCH. CONFIRED CRACKS USING NDT HFEC. REPAIRED THE R/H WING L/E SKIN BEADED DOUBLER IAW SRM 57-10-00, FIGURE 71, VOL 1.

Part: FLOOR SUPPORT — CORRODED (BS 1099) · airframe 62,922 hrs · 21,469 cycles

FWD CARGO BAY BS 1099, RBL 47 - 49 AFT BULKHEAD FLOOR SUPPORT ANGLE CORRODED ON THE UNDERSIDE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG ADA 7667.

Part: SKIN — WORN (BS 2150) · airframe 62,922 hrs · 21,469 cycles

AFT, R/H FUSELOGE, ABOVE AND AFT OF HORIZ, STA 2150, 4 NUTPLATE NUTS WORN THROUGH NUTPLATE AND SKIN. SRM 53-20-00, FIG 22 VOL 1. REPAIRED NUTPLATES PER EA # 8-5320-T0337311, PART # 1 AND SRM 53-20-00 FIG 22 VOL 1

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,922 hrs · 21,469 cycles

STA APPROX 2150, AFT ACESSORY COMPARTMENT, R/H SIDE, RUSTED NUTPLATES AND CRACK/CORROSION. NOTE: NUTPLATES HOLD ON FILLET PANEL # AJC7470-4, LOWER NUTPLATES. WORK IN CONJUNCTION WITH NR#374. REPAIRED PER SRM CH 53-20-00,FIG 22, V1.

Part: BLOCK — CRACKED (MLG) · airframe 62,922 hrs · 21,469 cycles

CENTER LANDING GEAR, L/H PILLOW BLOCK WAS FOUND CRACKED. REMOVED AND REPLACED PILLOW BLOCK. REF WC 32T7701-C. CMM 32-15-01.

Part: NONE — NONE · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK , AT APPROXIMATE STA. 905, RBL 47, HAS AN EXISTING SEAT TRACK PLUG REPAIR. DOT 94. EXISTING SEAT TRACK REPAIR PREVIOUSLY INSTALLED IN REFERENCE TO SRM 53-70-00 FIGURE 2, SHEET 1,2.

Part: NONE — NONE (NONE) · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK, AT APPROXIMATE STA. 1331, RBL 47, HAS AN EXISTING SEAT TRACK PLUG REPAIR. EXISTING SEAT TRACK REPAIR PREVIOUSLY INSTALLED IN REF. TO SRM 53-70-00 FIGURE 2 SHEET1

Part: PANEL — WORN (ZONE 400) · airframe 62,922 hrs · 21,469 cycles

NR 2 ENGINE LT LOWER FWD EDGE OF INLET HAS HEAVY WEAR FROM FAN COWL WHEN CLOSED. FABRICATE AND INSTALLED AJC7415-95 PANEL PER DAC DRAWING AJC7415.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 62,922 hrs · 21,469 cycles

FWD CARGO COMPARTMENT BILGE - STA 791, LBL 17, FLOOR SUPPORT IS CRACKED. (MARKED) REMOVED AD REPLACED FLOOR SUPPORT PER DOUGLAS DRAWING#ADA-0235.

Part: NONE — NONE · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: LEFT WING, FIXED LEADING EDGE, UPPER SURFACE, AT APPROX. STA. XFS 235, HAS AN EXISTING DOUBLER, APPROX. 10X7 INCHES. DOT 17. REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-10-00 FIG. 15A SH.1 VOL.1 . REF E.A. 8-5100- T0336014 "REPAIR CATALOG MD10 REPAIR ID" ATTACHMENT A-1 #17. "MAJOR REPAIR"

Part: SKIN — DAMAGED (BS 545) · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: LOWER FUSELAGE, STA. 545, LONG. 42R, HAS AN EXISTING DOUBLER AT AFT UPPER CORNER OF ACM EXHAUST CUT-OUT. DOT 5. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-20-00 FIG. 2 VOL.1 REFERENCE E.A. 8-5100-T0336013 "REPAIR CATALOG MD10 REPAIR ID" ATTACHMENT A-1 #5.

Part: NONE — NONE (NONE) · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: LOWER FUSELAGE, RIGHT SIDE , AT APPROX. STA. 755, LONGERON 42R- 43R, HAS AN EXISTING SKIN REPAIR APPROX. 9X12 INCHES. DOT 11. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-20-00 FIG. 6 SH. 7 VOL.1. REFERENCE E.A. 8-5100-T0336013 "REPAIR CATALO-MD10 REPAIR ID" ATTACHMENT A-1 # 11. REPAIR WAS PREVIOUSLY INSTALLED ON W.O. 67397, N00064 AT 20491 CYCLES. INITIAL INSPECTION DUE BY 35,491 CYCLES.

Part: NONE — NONE (NONE) · airframe 62,922 hrs · 21,469 cycles

REPAIR ASSESSMENT: LEFT WING, INBOARD FLAP, LOWER SURFACE, AT APPROX. STA. XIFH 190, HAS AN EXISTING SKIN SPLICE REPAIR. DOT 22. EXISTING REPAIR PREVIOUSLY INSTALLED IN REFERENCE TO SRM 57-10-00 FIG 3.

Part: SKIN — CRACKED (RT WING) · airframe 62,922 hrs · 21,469 cycles

RIGHT WING SKIN AT ANTI-ICE TELESCOPING DUCT CUT OUT UPPER INBOARD CORNER HAS A 1 INCH CRACK. INSTALLED A REPAIR DOUBLER IAW SRM 57-10-00, FIG 103, SH 2 VOL 1.

Part: FILLET — WORN (HORIZONTAL STAB) · airframe 62,922 hrs · 21,469 cycles

EXTERIOR FUSELAGE; RH HORIZONTAL AFT FILLET AJC7470-4 HAS NUMEROUS MISSING/LOOSE FASTENERS. REMOVED AND REPLACED NUMEROUS LOOSE/MISSING FASTENERSAND NUTPLATES ON JPF, STEPS 1 & 2

Part: PANEL — CHAFED (RT WING SLAT) · airframe 62,922 hrs · 21,469 cycles

RIGHT SLAT NR 8 OTBD END SEAL FASTENERS CHAFING AGAINST WING EXHIBIT GOUGES. REMOVED AND REPLACED THE RT WING L/E PANEL ARB4304-2 IAW DWG ARB4302. REPAIRED AND INSTALLED AND OPS CHECKED GOOD. IAW AMM 27-80-01-4.

Part: ROLLER TRAY — CORRODED (BS 599-1099) · airframe 62,922 hrs · 21,469 cycles

FWD CARGO BAY, BS 959 - 1099 ROLLER TRAY CORRODED AT THE LOCKS AND ROLLER AREAS. REMOVED AND REPLACED THE ROLLER TRAY IAW SRM 51-31-01. FOUND TO BE BEYOND LIMITS IAW SRM 51-21-02, VOL 2, PAGE 6, PARA (I). FABRICATED IAW DWG ADJ7036, INSTALLED IAW ADJ6230 AND SRM 51-31-01, V 2.

Part: SEAT TRACK — WORN (BS 879) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK BS 879 X=27.50 LBL WORN BEYOND LIMITS. REPLACED THE SEAT TRACK FROM BS 869 TO 909 IAW SRM 53-70-00, FIG 1, VOL 1, AND DRAWING SR10-53-002.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK RBL 47.50 NEAR STA 1501 SHOWS SEVERAL SEAT TRACKS DAMAGED. REPLACED DAMAGED SEAT TRACK FROM STA 1491 TO STATION 1551, RBL 247.5 REF SRM 53-70-00 FIG 1 VOL 1 AND DRAWING SR10-53-002.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK LBL 27.50 NEAR STA 1520 DAMAGED. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA 1401 TO 1531 LBL 27. REF SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-01 VOL 2.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK RBL 27.50 NEAR STA 1521 DAMAGED. REMOVED MARKED DAMAGED PART OF THE SEAT TRACK AND PLUGGED SEAT TRACK AT MAIN DECK, RBL 27.50 NEAR STA 1521 IN REF TO SRM 53-70-00 FIG 2A, PAGE 11 AND DWG SR10-53-501.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK STA 595 X= -27.50 RBL SHOWS LIGHT WEAR. REMOVE AND REPLACED SECTION OF SEAT TRACK BETWEEN STA 585 AND STA 645 AT RBL 27.50 IN REF TO SR10-53-501 AND SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (BS 1635-1643) · airframe 62,922 hrs · 21,469 cycles

MAIN DECK SEAT TRACK RBL 8.50 NEAR BS 1635 DAMAGED. REPAIRED IAW SRM 53-70-00, PAGE 9, FIG 2, SHEET 1, VOL. 1, AND DWG SR-10-53-501.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,922 hrs · 21,469 cycles

R/H HORZ STAB UPPER AFT SKIN PANEL HAS A .75 IN. CRACK FWD OF THE REAR SPAR FWD BARREL NUT HOLE. STOP DRILLED CRACK REF WORK CARD 55X1203ALI-P4. CRACK WITHIN LIMITS. MINOR REPAIR.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,922 hrs · 21,469 cycles

R/H HORZ STAB UPPER AFT SKIN PANEL HAS A .75 IN. CRACK FWD OF THE REAR SPAR FWD BARREL NUT HOLE. (ENDS MARKED)

Part: TRIM MOTOR — LEAKING (STABILIZER) · airframe 62,795 hrs · 21,407 cycles

HYD 3 FAIL" LVL 2 ALERT RIGHT AFTER LEVEL OFF AT FL330. HYD LEVEL SLOWLY BLED TO ZERO. COMPLIED WITH QRH. REMOVED AND REPLACED HYDRO SYSTEM NR 3 STAB TRIM MOTOR IN REFERENCE TO AMM 27-43-01-2, OPS CHECKS GOOD. SERVICED NR 3 SYSTEM HYDRAULIC RESERVOIR PER AMM 12-13-02-3, NO LEAKS OR FAULTS AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 NACELLE) · airframe 62,686 hrs · 21,359 cycles

AT 5000 FT, RECEIVED A NR 1 ENGINE FIRE INDICATION. RAN QRH AND SHUT DOWN THE NR 1 ENGINE. NO ABNORMAL ENGINE PARAMETERS OBSERVED. FIRED BOTH FIRE BOTTLES. CHECKED THE NR 1 ENGINE FIRE HANDLE ADJUSTMENT IAW MM 26-20-00-5, AND 76-20-01-2, ALL CHECKED GOOD. CHECKED THE NR 1 ENGINE FIRE EXINGHUSHING SYSTEM IAW MM 26-21-02-4, CHECKED GOOD. FIRE DETECTION SYSTEM FAULT COMPLIED WITH ON WRI 26-10/4773. AIRCRAFT OK FOR SERVICE.

Part: THERMOCOUPLE — MALFUNCTIONED (EGT) · airframe 62,674 hrs · 21,352 cycles

DURING CLIMBOUT, RECEIVED A LEVEL 1 NR 2 ENGINE EXCEDENCE. NR 2 EGT MOMENTARY BETWEEN 800-900, PULLED NR 2 THROTTLE TO IDLE, EGT DECREASED TO NORMAL. EGT NEEDLE JUMPED WIDELY THROUGH FULL RANGE OF EGT & X INDICATION FOR 30 SECONDS. GAUGE REACHED 1055 DURING RAPID NEEDLE MOVEMENT AFTER PULLING TO FLIGHT IDLE GAUGE APPEARED NORMAL, READ 100 DEGREES HOTTER THAN NR 1 AND NR 3 EGT ON GROUND. ACCOMPLISHED AN EGT RESISTANCE CHECK IAW EO 8-7257-7-5004, PT 3, AND AMM 77-21-01-2. FOUND SOME MARGINAL READINGS ON HARNESSES, R & R ALL EGT THERMOCOUPLE HARNESSES IAW AMM 77-21-01-2-0, R & R EGT THERMOCOUPLE LEADS IAW AMM 77-21-02-2. RAN NR 2 AND 3 ENGINES IAW JRH, NO FLUCTUATIONS IN EGT , OPS CHECKED GOOD.

Part: SUPPORT FITTING — CORRODED (BS 1376) · corrosion level 2 · airframe 62,429 hrs · 21,221 cycles

CORROSION FOUND ON SUPPORT FITTING, FOUND TO BE OUT OF LIMITS. FABRICATED A NEW SUPPORT FITTING IAW DRAWING AEA 7301-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,079 hrs · 21,045 cycles

DURING A WALK AROUND INSPECTION, FOUND A DENT IN THE FUSELAGE, 14 INCHES FWD OF THE ACCESSORY DOOR. INSTALLLED A REPAIR IAW 53-20-00.

Part: SKIN — DAMAGED (LT WING SLAT) · airframe 61,380 hrs · 20,745 cycles

LEFT WING FIXED LEADING EDGE NR 2 INBOARD SLAT TOP SKIN HAS A CHAFED HOLE. REPAIRED IAW SRM 57-10-00 FIGURE 15A, SHEET 1.

Part: CONNECTOR — DAMAGED (COCKPIT) · airframe 60,894 hrs · 20,511 cycles

SPARKS FROM THE BOOT AT THE BOTTOM OF THE CO-PILOTS YOKE. RETERMINATED CONNECTOR R5-932 AT F/O'S CONTROL COLUMN. REF STD MX PRACTICES AND WDM 31-31-11. SECURED R5-932 AND CONTROL COLUMN BOOT. F/O CONTROL WHEEL POSITION READOUT NORMAL. REF MM 31-31-00-5. OK FOR SERVICE.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 59,733 hrs · 20,033 cycles

MCD TWO EACH INNER SKINS HAVE DAMAGE BELOW DOOR ACTUATOR CUT OUT. INSTALLED PN ACA7326-5 IAW DWG ACA7326 & SRM 52-10-01 FIG 9.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

CENTER CARGO COMPARTMENT, STATION 1741 CTR FLOOR LOCK, UNDERNEATH SUPPORT FLOORBEAM IS CRACKED IN RADIUS. REPAIRED IAW SRM 53-00-01 FIG 9.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN CABIN APPROX STATION 1260, RBL 48, SEAT TRACK LUG OBLONG, INCLUDING IMPROPERLY DRILLED FLOOR BOARD HOLES ON SEAT TRACK. R & R DAMAGED SEAT TRACK IAW SRM CH 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN CABIN APPROX STATION 126, RBL 48, SEAT TRACK LUG OBLONG, INCLUDING IMPROPERLY DRILLED FLOOR BOARD HOLES ON SEAT TRACK. R & R DAMAGED SEAT TRACK IAW SRM CH 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN CABIN SEAT TRACK LOBE DAMAGED. APPROX STATION 600 - 615, LBL 48.00. R & R SEAT TRACK IAW SRM 53-70-00 VOLUME 1.

Part: PULLEY — DAMAGED (L1 DOOR) · airframe 59,733 hrs · 20,033 cycles

L1 DOOR UPPER 3 EACH PULLEYS ARE DAMAGED DUE TO STRIPPED CABLE COATING. R & R 3 EACH CABLE PULLEYS FROM L1 UPPER IAW MM 20-50-02-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 600 LT, X=27.50. R & R SEAT TRACK, MAIN DECK STATION 600 LT, X=27.50 IAW SRM 53-70-0 VOLUME 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1500 - 1510, LBL12. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM CH 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1500 - 1510, RBL12. R & R DAMAGED SECTION IAW SRM CH 53-70-00.

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 59,733 hrs · 20,033 cycles

LEFT HORIZONTAL STAB, NR 2 LE OTBD FLANGE, INBD LOWER SIDE OF FLANGE IS CRACKED. R & R ALC 7052-17 FLANGE IAW DWG ALC7052.

Part: SUPPORT — CRACKED (TEF FLAP) · airframe 59,733 hrs · 20,033 cycles

RT OUTBOARD FLAP, INBOARD HINGE FITTING SUPPORT CRACKED AT STA XOSP 557. REMOVED AND REPLACED HINGE FITTING SUPPORT REF TO EA 8-5710-T0322765.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,733 hrs · 20,033 cycles

MAIN CABIN SEAT TRACK LUG OBLONG, APPROX STATION 1381, RBL 36. R & R SEAT TRACK IAW SRM 53-70-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 589 hrs · 19,703 cycles

DURING THE EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW ALERT. R & R THE BATTERY PACK IAW MM 33-51-01-4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 590 hrs · 19,710 cycles

DURING THE EMERGENCY LIGHT TEST RECEIVED A LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW ALERT. R & R BATTERY PACK IAW MM 33-51-01-4. OPS CHECKED IAW MM 33-51-01 501. OPS CHECKED NORMAL.

Part: CAP — DAMAGED (RUDDER) · airframe 57,334 hrs · 18,955 cycles

AFT UPPER RUDDER TE TIP HAS LIGHTNING STRIKE. R & R AFT UPPER RUDDER CAP & STATIC WICK IAW SRM 51-31-01. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,334 hrs · 18,955 cycles

FUSELAGE BELLY SKIN AFT OF TACAN ANTENNA BETWEEN BS 808 - 840 STRINGER 50L - 50R HAS CREASE. EVALUATED DENT LIMITS IAW SRM 53-20-00 FIG 13 SH 2. SUBMITTED EA FOR PROXIMITY OUT OF LIMIT. ACCOMPLISHED EA 8-5330-T0309756 PART 1 FUSELAGE PLATES & SKINS FUSELAGE BELLY SKIN DENT AFT AF TACAN ANTENNA. PART 2 INSPECTION INTERVAL AT NEXT C CHECK & PART 3 INSPECTION INTERVAL AT FOLLOWING C CHECK. MAJOR REPAIR.

Part: PLATE — GOUGED (LT WING) · airframe 57,334 hrs · 18,955 cycles

LEFT WING INBD TE ADJACENT TO OTBD FLAP VANE. METAL STRIKE PLATE HAS GOUGE. BLENDED LT WING INBD TE METAL STRIKE PLATE. LENGTH = 3.3 INCHES, WIDTH = 1.9 INCHES & DEPTH = 0.0295 INCHES. FOUND ACCEPTABLE IAW EA 8-5750-T0309660 PS P1. MINOR REPAIR.

Part: RIB — DAMAGED (RT AILERON) · airframe 57,334 hrs · 18,955 cycles

RIGHT OTBD AILERON OTBD END OF TE WEDGE X948 DISBONDED & LOOSE. REMOVED TE CLOSE OUT RIB IAW SRM 51-31-01. FABRICATED NEW CLOSE OUT RIB ON T14 1079273. INSTALLED NEW CLOSE OUT RIB IAW SRM 51-35-01. BROKEN CLOSE OUT RIB CAUSED THE APPEARANCE OF DELAMINATION. MAJOR REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,334 hrs · 18,955 cycles

GOUGED MARK ON FUSELAGE SKIN AT FWD CARGO DOOR CUT OUT LOWER FWD CORNER. NO ALLOWABLE DAMAGE ON AN EXISTING REPAIR. R & R NR 1 DOUBLER ON EXISTING REPAIR IAW SRM VOL I 53-50-00 FIG 26 SHT 3. MATERIAL IS 2024-T3 .090C BATCH 2540972. SKIN PN IS ADA3139-501 STATION 890 LONGERON 39R TO 42R. MAJOR REPAIR.

Part: SKIN — DAMAGED (RUDDER) · airframe 57,334 hrs · 18,955 cycles

MULTIPLE LIGHTNING STRIKES AT LT SIDE OF UPPER AFT RUDDER NEAR THE TIP. REMOVED, RE-INSTALLED & PERFORMED FUNCTIONAL CHECK UPPER AFT RUDDER IAW AMM 27-20-02-4, CHECKED GOOD. FABRICATED DOUBLER STRAP & SKIN REPAIR IAW SRM 55-10-00 & 55-31-01 & CHECKED CLEARANCE BETWEEN AFT UPPER & AFT LOWER RUDDER IAW AMM 27-20-02-6. FOUND WITHIN LIMITS EA 8-5540-T0309622 REV NO PS P1 ESTABLISHED FOR TRACKING RSC. MAJOR REPAIR.

Part: SKIN — GOUGED (TE FLAP) · airframe 57,334 hrs · 18,955 cycles

RIGHT INBD FLAP UPPER SKIN GOUGED AT NUMEROUS LOCATIONS, XIFH 250 - 295. BLENDED UPPER SKIN DAMAGE AREA DIM L=.100", W=.050", D=.002". L=.100", W=.050", D=.002". L=.150", W=.100", D=.003". L=.100", W=.080", D=.002". L=.100", W=.080", D=.002". FOUND TO BE IN LIMITS IAW SRM 57-00-01 FIG 1A. DIM L=.800", W=.300", D=.050". L=1.0", W=.200", D=.022. L=1.5", W=.500", D=.045" FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 FIG 1A. REPAIRED THREE EACH UPPER SKIN DAMAGE AREAS IAW SRM 57-00-01 FIG 4. PN NRC6055-506, SN 48313, SKIN PANEL PN IS ARC2735-502. MAJOR REPAIR. EA 8-5750- T0309601 B PT1 ESTABLISHED FOR RSC TRACKING.

Part: PANEL — CHAFED (RT HORIZ STAB) · airframe 57,334 hrs · 18,955 cycles

RIGHT HORIZONTAL STAB PNL 352BZ HAS CHAFING WEAR. EVALUATED CHAFE, FOUND CHAFE MARK LESS THAN 2D FROM FASTENER HOLE. FOUND TO BE OUT OF LIMITS IAW SRM VOL 1, 55-00-01, FIG 1A SHT 1. FABRICATED NEW PANEL ON TR T14 1078626, 7075-T6, BATCH 0001689641. TRANSFERRED STIFFENER FROM DAMAGED PANEL TO NEW PANEL IAW SRM VOL 2 51-31-01. CATEGORY A MAJOR REPAIR.

Part: STIFFENER — CRACKED (NR 3 PYLON) · airframe 57,334 hrs · 18,955 cycles

NUMBER 3 ENG PYLON AFT LOWER FAIRING HAS CRACK ON LAST TWO STIFFENERS. REMOVED CRACKED RIBS TWO EACH IAW SRM VOL II 51-31-01. GENERATED & REVISED EA 8-5480-T0309537 P1. WELDED CRACKS ON TRAVELER'S T14 1079877 & T14 1079876. LOCATED, DRILLED & INSTALLED TWO EACH RIBS IAW SRM 51-31-01. MINOR REPAIR. PN OF THE TWO RIBS ARE AUB7375-47 & AUB7375-49. CRACK LENGTHS WERE .4 & .55 INCHES.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 57,334 hrs · 18,955 cycles

FUSELAGE SKIN AFT OF AFT CARGO DOOR CUT OUT LOWER CORNER HAS THREE EACH DENTS. MEASURED DENTS IN SKIN L 087 X D 040, L 087 X D 039, L1.10 X D.10 FOUND ALL THREE ARE OUT OF LIMITS IAW SRM 53-20-00, FIG 13 TABLE A VOL 1. CUT OUT DAMAGE IAW SRM 53-50-00 FIG 26 SH 3. FABRICATED FILLER & DOUBLER 2 USING 2024-T3 071C BATCH 2530701. FABRICATED DOUBLER 1 USING 2024-T3 .080C BATCH 2627022. TREAT & PRIMED IAW SRM 53-50-00 FIG 26 SH 4 STEPS 1 - 7. INSTALLED FILLER & REPAIR DOUBLERS IAW SRM 53-50-00 FIG 26 STEPS 8 - 14A. TOUCHED UP & PAINTED AREAS IAW SRM 51-21-01. MAJOR REPAIR.

Part: SKIN — WORN (FUSELAGE) · airframe 57,334 hrs · 18,955 cycles

AFT FUSELAGE ACCESS DOOR 311AB CUT OUT UPPER SURFACE HAS WEAR MARKS. OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. PERFORMED REPAIR BY COMPLYING WITH EA 8-5330-T0309419 DATE JUL 03, 2014. MAJOR REPAIR.

Part: SKIN — CHAFED (RT AILERON) · airframe 57,334 hrs · 18,955 cycles

RIGHT INBD AILERON, LOWER SECTION OF INBD END LE HAVE CHAFED MARK. R & R SKIN & SUPPORT BRACKET IAW SRM 51-31-01 PG 1 ON RT INBD AILERON LOWER SECTION OF INBD LE. SKIN FABRICATED ON T14 1078081 IAW SRM 57-51-01. MAJOR REPAIR.

Part: STIFFENER — CRACKED (R2 DOOR) · airframe 57,334 hrs · 18,955 cycles

UPON REMOVAL & REPLACEMENT OF R2 DOOR BEAM NR 2, A FWD UPPER STIFFENER WAS CRACKED AT LOWER END DURING RIVET REMOVAL. R & R ONE EACH STIFFENER AT FWD UPPER R2 DOOR BEAM NR 2 IAW SRM 51-31-01. STIFFENER WAS FABRICATED ON T14 1078173 IAW SRM 52-12-01. PN ADA3756-503 LOCATED AT STATION 802.50, MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOOR PANEL PUNCTURED BS 1900 RBL 50. R & R MAIN DECK FLOOR PANEL AT BS 1900, RBL - 50 IAW AMM 53-21-08-04. FABRICATED NEW FLOOR PANEL ON T14/1077523. MAJOR REPAIR.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,334 hrs · 18,955 cycles

AFT CARGO FRAME STATION 1841 UPPER CHORD HAS CORROSION UNDER NUTPLATES FROM LONGERON 43L TO 43R. REMOVED CORROSION FROM -43 SUPPORT AT FS 1841 IAW SRM 51-21-01. ORIGINAL THICKNESS .125, .079 MATERIAL REMAINING. OUT OF LIMIT IAW SRM 53-00-01, FIG 1B, PG 12. RECEIVED REPLACEMENT SUPPORT PN AGA7170U43. LOCATED & DRILLED SUPPORT IAW SRM 51-31-01 & DWG AGA7170U43, REV B, SH 1. INSTALLED -43 SUPPORT & SURROUND STRUCTURE IAW SRM 51-31-01 & DWG AGA7170, REV B, SH 1. CLASS 1 MINOR REPAIR.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOORBOARD PUNCTURED AT SEVERAL SPOTS BS 791 - 840 LBL 76 - 106. RECEIVED NEW MAIN DECK FLOOR PANEL BS 791 - 840 LBL 76 - 106 ON T141077528. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOORBOARD DAMAGED BS 765 BLO RECEIVED NEW FLOOR PANEL ON MAIN DECK BS 765 BL0 ON T14/1077527. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOORBOARD PUNCTURED BS 655 - 735 BL0 FOUR LOCATIONS. RECEIVED NEW MAIN DECK FLOOR PANEL BS 655 - 735 BL0 ON T14/1077525. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 57,334 hrs · 18,955 cycles

MAIN CARGO DECK FLOOR PANEL 293HF TOP SKIN, AFT END CRACKED. FABRICATED MAIN CARGO DECK FLOOR PANEL 293HF ON T141076890 PER SRZ-25-005 IAW VOL II SRM 51-62-01 AT RBL 4 - RBL 4 BS 1910-2007. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 57,334 hrs · 18,955 cycles

CABIN FLOOR PANEL 283JF DELAMINATED. FABRICATED NEW CABIN FLOOR PANEL 283JF ON T141077202 IAW SRZ-25-005 IAW VOL II SRM 51-62-01 AT RBL 27 - 46 BS 1741 - 1821. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 57,334 hrs · 18,955 cycles

CABIN FLOOR PANEL 283CF HAS MISSING EDGE SEALANT. FABRICATED FLOOR PANEL 283CF IAW SRM VOL II 51-62-01 & DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 57,334 hrs · 18,955 cycles

CABIN FLOOR PNL 252FF HAVE DAMAGED SEALANT ON EDGES. FABRICATED NEW CABIN FLOOR PANEL 252FF ON T14 1077204 IAW SRZ-25-00 IAW VOL II SRM 51-62-01 AT RBL 46- RBL 74 BS 1099 - 1159. MAJOR REPAIR

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOORBOARD PUNCTURED BS 1039 LBL 10. FABRICATED NEW FLOOR PANEL AT BS 1039 LBL 10 IAW SRZ-25-005 & SRM VOL II 51-22-01 ON VTAM T14/1076889.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 57,334 hrs · 18,955 cycles

MAIN DECK FLOORBOARD DAMAGED BS 695 LBL 85. FABRICATED NEW MAIN DECK FLOORBOARD AT BS 695 LBL 85 ON T141076888 IAW SRZ-25-005 IAW VOL II SRM 51-62-01. MAJOR REPAIR.

Part: DISPLAY — FAILED (COCKPIT) · airframe 56,046 hrs · 18,403 cycles

THIRTY MINUTES INTO FLIGHT, MCDU 1 SHOWED LSK 1L BLANK (NO FMC) 100 MINS LATER MCDU 2 WENT BLANK AND FMC-2 DROPPED OFF NEVER GOT "MAP FAIL" ON MAP DISPLAY. WHEN ENG'S WERE SHUTDOWN IN PARKING GROUND POWER TOOK OVER, MCDU 2 CAME BACK UP.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 55,299 hrs · 18,077 cycles

DURING PRE FLIGHT CHECK, EMERGENCY LIGHT DID NOT TEST, EMERGENCY LIGHT BATTERY 1 LOW MESSAGE DISPLAYED REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-01-4. OPS GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 53,946 hrs · 17,531 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT DOES NOT COME ON WITH LOSS OF POWER. SWITCH IS IN ARM, GO TO "ON" LIGHT WILL COME ON. PERFORMED EMERGENCY LIGHTING ADJUSTMENT AND TEST IAW MM 33-50-00-5. OPS CHECKED OK.

Part: CONTROL VALVE — LOOSE (ZONE 300) · airframe 53,943 hrs · 17,527 cycles

HORIZONTAL STABILIZER LOWER PRIMARY TRIM CONTROL VALVE FOUND FLOW CONTROL VALE BORE .75" PRESSURE PASSAGE BORE WITH A METAL ORIFICE PLUG STUCK IN IT. THIS IS AREA OF HFEC INSP AND WAS UNABLE TO COMPLY WITH THIS PROCEDURE DUE TO BLOCKAGE. REPLACED LOWER PRIMARY TRIM CONTROL VALVE WITH SERVICEABLE ONE.

Part: LANDING LIGHT — DAMAGED (FUSELAGE) · airframe 53,870 hrs · 17,500 cycles

ON POST FLIGHT WALK AROUND, FOUND RT FUSELAGE LANDING LIGHT MISSING, AND WIRING TO LIGHT EXPOSED. PULLED AND TAGGED RT LANDING LT CONTROL & LAMP CB'S. FOUND NO EVIDENCE OF DAMAGE TO ACFT FROM MISSING LANDING LIGHT. REPLACED LANDING LIGHT ASSY IAW AMM 33-41-00-2. CHECKED GOOD.

Part: BULB — INOPERATIVE (DISARM LIGHT) · airframe 52,262 hrs · 16,861 cycles

RT CABIN DOOR DISARM LIGHT INOP. R & R 2 EA BULBS IN DISARM LIGHT. FINAL CLOSED.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 ENGINE) · airframe 52,089 hrs · 16,797 cycles

AT 98 KTS GOT A NR 2 ENG EXCEEDANCE ALERT REJECT TAKEOFF. PERFORMED FAN (N1) OVERSPEED INSP, FAN BLADES MOTOR FREE FOR ROTATION FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FREE FROM PARTICLES IAW AMM 72-00-00-6-2. ACFT OK FOR SERVICE. COMPLIED WITH AMM 72-00-00-6-2, FOR FAN (N1) OVERSPEED BETWEEN 119.6 AND 122 WITH NO DEFECTS NOTED. IAW ACARS N1 EXCEEDANCE WAS 119.7. FINAL CLOSED.

Part: CABLE — OUT OF POSITION (COCKPIT WINDOW) · airframe 52,043 hrs · 16,781 cycles

CAPT'S LT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW CRANK CABLE OFF TRACK ON MOST AFT PULLEY. REINSTALLED CABLE AND PROPERLY POSITIONED CABLE GUIDE PIN. WINDOW OPS CHECK NORMAL. REF: MM 56-12-01-2, FINAL CLOSED.

Part: INDICATOR — STICKING (FUEL SYSTEM) · airframe 52,001 hrs · 16,765 cycles

ON SHORT FINAL RECEIVED FUEL QTY/USED CK LEVEL 2 ALERT LANDED-CLEARED RUNWAY-HAD FIRE DEPT CK FOR LEAKS-NONE WERE SEEN-TAXIED TO BLOCKS. ONCE PARKED, ALERT CLEARED. EXPECTED FUEL QTY=24.4 ACTUAL FUEL QTY=23.6 RELEASED FOR SERVICE IAW MEL: 28-01-01 CATEGORY: A EXPIRATION: 15APR11 "MEL 28-01-01: TANK NR 2 FUEL QTY - INOP FUEL TO KNOWN QTY, AND AFTER REFUELING AND PRIOR TO EACH SUBSEQUENT DEPARTURE, VERIFY TANK NO 2 QTY WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPS NOT AUTHORIZED ABOVE 78 DEGREES N LAT. OPERATE FSC IN MANUAL." IAW MEL 28-01-01 NR 2 TANK FUELED TO KNOWN QTY AND FUEL QTY VERIFIED WITH FUEL LEVEL STICKS. STICK NRS AND STICK READINGS ARE RT AFT 14 LT AFT 14 AND FWD 7.5, FUEL QTY TNK 2 IS 22.4KLBS. ACFT OK SVC. SYS PLACED ON MEL 28-01-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,627 hrs · 16,619 cycles

AFTER APU START, WHEN PACKS TURNED ON HAD FUEL ODOR FOR APROX 20 SECONDS. CONDUCTED A NORMAL APU START, REF JRH, 3-5,3-6 3-7, RAN PACKS, NO ABNORMAL ODORS NOTED, PACK OPS GOOD REF MM 21-00-00, COULD NOT DUPLICATE.

Part: ENGINE — BIRD INGESTION (NR 3) · airframe 51,517 hrs · 16,580 cycles

MULTIPLE BIRD STRIKES, FRONT WINDSCREEN AND NR 3 ENGINE. MODERATE VIBRATION, DECLARED AN EMERGENCY, COMPLIED WITH QRH, DIVERTED. (DEPARTED 16R BIRD STRIKE AT 2,500 FT MSL) FIRED BOTH BOTTLES INTO NR 3 ENGINE. LOST "B" LOOPS.

Part: ENGINE — INOPERATIVE (NR 2) · airframe 50,787 hrs · 16,282 cycles

MANUAL FUEL/PUMPS ON HAD PROBLEM STARTING NR2. 1ST ATTEMPT-ENGINE ROLLED BACK AFTER 40 PERCENT, N1. SECOND ATTEMPT SLOW BUT STARTED OK. CHECKED POWER SEVERAL TIMES ON TAXI-ALL OK. PASSING 19K ENG 2 FLAMED OUT. RAN CHECKLIST,RECYCLED PUMP SWITCHES, RESTARTED WITH NO OTHER PROBLEMS. REPLACED NR 2 ENG REF WC 71T1101 AND WC 71T1701 ACCOMPLISHED POWER ASSURANCE REF JRH CH 7 CHECKS GOOD.

Part: SKIN — GOUGED (ZONE 100) · airframe 50,677 hrs · 16,219 cycles

EXISTING GOUGE IN FUSELAGE SKIN ADJACENT TO NOSE JACK POINT ALIGNMENT HOLE REPAIRED IAW EA 8-5330-123164.

Part: SKIN — WORN (RT WING) · airframe 50,677 hrs · 16,219 cycles

RT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.

Part: SKIN — WORN (LT WING) · airframe 50,677 hrs · 16,219 cycles

LT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 50,677 hrs · 16,219 cycles

LT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.

Part: SKIN — WORN (NR 2 SLAT) · airframe 50,677 hrs · 16,219 cycles

LT WING, SLAT NR 2 FOUND DEEP WEAR ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 31, VOL I.

Part: SKIN — DAMAGED (ZONE 200) · airframe 50,677 hrs · 16,219 cycles

MAIN CABIN LOCATED AND DRILLED OUT GATELINK ANTENNA DOUBLER IN WRONG POSITION, BTWN LONG NR 2 RT & LONG NR 3 RT IN LIEU OF LONG NR 3 RT & LONG NR 4 RT REF DWG 72749-504. REPAIRED AREA IAW SRM 53-20-00 VOL I, FIG 13.

Part: BULKHEAD — DENTED (ZONE 100) · airframe 50,677 hrs · 16,219 cycles

DURING INSP AFT FUSELAGE EXT FOUND DEEP NICK ON BULKHEAD SKIN LOWER SIDE. REPAIRED AREA IAW SRM 53-00-01, FIG 10 & SRM 51-00-01, FIG 100, VOL I.

Part: SUPPORT ANGLE — CRACKED (BS 2122) · airframe 50,677 hrs · 16,219 cycles

DURING INSP, AFT FUSELAGE UPPER ATTIC AREA FOUND CRACK ON ANGLE SUPPORT. REPAIRED AREA IAW SRM 53-30-00 FIG 2B VOL I.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 50,677 hrs · 16,219 cycles

AFT FUSELAGE INT FOUND CRACK ON TEE CAP VERTICAL STIFFENER. REPAIRED AREA IAW SRM 53-00-01, FIG 19, VOL I.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 50,677 hrs · 16,219 cycles

DURING INSP LT WING LWR SURFACE FOUND SUSPECT CORROSION UNDER SKIN OF OTBD AILERON AND AROUND HEADS OF FASTENERS. REPAIRED AREA IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.

Part: FRAME — WORN (BS 1621) · airframe 50,677 hrs · 16,219 cycles

MAIN CABIN DEFORMATION AND WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00, FIG 4, VOL I.

Part: FRAME — CRACKED (ZONE 500) · airframe 50,677 hrs · 16,219 cycles

LT AIR CONDITIONING COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00, FIG 4, VOL I.

Part: MEMBRANE — CRACKED (ZONE 200) · airframe 50,677 hrs · 16,219 cycles

COCKPIT FLOOR STRUCTURE HAVE BEEN FOUND CRACK ON MEMBRANE AND ON STIFFENERS. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,677 hrs · 16,219 cycles

FWD CARGO COMPT DURING MOD, REMOVED PART FOUND 6 EA MODERATELY CORRODED CHANNELS UNDER SHOE BRAKES. REPAIRED AREA IAW SRM 53-70-00 FIG 7, SHT 5, VOL I.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,677 hrs · 16,219 cycles

FWD CARGO COMPT DURING MOD REMOVED ACTION FOUND MODERATE CORROSION UNDER THE SHOE BRAKE CHANNEL. REPAIRED AREA IAW SRM 53-70-00, FIG 7, SHT 5, VOL I.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,677 hrs · 16,219 cycles

DURING INSP OF HORIZ STABILIZER, FOUND SKIN PANEL PLANKS CRACKED. IAW EO NR 8-5510-7-2307 PT1, SECT. C, STEP 1 AND 2 VERIFY APPLICABILITY OF EO NR 8-5510-7-4308 PT 2. REPAIRED AREA IAW EA 8-5510-133464 & EA 8-5510-133465.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,677 hrs · 16,219 cycles

AFT CARGO COMPT, SEVERE CORROSION WITH EXFOLIATION ON SUPPORT. REPAIRED AREA IAW SRM 53-70-00 FIG 13 SHT 1 VOL I.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,677 hrs · 16,219 cycles

AFT CARGO COMPT, SEVERE CORROSION WITH EXFOLIATION ON SUPPORT. REPAIRED AREA IAW SRM 53-70-00 FIG 13 SHT 1 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 50,677 hrs · 16,219 cycles

DURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DENT 2.50" X 1.50" DEEP 0.066" ON SKIN. REPAIRED AREA IAW SRM 53-20-00, FIG 13, SHT 5 VOL I.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 50,677 hrs · 16,219 cycles

RT WING OTBD FLAP UPPER SURFACE FOUND CRACKED ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.

Part: CSD — LEAKING (NR 2) · airframe 50,433 hrs · 16,044 cycles

ON TAKEOFF ROLL GOT NR 2 CSD OIL PRESS LOW LIGHT FLUCTUATING WITH ALTERNATING GEN 2 OFF AND AC BUS TIE 2 ISOL LIGHTS. NR 2 ENG INSTRUMENT GAUGES AND LANDING GEAR LIGHTS FLASHING ALONG WITH INTERMITTENT MASTER CAUTION. ABORTED TAKEOFF AND RAN QRH. CSD OIL LIGHT AND ALL ELECTRICAL INDICATIONS WENT OUT OR STABILIZED WHEN ACFT STOPPED. NOTICED ALL AC LOAD METERS FLUXING WITH GEN 2 ON. SHUT OFF NR 2 GEN AND DISCONNECTED CSD. LOW SPEED REJECT. OPENED PATIO DOORS AND NR 2 ENGINE FAN COWLINGS. REACTIVATED NR 2 CSD AND FOUND OIL LEVEL TO BE LOW, SERVICED CSD TO FULL. PERFORMED ENGINE RUN PER DC10 JRH CHAPTER 6 AND DISCOVERED SMALL OIL LEAK AT THE CHARGE FILTER CAP ASSY, REF IPC 24-11-10 -01, ITEM 470. REPLACED BAD O-RING ON FILTER HOUSING PER STANDARD MAINTENANCE PRACTICES. PERFORMED SECOND ENGINE RUN PER DC10 JRH CHAPTER 6, NO LEAKS NOTED, NR 2 CSD AND GENERATOR FUNCTION NORMALLY PER JRH 9-2. CLOSED AND SECURED FAN COWLINGS AND PATIO IN ACCORDANCE WITH DC10-30 MM 71-00. ACFT OK FOR SERVICE.

Part: ENGINE — FAILED (NR 3) · airframe 49,345 hrs · 15,507 cycles

NR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1, THROTTLE AT IDLE N137 PERCENT EGT 600-700 DEG. INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE NR 3 ENGINE. PERFORMED IDLE AND FLT IDLE RUNS. ALSO PERFORMED A MAX POWER ASSURANCE RUN. ALL ENGINE PARAMETERS WERE NORMAL AND ACFT OK FOR SERVICE. FUEL FLOW DISCREPANCY WAS ALSO CLEARED WITH ENGINE REMOVAL AND REPLACEMENT.

Part: COMPRESSOR — STALLED (NR 3 ENGINE) · airframe 49,345 hrs · 15,507 cycles

NR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1,-THROTTLE AT IDLE N137 PERCENT EGT 600-700 DEG INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE #3 ENGINE. PERFORMED IDLE AND FLT IDLE RUNS. ALSO PERFORMED A MAX POWER ASSURANCE RUN. ALL ENGINE PARAMITERS WERE NORMAL AND A/C OK FOR SERVICE. FUEL FLOW DISCR. WAS ALSO CLEARED WITH ENGINE R & R.

Part: WASTE TANK — LEAKING (LAVATORY) · airframe 49,176 hrs · 15,425 cycles

FWD ELECTRONIC COMPARTMENT RIGHT SIDE HAS EVIDENCE OF LEAK; BLUE WATER THROUGHOUT THE E/E COMPARTMENT. REMOVED AND REPLACED THE LAV TANK ASSY P/N 1-119095-55; S/N 10-52-05 IAW DC-10-30 AMM 38-31-05-02. COMPLIED WITH EA 8-3831-116953 PT 1; " WATER AND WASTE, WASTE DISPOSAL, TOILET TANK VENT LINE, INTERIM REPAIR" DATED 03-10-08. OPS CHECK GOOD IAW DC-10-30 AMM 38-31-05-2.

Part: FLOOR PANEL — TORN (BS 1521-1601) · airframe 49,174 hrs · 15,422 cycles

CENTER PIT PANEL "183 BG" IS PUNCTURED. FABBED NEW FLOOR PANEL 183 BG IAW DWG SRZ 25-005 REV E. MAJOR REPAIR.

Part: SUPPORT — MISREPAIRED (HORIZONTAL STAB) · airframe 49,174 hrs · 15,422 cycles

REWORK OF JOB CARD E8-5340-7-3305 PT4 (INSPECT HORIZONTAL STABILZER SECTION PIVOT SUPPORT AD 96-25-15) STEP 3-A. SHOULD HAVE HAS 6 EACH ADDED HOLES, ONLY 5 WERE DRILLED. REPAIRED HORIZONTAL STAB PIVOT SUPPORT IAW FEDEX EA 8-5340-116955. MAJOR REPAIR.

Part: CARGO TRACK — GOUGED (BS 775) · airframe 49,174 hrs · 15,422 cycles

WHILE ACCOMPLISHING "C" CHECK AT TIMCO, THE OUTBOARD RAIL OF THE CARGO LOADING SYSTEM AT 3L POSITION WAS FOUND WITH DAMAGE AT ITS FWD EDGE. TRIM AWAY THE FWD END OF THE SUBJECT RAIL TO REMOVE THE DAMAGE. RESTORE THE ORIGINAL END PROFILE BY COPING FROM THE RAIL AT 3R POSITION IAW EA 8-2550-118438, DATED 2/18/08. MINOR REPAIR PER FEDEX GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX LBL-90, BETWEEN STA 1481 TO 1561 IS DELAMINATED. MAT ID A402H35039-003 PO 5990899.1. POTTING COMPOUND 1619 A/B PO 606417.3, INSERT SLS 5094A3-400-2 PO 595225, INSERT SLP 5094A3-2 PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.4. LOCATED HOLES, POTTED EDGES AND INSERTS. INSTALLED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F, MINOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX LBL-60, BETWEEN STA 1239 TO 1321 IS DELAMINATED. MAT ID A402H35039-003 PO 590899.1. FABRICATED NEW BOARD, MAT ID POTTING COMPOUND 1619 A/B PO 666417.3. INSERT SLS 5094A3-400-2 PO 595255, INSERT SLP 5094A3-2 PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.4. LOCATED HOLES FOR INSERTS, POTTED EDGE AND STARTED CURE, CURE COMPLETE. SANDED EDGE, POTTED INSERTS. INSTALLED ANTI-SKID IAW FEDEX DC10-30 DWG SRZ 02-005 REV F, MINOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN CABIN FLOORBOARD AT APPROX LBL-20, BETWEEN STA 495 TO 615 IS DELAMINATED. MAT ID A420H PO 590899.1 IAW FEDEX DWG SRZ 25-005 REV F. FABBED FLOORBOARD PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTTING COMP 1619 A/B PO 6064173. INSERT SLS 5094A3-400-Z, PO595225, INSERT SLP 5094AA-2,PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.1 IAW FEDEX DWG SRZ 25-005 REV F. LOCATED AND POTTED INSERTS IAW FEDEX DWG SRZ 25-005-REV F. INSTALLED ANTI-SKID, POTTED AND SANDED EDGES IAW FEDEX DWG SRZ 25-005 REV F, MINOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOOR PNL FROM STA 1341, LBL-20 FWD EDGE IS DELAMINATED. MAT ID A402H PO590899.1 IAW FEDEX DWG SRZ 25-005 REV F. FABBED FLOOR PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTING COMP 1619 A/B PO 606417.3. INSERT SLS 5094A3-400-2 PO 595225, INSERT SLP 5094AA-2 PO 595242. ADHESIVE EPIBOND 420A/B PO 594846.4 IAW FEDEX DWG SRZ 25-005 REV F. LOCATED INSERTS AND POTTED INSERTS IAW FEDEX DWG SRZ 25-005 REV F. INSTALLED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F. POTTED AND SANDED EDGES IAW FEDEX DWG SRZ 25-005 REV F, MINOR REPAIR.

Part: INDICATOR — INOPERATIVE (R1 DOOR SLIDE) · airframe 49,174 hrs · 15,422 cycles

R-1 SLIDE DISARM LIGHT IS INTERMITTENT. REMOVED AND REPLACED R-1 DOOR "SLIDE DISARMED" ANNUNCIATOR IAW DC10 AMM 33-00- 00-2. OPS CHECK GOOD IAW DC10 AMM 52-70-00-2. MINOR REPAIR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,174 hrs · 15,422 cycles

EMERGENCY LIGHTS DO NOT OPERATE CORRECTLY AND FAILED TEST. REMOVED AND REPLACED EMERGANCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51-01-2. OPS CHECK GOOD IAW AMM 33-51-01-2. LOCATED BEHIND PANEL 231 AC, CEILING PANEL AFT OF LEFT FWD PASSENGER DOOR. MINOR REPAIR.

Part: BRACKET — CORRODED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN WEB STA 590 TO STA 695 BRACKET HAS NUMEROUS NICKS. FABRICATED NEW - 13 CLIP IAW DWG ACA 7216 REV L. ALODINED CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 25, VOL II. PRIMED CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 21, VOL II. PAINTED CLIP IAW MD/DC-10-30 SRM 51-21-02 PG 8, VOL II. INSTALLED CLIP IAW DAC DWG NR ACA 7216 REV L AND MD/DC-10-30 SRM 51-33-01 PG 25, VOL II.

Part: BRACKET — DAMAGED (BS 365-363) · airframe 49,174 hrs · 15,422 cycles

WEB SUPPORT BRACKET ACA 7218-31 HAS TOOLING MARKS. BLENDED TOOLING MARKS ON WEB SUPPORT BRACKET IAW SRM 51-21-02, VOL II. ORIGINAL MATERIAL THICKNESS .090 IAW DWG ACA 7218 REV E MATERIAL LOSS .068, OUT OF LIMITS IAW SRM 53-00-01, VOL I. FABRICATED NEW ACA 7218-31 BRACKET BY FORMING AND DRILLING IAW DWG ACA 7218 REV E. ALODINED, PRIMED IAW SRM 51-21-02 PG 8, VOL II. PART MARKED PER FEDEX GMM 7-0-1000. BRACKET INSTALLED ON CARD NR 52305547.

Part: RETAINER — TORN (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

CTR CARGO DOOR FWD LOWER L/E SEAL RETAINER IS BROKEN (INTERIOR). REMOVED AND INSTALLED RETAINER IAW DC-10 SRM 51-35-01, VOL II. MAT ID .032 7075-T6 PO NR 547197.3 AND FABBED IAW DAC DWG ANB 7328. ALODINE AND PRIME IAW DC-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001.

Part: FLOORBOARD — DELAMINATED · airframe 49,174 hrs · 15,422 cycles

CABIN FLOORBOARD BS 675 LBL 27.50 DELAMINATED AND CRACKED. FABBED FLOORBOARD IAW DWG SRZ 25-005 REV F. LOCATED AND POTTED INSERTS IAW DWG SRZ 25-005 REV F. INSTALLED NON-SKID, POTTED AND SANDED EDGES IAW DWG SRZ 25-005 REV F. INSTALLED NEW FLOORBOARD IAW SRM 51-31-01 VOL II. MINOR REPAIR.

Part: FLOORBOARD — DELAMINATED (BS 495-615) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX BL-0 BETWEEN STA 495 TO 615 IN DELAMINATED. FABRICATED NEW FLOOR BOARD PANEL STA 495 TO 615, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW SRZ 25-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01, VOL II.

Part: PANEL — CHAFED (RT PYLON) · airframe 49,174 hrs · 15,422 cycles

NR 3 PYLON AFT "V" PANEL NR 488 GL, ATTACHMENT HOLES CHAFFED. BLENDED DAMAGED AREAS, MAXIMUM DEPTH .055 IAW SRM 54-00-01, FIG 1A VOL I. FABRICATION PER EA NR 8-5480-118437. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II, PG 21-24. INSTALLED DOUBLER AND FILLERS PER SRM 51-35-01 AND 51-33-01, VOL II.

Part: WIRE — BROKEN (R1 DOOR) · airframe 49,174 hrs · 15,422 cycles

BY R-1 DOOR AIR BOTTLE TERMINAL BLOCK 53-901 HAS BROKEN WIRES AND TERMINAL BLOCK. REPLACED TERMINAL STRIP 53-901 IAW WDM 33-52-01. OP'S CHECKED EMERGENCY EXIT LIGHTS IAW 33-51-01-2, OPS CHECK GOOD. MINOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN SEAT TRACK SCALLOPS ARE GOUGED FROM STA 1461 TO 1521 BL 48L. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW FEDEX DWG NR NEA 6022 REV AM. INSTALLED SPLICE HAT AND 2 SPLICE PLATES IAW MD-10 / DC-10 SRM 53-70-00, VOL I. ALODINED/PRIMED AND TOP COAT IAW MD-10/DC-10 SRM 51-21-02, VOL II.

Part: FLOORBOARD — DELAMINATED (BS 595-675) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX LBL - 90, BETWEEN STA 595 TO 675 IS DELAMINATED. FABRICATED NEW FLOORBOARD STA NR 595 - 675. POTTED EDGES, COMPLETED CURE AND SANDED, INSTALLED INSERTS, APPLIED NON-SKID MARKED MANUAL IAW SRZ 25-005 REV F. INSTALLED IAW SRM 51-31-01, VOL II.

Part: BEAM — CRACKED (ZONE 800) · airframe 49,174 hrs · 15,422 cycles

CABIN OVERWING DOOR LT SIDE AFT UPPER STOP FITTING IS CRACKED. REMOVED AND REPLACED BEAM IAW FEDEX DWG NR ADA 3462 REV AE AND MD-10/DC-10 SRM 51-31-01, VOL II.

Part: FLOORBOARD — DELAMINATED · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX RBL-90, BETWEEN STA 800 TO 850 IS DELAMINATED. REMOVED FLOORBOARD IAW AMM 53-21-01-2. FABBED FLOORBOARD IAW SRZ-25-005 REV F. LOCATED HOLES FOR INSERTS IAW DWG SRZ 25-005 REV F. POTTED EDGES AND STARTED CURE IAW DWG SRZ 25-005 REV F. CURE COMPLETED, SANDED EDGES IAW DWG SRZ 25-005 REV F. POTTED INSERTS IAW DWG SRZ 25-005 REV F. INSTALLED ANTI-SKID IAW DWG SRZ 25-005 REV F. MINOR REPAIR.

Part: FLOORBOARD — DAMAGED · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT LBL - 20, BETWEEN STA 1821 TO 1881 IS SPONGY. FABBED FLOORBOARD IAW SRZ-25-005 REF F. INSTALLED FLOORBOARD IAW SRM 51-31-01 VOL II. LOCATED, DIRLLED HOLES. INSTALLED INSERTS, INSTALLED ANTISKID IAW DWG SRZ 25-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01, VOL II. MINOR REPAIR

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 49,174 hrs · 15,422 cycles

UPPER CARGO COMPARTMENT, AFT SECTION, LT SIDE AT STA 1741, THE O/B PANEL NR 281 FE (ORANGE) (MARKED AS "14L") IS DELAMINATED AND HAS TWO SMALL PUNCTURES. FABRICATED NEW FLOOR PANEL 281FE, POTTED EDGE, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED PANEL IAW SRZ - 005 REV F. INSTALLED FLOOR PANEL IAW DC-10-30 SRM 51-31-01 VOL II.

Part: FLOORBOARD — DAMAGED (BS 595-675) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX LBL 38, BETWEEN STA 595 TO 675 IS WARPED. FABBED FLOORBOARD PANEL AT STA 595-675 IAW DWG SRZ 25-005 REV F. LOCATED HOLES, COUNTERBORED HOLES, POTTED INSERTS, POTTED EDGES, CURED EDGES, SANDED EDGES, APPLIED ANTI-SKID IAW DWG SRZ 25-005 REV F. MINOR REPAIR

Part: FLOOR PANEL — DAMAGED (BS 555) · airframe 49,174 hrs · 15,422 cycles

CABIN FLOOR PANEL AT STA 555 RBL 8.5 TO 27.5 HAS EDGE DAMAGE AND HOLES. FABRICATED NEW FLOOR PANEL STA 555, POTTED EDGES, COMPETED CURE AND SANDED EDGE POTTING, INSTALLED INSERTS AND APPLIED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F. THIS IS A MINOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOOR PNL AT STA 1481 TO 1561, LBL 40 FWD CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL STA 1481 TO 1561, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX SRZ 25-005 REV F.

Part: FLOORBOARD — DAMAGED (BS 1761-1821) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX RBL-20, BETWEEN STA 1821 TO 1761 IS SPONGY. FABBED FLOORBOARD, LOCATED AND POTTED INSERTS, POTTED AND SANDED THE EDGES AND APPLIED THE ANTI-SKID IAW DWG SRZ-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01 VOL II.

Part: FLOORBOARD — DELAMINATED (BS 899-979) · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN FLOORBOARD AT APPROX RBL-20, AT APPROX BETWEEN STA 899 TO 979 IS DELAMINATED. FABBED NEW FLOORBOARD STA 899 TO 979, POTTED EDGES, COMPLETED CURE AND SANDED. INSTALLED INSERT , APPLIED ANTI-SKID, MARKED PNL IAW FEDEX DWG SRZ 25-005 REV F. THIS IS A MINOR REPAIR.

Part: SUPPORT — WORN (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

AFT PIT, AFT BULKHEAD STRAP 187EA (NWJ6006-35) (NWJ6006-25NC) (MARKED AS "A2-A4) STRAP IS CRACKED ON THE (A2 END), HAS CORROSION, IS DENTED AND ALL 4 FASTENER HOLES ARE GOUGED. FORMED SUPPORT PER DAC DWG NWJ6006 REV C AND FEDEX GMM 7-0-1001, PG 2. FABRICATED SUPPORT PER FEDEX GMM 7-0-1001 AND DAC DWG NWS6006 REV B. ALODINED PER DC-10 SRM 51-21-01PARA 31, VOL II. PRIMED PER DC-10 SRM 51-21-01 PARA 24, VOL II. PAINTED PER DC-0 SRM 51-21-02, VOL II, PART MARKED PER FEDEX GMM 7-0-1001.

Part: STRAP — BENT (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

AFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B4/C4) IS DAMAGED, BENT, HAS 4 ELONGATED FASTENER HOLES AND IS CORRODED. MINOR REPAIR. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001, PG 2. FABBED HAT SECTION PER FEDEX GMM 7-0-1001 AND DAC DWG NWJ 6006 REV B. ALODINED PER DC-10 SRM 51-21-01 PARA 31, VOL II. PRIMED PER DC-10 SRM 51-21-01 PARA 24, VOL II. PAINTED PER DC-10 SRM 51-21-02, VOL II. PART MARKED PER FEDEX GMM 7-0-1001.

Part: STRAP — BENT (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

AFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B2/C2) IS DAMAGED, BENT, HAS ELONGATED FASTENER HOLES AND IS CORRODED. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001 PG 2. FABBED HAT SECTION PER FEDEX GMM 7-0-1001 AND DAC DWG NWJ 6006 REV B. ALODINED PER DC-10 SRM 51-21-01 PARA 31,VOL II. PRIMED PER DC-10 SRM 51-21-01 PARA 24,VOL II. PAINTED PER DC-10 SRM 51-21-20 VOL II. PART MARKED PER FEDEX GMM 7-0-1001.

Part: PANEL — CORRODED (FUEL TANK) · corrosion level 2 · airframe 49,174 hrs · 15,422 cycles

RT WING TANK PLATE PANEL NR 634 AT IS CORRODED. MACHINED NEW FUEL PANEL (545) IAW DAC DWG ARB 0872 REV AV AND ALODINED AND PRIMED, 545 FUEL PANEL IAW DPS 4.50 -127 AND MIL-C-5541 AFTER FINDING ORIGINAL PANEL WAS UNDER LIMITS AFTER CORROSION REMOVAL.

Part: FITTING — CRACKED (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

ACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 6 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-117632, STEP C. BORE HOLES B, C, AND D HAVE CRACK/CORROSION INDICATIONS. REAMED 4 EA. BOLT BORES, ACCOMPLISHED BHEC, FABERICATED AND INSTALLED 9 EA. REPAIR BUSHINGS IAW DC/MD-30 SRM 53-50-00 VOL I, FIG-17, PG-81 AND NTSPM 06-10-81.003.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

MCD DOOR JAMB, WEB CORRODED UNDER CENTERING GUIDE. REPAIRED AREA IAW EA 8-5710-116952.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,174 hrs · 15,422 cycles

RT MLG WW, MIDINTERCOSTAL INBD / OBRD SURFACES HAVE CORROSION JUST FWD OF AFT BULKHEAD. COROSION FOUND TO BE OUT OF LIMITS, REMOVED INTERCOSTAL, FABERICATED NEW AND INSTALLED IAW SRM 51-21-01 PG-28, VOL. II, SRM 53-00-01, FIG A, VOL I, SRM 51-35-01 & SRM 51-33-01 VOL II, DAC DAW EAE 0024 REV. 5, SRM 51-21-01 PG. 21-24 & SRM 51-21-02 VOL II.

Part: FITTING — CORRODED · airframe 49,174 hrs · 15,422 cycles

ACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 2 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-117632, STEP C. ALL FOUR BORE HOLES (A, B, C AND D) HAVE CRACK/CORROSION INDICATIONS. REAMED BOLT BORES IAW SRM 53-50-00 VOL I FIG 17 PG 81 AND ACCOMPLISHED BHEC OF BOLT BORES IAW NTSPM 06-10-01.003 AND FOUND CRACK INDICATION REMAINING IN BORE HOLE D (LWR JAMB SUPPORT FITTING ONLY). REMOVED SUPPORT FITTING, LOCATED AND DRILLED NEW FITTING AND INSTALLED IAW SRM 53-50-00 VOL I FIG 17 PG 81 AND 51-33-01 VOL II PG 1. FABRICATED REPAIR BUSHINGS AND INSTALLED IAW SRM 53-50-00 VOL I FIG 17 PG 81.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,174 hrs · 15,422 cycles

MCD SPOOL BRACKET NR 3 HAS CRACK INDICATION ON HOLES A AND B. REPAIRED IAW EA 8-5310-113030.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,174 hrs · 15,422 cycles

MCD SPOOL BRACKET NR 1 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REAMED ALL HOLES TO DIMENSIONS SHOWN IN TABLE 1 OF EA 8-5310-113030. PERFORMED HFEC OF ALL HOLES, NO DEFECTS NOTED. IAW NDT SPM 06-10-01-003. REPAIRED LOWER JAMB BEAMS IAW EA 8-5310-113030. REMOVED JAMB SUPPORT FITTING IAW SRM 51-33-01, VOL II ,PG 1. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 53-50-00 VOL I, FIG 17 & 51-33-01, VOL II, PG 1. INSTALLED INTERCOSTAL FS 635-655 IAW SRM 51-33-01, VOL II ,PG 1. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN SEAT TRACK HAS AREAS OF CORROSION STA 1481 TO 1531 LBL9. REMOVED, FABRICATED AND INSTALLED SEAT TRACK ATTACH LOBE AND SUPPORT STRUCTURE REPAIR IAW MD/DC10 -30 SRM 53-70-00 FIG 5 SHT 1 VOL 1,51-38-01 VOL II, 51-21-01 VOLII, 51-21-02 VOLII AND 51-40-02 VOLII.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,174 hrs · 15,422 cycles

MCD SPOOL BRACKET NR 7 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,174 hrs · 15,422 cycles

MAIN CABIN SEAT TRACK BETWEEN STA 1019 TO 1039 AT APPROX RBL - 48 IS CORRODED AND CRACKED. REMOVED AND REPLACED SEAT TRACK FROM STA 949 TO STA 1049 RBL48 IAW MD/DC10 -10 SRM 51-40-02 VOL II.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,174 hrs · 15,422 cycles

MCD SPOOL BRACKET NR 5 HAS CRACK INDICATION ON HOLES B, C, AND D. REPAIRED IAW EA 8-5310-113030. MAJOR REPAIR.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 49,174 hrs · 15,422 cycles

MCD SPOOL BRACKET NR 4 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,174 hrs · 15,422 cycles

AFT CARGO COMPT AT FS 1952 BETWEEN L47-48R SHEAR TIE IS CORRODED. REMOVED, FABERICATED AND INSTALLED SHEAR TIE IAW SRM 51-33-01, PG-1, VOL II & DWA AGA7133 REV.H. & SRM 51-35-01 VOL II.

Part: SKIN — DENTED (ZONE 600) · airframe 49,174 hrs · 15,422 cycles

RIGHT WING TRAILING EDGE LOWER SKIN SURFACE DENTED INBD OF OUTBD MAIN FLAP INBD END. REMOVED PANELS TO FOM IAW MD/DC10 SRM 51-31-01 VOL II, CUTOUT DAMAGE AREA IAW MS/DC10 SRM 57-00-01 VOL I. MATERIAL ID FOR DOUBLER REPAIR 2024 T-3, .090 PO NR 575582.1, IAW MD/DC10 SRM 57-10-00 VOL I. FABRICATED REPAIR IAW MD/DC10 SRM 57-10-00 VOL I. ALODINED AND PRIMED IAW MD/DC10 SRM 51-21-01 PAGE 24 AND PAGE 21 VOL II. INSTALLED DOUBLER REPAIR IAW MD/DC10 SRM 51-35-01 VOL II. INSTALLED ACCESS PANELS IAW MD/DC10 SRM 51-31-01 VOL II.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 49,174 hrs · 15,422 cycles

RT WING, NR 5 L/E SLAT HAS DENTS 5EA ON L/E SKIN. CUT OUT DAMAGED AREA, FABERICATED DOUBLERS, SPLICE PLATE, BAFFLES, SEAL, FILLER AND INSTALLED REPAIR IAW SRM 57-10-00 FIG.II, VOL I, SRM51-21-01 VOL II AND SRM 51-35-02 VOL II.

Part: SKIN — DENTED (CARGO DOOR) · airframe 49,174 hrs · 15,422 cycles

CENTER CARGO DOOR FWD LOWER EDGE IS DENTED. REPAIRED CENTER CARGO DOOR FWD LOWER EDGE IAW DC10 SRM 52-10-00 VOL I FIG 17 SHEET 1.

Part: SWITCH — DEFECTIVE (NR 3 MANIFOLD) · airframe 44,035 hrs · 13,263 cycles

NR 3 MANIFOLD FAIL ILLUMINATED IN FLT. C/W QRH PROCEDURES, LIGHT EXTINGUISHED. PERFORMED DECAY CHECK OF NR 3 PNEU SYS IAW JRH AND PASSED ITERROGATED FAULT INDICATOR IN CAC AND FOUND RIGHT WING PRESS SWITCH FAULTED WITH APU AIR CHECKED ALL ANTI-ICE TUBING AND LINES ON RT WING FOR LEAKS. CHECKED ALL SLATS FOR EXCESSIVE AIR, ALL NORMAL. REMOVED ALL PERI SEAL CONNECTORS FROM ALL HEATED SLATS AND VISUALLY INSP INSIDE OF PICCOLO TUBES FOR OBVIOUS DAMAGE, ALL NORMAL. FOUND NR 3 MANIFOLD FAIL FAULT BALL REMOVED AND REPLACED NR 3 MANIFOLD FAIL DETECT SWITCH FOUND WORN PERI SEALS ON I/B AND O/B OF NR 6 SLAT. REMOVED AND REPLACED SEALS, OPS CHECKED MAINIFOLD FAIL SYSTEM, OPS CHECK OK. LEAK CHECK OK.

Part: SUPPORT — BROKEN (FIRE LOOP) · airframe 41,666 hrs · 12,418 cycles

ON TAKEOFF AT 1200 FT AGL THE EGT ON NR 1 ENG WENT TO 960 DEGREES INDICATED VERY RAPIDLY. TOOK 4 THROTTLE WIDTHS TO BRING THE EGT BACK INTO PARAMETERS AND ENG RUNNING SMOOTLY. DUMPED APPROX 20K LBS OF FUEL. INITIAL VISUAL INSPECTION REVEALED SEVERAL BROKEN PNEU DUCT SUPPORT STRUTS, MANY BROKEN CLAMPS, RUPTURED HIGH PRESSURE TURBINE COOLING DUCT AT 12 O'CLOCK POS BROKEN FIRE LOOP SUPPORT TUBE ETC AND METAL IN TAILPIPE. INTERROGATED NR 1 EGT INDICATOR, DATA SHOWED 975 DEG FOR 10 SEC.

Part: ACCESS PANEL — MISSING (CARGO DOOR) · airframe 41,583 hrs · 12,392 cycles

DURING MAINT WALKAROUND FOUND CTR CARGO DOOR PRESSURE RELIEF ACCESS PANEL MISSING FROM A/C. INSTALLED PANEL PER MM 53-53-00.

Part: HYDRAULIC LINE — LEAKING (CARGO BAY) · airframe 33,639 hrs · 9,968 cycles

EVIDENCE OF HYD LEAK COMING FROM AFT CARGO COMPARTMENT. *S/D* REPAIRED PIPE ASSY AGK7002-553 PER MM 20-10-01-2 AND REPLACED PNEU DUCT INSULATION BLANKETS.

Part: ANGLE — CRACKED (HORIZ STAB)

NR 3 RT LEAD EDGE ASSY FOR HORIZONTAL HAS 7 INCH STRESS CRACK, RUNNING THRU HOLES ON UPPER FLANGE. *S/D* REMOVED AND REPLACED T-ANGLE REF SRM 55-10-00. RE-INSTALLED NR 3 RT LEADING EDGE ASSY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,289 hrs · 9,314 cycles

FWD CARGO DOOR CUTOUT FWD SIDE FOUND EXTERIOR SKIN AT L 39-40 DAMAGED. *S/D* REMOVED DAMAGED AREA PER SRM 53-50-00 FIG 9 SHEET 3 VOL 1 AND 51-21-01 VOL II. REPAIRS ARE REPAINTED PER SRM 51-21-02 VOL II. FASTENERS INSTALLED PER 51-33-01 VOL II.

Part: HYDRAULIC SYS — HIGH TEMP (NR 2)

98-0167 STA-DXB: DURING TAXI OUT HYD SYS NR 2 READ 50-50 DEG AFTER APPROX 8 MIN OF FLT TEMP NR 2 HAD INCREASE TO 60 DEG TMP SHORTLY INCREASE TO 70 DEG RED TABS REFER TO ND TEMP INCREASE WITHIN 5 MIN TO 90 CONT RED TAB PROC WITH NR 2 SYS SHUT DOWN. WHEN TMP APPROX 98 DEG RT TEMP HI LITE FLICKER CONT 728 REMAIN OUT. ALL LITE TEST OK. TEMP PASS 100 DEG ND CONT TO 105 WITHIN 30 MIN DURING DESCENT TEMP DIMINISH TO BELOW 100. ON FINAL APPROACH WITH ALL SYS SWITCH ON/ARMED TEMP DIMINISH TO 80 DEG THAN FURTHER TO 57 DEG DURING TAXI. OPEN ND CLOSE NR 2 FAN COWL AND WORK PLATE FORM LOCKS CK OK. HYD RESERVOIR SYS 2 REMOVED AND NEW RESERVOIR INSTALL. ENG NR 2 TEST RUN FOR TO CK HYD TEMP FND WITHIN LIMIT, CK FOR LE

Part: FIRE BOTTLE — DISCHARGED (NR 2 ENGINE)

ON PRE FLT CK, FOUND NR 2 ENG FIRE AGT 2 LOW LIGHT CAME ON. ON CK FOUND NR 2 ENG NR 2 BOTTLE DISCHARGE CARTRIDGE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE AND CARTRIDGE AS PER M/M 26-21-02 AND M/M 26-21-01. ALSO, WIRING AND AGENT DISCHARGE S/W (S1-164) FUNCTION OK. CARTRIDGE (P/N 876296).

Part: PICCOLO TUBE — LEAKING (NR 5 LE SLAT)

AIRCRAFT WING ANTI-ICE SET UP FOR USE ON TAKEOFF, ABOUT 10 TO 15 SECONDS AFTER LIFT OFF. NR 1 MANIFOLD FAIL LIGHT ILLUMINATED. TURNING OFF WING ANTI-ICE TURNED OFF MANIFOLD FAIL LIGHT. TROUBLESHOT SYSTEM FOUND NR 5 LEFT HAND SLAT PICCOLO TUBE OUTBOARD END LEAKING. REMOVED PICCOLO TUBE FROM NR 5 SLAT, REPAIRED AS PER ENGINEERING AUTHORIZATION 8-3010-32015, INSTALLED IN AIRCRAFT. PRESSURE CHECK GOOD, OPERATED SLATS AND WING ANTI-ICE SEVERAL TIMES AND FUNCTIONAL CHECK WAS GOOD.