N68054

Part: LIGHT — INOPERATIVE (SLIDE INDICATOR) · airframe 65,224 hrs · 29,460 cycles

R1 DOOR SLIDE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED PRESSURE INDICATION LIGHT ASSY IAW AMM 25-61-03-2, OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 64,619 hrs · 29,148 cycles

PACK ONE HAS STRONG ODOR. NR 1 COALESCER ALREADY REPLACED, RAN PACKS, NO ODOR AT THIS TIME IAW M/M 21-54-03-2.

Part: COALESCER BAG — ODOR (CABIN) · airframe 64,619 hrs · 29,148 cycles

PACK ODOR LIKE DIRTY SOCK. R & R NR 2 AND NR 3 COALESCER BAGS IAW MM 21-54-03-2, RAN PACKS FOR 20 MIN AT FULL HOT, FOUND NO FOUL ODOR IN ACFT AT THIS TIME, OK TO CONTINUE.

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 63,825 hrs · 28,736 cycles

AFT CARGO COMPARTMENT DOOR SILL HAS CORROSION AT NUTPLATE HOLES AS MARKED. REMOVED CORROSION AT 12 EA HOLES IAW SRM 51-21-01, 12 EA AREAS ARE WITHIN LIMITS IAW SRM 53-00-01. 1 NUTPLATE HOLE IS OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01, FIG 8, SH 8. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 63,825 hrs · 28,736 cycles

RT WING REAR SPAR LOWER CAP EO 8-5710-7-5007, PT 2 INSP FOUND CRACK AT FWD, OTBD HOLE COMPLIED WITH EA 8-5710-156726 FOR RT WING REAR SPAR LOWER CAP REPAIR OF FWD OTBD HOLE.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 63,825 hrs · 28,736 cycles

RT WING OTBD FLAP UPPER SURFACE 21" FROM THE OTBD EDGE HAS 3EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE CRACKS AT 21" FROM OTBD EDGE IAW SRM 57-10-00, FIG 6 , SH 1-3. MAJOR REPAIR.

Part: SKIN — CRACKED (BS 2130-2133) · airframe 63,825 hrs · 28,736 cycles

AFT FUSELAGE OUTER SKIN IS CRACKED APPROX. 3" AT BS 2132 BETWEEN L4R AND L5R. REMOVED DAMAGE IAW SRM 53-00-01, NDT HFEC CHECKED GOOD IAW NTSPM 06-10-01, FABRICATED REPAIR USING 7075-T6 .071 BATCH 0002069744 IAW SRM 53-00-01, FIG 4, SH 2 TREATED AND PRIMED AS REQUIRED IAW SRM 51-21-01. INSTALLED REPAIR IAW SRM 51-31-01. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 63,825 hrs · 28,736 cycles

RT WING OTBD FLAP UPPER SURFACE STA XORS 587 HAS 2 EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE AT STA XORS 587 IAW SRM 57-10-00 VOL 1,FIG 85 SHEET 3. MAJOR REPAIR.

Part: DOUBLER — WORN (FUSELAGE) · airframe 63,825 hrs · 28,736 cycles

AFT FUSELAGE ACCESS DOOR 311AB CUTOUT DOUBLER WORN AND RT SIDE IS ALMOST KNIFE EDGE. REPAIRED IAW EA8-5310-150998

Part: CARGO TRACK — CORRODED (BS 1800-1920) · corrosion level 2 · airframe 63,825 hrs · 28,736 cycles

AFT CARGO COMPARTMENT SEAT TRACK AT RBL 25 BETWEEN FS 1800 TO 1920, HAS GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK IAW SRM 51-31-01, MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 1940-1964) · corrosion level 2 · airframe 63,825 hrs · 28,736 cycles

AFT CARGO COMPARTMENT SEAT TRACK, RBL 25 BETWEEN FS 1940 TO FS 1964, GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK AT IAW SRM 51-31-01, MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1902) · corrosion level 2 · airframe 63,825 hrs · 28,736 cycles

AFT CARGO COMPARTMENT FLOORBEAM BS 1902 IS CORRODED FROM RBL15 TO LBL15. REMOVED DAMAGE IAWSRM 53-00-01 FIG.8 AND SRM 51-31-01. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 53-00-01. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-00-01 FIG 8 AND SRM 51-31-01. MAJOR REPAIR.

Part: CARGO TRACK — GOUGED (BS 1920-1964) · airframe 63,825 hrs · 28,736 cycles

AFT CARGO BAY CARGO TRACK, LBL 25 BETWEEN BS 1920-1964 GOUGED AND CORRODED. REMOVED, AND FABRICATED, REPAIR SPLICES AND PLATES AND REPLACED CARGO TRACK IAW SRM 53-70-00 FIG.1 AND SRM 51-31-01. MAJOR REPAIR.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 63,825 hrs · 28,736 cycles

LEFT WING, INBD FLAP, LOWER OTBD SKIN PUNCTURED. TRIMMED OUT DAMAGE IAW 57-00-01, HFEC IAW NTSPM 06-10-01. NO CRACKS NOTED. FABRICATED SKIN DOUBLER, TEE DOUBLERS, TEE FILLER AND SKIN FILLER IAW SRM 57-00-01 FIG.3 INSTALLED ALL REPAIR PARTS IAW SRM 57-00-01 FIG.4 AND SRM 51-31-01. MAJOR REPAIR.

Part: PULLEY — WORN (L1 DOOR) · airframe 63,825 hrs · 28,736 cycles

L1 DOOR FWD DRIVE TRACK, UPPER FORWARD PULLEY WORN. FURTHER INSPECTION FOUND PULLEY TO BE SPLIT. MINOR REPAIR R & R L1 DOOR UPPER FWD DRIVE PULLEY IAW SRM 51-31--01 AND MM 52-11-00. NO RIG DISTURBED AND OPS CHECKED GOOD IAW MM 52-11-00-5.

Part: SHEAR TIE — CRACKED (BS 1800 L18R) · airframe 63,825 hrs · 28,736 cycles

MCD CABIN RT SIDEWALL AT STA 1800 AT L-18 SHEAR TIE CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF SHEAR TIE IAW SRM 53-30-00 FIG 10, SRM 51-31-01 AND SRM 51-21-02. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1801-1821) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT RBL 45.5 BETWEEN FS 1801 AND FS 1821 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK SECTION, REPAIR SPLICES AND PLATES. INSTALLED REPAIR PARTS IAW SRM 53-70-00 AND SRM 51-31-01. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (BS 1821-1841) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT RBL 45.5 BETWEEN FS 1821 AND FS 1841 UPPER LOBE HAS ELONGATED HOLE. REPLACEMENT ACCOMPLISHED ON NON-ROUTINE N00471 AND IS CLASSIFIED AS MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1721-1741) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT LBL 45.5, FS 1721-1741 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED REPAIR SLICES AND PLATES AND INSTALLED IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — GOUGED (MAIN DECK) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT LBL 45.5 BETWEEN FS 1721 AND FS1741 LOBE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED TRACK , REPAIR SPLICES AND PLATES IAW SRM 53-70-00 FIG.1 VOL.1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT LBL45.5 BETWEEN FS 1621 AND 1641 UPPER LOBE HAS ELONGATED HOLE. REMOVED DAMAGED SEAT TRACK SECTION , FABRICATED TRACK, REPAIR SPLICES AND PLATES IAW SRM 53-70 00 FIG.1 VOL. 1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (MAIN DECK) · airframe 63,825 hrs · 28,736 cycles

SEAT TRACK AT LBL 45.5 BETWEEN FS 1621 AND FS 1641 UPPER SURFACE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG.1 FABRICATED REPAIR SLICES AND PLATES IAW SRM 53-70-00 FIG 1. INSTALLED TRACK SECTION, SPLICES AND PLATES IAW SRM 53-70-00 FIG 1.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 62,906 hrs · 28,336 cycles

AFTER O2 MASK WERE USED IN FLIGHT ALL 3 O2 BOTTLES DROPPED TO 0 PSI. SERVICED ALL 3, CREW O2 BOTTLES PER AMM 12-14-35. CHECKED ALL BOTTLES AND MASK SYSTEMS FOR LEAKS PER AMM 35-11-00-06-0. FOUND ONE RT COURIER MASK SLIGHTLY LEAKING AT INTIAL BOTTLE RESERVICE. LEAK STOPPED AFTER 500 PSI WAS ADDED TO O2 BOTTLES. PER CREW SUSPECT FIRST OFFICERS MASK WAS STUCK IN ON POSITION AFTER IT'S USE. OPERATED ALL MASKS AFTER SERVICE. ALL MASKS OPERATE NORMALLY PER AMM 35-11-00-06-0.

Part: BUNGEE CYLINDER — DAMAGED (LT MLG) · airframe 62,422 hrs · 28,125 cycles

AFTER T/O, LT MAIN REMAINED UNSAFE FOLLOWED QRH CYCLED NO CHANGE. GEAR APPEARED TO BE DOWN ENTIRE TIME. UNEVENTFUL LANDING. REMOVED & REPLACED L/H MLG BUNGEE CYCLINDER ASSY ACFT OK FOR SERVICE.

Part: SEAT TRACK — DAMAGED (BS 1229-1286) · airframe 58,017 hrs · 26,124 cycles

MAIN CABIN, BS 1240, LBL 48, SEAT TRACK SCALLOP CHIPPED AND WORN RE-EVALUATED TRACK. TRACK HAS CHIPPED/BROKEN AREAS. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED DAMAGED SECTION AND INSTALLED FABED/NEW SECTION IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1, DC/MD10-10 SRM 51-33-01 VOL II PG 1. MAT ID NEW TRACK. FABED NEW SECTION IAW DC/MD10-10 SRM 53-70-00 VOL I PG 4. ALODINED AND PRIMED TRACK IAW DC/MD10-10 SRM 51-21-01 VOL II PGS 1-24. REMOVED AND REINSTALLED FLOOR PANELS IAW MD10-10 M/M 53-21-01-2.

Part: DOOR FRAME — CORRODED (MAIN CARGO DOOR) · corrosion level 2 · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR JAMB TOP SURFACE UNDER NR 5 SPOOL FITTING HAS EXFOLIATION, STA 712. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 FIG 1 VOL I. ORIGIONAL .100, REMOVED .047, REMAINING .053. LOCATION OF DAMAGE AT STA 712, LBL 117. UPPER JAMB ACA7226-1 WAS REPLACED ON NON-ROUTINE N00665.

Part: DOOR FRAME — CORRODED (MAIN CARGO DOOR) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB TOP SURFACE MOST AFT PART OF JAMB AT STA 766 HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 VOL I. ORIGIONAL .100, REMOVED.027, REMAINING .073. LOCATION OF DAMAGE STA 766, LBL 117. UPPER JAMB ACA7226-1 WAS REPLACED ON NON- ROUTINE N00665

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 58,017 hrs · 26,124 cycles

CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1139 LBL 48 EVALUATED SEAT TRACK, FOUND BROKEN SCALLOP, OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED AND REPLACED OUT OF LIMIT SECTION IAW DC/MD10 SRM 51-31-01 VOL II PG 1 AND DC/MD10 SRM 51-33-01 VOL II PG 1. MAT ID SEAT TRACK, SPLICE HAT AND PLATE. SCALLOPED SEAT TRACK. FAB`D SEAT TRACK AND SPLICE HAT AND PLATE IAW DC/MD10 SRM 53-70-00 VOL I PG 3 AND 4. ALODINED AND PRIMED SEAT TRACK, SPLICE HAT AND PLATE IAW DC/MD10 SRM 51-21-01 VOL II PG 1 AND 21, MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 58,017 hrs · 26,124 cycles

MAIN CABIN APPROX AT STA 1256 AND STA 1264 SEAT TRACK SCALLOPS (3EA) ELONGATED (N7513) AT LBL 48 EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. MAT ID S4929150 PO NR 595343.1 IAW DC/MD10 SRM 53-42-01 FIG 5 VOL III. FABRICATED SEAT TRACK IAW DC/MD10 SRM 53-70-00 PG 4 VOL I FIG 1. ALODINED AND PRIMED IN REF TO DC/MD10 SRM 51-21-01 VOL II PG 5.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,017 hrs · 26,124 cycles

MAIN CABIN APPROX AT STA 1531 LBL 27 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STA 1490 TO 1531 LBL 27 IAW DC-10/MD-10 SRM 53-70-00, VOL I, FIG 1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 792 LBL 49. CHECK LIMITS AND IS OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. FABRICATED SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 SRM 53-70-00 PG 4 FIG 1 VOL I. DRILLED NEW SEAT TRACK IAW DC/MD10-10 51-31-01 VOL II PG 1. INSTALLED SEAT TRACK, SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

FOUND MAIN CABIN, BS 1085, RBL 28, SEAT TRACK SCALLOP CHIPPED. BLENDED AREA; CHECKED LIMITS. GAP BETWEEN SCALLOPS IS.520 MAX ALLOWED IS .500 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED DAMAGED TRACK SECTION AND INSTALLED NEW SECTION IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. MAT ID NEW TRACK SECTION FABED NEW TRACK IAW DC/MD10-10 SRM 53-70-00 VOL I FIG 1. ALODINED AND PRIMED NEW SECTION IAW DC/MD10-10 SRM 51-21-01 VOL II PG 1-24, REMOVED AND REINSTALLED FLOOR PANELS IAW DC/MD10-10 M/M 53-21-01-2

Part: ANGLE — CHAFED (NR 1 PYLON) · airframe 58,017 hrs · 26,124 cycles

NR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACHMENT PIN & BUSHING, INSPECTED AREA OF BEARING & BUSHING IAW FEDEX WORK CARD 54X1201ALI-P1 LUBED THRUST LINK BEARING IAW FEDEX MM 12-21-02-3, NO DISCREPANCIES NOTED

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1059 LBL 48. FOUND TO BE OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 PGS 21 & 22 VOL I REMOVED TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10. IAW DC/MD10-10 SRM 53-42-01 VOL III PGS 13 & 14. FABRICATED SEAT TRACK IAW DC/MD10-10 SRM 53-70-00 VOL I PGS 3 & 6A. ALODINED AND PRIMED IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10 STA 989-1109 LBL 48 REMOVED AND INSTALLED FLOORBOARDS STA 979-1159 LBL 26-76 IN REF TO MD10 AMM 53-21-01-2

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. BLENDED AREA .500 MAX LIMIT GAP .510 REMAIN. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 & 22. MAT ID TRACK, SPLICE HAT & PLATE. REMOVED DAMAGED TRACK INSTALLED NEW SECTION IAW DC/MD10-10 SRM 51-31-01 PG 1 VOL II. ALODINED AND PRIMED PARTS IAW DC/MD10-10 SRM 51-21-01 VOL II PG 1-24, REMOVED AND REISTALLED FLR PANELS IAW MD10-10 AMM 53-21-01-2. FABED PARTS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 3 & 4

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 814 LBL 29. CHECKED LIMITS ON SEAT TRACK SCALLOPS. SCALLOPS TO SCALLOPS IS .510 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. DIAL CALIPERS USED T8278D. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. DRILLED NEW SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL I I PG 1. ALODINED AND PRIMED SEAT TRACK IAW DC/MD10-10 SRM 51-21-01 VOL II PG 21. INSTALLED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

FOUND MAIN CABIN AT STA 1441 RBL 48 SEAT TRACK WORN. BLENDED SEAT TRACK, WIDTH OF SCALOP HAS .200 REMAINING MIN IS .260 OUT OF LIMITS IAW DC 10 SRM 53-70-00 VOL I PG 21". REMOVED AND REPLACED DAMAGED SECTION OF TRACK IAW DC/MD10 51-31-01. ALODINED & PRIMED TRACK AND SPLICE HAT & PLATE IAW DC 10 SRM 51-21-01. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 7 SPOOL LOCATION, ALL FOUR HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES A,B,D WITH CRACK INDICATION. REPLACED NR 7 FITTING IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA7224 REV G.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 4 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO .460 TO REMOVE CORROSION. WITHIN LIMITS OF MD/DC10-10 SRM 53- 50-00 FIG 17 VOL I. HOLE D REAMED TO REMOVE CORROSION AND INSTALLED BUSHING IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. NDT FOR CRACKS HOLES A,B,C,D, NO DEFECTS NOTED IAW NTSPM 06-10-01-003. TOOL T8203A MEASURING TOOL T8723K

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 6 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO 0517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES B AND C WITH CRACK INDICATION. REPLACED NR 6 FITTING IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA 7224 REV G.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 5 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES A,B,D WITH CRACK INDICATION. REPLACED NR 5 FITTING IAW SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA 7224 REV G.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 1 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE COROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. REPLACED FITTINGAFA7132-1 IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA7224 REV G.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR LOWER JAMB AT NR 2 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE CORROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. REPLACED NR 2 FITTING AFA7132-1 IN REF TO MD/DC10-10 SRM 51-33-01 VOL II AND DAC DWG ACA7224 REV G.

Part: BEAM — CORRODED (FUSELAGE) · airframe 58,017 hrs · 26,124 cycles

MAIN CARGO DOOR JAMB TOP SURFACE UNDER CENTERING GUIDE HAS SURFACE CORROSION, STA 660. REMOVED AND REPLACED BEAMS ACA7225-1 AND ACA7226-1 IN REF TO DAC DRAWING ACA7224 REV G AND DC/MD10-10 SRM 51-31-01 VOL II PG 1, MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DC/MD10-10 SRM 51-35-01 VOL II PG1

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,017 hrs · 26,124 cycles

RT HORIZONTAL STAB UPPER REAR SKIN PANEL HAS APPROXIMATELY A I/2 INCH LONG CRACK INDICATION. REPAIRED RIGHT HAND HORIZONTAL STAB SKIN PANEL IN REFERENCE TO EA 8-5510-109228.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,144 hrs · 25,716 cycles

EXFOLIATION CORROSION LOCATED AT LOWER AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. CORROSION EXCEEDED SRM LIMITS AFTER REMOVAL, REQUIRED EA TO FLY UNTIL NEXT C CHECK.

Part: LOOP — FAULTY (NR 2) · airframe 55,545 hrs · 25,046 cycles

CLIMBOUT FROM MEMPHIS GOT A LEVEL 3 AIR MAN NR 2 FAILED WARNING WENT AWAY AFTER THROTTLE WAS AT IDLE FOR A COUPLE OF MINUTES, DUMPED 6000 LBS FUEL FOR LANDING. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 05SEP06 "MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP, INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START."

Part: NONE — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

EXT MOD DOUBLER/RPR JUST FWD OF NR 10 RPR LOCATION SHEET AT 6 O`CLOCK STA 1581. ACCOMPLISHED EA# 8-5330-95694.

Part: SEAT TRACK — CORRODED (BS 835) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN STA 835 X 107 FOUND SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REMOVED CORROSION IAW SRM 53-70-00 FIG 5 VOL 1 FOUND OUT OF LIMIT. TO GAIN ACCESS FOR REPAIR TRACK, REMOVED L2 DOOR IAW MM 52-12-03-02. CUT AND REMOVED SEAT TRACK SECTION FROM STA 765-869. REPLACED WITH NEW ONE AND SPLICED IAW SRM 53-70-00 FIG 1 VOL 1. PERFORMED GVI ON DOOR PRESSURE SEAL AND FOUND OK. AFTER REPAIR REINSTALLED L2 DOOR IAW MM 52-12-03-2. FABRICATED PARTS IAW PARTS TRAVELER F166661-7, F166661-3 AND SRM 53-70-00 FIG 1 VOL 1.

Part: INTERCOSTAL — CORRODED (BS 1681-1701) · airframe 55,123 hrs · 24,867 cycles

CTR CARGO COMPT CORROSION WITH EXFOLIATION ON INTERCOSTAL STA 1681-1701 L43 RT. REMOVED ROLLER, CHANNEL AND FASTENER IAW SRM 51-31-01 AND 51-35-01 VOL 2 AT STA 1681. REMOVED CORROSION IAW SRM 51-21-01 VOL 2, MTL REMOVED IS O/L IAW SRM 53-50-0 VOL 1, PERFORMED EA 8-5315-96077. REINSTALLED PARTS IAW SRM 51-31-01 AND SRM 51-35-01 VOL 2 AT STA 1710. REMOVED FASTENER TO GAIN ACCESS IAW SRM 51-35-01 VOL 2. CORROSION REMOVED AT STA 1710 IS O/L IAW SRM 53-50-01 VOL 1 ON AFA3873-7 ANGLE ON LONG 43. TRIMMED WEB FOR ACCESS AT STA 1708 L 40, INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-01 FIG 7 VOL 1. RE-INSTALLED WEB, FASTENERS AND INSTALLED DOUBLER REPAIR.

Part: CHANNEL — CORRODED (BS 869-849) · airframe 55,123 hrs · 24,867 cycles

FWD CARGO COMPT AT STA 869 AND 849 WAS FOUND WITH 2 SEVERE CORROSION AT X33 LT ON ROLLER CHANNEL. REMOVED RESTRAINT CATCH IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND IAW SRM 51-35-01 PAGE 1/13 VOL 2. CUT CHANNEL BETWEEN STA 840 AND 824, PERFORMED REPAIR IAW SRM 53-70-00 FIG 17 VOL 1 USING EXISTING SPLICE AT STA 879. REINSTALLED RESTRAINT CATCH IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND IAW SRM 51-35-01 PAGE 1/13 VOL 2. FABRICATED PARTS IAW DETAIL. PARTS TRAVELER F167195/N01195 AND IAW SRM 53-70-00 FIG 17 VOL 1.

Part: NONE — NONE (NONE) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER AT FUSELAGE SKIN STA 577-595 LONGERONS 30-32 LT. REMOVE WEB TO GAIN ACCESS IAW SRM 51-33-01 VOL 2. REMOVED BLIND RIVETS IAW SRM 51-35-01 PAR 1-5 VOL 2. INSTALLED NEW FASTENERS IAW SRM 53-50-00 FIG 3 VOL 1. AFT REWORK ACTION THE EXISTING REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST BY FEDEX EO 8-5100-7-5001 P1. REINSTALLED WEB REMOVED TO GAIN ACCESS IAW SRM 51-33-01 VOL 2.

Part: NONE — NONE · airframe 55,123 hrs · 24,867 cycles

EXTERNAL FUSELAGE AT STA 1001 BETWEEN LONGERONS 39-42 RT FOUND EXT DOUBLER. REPAIR FWD CARGO DOOR AFT JAMB. AFTER REPLACED QTY NR 2 HI-LOCKS IAW SRM 53-50-00 FIG 22 VOL 1. REPAIR IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN INT STRUCTURE STA 1256 X107 LT FOUND 3EA CRACK ON LOWER L3 JAMB DOOR WEB. REPAIRED IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F166702/N00702 AND IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 55,123 hrs · 24,867 cycles

DURING INSPECTION OF HORIZ STAB, INSP CONSTANT SECTION FOUND CRACK ON PANEL P/N 7207-1 POSITION 15. ACCOMPLISHED EA NR 8-5510-93811, REINSTALLED FAIRING IAW SB 55-16 AND IAW SRM 51-31-01 PAR 6 VOL 2.

Part: NONE — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

STA 969-989 X-47.5 SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH HI-LOKS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION ON SEAT TRACK SPLICES THE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST BY FEDEX EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

FOUND STA 999 BETWEEN LONGERONS 38-40 RT FWD CARGO DOOR SFT JAMB HAS A FRAME REPAIR. REMOVE TORQUE BOX ACCESS COVER, REMOVED ALUMINUM FOIL , REMOVED SEALANT AND CLEAN AREA IAW SRM 51-21-01 PAR 22 VOL 2, PERFORMED DVI IAW EA #8-5230-95696. FOUND IN COMPLIANCE WITH CRITERIA REQUEST OF EO #8-5100-7-5001 P2. REINSTALLED ALUMINUM FOIL, RESTORE SEALANT IAW DPS 2.50-4.2. REINSTALLED TORQUE BOX ACCESS PANEL IAW SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

FOUND STA 899 BETWEEN LONGERON 38-40 RT FWD CARGO DOOR FWD JAMB, HAS A FRAME REPAIR. REMOVED TORQUE BOX ACCESS COVER, REMOVED ALLUMINIUM FOIL, REMOVED SEALANT AND CLEAN AREA IAW SRM 51-21-01 PAR 22 VOL 2. PERFORMED DVI IAW EA #8-5230-95696 FOUND IN COMPLIANCE WITH CRITERIA OF EO NR 8-5100-7-5001 P2, REINSTALLED ALLUMINIUM FOIL. RESTORE SEALANT IAW DPS 2.50-4.2, REINSTALLED TORQUE BOX ACCESS PANEL IAW SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2.

Part: NONE — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 801-834 X 27.5 EXISTING SEAT TRACK SPLICE REPAIR. FABRICATED PART IAW DETAIL PART TRAVELER F167228/N01228 AND IAW SRM 53-70-00 FIG 1 VOL 1. REPLACE SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1 USING EXISTING SPLICE AFTER REWORK RETURN IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

FOUND MAIN CARGO COMPT STA 615-675 X-8.5 EXISTING SEAT TRACK SPLICE REPAIR. FABRICATED PART IAW DETAIL PART TRAVELER NRC F167224/N01224 AND SRM 53-70-00 FIG 1 VOL 1. REPLACED SEAT TRACK FROM STA 605 TO STA 665 IAW SRM 53-70-00 FIG 1 VOL 1. REMOVED ON SEAT TRACK SPLICES THE GANG CHANNEL AND REPLACED SCREWS WITH HI-LOCKS IAW SRM 53-70-00 FIG 1 VOL 1. AFTER REWORKED ACTION ,THE EXISTING SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST ON FEDEX EO #8-5100-7-5001 P2.

Part: LONGERON — CRACKED (BS 1671-1681) · airframe 55,123 hrs · 24,867 cycles

CTR CARGO COMPT CRACK 8 INCHES ON LONGERON 44 RT FROM STA 1671 TO STA 1681. CUT CAP FRAME AT STA 1681 LONG 44-45, REPLACED LONGERON IAW SRM 51-33-01 PAR 6-10 VOL 2. INSTALLED SPLICE REPAIR IAW SRM 53-30-00 FIG 5-8 VOL 1.

Part: NONE — NONE (NONE) · airframe 55,123 hrs · 24,867 cycles

LT WING INBOARD FLAP UPPER SKIN STA XIFH 126 FOUND DOUBLER REPAIR. REMOVE PANEL IAW SRM 51-31-01 PAR 6 VOL 2, REMOVED OLD REPAIR DOUBLER AND SEALANT IAW SRM 51-33-01 PAR 6 VOL 2 AND MM 12-22-02-01-7, PERFORMED NEW REPAIR DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1. REINSTALLED PANEL IAW SRM 51-31-01 PAR 6 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F167104/N01104 AND IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

HORIZONTAL STAB O/B SECTION LOWER SIDE HAS EXISTING REPAIR XCH 44.5567. REMOVED PAINT IAW SRM 51-21-01 PAR 21 VOL 2, PERFORMED NDI IAW NDT SP 4-6 FOUND STUD PANEL IS IN 7075-T651 COLD MATERIAL, TREATED AREA IAW SRM 51-21-01VOL 2. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA EO NR 8-5100-7-5001 P2.

Part: NONE — NONE · airframe 55,123 hrs · 24,867 cycles

RT WING NR 8 L/E SLAT FLUSH REPAIR ON EXT SKIN. REMOVED EXISTING REPAIR IAW SRM 51-35-01 PAR 6 VOL 2, PERFORMED NEW REPAIR IAW SRM 57-10-00 FIG 11 VOL 1, FAB PART IAW DETAIL PART TRAVELER F167113/N01113 AND SRM 57-10- 00 FIG 11 VOL 1.

Part: SEAT TRACK — WORN (BS 1129-1249) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN DEEP WEAR ON SEAT TRACK X-47 STA 1151. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1 VOL 1BETWEEN STA 1129 AND STA 1249 X-47. FABRICATED PART IAW DETAIL PART TRAVELER NR F167196/N01196 AND SRM 53-70-00 FIG 1 VOL 1.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

FOUND MAIN CARGO COMPT STA 791-830 X-8.5 EXISTING SEAT TRACK SPLICE REPAIR. PERFORMED VISUAL INSPECTION OF SEAT TRACK SPLICE REPAIR FOR CRITERIA REQUEST BY EO NR 8-5100-7-5001P2. FOUND REPAIR IN COMPLIANCE.

Part: NONE — NONE · airframe 55,123 hrs · 24,867 cycles

LT HORIZONTAL STAB REAR SPAR STA XE 77.100 HAS DOUBLER REPAIR UPPER SKIN. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: DOUBLER — DAMAGED (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT WING L/E NR 2EA CRACK 1" LONG INTERNAL DOUBLER AT STA XOS 645. PERFORMED REPAIR DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1. FAB PART IAW DETAIL PART TRAVELER F166372/N00372 AND IAW SRM 57-10-00 FIG 71 VOL 1.

Part: REPAIR — MISINSTALLED · airframe 55,123 hrs · 24,867 cycles

EXISTING DOUBLER STA 1871-1877 LONG 51-52 RT. REMOVED EXISTING REPAIR IAW SRM 51-35-01 VOL 2, PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1. FAB PART IAW DETAIL PART TRAVELER F167062/N01062 AND SRM 53-20-00 FIG 6 VOL 1.

Part: REPAIR — MISREPAIRED (SEAT TRACK) · airframe 55,123 hrs · 24,867 cycles

FOUND STA 1511-1551 X 8.5 SEAT TRACK SPLICE REPAIR. PERFORMED INSP ON SEAT TRACK SPLICE REPAIR REWORKED FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. FAB PART IAW DETAIL PART TRAVELER NR F167238/N01238 AND SRM 53-70-00 FIG 1 VOL 1. REPLACED SEAT TRACK SECTION FROM STA 1471 TO 1551 BY 8.5 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 725-775 EXISTING TRACK SPLICE REPAIR AT X 47.5. FAB PART IAW DETAIL PART TRAVELER NR F167220/N01220 AND SRM 53-70-00 FIG 1 VOL 1. REPLACED EXISTING SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH HI-LOCKS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE EXISTING SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST ON FEDEX EO NR 8-5100-7-5001 P2.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 55,123 hrs · 24,867 cycles

LEFT WING L/E CRACK INTERNAL DOUBLER AND SPLICE AT STA XOS 670. REPLACED DOUBLER IAW SRM 51-33-01 PAR 6-10 AND SRM 51-35-01 PAR 1-5 VOL 2 AND IAW DWG 1249, PERFORMED REPAIR DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.

Part: REPAIR — MISINSTALLED (SEAT TRACK) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 889 - 969 X-47.5 SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED SCREWS WITH HI-LOKS IAW SRM 53-70-00 FIG 1 VOL 1, AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 700-735 X-47.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH LOCK FASTENER IAW SRM 57-70-00 FIG 1 VOL 1. AFT REWORK THE EXISTING REPAIR ON SEAT TRACK RETURNED IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — MISINSTALLED (SEAT TRACK) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 595-645 X=47.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN REQUIRED CRITERIA OF EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 879-889) · airframe 55,123 hrs · 24,867 cycles

EXT MOD DOUBLER REPAIR JUST AFT OF NR 9 ON REPAIR LOCATION STA 879-889. REMOVED OLD DOUBLER AND PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1. FAB PARTS IAW DETAIL PARTS TRAVELER F167066/N01066 AND IAW SRM 53-20-00 FIG 6 VOL 1.

Part: REPAIR — UNKNOWN (BS 1154) · airframe 55,123 hrs · 24,867 cycles

INT FUSELAGE STA 1154 FOUND PANEL REPAIR. REMOVED OLD DOUBLERS IAW SRM 51-35-01 VOL 2. PERFORMED GVI ON AREA, NO CRACK FOUND, PERFORMED NDI INSPECTION, NO DAMAGE FOUND. TREATED AREA IAW SRM 51-21-01 VOL 2 AND INSTALLED NEW -3, -5, -7, DOUBLERS IAW SRM 53-40-00 FIG 4 VOL 1.

Part: BEAM — CRACKED (BS 1009) · airframe 55,123 hrs · 24,867 cycles

PERFORMED GVI IAW EA 8-2580-93325 FOUND IN FWD CARGO COMPT 1EA CRACK 2.5 INCH LONG ON BEAM STA 1099 X = 58. PERFORMED REPAIR SPLICE IAW SRM 53-60-01 FIG 3 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F166833/N00833 AND IAW SRM 53-60-01 VOL 1.

Part: REPAIR — MISINSTALLED (SEAT TRACK) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 830 - 899 X-47.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1, AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUEST ON EO 8-5100-7-5001 P2.

Part: WEB — CRACKED (BS 1505) · airframe 55,123 hrs · 24,867 cycles

UNDER WING TO BODY AFT SIDE OF LEFT MLG W/W FOUND 1EA CRACK 5 INCHES LONG ON WEB AT STA 1505. PERFORMED REPAIR IAW SRM 53-50-00 FIG 2A SHT 1 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F166194/N00194 AND IAW SRM 53-50-00 FIG 2A SHT 1 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN STA 879 - 939 X = 47.5 EXISTING SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUIRED ON EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSLEAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 615 - 655 X = 27.5 EXISTING TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1, AFT REWORKED ACTION OF SEAT TRACK SPLICE REPAIR, RETURNED IN COMPLIANCE WITH CRITERIA REQUIRED ON EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 615 - 655 X = 8.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH HI-LOKS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUIRED ON EO 8-5100-7-5001 P2.

Part: REPAIR — MISINSTALLED (BS 700) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 700 - 735 X-47.5 EXISTING SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE EXISTING REPAIR ON SEAT TRACK RETURNED IN COMPLIANCE WITH CRITERIA REQUEST ON EO 8-5100-7-5001 P2.

Part: SEAT TRACK — CORRODED (BS 1901-2007) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN BETWEEN STA 1901 TO 2007 X-107 FOUND CORROSION WITH EXFOLIATION INSIDE TRACK. FABRICATED PARTS IAW DETAIL PARTS TRAVELERS F166664/N00664 AND SRM 53-70-00 FIG 1 VOL 1. REMOVED PARTS IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01 PAGE 34/47 AND SRM 51-31-01 PAGE 36/41 VOL 2 AND MM 53-1-02-2, REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 3-4 AND FIG 6 VOL 1. REINSTALLED PARTS IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01 PAGE 34/47 AND SRM 51-31-01 PAGE 36/41 AND MM 53-21-02-2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING SPOILER NR 4 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING SPOILER NR 2 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING UPPER SPOILER NR 1 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (RT WING) · airframe 55,123 hrs · 24,867 cycles

RIGHT WING NR 5 SPOILER UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

RIGHT WING SPOILER NR 4 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (N/A) · airframe 55,123 hrs · 24,867 cycles

LEFT WING SPOILER NR 5 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING UPPER SIDE STA XORS 402 JUST FWD OF I/B AILERON FOUND BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

RIGHT WING NR 3 SPOILER UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING UPPER SKIN STA XORS 180 FOUND BONDED REPAIR PANEL P/N ARC0269. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING UPPER SIDE STA XORS 103 FOUND BONDED REPAIR PANEL P/N ARC0340. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN · airframe 55,123 hrs · 24,867 cycles

LEFT WING UPPER SIDE STA XORS 403 JUST FWD I/B AILERON FOUND BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — MISINSTALLED (BS 909-969) · airframe 55,123 hrs · 24,867 cycles

STA 909 - 969 X-27.5 SEAT TRACK SPLICE REPAIR. PERFORMED INSPECTION ON SEAT TRACK SPLICE REPAIR FOUND NOT IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 FOUND SCREWS INSTEAD OF HI-LOK AND GANG CHANNEL INSTEAD OF NUT REMOVED GANG CHANNEL AND REPLACED BOLTS WITH HI-LOKS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORK RETURNED IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 1986-1995) · airframe 55,123 hrs · 24,867 cycles

EXT PLUG REPAIR STA 1986 - 1995 LONG 44 RIGHT. REMOVED OLD REPAIR IAW SRM 51-35-01 VOL 2. PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN FOUND NR 2EA CRACK .75 INCH LONG ON LOWER AFT WEB JAMB DOOR NR 3 RIGHT AT STA 1305 LONG 26 RIGHT. FABRICATED PART IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1 AND DETAIL PART TRAVELER F166704/N00704 INSTALLED PART IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1.

Part: REPAIR — NONE (BS 1009-1089) · airframe 55,123 hrs · 24,867 cycles

STA 1009 - 1089 X = 8.5 SEAT TRACK SPLICE REPAIR. PERFORMED INSPECTION ON SEAT TRACK SPLICE REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 775-791) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER FUSELAGE SKIN. REMOVED OLD REPAIR IAW SRM 53-33-01 VOL 2. PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1.

Part: REPAIR — CORRODED (SEAT TRACK) · airframe 55,123 hrs · 24,867 cycles

STA 1696 X = 27.5 EXISTING SEAT TRACK PLUG REPAIR. REMOVED CHANNEL IAW SRM 51-31-01 PAR 36/41 VOL 2. CLEANED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 VERIFICATED LIMITS IAW SRM 53-70-00 FIG 2 SHT 2 VOL 1 ORIGINAL THK IS .562 INCH IAW SRM 53-70-00 SHT 2 FIG 2 VOL 1, RESIDUAL THK IS .560 INCH % REMOVED MATERIAL IS 0.3 THK IS IN LIMITS IAW SRM 53-70-00 FIG 2 VOL 1. TREATED AREA IAW SRM 51-21-01 PAR 36/41 VOL 2 PERFORMED VISUAL INSP. REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST OF EO 8-5100-7-5001 P2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

DISCREPANCY MAIN CABIN INT FWD DOOR JAMB NR 3 RT FOUND NR1 EA CRACK 2 INCH LONG ON INTERCOSTAL PLANE JAMB ST STA 1256 Z-19. REMOVED DOUBLER AND TRIMMED OUT CRACK ON WEB FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-10-01 FIG 10 AND SRM 51-33-01 PAR 6-10 VOL 2 FABRICATED PARTS IAW DETAIL PARTS TRAVELER F167200/N01200 AND SRM 53-00-01 FIG 10 AND DWG AEA0210.

Part: SPLICE — DAMAGED (MAIN CARGO BAY) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 1129-1169 X-75.25 SEAT TRACK SPLICE REPAIR. PERFORMED VISUAL INSP OF SEAT TRACK SPLICE REPAIR FUS STA 1129-1169 X-75.25 FOLLOWING CRITERIA OF EO NR 8-5100-7-5001 P2.

Part: BULKHEAD — CRACKED (BS 1501) · airframe 55,123 hrs · 24,867 cycles

DISCREPANCY CLG SPACE FOUND 1EA CRACK 1 INCH LONG ON SKIN OF BLKHD AT STA 1501 X30 RT. PERFORMED REPAIR DOUBLER IAW SRM 53-00-00 FIG 10 VOL 1 AND REPLACED FIITING IAW SRM 51-33-01 PAR 6-10 VOL 2.

Part: DOUBLER — DAMAGED (RT WING FLAP) · airframe 55,123 hrs · 24,867 cycles

DISCREPANCY RT WING OB FLAP UPPER SKIN XOFH 599 EXTERNAL DOUBLER. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 VOL 1.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 55,123 hrs · 24,867 cycles

DISCREPANCY LT WING OB FLAP UPPER SKIN AT STA XOF 458 HAS DOUBLER REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-35-01 VOL 1 AND PERFORMED NEW REPAIR. DOUBLER IAW SRM 57-10-00 FIG 9 VOL 1.

Part: SKIN — WORN (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT 1R REF FOUND LE FWD WEAR ON SKIN. PERFORMED REPAIR DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1 FABRICATED PART IAW SRM 57-00-01 FIG 4 AND DETAIL PART TRAVELER F166343/N00343.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN FOUND NR 2EA CRACK .75 INCH LONG ON LOWER FWD WEB JAMB DOOR NR 3 RIGHT AT STA 1256 LONG 27 RIGHT. REPAIRED WEB JAMB DOOR NR 3 RIGHT STA 1256 IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1, AFTER REMOVED DOUBLER, FABRICATED PART IAW DETAIL PART TRAVELER F166706/N00706 AND IAW SRM 53-50-00 FIG 19 VOL 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT WING L/E 2EA CRACK 1 INCH LONG INTERNAL DOUBLER AT STA XOS 589. PERFORMED REPAIR IAW SRM 57-10-00 FIG 71 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER NR N00374 AND IAW SRM 57-10-00 FIG 71 VOL 1.

Part: REPAIR — NONE (FUSLEAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CARGO COMPT STA 989-1109 X-47.5 FOUND EXISTING SEAT TRACK SPLICE REPAIR. PERFORMED INSPECTION ON SEAT TRACK SPLICE REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

STA 939 X 27.5 EXISTING TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.

Part: REPAIR — NONE (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT WING INBOARD AILERON AT STA XIA 341 LOWER SKIN HAS DOUBLER REPAIR. PERFORMED GVI ON DOUBLER REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

LT WING INBOARD AILERON AT XIA 341 UPPER SKIN HAS DOUBLER REPAIR. PERFORMED A GVI ON DOUBLER REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

STA 1809 X 27.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED A GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

STA 1440 X - 47.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

STA 1491 X -47.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.

Part: REPAIR — NONE (HORIZONTAL STAB) · airframe 55,123 hrs · 24,867 cycles

EXISTING DOUBLER REPAIR ON LT HORIZONTAL STAB UPPER SKIN AT XE 77.100. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FRAME) · airframe 55,123 hrs · 24,867 cycles

STA 645 BETWEEN LONGERONS 11-13 RT FOUND FRAME REPAIR. PERFORMED EA 8-5330-95683.

Part: REPAIR — UNKNOWN (BS 515-525) · airframe 55,123 hrs · 24,867 cycles

FLUSH REPAIR AT FUSELAGE SKIN FROM STA 515 TO STA 525 AT LONG 17 LT. PERFORMED INSPECTION FOUND REPAIR IN COMPLIANCE WITH CRITERIA REQUEST BY EO8- 5100-7-5001 P1 AND EA 8-5330-94664.

Part: REPAIR — UNKNOWN (FRAME) · airframe 55,123 hrs · 24,867 cycles

STA 715 BETWEEN LONGERONS 11-13 RT FOUND FRAME REPAIR. PERFORMED EA 8-5330-95683.

Part: REPAIR — UNKNOWN (FRME) · airframe 55,123 hrs · 24,867 cycles

STA 735 BETWEEN LONGERONS 11-13 RT FOUND FRAME REPAIR. PERFORMED EA 8-5330-95683.

Part: FRAME — CRACKED (BS 455) · airframe 55,123 hrs · 24,867 cycles

FWD AVIONIC COMPT FOUND 1 CRACK 1" LONG ON FRAME STA 455 LT SIDE (REMOVED PART FOR ACF). TRIMMED OUT CRACK AND PERFORMED REPAIR IAW SRM 53-30-00 FIG 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F166546/N00546 AND IAW SRM 53-30-00 FIG 4 VOL 1.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL FUSELAGE AT STA 550 TO 570 BETWEEN LONG 46 TO 48 LT FOUND EXISTING REPAIR DOUBLER. PERFORMED GVI FOUND REPAIR NOT IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. REMOVED EXISTING REPAIR IAW SRM 51-35-01 PAR 1-5 VOL 2. PERFORMED NEW REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161048/N01048 AND IAW SRM 53-20-00 FIG 2 VOL 1.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,123 hrs · 24,867 cycles

RT WING L/E FOUND 1 CRACK 5" LONG ON INTERNAL DOUBLER AT STA XORS 562. INSTALLED DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F166195/N00195 AND IAW SRM 57-10-00 FIG 71 VOL 1.

Part: DOOR — WORN (NR 2 NACELLE) · airframe 55,123 hrs · 24,867 cycles

NR 2 NACELLE DOORS DEEP WEAR ON FRAME LOWER RT SIDE AFT INLET DUCT STA 2200. TRIMED OUT DAMAGED TO FRAME FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 54- 00-01 FIG 11 AND 54-10-00 FIG 14 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER F166598/N00598 AND SRM 54-10-00 FIG 14 VOL 1.

Part: SEAT TRACK — CORRODED (BS 1721-1741) · airframe 55,123 hrs · 24,867 cycles

MAIN DECK LOADING SYSTEM AND SEAT TRACKS WERE BROKEN AND SEVERE EXFOLIATION. CORROSION ON SEAT TRACK FROM STA 1721 TO STA 1741 AT X-107. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION IAW SRM 53-70-00 FIG 1 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F166721/N00721 AND IAW SRM 53-70-00 FIG 1 VOL 1.

Part: REPAIR — NONE (HORIZ STAB) · airframe 55,123 hrs · 24,867 cycles

FOUND LEFT HORIZONTAL STAB INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.

Part: REPAIR — NONE (HORIA STAB) · airframe 55,123 hrs · 24,867 cycles

LT HORIZONTAL STAB FRONT SPAR UPPER SIDE DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-20-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 55,123 hrs · 24,867 cycles

LT HORIZONTAL STAB INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (HORIZONTAL STAB) · airframe 55,123 hrs · 24,867 cycles

LEFT HORIZONTAL STABILIZER DETACHABLE ELEVATOR LOWER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (ELEVATOR) · airframe 55,123 hrs · 24,867 cycles

RIGHT HORIZONTAL STABILIZER INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: SKIN — UNKNOWN (TE FLAP) · airframe 55,123 hrs · 24,867 cycles

LEFT WING OUTBOARD FLAP UPPER SKIN AT STA XOF 563 TO STA XOF 569 FOUND TWO EXTERNAL DOUBLERS. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (ELEVATOR) · airframe 55,123 hrs · 24,867 cycles

RIGHT HORIZONTAL STABILIZER INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: BULKHEAD — CRACKED (BS 575) · airframe 55,123 hrs · 24,867 cycles

AIR CONDITIONING COMPT LT FOUND CRACK 2 INCHES LONG ON VERTICAL BULKHEAD AT STA 575 X24 LT SIDE. TRIMMED OUT CRACK AND PERFORMED REPAIR IAW SRM 53-30-00 FIG 6 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F166291/N00291 AND IAW SRM 53-30-00 FIG 6 VOL 1.

Part: REPAIR — UNKNOWN (AILERON) · airframe 55,123 hrs · 24,867 cycles

LEFT WING INBOARD AILERON AT XIA 306 LOWER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 5 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: BULKHEAD — WORN (BS 575) · airframe 55,123 hrs · 24,867 cycles

AIR CONDITIONING COMPT LT FOUND DEEP WEAR ON VERTICAL BULKHEAD STIFFENER AT STA 575 X 24 LT SIDE. BLENDED OUT WEAR IAW SRM 51-21-01 PART 34 VOL 2. MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1B VOL 1 AND SRM 53-12-01 FIG 15 ITEM 9 VOL 3. PERFORMED REPAIR IAW SRM 53-00-01 FIG 9 SHT 8 VOL 1.

Part: REPAIR — UNKNOWN (WING) · airframe 55,123 hrs · 24,867 cycles

LT WING OUTBOARD FLAP LOWER SKIN AT STA XOF 467 FOUND DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 7 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (WING) · airframe 55,123 hrs · 24,867 cycles

LT WING OUTBOARD FLAP LOWER SKIN AT STA XOF 458 TO XOF 462 FOUND DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT WING INBOARD FLAP UPPER SKIN AT STA XIFH 293 FOUND REPAIR DOUBLER. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (WING) · airframe 55,123 hrs · 24,867 cycles

LT WING NR 1 SLAT AT STA XORS 97 OUTER SKIN HAS FLUSH REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 43 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN AT STA 1681 AND 1700 X 19 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN AT STA 939 X 19 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

MAIN CABIN AT STA 1199 AND 1299 X-55 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (LT WING) · airframe 55,123 hrs · 24,867 cycles

LT WING DROOPED L/E AT STA XORS 299 UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 55 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 55,123 hrs · 24,867 cycles

INTERNAL FUSELAGE AT STA 1154 X-72 FWD PRESSURE BULKHEAD PANEL REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 1227) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR AT STA 1227 BETWEEN LONG 40 AND 41 RT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — NONE (BS 2007-2018) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR FROM STA 2007 TO STA 2018 BETWEEN LONG 41 AND 48 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 1801-1821) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR ON FUSELAGE FROM STA 1801 TO STA 1821 BETWEEN LONG 36 AND 39 RT SIDE. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 680-690) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR FROM STA 680 TO STA 690 AT LONG 28 LT Z-30 UPPER CARGO DOOR JAMB LWR SILL. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 1511-1520) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR FROM STA 1511 TO STA 1520 BETWEEN LONG 52 AND 51 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 579-590) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL DOUBLER REPAIR AT FUSELAGE FROM STA 579 TO STA 590 BETWEEN LONG 44 AND 46 LT. PERFORMED AN INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 635-675) · airframe 55,123 hrs · 24,867 cycles

EXTERNAL FUSELAGE DOUBLER REPAIR FROM STA 635 TO STA 675 LONG 28 LT Z-30. PERFORMED AN INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: VALVE — MALFUNCTIONED (MLG DOWNLOCK) · airframe 55,049 hrs · 24,835 cycles

AFTER TAKEOFF DURING GEAR RETRACTION, RT MLG RED LIGHT FRONT AND REAR PANEL REMAINED ILLUMINATED. QRH COMPLIED W/ RECYCLED GEAR AT 180 KNOTS. LIGHTS REMAINED ILLUMINATED AND EVENTUALLY EXTINGUISHED IN APPROX 5 MINUTES. CHECKED PROX SENSORS AND WIRING, ALL LOOK OK. PERFORMED BITE TEST ON PROX ELECTRONIC UNIT NO FAULTS. CHECKED SENSOR GAP PER M/M 32-34-03-02, ALL WITHIN LIMITS. INSTALLED GEAR PINS, REMOVED TARGET SENSOR FROM RLG DOWN LOCK, SIMULATED FLIGHT CONDITIONS WITH GEAR UP. PER TAFI 32-30-00 CODE "AL" PRESSURIZED HYDRAULIC SYSTEM AND CHECKED ALL COMPONENTS FOR BYPASSING OR INTERNAL LEAKAGE. ALL CHECK OK. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR RESTRICTOR VALVE PER MM 32

Part: UPLOCK SENSOR — OUT OF ADJUST (RT MLG) · airframe 54,824 hrs · 24,721 cycles

RETRACTED GEAR AFTER T/O, RT MLG INDICATED UNSAFE UP BOTH PANELS. COMPLIED WITH QRH. FOLLOWING SECOND RETRACT, RED LIGHT EXTINGUISHED AFTER SEVERAL MINUTES, A/S 205KTS. BITE CHECKED PROX SENSOR BOX, CHECK GOOD. INSP RT MLG UPLOCK SENSOR, SENSOR WIRING, AND TARGET. WIRING LOOKED OK AND TERMINAL ENDS CLEAN. FOUND TARGET AND SENSOR AIR GAP NOT PARALLEL. ADJUSTED SENSOR SHIMS SO THAT AIR GAP WAS PARALLEL TO TARGET AND TO OBTAIN PROPER CLEARANCE PER AMM 32-34-03-2 1.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (MLG) · airframe 53,599 hrs · 24,086 cycles

AFTER RAISING THE GEAR HANDLE DURING TAKEOFF, THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FOR ABOUT ONE MINUTE, THEN WENT OUT. FACT, R/R RIGHT HAND MLG DOWN LOCK PROXIMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (MLG) · airframe 53,598 hrs · 24,085 cycles

TPA CLOSER AFTER RAISING THE GEAR HANDLE DURING TAKEOFF,THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FOR ABOUT ONE MINUTE, THEN WENT OUT. ENT BY: 004631 RPT BY: 096848 FACT 03SEP04 19:27 TPA R R & R RT MLG DOWN LOCK PROXIMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE.

Part: SKIN — CORRODED (LT AILERON) · airframe 53,226 hrs · 23,915 cycles

LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,226 hrs · 23,915 cycles

FORWARD PIT AT APPROX FS 980 AT LONGERON 52 FRAME HAS CORROSION. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC10 SRM 53-00-01 FIG 8 VOL 1 AND 52-21-01 VOL 2 AND 51-33-01 VOL 2.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 53,226 hrs · 23,915 cycles

CORROSION AT FORWARD LOWER CARGO ROLLER TRAY AT RBL 28, FS 889 ON TOP PLATE, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION, FABRICATED T-SUPPORT, DOUBLERS AND INSTALLED IAW DC10 SRM 51-31-01 VOL 2.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,226 hrs · 23,915 cycles

FORWARD CARGO DOOR CUTOUT, FORWARD LOWER CORNER WEB IS CORRODED FS 895, RBL 52. REMOVED DAMAGED FRAME AREA IAW DC10 SRM 53-50-00 VOL 1. FABRICATED SPLICE PLATE AND INSTALLED REPAIR DOUBLERS AND SPLICE PLATE IAW DC10 SRM 53-50-00 VOL 2.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,226 hrs · 23,915 cycles

CORROSION ON NUT PLATE CHANNEL AT FORWARD LOWER CARGO UNDERFLOOR BETWEEN FS 859 AND 879 AT RBL 28. CORROSION FOUND TO BE INTERGRANULAR AND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW DC10 SRM 53-00-01 VOL 1.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · airframe 53,226 hrs · 23,915 cycles

LOWER FORWARD CARGO COMPARTMENT, CORROSION ON BOTTOM SIDE OF ROLLER TRAY AT FS 875 AT LBL 28. CORROSION FOUND TO BE INTERGRANULAR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW DC10 SRM 53-42-01 VOL 3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 53,226 hrs · 23,915 cycles

FORWARD CARGO DOOR SILL FITTING CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND 51-31-01 VOL 2.

Part: SKIN — CORRODED (LT AILERON) · airframe 53,226 hrs · 23,915 cycles

LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

MAIN CARGO AREA STATION 925 SEAT TRACK AT LBL 47 EDGE IS CRACKED. CUT OUT DAMAGE SECTION OF TRACK, FABRICATED SEAT TRACK, SPLICE PLATE AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-31-01 VOL 2.

Part: STATIC PORT — OUT OF ADJUST (PITOT/STATIC SYS) · airframe 53,225 hrs · 23,915 cycles

RIGHT HAND ALTERNATE STATIC PORT FAILS HIGH/LOW MISMATCH CHECK AT AFT SIDE OF PORT. SKIN HAS .005 INCH DIFFERENCE IN HEIGHT (.002 INCH MAX ALLOWED). ADJUSTED RIGHT HAND STATIC PORT IAW DC10 MM 34-11-01-2, PARAGRAPH B (4). ALL TOLERANCES ARE WITHIN SPECIFIED LIMITS WITH TOP .001, BOTTON .003, FORE .001 AND AFT AT .001 IAW DC10 MM 34-11-01-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

FORWARD CARGO DOOR SILL FITTING IS CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. TRIMMED OUT DAMAGE FLANGE IAW DC10 SRM 53-50-00 FIG 11. FABRICATED REPAIR ANGLE IAW DC10 SRM 53-50-00 FIG 11 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2 AND 53-50-00 FIG 11 VOL 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

FORWARD PIT APPROX STATION 980 LONGERON 52 FRAME HAS CORROSION. REMOVE CORROSION IAW DC10 SRM 51-21-01 VOL 2, ORIGINAL THICKNESS .071 IAW DC10 SRM 53-13-01 FIG 8 VOL 3. MATERIAL REMOVED .032 INCH, MATERIAL REMAINING .039 INCH. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW DC10 SRM 53-00-01, VOL 1, FIG 8 AND DC10 SRM 51-33-01 VOL 2.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

FORWARD CARGO PIT AT DOOR CUTOUT STATION 1002 CHORD FOUND CORRODED INSIDE TORQUE BOX. REMOVED CORROSION IAW DC10 SRM 53-00-01 VOL 2, FOUND TO BE OUT OF LIMITS, FABRICATED ANGLE IAW DC10 SRM 51-21-01 VOL 1 AND 53-50-00 VOL 2. INSTALLED TWO STRAPS AND INTERCOSTALS AND BRACKETS REMOVED TO FACILITATE, INSTALLED SR 10530048-17 AND -7 PARTS IAW DC10 53-50-00 VOL 1.

Part: FLAP TRACK — WORN (T/E FLAP) · airframe 53,225 hrs · 23,915 cycles

LEFT HAND INBOARD FLAP TRACK HAS SIGNS OF WEAR (6 PLACES), MARKED. CHECKED LIMITS ON LEFT HAND INBOARD FLAP TRACK NUMBER 2 IAW DC10-10 F/E MM 27-50-03-2, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW DC10-10 MM 27-50-03-2 STEP 4B (2) (A).

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

FORWARD CARGO DOOR CUTOUT, AFT LOWER CORNER, WEB CORRODED, APPROX FS 1002, RBL 52. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW FRAME SECTION AND REPAIR DOUBLERS AND ANGLE SPLICES IAW DC10 SRM 53-13-01 VOL 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

RIGHT HAND ALTERNATE STATIC PORT FAILS WAVINESS INSPECTION AT POSITIONS 4, 4A AND 4W. REMOVED ALTERNATE STATIC PORT AND AVIONICS PRESSURE SWITCH FLEX HOSE IAW DC10 MM 34-11-01-2 AND DC10 MM 33-11-00. REWORKED SKIN AROUND STATIC PORT IAW DC10 SRM 53-20-00 VOL 1. REINSTALLED ALTERNATE STATIC PORT AND AVIONICS FLEX HOSE IAW DC10 MM 34-11-01-2, PERFORMED LEAK CHECK OF ALTERNATE STATIC SYSTEM IAW DC10 MM 34-11-00, NO LEAKS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

T-CAP CORRODED IN FORWARD PIT AT STATION 909 RBL 30. REMOVED AND REPLACED T-CAP IAW DC10 SRM 51-31-01 VOL 2.

Part: RIB — CRACKED (NR 2 NACELLE) · airframe 53,225 hrs · 23,915 cycles

NUMBER 2 ENGINE INLET STRUCTURE RIB CRACKED AT SPLICE AT 1 O’CLOCK POSITION, ACCESS THROUGH PANEL 362JR. REMOVED SPLICE, INTERCOSTAL AND STIFFENER SECTION IAW DC10 SRM 51-35-01 VOL 2, FORMED STIFFENER AND SPLICE IAW DC10 SRM 51-10-00 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 54-10-00 VOL 1 AND 54-35-01 AND 54-33-01 VOL 2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

CENTER ACCESSORY COMPARTMENT UPPER RIGHT HAND CUSP WEB HAS CRACKS AROUND LIGHTING HOLES BETWEEN FS 1139 AND FS 1156. FABRICATED REPAIR DOUBLER AND INSTALLED WEB REPAIR AND DOUBLERS IAW DC10 SRM 51-35-01 VOL 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

MAIN CARGO APPROX STATION 910 SEAT TRACK AT RBL 27 IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, LOCATED AND DRILLED REPAIR SECTION AND INSTALLED SEAT TRACK REPAIR IAW DC10-10 SRM 53-70-00 VOL 1 AND DC10-10 SRM 51-31-01 VOL 2.

Part: SEAT TRACK — INCORRECT (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

SEAT TRACK ON WL 27R BETWEEN 615-670 MAIN UPPER CARGO HAS A BIG GAP TWO PLACES. REMOVED SEAT TRACK SECTION AND INSTALLED NEW TRACK SECTION IAW DC10 SRM 51-31-01 VOL 2 AND DC10 SRM 51-21-01 VOL 2.

Part: STRAP — OUT OF LIMITS (T/E FLAP) · airframe 53,225 hrs · 23,915 cycles

LEFT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD STRAP P/N ARC 2517-1 IS OUT OF LIMITS IAW DC10 CMM 57-52-01. REMOVED OUT OF LIMITS STRAP, LOCATED AND DRILLED HOLES IN NEW STRAP IAW DAC DWG ARC 2512. LOCATED BUSHING HOLE IAW DAC DWG ARC 2512 AND EA 8-5710-77549. INSTALLED NEW STRAP IAW DAC DWG ARC 2512 AND DC10-10 MM 20-50-02-2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,225 hrs · 23,915 cycles

MAIN CARGO AREA FS 925 SEAT TRACK RBL 47 EDGE IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, FABRICATED REPAIR PARTS, AND SLICE PLATES IAW DC10 SRM 53-70-00 VOL 1 AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2.

Part: MOTOR — RUPTURED (RUDDER) · airframe 49,986 hrs · 22,620 cycles

RUDDER MOTOR PUMP RUPTURED AND LEAKING EXCESSIVELY. R&R LWR RUDDER NON REVERSIBLE MOTOR PUMP PER MM 27-26-01-2.

Part: ANGLE — CRACKED (RT HORIZ STAB)

THE RT HORIZ STAB CENTER L/E SECTION O/B RIB UPPER CHORD ANGLE IS CRACKED IN 3 PLACES ON IN FLANGE BETWEEN RADIUS AND FASTENERS HOLES. REMOVED AND REPLACED UPPER CHORD ANGLE PER SRM 55-00-01.

Part: SPAR WEB — CRACKED (NR 1 PYLON)

THE NR 1 PYLON CENTER SPAR WEB WAS FOUND CRACKED. CRACK EMANATED FROM LAST LIGHTENING HOLE DIAGONALLY TO THE I/B AFT CORNER ATTACH BOLT HOLE, CRACK TERMINATES AT EXISTING FASTENER HOLE. FABRICATED AND INSTALLED REPAIR PER SRM 54-00-01 PAGE 11.