N315UP

Part: SKIN — DAMAGED (RUDDER) · airframe 71,131 hrs · 24,134 cycles

EVIDENCE OF LIGHTNING STRIKE ON RUDDER R/H SIDE TRAILING EDGE AT APPROXIMATELY RUDDER STATION 255. PERMANENT REPAIR COMPLIED WITH PER EO-93077-REQ3. DEFERRAL REMOVED.

Part: DOOR — LEAKING (ZONE 800) · airframe 70,256 hrs · 23,747 cycles

AIR LEAK COMING FROM L2 LOWER LEFT HAND CORNER AT 390 FT CABIN ALT 6800 DIFF 8.4 ACCOMPLISHED PNEUMATIC LEAK TEST IAW MM 21-31-00-705-009. BROUGHT CABIN DIFFERENTIAL TO 4, NO LEAKS KNOTED.

Part: FMC — INOPERATIVE (FIRST OFFICER'S) · airframe 68,796 hrs · 23,180 cycles

**DIVERSION** BOTH FMC€™S -> PUSHING NUMEROUS FUNCTION BUTTONS PULLS UP WRONG PAGE. REMOVED AND REPLACED F/O FMC IAW AMM 34-61-02. OPS CHECK GOOD.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 68,150 hrs · 22,915 cycles

FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432-1520, LBL 55 - LBL 77.5, P/N: 146T5869-43 (REPAIR) IAW AMM 53-01-06-400-801 REV.141 INSTALL MAIN DECK CARGO FLOOR PANEL. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV 141 RESTORED MAIN DECK CARGO HANDLING

Part: FLOOR PANEL — CRACKED (BS 1432-1520) · airframe 68,150 hrs · 22,915 cycles

MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432 ~ 1520, LBL55~ LBL77.5, P/N:146T5869-89 (REPLACE) REMOVE MAIN DECK CARGO FLOOR PANEL AREA SEALANT I.A.W AMM 53-01-06-000-801 REV 141 AND CONDITION CHECK NORMAL. ACCOMPLISHED ACCESS FLOOR PANEL OK TO INSTALL CHECK, PANEL NO:251XFF.

Part: TRIM PANEL — BROKEN (MAIN DOOR) · airframe 68,150 hrs · 22,915 cycles

FAULT - FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN (REPLACE)

Part: HINGE — DEFORMED (LEVER COVER) · airframe 68,150 hrs · 22,915 cycles

FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE)

Part: HINGE — DEFORMED (DOOR ARM LEVER) · airframe 68,175 hrs · 22,924 cycles

FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. REPLACED HINGE ASSY I.A.W AMM 20-11-00-910-802 REV.141.

Part: SPLINE — BROKEN (MAIN DOOR) · airframe 68,175 hrs · 22,924 cycles

FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED DOORWAY SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141.

Part: LIGHT — INOPERATIVE · airframe 66,788 hrs · 22,363 cycles

*SDR FILED OPEN* EXTERNAL FUSELAGE EMERGENCY LIGHT BULB INOP RELAMPED EXTERNAL EMERGENCY LIGHT REF AMM 33-51-16. OPS CK OK.

Part: DOOR — OUT OF ADJUST (FWD CARGO) · airframe 66,032 hrs · 22,061 cycles

INSPECTION TYPE:NA**ATB** DURING CLIMB OUT EICAS MSG "FWD CARGO DOOR" AIR TURN BACK. DEFERRED FWD LWR CARGO DOOR IND PER MEL 52-71-1-1. C/W DMP 52-71-1-1 FWD LWR CARGO DOOR VISUALLY VERIFIED CLOSED AND LOCKEDPERFORMED PSEU BITE IAW FIM 32-09-00/101 FIG 103. FOUND S893 PREVIOUS FAULT. PERFORMED ADJUSTMENT CHECK IAW AMM 52-33-00/501, ADJUSTMENT GOOD. RESET PSEU, NO FAULT CANNOT DUPLICATE. DEFERRAL CLEARED. NO DMP, PLACARD REMOVED

Part: NONE — NONE (R/H VST TORQUE) · airframe 64,012 hrs · 21,246 cycles

INSPECTION TYPE:C13DISBOND DAMAGE ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDE.REPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.82.01 AND 767-300F SRM 51-70-10-2R REPAIR GENERAL REV.82.01.

Part: NONE — NONE (R/H VST TORQUE) · airframe 64,012 hrs · 21,246 cycles

INSPECTION TYPE:C13DISBOND DAMAGE (APPROX 7.0'' X 6'') ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDEREPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.82.01 AND 767-300F SRM 51-70-10-2R REPAIR GENERAL REV.82.01

Part: NONE — NONE (M/D FLOOR PNL) · airframe 64,012 hrs · 21,246 cycles

INSPECTION TYPE:C13DAMAGE ON M/D CARGO FLOOR PNL AT STA 287-STA412 , RBL 77 - RBL 88.FABRICATE THE REPLACEMENT FLOOR PNL PER EO NO. B767-5320-9693-I

Part: ATTACH ANGLE — CORRODED (BS 212-237) · airframe 60,916 hrs · 20,105 cycles

INSPECTION TYPE: LDS CORROSION FOUND ON SUPPORT ANGLE AT FS 212-237, LBL 64.0 (FLIGHT DECK FLOOR). SUPPORT ANGLE AT FS 212-237, LBL 64.0 (FLIGHT DECK FLOOR) REPLACED WITH MADE REPAIR PART, IAW CASCADE AEROSPACE EO NR 13871 AND UPS EO NR B767-77863-A REV DATE 09/17/2020. THIS REPAIR IS CONSIDERED MINOR.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 60,018 hrs · 19,821 cycles

INSPECTION TYPE:N/AWHEN SWITCH IS CLOSED FOR NORMAL POSITION OF FLIGHT THE SWITCH FUNCTION GOES TO "OFF" AND THE "DISARMED" LIGHT ILLUMINATES.REMOVED AND REPLACED THE EMERGENCY LIGHTS CONTROL PANEL IAW AMM 33-51-08 OPS CHECK GOOD AT THIS TIME ESR: IPC 33-51-08.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2005-8) ON STA 785.9 , RBL 11REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B767-5740-58151-B , BOEING SRID : 3-4620819146 AND UPS EO B767-5710-75257-A

Part: STIFFENER — CRACKED (BS 785) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.AW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B77-5740-58151-B , BOEING SRID : 3-4620819146 AND UPS EO B767-5710-75257-A

Part: STIFFENER — CRACKED (STA 785.9) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-12) ON STA 785.9 , RBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 UPS EO B767-5740-58151-B , BOEING SRID : 3-4620819146 AND UPS EO B767-5710-75257-A

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON #10 SLAT L/E SKIN (P/N : 114T4103-4) NEAR OSS 724REPAIR I.A.W 767-300F SRM 57-43-01-2R-1 REV.76.01

Part: STIFFENER — CRACKED (BS 785) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-6) ON STA 785.9 , RBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B767-5740-58151-B , BOEING SRID : 3-4620819146 AND UPS EO B767-5710-75257-A

Part: STIFFENER — CRACKED (BS 785.9) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-5) ON STA 785.9 , LBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B767-5740-58151-B , BOEING SRID : 3-4620819146 AND UPS EO B767-5710-75257-A

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 59,514 hrs · 19,622 cycles

INSPECTION TYPE:C12CRACK ON #2 PYLON INBD SKIN ASSY (P/N : 311T2450-23) NEAR NAC 240.50REPAIR I.A.W BOEING SRID : 3-4623448622 AND UPS EO B767-5430-75336-A

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 58,834 hrs · 19,383 cycles

WHEN EXTERNAL POWER TURNED OFF IN COCKPIT EMERGENCY EXIT SIGNS & LIGHTS CAME ON WITH EMERGENCY LIGHT SWITCH TURNED OFF. R&R EMERGENCY EXIT OVERHEAD PANEL ON P11 REF MM 33 51 08 EMERGENCY EXIT LIGHTS OPS CKS OK 33 51 08 01A OOS

Part: CONTROL PANEL — DEFECTIVE (EMERGENCY LIGHT) · airframe 58,630 hrs · 19,302 cycles

INSPECTION TYPE:N/A EMER LITE CONTROL PANEL DISARMED LIGHT WILL NOT SNAP INTO LOCKED POSITIONREF MM 33 51 08. INSTALLED SERVICES ABLE PANEL ASSY OPS CHECK GOOD SN ON 000050 EFF 31 12 11 51 A.

Part: TIRE — BLOWN (MLG) · airframe 58,182 hrs · 19,142 cycles

INSPECTION TYPE:N/A EMERGENCY DECLARED - #3 MAIN TIRE BLOWN ON TAKE OFF. REMOVED #3 MAIN TIRE INSPECTED AXLE AND #3 BRAKE ASSY NO DEFECTS NOTED INSTALLED (3) REPLACED #3 MAIN TIRE ASSY SPACER AND WASHER VEREFIED INSTALLED REF MM CH 32-45-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 55,658 hrs · 18,244 cycles

RIGHT FORWARD WINDOW CRACKED. REPLACED RT 1 WINDOW IAW AMM 56-11-01-404-017 REV 124.01. EFF REF IPC: 56-11-01-01A ITEM 015K REV 94.00.

Part: PANEL — DAMAGED (DOOR) · airframe 55,250 hrs · 18,083 cycles

CREW ENTRY DOOR HANDLE PANEL DAMAGE. REMOVED AND REPLACED L1 EXTERIOR DOOR HANDLE PANEL MM 52-11-26-004-001, AND 52-12-25-00.

Part: TEE FITTING — CRACKED (NLG WW BLKHD) · airframe 54,931 hrs · 17,970 cycles

INSPECTION TYPE: C11, CRACK FOUND ON THE NOSE W/W AFT BULKHEAD VERTICAL TEE, BS 287 , RBL 25 , WL 173. REPAIRED IAW EO B767-5310-20118-F, AND SRM 51-70-12, FIGURE 1 , REV 70.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 54,931 hrs · 17,970 cycles

INSPECTION TYPE: C11, DAMAGE ON THE MAIN DECK CARGO FLOOR PANEL, BS 972 - 1112. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,115 hrs · 17,632 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51-07. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 53,973 hrs · 17,566 cycles

INSPECTION TYPE: MAIN CARGO SMOKE DETECTOR 1 EICAS MESSAGE. TROUBLESHOT IAW FIM 26-14-00, FOUND TAIM INOPERATIVE. R & R THE TAIM IAW AMM 26-14-00/401, AND OPS TESTED GOOD IAW AMM 26-14-00.

Part: PRESSURE SWITCH — INOPERATIVE (RT ENGINE) · airframe 52,884 hrs · 17,204 cycles

RIGHT ENGINE OIL FILTER STATUS LIGHT ILLUMINATED IN FLIGHT, LEFT/RIGHT OIL PRESS WAS 65, LEFT/RIGHT OIL TEMP WAS 87, LEFT/RIGHT OIL QUANTITY WAS 16T/S PER FIM79-35-00-815-803-H00 BLOCK 1 & 21, CHKD SCAVENGE FILTER AND MASTER CHIP DETECT NO METAL FOUND, REPLACED FILTER AND OIL FILTER DIFF PRESS SW, ENG RUN CHECK OK.

Part: BLOCKER DOOR — CRACKED (THRUST REVERSER) · airframe 52,580 hrs · 17,111 cycles

NR 1 ENGINE INBOARD RT THRUST REVERSER BLOCKER DOOR AT 8:00 OCLOCK POSITION HAS MULTIPLE CRACKS. REMOVED & REPLACED THE BLOCKER DOOR IAW AMM 28-31-14, OPS CHECKED GOOD.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,973 hrs · 16,531 cycles

OVERHEAD EMERGENCY LIGHT CONTROL PANEL NOT ARMED, LIGHT INOPERATIVE. TRIED TO RELAMP BUT LIGHT CARRIER CAME APART. NO SPARE LIGHT ASSY IN NRT. REPLACED EMERGENCY LIGHT CONTRL PANEL IAW AMM 33-51-08-401, OPS CHK OK. IPC REF 31-21-11-51A, ITEM 15.

Part: STRUT — INOPERATIVE (RAFT DOOR) · airframe 50,786 hrs · 16,467 cycles

LIFE RAFT ACCESS DOOR DOES NOT STAY OPEN. R & R GAS STRUT IAW MM 20-11-00-910. IPC REF 25-62-55-01, ITEM 480.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 50,370 hrs · 16,320 cycles

MAIN CARGO FLOOR PANEL DAMAGED AT BS 412, FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

Part: STRINGER — CRACKED (BS 1550) · airframe 50,322 hrs · 16,307 cycles

INSPECTION TYPE:C10, CRACK, 3" WAS FOUND ON THE STRINGER 20R AT BS 1550. REPAIR IAW SR: PN 4-3138709764 WITH FAA APPROVED 8100-9 FORM DATE: 16FEB2016 AND EO: B767-5310-59824-A.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 49,903 hrs · 16,147 cycles

MCD FLOOR PANEL DAMAGED, POSITION NR 11 CENTER. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: SPRING — WORN (CREW DOOR) · airframe 49,823 hrs · 16,105 cycles

CREW DOOR EXTERNAL DOOR HANDLE ASSY IS WORN IN 2 PLACES. R & R PAWL, SPRING AND PIN. OPS CHECKED NORMAL IAW MM 52-12-215. ACFT OK FOR SERVICE.

Part: LINE — RUPTURED (FUEL SYSTEM) · airframe 49,713 hrs · 16,064 cycles

DURING CLIMB, LEFT ENGINE FAILED. AIR RETURN. R & R RUPTURED FUEL LINE.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL BS 280-412 RT SIDE DAMAGED AT AFT END. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND CRACK DAMAGE ON CARGO FLOOR PANEL 231CFF AT BS 412 TO 529, LBL 33 TO 54.75. FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 46,083 hrs · 14,638 cycles

INSPECTION C09, THREE DENTS ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV 58.0, SRM 51-70-10-2R-2 REPAIR 2, FIG 203, REV 58.00.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND CRACK DAMAGE ON CARGO FLOOR PANEL 232GFF AT BS 529 TO 654 +22, RBL 33 TO 54.75. FABRICATED REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND CRACK DAMAGE ON M/D CARGO FLOOR PANEL 231JFF AT BS 529 TO 654+ 22, LBL 54.75 TO 77.5. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND CRACK DAMAGE ON CARGO FLOOR PANEL 231FFF AT BS 529 TO 654+ 22, LBL 11 TO RBL 11. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: CARGO TRACK — WORN (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND WORN OUT ON THE STUD HOLE OF SEAT TRACK AT BS 879, LBL 11. REPAIRED IAW SRM 53-00-52, REPAIR 8, REV 58.00.

Part: CARGO TRACK — WORN (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND WORN OUT ON THE STUD HOLE OF CARGO TRACK AT STA 879, RBL 33. REPAIRED IAW SRM 53-00-52, REPAIR 8, REV 58.00

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 46,083 hrs · 14,638 cycles

INSPECTION C09, DENT ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP AT AT IFS 142.25. REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 FIG 201, REV 58, & SRM 51-70-10-2R-2, REPAIR 2, FIG 203, REV 58.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 46,083 hrs · 14,638 cycles

INSPECTION C09, DENT ON THE LT WING OTBD FLAP UPPER PANEL INNER SURFACE AT T/E FLAP STA 78.75. REPAIRED IAW -SRM 57-53-01-2R-1 REPAIR 1, FIG 201, REV.58, SRM 51-70-10-2R-2, REPAIR 4, FIGURE 201, REV 58.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,083 hrs · 14,638 cycles

C09 INSPECTION, FOUND CRACK DAMAGE ON CARGO FLOOR PANEL 231BFF AT BS 412 TO 529 , LBL 11 TO 33. FABRICATED REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 46,083 hrs · 14,638 cycles

INSPECTION C09, DENT ON THE T/E COVER PANEL UPPER SKIN OF LT WING INBD MAIN FLAP AT IFS 184.7. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1, FIGURE 201, REV 58.0 0. 2. SRM 51-70-05-0G-0-GENERAL, REV. 58.00.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL NR 5 IS DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD FLOOR PANEL DAMAGED. REMOVED DAMAGE IAW SRM 53-00-50-2R (D,2). DENTS REMOVED. C/W STEP 4-8, SRM 53-00-50-2R. REPAIR INSTALLED. PRECURED REPAIR DOUBLER IAW SRM 53-00-50-2R, PARA 4D, STEPS 9 & 10. CURE C/W OF REPAIR DOUBLER .

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

POS NR 6, AFT RT BL-4 MCD FLOOR PANEL DAMAGED.

Part: FLOORBOARD — DENTED (MAIN CARGO)

TWO DENTS IN FLOORBOARD 5.5 INCHES FROM RT EDGE. 46 INCHES FROM FWD/EDGE. REPAIR FLOORBOARD IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL HAS 2.5 X .5 HOLE THRU TOP SKIN & CORE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: CONTACT — DIRTY (T/E FLAP SYSTEM)

TRAILING EDGE FLAP SYS EICAS MESSAGE T/E FLAP ASYM DISPLAYED. T/E LIGHT ON. NO FLAP MOVEMENT - EMERGENCY DECLARED. REMOVED FSEU AND CLEANED CONTACTS REINSTALLED FSEU AND OPS CHECKED IAW MM27-51-01-404-130.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK, FLOOR PANEL DAMAGED, DEF 475165. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C FWD CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 1"X0.7"X0.02" AT STA 728.5,RBL 16.2 CUT OUT THE UPPER SKIN AND CORE WITH 1" DIAMETER. REPAIR IAW REV:52 B767-300F, SRM 53-00-50. REPAIR GENERAL FIGURE 201, PARA.4.C

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, FOUND CABIN INTERIOR M/D CARGO FLOOR PANEL DENTED AT STA 1197+15, CENTER NR 25542, DENT 0.7" (LENGTH) X 0.6"(WIDTH) X 0.090"(DEPTH). REPAIRED IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, DENT-FWD CABIN INTERIOR M/D CARGO FLOOR PANEL DENTED AT STA 883, RBL 84, NR 28116. DENT 2.8"(LENGTH) X 2.5"(WIDTH) X 0.95"(DEPTH) REPAIRED IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 0.9" X 0.3" X 0.060" AT STA 1001, RBL 33 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION 1.0" DIAMETER. REPAIR IAW REV:52 SRM 53-00-50 REPAIR GENERAL FIGURE 201, PARA 4.C.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 2.5" X 2.5" X 0.030" AT STA 1001, LBL 31 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION LXW=2.7" X 2.5". REPAIR IAW REV: 52, SRM 53-00-50, REPAIR GENERAL FIG 201, PARA 4 D

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 2.0" X 1.0" X 0.040" AT STA 906, LBL 86 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION LXW=1.5"2.1".REPAIR IAW REV:52 SRM 53-00-50, REPAIR GENERAL FIGURE 201, PARA 4D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY LOWER SKIN AND CORE DAMAGE ABOUT 2.0" X 0.4" X 0.010" AT STA 959, LBL 20 CUT OUT THE LOWER SKIN AND CORE WITH DIMENSION LXW=3.1" X 1.0". REPAIR IAW REV:52 SRM 53-00-50, REPAIR GENERAL FIG 201 PARA 4D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, DENT-FOUND CABIN INTERIOR M/D CARGO FLOOR PANEL DENTED AT STA 1197, LBL 80, NR 28154. DENT 9.2" (LENGTH) X 0.6"(WIDTH) X 0.095"(DEPTH). REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 1.0" X0.5" X 0.200" AT STA 1001,RBL 33 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION LXW=1.7" X 2.0". REPAIR IAW REV:52 SRM 53-00-50, REPAIR GENERAL FIG 201 PARA 4 D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, CARGO COMPARTMENT FLOOR PANEL ASSEMBLY UPPER SKIN AND CORE DAMAGE ABOUT 9"X0.6"0.01" AT STA 1197+89 LBL 4.7 AND RBL 4.7 CUT OUT THE UPPER SKIN AND CORE LXW=1.6"X9.4". REPAIR IAW REV:52 SRM 53-00-50. REPAIR GENERAL FIG 201, PARA 4.D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 0.5" X 1.0" X 0.1" AT STA 1518, RBL 66 CUT OUT THE UPPER SKIN AND CORE WITH 1.1" DIAMETER AT STA 1518, RBL 66. REPAIR IAW REV:52 SRM 53-00-50, REPAIR GENERAL FIGURE 201, PARA 4.D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 1.0" X 0.7" X 0.020" AT STA 371, RBL 50 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION 1.2" DIAMETER. REPAIR IAW REV:52 SRM 53-00-50, REPAIR GENERAL FIGURE 201, PARA 4D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 1R HAS 3 HOLES LESS THAN 3 IN DIA 3 EA HOLES DIMENSION 0.8" X 1.3",0.9" X 1.2", 1.0" X 1.5", STA 355-STA365, RBL 82-RBL 89. REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 0.5" X 2.5"X 0.152" AT STA 1509, LBL 2 AND 2.5"X2.1"X0.058" AT STA 1509 LBL 1 CUT OUT THE UPPER SKIN AND CORE DIMENSION LXW=3.5"X3". REPAIR IAW REV:52 SRM 53-00-50. REPAIR GENERAL FIG 201,PARA.4.D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 0.5" X 0.5"X 0.1" AT STA 1387, RBL 84 AND 0.4" X 0.4" X 0.1" AT STA 1389 RBL 84 CUT OUT THE UPPER SKIN AND CORE WITH 0.5" DIAMETER AT STA 1387, RBL 84 AND 0.4" DIAMETER AT STA 1389, RBL 84. REPAIR IAW REV:52 SRM 53-00 -50 REPAIR GENERAL FIGURE 201 PARA 4.C.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 3L FWD OTBD PANEL HAS 1 HOLE LESS THAN 3 IN DIA, 1EA HOLE DIMENSION 0.75" X 0.5", STA 654+9, LBL 80. REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 2C HAS 1 HOLE LESS THAN 3 IN DIA, 1EA HOLE: DIMENSION 0.75"X0.87", STA 490,RBL 6. REPAIR IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 1R HAS 1 HOLE LESS THAN 3 IN DIA, 1 EA HOLE DIMENSION 1.8" X 2.3", STA 366, RBL 69. REPAIR IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 0.4" X 0.4"X 0.0625" AT STA 1368,RBL 1 AND 1.9"X1.4"X0.06" AT STA 1375 RBL 4 CUT OUT THE UPPER SKIN AND CORE WITH 0.5" DIAMETER AT STA 1368,RBL 1 AND 2" DIAMETER AT STA 1375,RBL 4. REPAIR IAW REV:52 SRM 53-00-50 REPAIR GENERAL FIGURE 201 PARA.4.C. AND 4.D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 2L HAS 1 HOLE LESS THAN 3 IN DIA, 1EA HOLE DIMENSION 1.4" X 0.9", STA 492, LBL 80. REPAIR IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMAGE ABOUT 1.0" X 0.3"X 0.114" AND 3" X 3.2"X0.1" AT STA 644, RBL 83 CUT OUT THE UPPER SKIN AND CORE WITH DIMENSION LXW=4.1"X3.5". REPAIR IAW REV:52, SRM 53-00-50. REPAIR GENERAL FIGURE 201 PARA.4D.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 7R HAS 1 HOLE LESS THAN 3 IN DIA, 1EA HOLE: DIMENSION 0.5"X0.4", STA 1007, RBL 82.0. REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT POSITION 3L FWD 3RD PANEL FROM OUTBD HAS 1 HOLE LESS THAN 3 IN DIA, 1EA HOLE DIMENSION 0.75"X 0.5", STA 654+8", LBL 49.2". REPAIR IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 42,251 hrs · 13,139 cycles

INSPECTION TYPE:C, MAIN DECK CARGO COMPARTMENT FLOOR PANEL ASSY UPPER SKIN AND CORE DAMGE ABOUT 0.4"X0.4"X0.0975" AT STA 1509, RBL6.5 CUT OUT THE UPPER SKIN AND CORE WITH 0.5" DIAMETER. REPAIR IAW REV:52, SRM 53-00-50, REPAIR GENERAL FIGURE 201,PARA.4.C.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

HOLE IN MAIN DECK FLOOR PANEL. REPAIRED IAW SRM 53-00-2R.

Part: DISPLAY — FAILED (COCKPIT)

ATB - ON CLIMB OUT LOST CAPT'S EHSI SCREEN, ALT SELECTED STILL NO SCREEN. APPROX 2 MINUTES LATER CAPT LOST EADI THEN UPPER EICAS SCREEN. AFTER 30 SECONDS, BOTH CAPT AND F/O SMELLED ELECTRICAL BURNING. FOUND SLIGHT WATER CONDENSATION ON CAPTS EHSI. R & R SAME IND IAW AMM 34-22-04-4. OPS CK OK. ALSO, OPS CHECKED EICAS DISPLAYS IAW AMM 31-41-01-4.

Part: ELEMENT — SHORTED (RT ENGINE)

INSPECTION TYPE:ETOP, ATB- ON CLIMB OUT THROUGH FLIGHT LEVEL 14,000, RT ENGINE DUCT LEAK. THEN RECEIVED FWD EQUIPMENT OVERHEAT MSG. CHECKLIST ACCOMPLISHED. T/S IAW FIM 26-18-00, F104 STEP 1 TO 34. FOUND SENSING ELEMENT TS216 SHORTED. R & R TS216 IAW WDM 26-18-21. AWD AMM 26-18-01/401. OPS CHECK SATISFACTORY.

Part: PACKING — BROKEN (HYD FILTER)

ATB - C SYS HYD QTY LIGHT FOLLOWED BY C SYS HYD PRESSURE EICAS MESSAGE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. FOUND RT LCCA FILTER COVER PACKING BROKEN. REPLACED PACKING AND LEAK CHECK OK. SERVICE RESERVOIR TO FULL. REF IPC 27-11-14-03, ITEM 140.

Part: CONTROL CABLE — ICED (HORIZONTAL STAB)

CREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. R & R RT POSITION MODULE CABLES AND LOWER TERMINAL ASSY/ TURNBUCKLE BODY, REF B, AMM 27-48-01-4 THRU STEP 3.D.(6). R & R THE CTR POSITION TRANSMITTER MODULE CABLES, LOWER TERMINAL ASSY/ TURNBUCKLE BODY REF AMM 27-48-01-4 UP THRU STEP 3.D(6). REMOVED LT STAB TRIM POS TRANSMITTER MODULE IAW MM 27-48-01-4.

Part: CONTROL CABLE — DAMAGED (HORIZONTAL STAB)

CREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. (OPEN)

Part: FLOOR PANEL — PUNCTURED (STA 434, RBL 83)

REF D425460 MAIN CARGO DECK, POSITION 2, OTBD FLOOR PANEL PUNCTURED. STA 434, RBL 83. ACCOMPLISHED MAJOR REPAIR IAW EO B767-5320-9693-G.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: 7C EMP - VERTICAL FIN L/E RT LOWER FIXED PANEL FOUND DELAMINATED. METAL HOT BAND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4 FIG 201. SHEET 1, REV. 45.

Part: PANEL — CHIPPED (LT WING TE FLAP) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, LT WING INBD MAIN FLAP OTBD EDGE MID AREA CHIPPED. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5H REV 45.

Part: WEDGE — DAMAGED (RT WING TE FLAP) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: C RT WING OTBD T/E FLAP INBD T/E WEDGE CHIPPED COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5G, FIG 14, REV 45.

Part: FLOOR SUPPORT — CRACKED (BS 1087) · airframe 36,885 hrs · 11,429 cycles

AFT CARGO COMPT STA 1087 RBL 25" FLOOR SUPPORT CLIP FOUND CRACKED. AFT CARGO COMPT STA 1087 RBL 25" FLOOR SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 45.

Part: FLOOR SUPPORT — CRACKED (BS 1087) · airframe 36,885 hrs · 11,429 cycles

AFT CARGO COMPT STA 1087 LBL 25" FLOOR SUPPORT CLIP FOUND CRACKED. AFT CARGO COMPT STA 1087 LBL 25" FLOOR SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 45.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 654+22 TO 690, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 36,885 hrs · 11,429 cycles

INSP TYPE: C LT WING - INBD MAIN FLAP INBD AFT FLAP HINGE FTG FOUND CRACKED LT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1 FIG201 REV45 ORG MATL IS 7075T73 FORGING, CRACK LENGTH IS 1.5" AT INBD FLANGE & 0.5" AT OTBD FLANGE. DAMAGED CUTOUT SIZE IS 1.5" X 0.75" (2 LOCATIONS) THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL AND 10134-2007-7075T6511 AS REPAIR ANGLES. REPAIR SIZE IS 2" X 4"

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, LT WING NR 4 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS 641.6 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 45, ORG MATL IS CLAD 7075T6-0.063", REPAIR LENGTH IS 0.15", DAMAGED CUTOUT IS 9" X 7.25". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD 7075T6-0.071" AS DOUBLER CLAD 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10 3/8".

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: 7C NO,1 PYLON - EXTERNAL SKIN CRACKED AT PYLON PANEL NR 432AL CUTOUT AREA. SKIN REPAIRED IAW HX RS NR R54-50-36587 A MATERIAL 2024T3-0.080" CRACK LENGTH 0.5",0.1875"DIA STOP HOLE DRILLED AT THE CRACK END. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AMS4911- 0.090" SHEET AS REPAIR DOUBLER. REPAIR SIZE 11.5"X10" THIS REPAIR IS TIME LIMITED FOR REPEAT INSP. REFER EO NR B767-5430-36284-A

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:C, RT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, LT WING NR 4 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS 572.875 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV 45 ORG MATL IS CLAD 7075T6-0.063", CRACK LENGTH IS 0.13", DAMAGED CUTOUT IS 9" X 7.375". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR W/MATL CLAD 7075T6-0.071" AS DOUBLER CLAD 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10 3/8".

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, LT WING NR 3 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR3 SLAT OTBD AREA AT OSS792.4 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV45 ORG MATL IS CLAD 7075T6-0.063" CRACK LENGTH IS 0.09" DAMAGED CUTOUT IS 8.875"X7.125" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD 7075T6-0.071" AS DOUBLER CLAD 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12"X10.125".

Part: FLOOR SUPPORT — CRACKED (BS 1581) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:C, AFT BULK CARGO STA 1581 RBL 70" CABIN FLOOR ANGLE FOUND CRACKED. AFT BULK CARGO STA 1581 RBL 70" CABIN FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: FLOOR SUPPORT — CRACKED (BS 1581) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:C, AFT BULK CARGO STA 1581 LBL 70" FLOOR ANGLE FOUND CRACKED. AFT BULK CARGO STA 1581 LBL 70" CABIN FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 36,885 hrs · 11,429 cycles

LT WING NR 3 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.4 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 REV 45 ORG MATL IS CLAD7075T6-0063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD7075T6-0.071" AS DOUBLER, CLAD 7075T6-0063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10.125"

Part: SKIN — CRACKED (NR 9 SLAT O/B) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, RT WING NR 9 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS 641.74 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV 45. ORG MATL IS CLAD 7075T6-0.063", CRACK LENGTH IS 0.14", DAMAGED CUTOUT IS 8.875" X 7.375". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD 7075T6-0.071" AS DOUBLER CLAD 7075T6-0.063" AS REPAIR. REPAIR SIZE IS 12" X 10 3/8".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1114 TO 1197+22, L11 TO L33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 372 TO 412, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1207 TO 1344, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: STIFFENER — CRACKED (BS 246) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: 7C, AV COMPT STA 246 AFT LBL 50 CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 AFT LBL 50" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 36,885 hrs · 11,429 cycles

INSP TYPE: 7C AFT OF FWD CARGO CENTER TANK FW LBL 10.94" STIFFENER UPPER FOUND CRACKED STIFFENER UPPER AREA REPAIRED IAW HX RS NR R57-10-36582A MATERIAL BAC1518-749-2024T3511,CRACK LENGTH 0.7" CUT OFF LENGTH 19.5" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AS REPLACEMENT SECTION. 2024T351-0.250" AS REPAIR STRAPS, 2024773-0.100" AS REPAIR STRAP AS WELL. REFER UPS EO NR B767-5710-36283A FOR DETAIL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200.) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE: 7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 731 TO 833, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 654+22 TO 690, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (MCD, ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: STIFFENER — CRACKED (BS 246) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:C, AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1207 TO 1344, R33 TO R55. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FPIMD DAMAGED AT STN 654+22 TO 690, R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,885 hrs · 11,429 cycles

INSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 833 TO 930, L11 TO L33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOORBOARD — DENTED (CARGO BAY)

INSPECTION TYPE:N/A D407591: MCD POS 11L FLOOR HAS 2 DENTS. FABRICATED NEW FLOORBOARDS PER B767-5320-9693-F.

Part: FLOORBOARD — DENTED (CARGO BAY)

INSPECTION TYPE:N/A REF D407590: TWO DENTS IN MAIN CARGO DECK FLOORBOARDS POS 4R TRANSFERRED FROM LOG PG 297108 ITEM 3. FABRICATED 2 NEW FLOOR PANELS PER EO B767-5320-9693-F.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A REF D407584 CENTER CARGO FLOOR POS 6 HAS FOUR HOLES MCD. FABRICATED 2 FLOOR PANELS PER B767-5320-9693-F.

Part: SHUTTLE VALVE — MALFUNCTIONED (RT BRAKE)

INSPECTION TYPE:N/A A/C PULLED LEFT USING AUTOBRAKES. RIGHT BRAKES INOP. REMOVED AND REPLACED AUTOBRAKE SHUTTLE VALVE PER MM 32-42-10-4, NO HELP. REMOVED AND REPLACED NORMAL AUTO SKID MODULE PER MM 32-42-02-4. GROUND OPS CHECKS GOOD AND LEAK CHECKS GOOD, OK FOR SERVICE.

Part: YAW DAMPER — INOPERATIVE (FLIGHT CONTROL)

A/C YAWED CONTINUOUSLY LT AND RT AT HIGH SPEEDS. T/S FOUND M509 RT UPR YAW DAMPER SERVO LVDT RESISTANCE VALUE ABNORMAL AND M317 O/B SPOILER NR 12 PCA LVDT PIN 8 SHROTED TO CASING. BOTH M509 RT UPPER YAW DAMPER SERVO AND M317 O/B SPOILER NR 12 PCA REPLACED. YAW DAMPER SERVO INSTALLATION TEST O/B SPOILER NR 12 PCA INSTALLATION TEST NORMAL.

Part: VALVE — MALFUNCTIONED (PARKING BRAKE)

INSPECTION TYPE:N/A BTB - A/C TURNS LEFT DURING BRAKING. REMOVED AND REPLACED PARKING BRAKE VALVE IAW AMM 32-44-04-4.

Part: COMPUTER — INOPERATIVE (FLT MANAGE)

INSPECTION TYPE:ETOP BTB - LT FMC SINGLE SOURCE MESSAGE. (08-17-07] ACCOMPLISHED FIM 34-61-00 FIG 108A, ALL TESTS PASSED. THE SYSTEM IS OK.

Part: WINDOW — DEFECTIVE (COCKPIT)

INSPECTION TYPE:N/A CREW PREFLIGHT - CAPTAIN'S SIDING WINDOW HARD TO OPEN. A/C REMOVED FROM SERVICE. REMOVED AND REPLACED L2 WINDOW PER 56-11-02-4.

Part: ACARS — INOPERATIVE (COCKPIT)

ACARS - NO COMMUNICATION. TRANSMISSION ON LT HF INOP AT ALL STATIONS. T/S FOUND LT HF TRANSCEIVER FAULT. R/R LT TRANSCEIVER. OP CHECK NORMAL PER MM 23-11-03.

Part: SEAT TRACK — CORRODED (BS 512-619) · airframe 25,676 hrs · 8,152 cycles

AREAS OF CORROSION ON SEAT TRACK AT BS 512, BS 556, BS 576, BS 619 LBL 88 WL 200. REMOVED AND REPLACED SEAT TRACK PER DWG 143T5242 AND SRM 51-40-02, 51-40-03.

Part: GENERATOR — LEAKING (RIGHT)

ATB - RT GENERATOR FAILED, EMERGENCY DECLARED. SERVICE RT IDGE WITH 2 QTS OIL GWL 0558164/REMOVED NR 2 ENG IDG IAW MM 24-11-01 DW 0558595\ TRANSFERRED FITTINGS WITH NEW O-RINGS TW 1229598 REF MM 24-11-01 INSTALLED NEW IDGE ON NR 2 ENG OPS AND LEAK CK GOOD.

Part: GENERATOR — DISCONNECTED (RT)

INSPECTION TYPE: ETOP ATB - DUE RT GEN DRIVE MSG DISPLAYED ON T/O AT 100 KTS. ONE ELEC SOURCE REMAINING. FOUND RT GEN DISCONNECTED AND OIL LEVEL LOW AND FILL UNION LOOSE. RECONNECTED IDG IAW 24-11-01. TIGHTENED FILL UNION AND SERVICED IDG IAW 12-13-03-3 ENG RUN CARRIED OUT SYS NOW SATIS AND NO LEAKS FOUND.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT SWITCH PANEL ANNUNCIATOR DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL AND PERFORMED CHECK OK IAW 33-51-08.

Part: ENGINE — FLAMED OUT (RIGHT)

INSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED.

Part: CLAMP — BROKEN (LT HEAT EXCHANGE)

INSPECTION TYPE:ETOP ATB - LT PACK INOPERATIVE LIGHT ILLUM AND LT (PACK TEMP) EICAS MESSAGE. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED AND RESET PUSHED. REMOVED AND REPLACED BROKEN CLAMP TO HEAT EXCHANGER RVM, LT PACK. OPS CHECK NORMAL IAW MM 21-50-00.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE: ASV, EMERGENCY LIGHT ABOVE LT SUPERNUMERARY SEAT INOP. RELAMPED, OPS CHECKS OK.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:N/A, MX INSPECTION - LT WING UPPER SKIN PANEL CRACKED INC NR RSOO-118. *S/D* REMOVED AND REPLACED PANEL IAW SRM 51-40-0 (P/N 113T1654-235).

Part: GEAR LEVER — MALFUNCTIONED (COCKPIT)

GEAR LEVER WOULD NOT MOVE TO UP POS INFLT WAS FREE TO MOVE TO UP POS WHEN LOCK OVRH PUSHER. FLIGHT RETURNED TO SDF PER AMC. AIR TURN BACK, FOUND LEVER LOCK CIRCUIT BREAKER NOT COMPLETELY IN. RESET BREAKER AND OPS CHECKED LANDING GEAR CONTROL PER MM 32-31-00. OK FOR SERVICE.