N319UP

Part: DRAIN — INOPERATIVE · airframe 67,093 hrs · 22,861 cycles

FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). ACCOMPLISHED EO-82173-JIC001.

Part: DRAIN — NONE · airframe 67,092 hrs · 22,860 cycles

(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). C/W EO-82173.

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 67,093 hrs · 22,861 cycles

FOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR). REMOVE ADJACENT FASTENERS AROUND CRACKED HOLE TO SEPARATE STRUCTURE I.A.W SRM 51-40-02-0G REV.90 IN ORDER TO HAVE NDT DOUBLE CHECK. INSTALL REMOVED FASTENERS I.A.W SRM 51-40-02-0G REV.90 AFTER NDT VERIFY NO CRACK INDICATION. INSTALLED SCUFF PLATE OF AFT & MID ENTRY DOOR I.A.W AMM 53-13-01-424-005 REV.143. INSTALLED ENTRY DOOR AFT SIDE DOOR TRACK OF LOWER SIDE I.A.W AMM 52-12-01-404-024 REV.143. INSTALLED DOOR DOORWAY LINING OF AFT DOOR I.A.W AMM 52-12-02-404-025 REV.143.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DEND - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 977 TO STA 1107 LBL-22 P/N: 145T5876-72. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA-930 TO STA 973 LBL-65 (P/N: 145T5876-79) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

DENT AND BROKEN - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1043 RBL-45 (P/N: 145T5876-75) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 742 TO STA 830 LBL-11 TO RBL-11, 145T5876-68. (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 933 TO STA 984 LBL-85 (P/N: 145T5876-78) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 67,093 hrs · 22,861 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 830 TO STA 933 LBL-58 P/N:145T5876-57 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONFIRM REPAIR PER SREO.

Part: SKIN — DEBONDED (10) · airframe 67,092 hrs · 22,860 cycles

FOUND DISBOND AT NO.10 SPOILER UPPER SURFACE. (REPAIR). I.A.W AMM 20-11-00-910-802 REV.143 INSTALLED THE #10 SPOILER INBOARD SEAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 930 TO STA 977 RBL-81 P/N:145T5876-84 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1043 LBL-45 (P/N: 145T5876-71) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: ANGLE — CRACKED (ZONE 100) · airframe 67,092 hrs · 22,860 cycles

THE ANGLE OF BULK CARGO COMPARTMENT LEFT AREA WITH CRACK AT STA 1578 LBL 60. (REPLACE). I.A.W AMM 25-59-01-404-019 REV.143 INSTALL MAIN DECK CARGO DADO PANEL AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND FLOOR PNL BROKEN AND DENT AT STA 930 STA 973 LBL-33 (P/N: 145T5876-81) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 977 TO STA 1087 LBL 81 P/N: 145T5876-22. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1107 LBL 11 TO RBL-11 P/N:145T5876-73 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: ANGLE — CRACKED (ZONE 100) · airframe 67,092 hrs · 22,860 cycles

THE ANGLE OF BULK CARGO COMPARTMENT RIGHT AREA WITH CRACK AT STA 1578 RBL 60. (REPLACE). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 742 TO STA 830, LBL-65 P/N: 145T5876-63 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1109 RBL-22 P/N: 145T5876-74. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 67,092 hrs · 22,860 cycles

CRACK ON DOUBLER COMMON TO BULKHEAD FWD SIDE AT STA 1809, LBL 28.5. (EVALUATE). I.A.W AMM 20-10-09-404-007 REV 143 DO A LEAK CHECK TEST FOR THE HYDRAULIC TUBE, RESULT WAS NO LEAK FOUND. CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 930 TO STA 973 LBL-44 (P/N: 145T5876-80) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: BUMPER — DAMAGED (ZONE 800) · airframe 67,092 hrs · 22,860 cycles

FOUND THE CREW ENTRY DOOR FORWARD DOORWAY LINING BUMPER WITH BROKEN DAMAGE. (REPLACE) OK TO WORK.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

FAULT - BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 830 TO STA 933 LBL-58. (REPAIR) OK TO WORK

Part: BUMPER — DAMAGED (ZONE 800) · airframe 67,093 hrs · 22,861 cycles

FOUND THE CREW ENTRY DOOR FORWARD DOORWAY LINING BUMPER WITH BROKEN DAMAGE. (REPLACE). REPLACE DOORWAY LINING BUMPER I.A.W AMM 52-12-02-004-001 REV.143 AND AMM 52-12-02-404-025 REV.143. / JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

FOUND THE MAIN DECK CARGO FLOOR PANEL DENT AND BROKEN, P/N: 141T5856-3. (REPAIR). I.A.W AMM 53-01-06-400-801 REV.143 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 67,092 hrs · 22,860 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, P/N:453T7025-12 (REPAIR). .I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 AND AMM 25-58-05-404-026 REV 143 RESTORED MAIN DECK CARGO HANDLING.

Part: HINGE FITTING — CRACKED (ZONE 600) · airframe 67,092 hrs · 22,860 cycles

CRACKED SUPPORT RIB RIGHT WING NO : 10 SPOILER INBOARD SUPPORT RIB (REPLACE). I.A.W AMM 27-61-02-424-023 REV.143 AND AMM 27-61-00-825-072 REV.143 ADJUST THE NO.12 SPOILER PCA AND RESULT WAS SATISFIED. I.A.W AMM 20-10-09-404-007 REV.143 DO A LEAK CHECK TEST FOR THE HYDRAULIC TUBE, RESULT WAS NO LEAK FOUND.

Part: SEAL DEPRESSOR — DAMAGED (ZONE 800) · airframe 66,836 hrs · 22,752 cycles

FWD CARGO DOOR SEAL DEPRESSOR UPPER AFTER WITH DAMAGE, DENT, SCRATCH AND HOLE SREO-8088-REQ001 ((APPX A) INTERIM REPAIR: B767: CARGO DOOR SEAL DEPRESSORS AND ADJACENT FORMED ANGLES - REPAIR OF IMPACT DAMAGE (SREO) OPEN

Part: SEAL DEPRESSOR — DAMAGED (ZONE 100) · airframe 66,979 hrs · 22,814 cycles

FWD CARGO DOOR SEAL DEPRESSOR UPPER AFTER WITH DAMAGE, DENT, SCRATCH AND HOLE. MATCH DRILLED SEAL DEPRESSOR PER EXAMPLE & INSTALLED SEAL DEPRESSOR IAW SRM-51-40-02.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 65,885 hrs · 22,350 cycles

*MAJOR REPAIR* ( SHEET -METAL EVAL ) - POSITION 7C - MCD FLOOR BOARD ( DAMAGED UPON REMOVAL REMOVAL. AFT LH FASTENER INSERT ( MARKED WITH TAPE. UNDERSIDE FWD PANEL LAYER PEELING-SEPARATED ( MARKED WITH TAPE.) INSTALLED POS 7 MCD FABRICATED FLOOR PNL PER AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 65,885 hrs · 22,350 cycles

*MAJOR REPAIR* MAIN CARGO DECK FLOOR PANEL DAMAGED AT POS 2R. DAMAGE AT AFT END OF PANEL WHERE LONG GUIDE ASSY ATTACHES.***SM13/LMX8*** INSTALLED MCD FLOOR BOARD @STA 280-390 WITH REF TO AMM 53-01-06

Part: FLOOR PANEL — UNKNOWN (UNKNOWN) · airframe 65,325 hrs · 22,111 cycles

MAIN CARGO DECK CENTER FLOOR PANEL BETWEEN POSITION 10 AND 11 DAMAGED INSTALLED FLOOR PANEL IAW AMM 53€“01-06

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 65,344 hrs · 22,122 cycles

*** SUPPLEMENTAL SDR *** MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 11L/11R INSTALLED NEW FITTINGVAT POSITION 11L/11R IAW AMM 20-11-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,325 hrs · 22,111 cycles

LH SIDE OF FUSELAGE AFT OF ADP EXHAUST PANEL 195PL DAMAGED ASSIGNED EO-88576-REQ1 FOR TEMPORARY REPAIR. OPEN

Part: PANEL — DAMAGED (UNKNOWN) · airframe 65,462 hrs · 22,168 cycles

**SUPPLEMENTAL SDR**LH SIDE OF FUSELAGE AFT OF ADP EXHAUST PANEL 195PL DAMAGED***SM40/LMX10***AWP REQ#471333*** COMPLIED WITH EO. 88576 REQ 2, REFERENCE BARCODE T3F18E003D7WD FOR NEW DEFERRAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,325 hrs · 22,111 cycles

*SDR FILED OPEN* MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 11L/11R INSTALLED NEW FITTINGVAT POSITION 11L/11R IAW AMM 20-11-00

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 65,344 hrs · 22,122 cycles

*** SUPPLEMENTAL SDR *** MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 7C C/W SREO-44173-REQ001 FOR LOCK.213 POS 7C REF. (T3F18E0037UUA)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,325 hrs · 22,111 cycles

MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 7C. OPEN

Part: SKIN — DAMAGED (UNKNOWN) · airframe 65,203 hrs · 22,056 cycles

SKIN BUBBLING L SIDE OF FUSELAGE AFT OF ADP EXHAUST. DRILLED, TRIMMED AND COUNTERSUNK NEW PANEL PER SRM 51-40-02-0G-0. STARTED INSTALLATION PER AMM 53-52-01. COMPLETED REMAINING STEPS OF AMM 53-52-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,100 hrs · 22,004 cycles

*** SDR FILED OPEN *** SKIN BUBBLING L SIDE OF FUSELAGE AFT OF ADP EXHAUST REMOVED AFT LOWER FUSELAGE PANEL 195PL REF B767 AMM 53-52-01 AND ROUTED TO SHEETMETAL SHOP FOR REPAIR

Part: ENGINE — SURGES (LEFT) · airframe 64,968 hrs · 21,954 cycles

AIR TURNBACK L ENG SURGING AIRCRAFT YAWING N2 SURGING. CONTINUED WITH ENG RUNNING. LANDED ONT (+/- 10% N2 REPEATEDLY ON CLIMBOUT ) COMPLETED MPA TEST PER TASK 71-00-00-735-078-H03. OPS CHECK GOOD NO FAULTS NOTED AND NO SURGING DURNING RUN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,966 hrs · 21,952 cycles

*SDR FILED OPEN* AIR TURNBACK L ENG SURGING AIRCRAFT YAWING N2 SURGING. CONTINUED WITH ENG RUNNING. LANDED ONT (+/- 10% N2 REPEATEDLY ON CLIMBOUT )

Part: DOOR — FAILED (NLG DOOR RT) · airframe 65,012 hrs · 21,973 cycles

RIGHT NOSE GEAR DOOR FAILED TO RETRACT. INSTALLED NLG DOOR STRUT ASSEMBLY WRT AMM 32-22-02. RIGGED AS REQD AND PERFORMED FUNCTIONAL CHECK WRT 32-22-02. NO DEFECTS NOTED. RII PERFORMED FOR NLG SWING REF 32-22-02. RII HAS BEEN ACCOMPLISHED AND TEMPORARY LABOR SKILL HAS BEEN REMOVED.

Part: SHEAR WEB — CORRODED · airframe 64,426 hrs · 21,711 cycles

FAULT - SHEAR WEB CORR FRS 470/510 & LBL 11.0/33.0 DISPLACED 2 CEILING PANELS IN FWD CARGO PIT LOWER FRS 470 AND FRS 510 FOR ACCESS IAW SRM 51-40-02. REMOVED SHEAR WEB PANEL DAMAGE, IAW SRM 51-40-02. INSPECTED PANEL, OUT OF LIMITS IAW B767 SRM 53-30-53-1A-1. FABRICATED NEW SHEAR WEB FROM 7075-T6.071C, BATCH # 0003993959. LOCATED AND MATCH DRILLED NEW SHEAR WEB IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOPCOAT IAW AMM 51-21-15. INSTALLED NEW SHEAR WEB PANEL IAW SRM 51-40-02. APPLIED CIC IAW B767 AMM 51-24-09. INSTALLED FWD CARGO PIT CEILING PANELS IAW AMM 25-52-02-401. REVIEWED DOCUMENTS FOR COMPLETION.

Part: SHEAR WEB — CORRODED · airframe 64,426 hrs · 21,711 cycles

FAULT - SHEAR WEB CORROSION STA 280, RBL 18- RBL 28 REMOVED FASTENERS (50EA) AT MAIN CARGO FWD FLOOR PAN SHEAR WEB STA 280 BETWEEN RBL 18 TO RBL 28 IAW B767 SRM 51-40-02. CLEANED & INSPECTED DAMAGED AREA, PITTING CORR NOTED BETWEEN RBL 27.00 TO RBL 30.50 FROM FRS 279.40 TO FRS 284.80. COMPLETE PERFORATION OF SHEAR WEB P/N 141T5402-6. OUT OF LIMITS IAW B767 SRM 53-10-51-1A-2, DETAIL 3. DISPLACED SHEAR WEB BETWEEN RBL 18 AND RBL 28 FROM STA 280 TO STA 340 IAW SRM 51-40-02. REMOVED (2EA) STIFFENERS LOWER PAN SHEAR WEB BETWEEN STA 340 AND STA 320 IAW SRM 51-40-02. REMOVED FITTING UPPER PAN SHEAR WEB IN STA 280 IAW SRM 51-40-02. REMOVED 2 ANGLES IN PAN SHEAR WEB STA 270 IAW SRM 51-40-02. REMOVED PLATE LOWER PAN SHEAR WEB STA 280 IAW SRM 51-40-02. REMOVED PAN SHEAR WEB BETWEEN STA 270 AND STA 340, FROM RBL 18 TO RBL 28 AND E1/E2 RACK TOP STIFFENER. RECEIVED MATERIAL P/N 7075-T6.071C, BATCH #0003993959. FABRICATED, LOCATED AND DRILLED PAN SHEAR WEB WITH MATERIAL P/N 7075-T6.071C. IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. PAINTED PAN SHEAR WEB IAW AMM 51-21-15. INSTALLED SHEAR WEB AT STA 280 TO 340, FROM RBL 18 TO RBL 28 IAW SRM 51-40-02. INSTALLED (2EA) STIFFENER ANGLES, LOWER PLATE AND FITTING UPPER PAN SHEAR WEB AND TWO ANGLES IAW 51-40-02. APPLIED CIC IAW B767 AMM 51-24-09. INSTALLED DRIP PANS AND E1/E2 RACK STIFFENER IAW B767 SRM 51-40-02-0G. REINSTALLED UPPER PAN FITTING IN UPPER PAN IAW SRM 51-40-02. REINSTALLED PLATE LOWER PAN SHELL IAW SRM 51-40-02. REINSTALLED TWO ANGLES IN PAN SHELL IAW SRM 51-40-02.

Part: DOOR — NONE (CABIN) · airframe 64,135 hrs · 21,588 cycles

L FWD ENTRY DOOR EICAS ILLUMINATED FOR 3 SECONDS THE EXTINGUISHED DURING PUSHBACK. EACH FLT REINSPECT- CREW ENTRY DOOR INDICATING SYSTEM - ALL DOOR EXCEPT MAIN CARGO DOOR. MEL 52-71-1-1 DMP DI LOG UPDATED.R/R BENT ENTRY DOOR SENSOR BRACKET & ADJUSTED SENSOR S194 PER AMM 52-71-00. SYS OPS NORMAL. THIS CLEARS M802867.

Part: FLOOR PANEL — NONE (M/D FLOOR) · airframe 64,054 hrs · 21,558 cycles

INSPECTION TYPE:C13*MAJOR REPAIR* BROKEN DAMAGE ON MAIN DECK FLOOR PANEL (PANEL NO.:231KFF, PN:143T5876-89) BETWEEN STA 554 AND 654+22 AND BETWEEN LBL 77 AND 88.FABRICATE REPLACEMENT FLOOR PANEL I.A.W UPS SREO NO.B767-5320-9693-I.

Part: SKIN — CRACKED (NO.9 SLAT SKIN) · airframe 64,054 hrs · 21,558 cycles

INSPECTION TYPE:C13*MAJOR REPAIR* CRACK ON NOSE SKIN(P/N:114T4104-4) OF NO.9 SLAT AT OSS 641.945REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01

Part: SKIN — CRACKED (NO.9 SLAT SKIN) · airframe 64,054 hrs · 21,558 cycles

INSPECTION TYPE:C13*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4104-4) OF NO.9 SLAT AT OSS 572.55REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,054 hrs · 21,558 cycles

INSPECTION TYPE:C13*MAJOR REPAIR* CRACK FOUND ON FUSELAGE SKIN AT STA 1654, S-13ARREPAIR I.A.W 767-300F SRM 53-80-01-2R-7 REV.85.01

Part: SKIN — CRACKED (NO.10 SLAT SKIN) · airframe 64,054 hrs · 21,558 cycles

INSPECTION TYPE:C13*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4103-4) OF NO.10 SLAT AT OSS 723.94REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV 85.01

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 63,811 hrs · 21,452 cycles

MAIN CARGO FLOOR PANEL AT POSITION A 2 STA 280-412 RBL 88.5 HAS A HOLE PUNCTURED IN IT. FABRICATED REPLACEMENT FLOORBOARD 141T5856U13 PER SAMPLE AND SREO B767-5320-9693-I. FABRICATED A NEW FLOORBOARD ON NR 684239.

Part: ALTIMETER — INOPERATIVE (FIRST OFFICER'S) · airframe 63,687 hrs · 21,395 cycles

INSPECTION TYPE:NAFO ALTIMETER ERRATIC IN CLIMB, CRUISE & DESCENT. DURING CLIMB IT HESITATES, ALMOST REVERSES COURSE BEFORE CLIMBING MORE. THIS HAPPENS APPR. EVERY 100 FT. THIS BEHAVIOR IS THE SAME IN DESCENT. DURING CRUISE IT HOLDS STEADY THEN JUMPS UP & DOREMOVED AND REPLACED RIGHT AIR DATA COMPUTER PER M 34-12 01. NO CURRENT FAULTS ON 30 CHECK

Part: WEB — CORRODED (STA 566) · airframe 59,406 hrs · 19,847 cycles

INSPECTION TYPE: C12 COROSSION ON WEB (P/N:143T5014-27)OF FWD CARGO FLOOR STRUCTURE NEAR STA 566, RBL 24. REPAIR IAW BOEING SRID:3-4901064662 AND UPS EO B767-5320-78931-A.

Part: SPLICE — CORRODED (STA 877) · airframe 59,406 hrs · 19,847 cycles

INSPECTION TYPE: C12 CORROSION ON SPLICE TEE (P/N:145T8629-2) ON KEEL BEAM LOWER PANEL SUPPORT STRUCTURE NEAR STA 877, BETWEEN RBL 10-LBL 10. REPAIR IAW BOEING DWG 145T8629 SH 1, REV "B" AND BOEING 767-300F SRM 51-40-02, REV 79.

Part: SPLICE — CORRODED (STA 830) · airframe 59,406 hrs · 19,847 cycles

INSPECTION TYPE: C12 COROSSION ON SPLICE TEE (P/N:145T8629-2) ON KEEL BEAM LOWER PANEL SUPPORT STRUCTURE NEAR STA 830, BETWEEN RBL 10-LBL 10. REPAIR IAW BOEING DWG 145T8629 SH 1, REV "B" AND BOEING SRM 767-300F 51-40-02, REV 79.

Part: SPLICE — CORRODED (STA 907) · airframe 59,406 hrs · 19,847 cycles

INSPECTION TYPE: C12 CORROSION ON SPLICE TEE (P/N:145T8629-3) ON KEEL BEAM LOWER PANEL SUPPORT STRUCTURE NEAR STA 907, BETWEEN RBL 10-LBL 10. REPAIR IAW BOEING DWG 145T8629 SH 2, REV "A" AND BOEING SRM 51-40-02, REV 79.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 58,847 hrs · 19,638 cycles

MAIN CARGO P1 RT SIDE NR 2 FLOORBOARD DAMAGED. THIS IS A MAJOR REPAIR, TRANSFERRED TO NRC 670726 5144926 10-3-20. COMPLETED FABRICATION OF FLOOR PANELD, PER EO B767 5320 9693-I, ALL WORK COMPLETED ON NRC 670726. COMPLETED FABRICATION OF FLOOR PANEL, PER EO B767-5320-9693-I. ALL WORK COMPLETED ON NRC 670726.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 58,847 hrs · 19,638 cycles

INSPECTION TYPE: N/A FLOOR PANEL DAMAGED. FABRICATED NEW PANEL, IAW B767-5320-9693.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 58,847 hrs · 19,638 cycles

MAIN CARGO P1 RT SIDE NR 1 FLOOR BOARD DAMAGED. THIS IS A MAJOR REPAIR, TRANSFERRED TO NRC NR 670725 514476 10-3-20. COMPLETED FABRICATIONOF FLOOR PANEL, PER EO B767 5320 9693-I ALL WORK COMPLETED ON NRC NR 670725. COMPLETED FABRICATION OF FLOOR PANEL, PER EO B767-5320-9693-I. ALL WORK COMPLETED ON NRC 670725.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 58,847 hrs · 19,638 cycles

INSPECTION TYPE: N/A FLOOR PANEL DAMAGED. FABRICATED NEW PANEL, IAW B767-5320-9693.

Part: CAP — MISSING (THRUST REVERSER) · airframe 57,935 hrs · 19,249 cycles

INSPECTION TYPE:N/ALEFT ENG LEFT REVERSER HALF CENTER INNER CLEVIS PIN ACCESS PLUG CAP MISSINGINSTALLED NEW CAP IN INNER CLEVIS PIN ACCESS LEFT ENG LEFT REV HALF REF AMM 78-31-10

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55,597 hrs · 18,393 cycles

INSPECTION TYPE:N/A TRAILING EDGE FLAP DISAGREE EICAS MSG: LIGHT APPEARED AFTER SELECTING 15 FLAPS. LANDED FLAPS 20(DEG). EMERGENCY DECLARED. PERFORMED FIM 27-51-00-815-838 FOUND FAULT CODE TE DISAGREE NR 27-51104 ON FSEU, STEP 1. CLEARED CODE & CONTINUED STEPS 2 TO 4. FAULT WOULD NOT DUPLICATE. NO FAULTS AT THIS TIME. PERFORMED FIM. 27-51-00-815. STEPS 1,41,2,3,4,5,26 R/R FSEC PER MM. 27-51-01-401. SYS TES.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 55,130 hrs · 18,207 cycles

INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533- STA 654 PLUS 22, LBL 11- LBL 33, PNL NR 231GFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 55,130 hrs · 18,207 cycles

INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533- STA 654 PLUS 22, LBL 55- LBL 77, PNL NR 231JFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,113 hrs · 18,205 cycles

INSPECTION TYPE:C11 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, LBL 25, WL 159 EO B767-5310-20118-F AND SRM 51-70-12 GENERAL, FIGURE 1, REV. 73.00.

Part: PANEL — MISSING (LT WING SLAT) · airframe 53,282 hrs · 17,503 cycles

LEFT WING NR 4 SLAT L/E PANEL MISSING. REINSTALLED IAW DRAWING 114T4260.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 52,537 hrs · 17,246 cycles

MCD FLOOR PANEL DAMAGED AT POSITION 8/9L BS 1115, LBL 36. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-96-93-1.

Part: TRU — FAILED (APU) · airframe 52,241 hrs · 17,134 cycles

APU TRU START CIRCUIT BREAKER TRIPPED ON P32 PANEL. REPLACED APU TRU IAW AMM 24-32-04-4. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 50,769 hrs · 16,568 cycles

AIRCRAFT HAD DIFFICULTY CLIMBING THRU FL 31000. RT ENG FUEL FLOW AT .7 (700 LBS/HR), N1, EGT AND N2 WERE SIGNIFICANTLY BELOW LT ENG. CONDUCTED QRH ENGINE INFLIGHT. START CHECKLIST AND RT ENG STARTED WITH NO PROBLEMS. ENGINE OPERATED WITHIN ALL LIMITATIONS AND PARAMETERS. R & R ECU IAW AMM 73-21-15, NO FAULTS IAW 73-21-27-01, R & R THE NR 2 HMU AND TEST GOOD IAW AMM 73-21-14-401.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,752 hrs · 16,565 cycles

INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV.67, AND EO B767-5740-58151-A.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,752 hrs · 16,565 cycles

INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 11. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 67, AND EO B767-5740-58151-A.

Part: STRINGER — CRACKED (BS 1508-1519) · airframe 50,752 hrs · 16,565 cycles

INSPECTION TYPE: C10, CRACK WAS FOUND ON THE STRINGER 20L AT BS 1508 AND 1519. REPAIR IAW SRM 53-00-03-2R-5, REPAIR 5, REV.67, AND EO B767-5310-63458-A.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,563 hrs · 15,772 cycles

EXIT SIGN ADJACENT TO L1 DOOR BROKEN, ATTACTHED EXIT SIGN LENS COVER, OPS CHECKED NORMAL.

Part: EVAS UNIT — INOPERATIVE (COCKPIT) · airframe 47,885 hrs · 15,526 cycles

F/O EVAS UNIT WITHOUT FUNCTION. F/O EVAS UNIT REPLACED IAW AMM 25-69-00, PB 401, REV. 116.03, DATED 12-08-15. PN OFF-ON: 107STC-268, SN OFF: 0019 X 06P, SN ON: 0030 X 09P. EFF REF IPC: 25-60-00-90, ITEM -002 REV 79.00, DATED 11-12-15.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 47,383 hrs · 15,301 cycles

FLIGHT DECK EXIT LIGHT INOPERATIVE. COVER FELL OFF IN FLIGHT IAW AMM 33-51-01. REINSTALLED LENS LIGHT. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 47,162 hrs · 15,213 cycles

EMERGENCY EXIT LIGHT DO NOT TURN OFF WHEN SWITCH IS PLACED TO OFF. REPLACED EMERGENCY LIGHT CONTROL PANEL IAW MM 33-51-08-401. PN ON AND OFF 233N3219-300. SN ON D00101, SN OFF D00071.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,070 hrs · 15,169 cycles

FOUND EMERGENCY LIGHT ILLUMINATED WITH SWITCH IN OFF POSITION. R & R EMERGENCY POWER SUPPLY IAW AMM 33-51-07-4, REV 114.03. OPS CHECKED OK.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 47,043 hrs · 15,156 cycles

AFTER ACFT SHUTDOWN EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN THE OFF POSITION. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD IAW AMM 33-51-16-962.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 46,855 hrs · 15,092 cycles

MAIN CARGO DECK FLOOR PANEL IN POSITION 2R HAS A PUNCTURE DAMAGE LOCATED APPROX 7" AFT OF FWD EDGE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FAILSAFE — CORRODED (BS 955) · airframe 46,380 hrs · 14,919 cycles

INSPECTION TYPE:C9, DURING THE ACCOMPLISHEMENT OF EO B767-5350-17922-M, APPENDIX D, FOUND CORROSION. REPAIRED CORROSION DAMAGE AND DEVIATIONS IAW B767-5710-56898-A AND B767-5340-56914-A IAW SR: 3-3134629013, 3-3165746532, WITH APPROVED 8100-9 FORM.

Part: FLOOR PANEL — DENTED (M/D CARGO) · airframe 46,380 hrs · 14,919 cycles

INSPECTION TYPE:C9, FOUND DENT, M/D CARGO FLOOR PANEL, 241MFF BETWEEN STA 412-STA 533, LBL 11-LBL-33 FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — CRACKED (M/D CARGO) · airframe 46,380 hrs · 14,919 cycles

INSPECTION TYPE:C9, FOUND CRACK MAIN DECK CARGO FLOOR PANEL, 242JFF, BETWEEN STA 930-STA 972, RL 11-RBL 33. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-H.

Part: ANNUNCIATOR — BROKEN (COCKPIT)

FLIGHT DECK EMERGENCY LIGHTS PANEL, ANNUNCIATES LIGHTS INOPERATIVE. ANNUNCIATOR LIGHT FOUND BROKEN. REPLACED EMERGENCY LIGHTS PANEL IAW AMM 33-51-08-404-010. CKS OK, EFF REF IPC 33-51-08-01A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL 3, & 4R DAMAGED. FABRICATE NEW FLOOR PANEL IAW EO B767-5320-9693.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 42,474 hrs · 13,333 cycles

INSPECTION TYPE:C08, CRACK-FOUND A CRACK ON CARGO FLOOR PANEL 251CFF AT BS 1118 AND LBL 34.5. THE DIMENSION OF CRACK LENGTH IS APPROX 6". REPAIRED IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (MAIN CARGO) · airframe 42,474 hrs · 13,333 cycles

INSPECTION TYPE:C08, DENT-FOUND A DENT ON CARGO FLOOR PANEL 251XFF AT BS 1491 AND LBL 84. THE DIMENSION OF DENT IS 4 IN(L) X 3 IN(W) X 0.214 IN(D). REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (MAIN CARGO) · airframe 42,474 hrs · 13,333 cycles

INSPECTION TYPE:C08, DENT-FND A DENT ON M/D CARGO FLOOR PANEL 252JFF AT BS 1263 AND RBL 86. THE DIMENSION OF DENT IS 3 IN(L) X 2 IN(W) X 0.196" (DEPTH ). REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK POS 12L HAS A HOLE IN FLOOR PANEL AFT SIDE ON 2ND PANEL D408945. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — TORN (BS 1307)

FLOOR PANEL, BS 1307 HAS A TEAR. FABRICATED NEW FLOOR PANEL IAW EO 767-5320-9693-H.

Part: FLOOR PANEL — TORN (BS 1263)

MAIN CARGO DECK FLOOR PANEL, BS 1263 HAS A TEAR. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL, BS 1463, POS 10-11, CTR HAS A HOLE PN 146T58 69-78. FABRICATED NEW FLOOR PANEL IAWEO 767-5320-9693-H.

Part: SKIN — DAMAGED (RUDDER)

RUDDER T/E SKIN DAMAGED ON UPPER RT SIDE 12" UP FROM BOTTOM EDGE. REPAIRED IAW EO B767-5540-47177-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

INSPECTION TYPE:PS, MAIN CARGO FLOOR PANEL AT POSITION 2R IS DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL A402H.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS NR 1 DAMAGED. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS NR 10R HAS HOLE IN FWD END. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

MAIN DECK FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS NR 1 DAMAGED 39" AFT OF FWD END. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS NR1 3RD FROM RT SIDE HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FLOOR PANEL POS NR 7R HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS NR 4 CENTER HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CABIN)

HOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

HOLE IN FLOOR PANEL POS NR 8R. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: WINDOW — ARCED (COCKPIT)

INSPECTION TYPE: ETOP DIV - AT 30,000 R FWD WINDSCREEN STARTED ARCING IN LWR CTR SECTION. ARCING VERY QUICKLY PROGRESSED TO A GROWING RED EMBER WHICH THEN SPREAD ALONG LOWER LT OF WINDSCREEN, AT WHICH POINT WE SECURED POWER TO RT FWD WINDSCREEN. ARCING STOPPED, RED EMBERS DIMINISHED. LANDED AT NEAREST AIRPORT. WINDSHIELD HAD DEFORMITY IN LOWER CTR SEC. R & R R-1 WINDOW IAW M/M 56-11-01-4. REVERSED DMP.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

REF D460011 MAIN CARGO DECK FLOOR PANEL POS 11R OTBD DAMAGED. IDENTIFIED FLOOR PANEL FROM 11R OTBD AS PN146T5869-50 IAW EO B767-5320-9693- FAB A REPLACEMENT FLOOR PANEL BY CUTTING OUT NEW FLOOR PANEL FROM A402H AND MARKED INSERT LOCATION USING EXISTING FLOOR PANEL AS TEMPLATE DRILLED AND CLEANED HOLES OF DEBRIS, INSTALLED INSERTS USING BMS 5-107 MARKED UNDER SIDE OF PANEL WITH THIS EO.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

MCD FLOOR PANEL POS 14R OTBD PANEL 2EA HOLES IDENTIFIED PANEL FROM POS 14R OTBD AS PN 146T5869-88 IAW EO B767-5320-969 3 FAB A REPLACEMENT PANEL BY CUTTING OUT NEW PANEL FROM A402H AND MARKED INSERT LOCATION USING EXISTING PANEL AS TEMPLATE DRILLED AND CLEANED HOLES OF DEBRIS INSTALLED INSERTS USING BMS 5-107 MARKED UNDER SIDE OF PANEL WITH THIS EO. INSTALLED ON L/P371754 FOR INSTALLATION.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

POS 7R HAS A DAMAGED MAIN DECK FLOOR PANEL ON 3RD PANEL FROM RT, 2" FROM AFT EDGE AND 9" FROM OTBD EDGE HOLE MEASURE .5 INCHES IN DIAMETER. INSTALLED TEMPORARY REPAIR REF EO B767-5320-27374-B. REPAIR BY NEXT C-CHECK. REINSPECT 81 DAYS 650 FLIGHT HOURS, 305 FLT CYCLES.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

POSITION 7R DAMAGED MAIN DECK FLOOR PANEL. DAMAGE IS LOCATED ON 2ND FLOOR PANEL INBD FROM RT. 38 INCHES FROM AFT EDGE. DAMAGE IS 3" BY 1". MAJOR REPAIR. REMOVED FLOOR PANEL. INSTALLED FLOOR PANEL IAW MM 53-01-26-4 THRU PAR 4(8). INSTALLED TAPE TO PANEL IAW MM 53-01-06-4.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

POSITION 6C HAS A DAMAGED MAIN DECK FLOOR PANEL. DAMAGE LOCATED ON CENTER PANEL, 41 INCHES FROM FWD EDGE DAMAGE TO PANEL, 3 HOLES .5 INCHES IN DIAMETER. MAJOR REPAIR. REMOVED PANEL AND TRANSFERRED TO NRC 502193. INSTALLED TAPE AND COMPLETED INSTALLATION OF PANEL IAW MM 53-01-06-4.

Part: FLOOR PANEL — DAMAGED

FLOOR PANEL DAMAGED. FABLICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.

Part: FLOOR PANEL — DAMAGED

FLOOR PANEL DAMAGED AFT EDGE CTR OF THE PANEL. FABRICATED FLOOR PANEL IAW EOB767-5320-9693-H AND REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPS CHECKED OK.

Part: FLOOR PANEL — DAMAGED (BS 1210-1270)

FLOOR PANEL MAIN DECK DAMAGED PANEL LOCATED APPROX STA 1210 TO 1270. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (BS 680-764)

FLOOR PANEL MAIN DECK DAMAGED LOCATED APPROX STA 680 TO 764. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.

Part: PANEL — DELAMINATED (RT WING AILERON) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, RT WING INBD AILERON L/E LWR PANEL FOUND DAMAGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 49.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE: C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 49.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, NR 2 PYLON - ACCESS PANEL 442AL CUTOUT SKIN CRACKED APP. 2 " LONG. NR 2 PYLON ACCESS PNL 442AL CUTOUT SKIN REPAIRED IAW R54-54-36993 & 767-5430-42012, CRACK LENGTH 2", CRACK STOP AT FASTENER HOLE, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL AMS4911-0090IN AS EXTERNAL REPAIR DOUBLER. REPAIR SIZE IS 12" X 9.75"

Part: FLOOR PANEL — PUNCTURED (BS 1114-1197) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 5 PUNCTURES AND 9 DENT MARKS AT STA 1114 TO 1197+22 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (BS 412-540) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 7 PUNCTURES AND 6 DENTS MARKS AT BS 412 TO 540 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (BS 893-932) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 6 PUNCTURES AND 7 DENT MARKS AT STA 893 TO 932 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 6 PUNCTURES AND 5 DENT MARKS AT STA731 TO 764 L77 TO L88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 4 PUNCTURES AND 6 DENT MARKS AT STA930 TO 975 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR VERTICAL STIFFENER AT STA 785.9, LBL 32.94, TOP AREA FOUND CRACKED. STIFFENER REPAIR IAW RS 57-10-36983 REV A & EO B767-5710-41964-A AT STA 785.9 LBL 32.94 ORG MAT'L BAC1518-749-2024T3511 CRK LENGTH 2" CUT OFF LENGTH 16.5" REPAIR CLASSIFIED AS MAJOR REPAIR, WITH MAT'L BAC1518-749-2024T3511 AS REPLACEMENT SECTION, 2024T351-0250IN & 2024T3-0100IN REPAIR STRAP & 7075T651 BARE 0250IN REPLACED CLEVIS PLATE.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, EMP - LT VERT STAB AUX SPAR TO FRONT SPAR FIXED PNL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 3, REV.49. REF RS R55-31-36990, REV A AND EO B767-5530-41990-A.

Part: RIB — CRACKED (RT WING) · airframe 37,781 hrs · 11,738 cycles

INSPECTION TYPE:C, RT WING - INBD AILERON INBD HINGE BEARING SUPPORT RIB AFT FLANGE FOUND CRACKED. RT WING - INDB AILERON HINGE SUPPORT RIB AFT FLANGE REPAIRED IAW HX RS NR R57-51-36986, REV A AND EO NR B767-5740-41962-A, ORG MAT'L DIE FORGING 7075-T73 CRACK LENGTH 1.5" FINAL CUTOUT SIZE IS 1.8 X 0.90 THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AND 10133-2001-7075T6511 AS REPAIR CLIP, REPAIR SIZE IS 1.5" X 2".

Part: WARNING LIGHT — ILLUMINATED (EQUIP COOLING)

INSPECTION TYPE:E, TOP ATB DUE TO FWD EQUIPT OVERHEAT. RAN CHECK LIST & FWD EQUIPT OVERHEAT EICAS MESSAGE CAME BACK ON. THEN GOT R FMC FAIL. PERFORMED T/S IAW FIM 21-58-00 FIG 115. PERFORMED T/S IAW FIM 28-58- 00, FIG 105. ALL CHECKS PASS OK. CHECKED CONICAL SCREEN ON FAN SUPPLY. FOUND CLEAR. NO DAMAGE TO DUCTING. OK FOR SERVICE.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A DAMAGE TO FLOOR PANEL AT 7 RT REF D412512 EDGE BAND DAMAGE. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POS 6 DAMAGED. REPAIRED PER EO B767-5320-34684-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POS 7R DAMAGED. REPAIRED PER EO B767-5320-34683-A.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5 REV 43.

Part: STIFFENER — DEFORMED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C BULK CARGO - STA 1480 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT LBL 9. BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT LBL 9.

Part: STIFFENER — DEFORMED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C BULK CARGO STA 1461 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1461 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C WING CENTER SECTION FWD BULKHEAD VERTICAL STIFFENER FOUND CRACKED JUST AT RBL 10, WL 195. CRACK 3.75 INCH LENGTH. WING CTR SECTION FWD BULKHEAD STA 785.9 WL 195 RBL 10 VERTICAL STIFFENER REPAIRED AS PER HX RS R57-11-36287 REV B AND UPS EO B767-5710-32138-B THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MAT'L 2024T351-0250 IN AND 2024T3-0100 IN FOR REPAIR LENGTH 19.25 APPROX.

Part: STIFFENER — DEFORMED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C BULK CARGO - STA 1502 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1502 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:6C MEC - MAIN DECK FLOOR SUPPORT ATT STIFFENER FOUND CRACKED JUST AT STA 246 RBL 10 - RBL 11. MEC - MAIN DECK FLOOR SUPPORT ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT STA 246 RBL 10 - RBL 11.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP LWR PNL 555EB FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.

Part: STIFFENER — DEFORMED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C MEC - BS 246 CABIN FLOORBEAM AFT FACE ATT CLIP CRACKED AT LBL 50 (CRACK 1 INCH LENGTH). MEC - BS 246 CABIN FLOORBEAM AFT FACE ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT LBL 50.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C MEC STA 246 CABIN FLOORBEAM FWD FACE ALTERNATE L/G ELECT ACT SUPPORT ANGLE CRACKED AT LBL 25 (CRACK 0.625 INCH LENGTH). MEC STA 246 CABIN FLOORBEAM FWD FACE ALTERNATE L/G ELECT ACT SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: FITTING — CRACKED (LT WING) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP FOUND CRACK. CRACK 0.75 INCH LENGTH. LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE I/B AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-04) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER T/E MID AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-02) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE MID AREA THE EXISTING REPAIR PATCH (REF SURVEY SEQ 319-W3-03) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C LT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FITTING FOUND CRACKED. CRACK 1.25 INCH AND 1.5 INCH LENGTH. LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 SHT 1 TO 5 REV 43. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075T6511, REPAIR SIZE IS 2 INCH X 2 INCH.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C RT WING NR 7 SLAT LWR CLOSURE PANEL I/B AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W4-01) DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.

Part: SUPPORT — CRACKED (FWD CARGO BAY) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 480.75 DOOR SILL BALLMAT PANEL FOUND CRACKED. CRACK 3.75 INCH LENGTH. FWD CARGO COMPT STA 480.75 DOOR SILL BALLMAT PANEL SUPPORT REPAIRED AS PER HX RS R53-00-36286 REV B AND UPS EO B767-5300-32787-A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2 SECOND FLOORBOARD FROM RIGHT STATION 412 .5 INCH PUNCTURE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 32,679 hrs · 10,077 cycles

INSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2, FWD RIGHT CORNER OF RIGHT O/B PANEL AT STN 412 (PUNCTURE ABOUT .75 INCH). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

POSITION 10 L HAS A HOLE 1 INCH IN DIA IN THE FWD O/B CORNER (DEFERRAL 390713). TRANSFERRED TO NRC 353656. VERIFIED FABRICATION OF NEW PANEL PER EO B767-5320-9693-E, APPX B, STEPS 3-6. OK TO INSTALL FLOORBOARD. INSTALLED PANEL ON L/P 012206 THIS CLEARS D390713

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 8R HAS 1 INCH DIA HOLE I/B AFT CORNER 2 HOLES 1 INCH DIA. REPAIR PER EO B767-5320-32410-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 2R HAS DAMAGE. EXISTING REPAIR DAMAGED 1" X 2" UPPER SKIN AND CORE DAMAGED IN THE AFT POSITION OF AN EXISTING REPAIR LOCATED 2 INCHES FROM AFT EDGE. EXISTING REPAIR IS 4" X 4". REPAIR PER EO B767-5320-32411-A.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOORBOARD DAMAGED. REPLACED FLOORBOARD IAW EO B767-5320-9693-E.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOORBOARD DAMAGE. FABRICATED NEW PANEL IAW EO B767-5320-9693-E.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 2R HAS 1 INCH HOLE, 2 INCHES AFT OF THE CENTER LOCK, 1 INCH HOLE 2 INCHES AFT OF FWD EDGE OF PANEL 6 INCHES FROM RT EDGE, .75 INCH HOLE AFT OF FWD EDGE OF PANEL 3 .5 INCH FROM EDGE. REPAIR PER EO B767-5320-32412-A.

Part: THERMAL SWITCH — INOPERATIVE (LT BLEED DUCT)

INSPECTION TYPE:ETOP ATB - DUCT LEAK LIGHT ILLUM. EICAS MSG: LEFT BLEED DUCT LEAK DISPLAYED. FUEL DUMPED. REPLACED M691 CONTROL CARD PER MM 26-10-01-4. REPLACED S236 THERMAL SWITCH PER MM 26-18-01-4. REMOVED AND REPLACED S237 THERMAL SWITCH PER MM 26-18-01-4.

Part: CAP — CRACKED (SPOILER ACTUATOR)

INSPECTION TYPE:N/A ATB - AFTER TAKEOFF RECEIVED CTR HYD QTY LIGHT FOLLOWED BY LOSS OF CENTER HYD PRESSURE. QTY INDICATED .08 IN CENTER SYSTEM. FOUND NR 3 SPOILER ACT LEAKING FROM FILTER CAP. REPLACED NR 3 SPOILER PCA FILTER CAP AND PACKING.

Part: TRANSMITTER — INOPERATIVE (TE FLAPS)

INSPECTION TYPE:ETOP CLEARING THE RUNWAY FLAP ASSY MESSAGE DISPLAYED FOR 3-4 SECONDS THEN CLEARED. REMOVED AND REPLACED NR 1 T/E FLAP POSITION TRANSMITTER IAW MM 27-51-45-2. OPS CHECK GOOD.

Part: CONNECTOR — CORRODED (TE FLAP XMITER)

INSPECTION TYPE:ETOP BLOCK TURN BACK DUE TO EICAS MSG FLAP/SLAT ELEC DISPLAYED. BITE CHECK FSEU-FAULT-1 LT O/B TRANSMITTER. FOUND CORROSION IN CONNECTOR. CLEANED. OPS CHECK PER MM 27-58-00-5. CHECKED OK.

Part: PUMP — LEAKING (LT ENG SCAV OIL)

INSPECTION TYPE:ETOP LEFT ENGINE OIL QTY DECREASE IN FLIGHT, DIVERSION TO CTS EMERGENCY DECLARED. FOUND OIL LEAKING FROM LT ENGINE SCAV OIL PUMP OUTLET PORT TO THE OIL PRESS TRANSMITTER, R/R LUB AND SCAV OIL PUMP ASSY AND REDUCER-TUBE AND OIL LEAK CHECK OK WITH ENG RUN PER MM79-21--03

Part: LIGHT — INOPERATIVE (COCKPIT)

EXTERIOR EMERGENCY LIGHT INOP. RELAMPED AND TESTED PER MM 33-51-16-2, CHECKED OK.

Part: SHUNT — FAILED (RT ENGINE EGT)

INSPECTION TYPE:IN PILOT REPORT - RT ENG EGT FLUCTUATES. INSPECTED CONNECTIONS ON THERMOCOUPLES AND CONNECTIONS ON JUNCTION BOX. RAN RT ENG ALL INDICATIONS NORMAL AT THIS TIME. REMOVED AND REPLACED EGT SHUNT.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN)

INSPECTION TYPE:ETOP PILOT REPORT PRESSURIZATION AUTO 1 DID NOT INITIATE AT FL 370 DESCENDING INTO ONT. MANUAL PRESSURIZATION INITIATED AT FL 200. PRESSURIZATION AUTO 2 ON DEFFERAL. REMOVED AND REPLACED OUTFLOW VALVE, VALVE CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT)

INSPECTION TYPE:ETOP LT ENGINE POWER FLUX AT A CONSTANT THRUST SETTING. BOTH CLB 2 AND CLB PWR SETTING. NOTICEABLE YAW IN ADDITION TO ALL ENG INDICATION FLUX. REPEAT WRITE UP SEE CONTROL NR 9827042 FOR PREVIOUS WRITE UP. REPLACED N1 SENSOR PERFORMED ENG RUNS AND L PIMU CHECK OPS CHECK OK PER MM 77-12-01. P/N 8TJ163AAB1 ON AND OFF S/N OFF GDBA0800 ON 1274F.

Part: ENGINE — MALFUNCTIONED (LEFT)

INSPECTION TYPE:ETOP LEFT ENGINE POWER FLUCTATES AT A CONSTANT SETTING (THRUST). CONDITION WAS INTERMITTENT ON CLIMB-OUT IN BOTH CLB 2 AND CLB PWR. N1,EGT,N2, AND FUEL FLOW ALL FLUXED WITH NO POWER SETTING CHANGE. PERFORMED BITE CHECK PER FIM 73-21-00 COMBINED WITH ENGINE RUNS. NO STATUS MSG OR CURRENT FAULTS.

Part: SWITCH — FAILED (LT VOR PANEL)

VOR FREQ DISPLAY DOES NOT RESPOND PROPERLY TO SELECTOR OPERATION. WHEN TOGGLING THE AUTO/MAN SELECTOR SWITCH, SWITCH OPERATION FROZE AN ELECTRICAL BURNING SMELL WAS NOTICED BY ALL CREW MEMBERS. AUTO/MAN SWITCH FROZE. REMOVED AND REPLACED CAPT'S VOR CONTROL PANEL, OPS CKS GOOD PER MM 34-51-02 PN/ON 285 T0554-5 OFF 285T0554-5 SN/ON D02419 OFF D02757.