N220CY

Part: WARNING MESSAGE — ILLUMINATED (ZONE 100) · airframe 101,517 hrs · 19,363 cycles

DURING TAXI OUT, EICAS MESSAGE CARGO A/C CONT.ILLUMINATED, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX THEN DEFERRED FWD CARGO A/C SYSTEM IAW MEL 21-28-1 ACCOMPLISH MAINT. PROCEDURE IAW MEL 21-28-1 PLACARD INSTALLED MBCB 4/26/26 A/C REMAINS ETOPS 180. AND RETURNED A/C TO SERVICE.

Part: INDICATOR — FLUCTUATES (ZONE 200) · airframe 101,081 hrs · 19,189 cycles

ON INITIAL CLIMB FROM KCVG STATNDY ATTITUDE INDICATOR BECAME ERRACTIC AND UNRELIABLE AC RETURNED TO FIELD AND RETURNED TO BLOCKS ,MTX GROUNDED AC .MTX TROUBLE SHOT AND REMOVED AND REPLACED THE STBY INTEGRATED INDICATOR REF B767 AMM SUPPLEMENT 34-20-00. ALL OPS NORMAL.. MTX RETURNED AC TO SERVICE .

Part: SEAL — BROKEN (FIRST AID KIT) · airframe 100,923 hrs · 19,109 cycles

DURING SERVICE CHECK SECURITY SEAL MISSING ON FIRST AID KIT. INVENTORY NON-COMPLIANT. MTX REMOVED AND REPLACED FIRST AID KIT IAW B767 AMM 25-64-03. AC COMPLIANT,

Part: ELEVATOR — MALFUNCTIONED (ZONE 200) · airframe 100,698 hrs · 19,010 cycles

DURING CRITICAL CHECK, RT ELEVATOR INDICATION WAS 2/3 FROM TOP AND BOTTOM. LEFT ELEVATOR INDICATION WAS NORMAL. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE DEFERRED RT ELEVATOR INDICATION AS PER MEL 27-08-1 MBCB 08-02-2025. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE DETECTOR — FALSE ACTIVATION (ZONE 100) · airframe 100,575 hrs · 18,935 cycles

AFT CARGO FIRE MESSAGE DURING TAKE-OFF ROLL AT 100 KNOTS, ABORT ACTIVATED, (ATO) MSG EXTINGISHED ON TAXIWAY - (CREW MENTIONED THE BRAKE TEMPS WERE NORMAL). A/C RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED IAW MEL ABX-26-16-1. FAK INSPECTED FOR POSSIBLE SOURCES OF FIRE. PLACARD INSTALLED. INSPECTED FOR FIRE. NO EVIDENCXE FOUND. A/C RETURNED TO SERIVCE. A/C REMAINS NON ETOPS.

Part: START VALVE — INOPERATIVE (NR 2) · airframe 100,528 hrs · 18,910 cycles

DURING TAXI OUT WHILE STARTING #2 ENGINE ,#2 ENGINE START VALVE WILL NOT OPEN DURING START. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED #2 START VALVE IAW MEL ABX-80-00-2-1.AC RELEASED NO ETOPS .AND RETURNED A/C TO SERVICE.

Part: OIL SYSTEM — LOW (ZONE 400) · airframe 100,486 hrs · 18,889 cycles

DURING TAXI OUT ON ENGINE START, RT ENGINE QUANTITY WAS 9. A/C RETURNED TO GATE (BTB). SERVICED RT ENGINE IAW B767 AMM 12-13-01. VERIFIED OIL CAP AND ACCESS PANEL WERE CLOSED. RETURNED A/C TO SERVICE.

Part: ELEVATOR — UNKNOWN (ZONE 600) · airframe 100,478 hrs · 18,884 cycles

DURING TAXI OUT, RIGHT ELEVATOR ONLY SHOWS ~ 80% TRAVEL UP AND DOWN. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED IAW MEL AMM 27-38-00. RETURNED A/C TO SERVICE. AMENDED: MTX DEFERRED IAW MEL AMM 27-38-00, AMENDED TO: MTX DEFERRED IAW MEL-ABX-27-08-1.

Part: START VALVE — MALFUNCTIONED (ZONE 500) · airframe 100,344 hrs · 18,793 cycles

DURING TAXI WHILE STARTING RH ENGINE ,R STARTER CUTOUT AFTER STARTING RIGHT ENGINE.AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC . TROUBLE SHOT AND PERFORMED CONTINUITY CHECK OF RH ENG PER WDM 80-11-11 FOUND VLV STUCK ELECTRICALLY, REMOVED AND REPLACED RH ENG STARTER CONTROL VALVE PER AMM 80-11-02. PERF RH ENG RUN PER AMM 71-00-00. OPS OK GOOD. A/C REAMAINS NO ETOPS.AND RETURNED AC TO SERVICE.

Part: APU — FAULTED (ZONE 100) · airframe 100,178 hrs · 18,723 cycles

APU AIR PRESSURE LOW DURING START (11 PSI)DURING LH ENGINE START HUNG AT 25% N2 ON TAXI OUT. AC RETURNED TO GATE (BTB) . MTX GROUNDED AC AND DEFERRED APU IAW MEL ABX-49-11-1A ACCOMPLISHED MPM PLACARD INSTALLED AND AC REMAINS NO ETOPS MBCB 12-20-2024 AC RETURNED TO SERVICE .

Part: START VALVE — MALFUNCTIONED (ZONE 600) · airframe 99,654 hrs · 18,484 cycles

"DURING PUSHBACK AFTER SELECTING RIGHT ENGINE TO GROUND, R ENG STARTER EICAS MESSAGE APPEARED WITH NO ENGINE ROTATION A/C RETURNED TO GATE AND MTX GROUNDED AC . DEFERRED THE START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1 . RETUNED AC TO SERVICE . AIR CRAFT DEPARTED , NEXT LEG REMOVED AND REPLACED R/H ENGINE STARTER CONTROL VALVE IAW B767 AMM 80-11-02. OPS CHECK AND LEAK CHECK GOOD. NO REACTIVATION PROCEDURE APPLIED. PLACARD REMOVED. A/C RELEASED ETOPS 180. REF LP 38918-96/1"

Part: WARNING MESSAGE — ILLUMINATED (FWD CARGO AIRCON) · airframe 99,303 hrs · 18,309 cycles

FWD CARGO AC CONTROL STATUS MESSGE DURING TAXI , AC RETURED TO THE GATE AND MAINTENANCE GROUNDED AC AND DEFERRED THE FWD CARGO AIR COND.SYSTEM IAW ABX 21-28-1 AND RETURNED AC TO SERVICE . AC DEPARTED.

Part: EEC — FAULTED (RIGHT) · airframe 98,887 hrs · 18,124 cycles

ON ENGINE START, STATUS MESSAGE: R ENG EEC C1. DEFERRED PER ABX-73-21-1-4.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 98,355 hrs · 17,880 cycles

TWO ENGINE SURGES DURING LEVEL OFF. COULD NOT DETERMINE WHICH ENGINE WAS. (AUTO EVENT SHOWS LEFT ENGINE) AC GROUNDED AND BEING WORKED THIS SDR WILL BE AMENDED WHEN COMPIED WITH. WORK DONE IN CVG .REMOVED AND REPLACED RH ENGINE FOR DAMAGE FOUND DURING BORO. DURING ENGINE RUNS LH ENGINE SURGED AND REPLACED LH ENGINE IP CHECK VAVE . OPS CHECK GOOD AFTER ENGINE RUNS .AC RETURNED TO SERVICE "NO ETOPS ".

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 98,329 hrs · 17,865 cycles

L. ENG HUNG START. FOLLOWED CHECKLIST- NO HELP. 2ND START ALSO HUNG.DURING TAXI AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE .FOUND LOOSE CONNECTOR ON L ENGINE RIGHT HPC SECONDARY FLOW CONTROL SOLENOID. RESECURED PER AMM 75-33-04. ENGINE IDLE RUN PER AMM 71-00-00 OK. A/C REMAINS. NO ETOPS. AC RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 98,017 hrs · 17,732 cycles

RT FWD FUEL PUMP EICAS MESSAGE & RT FWD PRESSURE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE. T/S AND VERIFIED PRESS LIGHT CONNECTION AND CLEARED. NO EICAS MSG OR PROBLEM FOUND. VERIFIED CONNECTION IN OVERHEAD PANEL WITH PUMP RUNNING WITH NO DEFECT. AMM 28-22-03. AIRCRAFT RETURNED TO SERVICE

Part: SKIN — DAMAGED (ZONE 300) · airframe 97,652 hrs · 17,591 cycles

DURING AIRCRAFT C-CHECK IN GSO (GREENSBORO, NORTH CAROLINA), HAECO MAINTENANCE DISCOVERED LIGHTNING STRIKE DAMAGE AND PREVIOUS BLENDOUT REPAIRS ON THE RIGHT HAND / LEFT HAND TAILCONE SKIN. SEE FIGURE 1 FOR DETAILS. THE DAMAGE WAS EVALUATED PER REF /C/ AND FOUND TO BE BEYOND PUBLISHED LIMITS. THE SKIN IS MADE FROM 321 ANNEALED CRES X 0.025” PER REF /B/. THE TAILCONE ASSEMBLY IS CLASSIFIED AS SECONDARY STRUCTURE PER REF /A/. HAECO ENGINEERING CONTACTED FLIGHT VEHICLES CONSULTING INC. REQUESTING FURTHER EVALUATION AND REPAIR APPROVAL. REPAIRED PER ABX-REA-5385-65044-00

Part: SKIN — CRACKED (ZONE 100) · airframe 97,652 hrs · 17,591 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, DENT AND CRACK DAMAGE WAS FOUND ON THE FUSELAGE SKIN P/N 148T3251-4. THE DAMAGE IS LOCATED AT STA 1710.5 BELOW THE S-36L SKIN LAP JOINT WITHIN A SKIN CHEM MILLED POCKET WITH A THICKNESS OF 0.056-INCH. THERE ARE NO APPLICABLE REPAIRS IN THE SRM FOR THIS DAMAGE LOCATION. THE REPAIR ACCOMPLISHED IS ACCEPTABLE AND HAS STAGE 1 APPROVAL FOR STATIC STRENGTH PER FAA FORM 8110-3 SIGNED BY ROBERT MANASHI, DER T 876272412, DATED 08-JUN-2023. REPAIRED PER ABX-REA-5385-65041-00.

Part: SKIN — FAULTY (ZONE 100) · airframe 97,652 hrs · 17,591 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MX WAS REQUIRED TO RE-INSPECT AND REPLACE (5/32”) BLIND FASTENERS IN AN EXISTING REPAIR DESCRIBED IN ABX “WATCH ITEM” WI-220CY-06202022. UPON REMOVAL OF THE REPAIR AND EVALUATION, IT WAS FOUND THAT REPLACEMENT FASTENERS ARE (3/16”) SOLID RIVETS RIVET WITH REQUIRED MINIMUM FASTENER SPACING OF 0.90 INCHES AND MAXIMUM OF 1.25 INCHES PER SRM 53-00-01, REPAIR 29 OR REPAIR 1, TABLE II. SEVERAL EXISTING SPACINGS ARE REPORTED FROM 0.86 INCH TO 0.89 INCHES. AT THE NEW FASTENER LOCATION, THE RECORDED SPACING WILL BE 0.780 TO 0.85 INCHES. IN ADDITION, EXISTING TRIM RADIUS AT CUTOUT IS 3/8” INCHES (UPPER LEFT) AND 7/16” (UPPER RIGHT). REFERENCE SRM REQUIRES MINIMUM TRIM RADII OF 0.50-INCHES. THE REPAIR ACCOMPLISHED IS ACCEPTABLE AND HAS STAGE 1 APPROVAL FOR STATIC STRENGTH PER FAA FORM 8110-3 SIGNED BY ROBERT MANASHI, DER T 876272412, DATED 07-JUN-2023. REPAIRED PER ABX-REA-5365-65027-00.

Part: SKIN — CORRODED (ZONE 600) · airframe 97,652 hrs · 17,591 cycles

"DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MX REPORTED CORROSION DAMAGE ON THE RH WING LOWER SKIN NO. 1 PANEL, 112T4701-4, BETWEEN RSS 852.00 AND RSS 879.30. SIX (6) FASTENERS WERE REMOVED AND AFFECTED AREA WAS BLENDED PER B767-300 SRM 51-20-01. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS PER B767-300 SRM 57-20-01, ALLOWABLE DAMAGE 1, TABLE II. THE REPAIR ACCOMPLISHED IS ACCEPTABLE AND HAS STAGE 1 APPROVAL FOR STATIC STRENGTH PER FAA FORM 8110-3 SIGNED BY ROBERT MANASHI, DER T 876272412, DATED 12-JUN-2023. " REPAIRED PER ABX-REA-5725-65040-00.

Part: FAIRING — DAMAGED (ZONE 400) · airframe 97,652 hrs · 17,591 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE NO. 2 PYLON AFT FAIRING INBOARD HYDRAULIC BAY CLOSEOUT PANEL (313T3381-212) HAS NUMEROUS DAMAGES. DUE TO THE EXTENT OF DAMAGES, MAINTENANCE OPTED TO REPLACE SEVERAL PARTS OF THE PANEL. THE DRAWING 313T3381-212 IS BONDED /MANUFACTURED PER BAC5514-570 (DRAWING FL 1). MAINTENANCE CANNOT ACCOMPLISH THE BAC5514 ENTIRETY AND REQUESTED TO REPLACEMENT PARTS AND BOND PER B767- 300 SRM 51-70-10 (SRM 54-53-70). REPAIRED PER ABX-REA-5450-65039-00

Part: SEAL DEPRESSOR — GOUGED (ZONE 400) · airframe 97,652 hrs · 17,591 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED GOUGE DAMAGE ON THE NO. 2 STRUT, OUTBOARD FIRE SEAL DEPRESSOR (113T4011-14). THE POST-BLEND MEASUREMENT IS 0.051 REMAINING MATERIAL FROM INITIAL THICKNESS OF 0.075-INCH THICK (MEASURED). NO PUBLISH APPROVED DOCUMENT IS AVAILABLE FOR ALLOWABLE DAMAGE LIMITS OR REPAIR FOR THE SUBJECT PART. REPAIRED PER ABX-REA-5400-65043-00

Part: FLAP — DENTED (ZONE 600) · airframe 97,652 hrs · 17,591 cycles

WHILEIN C-CHECK IN HAECO MAINTENANCE DISCOVERED R/W I/B FLAP, AFT FLAP TOP SIDE HAS A DENT. MARKED IN RED. EVALUATED DENT ON R/W I/B FLAP AFT FLAP UPPER SURFACE LOCATED 59.25" FROM O/B EDGE 14.5" FROM THE T/E. DENT MEASURE 3.1" LONG, .7" WIDE, .0075 DEPTH IAW ABX B767-300 SRM 57-53-01 FIG 101 NOTED C. REPAIRED DAMAGE IAW ABX B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-10 REPAIR 3 & 4. RESTORED FINISH IAW ABX 767-300 SRM 51-21-10.

Part: PIN — OUT OF TOLERANCE (MAIN CARGO DOOR) · airframe 97,652 hrs · 17,591 cycles

MDCD LATCH CAM PIN #'S 12,10, 6,4,2 AND FAILED DIMENSION CHECK WHILE IN C-CHECK HAECO AMERICAS. MAINTENANCE REPLACED MDCD LATCH CAM PINS IAW 767 AMM 52-32-11. OPERATIONAL CHECKED GOOD, NO ADJUSTMENTS REQUIRED.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 97,652 hrs · 17,591 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS,MAINTENANCE FOUND FWD CARGO DOOR CUTOUT, LOWER TORQUE BOX WEB UPPER SURFACE IS CORRODED FROM APPROX STA 515-544 RBL 25 - 35 (MARKED). REMOVED CORRODED TORQUE BOX WEB, FABRICATED NEW WEB AND REINSTALLED NEW WEB IAW B767-300 SRM 51-40-02, 51-40-05, 51-20-01, AMM 51-21-10, & BAC DWG 143T5014 REV B. REPAIRED PER ABX-REA-5330-65042-00 AND REO-G24485 REV IR

Part: PUMP — OVERHEATED (LEFT ENGINE) · airframe 97,484 hrs · 17,530 cycles

L PRIM HYD OVHT DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED CASE DRAIN FILTER I/A/W AMM 29-11-17. REMOVED AND REPLACED EDP MODULE FILTER I/A/W AMM 29-11-15. REMOVED AND REPLACED L EDP I/A/W AMM 29-11-05. OP'S CHECK GOOD. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — DEFECTIVE (LEFT ENGINE) · airframe 97,398 hrs · 17,501 cycles

LEFT ENGINE BLEED OVERHEAT EICAS MESSAGE PERFORMED QRH PROCEDURE, LIGHT EXTINGUISHED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE AS PER FIM 36-10 F/T 867. FOUND PRSOV FAULTY, REMOVED AND REPLACED LEFT ENG. PRSOV ASSY. IAW AMM 36-11-09, NO CLEAR LEAKS NOTED, PART EFFECTIVITY VERIFIED. A/C RETURNED TO SERVICE. AICRAFT DEPARTED AND HAD L ENG BLEED LIGHT ILLUMINATED ASSOCIATED WITH L PACK OFF.CREW ELECTED TO RETURN TO MIA AND LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED PRESSURE REGULATIONG VALVE CONTROLLER IAW AMM 36-11-18 PERFORMED ENGINE RUN UP. IAW AMM 70-00-00 OPS CHECK NORMAL. PART EFFECTIVITY VERIFIED A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — DEFECTIVE (ZONE 100) · airframe 96,414 hrs · 17,198 cycles

R PACK OFF EICAS MESSAGE APPEARS DURING TAXI, UNABLE TO TROUBLESHOOT VIA QRH, MEL NOT CREW DEFERRABLE ETOPS 180, IN AUTO POSITION OR N POSITION PACK OFF STAYS ILLUMINATED AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED FLOW CONTROL CARD ASSEMBLY (M864 AT P50 PANEL) IAW B767 AMM 21-51-09, NO HELP. DEFERRED PER 21-51-3-1. PLACARDS INSTALLED. MBCB 10/30/2022. MEL MAINTENANCE PROCEDURE COMPLIED WITH . NO DEACTIVATION PROCEDUCE - LEFT PACK AUTO DEFERRED. AIRCRAFT RETURNED TO SERVICE

Part: SWITCH — STICKING (STAB TRIM) · airframe 96,061 hrs · 17,110 cycles

DURING T.O. ROLL, AIRSPEED ,80KTS. UNSCHEDULED STAB TRIM EICAS/ MASTER CAUTION. ABORTED TAKE-OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENACE. MAINTENANCE REMOVED + REPLACED ALT STAB TRIM SWITCH ASSY PER B767 AMM 27-41-03 OPS NORMAL NO DEFECTS.AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTED (STAB TRIM) · airframe 95,956 hrs · 17,076 cycles

ON TAKEOFF ROLL EICAS MESSAGE "UNSCHD STAB TRIM" EXECUTED SLOW SPEED ABORT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED MCDP TEST 65 C/W PER FIM TASK 22-04 FT 811. FAILED TEST. RH STAB TRIM AIL MODULE ASSY REPLACED IAW AMM 27-09-00 + TESTED SATIS. AIRCRAFT RETURNED TO SERVICE.

Part: EICAS — FALSE INDICATION · airframe 95,838 hrs · 17,055 cycles

T.O. WARNING ALERT ON TAKE OFF ROLL WITH UNSCHED STAB TRIM EICAS MSG W. ASSOCIATED MASTER CAUTION LIGHTS AND TAKE OFF WARNING HORN (STAB TRIM DISCRETE LIGHT ILLUMINATED) THRUST LEVERS ADVANCED, THRUST BUTTON SELECTED, AUTO-THROTTLES ADVANCED THRUST LEVERS, AND AIRCRAFT ACCELERATED TO APPROX 20 KTS WHEN TAKE-OFF WAS ABORTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET STAB TRIM AILERONS LOCKOUT CBS.BITE TEST CARRIED OUT IAW AMM 22-00-00 TESTED SATIS. AIRCRAFT REMAINS ETOPS 180 AND CAT IIIB STATUS.AIRCRAFT RETURNED TO SERVICE.

Part: NONE — DEFECTIVE (ZONE 100) · airframe 95,631 hrs · 17,011 cycles

SLOW DEPRESSURIZATION OCCURRED AT 36,000 FEET. CONTROL OF CABIN PRESSURE REGAINED SOMEWHERE BETWEEN 20,000 FEET. AIRCRAFT DIVERTED TO JAX WITH NO ADDITIONALPROBLEMS. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER #2 IAW AMM 21-31-02, ALSO AS A PRECAUTIONARY R&R CABIN PRESSURE SELECT PANEL IAW AMM 21-31-01; PERFORMED OPERATIONAL CHECK UNABLE TO DUPLICATE THE FAULT AT THIS TIME, OPS CHECK NORMAL. AIRCRAFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 95,493 hrs · 16,982 cycles

AT FL380 CABIN ALT WARNING AND HORN WENT ON, CABIN ALT APPROX 12000 FT MODE SELECT AUTO 1 CREW ELECTED TO PERFORM AN AIR TURN BACK. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT GROUNDED BY MAINTENANCE . MAINTENANCE DEFERRED PRESSURIZATION SYSTEM CONTROLLER #1 IAW MEL 21-31-1A. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (ZONE 100) · airframe 95,420 hrs · 16,966 cycles

UNSCHED STAB TRIM EICAS MESSAGE ON TAKEOFF ROLL AT APPROX 65 KTS. ABORTED TAKEOFF. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT SYSTEM. NO FAULT ON SAM L/H OR R/H FOUND R/H STCM FAULT RESET AND MAINTENANCE PROCEDURE 27-91-2 PERFORMED TESTED OK AIRCRAFT REMAIN CAT IIIB. AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 95,336 hrs · 16,941 cycles

AFT CARGO OVHT DURING TAXI, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED PER MEL 21-40-2-1A2. MBCB 05/24/2022. AIRCRAFT REMAINS ETOPS 180. NO MX PROCEDURES REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 94,201 hrs · 16,617 cycles

ON TAXI OUT IT WAS FOUND THAT LOW SYSTEM HYDRAULIC PRESSURE LIGHT INOP, AIRCTAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RELAMPED & DIODE CARD CLEANED- IAW AMM 20-00-00 SYSTEM SERVICEABLE. AIRCRAFT RETURNED TO SERVICE

Part: SURGE VALVE — STICKING (APU) · airframe 94,014 hrs · 16,570 cycles

DURING LEFT ENGINE START ONLY, DUCT PRESSURE GAUGE FLUCTUATIONS 10-30PSI AND ONLY ABLE TO ACHIEVE 16% N2 VERY SLOW TO SPOOL, NO PARAMETERS EXCEEDED. RT START NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED K10247 AND K10250, L & R ENG START 2 RELAYS. REMOVED AND REPLACED APU SURGE VALVE IAW B767 AMM 49-53-01. OPS CHECK GOOD. DUCT PRESSURE STAYED AT 38PSI THROUGHOUT START AND L ENG N2 2890 AT MAX MOTOR. OPS CHECK GOOD. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 94,008 hrs · 16,566 cycles

APU PNEUMATICS DROP ALL CYCLE BETWEEN 15-20 PSI DURING LEFT ENGINE START.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE APU PER MEL 49-11-1A. PLACARD INSTALLED; AIRCRAFT REMAINS NON ETOPS.AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 93,675 hrs · 16,466 cycles

F/O WINDOW OPENED DURING TO ROLL. CREW ABORTED TAKE OFF, BRAKE TEMP LIGHT ON AFTER 80 KT ABORT, WHEELS #2 AND #3 BOXED AND SHOWING 5 ON EICAS. AIRCRAFT RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED BY MAINTENANCE, MAINTENANCE INSPECTED ALL LINKAGES, DETENT AND WINDOW MECHANISM AS PER AMM 56-11-04 OPEN AND CLOSED WINDOW PER AMM 56-11-01, WINDOW IS CLOSED. LATCH AND SECURED. APPLY PRESSURE FOR DOUBLE CHECK,WINDOW REMAIN CLOSED, LATCHED AND SECURED. INSPECTED BRAKE HIGH TEMP, NO DEFECT NOTED AND NO DAMAGE ON TIRES. A/C OK FOR CONTINUE SERVICE AS PER AMM 32-41-08. AIRCRAFT RETURNED TO SERVICE.

Part: STARTER — SPARKS (RIGHT ENGINE) · airframe 93,675 hrs · 16,466 cycles

R STARTER CUT OUT EICAS GROUND PERSONAL REPORTS LARGE AMOUNT OF SPARK EXITING RT ENG.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.DURING INSPECTION FOUND STARTER TO BE THE SOURCE OF SPARKS R&R STARTER R/H IAW B767 AMM 80-11-01 A/C REMAINS ETOPS 180 OPERATIONAL. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (LT HF SYS) · airframe 92,868 hrs · 16,234 cycles

LEFT HF RECEIVES BUT UNABLE TO XMIT, ALL THREE STATIONS.CREW DECIDED TO PERFORM AIR TURN BACK AS A PRECAUTION. AIRCRAFT WAS GROUNDED BY MAINTENANCE. CIRCUIT BREAKER WAS CYCLED IAW AMM 23-11-715-203, OPS NORMAL. OVERWEIGHT LANDING PERFORMED. AIRCRAFT RELEASED ETOPS 180.

Part: STRAP — CORRODED (DOOR SILL) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C-CHECK AFT CARGO SILL BEAM UPPER STRAP WAS FOUND TO HAVE CORROSION FROM STATION 1263 TO 1351. REPLACED CHORD IAW B767-300 SRM 51-40-05 AND 51-40-02

Part: BEAM — CORRODED (NLG WW) · corrosion level 2 · airframe 92,764 hrs · 16,196 cycles

DURING C-CHECK NWW FWD FACE 'AFT LOCK LINK BEAM AT WL 147 CORRODED ON TOP RIGHT SIDE LUG BACK UO FITTING. FOUND TO BE OUT OF LIMITS, BEAM WAS REPLACED IAW B767-300 SRM 53-10-14

Part: STIFFENER — CORRODED (BS 966) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C-CHECK RH STA.966 STIFFENER WAS FOUND TO BE CORRODED. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED.

Part: SKIN — CRACKED (BS 782 S37-38R) · airframe 92,764 hrs · 16,196 cycles

DURING AIRCRAFT CURRENT C-CHECK AT AIRBORNE (TPA), MAINTENANCE DISCOVERED A CRACK IN FUSELAGE SKIN (P/N 143T3262-4) AT STA 782 BETWEEN STRINGERS 37R AND 38R. THE CRACK WAS REMOVED BY TRIMMING OUT (2.3” X 2.75”), SEE (FIGURE 1, SHEET 2). THE SKIN IS FABRICATED FROM 2024-T3 X 0.140” CLAD SHEET PER QQ-A-250/5 AND MACHINED DOWN TO 0.063”. THERE ARE NO REPAIRS FOR THE SPECIFIC LOCATION IN THE 767-300 SRM. THIS REA PROVIDES DIRECTION FOR THE REPAIR OF THE FUSELAGE SKIN AT THE SUBJECT LOCATION, AS APPROVED BY FLIGHT VEHICLES CONSULTING, INC. (FVCI).

Part: SUPPORT ANGLE — CORRODED (BS 1605 LBL64) · airframe 92,764 hrs · 16,196 cycles

DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE MAIN CABIN FLOOR PANEL SUPPORT ANGLE (P/N 368-53-16-94490-201) AT STA 1605, LBL 64. THE CORROSION WAS REMOVED BY BLENDING PER SRM 51-10-02 AND EXCEEDING 10% NOMINAL MATERIAL LOSS. THERE IS NO REPAIR DATA GIVEN IN THE IAI SUPPLEMENTAL SRM FOR THIS ANGLE. THE ANGLE IS FABRICATED FROM 7050-T7451 PLATE. THIS REA PROVIDES DIRECTION FOR THE REPAIR OF THE FLOOR PANEL SUPPORT ANGLE AT THE SUBJECT LOCATION.

Part: FAILSAFE — CORRODED (BS 505 RBL44) · airframe 92,764 hrs · 16,196 cycles

DURING C-CHECK, FOUND CORROSION ON FAIL SAFE STRAP LOWER SURFACE AT STA505 AROUND FASTENER HOLE AND SHEARED BOLT AT STA494 AT RBL44. REMOVED CORROSION AND EVALUATED AREA AT FWD. CARGO DOOR SILL FAIL SAFE STRAP LOWER SURFACE. ORIGINAL MATERIAL .200", MATERIAL REMAINING AT LOWEST POINT .138". FOUND TO BE WITHIN LIMITS PER ABX AIR ABX-REA-5331-64115-00.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 92,764 hrs · 16,196 cycles

DURING C-CHECK,MAIN CABIN SEAT TRACK HAS CORROSION AT STA 1487-1518 AT RBL 75. REMOVED CORROSION, EVALUATED AREA FOUND TO BE OUT LIMITS IAW B767-300 SRM 53-00-52. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW B767-300 SRM 51-40-02, SRM 51-40-05 AND IAI'S SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 1605 LBL 54) · corrosion level 2 · airframe 92,764 hrs · 16,196 cycles

CORROSION ON CABIN SEAT TRACK STA 1605 AND LBL 54.REMOVED CORROSION AREA ON CABIN SEAT TRACK 1605 AND LBL54, ORIG. MAT .080", MAT LOSS .024", MAT REMAINING .056". FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00-02 DETAIL VII. FABRICATE, LOCATED AND DRILLED NEW SECTION SEAL TRACK BAC 1520-2772-7150T7751 PEMCO LOT N. C829866 AND ANGLES 2 EA & STRAP. REPAIR PEMCO LOT N. AUTO-503973 AND INSTALLED REPAIR PART SECTION SEAT TRACK ANGLES & STRAP IAW B767-300 SRM 53-00-52 REPAIR 3.

Part: FAILSAFE — CORRODED (BS 955) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C-CHECK FAILSAFE STRAP AT LT STA955 REQUIRED REPAIR. REPAIR WAS COMPLETED IAW AMES EO 47207ORD03

Part: STRINGER — CRACKED (BS 413 S32R) · airframe 92,764 hrs · 16,196 cycles

DURING C-CHECK FWD CARGO COMPARTMENT,  STRINGER 32R HAS DAMAGE ON UPPER FLANGE RADIUS  AND END OF FLANGE AT STA413.REMOVED DAMAGE AND EVALUATED FWD. CARGO COMPARTMENT, STRINGER 32R AT STA. 413. FOUND TO BE OUT OF LIMITS IAW B767-300, SRM 53-00-03 NOTE A CRACKS ARE NOT PERMITTED. REPLACED WITH NEW STRINGER IAW B767-300 SRM 51-40-02 & SRM 53-00-03.

Part: PIN — WORN (CRGO DOOR LATCH) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C-CHECK,MDCD LATCH CAM PINS 4, 10 AND 12 FAIL DIAMETER MEASUREMENT CHECKS. REMOVED AND REPLACED MDCD LATCH CAM PINS 4, 10, AND 12 IAW B767-300 AMM SUPPLEMENT 52-32-00. ADJUSTMENT CHECK GOOD, NO ADJUSTMENT NEEDED.

Part: SKIN — CORRODED (RT WING) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C-CHECK, RIGHT WING UPPER SKIN AT WING TO BODY FAIRING, SKIN BELOW FWD OVERWING HATCH HAS CORROSION. CORROSION REPAIRED IAW ABX REA-5725-64113-00

Part: FLOOR SUPPORT — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 92,764 hrs · 16,196 cycles

DURING C CHECH, INTERCOSTAL FOUND CORRODED AT FS 1263-1285 RBL 21.5 OUT OF LIMITS, REPLACED IAW B767-300 SRM 51-21.

Part: WEB — CORRODED (AFT CARGO DECK) · corrosion level 2 · airframe 92,764 hrs · 16,196 cycles

DURING C CHECK, AFT CARGO DECK WEB HAS MULTIPLE AREAS OF CORROSION STA"S 1263-1280 AND RBL30 - RBL44. REMOVED CORROSION FROM AFT PIT DECK WEB IAW B767-300 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .071", REMOVED .071", REMAINING .000". OUT OF LIMITS IAW B767-300 SRM 53-00-51 FIG 101 DETAIL 2. LOCATED, DRILLED AND INSTALLED NEW WEB PART NUMBER 146T5000-169 IAW B767-300 51-40-02 AND 51-40-05.

Part: SKIN — CORRODED (LT WING) · airframe 92,764 hrs · 16,196 cycles

WHILE IN C- CHECK LH UPPER WING WAS FOUND TO BE EXFOLIATED. REPAIRED IAW ABX-REA-5725-64112-00. REQUIRES REPETITIVE INSPECTION NOT TO EXCEED 48 MONTHS.

Part: DISPLAY — INOPERATIVE (EICAS) · airframe 92,591 hrs · 16,154 cycles

LWR EICAS DISPAY INOP IN LEFT POSITION. AIR TURN BACK PERFORMED. AICRAFT GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE RIGHT EICAS COMP, THE BOTTOM EICAS DSIP. SWITCH MODULE AND THE EICAS SIGNAL CONSOLIDATION CARD IAW AMM 31-41-01, 31-41-04, AND 31-41-07 ALL OPS TESTS GOOD AT THIS TIME AIRCRAFT REMAINS ETOPS 180

Part: ISOLATION VALVE — INTERMITTENT (RT PNU SYS) · airframe 92,253 hrs · 16,063 cycles

EICAS MESSAGE RT BLEED ISO VALVE. BACK TO BLOCK, AIRCRAFT GROUNDED. DEFERRED, REMOVED/REPLACED RT BLEED ISO VALVE, IAW AMM 36-11-04. ACCOMPLISHED REACTIVATION PROCEDURES. REFERENCE CLEARING ACTION FOR DI 19878 ON L/P 38224-01/2. VERIFIED P/N 2780539-105 S/N 3108 ISOLATION VALVE INSTALLED RT POSITION EFFECTIVE FOR ETOPS, PER IPC 36-11-04-01 ITEM 60. PERFORMED SUCCESSFUL OPS CHECK OF ISOLATION VALVE, IAW AMM 36-11-04. THESE ACTIONS UPGRADE A/C TO ETOPS 180. PLACARD ROTATED TO 180.

Part: PRESSURE SWITCH — DETERIORATED (RT ENG OIL SYSTE) · airframe 92,101 hrs · 16,016 cycles

RT ENGINE OIL PRESS DISCRETE LIGHT + EICAS MESSAGE WERE ILLUMINATED AFTER ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED. REMOVED AND REPLACED LOW OIL PRESSURE SWITC,H AS PER B767 AMM 79-33-01. LEAK CHECK + OPERATIONS CHECK GOOD. AIRCRAFT REMAINS ETOPS 180 OPERATIONAL.

Part: CIRCUIT BREAKER — NOT CLOSED (COCKPIT) · airframe 91,609 hrs · 15,814 cycles

AFTER PUSH BACK FROM GATE, PRIOR TO ENGINE START LEFT AND RIGHT EEC EICAS MESSAGE DISPLAYED. AIRCRAFT PULLED BACK IN TO GATE AND WAS GROUNDED. MAINTENANCE FOUND BREAKERS ON P-6 PANEL NOT SET. RESET ALL BREAKERS, EEC INOP LIGHTS EXTINGUISHED WITH IRU'S ALIGNED. AIRCRAFT REMAINS NO ETOPS.

Part: BEARING — CORRODED (MLG TRUNNION) · airframe 91,431 hrs · 15,737 cycles

RIGHT MLG AFT TRUNNION BEARING HAS CORROSION. AIRCRAFT WAS GROUNDED WHILE IN MAINTENANCE FOR MLG CHANGE.

Part: SPLICE PLATE — DAMAGED (RT WING) · airframe 89,185 hrs · 14,663 cycles

DAMAGE ON RIGHT WING LEADING EDGE LOWER SPLICE PLATE AT LEADING EDGE STATIONS 568 AND 982. THE SPLICE PLATE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (BS 1087-1122) · corrosion level 2 · airframe 86,143 hrs · 13,310 cycles

CORROSION ON RIGHT SKIN COVERED BY SATCOM ANTENNA BETWEEN FUSELAGE BS 1087 AND 1122. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (BS 1087-1122) · corrosion level 2 · airframe 86,143 hrs · 13,310 cycles

CORROSION ON LEFT SKIN COVERED BY SATCOM ANTENNA BETWEEN BS 1087 AND 1122. SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: UNKNOWN — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 82,560 hrs · 12,046 cycles

UN-COMMANDED RAPID ROLLBACK OF BOTH ENGS TO THE IDLE POSITION, OCCURRED DURING CRUISE FLIGHT. THE AUTO THROTTLE ARM SWITCH WAS ON. THE ENG & WING ANTI-ICE SWITCHES WERE IN AUTO. THE THRUST LEVERS FOLLOWED ENGS TO IDLE POSITION. THE CREW THEN DISCONNECTED THE AUTO THROTTLES & TURNED THE ENG ANTI-ICE SWITCH TO ON. COMPLIED WITH THE ENG LIMIT OR SURGE OR STALL CHECKLIST. RESTORED NORMAL THRUST, RECONFIGURED SWITCH POSITIONS TO NORMAL & THE ENGS CONTINUED TO OPERATE WITH NO FURTHER ABNORMALITIES. ACCOMPLISHED MAINTENANCE CONTROL DISPLAY PANEL TESTS 52, 57 & 60 IAW FIM 22-04-FAULT TREE 802. NO CAUSE OF UN-COMMANDED ROLLBACK OF BOTH ENGS WAS FOUND.

Part: ANGLE — CRACKED (LT WING) · airframe 79,751 hrs · 11,142 cycles

ANGLE BRACKET FROM TOP OF FRONT SPAR TO INBD LE STRUCTURE ABOVE SLAT PDU CRACKED. R & R ANGLE BRACKET ON LE FRONT SPAR. INSTALLED TWO PA FASTENERS ON SPAR THROUGH FUEL TANK, LEAK CHECKED FASTENERS. REINSTALLED ACCESS PANELS IAW SRM 51-40-02, AMM 28-11-00 & AMM 27-81-11. SDR INFORMATION, PART 114T1305-269 CRACKED LENGTH, .05 PART NAME ANGLE LOC LE FROM WBL 97.95. ACFT WAS GNDED.

Part: ANGLE — CRACKED (LE SLAT) · airframe 79,751 hrs · 11,142 cycles

NUMBER 7 SLAT STA LES 155.00 UPPER AT SPAR INTERCOSTAL ANGLE CRACKED. FABRICATED BRACKET FROM 2024-0-.080 PO 0036528 IAW DRAWING 114T1305. SDR INFORMATION, CRACKED 1/4 INCH, LOC RT WING LES 155.0, PART 114T1342-106, PART NAME ANGLE, SN NSN. ACFT WAS GNDED.

Part: STRINGER — DENTED (FUSELAGE) · airframe 79,751 hrs · 11,142 cycles

FORWARD LOWER CARGO STRINGER 30L IS DENTED AT BS 506. REMOVED DAMAGED SECTION OF STRINGER. REMOVED STRINGER CLIPS & SKARTIES IN REPAIR AREA. REPAIRED STRINGER IAW REA-B653-60773-MR & SRM 53-00-03 FIG 201 REPAIR 2. REINSTALLED REMOVED COMPONENTS IN REPAIR AREA. SDR INFORMATION, DENT PART NUMBER 143T4001-50 SN NSN DENT 1 INCH X .C55 DEPTH PART NAME STRINGER FS 505 TO 506 EXACT STRINGER 30L. ACFT WAS GNDED.

Part: PRINTED CKT BOARD — FAULTY (FIRE WARNING) · airframe 79,165 hrs · 10,931 cycles

STATUS MESSAGE AFTER DISPATCH: RT ENG FIRE LP1 RT ENG FIRE LP1 DISPLAYED. RT ENGINE FIRE/OVERHEAT SYS FAILED ON APPROACH. ACCOMPLISHED FIRE/OVERHEAT SYS NON NORMAL IAW QRH. R & R AFLOTS CARD 10274. OPS CHECK GOOD IAW AMM 26-10-01. PART EFFECTIVITY VERIFIED. ACFT REMAINS ETOPS 180.

Part: SKIN — DENTED (CARGO DOOR) · airframe 77,614 hrs · 10,523 cycles

BULK CARGO DOOR DENTED AT LOWER FWD CORNER. REPAIRED IAW SRM.