N351CM

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 111,569 hrs · 20,976 cycles

FOLLOWING DAILY CHECK INSPECTIONS FOUND EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE PLACED DEFERRAL 65624 MINIMUM EQUIPMENT LIST 25-63-04-01 CATEGORY C. DUE 06 SEPTEMBER 2025. REMOVED AND REPLACED FLASHLIGHT BATTERY PER B767 AMM 25-64-00. OPERATIONAL CHECK GOOD. DEFERRAL 65624 CLEARED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,330 hrs · 20,261 cycles

RIGHT SIDE HF UNABLE TO TRANSMIT. CORRECTIVE ACTION PENDING.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,330 hrs · 20,261 cycles

NOTICED FUEL WAS GETTING INTO THE CENTER TANKS SO WE TURNED BOTH CENTER PUMPS ON BUT BOTH NO PRESSURE LIGHTS CAME ON AND WE COULD NOT USE THE FUEL IN THE CENTER TANK. AFTER ABOUT AN HOUR WE TRIED TO USE THE CENTER PUMPS AGAIN AND WE WERE ABLE TO USE EVERYTHING IN THE CENTER TANK (600 LBS). CORRECTIVE ACTION PENDING.

Part: START VALVE — FAILED · airframe 109,328 hrs · 20,260 cycles

LEFT STARTER CUTOUT EICAS MSG CAME ON AFTER STARTING BOTH ENGINES DUCT PRESSURE WAS NORMAL, AROUND 30 PSI. REPLACED LEFT ENGINE START VALVE REF B767-300 AMM 80-11-02. PART UNKNOWN TO TRAX.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,182 hrs · 20,227 cycles

PILOT REPORTED DURING WALKAROUND FOUND RH #3 ENGINE BLADE HAS A NICK AT AREA B. INSPECTED AND BLENDED RH ENGINE #3 BLADE NICK AT AREA B PER AMM 72-31-02. DYE PEN INSPECTION DMI'ED, COMPLETED WITH NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,059 hrs · 20,203 cycles

RIGHT ENG THRUST LEVER BINDING JUST ABOVE IDLE. LUBED RH THROTTLE CLUTCH PACKS AND PERFORMED THRUST LEVER LOAD TEST ON RH THRUST LEVER PER AMM 76-11-00 LOAD TEST OKAY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,007 hrs · 20,193 cycles

RIGHT HF RADIO INTERMITTENT. PERFORMED FIM 23-11 FAULT TREE 864 NO FAULTS NOTED AT THIS TIME. AC REMAINS ETOPS 180

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,957 hrs · 20,183 cycles

RIGHT HF RADIO INTERMITENT IN FLIGHT. PERFORMED RH HF RADIO OPS CHECK ON GROUND PER AMM 23-11-00, OPS CHECK GOOD BEING ABLE TO TRANSMIT AND RECEIVE ON GROUND.

Part: SWITCH — FAILED · airframe 108,812 hrs · 20,155 cycles

RIGHT ENGINE ANTI-ICE SWITCH STICKING OR NOT ENGAGING. REMOVED AND REPLACED ANTI-ICE PANEL ASSY IAW AMM 30-11-01 OPS CHECK GOOD. NO TRAX TIME INFO FOR UNIT REMOVED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,760 hrs · 20,143 cycles

MAIN DECK CARGO SMOKE DETECTORS ZONE 3 AT A LOOP AND ZONE 4 B LOOP INOP. DEFERRED MAIN CARGO DECK COMPARTMENT ZONE 3 A LOOP AND ZONE 4 B LOOP PER MEL 26-16-02-02, CAT C.

Part: UNKNOWN — UNKNOWN · airframe 108,694 hrs · 20,130 cycles

R ENG FUEL FILTER EICAS ON CLIMBOUT. RIGHT ENGINE EICAS FUEL FILTER MESSAGE PERFORMED BY AND FOLLOW FIM 73-11 FAULT TREE 803 PER FIM REMOVED AND REPLACED FUEL FILTER PER AMM 73-11-02, LEAK CHECK OKAY.

Part: VALVE — FAILED · airframe 108,652 hrs · 20,122 cycles

STATUS MESSAGE R ENG PRV. FOUND RIGHT SIDE EPR VALVE INOP. REMOVED AND REPLACED PRESSURE REGULATING RIGHT HAND SIDE PER AMM 36-11-18

Part: NONE — NONE · airframe 108,647 hrs · 20,121 cycles

STATUS PAGE R ENG PRV. PERFORMED B767 FIM 36-10, FAULT PAGE 878, NO FAULTS NOTED. MESSAGE CLEARED.

Part: NONE — NONE · airframe 108,617 hrs · 20,115 cycles

R ENG PRV ON EICAS ON LANDING. PERFORMED B767 FIM 36-10, FAULT TREE 878, NO FAULT NOTED, MSG CLEARED

Part: NONE — NONE · airframe 108,559 hrs · 20,103 cycles

LEFT AFT FUEL PUMP PRESSURE LIGHT STAYS ILLUMINATED. PERFORMED FIM TASK 28-22 FAULT TREE 819, FOUND LEFT AFT PRESSURE SWITCH INOP, REMOVED AND REPLACED LEFT AFT PRESSURE SWITCH PER AMM 28-41-01 OPS CHECK NORMAL. PART UNKNOWN TO TRAX, NO HOURS INFO.

Part: NONE — NONE (IDG) · airframe 108,283 hrs · 20,004 cycles

EVIDENCE OF OIL LEAK BY IDG ACCESS DOOR LEFT ENGINE. CLEANED LEFT ENGINE BY THE IDG IAW B767 AMM 79-00-00 AND MOTORIZE LEFT ENGINE IAW B767 AMM 71-00-00 NO LEAKS NOTED AT THIS TIME.

Part: FAULT LIGHT — ILLUMINATED (APU) · airframe 9,999 hrs · 9,999 cycles

TWO ATTEMPTED STARTS OF APU, FAULT LIGHT BOTH TIMES. RESET APU CONTROL UNIT, RESTARTED APU AFTER RESET OPS CHECK OK EN REF B767 FIN 49-11-00 CONFIG 3 APU BITE PROCEDURE

Part: SENSOR — FAILED · airframe 108,181 hrs · 19,959 cycles

SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED LEFT ELECTRICAL FAN INLET TEMP (T12) SENSOR IAW B767 AMM 73-21-06 TEST OKAY.

Part: EEC — FAULTED (LT ENGINE) · airframe 108,166 hrs · 19,951 cycles

EICAS MESSAGE L ENG EEC. PERFORMED FIM 73-21 FAULT TREE 804, SYSTEM CHECKS GOOD.

Part: EEC — FAULTED (LT ENGINE) · airframe 108,167 hrs · 19,952 cycles

EICAS MSG L ENG EEC COMES ON DURING DESCENT AROUND 10,000 FEET. DEFERRED PER MEL 73-21-01-01B.

Part: BLADE — NOT REPORTED (ENG FAN) · airframe 108,159 hrs · 19,947 cycles

FANBLADE REPAIR, PENDING PAPERWORK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,159 hrs · 19,947 cycles

#2 ENGINE BLADE #19 HAS SMALL NICK NEAR BLADE TIP. BLENDED SMALL NICK ON #2 ENGINE FAN BLADE IAW B767 CF6-80C ENGINES AMM 72-31-02 BLADE FOUND WITHIN SERVICEABLE LIMITS FOR NDT SEE LOG PAGE #B067604 (GOOD)

Part: APU — SHUTDOWN · airframe 108,085 hrs · 19,922 cycles

APU AUTO SHUTDOWN. CONNECTED EXTERNAL POWER IAWM B767 AMM 24-00-00 PERFORMED APU BITE IAW AMM 49-11 FAULT TREE 960, OPS CHECK NORMAL.

Part: BOOT — TORN · airframe 108,085 hrs · 19,922 cycles

APU FORWARD LOAD CONTROL VALVE RUBBER BOOT TORN. REPLACED LOAD CONTROL VALVE FWD RUBBER BOOT IAW 49-11-01, NO LEAKS NOTED.

Part: SHUTOFF VALVE — FAILED · airframe 108,021 hrs · 19,898 cycles

SUPPLEMENTAL INFORMATION. REMOVED AND REPLACED RH ENG HPSOV IAW B767 AMM 36-11-07 PENDING HPSOV INSTALLATION TEST STEP H (GOOD). PART IS UNKNOWN TO TRAX.

Part: SHUTOFF VALVE — WARNING MESSAGE · airframe 107,969 hrs · 19,877 cycles

EICAS MSG R ENG HPSOV ON FINAL APPROACH, STATUS MESSAGE. DEFERRED PER MEL 36-11-02-02 CAT C ON 12/7/2022 @ 0100Z. COMPLIED WITH MX PROCEDURES

Part: ECU — FAULTED (APU) · airframe 107,931 hrs · 19,863 cycles

DURING PREFLIGHT CHECK APU FAILED TO START, TWO ATTEMPTS. ACCOMPLISHED FIM 49-11 FAULT TREE 958, CLEARED ECU FAULTS. APU OPS CHECKED GOOD PER AMM 49-11-00

Part: CONNECTOR — FAILED (RT ENGINE EGT) · airframe 107,752 hrs · 19,792 cycles

AS PER CUSTOMER REQUEST, RIGHT ENGINE EGT INDICATION (ECM ALERT). FOUND CONNECTOR D10990 IN BAD CONDITION AND CHANNEL B WIRE BARE, FOUND LOWER THERMOCOUPLE DAMAGE AND 3 PROBES QUIT READING. REPLACED CONNECTOR D10990, THERMOCOUPLE 3,4,5 AND REPLACED RIGHT ENGINE SHUNT JUNCTION BOX AND RH ENGINE LOWER EGT THERMOCOUPLE CABLE.

Part: BLEED VALVE — FAULTED (RT ENGINE) · airframe 107,688 hrs · 19,770 cycles

ON PUSHBACK OUT OF MDSD WE TRIED TO START THE RIGHT ENGINE BUT WE COULD ONLY GENERATE 11.6 N2, DUCT PRESSURE WAS 20PSI. MI DUE TO ABOVE @MDSD 1826Z. DEFERRED APU BLEED VALVE ON 10/28 @ 1845Z CAT C, MX PROCEDURES COMPLIED WITH. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW B-767 AMM 49-53-01 OPS LEAK CHECK GOOD.

Part: HOSE — DAMAGED (COOLING) · airframe 107,601 hrs · 19,729 cycles

LH ENGINE THROTTLE CABLE COOLING HOSE DAMAGED. REMOVED AND REPLACED LH ENGINE THROTTLE CABLE COOLING HOSE REF BOEING AMM 76-11-02

Part: PRECOOLER — DAMAGED (NR 1 ENGINE) · airframe 107,601 hrs · 19,731 cycles

#1 ENGINE PRECOOLER HAS INTERNAL DAMAGE. REMOVED #1 ENG PRECOOLER IAW MM 36-11-15, INSTALLED #1 ENGINE PRECOOLER IAW AMM 36-11-15 NO LEAKS NOTED.

Part: DUCT — DAMAGED (LT ENGINE) · airframe 107,601 hrs · 19,731 cycles

#1 ENGINE LEFT INBOARD CORE COWL DUCT HAS INTERNAL DAMAGE AND MATING LIP WORN. REMOVED #1 ENGINE LEFT IB CORE COWL DUCT. INSTALLED #1 ENGINE LEFT IB CORE COWL DUCT IAW AMM 71-11-06

Part: IGNITER — INOPERATIVE (RT ENG NR 2) · airframe 107,525 hrs · 19,706 cycles

RH ENG IGNITOR #2 INOP. PERFORMED OPERATIONAL TEST OF IGNITION CONTROL SYSTEM RIGHT ENGINE, OPERATES NORMAL PER REF B767 AMM 74-00-00, REMOVED AND REPLACED #2 IGNITOR PLUG IAW AMM 74-21-02.

Part: PUMP — LOW PRESSURE (FUEL SYSTEM) · airframe 107,416 hrs · 19,664 cycles

LEFT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED WHEN SELECTED AND SUFFICIENT FUEL IN CENTER TANK. RESET THE UFI ASSY IAWM AMM 28-2200 OPS CHECK NORMAL FOR THE LEFT CENTER FUEL PUMP.

Part: TRANSMITTER — NOT REPORTED (FUEL FLOW) · airframe 107,361 hrs · 19,645 cycles

IN REFERENCE TO GE CUSTOMER NOTICE REPORT # 20220913052, REMOVE AND REPLACE FUEL FLOW TX AND REPORT TO MX CONTROL. REMOVED AND REPLACED RH ENGINE FUEL FLOW TRANSMITTER IAW AMM 73-31-01, OPS CHECK GOOD. NO PART INFO AT THIS TIME, PENDING DOCUMENTATION.

Part: NONE — FAILED · airframe 107,297 hrs · 19,625 cycles

RIGHT ENGINE FUEL FLOW DOES NOT REGISTER UNTIL ENG N2 IS 33% AT IDLE. FLOW 300 LBS LESS THAN LEFT. ON TO FLOW IS 3000 LBS LESS ON RIGHT. REMOVED AND REPLACED RIGHT ENG FUEL FLOW TX AS PER REF B767 AMM 73-31-01, PERFORMED OPERATIONAL TEST NORMAL AS PER REF B767 AMM 71-00-00

Part: NONE — NONE · airframe 107,262 hrs · 19,611 cycles

RIGHT ENGINE EGT THERMOCOUPLE HARNESS HAS BROKEN LEAD WIRE. REMOVED AND REPLACED RIGHT ENGINE UPPER EGT THERMOCOUPLE CABLE IAW AMM 77-21-102. PERFORMED RIGHT ENG RUN UP OPS CHECK NORMAL IAW AMM 71-00-00 AND REPLACED EGT THERMOCOUPLE IAW AMM 77-21-01

Part: NONE — NONE · airframe 107,223 hrs · 19,597 cycles

R GEN DRIVE LIGHT ILLUMINATED IN EICAS. DEFERRED PER MEL 24-11-01-01B CAT B ON 8/31/22. RESET RIGHT IDG PER B767 AMM 24-11-01. OPS CHECK GOOD.

Part: SENSOR — FAILED · airframe 107,223 hrs · 19,597 cycles

APU FAULT AIRBORNE - RTB DUE TO R GEN DRIVE INOP. TS OVERSPEED MSG SHUTDOWN @ ECU, PERFORMED FIM 49-11 FAULT TREE 968, REMOVED P2 SENSOR TUBE, WAS CLEANED AND PLACED BACK TO ORIGINAL CONFIG. REPLACED APU INLET PRESSURE SENSOR AS PER REF B767 AMM 49-61-04. NO TIME IN TRAX AVAILABLE.

Part: NONE — NONE · airframe 107,177 hrs · 19,576 cycles

EICAS MSG L ENGINE FIRE LOOP 1. DEFERRED L ENGINE FIRE LOOP PER MEL 26-11-01-01 CAT C ON 8/26/22. PERFORMED FIM 26-11-FT-804 ENGINE FIRE DETECT BITE PROCEDURE, FOUND LOWER AFT DET ELEMENT 1 WITH TERMINALS LOOSE ON DETECTOR RESPONDER, RESECURED OPS CHECK GOOD PER AMM TASK 26-11-00-715-075-003.

Part: NONE — NONE · airframe 107,177 hrs · 19,576 cycles

RIGHT ENGINE #37 BLADE BENT. INSPECTED AND REWORKED RT ENGINE #37 BLADE IN ACCORDANCE WITH AMM 72-31-02 WITHIN LIMITS. ENGINE RUN NORMAL AND GROUND VERIFICATION COMPLIED WITH.

Part: SMOKE DETECTOR — FAILED · airframe 107,124 hrs · 19,554 cycles

MAIN DECK CARGO FIRE PANEL A1 AMBER LIGHT ILLUMINATED, NO EICAS OR OTHER CAUTION/WARNING LIGHTS WERE DISPLAYED. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-16-01 OPS CHECK GOOD.

Part: EICAS — FAULT MESSAGE · airframe 106,970 hrs · 19,487 cycles

LEFT ENGINE FUEL FILTER EICAS MSG IN FLIGHT AND ON GROUND. ACCOMPLISHED FIM 73-11 FAULT TREE 803, NO CONTAMINATION FOUND ON FUEL FILTER. INSTALLED A NEW FUEL FILTER IAW AMM 73-11-02, ENGINE RUN FOR LEAK CHECK NO LEAKS.

Part: SKIN PANEL — DENTED · airframe 106,941 hrs · 19,473 cycles

DURING WALKAROUND FOUND DENT ON RH SIDE OF FUS BETWEEN STA 1439-1461, STRINGERS BETWEEN S-24 AND S-25, LENGTH 22.750" WIDTH 2.250 AND DEPTH 0.234. REPAIR ACCOMPLISHED PER NAC EO 767-53-0026

Part: ENGINE — NICKED · airframe 106,910 hrs · 19,460 cycles

CREW COMMENT #1 ENGINE BLADE #16 HAS A SMALL NICK APPROX 2" FROM BLADE TRIP. BLENDED SMALL NICK ON #1 ENGINE BLADE #16 APPROX 2" FROM TIP IAW B767 72-31-02, BLADE WITHIN SERVICEABLE LIMITS

Part: EICAS — FAULT MESSAGE · airframe 106,910 hrs · 19,460 cycles

L ENG PRV EICAS MESSAGE ON ENGINE START IN GATES @ MIA. REMOVED AND REPLACED LEFT ENGINE PRV IAW B767 AMM 36-11-18, AWAITING OPS CHECK AND LEAK CHECK SEE ITEM M-2 (GOOD). ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: NONE — NONE · airframe 106,910 hrs · 19,460 cycles

SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED C1383 CB "APU PRIME CONT" AND C20 "APU START" CB REF WD 49-61-11 APU OPS NORMAL IAW AMM 49-11-00 AND AMM 24-21-00. ETPS GND VERIFICATION COMPLIED WITH.

Part: COWL DOOR — DAMAGED · airframe 106,859 hrs · 19,437 cycles

RH ENGINE OB CORE COWL DUCT PRECOOLER EXIT DAMAGE. REMOVED AND REPLACED RH ENGINE OUTBOARD CORE COWL IAW AMM 71-11-06 PART INFO PENDING CHECK DOCUMENTATION

Part: APU — INOPERATIVE · airframe 106,852 hrs · 19,433 cycles

APU DOOR STATUS MESSAGE. PERFORMED MULTIPLE STARTS AND SHUTDOWNS, APUR OBSERVED TO OPERATE NORMAL PER FIM 49-11 FT 959, AND NO MESSAGES WERE OBSERVED, APU CHECKED NORMAL PER AMM 49-11-00

Part: COWLING — DAMAGED · airframe 106,841 hrs · 19,427 cycles

ACOUSTICAL LINER DAMAGED ON LH ENGINE AT 11 OCLOCK AND 8 OCLOCK POSITION. DEFERRED ACOUSTICAL SEGMENTS PER DMI 72-00 PER AMM 72-00-00 TABLE 645. CONTINUE IN SERVICE FOR 10 CYCLES ON 7/9/22 @ 0100Z

Part: COWLING — DAMAGED · airframe 106,840 hrs · 19,477 cycles

ACOUSTICAL LINER SEGMENT DAMAGED ON RIGHT HAND ENGINE @ 2 OCLOCK POSITION. DEFERRED ACOUSTICAL SEGMENT PER DMI 72-00 PER AMM 72-00-00 TABLE 645. CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES @ 7/9/22 @ 0120Z.

Part: NONE — NONE · airframe 106,827 hrs · 19,422 cycles

FLIGHT INTERRUPTION DUE TO APU DOOR STATUS MESSAGE DURING DEPARTURE @ 0410Z, 7/7/22. ITEM DEFERRED IAW MEL 49-15-01-01B CAT C, ETOPS PLACARD TURNED TO NO ETOPS, APU DOOR VISUALLY CHECKED CLOSED.

Part: NONE — NONE · airframe 106,687 hrs · 19,360 cycles

STATUS MSG RIGHT ENGINE FIRE LOOP 2. DEFERRED PER MEL 26-11-01-01 CAT C ON 6/20/2022 @0610Z. ETOPS VERIFICATION CW

Part: NONE — NONE · airframe 106,220 hrs · 19,331 cycles

LEFT ENGINE ACOUSTIC PANEL DAMAGED AT 10 OCLOCK POSITION AFT LOOKING FWD BEHIND FAN BLADES. APPLIED ADHESIVE COMPOUND AT LEFT ENGINE ACOUSTIC PANEL AT 10 0CLOCK POSITION AFT LOOKING FWD BEHIND FAN BLADES. IAW B767-300 AMM 72-32-00

Part: NONE — NONE · airframe 106,555 hrs · 19,304 cycles

RIGHT ENGINE DID NOT START ON #2 IGNITOR IN TTPP. TRNSFERRED TO MEL #74-00-01A CAT A. REMOVED AND REPLACED RIGHT ENG #2 IGNITOR PLUG IAW B767 AMM 74-21-02. ACCOMPLISHED IGNITOR PLUG TEST IAW B767 AMM 71-00-00 OPS CHECK GOOD AT THIS TIME. ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: NONE — NONE · airframe 106,548 hrs · 19,301 cycles

MI DUE TO STATUS MESSAGE R ENG SPEED CARD ON THE GROUND IN KMIA AFTER STARTING THE RIGHT ENGINE @ 0820Z. RERACKED R-N2 ENGINE SPEED CARD M1092 AND RESET CIRCUIT BREAKER SPEED SENSE R2 PER B767 AMM 73-21-54. ENGINE IDLE RUNUP PER AMM 71-00-00 OPS CHECK GOOD.

Part: NONE — NONE · airframe 106,548 hrs · 19,301 cycles

RIGHT FCS IN RUN BUT NO FUEL FLOW ON ENGINE START. RESTARTED, OK NORMAL START. ACCOMPLISHED FIM FAULT TREE 76-11 FT 812, REMOVED AND REPLACED FUEL IGN/CONTROL RELAY K169 PER AMM 76-11-11. ACCOMPLISHED ENGINE RUN PER AMM 71-00, OPS CHECK NORMAL ETOPS GROUND VERIFICATION COMPLIED WITH. NO PART INFO GIVEN.

Part: NONE — NONE · airframe 106,518 hrs · 19,289 cycles

LEFT ENGINE FIRE LOOP 2 MESSAGE, LOWER EICAS. TRANSFERRED TO MEL 26-11-01-01 ON 5/31/22 AT 0530Z NO MAINT ACTION REQUIRED, PLACARD INSTALLED, CAT C

Part: STARTER — FAILED · airframe 106,493 hrs · 19,276 cycles

RIGHT ENGINE STARTER EICAS MESSAGE ON START AT SYCJ, PERFORMED RIGHT ENGINE STARTER QRH PROCEDURES. REMOVED AND REPLACED RH ENGINE STARTER IAW AMM 80-11-01. ENGINE RUN FOR LEAK CHECK IAW AMM 71-00-00, NO LEAKS REMOVED AND INSTALLED START VALVE, CHECK OK. NO TRAX INFO FOR UNIT TIME.

Part: CONTROLLER — UNKNOWN · airframe 84,340 hrs · 14,172 cycles

LEFT ENGINE PRV. PERFORMED AIR SUPPLY BITE CHECKS PER AMM 36-23-00. FOUND L ENG PRV AND L ENG PRVC FAULT CODE. REMOVED AND REPLACED LEFT ENGINE PRV PER AMM 36-11-8 OPS CHECK AND LEAK CHECK OKA. REMOVED AND REPLACED LEFT ENGINE PRC CONTROLLER PER AMM 36-11-19 OPS CHECK AND LEAK CHECK OKAY, AC REMAINS ETOPS 180. PRV PN# 802170-10 SN# 921174 OFF. NO TRAX TIME UNIT INFO FOR EITHER PART.

Part: NONE — NONE · airframe 106,305 hrs · 19,207 cycles

REF TO REA 47303REA24 INTERIM REPAIR SEAT TRACK MAIN CARGO DECK STA 785 RBL 88.5. DEFERRED THE DAMAGED SEAT TRACK PER 49303REA24 AND NAC GMM DMI 5:31 SECTION 2 FOR MAINT TRACKING. PERMANENTLY REPAIR OR REPLACE THE DAMAGE SEAT TRACK LOC AT STA 785, RBL 88.5 BEFORE 50 CYCLES, VISUAL INSPECT THE CRACK PRIOR TO EACH FLIGHT.

Part: NONE — MISSING · airframe 106,220 hrs · 19,169 cycles

FOUND APU LEFT AFT VIBRATION ISOLATOR MISSING RETAINING NUT AND APU NOT FULLY SECURED. DEFERRED APU INOP PER MEL 49-11-01A CAT C ON 4/23/2022. REMOVED AND REPLACED LEFT AFT VIBRATION ISOLATOR IAW AMM 49-13-02. ACFT RELEASED NO ETOPS. NO TIME INFO ON TRAX.

Part: SWITCH — FAILED · airframe 106,183 hrs · 19,155 cycles

APU FAILED TO START. DEFERRED PER MEL 49-11-01A CAT C ON 4/19/22. REMOVED AND REPLACED DEICE VALVE SOLENOID AS PER REF B767 AMM 49-27-08 PERFORMED OPS CHECK NORMAL NO LEAKS. REQUIRED COLD SOAK START FOR ETOPS 180. NO TRAX TIME INFO AVAILABLE.

Part: FAN — FAILED · airframe 106,165 hrs · 19,147 cycles

STATUS MSG "FWD EQ EXH FAN" ON THE GROUND IN MDSD. DEFERRED PER MEL 21-58-04 ON 4-17-22 AT 1515 CAT C. PLACARD INSTALLED ACCOMPLISHED MX PROCEDURES. REMOVED AND REPLACED FWD EQUIP EXH FAN AS PER REF B767 AMM 21-58-06 PERFORMED OPS CHECK, FOUND NORMAL.

Part: NONE — NONE · airframe 106,146 hrs · 19,140 cycles

APU INLET DOOR CIRCUIT BREAKER HEAD BROKEN. REMOVED AND REPLACED C1385 IAW SWPM 20-30-0001 OPS CHECK NORMAL IAW AMM 49-11-00

Part: NONE — NONE · airframe 106,130 hrs · 19,134 cycles

SUPPLEMENTAL INFORMATION. CORRECTING CONTROL NUMBER VS NACA2022041300001

Part: CONTROLLER — FAILED · airframe 106,072 hrs · 19,110 cycles

SUPPLEMENTAL INFORMATION - REMOVED AND REPLACED APU CONTROLLER IAW B767 AMM 49-61-05 OPS CHECK NORMAL NO TIME INFO ON TRAX.

Part: NONE — NONE · airframe 105,984 hrs · 19,080 cycles

APU WOULD NOT START AFTER LANDING IN MIA. NO ENGINE ROTATION ON APU. PERFORMED APU ECU BITE PER B767 AMM 49-61-05 NO DEFECT NOTED. PERFORMED OPS CHECK OF APU PER B767 AMM 49-11-00, APU CHECKS GOOD. ETOPS GROUND VERIFICATION COMPLETED.

Part: VALVE — FAILED · airframe 105,977 hrs · 19,077 cycles

AFT CABIN TEMP EICAS MSG AND DISCRETE LIGHT ON. REMOVED AND REPLACED AFT TRIM AIR MODULATING VALVE, OPS CHECK AS PER AMM 21-61-07 AC REMAINS ETOPS 180. NO TIME INFO IN TRAX.

Part: NONE — NONE · airframe 105,973 hrs · 19,076 cycles

LEFT EEC INOP ON TAXI. DEFERRED LEFT EEC IAW MEL 73-21-01-01B CAT C. PERFORMED TS IAW FIM 71-01 FAULT TREE 823, ALSO PERFORMED LEFT ENGINE PMC CONNECTOR CLEANING IAW SWPM 20-60-01, PMC END TEST NORMAL IAW AMM 73-21-07/501. AC RELEASED ETOPS 180

Part: NONE — NONE · airframe 105,977 hrs · 19,077 cycles

CHECK APU OIL, CHECK FOR LEAK. DEFERRED PER MEL 49-11-01A CAT C ON 3/27/22 AT 1920Z AIRCRAFT REMAINS NON-ETOPS. ADJUSTED OIL CAPS LOCKING MECHANISM ACCOMPLISHED LEAK CHECK APU OPS CHECK, NO LEAKS NOTED DURING TWO HOURS CHECK.

Part: NONE — NONE · airframe 105,945 hrs · 19,064 cycles

SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED #2 IGNITOR PLUG IAW AMM 74-21-01 ACCOMPLISHED OPS CHECK FOUND GOOD. AC REMAINS NO ETOPS.

Part: CONTROL VALVE — INOPERATIVE (CABIN TEMP) · airframe 105,923 hrs · 19,056 cycles

AFT CABIN TEMP EICAS AND DISCRETE LIGHT ON IN FLIGHT. DEFERRED PER MEL 21-61-04-02 CAT C AFT ZONE TEMP CONTROL VALVE INOP. MX PROCEDURES COMPLIED WITH. 3/24/22 0610Z

Part: INDICATOR — INACCURATE (CABIN TEMP) · airframe 105,915 hrs · 19,052 cycles

MID COMPARTMENT TEMP READ ZERO DEGREES. CENTER TEMP INDICATOR WAS FOR FLIGHT DECK BUT IT IS NOT CONNECTED TO A TEMP BULB PER IAI WDM 21-65-11, THEREFORE INDICATION IS ZERO.

Part: NOT REPORTED — NOT REPORTED · airframe 105,877 hrs · 19,038 cycles

AFTER GROUND CREW HOOKED UP FOR TOW-IN APU SHUTDOWN INSTANTANEOUSLY. RESTARTED SUCCESSFULLY, BUT APU SHUTDOWN AGAIN AFTER TOW. PERFORMED APU BITE PROCEDURE PER B767 FIM 49-11 FAULT TREE 958, NO FAULTS FOUND AT THIS TIME. RESET BOX, OPS CHECK GOOD.

Part: NOT REPORTED — NOT REPORTED · airframe 105,873 hrs · 19,036 cycles

APU KICKED OFF AT ENGINE SHUTDOWN. RESET APU ECU, OPS CHECK NORMAL IAW B767 AMM/FIM 49-11 FAULT TREE 986

Part: NOT REPORTED — NOT REPORTED · airframe 105,765 hrs · 18,989 cycles

#1 ENGINE UPPER THERMOCOUPLE HARNESS DAMAGED. REMOVED AND REPLACED #1 ENGINE THERMOCOUPLE HARNESS PER B767 AMM 77-21-02, REPLACED 2 OCLOCK THERMOCOUPLE PROBE PER B767 AMM 77-21-01 HARNESS AND PROBE CHECK GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: CPU — CRACKED · airframe 105,749 hrs · 18,983 cycles

RH COWLING HAS A CRACK ON LOWER AREA 10" LONG FROM THE EDGE. REMOVED AND REPLACED CORE COWLING IAW B767 AMM 71-11-06 OPS CHECKED GOOD. NO TIME DATA IN SYSTEM.

Part: NOT REPORTED — NOT REPORTED · airframe 105,665 hrs · 18,945 cycles

AFT CARGO DOOR ELECTRICAL ARCING DURING MANUAL OPEN PROCEDURE. ACCOMPLISHED WIRE REPAIRS OF MULTIPLE WIRES PER WSPM 20-10-13

Part: NOT REPORTED — NOT REPORTED · airframe 105,609 hrs · 18,920 cycles

RH IGNITION RH ENGINE INOP. DEFERRED PER MEL 74-00-01B CAT C ON 2/6/22 @ 1300Z. AIRCRAFT RELEASED NO ETOPS. AS PER FIM 74-00 FT 808 REMOVED AND REPLACED RH IGNITOR PLUG IAW 74-21-02, OPS CHECK GOOD

Part: PUMP — FAILED · airframe 105,461 hrs · 18,855 cycles

MI DUE TO NO FUEL FLOW LH ENGINE WHEN FUEL CONTROL SWITCH TO RUN @ 1530Z @ TTPP. REMOVED AND REPLACED LH ENGINE FUEL PUMP PER B767 AMM 73-11-01, FUEL PUMP CHECKS GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH. UNIT IS PART OF DTO PARTS POOL, NO TIME INFO AVAILABLE.

Part: NOT REPORTED — NOT REPORTED · airframe 105,451 hrs · 18,851 cycles

LH ENGINE OUTBOARD CORE COWL HOLD OPEN ROD FWD ATTACH BRACKET IS BROKEN. DMI 71-11 PER MIKE BEVIS. 01-17-2022, 1635Z.

Part: NOT REPORTED — NOT REPORTED · airframe 105,444 hrs · 18,847 cycles

RIGHT ENGINE FAN BLADE #23 HAS SMALL NICK APROX 2 MM AND 14" FROM TIP. RIGHT ENGINE FAN BLADE 23 BLENDED AND FOUND WITHIN LIMITS IAW B767 AMM 72-00-00. FLUORESCENT PENETRANT INSPECTION COMPLETED, NO DEFECTS NOTED.

Part: NOT REPORTED — NOT REPORTED · airframe 105,420 hrs · 18,835 cycles

APU FAULT LIGHT ON. GVI INSPECTION OF APU COMPARTMENT OK, NO ECU FAULTS, APU OPERATES NORMAL WITH LOAD.

Part: NOT REPORTED — NOT REPORTED · airframe 105,396 hrs · 18,825 cycles

APU FAULTED. 2 RETRY ATTEMPTS FAULTED. RESET APU SYSTEM IAW FIM 49-11-103 SYSTEM CHECKS OK. AIRCRAFT REMAINS ETOPS 180.

Part: NOT REPORTED — NOT REPORTED · airframe 105,363 hrs · 18,807 cycles

APU AUTOSHUTDOWN DURING TOWING. ACCOMPLISHED ECU TEST, NO FAULTS. APU TESTS OK IAW AMM 49-61-05

Part: NOT REPORTED — NOT REPORTED · airframe 105,354 hrs · 18,802 cycles

APU SHUTDOWN AFTER PARKING SDQ. ACCOMPLISHED FIM 49-11 FAULT TREE 958, RESET ECU AND APU OPS CHECK NORMAL PER AMM 49-11-00

Part: NONE — NONE · airframe 105,305 hrs · 18,781 cycles

RIGHT ENGINE FAN BLADE #18 HAS A SMALL DENT 6 IN APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 18 AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X 0.5 MM. NDT INSPECTION ACCOMPLISHED, NO FAULTS NOTED.

Part: NONE — NONE · airframe 105,305 hrs · 18,781 cycles

RIGHT ENGINE FAN BLADE #19 HAS A SMALL DENT 2 INCH APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 19 @ 2" APPROX FROM TIP AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X .25 MM. NDT ACCOMPLISHED WITH NO FAULTS FOUND.

Part: NONE — NONE · airframe 105,277 hrs · 18,769 cycles

LH AC PACK CONNECTOR ASSY SEALS WORN. REMOVED AND REPLACED LH AC PACK CONNECTOR ASSY SEAL IAW AMM 36-11-01, NO LEAKS NOTED.

Part: ISOLATION VALVE — UNKNOWN · airframe 105,187 hrs · 18,733 cycles

DURING PRE-DEPARTURE SERVICE CHECK, FOUND LEFT ISOLATION VALVE CB POPPED OUT. REMOVED AND REPLACED LEFT ISOLATION VALVE IAW B767 AMM 36-11-04, OPS CHECK GOOD. NO PART INFORMATION AVAILABLE, VALVE NO LONGER IN SYSTEM.

Part: IGNITION UNIT — UNKNOWN · airframe 105,182 hrs · 18,730 cycles

APU FAILED TO START. REMOVED AND REPLACED APU IGNITOR BOX OPS CHECKED GOOD AT THIS TIME IAW B767 AMM 49-41-03. NO PART INFORMATION AVAILABLE, UNIT REMOVED FROM SYSTEM.

Part: NONE — NONE · airframe 105,172 hrs · 18,721 cycles

LEFT ENGINEHPSOV EICAS MESSAGE APPEARED ON FINAL THEN WENT AWAY. STATUS PAGE SHOWS L ENG HPSOV. DEFERRED LEFT HPSOV PER MEL 36-11-02-02 CAT C ON 12-7-21@ 2157Z, MAINTENANCE PROCEDURES COMPLIED WITH.

Part: NONE — NONE · airframe 105,140 hrs · 10,714 cycles

ON LANDING LOUD NOISE COMING FROM AIRPLANE AND EXCESSIVE VIBRATION IN BOTH THRUST LEVERS. DURING POST FLIGHT LOUD NOISE COMING FROM PACK AREA UNDER AIRPLANE. INSPECTED LH AIR CONDITIONING BAY AND FOUND LEFT PACK INLET BULB TS433 DISCONNECTED AND DAMAGED. REMOVED AND REPLACED LEFT PACK INLET BULB IAW B767-AMM 21-52-02 OPS LEAK CHECK GOOD, NO DISCREPANCIES FOUND. ETOPS GROUND VERIFICATION OK

Part: NONE — NONE · airframe 105,103 hrs · 18,699 cycles

DURING CLIMB TO CRUISE EICAS MESSAGE LEFT EEC WAS DISPLAYED. DEFERRED LH ELECTRONIC ENGINE CONTROL IAW MEL 73-21-01-01 B CAT C 12/2/21 @ 11:40Z

Part: NONE — NONE · airframe 105,052 hrs · 18,675 cycles

N1 VIBRATION ANALYZER RIGHT REACHING 3.7 ON RH ENGINE. RIGHT ENGINE N1 VIBRATION WITHIN LIMITS, MAX PERMITTED VIBRATION FOR CONTINUOUS OPERATION IS 4.0 IN ACCORDANCE WITH AMM SUBTASK 71-00-00 862-175-400

Part: NONE — NONE · airframe 105,013 hrs · 18,658 cycles

ON CLIMB OUT OF KMIA EICAS MESSAGE L ENG EEC AND ASSOCIATED L ELEC ENGINE CONTROL SWITCH INOP LIGHT ILLUMINATED. WE RAN THE L ENG EEC CHECKLIST IN THE QRH. DEFERRED LH ELECTRONIC ENGINE CONTROL IAW MEL 73-21-01-01B CAT C 11/21/21 @ 1350Z

Part: NONE — NONE · airframe 104,999 hrs · 18,651 cycles

APU FAULT ON START AFTER LANDING. PERFORMED FIM 49-11 FT 958, CLEARED ECU BITE MEMORY, APU OPS NORMAL IAW AMM 49-11-00

Part: NONE — NONE · airframe 104,954 hrs · 18,630 cycles

MI ON PUSHBACK @ KMIA DUE TO EICAS L ENG EEC 1110Z. PERFORMED TS IAW FIM TASK 73-21 FAULT TREE 817. ENG RUNUP IAW AMM 71-00-00/501. NO DISCREPANCIES NOTED.

Part: NONE — NONE · airframe 104,924 hrs · 18,616 cycles

DISCREPANCY: EICAS MESSAGE L ENG EEC. CORRECTIVE ACTION: DEFERRED AS PER MEL 73-21-01-01B CAT C ON 11/10/2021 TIME 0614Z AIRCRAFT RELEASED NON-ETOPS, PLACARD TURNED.

Part: NONE — UNKNOWN · airframe 104,780 hrs · 18,557 cycles

DISCREPANCY: DUCT PRESSURE GAUGE INDICATES 15 PSI DIFFERENCE BETWEEN RIGHT AND LEFT. RIGHT IS 15 PSI LESS THAN LEFT AT TAKEOFF AND CLIMB POWER. CORRECTIVE ACTION: REMOVED AND REPLACED RH PRSOV IAW AMM 36-11-09. OPS CHECK GROUND CHECK ETOPS VERIFICATON OK.

Part: NONE — NONE · airframe 104,795 hrs · 18,554 cycles

DISCREPANCY: PER CUSTOMER REQUEST REMOVE AND REPLACE RH PRSOV FILTERS. CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE PRSOV FILTERS IAW AMM 36-11-09 OPS AND LEAK CHECK GOOD, ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: PUMP — UNKNOWN · airframe 104,666 hrs · 18,495 cycles

DISCREPANCY: R FUEL VALVE EICAS MESSAGE DURING RIGHT ENGINE START, CORRESPONDING ENG VALVE INDICATOR LIGHT, NO LIGHT OFF. CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE FUEL PUMP PER B767 AMM 73-11-01. FUEL PUMP OPS CHECKS AND LEAKS CHECKS GOOD PER B767 AMM 71-00-00 ETOPS GROUND VERIFICATION COMPLIED WITH, AC RELEASES ETOPS 180

Part: PRESSURE SWITCH — UNKNOWN · airframe 104,662 hrs · 18,494 cycles

DISCREPANCY: APU SHUTDOWN AFTER STARTING AND RUNNING FOR 10 MINUTES. CORRECTIVE ACTION: DEFERRED PER MEL 49-11-01A ON 9-29-21@ 2155Z CAT C AC RELEASED NO ETOPS. REMOVED AND REPLACED GENERATOR FILTER DIFF PRESS SWITCH IAW 767 AMM 49-27-15, OPS CHECK LEAK CHECK GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: MEC — UNKNOWN · airframe 104,663 hrs · 18,494 cycles

DISCREPANCY: RIGHT ENGINE NO LIGHT OFF NO FUEL FLOW WITH 25% N2 AND 35 PSI DUCT PRESSURE. CORRECTIVE ACTION: REMOVED AND REPLACED MEC IAW AMM 73-21-01 OPS CHECK NORMAL ON RUNUP IAW AMM 71-00-00.

Part: PUMP — UNKNOWN · airframe 104,663 hrs · 18,494 cycles

DISCREPANCY: NO FUEL FLOW INDICATION ON RH ENGINE DURING STARTUP. CORRECTIVE ACTION: TRANSFERRED TO MEL 73-31-01-02 CAT C 10-1-2021 @ 1007Z. REMOVED AND REPLACED RH ENGINE FUEL PUMP PER B767 AMM 73-11-01. FUEL PUMP OPS CHECKS AND LEAKS CHECKS GOOD PER B767 AMM 71-00-00

Part: NONE — NONE · airframe 104,663 hrs · 18,494 cycles

DISCREPANCY: FUEL FLOW RIGHT ENGINE SHOWS ZERO. CORRECTIVE ACTION: RIGHT ENGINE FUEL FLOW OPS CHECKS GOOD PER B767 AMM 71-00-00

Part: NONE — NONE · airframe 104,656 hrs · 18,489 cycles

DISCREPANCY: APU FAULTED/SHUTDOWN TWICE. CORRECTIVE ACTION: PERFORMED FIM 49-11, RESET ECU AND PERRFORMED APU OPS CHECK IAW AMM 49-11-00. APU CHECK NORMAL, ETOPS VERIFICATION GOOD.

Part: NONE — NONE · airframe 104,606 hrs · 18,472 cycles

DISCREPANCY: FUEL FLOW RIGHT ENGINE SHOWS 0 PPH UNTIL N2 SHOWS 27%. TIME TO LIGHT OFF AND EGT RISE BOTH NORMAL. CORRECTIVE ACTION: TRANSFERRED TO MEL 73-31-01-02 CAT C. RIGHT ENGINE FUEL FLOW CHECKS GOOD PER B767 AMM 71-00-00.

Part: ECU — UNKNOWN · airframe 104,585 hrs · 18,463 cycles

DISCREPANCY: APU INOP. CORRECTIVE ACTION: REMOVED AND REPLACED ECU IAW AMM 49-61-05 OPS CHECK OK, ETOPS GROUND VERIFICATION GOOD.

Part: NONE — NONE · airframe 104,562 hrs · 18,655 cycles

DISCREPANCY: APU SHUTDOWN WITH FAULT LIGHT ON BLOCK IN MIA. CORRECTIVE ACTION: PERFORMED APU BITE TEST ON CONTROL SYSTEM, CHECK GOOD APU START OK IAW AMM 49-01-05

Part: SWITCH — FAULTED (GROUND TEST) · airframe 104,288 hrs · 18,332 cycles

DISCREPANCY: RH PRSOV GROUND TEST SWITCH IS NOT RETURNING TO THE OPEN POSITION. DEFERRED PER DMI 36-11-@2130 08-18-21

Part: SWITCH — FAULTED (THERMAL DUCT) · airframe 104,283 hrs · 18,328 cycles

START OF DESCENT RIGHT STRUT DETECTION LEAK EICAS MESSAGE. DEFERRED PER MEL 36-11-08-01A CAT C ON 15AUG21 @1415Z. MAINT PROCEDURES APPLIED AND PRV SECURED CLOSED. AC REMAINS ETOPS 120. SET PRV BACK TO NORM IAW AMM 36-00-00/901. THIS ACTION CLOSED MEL 36-11-08-01 08-15-21 2120Z. PERFORMED TS IAW FIM 26-18 FAULT TREE 804, FOUND RH ENGINE STRUT THERMAL SWITCH TS238 AND TS239 FAULTY. REMOVED AND REPLACED THERMAL DUCT SWITCHES IAW B767 AMM 26-18-01 OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE INDICATION (DUCT LEAK) · airframe 104,279 hrs · 18,326 cycles

DISCREPANCY: IN CRUISE FLIGHT EICAS R STRUT DCT LEAK. CORRECTIVE ACTION PERFORMED FIM 26-18 FAULT TREE 804, NO FAULTS FOUND.

Part: HINGE — DAMAGED (LT NACELLE DOOR) · airframe 104,282 hrs · 18,327 cycles

DISCREPANCY: LEFT ENGINE OIL SERVICING ACCESS DOOR HINGE PIN OUT OF PLACE. CORRECTIVE ACTION: RE-POSITIONED HINGE PIN @ LEFT ENGINE OIL SERVICING ACCESS DOOR PER B767 AMM 71-11-10, OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (RT BLEED) · airframe 104,273 hrs · 18,322 cycles

DURING CRUISE - RIGHT ENG BLEED LIGHT COMES ON. DEFERRED RIGHT ENGINE BLEED LIGHT (CF6-80C2) PER MEL 36-22-01-02 CAT C ON 8/13/21 @0600Z. MAINT PROCEDURES APPLIED AND R HPSOV SECURED CLOSED.

Part: BLOWER — FAILED (SMOKE DETECTOR) · airframe 104,255 hrs · 18,312 cycles

DISCREPANCY: CARGO DETECT EICAS MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED CARGO DETECTION BLOWER 17719 PER B767 AMM 26-16-02, BLOWER CHECKS GOOD.

Part: IDG — LEAKING (RT GENERATOR) · airframe 104,251 hrs · 18,310 cycles

RIGHT ENGINE IDG LEAKING OIL FROM FILL PORT DURING OPERATION. DEFERRED PER MEL 24-00-01-01 ON 10-AUG-2021 @1130Z CAT B. AC RELEASED ETOPS 120, MAINT PROCEDURE COMPLIED WITH. PLACARD REPOSITIONED TO ETOPS 120.

Part: IDG — LEAKING (RT ENGINE) · airframe 104,251 hrs · 18,310 cycles

RIGHT ENGINE IDG LEAKING OIL FROM OIL FILL PORT DURING OPERATION. DEFERRED PER MEL 24-00-01-01 ON AUG 10 21 @1130 Z CAT B. RELEASED ETOPS 120, MAINT PROCEDUR COMPLIED WITH. PLACARD REPOSITION TO ETOPS 120. REMOVED AND REPLAED RH IDG ADAPTERS IAW AMM 24- LEAK CHECK FOUND GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 104,255 hrs · 18,312 cycles

APU FAULT IN FLIGHT. ACCOMPLISHED BITE TEST ECU ALL NORMAL IAW AMM 49-61-00, OPS CHECK GOOD.

Part: ENGINE — VIBRATION (LEFT) · airframe 104,248 hrs · 18,309 cycles

LEFT ENGINE FAN VIBRATION PEAKS AT 3.5 ON CLIMBOUT. CORRECTIVE ACTION: ACCOMPLISHED AIRFRAME VIBRATION CONDITIONAL IAW AMM 05-51-38, FOUND NO DEFECTS. INSPECTION CHECK FOUND OK.

Part: STATUS MESSAGE — ILLUMINATED · airframe 104,215 hrs · 18,293 cycles

CARGO DET. AIR STATUS MESSAGE. CORRECTIVE ACTION: DEFERRED IAW MEL 26-16-01-03-01 CAT C @ 1318Z

Part: WARNING MESSAGE — ILLUMINATED (PITOT) · airframe 104,211 hrs · 18,292 cycles

EICAS MESSAGE "R AUX PITOT". CORRECTIVE ACTION: ITEM DEFERRED IAW MEL 30-31-01, AC OK FOR SERVICE, NO ETOPS - PLACARD ROTATED.

Part: SHUTOFF VALVE — MALFUNCTIONED · airframe 104,199 hrs · 18,286 cycles

LEFT AND RIGHT PNEUMATIC BLEED SPLIT. CORRECTIVE ACTION: REMOVED AND REPLACED PRSOV, OPS CHECK NORMAL IAW AMM 36-11-09

Part: BLOWER — FAULTED (SMOKE DETECTOR) · airframe 104,193 hrs · 18,284 cycles

DISCREPANCY: AFT DETECTION FAN EICAS MESSAGE PRESENT. CORRECTIVE ACTION: REMOVED AND REPLACED AFT SMOKE DETECTION BLOWER M719 PER B767 AMM 26-16-02, BLOWER OPS CHECKS GOOD.

Part: BYPASS VALVE — DAMAGED (NR 2 BLEED SYS) · airframe 104,144 hrs · 18,265 cycles

DISCREPANCY: PER MAINT CONTROL REQUEST TROUBLESHOOTING OF #2 ENGINE BLEED SYSTEM, BLEED PRESSURE FLUCTUATING IN CLIMB AND DESCENT WITH A 20 PSI SPLIT. CORRECTIVE ACTION: ACCOMPLISHED FIM 36-10-FT-831, FOUND LEFT ISOLATION BYPASS CHECK VALVE WITH SPRINGS DAMAGED, REMOVED AND REPLACED L ISOL CK VALVE PER AMM 36-11-05, LEAK CHECK GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH

Part: APU — UNKNOWN · airframe 104,094 hrs · 18,239 cycles

DISCREPANCY: APU DOOR MESSAGE. CORRECTIVE ACTION: RECONNECTED APU DOOR CANNON PLUG, ACCOMPLISHED PROCEDURE OPS CHECKED GOOD REF AMM 49-15-06

Part: FILTER — CLOGGED (PNEUMATIC SYSTEM) · airframe 104,058 hrs · 18,229 cycles

DISCREPANCY: MI ON THE GROUND IN KMIA @ 0900Z DUE TO NO RIGHT ENGINE BLEED AIR TO ACCOMPLISH A LEFT ENGINE CROSSBLEED START. RIGHT ENGINE BLEED AIR SWITCH OFF LIGHT HAS ILLUMINATED EVEN THOUGH THE BLEED SWITCH WAS IN THE ON POSITION. CORRECTIVE ACTION: PERFORMED FIM 36-10 FAULT TREE 837, FOUND CLOGGED PRSOV FILTER, REPLACED PER AMM 36-11-09. RIGHT BLEED SYSTEM OPS CHECKED AND CYCLED NORMALLY SEVERAL TIMES DURING ENGINE RUN PER 71-00-00

Part: CONTROL PANEL — MALFUNCTIONED · airframe 104,058 hrs · 18,224 cycles

DISCREPANCY: ON CROSSFEED START IN KMIA WE HAD NO DUCT PRESSURE TO START THE LEFT ENGINE. LEFT ENGINE BLEED AIR SWITCH OFF LIGHT WAS ILLUMINATED EVEN THOUGH THE SWITCH WAS IN THE OFF POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED THE BLEED AIR SUPPLY CONTROL PANEL IAW MM 36-11-26. OPS CHECK NORMAL.

Part: APU — FAILED · airframe 104,058 hrs · 18,224 cycles

APU WAS INOPERATIVE. REMOVED AND REPLACED APU IAW B767 AMM 49-11-01.

Part: TERMINAL — BROKEN (SHUTOFF VALVE) · airframe 103,930 hrs · 18,166 cycles

SUPPLEMENTAL ENTRY CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE HPSOV CONTROLLER IAW AMM 36-11-08. DURING TEST AIR SUPPLY HPSOV BITE FAILED. FOUND TERMINAL T1 BROKEN AT VALVE. REPLACED TERMINAL IAW SWPM 20-30-11 TEST NORMAL

Part: APU — FAULTED · airframe 104,015 hrs · 18,202 cycles

APU FAULT DURING GROUND START ATTEMPT. PERFORMED APU BITE PROCEDURE 49-11 FT 958, FIG 103, SYSTEM CHECKED NORMAL

Part: APU — MALFUNCTIONED · airframe 104,001 hrs · 18,197 cycles

DISCREPANCY: APU WON'T START. CORRECTIVE ACTION: ACCOMPLISHED BFCU BITE TEST PER 24-20 FT 814. FOUND FAULT "EXT PWR PIN E-F FAILURE". RESET AND OPS CHECKS GOOD. ACCOMPLISHED APU STARTING PROCEDURES PER AMM 49-11-00, OPS CHECK GOOD.

Part: EEC — MALFUNCTIONED (LEFT) · airframe 103,930 hrs · 18,166 cycles

IN FLIGHT, LEFT THROTTLE LAGGED BEHIND RT THROTTLE WITH HIGHER N2. MANUALLY REDUCED LT THROTTLE TO STAY IN LIMITS. MECHANICAL INTERRUPTION AT 2245Z IN CRUISE DUE TO LEFT EEC ISSUE. CORRECTIVE ACTION: NONE AT THIS TIME, AC IS AOG.

Part: ROD — INOPERATIVE (NR 2 NACELLE) · airframe 103,912 hrs · 18,158 cycles

NR 2 ENGINE OB COWL FWD HOLD OPEN ROD WILL NOT UNLOCK. CORRECTIVE ACTION: DMI 71-11,

Part: BLADE — DENTED (ENGINE) · airframe 103,857 hrs · 18,135 cycles

DISCREPANCY: REF. DMI 72-31 RIGHT ENGINE BLADE #16 DENTED. CORRECTIVE ACTION: PERFORMED NDT SPOT FLUORESCENT PENETRANT INSPECTION #16 BLADE LE NO CRACK INDICATION NOTED.

Part: BLADE — DENTED (RT ENGINE) · airframe 103,852 hrs · 18,132 cycles

DISCREPANCY: RIGHT ENGINE #16 DENTED. CORRECTIVE ACTION: BLENDED R ENGINE BLADE #16 FOUND WITHIN LIMITS PER AMM 72-31-02

Part: WARNING MESSAGE — ILLUMINATED (SHUTOFF VALVE) · airframe 103,847 hrs · 18,130 cycles

DISCREPANCY: RIGHT ENGINE HPSOV MSG/PACK AND BLEED OFF. CORRECTIVE ACTION: DEFERRED R ENGINE HPSOV PER MEL 36-11-02-02 CAT C. MAINTENANCE PROCEDURES COMPLIED WITH. ETOPS SS

Part: CIRCUIT CARD — MALFUNCTIONED (PNEUMATIC SYS) · airframe 103,764 hrs · 18,094 cycles

DISCREPANCY: RIGHT ENGINE HPSOV EICAS MESSAGE COMES ON MOMENTARILY ON FINAL. RIGHT ENGINE STATUS MESSAGE IS ON. CORRECTIVE ACTION: DEFERRED RH ENG HPSOV PER MEL 36-11-02-02. ACCOMPLISHED FIM 36-10 FAULT TREE. 837 BLEED AIR SUPPLY CARD PN# 285T1115-15 REPLACED. PERFORMED RH ENGINE RUN UP OPS CHECK NORMAL IAW AMM 71-00-00. ETOPS SS

Part: SHUTOFF VALVE — LEAKING (PNEUMATIC SYS) · airframe 103,696 hrs · 18,065 cycles

DISCREPANCY: #2 ENGINE HPSOV EICAS MESSAGE ON LANDING, TR DID NOT DEPLOY. CORRECTIVE ACTION: TROUBLESHOT AND FOUND LOOSE PRESSURE LINE, SECURED LINE PER AMM 36-11-07. OPS & LEAK CHECK GOOD.

Part: SHUTOFF VALVE — FAILED (PNEUMATIC SYS) · airframe 103,693 hrs · 18,064 cycles

DISCREPANCY: #2 ENGINE HPSOV EICAS MESSAGE IN FLIGHT. CORRECTIVE ACTION: PERFORMED FIM 36-10 FAULT TREE 843, CHECKED CONNECTORS & LINES TO HPSOV, FOUND NORMAL. REPLACED HPSOV IAW AMM 36-11-07, PERFORMED BITE TEST & LEAK TEST, CHECKED GOOD. ETOPS GROUND VERIFICATION ACCOMPLISHED. ETOPS SS.

Part: BLADE — DENTED (NR 2 ENGINE FAN) · airframe 103,689 hrs · 18,062 cycles

DISCREPANCY: #2 ENGINE #38 FAN BLADE DENTED. CORRECTIVE ACTION: BLENDED BLADE PER AMM 72-31-02. ETOPS SS.

Part: FAULT MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 103,649 hrs · 18,044 cycles

DISCREPANCY: R ENGINE HPSOV EICAS MESSAGE ON FINAL, STATUS MESSAGE STILL SHOWING. CORRECTIVE ACTION: DEFERRED PER 36-11-02-02. DEFERRAL CLEAR, TROUBLESHOT PER FIM FAULT TREE 833, REPLACED HPSOV IAW AMM 36-11-02-02 ON LP B048911 M5. ETOP GROUND VERIFIED OP CHECKED GOOD ON LP B048914 M8. ETOPS SIGNIFICANT SYSTEM.

Part: STARTER — INOPERATIVE (APU) · airframe 103,572 hrs · 18,013 cycles

DISCREPANCY: APU INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED APU STARTER PER AMM 49-41-01. OP CHECK GOOD. ETOPS SS'S.

Part: SHUTOFF VALVE — ERRATIC (RT ENGINE) · airframe 102,193 hrs · 17,419 cycles

DISCREPANCY: IN CRUISE AFTER 30 MINUTES GOT EICAS MESSAGE "RT ENGINE HPSOV". RETURNED TO KMIA. REPLACED RIGHT HPSOV, IAW AMM 36-11-07. OPERATIONS CHECKED GOOD DURING HIGH POWER ENGINE RUN. ETOPS SS.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 101,268 hrs · 17,086 cycles

DURING CLIMB OUT, NOTICED STRONG ELECTRICAL BURNING SMELL AND SMOKE ON FO SIDE. THE ELECTRICAL CONTACT ON THE LOWER RIGHT WINDOW WAS EXTREMELY HOT TO THE TOUCH. TURNED OFF RIGHT WINDOW HEAT AND SMELL DISSIPATED. R1 WINDOW HEAT BURN, DEFERRED PER MEL 30-41-01-01 CAT C.

Part: TEST PANEL — CONTAMINATED (FIRE DETECTION) · airframe 100,991 hrs · 16,967 cycles

DISCREPANCY, MAIN DECK CARGO & "CARGO FIRE" EICAS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED NNC AND RETURNED TO MIA. PERFORMED TROUBLESHOOTING AND FOUND FIRE/OVERHEAT TEST PANEL CONTAMINATED. REMOVED & REPLACED PANEL IAW AMM 26-11-01, TESTED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,537 hrs · 16,787 cycles

DURING WALK AROUND FOUND SKIN CORROSION DAMAGE AT STA1210 STR39R APPROXIMATELY 3 INCHES L X 1 IN W. ACCOMPLISHED A ONE DOUBLER REPAIR WITH SOLID RIVETS IAW B767-300 SRM 53-00-01 REPAIR 1 AND COMPLIED WITH AMES DOC#47303REA10.

Part: BRACKET — DAMAGED (LT WING) · airframe 99,564 hrs · 16,388 cycles

DISCREPANCY: LEFT WING @ WS97.95 AT STRUCTURE BRACKET LOWER HOLE HAS TOOLING MARKS FROM REMOVAL. CORRECTIVE ACTION: REPAIRED HOLES AS REQUIRED IAW AMES REA 47930REA04.

Part: SKIN — CRACKED (BS 325-336) · airframe 99,537 hrs · 16,388 cycles

DISCREPANCY: TEMPORARY REPAIR INSTALLED @ BS325-BS347, S35L-S36L, PERMANENT REPAIR OR DTA ANALYSIS REQUIRED. CORRECTIVE ACTION: REMOVED AND REPLACED TEMPORARY REPAIR @ BS325-BS347, S35L-S36L IAW AMES DOC. 47390REA01 AND B767-300 SRM 51-40-02 P7, AND AMM 51-21-10. SEE PARTIAL WORK ON BACK AND ON PWS #12, PAGE 1.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 99,564 hrs · 16,388 cycles

DISCREPANCY: RW T/E WEB ACCESS HOLE TO RMLG AFT TRUNNION NUT ASSY BENT AND CRACKED. CORRECTIVE ACTION: REPAIRED DAMAGE ON EDGE OF RMLG ACCESS HOLE FOR TRUNNION NUT BY INSTALLING FABRICATED REPAIR DOUBLER IAW B767 SRM 51-70-13 USING FASTENERS IAW B767 SRM 51-40-02, PARA 7.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 99,564 hrs · 16,388 cycles

DISCREPANCY: CORROSION ON TOP SKIN OF WING @ BODY SPLICE MARKED. CORRECTIVE ACTION: CLEAN UP OF CORROSION FOUND TO BE OUT OF LIMITS PER B767-300 SRM 57-20-01. AREA OF CORROSION CLEAN UP REPAIRED IAW AMES DOCUMENT 47390REA03.

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 99,537 hrs · 16,388 cycles

DISCREPANCY: PREVIOUS REPAIR IS CRACKED @ WS675 @ #9 SLAT AREA O/B CORRECTIVE ACTION: REMOVED AND REPLACED REPAIR @ WS675 IAW B767-300 SRM 57-41-13, REPAIR 1.

Part: APU — FAULTED · airframe 99,013 hrs · 16,186 cycles

APU FAILED TO START TWICE ON THE GROUND, EGT STALLED AT AROUND 775 FOR 15 SECONDS BEFORE FAULT. OPEN

Part: SHUTOFF VALVE — STUCK (LT ENGINE) · airframe 98,998 hrs · 16,181 cycles

EICAS MESSAGE "L ENG HPSOV" WHILE ON GROUND. FOUND LT ENG HPSOV STUCK IN OPEN POSITION. REMOVED ANND REPLACED L HPSOC AS PER AMM 36-11-07. INSTALLATION TEST GOOD. (ETOP SS).

Part: BATTERY — DISCHARGED (APU) · airframe 98,991 hrs · 16,176 cycles

APU START UNSUCCESSFUL AFTER MULTIPLE ATTEMPTS. REMOVED AND INSTALLED APU BATTERY IAW B767 AMM 24-31-04. TEST IS NORMAL AND APU OPS CHECK NORMAL IAW B767 AMM 49-11-00. RESECURED APU SYSTEM WIRE TERMINALS REF: B767 SWPM 20-20-00. OPS CHECK GOOD. (ETOPS SS).

Part: PRESSURE VALVE — FAULTY (LT ENGINE) · airframe 98,995 hrs · 16,179 cycles

AFTER ENGINE START IN MDSD, L ENGINE BLEED OFF EICAS MESSAGE APPEARED, AFTER POWER WAS APPLIED THE MESSAGE WENT AWAY AND WAS NOT PRESENT WITH A RECALL SELECTION. ACCOMPLISHED TROUBLESHOOTING TO LT ENG BLEED AND FOUND HPSOV AT FAULT. REMOVED AND REPLACED PER B767 AMM 36-11-07 AND FIM 36-11-/838 ACCOMPLISHED BITE. BITE SATISFACTORY.

Part: EXCITER — INOPERATIVE (APU)

APU SHUTDOWN AFTER IT WAS RUNNING FOR OVER 5 MINUTES ON THE GROUND. DEFERRED AS PER MEL 49-11-01 ON 8-1-19 AT 2235Z CAT "C". REMOVED AND REPLACED APU EXCITER BOX IAW AMM 49-41-03. OPS. NORMAL.

Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 98,383 hrs · 15,944 cycles

DISCREPANCY: MI DUE TO NR 1ENGINE FIRE/OVERHEAT EICAS MESSAGE. FIRE LOOP 2 STATUS MESSAGE ALSO ILLUMINATED. RESET SIX TIMES IN FLIGHT. AIRCRAFT RETURNED TO STATION. CORRECTIVE ACTION: PERFORMED FIM 26-11 FT 804 BLOCKS 1, 2, & 3. FOUND TERMINAL BROKEN AT LWR AFT LOOP 1. REPLACED TERMINAL PER SWPM 20-30-00 OPS CHECK GOOD.