N563NC

Part: ACTUATOR — FAILED (APU FUEL SHUTOFF) · airframe 86,717 hrs · 22,239 cycles

APU FUEL SHUT OFF VALVE FAILED AN OPS CHECK. APU FIRE SWITCH CHECK, DOES NOT CLOSE OR OPEN ELECTRICALLY. R & R THE APU SHUT OFF VALVE ACTUATOR IAW AMM 28-25-00-004-032, & AMM 28-25-02-404-008 STEPS 3.G. (3) - 3.G (8). PERFORMED APU FUEL FEED SYS TEST. TESTED GOOD IAW AMM 28-25-00-715-264.

Part: BLADES — MECHANIC ERROR (NR 2) · airframe 86,717 hrs · 22,239 cycles

NUMBER 2 ENG. SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. ENGINE R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605

Part: BOOT — DAMAGED (HEAT EXCHANGER) · airframe 86,717 hrs · 22,239 cycles

RIGHT COOLING HEAT EXCHANGER PLENUM BOOT IS DAMAGED. REMOVED AND REPLACED RT COOLING HEAT EXCHANGER BOOT IAW AMM 21-51-02-004-001, & AMM 21-51-02-404-019. OPS CHKD GOOD.

Part: SHUTOFF VALVE — STUCK (APU) · airframe 86,717 hrs · 22,239 cycles

APU ECU SELF TEST SHOWS FAULT - IGV ACT. PERFORMED APU ECU BITE TEST IAW AMM 49-61-05-742-045. NO FAULTS FOUND. BITE TEST PASSED. FOUND APU SHUTOFF VALVE STUCK IN CLOSED POSITION. RELEASED THE VALVE, SYSTEM CHECKED OK IAW AMM 49-11-00-802-002.

Part: ACTUATOR — FAULTED (FUEL SHUTOFF VLV) · airframe 86,717 hrs · 22,239 cycles

LEFT ENGINE FUEL SHUT OFF SPAR VALVE STUCK DURING OPS CHECK.. R & R SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11-404-008, STEP 3 G.14. NO DEFECTS NOTED ON OPS CK.

Part: BOOT — DAMAGED (A/C PCK PLENUM) · airframe 86,717 hrs · 22,239 cycles

LEFT COOLING PACK PLENUM BOOT IS DAMAGED. REMOVED AND REPLACED THE LT COOLING PACK PLENUM BOOT IAW AMM 21-51-07-004-001, AND 21-51-07-404-09. LEAK CHKD GOOD.

Part: PRECOOLER — DAMAGED (NR 2 ENGINE) · airframe 86,717 hrs · 22,239 cycles

NR 2 ENG PRE COOLER WAS DAMAGED. R & R NR 2 ENG PRE COOLER IAW AMM 36-11-15-004-003-001, AMM 36-11-15-404-080-005.

Part: SKIN — CORRODED (ZONE 500 FLAP) · airframe 86,717 hrs · 22,239 cycles

CORROSION FOUND ON LH I/B AFT FLAP UPPER SURFACE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 86,717 hrs · 22,239 cycles

STRINGER 32R IN AFT ACCESSORY COMPARTMENT IS CORRODED BETWEEN BS 1809-1832.

Part: SKIN — CORRODED (ZONE 600 FLAP) · airframe 86,717 hrs · 22,239 cycles

RH INBOARD AFT FLAP UPPER TRAILING EDGE SURFACE HAS CORROSION.

Part: INSULATION — DAMAGED (IDG WIRES) · airframe 86,717 hrs · 22,239 cycles

NR 2 ENG IDG WIRING INSULATION DAMAGED IN NUMEROUS AREAS. R & R THE DAMAGED IDG WIRING IAW WDM 24-21-21 AND SWPM 20-30-13, 20-20-12 AND 20-30-11 REFER TO OPS 50003 FOR ADDITIONAL DETAILS AND OP CHECK.

Part: PRESSURE SWITCH — NO TEST (ZONE 100) · airframe 86,717 hrs · 22,239 cycles

E/E COOLING SYSTEM DIFFERENTIAL PERSSURE SWITCH FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED PRESSURE SWITCH E/E COOLING SYSTEM IAW 21-58-29-004-001 AND 21-58-29-404-013. OPS CHECKED GOOD AMM 21-58-00-705174-008.

Part: LINKAGE — CORRODED (OUTFLOW VALVE) · airframe 86,717 hrs · 22,239 cycles

OUTFLOW VALVE DRIVE LINKAGE CORRODED. R & R THE LINKAGE ON OUTFLOW VALVE IAW AMM 20-11-00-993-809.

Part: OUTFLOW VALVE — FAULTED (ZONE 100) · airframe 86,717 hrs · 22,336 cycles

OUTFLOW VALVE DRIVE LINKAGE HAS IS CORRODED. RESOLVED ON W/O: 128197 TASKCARD: N/R-00420. REMOVED & REPLACED LINKAGE ON OUT FLOW VALVE IAW B767 AMM 20-11-00-993-809.

Part: OUTFLOW VALVE — FAULTED (ZONE 100) · airframe 86,717 hrs · 22,336 cycles

OUTFLOW VALVE LINKS ROD END AND ATTACHMENT HARDWARE CORRODED.

Part: BOOT — DAMAGED (A/C PACK PLENUM) · airframe 86,717 hrs · 22,239 cycles

RIGHT COOLING-HEAT EXCHANGER PLENUM BOOT IS DAMAGED. REMOVED AND REPLACED THE EXCHANGER BOOT IAW AMM 21-51-02-004-001 & AMM 21-51-02-404-019. OPS CKD GOOD.

Part: BOOT — DAMAGED (A/C PACK PLENUM) · airframe 86,717 hrs · 22,239 cycles

LEFT COOLING PACK PLENUM BOOT IS DAMAGED. REMOVED AND REPLACED LH COOLING PACK PLENUM BOOT IAW AMM 21-51-07-004-001 AND 21-51-07-404-09 LEAK CK GOOD.

Part: STRIP — MISSING (NR 1 IDG) · airframe 86,717 hrs · 22,239 cycles

#1 ENGINE IDG CABLE HARNESS HAS A MISSING FANNING STRIP AT TERMINAL ENDS. INSTALLED FANNING STRIP ON #1 ENGINE IDG CABLE HARNESS IAW AMM 24-11-01 PARA H.3. (B).

Part: CLAMP — DAMAGED (ZONE 400) · airframe 86,717 hrs · 22,336 cycles

NUMBER 1 ENGINE IDG CABLE HARNESS CLAMPS MISSING RUBBER INSULATORS (2 EA) AT APPROX 7 O'CLOCK POSITION. (RESOLVED ON W/O: 128197 TASKCARD: N/R-00048. REMOVED AND REPLACED # 1 ENG IDG CABLE HARNESS CLAMPS (2 EA) AT APPROX. 7 O'CLOCK POSITION IAW AMM SUBTASK 70-50-00-912-H00 TABLE 202.

Part: SHUTOFF VALVE — STUCK (APU FUEL) · airframe 86,717 hrs · 22,239 cycles

APU ECU SELF TEST SHOWS FAULT IGV ACT. PERFORMED APU ECU BITE TEST IAW AMM 49-61-05-742-045. NO FAULTS FOUND. BITE TEST PASSED. FOUND APU SHUTOFF VALVE STUCK IN CLOSED POSITION & RELEASED THE VALVE, SYSTEM CHECKED OK IAW AMM 49-11-00-802-002.

Part: PRESSURE SWITCH — NO TEST (ZONE 100) · airframe 86,717 hrs · 22,239 cycles

E/E COOLING SYSTEM DIFFERENTIAL PERSSURE SWITCH FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED PRESSURE SWITCH IAW 21-58-29-004-001 AND 21-58-29-404-013. OPS CHECK GOOD.

Part: STARTER — FAILED (APU) · airframe 86,653 hrs · 22,316 cycles

APU WILL NOT START. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01 OPS CHECK NORMAL.

Part: IGNITER — INOPERATIVE (RT ENGINE) · airframe 86,643 hrs · 22,314 cycles

R ENG #1 IGNITOR INOP. REMOVED AND REPLACED RH IGNITOR PLUG IAW AMM 74-21-02 OPS CHECK OK IAW 74-00-00

Part: DUCT — CRACKED (NR 2 ENGINE) · airframe 86,384 hrs · 22,226 cycles

ON CLIMBOUT AT 400FT AGL, ENG #2 EGT EXCEEDED LIMITS, TOPPED AT 650 DEGREES F AFTER 3 SECONDS. REDUCED THRUST, EGT STAYED WITHIN LIMITS. ON FURTHER CLIMB, #2 OIL TEMP APPROACHED LIMITS (158 DEGREES F). INSPECTED RH ENGINE AND FOUND INTERMEDIATE BLEED AIR DUCT CRACKED. REMOVED AND REPLACED DUCT IAW AMM 36-11-01 NO LEAKS NOTED.

Part: BLADE — DAMAGED (ENG FAN) · airframe 86,167 hrs · 22,139 cycles

ON PREFLIGHT LEFT ENGINE FAN BLADE DAMAGE #30. REPAIRED BLADE ON LH ENGINE #30 PER AMM 72-31-02

Part: PROBE — FAULTED (RT ENGINE) · airframe 86,034 hrs · 22,078 cycles

R ENG EEC STATUS MESSAGE. PERFORMED FIM 71-01 FT 803 PMU BITE PROCEDURE SHOWED 2.9 BLEED VALVE THERMOCOUPLE PROBE CH-B OPENED. REMOVED AND REPLACED CH-B PROBE IAW AMM 75-32-06

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 85,850 hrs · 22,000 cycles

DURING READINESS CHECK LIST FOUND RIGHT GENERATOR DRIVE LIGHT OFF WITH R ENG IN CUTOFF. REPLACED IDG IAW AMM 24-11-01

Part: IDG — DISCONNECTED (ZONE 400) · airframe 85,825 hrs · 21,987 cycles

RIGHT ENG GENERATOR INOP. DEFERRED RIGHT ENG GENERATOR IAW MEL 24-00--01-02 RECONNECTED IDG PERFORMED BPCU BITE PER FIM 24-20 NO FAULTS FOUND.

Part: OUTFLOW VALVE — MALFUNCTIONED (ZONE 100) · airframe 85,469 hrs · 21,854 cycles

OUTFLOW VALVE INDICATING HALF OPEN DURING WHOLE FLIGHT AND DIFF PRESSURE INDICATING HALFWAY ON THE YELLOW LINE, VERY CLOSE TO MAX DIFF PRESS. PERFORMED FIM PROCEDURES 21-31 FT 803 NO FAULTS FOUND.

Part: MONITOR — FAILED (ZONE 200) · airframe 85,449 hrs · 21,834 cycles

R ENG VIBE GAUGE ERRATIC ENTIRE FIGHT. VARIES BETWEEN .1 - 1.8. REMOVED AND REPLACED AVM IAW AMM 77-31-03 TEST OK.

Part: PRESSURE SWITCH — FAULTED (ZONE 100) · airframe 85,214 hrs · 21,745 cycles

RIGHT CENTER FUEL PUMP DOES NOT LOAD SHED PRIOR TO ENGINE START. REMOVED AND REPLACED R CENTER OVERPRESSURE SWITCH IAW B767-300 AMM 28-42-01 OPS TEST NORMAL.

Part: STARTER — FAILED (RT ENGINE) · airframe 85,187 hrs · 21,731 cycles

RH ENGINE FAILED TO START. NO ROTATION WHEN START WAS SELECTED. REMOVED AIR STARTER FROM RH ENGINE, FOUND METAL DEBRIS INSIDE THE STARTER. STARTER GEARSHAFT FOUND SHEARED. REMOVED AND REPLACED STARTER AND STARTER DRIVE GEARSHAFT IAW AMM 42-61-03-040-11 AND 80-11-01 OPS CHECK LEAK CHECK GOOD.

Part: ISOLATION VALVE — FAILED (RT BLEED SYS) · airframe 85,132 hrs · 21,708 cycles

RIGHT ISOLATION VALVE SWITCH INDICATES OPEN IN THE OFF POSITION. DEFERRED RH BLEED ISOLATION VALVE PER MEL 36-11-06. REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL PANEL M15 IAW B767 AMM 36-11-26 OPS CHECK GOOD.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 85,089 hrs · 21,688 cycles

WEATHER RADAR HAS SOLID LINE IN THE SWEEP LEFT AND RIGHT SIDE. PERFORMED OPS CHECK OF LT AND RIGHT RADAR SYSTEM, OPS CHECK GOOD. IAW B767 AMM 34-43-00

Part: WARNING MESSAGE — FALSE INDICATION (ZONE 400) · airframe 84,743 hrs · 21,546 cycles

MI DUE TO R ENG BLEED OFF EICAS MESSAGE DURING TAXI@ 1050Z. TROUBLESHOT WITH FIM 36-10 FT 868, NO FAULTS FOUND, OK TO CONTINUE SERVICE

Part: SHUTOFF VALVE — FAILED (RT A/C PACK) · airframe 84,745 hrs · 21,548 cycles

RIGHT PACK DUCT PRESSURE SURGES BETWEEN 10 AND 30 PSI DURING DESCENT. REMOVED AND REPLACED RH PRSOV LEAK TEST GOOD IAW AMM 36-11-09

Part: CONTROLLER — FAILED (LT ENGINE) · airframe 84,724 hrs · 21,538 cycles

L ENG PRV. INSTALLED ASSY CONTROLLER PRESSURE 707 PW FROM SECTION E TO 13 SUBTASK 36-11-19-424-016-003.

Part: ENGINE — FAULTED (LEFT) · airframe 84,724 hrs · 21,538 cycles

L ENG EEC C1. L ENG EEC C1 STATUS MESSAGE ASSOCIATED WITH L ENG AO VALVE , REMOVED AND REPLACED #1 ENGINE

Part: VALVE — UNKNOWN (LT ENGINE) · airframe 84,724 hrs · 21,538 cycles

L ENG A/O VALVE. L ENG A/O VALVE. REMOVED AND REPLACED #1 ENGINE.

Part: VALVE — FAULTED (LT ENGINE) · airframe 84,712 hrs · 21,557 cycles

L ENG AO VALVE. TS PER FIM 7101 FT 803 FOIUND THE EEC CHA/B ADC TR-CK FAIL MESSAGE. CARRIED OUT THE FIM 71-01 FT TASK 830 FOUND THE WIRING CONT CHECK IS GOOD. ENG RUN NO ISSUES.

Part: EEC — FAULTED (LT ENGINE) · airframe 84,712 hrs · 21,557 cycles

L ENG EEC C1. TS PER FIM 73-21 FT 878 FOUND THE EEC CH A/6 ADC TR-CK FAIL MESSAGE. CARRIED OUT THE FIM 71-01 TASK 830 FOUND THE WIRING CONT CHECK IS GOOD. ENG RUN NO ISSUES.

Part: VALVE — FAILED (HEAT EXCHANGER) · airframe 84,712 hrs · 21,537 cycles

FOUND THE L ENG EEC MSG. REPLACED #1 ENG AIR/OIL HEAT EXCHANGER VALVE IAW AMM 79-21-09

Part: CONTROL PANEL — FAILED (HF COMMS) · airframe 84,712 hrs · 21,537 cycles

FOUND THE RH HF CONTROL PANEL MALFUNCTION. REMOVED AND REPLACED THE RH HF CONTROL PANEL IAW AMM 23-11-02

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 84,712 hrs · 21,537 cycles

FOUND RH AIR CONDITION TCV MALFUNCTION. REMOVED AND REPLACED PACK TCV IAW AMM 21-54-12

Part: SKIN — CRACKED (RT NACELLE) · airframe 84,712 hrs · 21,537 cycles

FOUND RH PYLON IB SKIN CRACK AT NAC STA 170.78 BELOW PANEL 442 AL. THE CRACK LENGTH IS 1.4". RH PYLON INBOARD SKIN CRACK REPAIRED IAW EO 767-54-0007

Part: CONNECTOR — DAMAGED (RT A/C PACK) · airframe 84,712 hrs · 21,537 cycles

REMOVED AND REPLACED RH PACK COMPRESSOR O/H SWITCH CONNECTOR @1562 BACKSHELL CLAMP IAW SWPM 21-61-11

Part: CONNECTOR — CRACKED (LT A/C PACK) · airframe 84,712 hrs · 21,537 cycles

FOUND LH PACK COMPRESSOR OH SWITCH CONNECTOR D01576 CRACKED. REMOVED AND REPLACED CONNECTOR D01576 IAW SWPM 20-61-00

Part: SHUTOFF VALVE — NO TEST (NR 2 ENGINE) · airframe 84,712 hrs · 21,537 cycles

DURING #2 ENG TCC AIR SHUTOFF VALVES TEST, FOUND HPT TCC AIR SHUTOFF VALVE FAILED. REMOVED AND REPLACED #2 ENG HPT TCC AIR SHUTOFF VALVE IAW AMM 75-24-03. OPS CHECKS AND ADJUSTMENTS OK.

Part: CONNECTOR — CRACKED (A/I PRESS SWITCH) · airframe 84,712 hrs · 21,537 cycles

LH WING TAI PRESSURE SWITCH CONNECTOR D2388 CRACKED. REPLACED L WING TAI PRESSURE SWITCH CONNECTOR D238 IAW SWPM 20-61-11, TESTED PER 30-41-04 OPS CHECK GOOD.

Part: SHUTOFF VALVE — NO TEST (LEFT) · airframe 84,712 hrs · 21,537 cycles

LH PRSOV BITE TEST FAIL. REMOVED AND REPLACED LH PRSOV IAW AMM 767-36-11-09

Part: SWITCH — FAILED (BAROMETRIC) · airframe 84,712 hrs · 21,537 cycles

FOUND THE BAROMETRIC SWITCH S495 MALFUNCTION. REMOVED AND REPLACED #2 ENG BAROMETRIC SWITCH S495 AS PER AMM 75-23-04. PART IS UNKNOWN TO TRAX.

Part: DOOR FRAME — CRACKED (FWD SERVICE DOOR) · airframe 84,712 hrs · 21,537 cycles

FOUND A CRACK AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWE CORNER FASTENING HOLES. THE DAMAGED AREA WAS TRIMMED OUT. REPAIR PARTS MADE AND INSTALLED IAW SRM 53-10-01-2R.

Part: BOLT — FAILED (COWL DR HINGE) · airframe 84,712 hrs · 21,537 cycles

FOUND #2 ENG CORE COWL HINGE BOLT COULD NOT SELF LOCK. REPLACED #2 ENG CORE COWL HINGE BOLT IAW 767-300 AMM 71-11/

Part: TORQUE BOX — CRACKED (RT NACELLE) · airframe 84,712 hrs · 21,537 cycles

FOUND RH PYLON FWD TORQUE BOX UPPER SKIN OB DRAIN HOLE CRACK. THE CRACK LENGTH IS 2.7", REPAIRED AS PER DRAFT EO 767-54-0006

Part: VALVE — FAILED (LT NACELLE) · airframe 84,712 hrs · 21,537 cycles

L NAC COOLING VALVE TEST FAIL. REMOVED AND REPLACED THE NAC COOLING VALVE AS PER B767-300 AMM 75-23-02. PART IS UNKNOWN TO TRAX.

Part: SMOKE DETECTOR — INOPERATIVE (EQUIP COOLING) · airframe 84,712 hrs · 21,537 cycles

DURING ENE COOLING SYSTEM EQUIP COOL TEST, SMOKE LIGHT NOT ON. REMOVED AND REPLACED EQUIP COOLING SMOKE DETECTOR, INSPECTION TEST GOOD IAW AMM 21-58-19

Part: DUCT — CRACKED (APU) · airframe 84,712 hrs · 21,537 cycles

LH WW APU AIR BLEED DUCTING FOUND CRACK. REPLACED LH WW APU AIR BLEED DUCTING CARRIED OUT LEAK CHECK FOUND SATIS PER 767-300 AMM 36-11-01

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 84,697 hrs · 21,536 cycles

L ENG HPSOV. PERFORMED AIR SUPPLY BITE TEST, STATUS MESSAGE CLEARED, NO FAULTS NOTED.

Part: CONTROLLER — NO TEST (PNEUMATIC SYS) · airframe 84,712 hrs · 21,537 cycles

PERFORM RH AND LH PNEUMATIC HEALTH CHECK. PERFORMED RH AND LH PNEUMATIC HEALTH CHECK IAW AMM 36-00-22. REPLACED HPC PN# 773289-15 SN# 200008067 4659FH 1488 FC. REPLACED PRVC PN# 792755-16 SN# 910169 FH AND FC UNKNOWN. REPLACED PRV PN# 820170-10 SN# A95030012 4659FH 1488 FC. REPLACED PRVC PN# 792755-14 SN# 920413. 4581 FH 1470 FC.

Part: CONTROL PANEL — FAILED (HF RADIO) · airframe 84,534 hrs · 21,499 cycles

RIGHT HF RADIO BLANK/NO POWER. REMOVED AND REPLACED HF COMM CONTROL PANEL PER AMM 23-11-02.

Part: CONTROL PANEL — FAULTED (HF RADIO) · airframe 84,528 hrs · 21,498 cycles

RIGHT HF RADIO BLANK/NO POWER. RESET HF COMM CONTROL PANEL PER AMM 23-11-00. OPS CHECK GOOD.

Part: HF COMM — FAULTED (RIGHT) · airframe 84,485 hrs · 21,989 cycles

RIGHT HF RADIO FAIL IN ITS DISPLAY WINDOW. RESET RH HF CONTROL PANEL PER AMM 23-11-00 OPS CHECK GOOD.

Part: CONTROL PANEL — FAILED (RT HF COMMS) · airframe 84,343 hrs · 21,460 cycles

RH HF COMM CONTROL PANEL CASE DIGIT TURNING KNOB INOP. REMOVED AND REPLACED RH HF COMM CONTROL PANEL PER AMM 23-11-02 OPS CHECK GOOD. UNIT IS UNKNOWN TO TRAX

Part: DISPLAY — INOPERATIVE (HF SELECT PANEL) · airframe 84,160 hrs · 21,424 cycles

RH HF SELECT PANEL DISPLAY INOP. DEFERRED PER MEL 23-11-01-02B CAT C@ 0154Z 2-28-2024. REMOVED AND REPLACED HF FREQ SELECT PANEL PER AMM 23-11-02 OPS CHECK GOOD.

Part: LATCH HANDLE — OUT OF ADJUST (FO WINDOW) · airframe 84,098 hrs · 21,412 cycles

FO WINDOW OPENED DURING TO ROLL. ADJUSTED TENSION ON WINDOW LATCHING HANDLE, AND WINDOW'S INBOARD/OUTBOARD ALIGNMENT PER AMM 56-11-02. CHECKS GOOD FOR SECURITY, NO DEFECTS FOUND, ADJUSTMENTS MADE TO THE UPPER SERVICEABLE LIMITS

Part: BLADE — CRACKED (NR 1 ENG FAN) · airframe 84,077 hrs · 21,408 cycles

#1 ENG #28TH BLADE HAS A 3.968 MM CRACK ON THE LEADING EDGE AREA F SURFACE, 8" FROM THE PLATFORM BASE. PERFORMED 1ST STAGE FAN BLADE REPAIR ON #1 ENG #28 BLADE PER AMM 72-31-02, PERFORMED FLUORESCENT PENETRANT INSPECTION, OK FOR SERVICE FINAL DEPTH 4.783 MM

Part: WARNING LIGHT — INOPERATIVE (WINDOW HEAT) · airframe 83,990 hrs · 21,391 cycles

PILOT REPORTED R1 WINDOW HEAT LIGHT INOP DURING FLIGHT. FLIGHT DECK WINDOW HEAT SYSTEM #2 SIDE DEFERRED IAW MEL 30-41-01.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 83,893 hrs · 21,372 cycles

LEFT ENGINE ANTI-ICE. REMOVED AND REPLACED ENGINE THERMAL ANTI-ICE VALVE IAW AMM 30-21-03 OPS CHECK OK. UNIT IS UNKNOWN TO TRAX.

Part: FAIRING — DAMAGED (LT WNG-BDY) · airframe 83,821 hrs · 21,359 cycles

IMPACT DAMAGE FOUND AT LH AFT WING/BODY FAIRING 195PL, STA 1222-1230, WL-160. COMPLETED TEMP REPAIR PER NAC EO 767-53-0040. DVI OF TAPE ONCE PER FLIGHT DAY, REPLACE IF DETERIORATED. ONCE PER WEEK TAP TEST, ANY GROWTH IN DAMAGE MUST NOTIFY NAC ENGINEERING.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,597 hrs · 21,311 cycles

FOUND #2 ENG INBOARD EXH COWL HOLD OPEN ROD BROKEN. ITEM PUT ON DEFERRAL PER DMI 71-11 CAT A, EXPIRING ON 1/1/24

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,414 hrs · 21,272 cycles

RIGHT SIDE HF TUNING SELECTOR DOES NOT ADJUST NUMBER FROM #2, UNABLE TO USE DIFFERENT FREQUENCIES. FOUND RH HF PANEL SELECTOR SWITCH INOP, REMOVED AND REPLACED PANEL ASSY HF COMMUNICATIONS, OPS CHECK GOOD. PER AMM 23-11-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,287 hrs · 21,246 cycles

FOUND #2 ENGINE BLADE #20 AREA A LEADING EDGE HAS A NICK. BLENDED #2 ENGINE BLADE #20 AREA A NICKS PER AMM 72-31-00 BLENDED BLADE WITHIN LIMITS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,067 hrs · 21,201 cycles

APU BLEED AIR NO START. DEFERRED APU BLEED VALVE PER MEL 36-11-04

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,037 hrs · 21,195 cycles

AFTER RIGHT ENGINE START APU BLEED VALVE ON EICAS. DEFERRED APU BLEED VALVE PER MEL 36-11-04 10-7-23

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,042 hrs · 21,196 cycles

LEFT SIDE WX FAIL. DEFERRED PER MEL 34-43-01, LEFT SYSTEM WEATHER RADAR INOP CAT D, 10/8/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,032 hrs · 21,194 cycles

FOUND ON DAILY CHECK APU DUCT AIR SURGE HAS A HOLE. REMOVED AND REPLACED APU DUCT AIR SURGE PER AMM 49-53-01(2) OPS CHECK AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,017 hrs · 21,191 cycles

MECHANICAL IRREGULARITY NO AIR OUTPUT FROM APU. DEFERRED APU BLEED VALVE PER MEL 36-11-04

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,788 hrs · 21,144 cycles

APU FUEL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED APU FUEL FILTER ELEMENT IAW AMM 49-31-04 NO LEAKS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,714 hrs · 21,125 cycles

DURING POST FLIGHT WALK AROUND #1 ENGINE #15 BLADE HAD A NICK ON LEADING EDGE. BLENDED #1 ENG FAN BLADE #15 WHICH IS 18" FROM BLADE TIP .015" WITHIN SERVICEABLE LIMITS AS PER PW AMM 72-31-02. NDT INSPECTION COMLETED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,764 hrs · 21,109 cycles

#2 ENGINE BLADE #2 HAS NICK. REMOVED NICK AT #2 ENG #2 BLADE DISTANCE 3/4 LENGTH =-204 DEPTH .054, IS WITHIN LIMITS IAW B767-300 AMM 72-31-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,764 hrs · 21,109 cycles

#2 ENG #8 BLADE HAS NICK. REMOVED NICK AT #2 ENG BLADE #8. DISTANCE 11 1/8, DEPTH 0.65, LEGTH 0.458 IS WITHIN LIMITS. IAW B767-300 AMM 72-31-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,674 hrs · 21,109 cycles

#2 ENG BLADE #7 HAS NICK. REMOVED NICK @ #2 ENG BLADE #7 DISTANCE 2.25 LENGTH -80 DEPTH .084, IS WITHIN LIMITS IAW B767-300 AMM 72-31-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,663 hrs · 21,103 cycles

ON POST FLIGHT FOUND L ENGINE BLADE #15 DINGED AT TIP OF LEADING EDGE OUTWARD. REPAIRED BLADE #15 IAW B767 AMM 72-31-02. NDT GOOD.