N567NC

ATA 7220

Part: VANE — BROKEN (ENGINE) · airframe 70,209 hrs · 13,024 cycles

ONE EA FAN EXIT VANE OF THE NR 2 ENGINE HAS A BROKEN PLATFORM AT THE INNER BASE OF PART. PERFORMED EVALUATION IF 1 EACH FAN EXIT VALVE OF #2 ENG BROKEN PLATFORM NO ADITIONAL DEFECTS NOTED. REPAIRED FAN EXIT VALVE IAW 72-33-02-308-003-N00 .

ATA 7421

Part: IGNITER — WORN (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENG LOWER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 LOWER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.

ATA 7497

Part: CABLE — CRACKED (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENG LOWER IGNITION EXCITER CABLE BUSHING UNDER CERAMIC SLEEVE CRACKED. DOT 048200. REMOVED AND REPLACED NR 2 ENG LOWER IGNITION EXCITER CABLE IAW B767 AMM 74-21-01-004-001-N00. TEST OK. PO # GYR10300795. TW ID T100360-1 D/D 8/12/26. MECH: ALD025 10/06/2025 INSP: AQC029 10/06/2025 PC035 10/06/2025

ATA 2612

Part: CIRCUIT CARD — FAULTED (FIRE DETECTION) · airframe 70,215 hrs · 13,024 cycles

LEFT ENGINE FAILED AUTOMATIC FIRE / OVERHEAT LOGIC /TEST SYSTEM (AFOLTS) SYSTEM CHECK. CARDS WERE REPLACED WITH PN S332T301-181 SN 940, 699, 8823 AND 6780

ATA 7421

Part: IGNITER — WORN (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENGINE UPPER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 UPPER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.

ATA 7220

Part: VALVE — CRACKED (NR 1 ENGINE) · airframe 70,215 hrs · 13,024 cycles

IP VALVE ON #1 ENGINE HAS SIGNS OF CRACKING AND CORROSION ON FUSELAGE. INSTALLED SERVICEABLE IP VALVE ON # 1 ENG IAW AMM 36-11-06-404-033-002. NO LEAK NOTED.

ATA 7500

Part: SCREEN — DAMAGED (NR 1 ENG BLEED) · airframe 70,215 hrs · 13,024 cycles

NR 1 FAN EXIT CASE BLEED AIR DUCT, BLEED SCREENS 8 EA FROM UPPER DUCTS ARE BROKEN / MISSING. REMOVE AND REPLACE 6 EA SCREENS ON #1 ENG ESN 724378 IAW AMM 72-00-00-416-342-N00 REMAINING 2 EA UPPER SCREENS FOUND TO BE IN SERVICEABLE CONDITION IAW AMM TASK 75-32-206-001-N00 TABLE 603

ATA 7700

Part: SENSE LINE — CHAFED (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

STATIC PRESSURE SENSE LINE TUBE CHAFED ON #2 ENG. INBD FAN COWL. REMOVED AND REPLACED STATIC PRESSURE SENSE LINE TUBE ON #2 ENG INBD FAN COWL. LEAK TEST AND STATIC TEST GOOD IAW B767 AMM 71-00-02-844-002-N00 STEP 2 AMM 71-00-02-844-077-N00 STEP 7 AMM 71-00-00-795-014-N00 AND AMM 71-00-00-745-002-N00

ATA 2430

Part: CONTROL UNIT — FAULTED (ELECTRICAL) · airframe 70,215 hrs · 13,024 cycles

BUSS POWER CONTROL UNIT HAS A FAULT MESSAGE IDG / OIL OUT. PERFORMED BPCU BITE PROCEDURE PER B-767 FIM 24-30 FAULT TREE 801. BITE PROCEDURE OK.

ATA 7200

Part: LINER — MISINSTALLED (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

6 TO 7 O'CLOCK (LOOKING FWD) FAN EXIT LINER NOT PROPERLY FAIRED ON #2 ENGINE. REPAIRED FAIRED FAN EXIT LINER ON #2 ENGINE AT 6 TO 7 O'CLOCK POSITION, REPLACED BROKEN SUPPORT BRACKETS FOR LINER REF MAN-PW4ENG-109 PG 18 AND SRM 51-40-02 STEP 4 (B).

ATA 7200

Part: SEALANT — MISSING (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

10 O'CLOCK (FWD LOOKING) FAN EXIT STRUT LOWER SURFACE MISSING SEALANT ON NR 2 ENGINE. APPLIED SEALANT ON FAN EXIT STRUT LOWER SURFACE #2 ENG AT 10 O'CLOCK PER B767 AMM 73-3405 TASK 72-34-05-404-005-N00 PAR D (3) (E).

ATA 7421

Part: IGNITER — WORN (NR 1 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 1 ENG. SYS. 1 TOP IGNITION EXCITER PLUG IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.

ATA 7261

Part: OIL TUBE — UNSECURE (NR 1 ENGINE) · airframe 70,215 hrs · 13,024 cycles

BROKEN CLAMP ON OIL TUBE FWD OF OIL TANK ON #1 ENGINE. INSTALLED NEW CLAMP ON FIRE EXT. TUBE FWD OF OIL TANK ON #1 ENGINE PER AMM 20-11-00 TABLE 213/20-11-00-993-830

ATA 7412

Part: EXCITER — DAMAGED (NR 1 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 1 ENG TOP IGNITION EXCITER INSIDE OUTPUT RECEPTACLE WELL HAS DAMAGE / SIGNS OF ARCING ON THE CONTACT BUTTON. REMOVED AND REPLACED #1 ENG TOP IGNITION EXCITER IAW B767 AMM 74-11-01-004-001-N00 AND AMM 74-11-01-404-019 STEP 3.

ATA 7261

Part: SEAL — DETERIORATED (NR 2 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENGINE SEAL ATTACHED TO OIL DRAIN COLLECTOR IS DAMAGED & DETERIORATING. REMOVED & REPLACED NR 2 ENG SEAL ATTACHED TO OIL DRAIN COLLECTOR IAW AMM 51-31-01-302-001 AND 51-31-01-392-013.

ATA 5400

Part: CLAMP — MISINSTALLED (ZONE 400) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.

ATA 7200

Part: SEALANT — MISSING (ENGINE) · airframe 70,215 hrs · 13,024 cycles

SEVERAL FAN EXIT (INNER FRONT) FAIRINGS SEGEMENTS MISSING SEALANT AROUND COMPRESSOR SECTION CASE ON NR 2 ENG. APPLIED RTV SEALANT TO FAN EXIT (INNER FRONT) FAIRING SEGMENTS IAW B767-300 REF. AMM 72-34-03.

ATA 5400

Part: CLAMP — UNSECURE (ZONE 400) · airframe 70,215 hrs · 13,024 cycles

NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED. PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148 .

ATA 7421

Part: IGNITER — WORN (NR 1 ENGINE) · airframe 70,215 hrs · 13,024 cycles

NR 1 ENG IGNITOR PLUG FOR SYSTEM 2 (BOTTOM PLUG) IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.

ATA 2897

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 70,096 hrs · 13,000 cycles

DURING TROUBLESHOOTING FOUND LEFT FWD FBP CONNECTOR D1550 PIN #6 WILL NOT SECURE. REPLACED FUEL PUMP CONNECTOR D1550 PER SWPM 20-61-00 OPS CHECK GOOD PER AMM 28-42-01

ATA 2822

Part: PRESSURE SWITCH — FAILED (FUEL BOOST) · airframe 70,096 hrs · 13,000 cycles

AFTER LEFT ENGINE START L FWD BOOST PUMP PRESSURE LIGHT ILLUMINATED AND ASSOCIATED EICAS MESSAGE. REPLACED LEFT FWD PUMP PRESSURE SWITCH OPS CHECK GOOD PER AMM 28-42-01 PART IS UNKNOWN TO TRAX.

ATA 7261

Part: COOLER — FAILED (RT ENGINE) · airframe 70,086 hrs · 12,998 cycles

RIGHT ENGINE OIL QTY DROPPED FROM 17 UNITS TO 12 DURING FLIGHT. SUSPECT OIL LEAK STILL PRESENT. FOUND OIL PUDDLING AT 6 OCLOCK OF ENGINE WITH EVIDENCE OF OIL LEAKAGE ON THE LH SIDE OF ENGINE CORE EMANATING FROM AIR/OIL COOLER. REMOVED AND REPLACED #2 ENGINE AIR/OIL COOLER IAW AMM 79-21-09 OPS CHECK LEAK CHECK GOOD. PART IS UNKNOWN TO TRAX.

ATA 7261

Part: HEAT EXCHANGER — LOOSE (ZONE 400) · airframe 70,081 hrs · 12,997 cycles

#2 ENGINE SHOWS SIGNS OF OIL LEAK. FOUND BNUT ON FUEL OIL HEAT EXCHANGER LOOSE, TIGHTENED B-NUT REF B767 300 AMM 20-41-60 OPS AND LEAK CHECK GOOD.

ATA 2150

Part: SENSOR — FAILED (ZONE 100) · airframe 70,065 hrs · 12,994 cycles

LEFT PACK TEMP EICAS MESSAGE CAME ON THEN WENT OUT BEFORE WE COULD DO THE QRH. PERFORMED L PACK TEMP CONTROLLER BITE PER FIM 21-51 FT 803. FOUND COMPUTER SENSOR FAULT,. REMOVED AND REPLACED LEFT PACK COMPRESSOR AUTO OUTLET SENSOR PER AMM 21-51-05 OPS CHECK GOOD. NO PART INFORMATION AVAILABLE IN TRAX

ATA 3150

Part: FAULT MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 70,060 hrs · 12,993 cycles

LEFT PACK OFF EICAS MESSAGE, LEFT PACK TEMP ON DESCENT. FOLLOWED QRH, DID NOT CLEAR. PERFORMED LEFT PACK BITE TEST FIM 21-51 FT 814 PACK FAULT CLEARED OPS CHECK GOOD.

ATA 2822

Part: RELAY — FAILED (BOOST PUMP) · airframe 70,060 hrs · 12,993 cycles

LEFT FWD BOOST PUMP GFI NEEDS REPLACED. REPLACED L FWD BOOST PUMP GFI RELAY PER 767 AMM 28-22-18, OPS CHECK GOOD. NO TIME INFO AVAILABLE IN TRAX.

ATA 2822

Part: PUMP — WARNING MESSAGE (ZONE 500) · airframe 70,059 hrs · 12,992 cycles

LEFT FORWARD FUEL PUMP CAME ON IN DESCENT. PERFORMED OPS TEST OF ENGINE FUEL FEED SYSTEM IAW AMM 28-22-00, OPS CHECKED GOOD.

ATA 2822

Part: PUMP — FAULTED (FUEL) · airframe 70,053 hrs · 12,991 cycles

LEFT FWD FUEL PUMP EICAS CAME ON IN-FLIGHT, AND LEFT FWD FUEL PUMP PRESSURE LIGHT ILLUMINATED. RAN THE QRH. PERFORMED FIM 28-22 FAULT TREE 819. BLED L FWD FUEL PUMP PRESSURE SENSE LINE PER AMM 28-22-03, OPS CHECK AND LEAK CHECK GOOD.

ATA 2800

Part: CONTROL PANEL — FAILED (FUEL SYSTEM) · airframe 70,038 hrs · 12,975 cycles

FUEL SYSTEM CONTROL PANEL HAS BROKEN KORRY LIGHT. REMOVED AND REPLACED FUEL MANAGEMENT PANEL REF 767-300 AMM 28-22-17 OPS CHECK GOOD.

ATA 2822

Part: PUMP — FAILED (FUEL BOOST) · airframe 70,038 hrs · 12,975 cycles

LEFT FWD BOOST PUMP DID NOT COME ON WITH SWITCH IN ON POSITION. REMOVED AND REPLACED LH FWD BOOST PUMP REF 767 AMM 28-22-03 OPS CHECK GOOD.

ATA 4920

Part: APU — MALFUNCTIONED (ZONE 100) · airframe 70,033 hrs · 12,974 cycles

APU WILL NOT START. PERFORMED APU STARTING AND OPERATION PER AMM 49-11-00, OPS CHECK OKAY.

ATA 2822

Part: PUMP — FAILED (FUEL BOOST) · airframe 70,033 hrs · 12,987 cycles

LEFT FWD FUEL PUMP PRESS LIGHT CAME ON. RAN THE QRH AND THE LIGHT WENT AWAY BUT IT CAME BACK ON PRIOR TO ENTERING OUR EEP. MI AT 1540 DUE TO LEFT FWD FUEL PUMP PRESSURE. REPLACED LEFT FWD BOOST PUMP IAW AMM 28-22-00 PERFORMED OPS CHECK PER AMM 28-22-00 BOTH OPS AND LEAK CHECK OKAY.

ATA 3150

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 70,020 hrs · 12,984 cycles

SHORTLY AFTER LEVEL OFF, STATUS MESSAGE LEFT FWD FUEL PUMP BUT NO FAULT FLAG ON PUMP SWITCH. MESSAGE CLEARED AFTER AROUND 30 SECONDS. PERFORMED OPS CHECK OF LEFT FWD FUEL PUMP, NO FAULTS FOUND. PER AMM 28-22-03.

ATA 3150

Part: WARNING LIGHT — ILLUMINATED · airframe 69,912 hrs · 12,951 cycles

LEFT FWD FUEL PRESS LIGHT ILLUMINATED. NO EICAS MESSAGE.

ATA 7500

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 69,664 hrs · 12,879 cycles

LH ENGINE BLEED DOES NOT CLOSE ON ENGINE SHUTDOWN, CAUSES A LOW RUMBLING NOISE WITH AIR HISSING OUT FROM APU BLEED. THIS HAS BEEN AN INTERMITTENT ISSUE. REMOVED AND REPLACED THE LH PRSOV IAW AMM 36-11-09 OPS NORMAL

ATA 4990

Part: BLEED AIR SYS — NO DISCREPANCY (ZONE 100) · airframe 69,662 hrs · 12,877 cycles

L ENG BLEED DOES NOT CLOSE ON ENGINE SHUTDOWN. CAUSES A LOUD NOISE WITH AIR RUSHING FROM APU BLEED. PERFORMED L ENGINE IDLE RUN PER AMM 71-00-00 L ENG BLEED VALVE OPERATED NORMALLY. AFTER ENGINE SHUTDOWN NO LEAKS NOTED WITH APU BLEED AIR IAW AMM 49-11-00

ATA 4900

Part: HOUR METER — INOPERATIVE (ZONE 100) · airframe 69,642 hrs · 12,868 cycles

APU HOUR METER INOP. REMOVED AND REPLACED THE POSITIVE TERMINAL OPS CHECK NORMAL IAW AMM 49-12-01

ATA 2150

Part: WARNING LIGHT — ILLUMINATED (LT A/C PACK) · airframe 69,627 hrs · 12,860 cycles

LEFT PACK LIGHT ON AFTER ENGINE START. DEFERRED PER MEL 21-51-01-01 CAT C ON 6/1/2025. REMOVED AND REPLACED THE LH PACK ON/OFF SWITCH IAW CMM 21-51-19, OPS CHECK NORMAL IAW AMM 21-51-00.

ATA 4900

Part: METER — STUCK · airframe 69,613 hrs · 12,853 cycles

APU HOURMETER STUCK AT 4644 HRS. REMOVED AND REPLACED APU HOURMETER IAW AMM 49-72-01 OPS CHECK NORMAL.

ATA 2150

Part: CONTROL VALVE — FAULTED (ZONE 100) · airframe 69,606 hrs · 12,850 cycles

LEFT PACK OFF EICAS MESSAGE AND ASSOCIATED PACK OFF DISCRETE LIGHT. ACCOMPLISHED LEFT CONTROLLER BITE TEST AND NO FAULTS RECORDED. PER COMPANY CONVENIENCE REMOVED AND REPLACED LEFT FLOW CONTROL AND SOV PER AMM 21-51-01 POST INSTALLATION CHECKS GOOD.

ATA 2150

Part: CONTROL VALVE — FAILED (ZONE 100) · airframe 69,698 hrs · 12,847 cycles

DURING ENGINE RUN RH FLOW CONTROL VALVE FAILED, REMOVED AND REPLACED RH PACK FLOW CONTROL VALVE IAW AMM 21-51-01 LEAK AND OPS CHECK GOOD.

ATA 3150

Part: WARNING LIGHT — INTERMITTENT (ZONE 200) · airframe 69,598 hrs · 12,847 cycles

RIGHT BLEED OFF INTERMITTENT DURING DESCENT. CORRECTIVE ACTION IN PROGRESS.

ATA 3150

Part: WARNING LIGHT — INTERMITTENT · airframe 69,598 hrs · 12,847 cycles

RIGHT BLEED OFF INTERMITTENT DURING DESCENT. OPS CHECKED RIGHT BLEED SYSTEM IAW AMM 31-11-00 AND 71-00-00 CHECKED NORMAL ON RUNUP. SEE PROJECT WORKSHEET FOR INSPECTION AND TROUBLESHOOTING AND MAINT ACTIONS.

ATA 2150

Part: A/C PACK — FAULTED (ZONE 100) · airframe 69,598 hrs · 12,847 cycles

RETURN TO LAX 2357 ALT 350FL RIGHT PACK OFF. REFER TO PROJECT WORKSHEET FOR TROUBLESHOOTING AND MAINTENANCE ACTIONS. REPLACED RH COMPONENTS LISTED ON B104065 THROUGH 067.

ATA 2150

Part: A/C PACK — INOPERATIVE (RIGHT) · airframe 69,598 hrs · 12,847 cycles

RETURN TO LAX 2357 ALT 350FL RIGHT PACK OFF. CORRECTIVE ACTIONS IN PROGRESS

ATA 2150

Part: A/C PACK — FAULTED (ZONE 100) · airframe 69,587 hrs · 12,843 cycles

RIGHT PACK OFF CAUTION ILLUMINATED 2 1/2 HOURS INTO FLIGHT. RAN QRH CHECKLIST, NO ACTIONS NEEDED, CONTINUED TO PHNL. PERFORMED RIGHT PACK TEMP CONTROLLER BITE PER FIM 21-51 FAULT TREE 844, NO FAULTS FOUND. R PACKS OPS CHECK GOOD ON GROUND PER AMM 21-51-00

ATA 2130

Part: BLEED VALVE — FAILED (ZONE 100) · airframe 69,514 hrs · 12,845 cycles

LEFT AND RIGHT PACK OFF EICAS MESSAGE FOLLOWED BY CABIN DEPRESSURIZATION FOLLOWED BY CABIN AUTO INOP EICAS. FOUND LEFT BLEED SYSTEM AT FAULT REPLACED COMPONENTS REF LOGPAGE B104059, B104060, AND B104061 FOUND LEFT ENG HP VALVE SHAFT BEARING EXCESSIVE PLAY. REMOVED AND REPLACED LH ENG HP VALVE. PART NOT IN TRAX, NO HOURS OR CYCLES.

ATA 7421

Part: IGNITER — FAULTED (RT ENGINE)

REMOVED AND REPLACED RIGHT ENG #2 IGNITER PLUG AND #2 IGNITION EXCITER OPS CHECK GOOD.