N399CM

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,664 hrs · 11,409 cycles

R GEN CONTROL PUSHBUTTON SWITCH FAULTY ON P5 ELEC CONTROL PANEL. REMOVED AND REPLACED GEN CONTROL SWITCH PER AMM 24-22-21

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,659 hrs · 18,906 cycles

APU DOOR STAYING OPEN AFTER SHUTDOWN ON DEPARTURE, FOUND CONNECTOR D052 CONTAMINATED, CLEANED CONNECTOR D502 PER SWPM 20-60-02 OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,591 hrs · 18,883 cycles

MI DUE TO PROBE HEAT EICAS MESSAGE AFTER ENGINE START ON THE GROUND AT TPBP. ACCOMPLISHED FIM 30-31 FT 802/803/804, ALL PROBLES WORKING NORMALLY WITH ENGINES OFF. CHECKED SSM 30-31-01 AND RESEATED RELAY K646 R PROBE HT N2 OPS CHECKED PER AMM 71-00-00 PITOT PROBES WORKING NORMALLY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,591 hrs · 18,883 cycles

EICAS MESSAGE PROBE HEAT AFTER LANDING AT TPBP. ACCOMPLISHED PITOT HEAT CHECK PER AMM 30-31-00 ADA OPS CHECK GOOD AMM 30-32-00, ALSO CW FIM 32-02 FT 803 PSEU FAULT CODE O7 NO FAULTS FOUND AFTER RESET, OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,588 hrs · 18,882 cycles

FOUND COUPLING OF COOLING DUCT AT 4 OCLOCK POSITION LOOSE. REMOVED AND REPLACED LPT COOLING DUCT AT 4 OCLOCK POSITION ON #1 ENGINE IAW AMMM 75-24-03

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,588 hrs · 18,882 cycles

DURING PREFLIGHT WALKAROUND FOUND BOLT STICKING OUT OF #1 ENGINE CORE COWL. INSTALLED BOLT ON #1 ENGINE LPT COOLING SUPPORT BLANKET AT 5 OCLOCK POSITION IAW AMM 75-24-03

Part: CONTROLLER — FAILED (UNKNOWN) · airframe 110,413 hrs · 18,804 cycles

R ENG PRV EICAS MSG ON CLIMB AND EXTINGUISH AROUND 18000 FT. PER FIM 36-10 FLT 847 REMOVED AND REPLACED PRV CONTROLLER IAW AMM 36-11-19 LEAK CHECK AND INSTALLATION TEST NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,156 hrs · 18,730 cycles

EGT INOP IN FLIGHT - LEFT. PERFORMED FIM FT TASK 804 FOUND THERMOCOUPLE LEAD LOOSE, RESECURED AND PERFORMED SYS TEST AND ETOPS VERIFICATION REF AMM 77-21-00-501 SYS OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,875 hrs · 18,666 cycles

IN FLIGHT LEFT EGT FLUCTUATED BETWEEN 300-600 MOST OF THE FLIGHT. PERFORMED FIM 77-21 FAULT TREE 806, FOUND THERMOCOUPLE CABLE CONNECTOR P3 LOOSE AND CAUSED EGT FLUCTUATION WHEN SHAKING ON THE GROUND. CLEANED AND REFORMED P3 CONNECTOR PER WPM 20-60-01

Part: SENSOR — FAILED (UNKNOWN) · airframe 109,790 hrs · 18,647 cycles

RIGHT PACK TEMP, RIGHT PACK TEMP INOP PACK OFF. TROUBLESHOOT RH PACK SYSTEM FOUND BAD WIRE AND DEFECTIVE COMPRESSOR OUTLET SENSOR. REMOVED AND REPLACED OUTLET SENSOR IAW AMM 21-51-06 OPS CHECK GOOD. AND SECURED LOOSE WIRE. PART UNIT UNKNOWN TO TRAX

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,564 hrs · 18,595 cycles

RIGHT GEN EICAS MESSAGE CAME UP JUST AS SOON AS THRUST REVERSERS WERE DEPLOYED AND IT WENT AWAY WHEN REVERSERS WERE STOWED. FOUND CANNON PLUG D01966 LOSE ON RH IDG. RESECURED CANNON PLUG PER SWPM 20-60-07, PERFORMED OPS CHECK ON RH IDG, OPS CHECK GOOD PER AMM 71-00-00

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,542 hrs · 18,590 cycles

SUPPLEMENTAL INFORMATION

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,549 hrs · 18,592 cycles

SUPPLEMENTAL INFORMATION

Part: UNKNOWN — UNKNOWN (UNKNOWN)

MX DELAY APU NO START. FOUND APU BATTERY DEAD, REPLACED BATTERY AND CHARGER PERFORM APU OPS CHECK REF B767-AMM 49-11-00-501 OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,508 hrs · 18,582 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED B767 21-31 FAULT TREE 812 AND 803, SYSTEM TESTS OK, NO FAULTS FOUND.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,508 hrs · 18,582 cycles

EEC INOP LIGHTS WILL NOT SWITCH ON WHEN SWITCHES TURN OFF. REPLACED EEC MODULE ASSY PER AMM 73-21-13

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

SX NR 6500161621 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 2" AFT OF STA1832 AND 9" ABOVE THE RH SIDE APU DOOR HINGE. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T=0.030", THE DEPTH OF CLEANUP X=0.002" < 15%T. FOUND WITHIN LIMITS AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

RHW I/B FLAP O/B AFT FAIRING LOWER SURFACE FOUND CRACK. RHW 2/B FLAP O/B AFT FAIRING LOWER REAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 2 & SRM 51-70-03. REV 122 - APR 15/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

FOUND THE NO.1 ENGINE CONNECTOR D10996P POOR CONDITION. THE NO.1 ENGINE CONNECTORE D10996P REPLACED AS PER B767-300 SWPM 20-61-11 REV 82 CARRIED OUT FUEL FILTER BYPASS WARNING TEST PER 73-34-00 REV 139. FOUND SATIS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

NO.2 ENG NOSE COWL L/E SKIN AT 10 O'CLOCK FOUND CORROSION. MEASURED THE REWORKED AREA AFT CORROSION REMOVALS, DEPTH OF CLEANUP = 0.037>10% ORIGINAL THICKNESS T =0.080", REMAINING THICKNESS = .043", FOUND EXCEED LIMIT AS PER B767-300 SRM 54-12-01-1A-1 REV 122 APR 15/2023. CARRED OUT THE REPAIR AT NOSE COWL LIP SKIN OF #2 ENG 10 O'CLOCK AS PER EO 5423-080 REV P1. EO 5423-080 REV COMPARED AND COMPLIED WITH EO 5423-080 REV 1R.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

HFEC INSPECTION FOUND 01 EA CRACK OF LEFT BS883.5 FRAME INNER CHORD TRANSITION RADIUS AT LBL 89 BELOW WL200,IT IS ABOUT 0.2 INCH LONG. CARRIED OUT THE REPAIR AT LH FRAME INNER CHORD OF BS 883.5 LBL89 BELOW WL200 AS PER SB 767-53A0209 REV. 2 JUNE 07, 203.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

- FOUND NO.1 ENG I/B AND O/B FAN COWL FWD LOWER CORNER DELAMINATION. NO. 1 ENG I/B AND O/B FA COWL FWD LOWER CORNER REPAIRED AS PER B767-300 SRM 54-22-01-2R-6 REV 122 -APR15/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

- RHW NO.9 SLAT L/E SKIN AT 41.25 INCH FROM I/B SIDE FOUND CRACK. REPAIRED THE RHW NO.9 SLAT L/E CRACKED SKIN AT 41.25 INCH FROM I/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,581 cycles

- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA960 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 960 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

FOUND R/H ENGINE FIRE DET WIRING W5324-456R-16 W5324-455R-16 DAMAGED. R/H ENGINE FIRE DET WIRING W5324-456-16 W5324-455R-16 REPLACED AS PER B767-300 SWPN 20-10-11-REV 82. CARRIED OUT FIRE DETECTION SYSTEM TEST AS PER B767-300 AMM 26-11-00 REV 139.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

RHW O/B FLAP I/B AFT SUPPORT FAIRING FOUND CRACK. RHW O/B FLAP I/B AFT SUPPORT FAIRING REPAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 1 & SRM 51-70-17. REV 122 - APR 15/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

- INSPECTION THE APU LOW PRESSURE FUEL FILTER DPI FOUND THE RED BOTTON WAS POPPED. FOLLOW B767-300 AMM 49-05-03 REV 139 DATE APR 22, 2023 WHEN DPI BUTTON IS POPPED, THE FUEL FILTER NEED CHANGED. REMOVED AND REPLACED THE FUEL FILTER AS PER B767-300 AMM 49-31-04 REV 139.00 DATE APR 22,2023. CARRIED OUT RESET THE BUTTON AND APU FUEL LEAK CHECK AS PER B767-300 AMM 49-31-04 REV 139 DATE APR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

- LH SCEONDARY HEAT EXCHANGER FOUND CRACK. REMOVED AND REPLACED LH SECONDARY HEAT EXHCNAGER AS PER B767-300 AMM 21-51-02 REV 139 DATE 12APR023 COMPONENT DESCRIPTION: SECONDARY EXCHANGER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

NO.2 ENG COOLING MANIFOLD SUPPORT LINK AT HPT 2 O'CLOCK FOUND WORN. REMOVED AND REPLACED NO.2 ENG COOLING MANIFOLD SUPPORT LINK BEARING AS PER B767-300 AMM 70-50-00 REV. 139 - APR 22/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN BETWEEN STR26R AND STR36R ,BETWEEN STA1832 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE DEPTH OF CLEANUP X=0.003" < 15% T. FOUND WITHING LIMITS AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

FOUND NO.1 ENG LPT COOLING AIR MANIFOLD TUBE BROKEN AT 1 O`CLOCK. REMOVED AND REPLACED NO.1 ENG LPT COOLING AIR MANIFOLD AS PER B767-300 AMM 75-24-03 REVISION NO. 139 - 22 APR 2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

PITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE AROUND STR 2R, BETWEEN STA 368 AND STA 390 THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE DEPTH OF CLEANUP X=0.005" <10%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

FOUND THE FWD CARGO LOWER DOOR CUTOUT A SUPPORT CORROSION AT STA487.67,RBL38 TO RBL 41. REMOVED AND REPLACED THE DAMAGED SUPPORT AT FWD CARGO LOWER DOOR CUTOUT STA 487.67 RBL38 TO RBL41 AS PER B767-300 SRM 51-40-02 REVISION NO. 122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

RHW NO.10 SLAT L/E SKIN AT 41.5 INCH FROM O/B SIDE FOUND CRACK. REPAIRED THE RHW NO.10 SLAT L/E CRACKED SKIN AT 41.5 INCH FROM O/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR 2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

FOUND THE NO.1 ENGINE UPPER ANG LOWER EGT HARNESS BROKEN. REMOVED AND REPLACED THE NO.1 ENGINE UPPER AND LOWER EGT HARNESS AS PER B767-300 AMM 77-21-02 REV 139. C/O THE INSTALLATION TEST FOUND SATIS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

- ENG SPEED FOUND NO.2 LPT VIBRATION SUDDENLY INCREASED. TROUBLESHOOTING PERFORMED AS PER B767-300 FIM 71-05 FAULT TREE 810 REV 139. REMOVED AND REPLACED NO. 2 ENGINE PRV I-SEAL AS PER B767-300 AMM 36-11-18 REV 139. PERFORMED AMM BITE TEST AS PER B767-300 FIM 77-31 FAULT TREE 203. SWITCHED THE ELECTRICAL CONNECTOR TO ALTERNATE / EXTERNAL NO. 1 ACCELEROMETER AS PER B767-300 AMM 77-31-01 REV 139. WIRING CHECKED AS PER B767-300 WDM 77-31-11 REV 18. RECONNECTED THE CRF ACCELEROMETER ELECTRICAL CONNECTOR AND PERFORMED THE ENGINE IDLE TEST AS PER B767-300 AMM 71-00-00 REV 139 NO 2 ENGINE LPT VIBRATION WITHIN LIMITS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

HFEC INSPECTION FOUND 01 EA CRACK ABOUT 0.3 INCH LONG OF THE RIGHT VERTICAL CHORD ON THE AFT BULKHEAD OF THE NOSE WHELL WELL AS MARKED .IT DOES NOT EXTENED BELOW WL159 AND REPAIR IAW BOEING 767-300 SRM 51-70-12. REPAIRED THE CRACKED RIGHT VERTICAL CHORD ON THE AFT BULKHEAD OF THE NOSE WHEEL WELL AS PER B767-300 SRM 51-70-12 FIG 1 REVISION NO 122 APR 15/2023. THIS REPAIR IS CAT "A" REPAIR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

SX NR 6500161718 - PITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE BETWEEN STR2L AND STR3L,FROM STA368 AND STA 390. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X=0.003" <10%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

NO.2 ENG LPT COOLING MANIFOLD AT 5 O'CLOCK FOUND BROKEN. REMOVED AND REPLACED NO.2 ENG LPT COOLING MANIFOLD AT 5 O'CLOCK AS PER B767-300 AMM 75-24-03 REV 139 - APR 22/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

SX NR 6500161617 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN AROUND STR26L ,BETWEEN STA1788 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X = 0.002" < 15%, FOUND WITHIN LIMITS AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA1003 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 1003 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122 - APR 15/2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

- PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 1.5" AFT OF STA132 AND LOOKING AFT AT 1 O'CLOCK. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.080", THE DEPTH OF CLEANUP X=0.004" <15%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

NO.1 ENGINE FOUND 03EA EGT THERMOCOUPLE PROBE LICATED AT 5 O'CLOCK, 6 O'CLOCK & 9 O'CLOCK TERMINAL BROKEN. REMOVED AND REPLACED THE NO. 1 ENGINE 03 EGT THERMOCOUPLEPROBE AS PER B767-300 AMM 77-21-01 REV 139 C/O THE INSTALLATION TEST FOUND SATIS. P/N OFF: 862-7

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,495 hrs · 18,580 cycles

FOUND NO.1 ENG AFT FAN CASE FLANGE CRACK OUT OLD STOP HOLE AT 4 O`CLOCK. MEASURED THE CRACK LENGTH: 5.9"<10" (MAX TOTAL CRACK LENGTH OF ONE SIDE OF FAN CASE). NO OTHER CRACK FOUND THIS SIDE OF FAN CASE. FOUND WITHIN LIMITS AS PER B767-300 AMM 72-33-00-206-001- H00 REV 139 APR 22/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 109,495 hrs · 18,580 cycles

NO.2 PYLON O/B AFT FAIRING ACCESS PANEL FWD HINGE ATTACHMENT FITTINGS FOUND CORROSION. REMOVED AND REPLACED THE ATTACHMENT FITTING AT #2 PYLON O/B AFT FAIRING ACCESS PNL FWD HINGE IAW SRM 51-40-02 REVISION NO.122 APR 15/2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,388 hrs · 18,560 cycles

MAIN DECK FIRE DETECTION B LOOP ZONES 1 TO 8 INOP. DEFERRED MAIN DECK CARGO FIRE DETECTION B LOOP IAW MEL 26-16-02-01 CAT C.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,148 hrs · 18,507 cycles

AFTER ENGINE START, BOTH LH AND RH ENGINES HAD LEFT AND RIGHT EICAS EEC MESSAGES. FOUND PITOT HEAT CBS OUT, RESET CBS. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 NO FAULTS NOTED. ETOPS GROUND VERIFICATION CW.

Part: COUPLER — UNKNOWN · airframe 109,019 hrs · 18,477 cycles

RIGHT HF INOP. REMOVED AND REPLACED RIGHT HF ANTENNA COUPLER IAW TASK 23-11-01-024-001/424-008. PERFORMED RH HF ANTENNA CHECK, OPS CHECK OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,019 hrs · 18,477 cycles

RIGHT HF RADIO COULD NOT TRANSMIT FOR MAJORITY OF FLIGHT. MX PERFORMED TASK 23-11-00-435, RIGHT HF TESTED OPS CHECK OK.

Part: VALVE — FAILED · airframe 108,920 hrs · 18,454 cycles

COULD NOT CHANGE COCKPIT TEMPERATUER WITH ANY OF THE TEMP CONTROL KNOBS. CARGO AREA WAS 80 DEGREE F, FLT DECK VALVE INDICATOR SHOWED FULL COLD. NO CHANGE IN AUTO MODE. FOUND PACK TEMP CONTROL VALVE INDICATING CLOSED/NOT MODULATING, VALVE CONTROL KNOB LOOSE AND JERKY. REPLACED PACK TEMP CONTROL VALVE IAW AMM 21-51-01 OPS CHECK AND LEAK CHECK NORMAL. PART IS UNKNOWN TO TRAX (ORIGINAL TO AC).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,786 hrs · 18,424 cycles

STATUS MSG R ENG PRV. PERFORMED FIM 36-10 FT 847, FOUND PRSOV TERMINAL 3 LOOSE, SECURED TERMINAL. PERFORMED AMM 36-23-01 NO FAULTS NOTED.

Part: BLOWER — FAILED (UNKNOWN) · airframe 108,755 hrs · 18,418 cycles

STATUS PAGE, CARGO DETECTION AIR INTERMITTENT IN FLIGHT. STAYED ON WHEN ON THE GROUND. REMOVED AND REPLACED CARGO SMOKE DETECTOR BLOWERS ONE AND TWO, IAW AMM 26-16-00, OPS CHECK GOOD. NO TIME INFO IN TRAX.

Part: NONE — NONE · airframe 108,627 hrs · 18,389 cycles

FUEL FLOW INDICATION ON LH ENGINE WAS ERRATIC AND UNSTABLE DURING THE FIRST 10 MINS OF FLIGHT. ALL OTHER INDICATIONS NORMAL. CLEANED D11000 CONNECTOR ON LH ENGINE FUEL FLOW TXMITTER PER SWPM 20-60-06, PERFORMED LH ENG IDLE RUN PER AMM 71-00-00, OPS CHECK GOOD.

Part: NONE — NONE · airframe 108,627 hrs · 18,389 cycles

RH ENGINE UPPER AND LOWER IGNITORS WORN. REMOVED AND REPLACED RH LOWER AND UPPER IGNITORS REF AMM 74-21-00, OPS CHECK GOOD.

Part: NONE — NONE · airframe 108,535 hrs · 18,369 cycles

RIGHT ENGINE FUEL FILTER STATUS MESSAGE. PERFORM RH FUEL FILETER REMOVE AND REPLACE PER AMM 73-11-02. PERFORMED LEAK CHECK GOOD.

Part: NONE — NONE · airframe 108,489 hrs · 18,358 cycles

FLIGHT DECK TEMP EICAS MSG APPEARED DURING DESCENT. FLIGHT DECK TEMP EICAS MSG DEFERRED PER MEL 21-61-02-03, CAT C. CLEARED MEL 21-61-02-03 REMOVED AND REPLACED FLIGHT DECK TRIM AIR VALVE. PN# INFORMATION PENDING LOGPAGE.

Part: UNKNOWN — UNKNOWN · airframe 108,470 hrs · 18,354 cycles

FLIGHT DECK TEMP EICAS MESSAGE APPEARED IN FLIGHT. PERFORMED CABIN ZONE TEMP CONTROLLER BITE TEST, NO FAULT PRESENT IAW FIM 21-61 FAULT TREE 803

Part: SWITCH — FAILED (APU) · airframe 9,999 hrs · 9,999 cycles

APU WOULD NOT START. REMOVED AND REPLACED APU INTAKE DOOR OPEN SWITCH PER AMM 49-15-02 OPS CHECKS APU GOOD.

Part: BLEED VALVE — FAULTED (LT ENGINE) · airframe 9,999 hrs · 9,999 cycles

L ENG BLEED OFF. PERFORMED AIR SUPPLY BITE PER AMM 36-23-00 FOUND LEFT PRSOV FAULTS REF LP B073510, REMOVED AND REPLACED LH PRSOV PER AMM 36-11-09 OPS CHECK GOOD.

Part: CONTROLLER — FAILED · airframe 108,207 hrs · 18,299 cycles

AFTER ENGINE START LEFT PACK WAS STILL OFF, NEED TO ADVANCE THRUST TO 40% N1 TO GET ON. REMOVED AND REPLACED LH HIGH PRESSURE CONTROLLER PER AMM 36-11-08. BITE CHECK OK AND PERFORMED LH ENGINE IDLE RUN AND IDLE CHECKS OK.

Part: SENSOR — FAULT MESSAGE · airframe 108,207 hrs · 18,199 cycles

LEFT PACK TEMP EICAS MESSAGE ON CLIMBOUT. FOLLOWED QRH, MESSAGE CLEARED. PERFORMED LEFT PACK TEMP CONTROLLER BITE PER AMM 21-51-14 FOUND MIX MAINT SENSOR FAULTS. REMOVED ADN REPLACED LH MIX MAINT SENSOR PER AMM 21-61-02 OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (CABIN TEMP) · airframe 108,186 hrs · 18,295 cycles

AFT CABIN TEMP. DEFERRED PER MEL 21-61-01-02 CAT C 1/5/2023 @ 0100Z

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 108,175 hrs · 18,293 cycles

CABIN TEMP INOP CAME ON MIDWAY THROUGH FLIGHT. COMPLY WITH QRH, TEMP REMAINED STABLE IN AFT CABIN. PERFORMED ZONE TEMPERATURE CONTROLLER BITE TEST, PASSED VERIFIED NO FAULT PER FIM 21-61 FT 803. OPS CHECK NORMAL, OK FOR SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 108,121 hrs · 18,280 cycles

APU FAULT WITH APU DOOR STATUS MESSAGE. BITE TESTED APU NO FAULTS FOUND OPS CHECK GOOD IAW FIM 49-11-00, APU STARTS NORMAL.

Part: FUEL FEED — ERRATIC (LEFT ENGINE) · airframe 108,032 hrs · 18,262 cycles

LH ENGINE FUEL FLOW ERRATIC WHEN ENG ANTI-ICE TURNED ON. CLEANED AND RESECURED CONNECTORS D17066, D4210 AND D4212 PER WDM 73-31-11. ENG GROUND TEST AND OPS TEST OK AND OBSERVED ON FLIGHTS, FF LH ENG SYS OK NO ISSUES.

Part: INDICATOR — ERRATIC · airframe 107,960 hrs · 18,246 cycles

LEFT ENGINE FUEL FLOW ERRATIC ON CLIMBOUT WITH ANTI-ICE ON. NORMAL WITH ANTI-ICE OFF. DEFERRED PER MEL 73-31-0102 CAT C.

Part: COUPLER — FAILED · airframe 107,953 hrs · 18,244 cycles

LEFT HF INOP. REMOVED AND REPLACED LH HF COUPLER PER AMM 23-11-01 OPS CHECK GOOD. RH COUPLER REPLACED FOR PRECAUTIONARY REASONS.

Part: TRANSCEIVER — FAILED · airframe 107,945 hrs · 18,242 cycles

HF #1 WILL NOT TRANSMIT. DEFERRED PER MEL 23-11-01-02A. REMOVED AND REPLACED HF#1 TRANSCEIVER.

Part: INDICATOR — ERRATIC (LT FUEL FLOW) · airframe 107,887 hrs · 18,229 cycles

L ENGINE FUEL FLOW INDICATION ERRATIC WHEN ENGINE ANTI-ICE IN USE. 4.5-6.5 FF. DEFERRED [PER MEL 73-31-01-02 CAT C @ 0600Z 12/2/22

Part: RELAY — TRIPPED (BOOST PUMP) · airframe 107,895 hrs · 18,231 cycles

RIGHT AFT FUEL PUMP EICAS MSG. PERFORMED FIM 28-22 FAULT TREE 831. RE-CYCLED RH AFT FUEL BOOST PUMP RESET RELAY AND CHECK OK.

Part: FUEL SYS — ERRATIC (LT ENG FUEL FLOW) · airframe 107,819 hrs · 18,214 cycles

L ENGINE FUEL FLOW ERRATIC ON CLIMB OUT WITH ENGINE ANTI-ICE SELECTED ON. FLOW FROM A STABLE 13.0 DROPS TO 6.5 AND IN-BETWEEN. CLEANED CANNON PLUG ON LH FUEL FLOW TRANSMITTER PER BOEING SWPM 20-60-01 OPS CHECK GOOD PER AMM 71-00-00 TEST 3.

Part: TERMINAL — DAMAGED (SHUTOFF VALVE) · airframe 107,576 hrs · 13,158 cycles

R HPSOV DEFERRED ON LOGPAGE B063815 ITEM P1 AS REFERENCE MEL 36-11-02-02 CAT C. REPAIRED TERMINAL CONNECTION ON RIGHT ENGINE HPSOV PER WFM36-11-62 AND OPS CHECK GOOD PER AMM 36-11-00

Part: NONE — NONE · airframe 107,017 hrs · 18,045 cycles

LEFT ENGINE #2 IGNITOR INOP. DEFERRED PER MEL 74-00-01A. REMOVED AND REPLACED #2 IGNITION LEAD ON LEFT ENGINE PER AMM 74-21-01. PERFORMED AUDIBLE TEST PASSED PER AMM 74-00-00

Part: EXCITER — FAILED · airframe 106,995 hrs · 18,035 cycles

HUNG START ON #1 ENGINE. FOUND NO IGNITION ON LH ENGINE FROM SOURCE 2. REPLACED LH ENGINE EXCITER 2 IAW AMM 74-11-01. REPLACED IGNITOR PLUG FOR PRECAUTIONARY MAINTENANCE. NO TIME INFO AVAILABLE ON TRAX.

Part: NONE — NONE · airframe 106,995 hrs · 18,035 cycles

SUPPLEMENTAL INFORMATION: FOUND IGNITER PLUG CERAMIC PLUG CRACKED, REMOVED AND REPLACED IGNITER PER AMM 74-21-02 OPS CHECK NORMAL AC REMAINS ETOPS 180 @ 2200Z 08/20

Part: BLOWER — FAILED · airframe 106,964 hrs · 18,029 cycles

FWD DET FAN EICAS MSG DISPLAYED. PERFORMED FWD DET FAN FAULT TREE FIM 26-16 813, REPLACED #1 BLOWER AND OPS CHECK GOOD PER AMM 26-16-02

Part: EICAS — FAULT MESSAGE · airframe 106,699 hrs · 17,973 cycles

R ENGINE HPSOV EICAS MESSAGE ON DESCENT. DEFERRED RIGHT ENGINE HPSOV PER MEL 36-11-02-02 CAT C @ 0730Z 8 JUL 22 MX PROCEDURES COMPLIED WITH

Part: NONE — UNKNOWN · airframe 106,684 hrs · 17,970 cycles

RIGHT ENGINE HPSOV MESSAGE. DEFERRED RIGHT ENG HPSOV PER MEL 36-11-02-02 CAT C @ 0049 7/7/22. REMOVED AND REPLACED RH BLEED AIR CIRCUIT ASSY PER AMM 36-11-12/401. OPS CHECK NORMAL NO FAULT NOTED AT THIS TIME. NO TIME INFO AVAILABLE IN TRAX.

Part: EICAS — FAULT MESSAGE · airframe 106,668 hrs · 17,967 cycles

RIGHT ENGINE HPSOV EICAS MESSAGE ON DESCENT, ALSO ON STATUS PAGE. DEFERRED RIGHT ENGINE HPSOV REF MEL 36-11-02-02 CAT C, RH HPSOV SECURED TO CLOSED POSITION AT 0730Z ON 7/4/2022, INSTALLED PLACARD. ACCOMPLISHED BITE CHECK PER AMM 36-11-07, NO FAULT NOTED AT THIS TIME, AC REMAINS ETOPS 180.

Part: NONE — NONE · airframe 106,663 hrs · 17,966 cycles

R ENGINE HPSOV STATUS MESSAGE IN FLIGHT. COMPLETED BITE CHECK IAW AMM 36-23-00, NO FAULT FOUND AIRCRAFT REMAINS ETOPS 180

Part: NONE — NONE · airframe 106,637 hrs · 17,961 cycles

R ENGINE HPSOV EICAS MSG BRIEFLY DISPLAYED AT TOP OF DESCENT. MSG DISAPPEARED AFTER 2 MINUTES. ACCOMPLISHED BITE CHECK PER AMM 36-11-7, NO FAULT FOUND. AIRCRAFT REMAINS ETOPS 180.

Part: NONE — NONE · airframe 106,602 hrs · 17,954 cycles

FOUND RH ENGINE PRV FORWARD CLAMPS HAVE PNEUMATIC LEAK. RH ENG PRV E-SEALS REMOVED AND REPLACED IAW AMM 36-11-18, LEAK CHECK GOOD.

Part: NONE — NONE · airframe 106,597 hrs · 17,953 cycles

CABIN ALT AUTO 1 STATUS MESSAGE ILLUMINATED. DEFERRED CABIN ALT AUTO 1 AS PER MEL 21-31-01A CAT C AT 2045Z ON 6/18/22

Part: NONE — NONE · airframe 106,585 hrs · 17,950 cycles

RIGHT ENGINE HPSOV AMBER EICAS ON DESCENT. DEFERRED AS PER MEL 36-11-02-02 CAT C RH HPSOV SECURED TO CLOSED POS AT 2041Z ON 6/17/22

Part: NONE — NONE · airframe 107,028 hrs · 19,099 cycles

DC FUEL PUMP ON EICAS MESSAGE ON MAINTENANCE PAGE. DEFERRED DC FUEL PUMP AS PER MEL 28-25-01 CAT C. PUMP DEACTIVATED PER MX PROCEDURES, PLACARD INSTALLED.

Part: NONE — NONE · airframe 106,461 hrs · 17,911 cycles

RIGHT AUX PITOT EICAS MESSAGE. REMOVED AND REPLACED RIGHT AUX PITOT STATIC PROBE PER B767 AMM 34-11-01. PITOT STATIC PROBE OPS AND LEAD CHECKS GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH.

Part: NONE — NONE · airframe 106,459 hrs · 17,910 cycles

MAIN DECK B4 SMOKE DETECTOR FAILED. DEFERRED PER MEL 26-16-02-02 CAT C AT 0720Z ON 6-3-22. MAINTENANCE PROCEDURES COMPLIED WITH.

Part: NONE — NONE · airframe 106,456 hrs · 17,908 cycles

LEFT FORWARD FUEL PUMP LOW PRESSURE LIGHT ON WITH SWITCH ON @KMIA ON 6/3/22 0107Z. RESET LEFT FORWARD FUEL BOOST PUMP CB PER 3767 WDM 28-22-11. LEFT FWD FUEL BOOST PUMP OPS CHECK GOOD, ETOPS GROUND VERIFICATION COMPLETE.

Part: NONE — NONE · airframe 106,277 hrs · 17,835 cycles

MECHANICAL INTERRUPTION (SIC) FLUID LEAK ON #1 ENGINE DURING STARTUP @ 1417Z IN KMIA. ACCOMPLISHED LEFT ENGINE DRY MOTORING AND WET MOTORING IAW AMM 71-00-00, NO LEAKS NOTED AT THIS TIME. AFTER ENGINE RUN AT IDLE POWER TO REMOVE REMAINING FUEL ALL NORMAL.

Part: SWITCH — UNKNOWN · airframe 106,277 hrs · 17,835 cycles

L ENG FUEL FILTER. REMOVED AND REPLACED THE LEFT ENGINE FUEL FILTER IAW B767 AMM 73-11-02 OPS CHECKS NORMAL, NO LEAKS NOTED. REMOVED AND REPLACED THE LEFT ENGINE FUEL PRESSURE SWITCH IAW B 767 AMM 73-34-01 OPS CHECK NORMAL, NO LEAKS NOTED.

Part: NONE — NONE · airframe 106,087 hrs · 17,770 cycles

APU STARTER WORN TO LIMITS. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01 OPS CHECK GOOD. PAPERWORK PENDING FOR PART REMOVAL.

Part: NONE — NONE · airframe 106,288 hrs · 17,841 cycles

APU STARTER POWER TERMINALS DAMAGED (TRANSFERRED FROM NR-000011 WO 119761). DEFERRED APU IAW MEL 49-11-01A CAT C @0010 Z 5-10-22, PLACARD TURNED MAINTENANCE PROCEDURES C/W. REPLACED APU STARTER WIRES IAW WDM 49-41-11 OPS CHECK OK ECU BITE OK. AIRCRAFT RELEASED NO ETOPS PENDING APU COLD SOAK (ACCOMPLISHED, GOOD).

Part: NONE — NONE · airframe 106,178 hrs · 17,795 cycles

LEFT ENGINE #2 IGNITION IS INTERMITTENT. DEFERRED LEFT ENGINE #1 IGNITION IAW MEL 74-00-01A CAT A 042922 0849Z. REMOVED AND REPLACED LEFT ENGINE #2 IGNITOR IAW B767 AMM 74-21-02. AUDIBLE TEST GOOD PER TASK 74-00-00-705-025-H00

Part: CONTROLLER — FAILED · airframe 106,130 hrs · 17,779 cycles

AT CRUISE LEFT ENGINE HPSOV EICAS ILLUMINATED, PERFORMED QRH. PER FIM 36-10 FAULT TREE 853 WAS REPLACED LEFT ENGINE HPC IAW AMM 36-11-08/401, INSTALLATION TEST NORMAL. NO TRAX INFO FOR UNIT.

Part: NONE — NONE · airframe 106,077 hrs · 17,768 cycles

APU OIL COOLING FLEXIBLE DUCTS WORN/TORN, FORWARD AND AFT. REPLACED BOTH FWD AND AFT FLEXIBLE DUCTS PER AMM 49-51-01

Part: NONE — NONE · airframe 106,045 hrs · 17,761 cycles

L HF RADIO INOP. PLACED ON MEL IAW MEL 23-11-01-02A CAT D 16 APR 1538Z, AIRCRAFT IS NOT ETOPS 180, PLACARD TURNED TO NON-ETOPS 180. REMOVED AND REPLACE L HF COMM IAW AMM 23-11-01-12, OPS CHECK GOOD NO DEFECTS NOTED. NO TIMES AVAILABLE IN TRAX.

Part: NONE — NONE · airframe 105,952 hrs · 17,740 cycles

LEFT ENGINE PRV STATUS ILLUMINATED. PERFORMED FIM 36-10 FAULT TREE 847. FOUND ONE OF PRV TERMINAL LUG NUT LOOSE. RE-TIGHTENED PRV TERMINAL NUT PER AMM 36-11-18. PERFORMED IDLE RUN ON LEFT ENGINE PER AMM 71-00-00. OPS CHECK GOOD. NO MESSAGES ETOPS VERIFICATION COMPLIED WITH AC REMAINS ETOPS 180

Part: VALVE — FAILED · airframe 105,872 hrs · 17,722 cycles

AT FL 340 L ENG HPSOV EICAS MESSAGE ILLUMINATED. RAN QRH 2.22. REPLACED #1 ENG HPSOV PER AMM 36-11-07, BOTH OPS AND LEAK CHECKS OK. AC REMAINS ETOPS 180, ETOPS GROUND VERIFICATION COMPLETED. NO TIME INFO IN TRAX FOR UNIT.

Part: TRANSCEIVER — UNKNOWN · airframe 105,797 hrs · 17,708 cycles

LH HF NOT TRANSMITTING. REMOVED AND REPLACED LH HF TRANSCEIVER IAW AMM 23-11-03/401 CHECK OK

Part: SELECTOR PANEL — FAILED · airframe 105,746 hrs · 17,698 cycles

UNABLE TO TRANSMIT ON HF FROM LH SIDE COMM PANEL. REPLACED LEFT AUDIO SELECT PANEL PER B767-AMM 23-51-01, OPS CHECK OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 105,638 hrs · 17,675 cycles

APU WON'T START. PERFORMED FIM TASK FIG 107/49-11-00 990-964-003. FOUND BAD IGNITOR PLUGS AND LEADS. RNR APU IGNITORS AND LEADS IAW AMM 49-41-02

Part: NOT REPORTED — NOT REPORTED · airframe 105,607 hrs · 17,668 cycles

APU FAULT WOULD NOT START. PERFORMED FIM 911 FT 958 AND FIM 49-11 FT 993 NO DEFECTS NOTED AT THIS TIME. AC GROUND VERIFICATION OK. AC REMAINS ETOPS 180

Part: NOT REPORTED — NOT REPORTED · airframe 105,591 hrs · 17,665 cycles

HF 1 &2 INOP, ONLY RECEIVING. INSPECTED CANNON PLUG IN HF RADIO, NO DEFECTS FOUND. IN EE BAY FOUND HF BOX NOT PROPERLY INSTALLED. RERACKED BOX AND OPS CHECKED GOOD WITH PILOT PRESENT. OPS CHECKED GOOD PER AMM 23-11-00 ETOPS GROUND VERIFICATION GOOD.

Part: COUPLER — INOPERATIVE · airframe 105,565 hrs · 17,660 cycles

RH HF RADIO WILL NOT TUNE OR TRANSMIT. DEFERRED PER MEL 23-11-01-02B. CAT C 2/7/2022 @0800Z RIGHT HF INOP. REPLACED RH HF COUPLER IAW AMM 23-11-01 OPS CHECK OK. NO UNIT TIME INFO, DTO POOL PART.

Part: COUPLER — UNKNOWN · airframe 105,532 hrs · 17,653 cycles

LEFT HF RADIO WILL NOT TRANSMIT OR TUNE. REF MEL 23-11-01-02B REPLACED LEFT HF COUPLER PER AMM 23-11-01 OPS CHECK OK. DTO PART POOL UNIT, NO TIME INFO.

Part: NOT REPORTED — NOT REPORTED · airframe 105,617 hrs · 17,670 cycles

APU FAULT X 2 ON THE GROUND. PERFORMED APU BITE FIM 49-11 FAULT TREE 987. LAST 3 STARTS NO LIGHT OFF. PERFORMED FIM 49-11 FAULT TREE 993, APU STARTUP SATISFACTORY.

Part: NOT REPORTED — NOT REPORTED · airframe 105,512 hrs · 17,649 cycles

APU WOULD NOT START AFTER LANDING - APU FAULT EICAS MESSAGE. PERFORMED FIM 49-11 FT 993. NO FAULTS NOTED, GROUND RUNUP VERIFICATION CHECK OK.

Part: START VALVE — UNKNOWN · airframe 105,502 hrs · 17,647 cycles

RH ENGINE EICAS MESSAGE ON START. DEFERRED #2 ENGINE START VALVE PER MEL 80-00-02-01 CAT C 2/1/2022 @ 0300Z. CLEARED MEL 80-00-02-01 #2 ENGINE START VALVE INOP. REPLACED #2 ENGINE START VALVE PER AMM 80-11-02 GROUND VERIFICATION CHECK OK.

Part: TRANSCEIVER — FAILED · airframe 105,438 hrs · 17,632 cycles

LEFT HF INOP, WON'T TURN OFF. REPLACED HF TRANSCEIVER IAW AMM 23-11-03 OPS CHECK NORMAL. GROUND VERIFICATION COMPLETED. NO TIME/CYCLES FOR TX AVAILABLE.

Part: NOT REPORTED — NOT REPORTED · airframe 105,443 hrs · 17,633 cycles

L HF RADIO, CANNOT TX, BOTH PILOT AND COPILOT PTT DO NOT ACTIVATE KEY ON TRANSMITTER. DEFERRED LH HF PER MEL 23-11-01-02B CAT C APPROVED BY TERRY SHUNK

Part: NOT REPORTED — NOT REPORTED · airframe 105,428 hrs · 17,630 cycles

LEFT HF RECEIVING NOT TRANSMITTING. OPS CHECKED OK PER AMM 23-11-00, NO DEFECTS NOTED.

Part: START VALVE — FAILED · airframe 105,423 hrs · 17,629 cycles

ABORTED LEFT ENGINE START FOR ENGINE VALVE DISCRETE LIGHT. MANUALLY STARTED ENGINE PER AMM 80-00-00, MEL 80-00-02-01 CAT C @ 01/24/2022 0527Z. REPLACED LEFT ENGINE START VALVE ASSY PER AMM 80-11-02-01-3G-3H. START VALVE TEST REQUIRED. ENGINE IDLE TEST PASSED OPS CHECKED GOOD.

Part: NOT REPORTED — NOT REPORTED · airframe 105,314 hrs · 17,605 cycles

LH PACK DUCT FOUND LEAKING. FOUND FAN AIR PLENUM CRACKED. REPLACED LH PACK AIR FAN PLENUM IAW AMM 21-51-02, LEAK CHECK NORMAL.

Part: NOT REPORTED — NOT REPORTED · airframe 105,306 hrs · 17,603 cycles

APU FAULT ON START X2. PLACED APU ON MEL 49-11-01A CAT C. CLEARED MEL 49-11-01A BITE TEST AND RERACK APU BOX IAW FIM 49-11-00-201, OPS CHECK GOOD NO DEFECTS NOTED. ETOPS PLACARD ROTATED 180 DEGREES

Part: CONTROL UNIT — UNKNOWN · airframe 105,269 hrs · 17,594 cycles

REPLACE WINDOW HEAT CONTROL UNIT RH SIDE. REMOVED AND REPLACED RH M-192 WINDOW HEAT CONTROL UNIT OPS CHECK GOOD. REF B767 AMM 30-4101. PART IS DTO POOL AND HAS BEEN EXCHANGED OUT, NO HOUR INFO AVAILABLE.

Part: VALVE — UNKNOWN · airframe 83,038 hrs · 13,876 cycles

LEFT ENG TAI VALVE (SIC). REPLACED LEFT ENGINE TAI VALVE PER AMM 30-21-03, BOTH OPS AND LEAK CHECKS OK. AC REMAINS ETOPS 180. DTO POOL PART EXCHANGED OUT, NO HOURS INFORMATION IN SYSTEM.

Part: NONE — NONE · airframe 105,114 hrs · 17,561 cycles

LEFT ENGINE PRV EICAS STATUS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED EICAS MSG ERASE PROCEDURE PER AMM 31-41-00. L ENG PRV STATUS MESSAGE CLEARED. PERFORMED AIR SUPPLY STATUS BITE PER AMM 36-23-00, FOUND L PRV WIRE FAULT. REPLACED K/46 AIR/GROUND RELAY. AIR BITE TEST PASSED. AC REMAINS ETOPS 180.

Part: NONE — NONE · airframe 104,640 hrs · 17,452 cycles

DISCREPANCY: BOTH BLEED DUCT PRESSURES ERRATIC ON TAKEOFF THROUGH 8000 FT. LEFT PRESSURE FLUCTUATED OVER 30 PSI ACCOMPANIED BY LOUD WHOOSHING SOUND. PERFORMED FIM TASK 36-10-00 AND BITE CHECKED THE ASCTV NO FAULTS FOUND. SYSTEM OPERATES NORMALLY OK TO CONTINUE

Part: NONE — NONE · airframe 104,483 hrs · 17,415 cycles

DISCREPANCY: STATUS SCREEN LH PRV DISPLAYED. CORRECTIVE ACTION: ERASED STATUS MSG L PRV PER AMM 31-44-00. MSG CLEARED AND BITE AIR SUPPLY MODULE 36-23-00, NO FAULT FOUND

Part: NONE — NONE · airframe 104,483 hrs · 17,415 cycles

DISCREPANCY: STATUS SCREEN LH PRV DISPLAYED. CORRECTIVE ACTION: ERASED STATS L ENG PRV PER AMM 31-44-00. MSG CLEARED AND BITE AIR SUPPLY MODULE 36-23-00, NO FAULT FOUND.

Part: NONE — NONE · airframe 104,408 hrs · 17,399 cycles

DISCREPANCY: PRIOR TO PUSHBACK FOR RIGHT ENGINE RUNUP, NOTICED THAT THE LEFT HAND ENGINE FUEL SPAR CIRCUIT BREAKER HAD TRIPPED. CONTACTED MAINTENANCE CONTROL AS TO THE SAME. CORRECTIVE ACTION: REPLACED LEFT ENGINE SPAR FUEL SHUTOFF VALVE PER AMM 28-22-11. OPS CHECK OK

Part: ENGINE — VIBRATION (RIGHT) · airframe 104,408 hrs · 17,399 cycles

DISCREPANCY: RIGHT ENGINE VIBRATION HIGH AT CLIMB PWR FL350. FAN VIBE 5.0 UNTIL THRUST REDUCED. NO SECONDARY ABNORMAL ENGINE INDICATION. CORRECTIVE ACTION PENDING.

Part: ENGINE — FAILED (#2) · airframe 104,408 hrs · 17,399 cycles

DISCREPANCY: RIGHT ENGINE VIBRATION HIGH AT CLIMB POWER FL350. FAN VIBE 5.0 WITH THRUST REDUCED. NO SECONDARY ABNORMAL ENGINE INDICATION SEEN. CORRECTIVE ACTION: REPLACED #2 ENGINE PER AMM 71-00-02 REF PROJECT WORKSHEET ITEM P1. GROUND IDLE LEAK CHECK GOOD. AIRCRAFT RELEASED TO NO ETOPS, PENDING INFLIGHT VERIFICATION

Part: BLADE — DAMAGED (NR 2 ENG FAN) · airframe 104,296 hrs · 17,372 cycles

#2 ENGINE FAN BLADE 9 HAS LEADING NICK 13" FROM TIP. CORRECTIVE ACTION: BLENDED BLADE PER AMM 72-31-02

Part: BLADE — DAMAGED (NR 2 ENG) · airframe 104,296 hrs · 17,372 cycles

ENGINE #2 BLADE #34 LEADING EDGE NICK, 7" FROM TIP. BLENDED BLADE PER AMM 72-31-02

Part: OVERHEAT LOOP — WARNING MESSAGE (RT ENGINE) · airframe 104,291 hrs · 17,371 cycles

DISCREPANCY: RH ENGINE OVERHEAT LOOP 2 EICAS MESSAGE. CORRECTIVE ACTION: REPLACED M690 CARD OPS CHECK PER AMM 26-11-00. GROUND VERIFICATION COMPLIED WITH, AC REMAINS ETOPS 180

Part: CONNECTOR — UNSECURE (FIRE LOOP) · airframe 104,292 hrs · 17,371 cycles

DISCREPANCY: STATUS MSG R ENG FIRE LOOP 1. CORRECTIVE ACTION: CLEANED AND RESECURED CONNECTOR D4230P, OPS CHECK GOOD PER AMM 26-11-00

Part: DUCT — DAMAGED (APU) · airframe 104,237 hrs · 17,358 cycles

DISCREPANCY: DURING SERVICE CHECKS, FOUND APU SURGE DUCT HAS A HOLE. CORRECTIVE ACTION: REPLACED APU SURGE DUCT IAW AMM 49-53-01 LEAK CHECK AND OPS CHECK GOOD.

Part: CONTROL CARD — FLUCTUATES (DUCT PRESSURE) · airframe 104,017 hrs · 17,309 cycles

DISCREPANCY: LEFT DUCT PRESSURE FLUCTUATES MORE THAN 20 PSI, NORMAL TO LOW RANGE AT TAKEOFF THRUST. STABLE AT CLIMB THRUST, FRM 36-10-01-01. CORRECTIVE ACTION: PERFORMED AIR SUPPLY BITE TEST PER AMM 36-23-00, FOUND L PRC WIRE FAULTS, REMOVED AND REPLACED LEFT ENGINE BLEED AIR CARD PER AMM 36-11-12, BITE CHECK OK. AC REMAINS ETOPS 180

Part: LINE — LOOSE (LT GENERATOR OIL) · airframe 103,819 hrs · 17,262 cycles

LEFT GEN DRIVE AND LEFT GEN OFF LIGHTS DURING TAXI. MI 1730Z. RETORQUED LOOSE LINE AT IDG FILTER HOUSING, POPOUT INDICATOR NOT POPPED. SERVICED IDG AND RAN ENGINE WITH OPS AND LEAK CHECK GOOD

Part: IDG — FAULTED (NR 1 GENERATOR) · airframe 103,804 hrs · 17,259 cycles

LEFT GENERATOR EICAS MESSAGE ON CLIMBOUT. REMOVED AND REPLACED #1 ENGINE IDG IAW AMM 24-11-01. OPS CHECK NORMAL, LEAK CHECK GOOD. ETOPS GROUND VERIFICATION GOOD. NOTE: REMOVED UNIT TIMES BELOW ARE FOR NAC ONLY, PREVIOUS TIME ON WING UNKNOWN.

Part: O-RING — LEAKING (SENSE LINE) · airframe 103,791 hrs · 17,255 cycles

DISCREPANCY: LEFT DUCT PRESSURE INDICATOR FLUCTUATES BETWEEN 15 AND 55 PSI AT TAKEOFF THRUST FROM TAKEOFF AND CLIMB UNTIL ABOUT 8000 FEET THEN BEGINS TO NORMALIZE. FOUND PRV SENSE LINE (SIC), REPLACED O-RING IAW AMM 36-11-18, OPS CHECK AND LEAK CHECK GOOD. AC REMAINS ETOPS 180.

Part: SENSOR — FLUCTUATES (DUCT PRESSURE) · airframe 103,600 hrs · 17,213 cycles

DISCREPANCY: LEFT DUCT PRESSURE FLUCTUATES ON CLIMB OUT. CORRECTIVE ACTION: PERFORMED FIM 36-20 FT 803, SYSTEM CHECK OK. PERFORMED AMM 36-10 FT 831, REPLACED FAN AIR TEMP SENSOR PER AMM 36-16-17, BOTH LEAK CHECK AND BITE TEST OK. GROUND VERIFICATION CHECK OK.

Part: TERMINAL — LOOSE (FIRE LOOP) · airframe 103,590 hrs · 17,211 cycles

DISCREPANCY: FOUND EICAS STATUS MESSAGE RIGHT ENGINE FIRE LOOP 1. CORRECTIVE ACTION: WHILE TROUBLESHOOTING PER FIM 26-11 FAULT TREE 804 FOUND LOOSE TERMINAL ON FIRE LOOP. CLEANED AND RESECURED PER AMM 26-11-02, OPS CHECK GOOD. GROUND VERIFICATION COMPLETE, AIRCRAFT REMAINS ETOPS 180

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 103,580 hrs · 17,209 cycles

DISCREPANCY: ON TAKEOFF AND CLIMB, THRU 2000 FT LEFT DUCT PRESSURE CYCLES RAPIDLY FROM 10-80 PSI. RIGHT DUCT PRESSURE CYCLES 85-45 PSI, BOTH STOP CYCLING BETWEEN 6-8K FEET. CORRECTIVE ACTION: PERFORMED FIM TASK 36-20 FAULT TREE 803 ENGINE RUN AND TAXI VERIFICATION COMPLETE. GROUND VERIFICATION COMPLETE, OPS CHECK GOOD. AIRCRAFT REMAINS ETOPS 180

Part: FIRE LOOP — WARNING MESSAGE (NR 1) · airframe 103,547 hrs · 17,202 cycles

STATUS MESSAGE RIGHT ENG FIRE LOOP ONE ILLUMINATED. INSTALLED UPPER AFT FIRE LOOP ASSY IAW AMM 26-11-02 OPS CHECK GOOD. GROUND VERIFICATION COMPLETED, AIRCRAFT REMAINS ETOPS 180.

Part: TERMINAL BLOCK — DAMAGED (FIRE DETECTION) · airframe 103,521 hrs · 17,196 cycles

EICAS STATUS MESSAGE FIRE LOOP 1. FOUND #2 ENG TS681 FIREWALL FIRE DETECTOR ONE OF TERMINAL LUGS DAMAGED. REPAIRED TERMINAL LUG PER SWPM 20-30-00, OPS CHECK GOOD. AC REMAINS ETOPS 180, GROUND VERIFICATION COMPLETE.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 103,508 hrs · 17,193 cycles

DISCREPANCY: CABIN ALT AUTO STATUS MSG. CORRECTIVE ACTION: PERFORMED FIM 21-31 TASK 809 AND 21-31 TASK 803. NO FAULTS NOTED, MSG ERASED.

Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 99,317 hrs · 16,368 cycles

IN THE COURSE OF SCHEDULED MAINTENANCE IT WAS NOTED, FLIGHT DECK ENTRY EMERGENCY FLASHLIGHT BATTERY DEAD. INITIATED DEFERRAL MAINTENANCE ITEM 19871. REMOVED AND REPLACED FLIGHT DECK ENTRY EMERGENCY FLASHLIGHT BATTERY, IAW B767 AMM 25-64-00 AND LOPA 767-300 DWG 25-767-01002. NO FURTHER FAULTS NOTED. THIS CLEARS DEFERRAL MAINTENANCE ITEM 19871. AIRCRAFT RELEASED TO SERVICE.