N566NC
Registered owner: NAS AIRCRAFT LEASING CO LLC, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
NUMBER 1 ENG FAN BLADE NR 37 HAS A DING APPROX. 1.75" ON L/E FROM BLADE TIP. REPAIRED DING AT NR 1 ENG, FAN BLADE NR 37 1.75" ON L/E FROM BLADE TIP IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS IAW AMM 72-31-02-206-100-N00.
NUMBER 2 ENG FAN BLADE HAS A NICK WITH A BURR ON L/E AT FAN BLADE TIP. REPAIRED NICK AT NR 2 ENG FAN BLADE ON L/E IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO CRACKS IAW AMM 72-31-02-206-100-N00. BLADE NR 23.
NUMBER 2 ENGINE FAN BLADE HAS 2 DINGS APPROX 3.5" APART FROM EACH OTHER 1ST DING APPROX 2.5" FROM FAN BLADE TIP ON L/E OF FAN BLADE. REPAIRED THE 2 DINGS AT NR 2 ENG FAN BLADE 2.5" AND 6" FROM FAN BLADE TIP IAW AMM 72-31-02-308-N00. PERFORMED HFEC, NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00. BLADE NR 31.
NUMBER 2 ENGINE FAN BLADE HAS A DING APPROX .5" ON L/E FROM FAN BLADE TIP. REPAIRED THE DING AT NR 2 ENG FAN BLADE 5" ON L/E FROM FAN BLADE TIP IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS IAW AMM 72-31-02-206-100-N00. BLADE NR 2.
NUMBER 2 ENG FAN BLADE HAS A NICK APPROX 2.5" ON L/E FROM FAN BLADE TIP. REPAIRED THE NICK AT NR 2 ENG FAN BLADE 2.5" ON L/E FROM FAN BLADE TIP IAW 72-31-02-308003-N00. PERFORMED HFEC, NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00. BLADE NR 3.
NUMBER 2 ENG FAN BLADE AT L/E TO FAN BLADE TIP HAS A NICK AND TIP IS SLIGHTLY BENT OUT. REPAIRED THE NICK AT NR 2 ENG FAN BLADE L/E CORNER IAW AMM 72-31-02-208-003-N00. PERFORMED HFEC NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00. BLADE NR 14.
NR 1 ENG. FAN CASE HAS GOUGES ON THE V-GROOVE FROM 8 O'CLOCK TO 9 O'CLOCK POSITION. REMOVED DAMAGED ON NR 1 ENG FAN CASE V-GROOVE FROM 8 O'CLOCK TO 9 O'CLOCK POSITION WAS FOUND WITHIN LIMITS IAW AMM 72-34-07, STEP 2.E, TABLE 801. REMOVED .030" DEPTH, MAXIMUM ALLOWED 0.125".
NUMBER 1 ENG. FAN CASE HAS A GOUGE ON THE V-GROOVE AT 3 O'CLOCK POSITION. REMOVED DAMAGE ON NR 1 ENG FAN CASE V-GROOVE AT 3 O'CLOCK POSITION WAS FOUND WITHIN LIMITS IAW AMM 72-34-07 STEP 2. E, TABLE 801. REMOVED 0.090 DEPTH, MAXIMUM ALLOWED 0.125".
NUMBER 1 ENG. FAN BLADE NR 12 HAS A DING APPROX. 1" ON L/E FROM BLADE TIP. THIS AREA WAS PREVIOUSLY BLENDED. REPAIRED DING AT NR 1 ENG FAN BLADE NR 12 1" ON L/E FROM BADE TIP AREA -A- IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS AT THE AREA REWORK IAW AMM 72-31-02-206-100-N00,
NUMBER 1 ENG. FAN BLADE NR 12 HAS A DING APPROX. 1" ON L/E FROM BLADE TIP. THIS AREA WAS PREVIOUSLY BLENDED. REPAIRED DING AT NR 1 ENG FAN BLADE NR 12 1" ON L/E FROM BADE TIP AREA -A- IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS AT THE AREA REWORK IAW AMM 72-31-02-206-100-N00,
NUMBER 1 ENG. FAN BLADE NR 27 HAS A DING APPROX. 1.75" ON L/E FROM BLADE TIP. EVALUATED DENT AT NR 1 ENG FAN BLADE NR 27 1.75" ON L/E FROM BLADE TIP FOUND TO BE IN LIMITS IAW AMM 72-31-02. PERFORMED HFEC, NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00.
NUMBER 2 ENGINE FUEL BY PASS VALVE LEAKING FUEL. PERFORMED LEAK CHECK OF NR 2 ENGINE FUEL BYPASS VALVE IAW AMM 71-00-00-795-003-N00. NO LEAKS NOTED, LEAK CHECKED GOOD. ENGINE IDLE AND MPA RUNS WERE PERFORMED AS PART OF LEAK CHECKED ATTACHMENT.
#1 ENG FAN BLADE # 27 HAS A DING APPROX 1.75" ON L/E FROM BLADE TIP DOT 063629 . REPAIRED DING AT #1 ENG FAN BLADE #12 1" ON L/E FROM BLADE TIP AREA A IAW B767 AMM 72-31-02-308-MOD PERFORMED HFEC NO CRACK FOUND AT THE AREA IAW AMM 72-31-02-206-100 MOD. NO ENGINE INFORMATION AVAILABLE.
21420 #1 ENG FAN BLADE # 3 HAS A DING APPROX 1.5" ON L/E FROM BLADE TIP DOT 063631. REPAIRED DING AT #1 ENG FAN BLADE #37 1.5 ON L/E FROM BLADE TIP IAW B767 AMM 72-31-02-308-003-MOD PERFORMED HFEC NO CRACK FOUND IAW AMM 72-31-02-206-100 MOD.
21421 #1 ENG FAN CASE HAS A GOUGE ON THE V-GROOVR AT 3 O'CLOCK POISTION DOT 012001. REMOVED DAMAGE ON #1 ENG FAN CASE V-GROOVE AT 3 O'CLOCK POSITION WAS FOUND WITHIN LIMITS PER B767 AMM 72-34-07 STEP 2 E TABLE 801 REMOVED 0.090 DEPTH MAX ALLOWED 0.125".
21422 #1 ENG FAN CASE HAS A GOUGE ON THE V-GROOVE AT 8 O'CLOCK TO 9 O'CLOCK POISTION DOT 012002. REMOVED DAMAGE ON #1 ENG FAN CASE V-GROOVE AT 8 O'CLOCK AND 9 O'CLOCK POSITION WAS FOUND WITHIN LIMITS PER B767 AMM 72-34-07 STEP 2 E TABLE 801 REMOVED 0.090 DEOTH MAX ALLOWED 0.125". NO ENGINE INFORMATION AVAILABLE.
#1 ENGINE FAN BLADE #37 HAS A DING APPROX 1.75" REPAIRED DING AT #1 ENG FAN BLADE #37 ON LE BLADE TIP IAW B767 AMM 72-31-308. ENGINE INFORMATION UNAVAILABLE.
21418 #1 ENG FAN BLADE # 27 HAS A DING APPROX 1.75" ON L/E FROM BLADE TIP DOT 063629. EVLAUATED DING AT #1 ENG FAN BLADE #37 1.75 ON L/E FROM BLADE TIP FOUND TO BE IN LIMITS IAW B767 AMM 72-31-02 PERFORMAED HFEC NO CRACKS FOUND IAW B767 AMM 72-31-02-206-100.
DURING WALK AROUND FOUND LH ENG HAS OIL LEAK. FOUND LT AIR/OIL HEAT EXCHANGER VALVE RETURN TUBE LEAKING OIL. TIGHTENED RETURN TUBE B-NUT PER AMM 79-21-09
DURING WALK AROUND FOUND LH ENGINE HAS OIL LEAK. FOUND LH ENG AIR/OIL HEAT EXCHANGER VALVE RETURN TUBE LEAKING OIL . TIGHTENED A/O HEAT EXCHANGER VALVE RETURN B-NUT PER AMM 79-21-09
FOUND THE LEFT ENGINE EEC C2 MAINT MESSAGE. FOUND LH ENG 21B LVDT CONNECTOR 0830OP BETWEEN P2N AND PIN 2 RESISTANCE OUT OF LIMIT REPLACED LH ENG INBD TR LOCK HYD ACTUATOR AND CARRIED OUT INSTALL TEST. ENGINE INFORMATION UNAVAILABLE.
FOUND THE LEFT ENG EEC C2 MAINT MSG. PERFORMED TIS FOUND LT ENG 21B LVDT CONNECTOR 0834OP BETWEEN P2N & PIN 2 RESISTANCE OUT OF LIMITS IAW FIM TASK 8038-71-01, TASK 848, REV 145. REMOVED AND REPLACED LT ENG INBD TR LOCK HYD ACTUATOR & CARRIED OUT INSTALL TEST
FOUND THE #2 EGT HARNESS WORN. REPLACED THE #2 EGT HARNESS FOUND SATIS PER AMM 77-21-02. ENGINE INFORMATION NOT AVAILABLE.
FOUND APU OIL QUANTITY MTR PACKING LEAK. REMOVED AND REPLACED THE APU OIL QTY TRANSMITTER PACKING AS PER B767-300 AMM 49-49-04 REV 145
FOUND APU OIL QTY TRANSMITTER PACKING LEAK. REMOVED AND REPLACED APU OIL QTY TRANSMITTER PACKING PER 767-300 AMM 49-49-04
LEFT & RIGHT HEAT EXCHANGERS INTERAL SURFACE FOAM SEALS FOUND WORN. REMOVED AND REPLACED LT & RT HEAT EXCHANGERS INTERNAL SURFACE FOAM SEALS IAW CARD 21-017-00-01
LH AIR CONDITIONING COMPARTMENT PLENUM FOUND PERFORATION. REMOVED AND REPLACED LH AIR CONDITIONING COMPARTMENT PLENUM AS PER 767-300 AMM 21-51-01
LEFT AIR CONDITIONING COMPARTMENT PLENUM FOUND PERFORATED. REMOVED AND REPLACED LT AIR CONDITIONING COMPARTMENT PLENUM IAW AMM 21-51-02, REV 145. FOUND GOOD.
FOUND RT ENGINE PRSOV HEALTH CHECK FAIL. REMOVED AND REPLACED THE NR 2 ENGINE PRSOV AND CARRIED OUT TEST IAW AMM 36-11-09 REV 145.
FOUND RH ENGINE PRSOV HEALTH CHECK FAIL. REMOVED AND REPLACED #2 ENGINE PRSOV AND CARRIED OUT TEST AS PER 767-300 AMM 36-11-09
RH HEAT EXCHANGER SLEEVE FOUND AIR LEAKAGE. REMOVED AND REPLACED RH AFT AIR CONDITIONER SURFACE BODY CROSS OVER DUCT SLEEVE SEAL AS PER AMM 36-11-00
RIGHT HEAT EXCHANGER SLEEVE FOUND AIR LEAK. REMOVED AND REPLACED RT AIR CONDITIONING AFT SURFACE BODY CROSS OVERDUCT SLEEVE SEAL IAW AMM 36-11-01 REV 145. NO LEAK.
FOUND ONE CRACK AT RT PYLON FWD UPPER SPAR WEB, HYDRAULIC HOLE AREA AT ABOUT NSTA 180. REPAIRED THE NR 2 PYLON FORWARD UPPER SPAR WEB IAW EO 767-54-0014 REV 1R AND EO 767-54-0014 REV 1R
DURING PERFORM MFEC INSPECTION OF LT SIDE NOSE WHEEL WELL BULKHEAD STIFFENER , ONE CRACK WAS FOUND AT BS 287 BETWEEN WL 159 TO WL 185 AS MARKED, IT IS ABOUT 1 INCH LONG. CARRIED OUT THE STIFFENER REPAIR AT LT SIDE NOSE WW BULKHEAD STA 287 LBL25 AS PER DRAFT EO 767-53-0018 REV 1R 107 AND PART 2 OF SB 767-53-0018 REV 1R
DURING PERFORM MFEC INSPECTION OF RH SIDE NOSE WHEEL WELL BULKHEAD STIFFENER , ONE CRACK WAS FOUND AT BS287 BETWEEN WL 159 TO WL 185 AS MARKED, IT IS ABOUT 0.8 INCH LONG. CARRIED OUT THE STIFFENER REPAIR AT LEFT SIDE NOSE WW BULKHEAD STA 287 LBL 25 AS PER DRAFT EO 767-53-0018 REV 1R07 AND PART 2 OF SB 767-53-A-0275 REV 1R
RH AIR CONDITIONING COMPARTMENT PLENUM FOUND PERFORATION. REMOVED AND REPLACED RH AIR CONDITIONING PLENUM COMPARTMENT AS PER B767-300 AMM 21-51-02 REV 145.
RIGHT AIR CONDITIONING COMPARTMENT, PLENUM FOUND PERFORATION. REMOVED AND REPLACED RT AIR CONDITIONING PLENUM COMPARTMENT IAW AMM 21-51-02, REV 145.
FOUND RT LOW LIMIT VALVE TORQUE MOTOR TEST FAILED. (CAN NOT TO MOVE TO OPEN.) REMOVED AND REPLACED RT LOW LIMIT VALVE AND CARRIED OUT LEAK TEST IAW AMM 21-51-11 REV 145, NO LEAK.
CLEANED AND SECURED ELECTRICAL CONNECTOR D4208P OPS CHECK OK WPM 36-11-62.
RH ENGINE OIL PRESS IND BLANK. CLEANED AND RESECURED ELECTRICAL CONNECTOR P4208P IAW WPM 36-11-62 OPS CHECK OK.
RH ENG LOOP 1 OVHT/FIRE STATUS MESSAGE. CLEANED AND RESECURED ELECTRICAL CONNECTOR D4230P IAW WPM 26-11-11 OPS CHECK OK.
R ENGINE VIBE METER GOES UP AND DOWN FROM 0.0 TO 1.1 PERFORMED AMM 71-00-00 R ENG VIBRATION N1 WITHIN LIMIT. PERFORMED R ENG FAN BLADE PART-SPAN SHROUD LUBE PER TASK CARD 72-433-01-02
THE OIL QTY ON THE RIGHT ENGINE WAS SHOWING AT 5 IN FLIGHT. LEFT ENGINE WAS 16. SERVICED RH ENGINE TO FULL PER AMM 12-13-01 RH ENGINE OIL CONSUMPTION WITHIN LIMITS. CLEANED RH ENGINE OIL TRANSMITTER PER SWM 20-60-01, NO LEAKS FOUND.
UNABLE TO TRANSMIT ON LEFT HF RADIO. REMOVED AND REPLACED LH HF TRANSCEIVER IAW B767 AMM 23-11-00 OPS CHECKED SATISFACTORY.
LEFT PACK DID NOT COME ON AFTER START. GOT PACK OFF EICAS, CAME ON ABOUT 2 MINUTES BY ITSELF. REMOVED LH FLOW CONTROL VALVE, INSTALLED ON RH SIDE OF AIRCRAFT. ETOPS GROUND VERIFICATION OK
HF RADIO #1 DOES NOT TX. CAN RX OK. REMOVED AND REPLACED LH HF TRANSCEIVER PER AMM 23-11-03 OPS CHECK GOOD. #1 HF TRANSMITS AND RECEIVES CLEARLY. PART IS UNKNOWN TO TRAX.
LEFT HF RADIO ON FULL VOLUME IS WEAK AND UNREADABLE. CAN HEAR THE RADIO IS WORKING BUT NOT LOUD ENOUGH TO UNDERSTAND. PERFORMED OPS CHECK ON LH HF RADIO PER AMM 23-11-00 SPEAKER AND HEADPHONE VOLUME GOOD.
APU FAILED TO START WHILE USING BATTERY AFTER REPOSITION. ADJUSTED IGV ACTUATOR BELL CRANK AND BLOCK ASSY. ALSO CONFIRMED IGV ROD DIMENSION A IN REF 767 AMM 49-52, APU OPS CHECK OK WITH BATTERY.
APU FAULT AFTER LANDING IN KMIA, APU RPM NEVER GOT HIGHER THAN 35%. ACCOMPLISHED FIM 41-11 FT 958, FOUND IGV ACTUATOR FAULT. REMOVED AND REPLACED IGV ACTUATOR PER B767 AMM 49-52-02 OPS AND LEAK CHECK GOOD.
APU WOULD NOT START ON 3 ATTEMPTS. GOES TO 30% BUT WILL NOT ADVANCE WITH APU FAULT LIGHT ILLUMINATED. DEFERRED PER MEL 49-11-01A. REMOVED AND REPLACED IGV ACTUATOR IAW 767 AMM 49-52-02 OPS AND LEAK CHECK GOOD.
LH AFT APU VIBRATION ISOLATION MOUNT WORN TO LIMITS. REMOVED AND REPLACED LH APU VIBRATION ISOLATION MOUNT IAW 767-300 AMM 49-11-01. PART UNKNOWN TO TRAX
FORWARD APU VIBRATION ISOLATION MOUNT WORN TO LIMITS. REMOVED AND REPLACED FORWARD APU VIBRATION ISOLATION MOUNT. PART UNKNOWN TO TRAX
RH AFT APU VIBRATION ISOLATION MOUNT WORN TO LIMITS. REMOVED AND REPLACED RH AFT APU VIBRATION ISOLATION MOUNT IAW 767-300 AMM 49-11-01. PART UNKNOWN TO TRAX
RIGHT ENGINE START AT THE GATE ABORTED DUE TO N2 NOT STABILIZED AT 2 MINUTES. N2 AT ABOUT 48% AT 2:25. FOUND INADEQUATE FROM GROUND AIR CART. REPLACED START CART, SECOND START WAS NORMAL IAW AMM 71-00-00
APU FAULT 2 ATTEMPTS KMIA. THIRD ATTEMPT FAILED, FOLLOWED FIM 49-11 FAULT TREE 989 REPLACED APU STARTER NO HELP. DEFERRED APU IAW MEL 49-11-01A CAT C ON 5/15/2025 @ 1850Z
EICAS MESSAGE R PACK TEMP IN CRUISE FLIGHT FROM MKIP TO KMIA. RAN THE QRH, ENDED UP TURNING THE PACK OFF. ACCOMPLISHED FIM 21-51 TASK 876-877 ISOLATION PROCEDURES. CONFIRMED R PACK INLET ACTUATOR FAULTY. REMOVED AND REPLACED RAM AIR INLET ACTUATOR IAW AMM 21-53-00. PART UNKNOWN TO TRAX.
APU DID NOT START (3 ATTEMPTS). PERFORMED APU BITE IAW FIM 49-11 FT 927 NO FAULTS NOTED.
RIGHT ENGINE VIBRATION INDICATOR INTERMITTENTLY READS BETWEEN 0.3 AND 5.0 DURING CLIMB OUT OF SPJC. REPLACED RH ACCELEROMETER IAW AMM 77-31-01
FWD EQUIP COOLING SUPPLY FAN EICAS MESSAGE IN VIEW. DEFERRED PER MEL 21-58-03-02-01 CAT C. REMOVED AND REPLACED FWD PACK SUPPLY FAN 1 IAW AMM 21-58-06.
APU FAULT 3 ATTEMPTS. DEFERRED APU PER MEL 49-11-01A CAT C. ACCOMPLISHED APU BITE PROCEDURE PER FIM 49-11-FT 987. MINIFLAG SUMMARY SHOWED NO FAULT CODES. CLEARED MEMORY AND STARTED APU, NORMAL OPERATION
OIL QUANTITY ON RIGHT SIDE DROPS DURING FLIGHT (8 QUARTS) - PERFORMED T675 TEST ON OIL QTY TRANSMITTER CHECK IAW WDM 79-31-11 NO DISCREPANCIES NOTED. SERVICED OIL TO 21 AS REQUIRED PER SERVICE CHECK TASK CARD B767-2B
RIGHT SIDE VIBRATION MONITOR OSCILLATES BETWEEN 0.5 TO 5.0 DURING CLIMB WITH NO VIBRATION FELT IN AIRCRAFT. ACCOMPLISHED WIRING CHECK FROM R ENG FAN ACCELEROMETER TO H132 D2708B NO WIRING ISSUES. ALSO APPLIED FIM 77-31 FT 807 AVM BITE/ERASE PROCEDURE. NO EICAS MESSAGE PRESENT.
ACCOMPLISHED FIM 21-51 FT 803. REMOVED AND REPLACED RH RAM AIR INLET DOOR ACTUATOR IAW 767 AMM 21-53-03 OPS CHECK GOOD.
RIGHT PACK TEMP IN CLIMB. DEFERRED PER MEL 21-51-03-01
LEFT ENGINE VIBRATIONS SEEM STUCK AT ZERO ALL CHANNELS. DEFERRED L ENG VIBRATION INOP PER MEL 77-31-01. REMOVED AND REPLACED AVM SIGNAL CONDITIONER IAW AMM 77-31-03.
R VIBE INDICATOR SHOWED OSCILLATION DURING CLIMB, 2.5 OR 4.0 THEN ZERO. ACCOMPLISHED FIM 77-31 FT 806 AND 807M NO DISCREPANCIES NOTED.
R STARTER CUTOUT EICAS MULTIPLE TIMES IN FLIGHT. REMOVED AND REPLACED RH ENGINE START VALVE IAW AMM 80-11-02
EICAS MESSAGE FWD EQUIP VAL AIR RETURN BACK. REMOVED AND REPLACED THE MANIFOLD INTERCONNECT VALVE. IAW AMM 21-58-01
FWD EQUIP VAL EICAS MESSAGE AND DISCRETE LIGHT. RETURNED TO MIA. REMOVED AND REPLACED THE MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01 OPS CHECK NORMAL.
RIGHT STARTER EICAS MESSAGE ILLUMINATED ON START. DEFERRED RH ENG START VALVES PER MEL 80-00-02-01
DURING WALK AROUND FOUND INTERMEDIATE CASE FAIRING ON #1 ENGINE 5 OCLOCK MISSING. DEFERRED PER DMI 72-34 ON 3/15/25, REPLACE THE FAIRING BEFORE 101ST HOUR OF OPERATION. INSTALLED MISSING PANEL ON #1 ENGINE IAW P&W SERVICE BULLETIN 72-778
APU PNEUMATICS INOP, 5 PSI OUTPUT. DEFERRED PER MEL 49-11-01-01
ACCOMPLISHED FIM 49-11 FT 987 BITE PROCEDURE FOUND FAULT CODE MINIFLAG 126. REMOVED AND REPLACED APU INLET GUIDE VANE ACTUATOR IAW AMM 49-59-02. TRAX PART TIME UNAVAILABLE.
APU FAULT. ATTEMPTED 3 STARTS NEVER GOT ABOVE 45%. REMOVED AND REPLACED ACTUATOR INLET GUIDE VANE OPS CK OK IAW AMM 49-51-02
LEFT RADAR FAILED. REMOVED AND REPLACED LEFT RADAR WX TRANSCEIVER IAW AMM 34-43-01 OPS CHECK GOOD.
FO WX RADAR INOP - NO DISPLAY. CAPT WX RADAR OK. PERFORMED WEATHER RADAR SYSTEMS ADJUSTMENT TEST PER AMM 344-43-00-715. TEST PASS WEATHER RADAR OPERATES NORMAL
L ENG VIBE INDICATOR SHOWS ZERO DURING ALL PHASES OF FLIGHT. PERFORMED FIM 77-31 FT 806 ALL OPERATION NORMAL. OSD: 3/3/2025
L ENG VIBE INDICATOR SHOWS ZERO DURING ALL PHASES OF FLIGHT. PERFORMED FIM 77-31 FT 806 ALL OPERATION NORMAL.
APU FAULT ON APPROACH AND ON GROUND. REMOVED AND REPLACED THE IGNITER PLUG IAW AMM 49-41-02, REMOVED AND REPLACED THE IGNITION LEAD IAW AMM 49-41-04 AND REMOVED AND REPLACED THE IGNITION UNIT IAW AMM 49-41-03.
#1 ENGINE #24 BLADE NICKED. REMOVED NICK FROM #1 ENGINE BLADE IAW AMM 72-31-02.
L ENG VIBE INDICATION SHOWS N2 0.0 IN ALL PHASES OF FLIGHT EXCEPT STARTUP. IT SHOWS FAN 0.0. PERFORMED AVM BITE HISTORY CHECK NO EICAS MESSAGES, ENGINE VIBE CHECK GOOD IAW AMM 77-31-00
FOUND REHEATER LEAKING AIR AT WELDING JOINTS. REMOVED AND REPLACED LH PACK REHEATER IAW AMM 21-51-07 LEAK AND OPS CHECK GOOD.
LEFT ENGINE VIBE SHOWS NO INDICATION. REMOVED AND REPLACED THE LEFT ENG ACCELEROMETER IAW AMM 77-31-01 OPS CHECK NORMAL.
DURING DAILY CHECK FOUND LEFT PACK INOP LIGHT ON AND L PACK TEMP EICAS MESSAGE. REMOVED AND REPLACED MIX MANIFOLD SENSOR IAW 21-61-02. PART IS UNKNOWN TO TRAX, NO HOUR INFO AVAILABLE.
RH SIDE WINDOW HEAT SYSTEM INOP, SENSOR #2 FAULT. DEFERRED RH WINDOW HEAT SYSTEM PER MEL 30-41-01-02 ON 1/16/2025@1350 CAT C
OIL TEMP RISING STEADILY TO 160 DEGREES STATUS MESSAGES R SCAV TEMP 1 R SCAV TEMP 2. REMOVED AND REPLACED RH ENGINE IAW AMM 71-00-02 OPS CHECK LEAK CHECK NORMAL
LH ENGINE BLADE #9 NICK FOUND. REMOVED NICK AT LH ENG BLADE 9 AT AREA A PER AMM 72-31-02. NDT HFEC AND FPI DEFERRED.
LH HF CONTROL HEAD 1 DIGIT INOP. REMOVED AND REPLACED LH HF CONTROL HEAD PER 767 AMM 23-11-02 OPS CHECK GOOD.
FORWARD EQUIP COOLING SUPPLY FANS 1. REMOVED AND REPLACED FORWARD RACK SUPPLY EXHAUST FAN IAW AMM 21-58-06.
LEFT PACK WILL NOT COOL ON GROUND. EXHAUST GROUND DOOR CLOSE TO GROUND. REMOVED AND REPLACED LEFT PACK EXHAUST DOOR ACTUATOR OPS CHECK OK PER 767 AMM 21-53-03. PART IS UNKNOWN TO TRAX, NO TIME INFO.
AT CRUISE FLIGHT L GEN OFF EICAS MESSAGE. PERFORMED QRH, CONTINUED TO DESTINATION. REMOVED AND REPLACED OVERFLOW DRAIN COUPLING, OPS AND LEAK CHECK OK IAW AMM 24-11-00. HOURS INFORMATION PENDING.
LEFT ENGINE #18 BLADE HAS A NICK. REPAIRED LH ENG BLADE PER AMM 72-31-02
LEFT ENGINE 2 FAILED START ATTEMPTS WITH #1 STARTER SELECTED. DEFERRED PER MEL 74-00-01B CAT C. REMOVED AND REPLACED LH ENGINE IGNITOR PLUG IAW AMM 74-21-02
STATUS MSG L ENG FIRE LOOP 2. ACCOMPLISHED FIM FT 804 TABLE B FOUND RESISTANCE 17.75L IN LIMITS REPLACED TS682 TERMINAL LUG PER SWPM 20-30-00 OPERATIONAL TEST GOOD.
APU DID NOT START (3 ATTEMPTS). TROUBLESHOT APU FOUND TRU INOP. REMOVED AND REPLACED K617 AND K 197, APU CHECKED NORMAL IAW AMM 49-11-00
APU FAULT TWICE WHILE IN KMIA. PERFORMED OPERATIONAL CHECK APU CHECK NORMAL IAW AMM 49-11-00
APU FAULT 2 ATTEMPS, SHOWS 25 OIL. PERFORMED OPS CHECK OF APU IAW AMM 49-11-00 CKECKED NORMAL
L GEN DRIVE EICAS MSG. ACCOMPLISHED FIM 24-20-FT 801 SERVICED IDG PER AMM 12-13-03. CHECKED L IDG WIRING CONNECTORS D10964 AND D10965 NO DISCREPANCIES NOTED PER FIM 24-20-001201 TASK 804. PERFORMED L IDG IDLE RUN, L IDG GENERATION NORMAL PER AMM 71-00-00.
APU FAILED TO START, 2 ATTEMPTS. PERFORMED OPERATIONAL CHECK, APU CHECKED NORMAL PER AMM 49-11-00
STATUS MESSAGE L ENGINE FIRE LOOP 2. PERFORMED OPERATIONAL CHECK OF THE LEFT ENGINE FIRE LOOP SYSTEM IAW AMM 26-11-00 OPS CHECK NORMAL.
WEATHER RADAR LEFT SIDE INTERMITTENT. RIGHT SIDE OK. CYCLED CB L WXR RADAR AND R WX RADAR TEST OK IAW AMM 34-43-01
2 FAILED APU STARTS. FOUND ECU CODES LATCHED IN MEMORY, REMOVED AND REPLACED ECU IAW AMM 49-61-05
APU FAULT. ACCOMPLISHED APU CENTRAL UNIT BITE TEST IAW AMM 49-61-05, NO FAULTS FOUND.
HIGH L ENG VIBRATION N1 5.0. ACCOMPLISHED FIM 77-31-FT 813 BLOCKS 1,2, AND 23 FOUND GROUND SHIELD TERMINAL LUG ON CONN D10994 BROKEN, REMOVED AND REPAIRED TERMINAL WIRING IAW WDM 77-31-11 AND SWPM 20-24-26.
APU FAULT - TEMP HUNG AT 783 DEGREES C BEFORE SHUTTING DOWN. ACCOMPLISHED FIM 49-11 FT 987, FOUND MINIFLAG 14 AND FAULTY LRU "PT SENSOR" MSG. DEFERRED PER MEL 49-11-01A CAT C
REMOVED AND REPLACED R FWD HEAT CONTROLLER IAW AMM 30-41-01 TEST OK. PART TIME UNAVAILABLE
PERFORM RESET OF CB AND OPS TEST OF 1R WINDOW HEAT IAW AMM 30-41-00 TEST OK.
#1 ENG SPEED CARD MESSAGE. PERFORMED L ENG SPEED CARD TEST, PER AMM 77-12-01-864 STATUS MESSAGE NOT SHOWING AT THIS TIME.
DURING APU CHECK, FOUND SURGE VALVE DUCT HOSE DAMAGED. REMOVED AND REPLACED APU SURGE VALVE DUCT HOSE IAW AMM 49-53-01
CABIN DIFF PRESSURE INDICATOR STAYED AT RED. REPLACED CABIN PRESSURE INDICATOR IAW AMM 21-33-01
REMOVED AND REPLACED RH VALVE AIR/OIL HEAT EXCHANGER ON #2 ENGINE LEAK AND OPS CHECK GOOD IAW 24-11-12 AND AMM 71-00-00. PART IS UNKNOWN TO TRAX.
L ENGINE SPEED CARD. REMOVED AND REPLACED LEFT ENGINE SPEED CARD IAW AMM 77-12-01 TEST REPORTED OK
LEFT WEATHER RADAR - NO SYSTEM DATA ON ND. REMOVED AND REPLACED WAVE GUIDE SWITCH RELAY ASSY PER AMM 34-43-04 OPS CHECK GOOD.
RIGHT IDG VALVE STATUS MESSAGE. APPLIED FIM 24-20 FAULT TREE 802 BLOCKS 1-6. REPLACED R 1DG VALVE FAILURE RELAY K1032 PER WDM 24-11-21. PERFORMED ENGINE CHECK PER B767-300 AMM 71-00-00
LEFT WEATHER RADAR INOP, SYS SHOWS WX NO DATA WHEN SELECTED. REMOVED AND REPLACED RT WX TX IAW AMM 34-43, OPS CHECK GOOD. PART UNKNOWN TO TRAX.
LEFT WEATHER RADAR INOP, SHOWS NO DATA WHEN SWITCHED TO LEFT RADAR. ACCOMPLISHED FIM 34-43 FT 805, WX RADAR BITE PROCEDURE BLOCKS 1 AND 2 TEST COMPLETED OK.
APU FAULT, APU WOULD NOT START. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. PART IS UNKNOWN TO TRAX.
STATUS MESSAGE L ENG PRV. PERFORM FIM 36-20 FT 804 FAULT CLEARED, OK FOR SERVICE.
NO BLEED AIR OUTPUT FROM RIGHT ENGINE AFTER START AT THE GAMTE. PERFORMED FIM 36-10 FT 809 REMOVED AND REPLACED RH PRSOV IAW AMM 71-00-00 OPS CHECK NORMAL. PART IS UNKNOWN TO TRAX.
AFTER LANDING, APU BLEED NOT PRODUCING AIR. DUCT PRESSURE INDICATING AT 5PSI, NO AC, PACKS INOP. REMOVED ECU, CLEANED RESEATED ECU IAW SWPM 20-61-00, OPS CHECK NORMAL.
AFTER ENGINE CHANGE, EICAS MESSAGES L ENG FIRE LOOP 1/2, L ENG OH 1/2. LEFT ENGINE HAS A KIDDE SYST INSTALLED, NEED TO INSTALL KIDDE SYST CARDS FOR FIRE AND OH PROTECTION. REMOVED AND REPLACED FIRE AND OH CARDS.
DURING ENGINE INSPECTION FOUND GOUGE ON OUTER FAN CASE AT 4 OCLOCK AND 8 OCLOCK POSITION. PERFORMED BLEND OUT IAW PW TASK 72-33-01-300-02
DURING ENGINE INSPECTION FOUND A SMALL PIECE MISSING FROM INTERMEDIATE CASE SEGMENT AT 5 OCLOCK POSITION. DEFERRED PER DMI 72-34 IS APPROVED FOR ONE FLIGHT CYCLE. REMOVED AND REPLACE INTERMEDIATE FAN CASE SERVICE BRACKET @ #1 ENG 5 OCLOCK POSITION IAW AMM 72-34-07
LEFT ENGINE CHANGE IS REQUIRED DUE TO BORESCOPE INSPECTION AS UNSERVICEABLE CONDITION ENGINE SN 724732. REMOVED AND INSTALLED LEFT ENGINE IAW AMM 71-00-02, LEAK CHECK AND ENGINE RUN GOOD.
DURING CLIMB, LEFT ENGINE N1 VIBE REACHED 3.0. AT TOP OF CLIMB, ENG N1 REACHED 5.0. LASTED 6-7 MINUTES UNTIL TOP OF DESCENT. VIBRATION FELT IN COCKPIT. PERFORMED FIM 71-05FT 806 STEPS 1-4 NO DEFECTS NOTED. BORESCOPE REQUIRED. BORESCOPE FOUND HPC # 5-7 DAMAGED AND UNSERVICEABLE DUE TO LE TIP CURLS AND DENTS. ENGINE CHANGE REQUIRED.
DURING POST-FLIGHT WALKAROUND FOUND #1 ENG BLADE 18 WITH TIP CURL AND TEAR. REMOVED AND REPLACED #1 ENGINEBLADE #18 IAW AMM 72-31-02
L ENG ANTI-ICE DOES NOT ALWAYS CLOSE, VALVE LIGHT STAYS ON, EXTINGUISHES LATER. REMOVED AND REPLACED LH ENGINE INLET TAI VALVE. PER AMM 30-21-03, OPS AND LEAK CHECK GOOD. UNIT UNKNOWN TO TRAX.
APU PNEUMATIC AIR NOT WORKING. DEFERRED PER MEL 49-11-01-A. PERFORMED FIM FAULT TREE 49-11-987. FOUND P2 SENSOR FAILED. REMOVED AND REPLACED P2 SENSOR, TEST OK IAW AMM 49-61-04.
#2 ENGINE LH AND RH IGNITORS WORN TO LIMITS. REMOVED AND REPLACED BOTH IGNITOR PLUGS IAW B767 AMM 74-21-02
APU WENT TO AUTO-SHUTDOWN, 2 ATTEMPTS TO START FAILED. ACCOMPLISHED APU CONTROL UNIT BITE TEST, NO FAULT FOUND IAW AMM 49-61-05.
KMIA CONFIG WARNING ON V1 FOLLOWED BY LE SLAT ASYM, PERFORMED QRH, RETURNED TO MIA. ACCOMPLISHED FIM 27-801 FT 809 FSEU BITE SHOWS NO CURRENT FAULTS. FT 803 FOUND RIGHT CARD INTERNAL FAULT, REMOVED AND REPLACED PSEU IAW B767 AMM 32-09-04. PART INFO UNKNOWN TO TRAX.
PILOT REPORTED ON POST FLIGHT CHECK THAT OBSERVED POSSIBLE NICKS ON #1 ENGINE BLADES 2 11 12 15 18. PERFORMED VISUAL INSPECTION, ALL NICKS ARE IN PERMITTED LIMITS WITHOUT REPAIRS PER AMM 72-31-02
APU DOOR EICAS MESSAGE. APU DOOR REMAINS OPEN. REMOVED AND REPLACED C868, PERFORMED APU OPS CHECK IAW 49-11-00 OPS CHECK GOOD.
DURING ENGINE 1 IGNITOR PLUGS INSPECTION FOUND IGNITOR PLUG WORN OUT. REMOVED AND REPLACED IGNITOR PLUG 1 ON ENGINE 1 PER AMM 74-21-02 OPS CHECK GOOD PER AMM 74-00-00
NOTICED HIGH VIBRATION FROM LEFT ENGINE AT TAKEOFF. IN CRUISE, LEFT ENGINE SHOWS VIBRATION N1 VARIABLE BETWEEN 3.7 & 4.1 @ FL350. ACCOMPLISHED FAN LUBE PER B767 AMM 72-31-02, MID SPAN SHROUD LUBE WAS PERFORMED PER WO 1223028 TC 767-72-433-01-01
ISOLATION VALVE EICAS MESSAGE. NO DUCT PRESSURE. REPLACED CENTER ISOLATION VALVE IAW AMM 36-11-04 OPS CHECK GOOD. PART UNKNOWN TO TRAX.
LEFT ISOLATION VALVE EICAS MESSAGE. NO DUCT PRESSURE INDICATED AND ASSOCIATED L ISLN LIGHT. SWAPPED LEFT AND CENTER ISOLATION VALVES PER AMM 36-11-04 INSTALLATION TEST PASSED.
WINDOW HEAT RT SWITCH INOP LIGHT CAME ON DURING FLIGHT. REMOVED AND REPLACED RT WHCU IAW B767 AMM 30-41-01 TESTS OK. PART UNKNOWN TO TRAX.
#2 ENGINE BLADES # 4, 9, 17, 23, 25, 27, 30 31, FOUND WITH NICKS IN VARIOUS LOCATIONS. ALL NICKS BLENDED IAW AMM 72-31-02 AND FOUND WITHIN LIMITS. PERFORMED NDT HFEC AND FPI INSPECTION PER AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED.
ON SERVICE CHECK INSPECTION FOUND APU LUBE OIL DIFFERENTIAL PRESSURE INDICATOR POPPED OUT. REMOVED AND REPLACED LUBE FILTER ELEMENT AS PER REF B767 AMM 49-27-03. PERFORMED OPS CHECK FOUND NORMAL.
RIGHT ENGINE SPINNER FOUND WITH CRACKS AROUND MOUNTING BOLT HOLES. REMOVED AND REPLACED RIGHT ENG CONE SEGMENT INLET IAW AMM 72-31-04
EICAS MESSAGE CABIN ALT AUTO 2 UPON CONNECTING GROUND POWER. DEFERRED PER MEL 21-31-01A CAT C
CABIN ALT AUTO 2 IN STATUS MSG. REMOVED AND REPLACED OUTFLOW VALVE AS PER B767 AMM 21-31-03. PART INFO UNKNOWN TO TRAX.
LEFT ENGINE N1 VIBRATION AVERAGED 3.2 TO 3.5 ON CLIMBOUT AND CRUISE, NO AIRFRAME VIBRATIONS. LUBED MID-SPAN SHROUD PER AMM 72-31-02, CHECKED ALL BLADES, NO DAMAGE NOTED.
RIGHT PACK TEMP EICAS, UNABLE TO RESET. MI @ 1146Z. DEFERRED PER MEL 21-51-01-01 CAT C AT 1225Z ON 1/11/24.
LEFT BLEED ISO VALVE EICAS. RETURN TO GATE MI 1304Z. PERFORMED LEFT ISOLATION VALVE OPS CHECK IAW AMM 36-11-04, PARAGRAPH G, OPS CHECK GOOD AT THIS TIME.
APU DID NOT START IN 3 ATTEMPTS. DEFERRED INOP APU PER MEL 49-11-01A CAT C ON 1/9/2024@0145Z.
#1 ENGINE BLADE #36 BENT OUT OF LIMITS FOUND AT WALKAROUND BEFORE DEPARTURE. REMOVED AND REPLACED FAN BLADES #36 AND #18 ON #1 ENGINE IAW AMM 72-31-02, VIBRATION CHECK NORMAL.
LEFT ENGINE FAN BLADE #18 HAS ONE NICK. BLENDED LEFT ENG FAN BLADE #18 PER MM 72-31-02, NDT DEFERRED. DYE PEN INSPECTION GOOD.
DURING DESCENT INTO AIRPORT, R FWD EICAS MESSAGE ILLUMINATED. PERFORMED TS IAW FIM 30-41-FT 803, FOUND CONTROLLER AND R1 WINDOW BAD/UNSERVICEABLE. DEFERRED WINDOW HEATING ELEMENT AT R1 WINDOW PER MEL 30-41-01-01. REMOVED ADN REPLACED R1 WINDSHIELD IAW AMM 56-11-01. UNIT IS NOT IN TRAX.
LH ENGINE ANTI ICE EICAS MESSAGE WHEN ANTI ICE SELECTED OFF AT LOWER POWER SETTINGS. ON PRELIM INSPECTION FOUND NO L ENG TAI EICAS MESSAGE. NOR VALVE LIGHT ILLUMINATED. PERFORMED L ENG TAI VAIVE OPERATIONAL CHECK, OPS CHECK GOOD.
DURING WALKAROUND RH ENGINE FOUND NICKS ON BLADES 9,14,15, 20 AND 36. ALL NICKS BLENDED PER AMM 72-31-02. NDT DEFERRED, ALL BLADES NDT CHECKED GOOD.
MI ON THE GROUND IN SPJC @0040Z WX NO DATA. WEATHER RADAR NOT WORKING. PEFORMED FIM 34-43 FAULT TREE 805. WXR SYSTEM OK.
DURING WALKAROUND IN MIA FOUND #1 ENG #32 BLADE WITH SMALL NICK. INSPECTED #1 ENGINE #32 FANBLADE AND FOUND WITHIN SERVICEABLE LIMITS PER AMM 72-31-02
RIGHT FWD WINDOW HEAT PB SHOWS INOP CAME ON IN FLIGHT QRH PROCEDURE PERFORMED REMOVED AND REPLACED RH WINDOW HEAT CONTROL IAW AMM 30-41-01 TEST OK. NO TRAX INFO AVAILABLE.
SMALL NICKS FOUND IN #2 ENGINE BLADES #'S 3,12,23,25,29. ALL NICKS BLENDED AND WITHIN LIMITS IAW AMM 72-31-02. DYE PENETRANT INSPECTION COMPLETED, NDN IAW AMM 70-11-06
#1 ENG COMPRESSOR INTERMEDIATE CASE FAIRING LOOSE RIVETS AT 3 OCLOCK POS. DEFERRED #1 ENGINE COMPRESSOR INTERMEDIATE CASE FAIRING RIVETS AT 3 OCLOCK PER DMI 72-34, REPLACE RIVETS BEFORE 101ST HOUR OF OPERATION PER AMM 72-34-05
L ENGINE ANTI ICE VALVE STICKING IN OPEN POSITION AT LOWER POWER SETTINGS. PERFORMED LH TAT VALVE OPS CHECK GOOD PER AMM 30-21-03
FOUND UPPER APU BONDING WIRE MISSING 2 EA. INSTALLED APU UPPER BONDING WIRES 2 EA IAW AMM 49-11-01
FOUND APU EXHAUST DUCT DAMAGED, LEFT SIDE. REMOVED AND REPLACED APU EXHAUST DUCT LEFT SIDE IAW AMM 49-11-01
ON CLIMBOUT LEFT ENGINE VIB INDICATION .5 TO 5.0 VERY QUICKLY, NO VIBRATION FELT AND IN CRUISE VIBE STAYS AT .4 NO CHANGE. TS PER FIM 77-31-00 FT 803 AND BITE DID NOT SHOW ANY FAULTS, PERFORMED FIM FT 808 AND FOUND LOOSE CABLES, RESECURED CABLES PER FIM 77-31 FT 808
DURING IDLE AT GATE, APU OIL LEVEL READS ZERO AT LOWER EICAS SCREEN. SERVICED APU OIL TO PROPER LEVEL IAW AMM 12-13-14, NO LEAKS NOTED, NO APU OIL QTY SERVICED GIVEN.
LEFT RADAR RT ALSO SHOWS WINDSHEAR MESSAGE. REMOVED AND REPLACED WEATHER RADAR R/T OPS NORMAL IAW AMM 34-43-01.
LEFT RADAR OTS. TS LH WXR, FOUND DEBRIS ON COOLING TRAY, REMOVED AND REPLACED LH WX TRANSCEIVER, OPS CHECK OK PER AMM 34-43-01. UNIT UNKNOWN TO TRAX.
ON CLIMBOUT DURING CLIMB EICAS LE SLAT ASYM LEADING EDGE LIGHT ON. QRH EXECUTED PER PROCEDURE. T/S REPLACED 5284 SENSOR IAW AMM 27-88-01, SPEU ADN FSEU OPS CHECK OK
L ENG EEC STATUS AFTER FCF. PERFORMED TROUBLESHOOTING IAW FIM 73-21 FT 828 AND FAULT MSG 350-17. REMOVED AND REPLACED LEFT ENGINE FUEL METERING UNIT IAW B767 AMM 73-21-01 POWER OPS AND LEAK CHECK GOOD.
L ENGINE CONTROL STATUS MESSAGE AFTER FCF. PERFORMED TROUBLESHOOTING IAW FIM 73-21 FT 828 AND FAULT MSG 350-17. REMOVED AND REPLACED LEFT ENGINE FUEL METERING UNIT IAW B767 AMM 73-21-01 POWER OPS AND LEAK CHECK GOOD.
#1 ENGINE LEAKING FROM SPINNER FAN/SECTION UPON SHUTDOWN. REMOVED AND REPLACED #1 ENGINE IAW MM 71-00-02 ENG RUN IN IDLE OPS CHECK NORMAL IAW AMM 71-00-00
L ENGINE CONTROL EICAS MESSAGE. PERFORMED FIM 73-21 FAULT TREE 825 AND 71-01 TASK 807 AND 826. NO DISCREPANCIES NOTED, OPS CHECK NORMAL.
WEATHER RADAR TILT SETTING NOT CALIBRATED CORRECTLY. OPS CHECK LEFT AND RIGHT WEATHER RADAR SYSTEM IAW AMM 34-43-00, OPS CHECK NORMAL.