N563NC
Registered owner: NAS AIRCRAFT LEASING COMPANY 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 2 ENGINE BLEED LIGHT ILLUMINATED DURING ENGINE RUN WITH HSPOV MESSAGE DISPLAYED ON ICAS. REMOVED AND REPLACED NR 2 ENG HPC IAW AMM 36-11-18-04-005-008 AND 36-11-08-04-0050-008 OPS CHECK GOOD.
NUMBER 1 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH LEAKING. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01-004-001 AND AMM 73-34-01-404-016 NO LEAK NOTED.
TROUBLESHOOT RT ENGINE HPSOV INDICATION FOUND DURING IDLE. PERFORMED EICAS MAINT MASSAGE ERASE PROCEDURE IAW AMM 31-41-00-912-009. SYSTEM OK.
TROUBLESHOOT RT ENGINE PRV INDICATION FOUND DURING IDLE. PERFORMED EICAS MAINT MESSAGE ERASE PROCEDURE IAW AMM 31-41-00-912-009, SYSTEM OK
NR 2 ENGINE, SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. THE ENGINE WAS R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605
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.
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
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.
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.
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.
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.
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.
RH INBOARD AFT FLAP UPPER TRAILING EDGE SURFACE HAS CORROSION.
STRINGER 32R IN AFT ACCESSORY COMPARTMENT IS CORRODED BETWEEN BS 1809-1832.
CORROSION FOUND ON LH I/B AFT FLAP UPPER SURFACE.
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.
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.
OUTFLOW VALVE DRIVE LINKAGE CORRODED. R & R THE LINKAGE ON OUTFLOW VALVE IAW AMM 20-11-00-993-809.
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.
OUTFLOW VALVE LINKS ROD END AND ATTACHMENT HARDWARE CORRODED.
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.
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.
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.
#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).
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.
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.
APU WILL NOT START. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01 OPS CHECK NORMAL.
R ENG #1 IGNITOR INOP. REMOVED AND REPLACED RH IGNITOR PLUG IAW AMM 74-21-02 OPS CHECK OK IAW 74-00-00
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.
ON PREFLIGHT LEFT ENGINE FAN BLADE DAMAGE #30. REPAIRED BLADE ON LH ENGINE #30 PER AMM 72-31-02
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
DURING READINESS CHECK LIST FOUND RIGHT GENERATOR DRIVE LIGHT OFF WITH R ENG IN CUTOFF. REPLACED IDG IAW AMM 24-11-01
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.
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.
R ENG VIBE GAUGE ERRATIC ENTIRE FIGHT. VARIES BETWEEN .1 - 1.8. REMOVED AND REPLACED AVM IAW AMM 77-31-03 TEST OK.
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.
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.
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.
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
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
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
L ENG PRV. INSTALLED ASSY CONTROLLER PRESSURE 707 PW FROM SECTION E TO 13 SUBTASK 36-11-19-424-016-003.
L ENG A/O VALVE. L ENG A/O VALVE. REMOVED AND REPLACED #1 ENGINE.
L ENG EEC C1. L ENG EEC C1 STATUS MESSAGE ASSOCIATED WITH L ENG AO VALVE , REMOVED AND REPLACED #1 ENGINE
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.
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.
FOUND THE L ENG EEC MSG. REPLACED #1 ENG AIR/OIL HEAT EXCHANGER VALVE IAW AMM 79-21-09
FOUND THE RH HF CONTROL PANEL MALFUNCTION. REMOVED AND REPLACED THE RH HF CONTROL PANEL IAW AMM 23-11-02
FOUND RH AIR CONDITION TCV MALFUNCTION. REMOVED AND REPLACED PACK TCV IAW AMM 21-54-12
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
FOUND LH PACK COMPRESSOR OH SWITCH CONNECTOR D01576 CRACKED. REMOVED AND REPLACED CONNECTOR D01576 IAW SWPM 20-61-00
REMOVED AND REPLACED RH PACK COMPRESSOR O/H SWITCH CONNECTOR @1562 BACKSHELL CLAMP IAW SWPM 21-61-11
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.
LH PRSOV BITE TEST FAIL. REMOVED AND REPLACED LH PRSOV IAW AMM 767-36-11-09
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.
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.
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.
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
FOUND #2 ENG CORE COWL HINGE BOLT COULD NOT SELF LOCK. REPLACED #2 ENG CORE COWL HINGE BOLT IAW 767-300 AMM 71-11/
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
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.
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
L ENG HPSOV. PERFORMED AIR SUPPLY BITE TEST, STATUS MESSAGE CLEARED, NO FAULTS NOTED.
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.
RIGHT HF RADIO BLANK/NO POWER. REMOVED AND REPLACED HF COMM CONTROL PANEL PER AMM 23-11-02.
RIGHT HF RADIO BLANK/NO POWER. RESET HF COMM CONTROL PANEL PER AMM 23-11-00. OPS CHECK GOOD.
RIGHT HF RADIO FAIL IN ITS DISPLAY WINDOW. RESET RH HF CONTROL PANEL PER AMM 23-11-00 OPS CHECK GOOD.
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
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.
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
#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
PILOT REPORTED R1 WINDOW HEAT LIGHT INOP DURING FLIGHT. FLIGHT DECK WINDOW HEAT SYSTEM #2 SIDE DEFERRED IAW MEL 30-41-01.
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.
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.
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
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
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
APU BLEED AIR NO START. DEFERRED APU BLEED VALVE PER MEL 36-11-04
AFTER RIGHT ENGINE START APU BLEED VALVE ON EICAS. DEFERRED APU BLEED VALVE PER MEL 36-11-04 10-7-23
LEFT SIDE WX FAIL. DEFERRED PER MEL 34-43-01, LEFT SYSTEM WEATHER RADAR INOP CAT D, 10/8/2023
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.
MECHANICAL IRREGULARITY NO AIR OUTPUT FROM APU. DEFERRED APU BLEED VALVE PER MEL 36-11-04
APU FUEL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED APU FUEL FILTER ELEMENT IAW AMM 49-31-04 NO LEAKS NOTED.
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.
#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
#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
#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
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.