N602KW
Registered owner: ALTA 767 SPV LLC, UT (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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
11 reports on file, 2018-09-11 – 2021-01-06.
Part: POWER LEVER — STUCK (LEFT) · airframe 72,326 hrs · 28,440 cycles
AT FL39,000 DURING CRUISE, LEFT THRUST LEVER WAS NOT RESPONDING AND EPR WAS STUCK AT 1.00. HAD TO DECENT TO FL36000 TO MAINTAIN AIRSPEED. EGT WAS BEING ERRATIC PRIOR TO THAT + OR MINUS 30 DEGREES. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS AVAILABLE.
Part: IDG — UNDERSERVICED (RIGHT) · airframe 72,326 hrs · 28,440 cycles
RIGHT GEN DRIVE EICAS MESSAGE AFTER TAKE-OFF, DRIVE DISC LIGHT CAME ON. CREW CALLED DISPATCH REPORTING RT IDG DRIVE/GEN. OFF EICAS MESSAGE, CREW FOLLOWED FCOM AND DECIDED TO RETURN FIELD (JFK). MOC CALLED JFK MX AND THEY WILL MEET THE AIRCRAFT UPON LANDING. INSPECTED AND SERVICED RT IDG, IDLE CHECK GOOD. APU PNEUMATIC PRESSURE AT 10 PSI, OPENED DMI. T/S PER FIM 24-20 FT 815 FOUND IDG OIL LEVEL LOW, SERVICED IDG OIL, PER AMM 12-13-03. RECONNECTED IDG DRIVE, PER AMM 24-11-01. PERFORMED ENGINE RUNS, PER 71-00-00. OPERATIONS CHECK SATISFACTORY. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS AVAILABLE.
Part: UNKNOWN — INOPERATIVE (EMERGENCY LIGHTS)
FAA PERFORMED AN INSPECTION ON THE AIRCRAFT 602 FOR A SERIES OF EMERGENCY EXTERIOR LIGHTS. THEY'RE AS FOLLOWS FOR SEATS 13 C-A/HK EMERGENCY EXIT INTEGRATED LIGHTS INOPERABLE. LEFT OVERWING EXTERIOR EMERGENCY LIGHTS C3J INOPERABLE. R-3 AFT EMERGENCY EXTERIOR LIGHT INOPERABLE. AFT CARGO COMPONENT (AFT) EMERGENCY EXTERIOR LIGHT INOPERABLE. BULK INTERIOR LIGHT WEAK ILLUMINATION. THESE FINDINGS WERE DISCOVERED DURING A FAA DAILY CHECK.
Part: ENGINE — OVERTEMP (LEFT) · airframe 72,089 hrs · 28,368 cycles
PASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT, AT FL380 TIME APPROXIMATE 0027Z. THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2, AND N3 WAS REDUCED WITH COMMAND THROTTLE REDUCED AND EGT BEGAN TO RISE (560 DEGS). THE PIC COMMANDED THE LT ENGINE TO BE SHUTDOWN. THE PIC RESTARTED THE ENGINE SUCCESSFULLY AT 25,000 FT AND THE ENGINE RAN NORMALLY DURING DECENT. THE PIC HAD DECLARED AN EMERGENCY WITH ATC INTO JFK. THE AIRCRAFT IS AOG IN JFK WITH AIRCRAFT MAINTENANCE WORKING THE ISSUE. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS AVAILABLE. SUPPLEMENTAL AS OF 10/8/20. REMOVED AND REPLACE ENGINE (716801 ENGINE).
Part: GENERATOR — DISENGAGED (LEFT) · airframe 72,089 hrs · 28,368 cycles
PASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT (AT FL380 TIME APPROXIMATE 0027Z). THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2 AND N3 WAS REDUCED WITH COMMANDED THROTTLE REDUCTION AND EGT BEGAN TO RISE (560 DEGS), THE PIC COMMANDED THE LT ENGINE BE SHUTDOWN. THE PIC RESTARTED THE ENGINE SUCCESSFULLY AT 25,000 FT & THE ENGINE RAN NORMALLY DURING DECENT. THE PIC HAD DECLARED AN EMERGENCY WITH ATC INTO JFK. THE AIRCRAFT LANDED UNEVENTFULLY WITH THE BOTH ENGINES UNDER POWER. AIRCRAFT IS AOG IN JFK WITH AIRCRAFT MAINTENANCE WORKING THE ISSUE. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS AVAILABLE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,049 hrs · 28,360 cycles
DURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,049 hrs · 28,360 cycles
DURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.
Part: BATTERY PACK — FAILED (CABIN) · airframe 72,034 hrs · 28,354 cycles
EMERGENCY LIGHT FOUND INOP DURING OPS CHECK OF L/H OVERWING SLIDE SYSTEM. REMOVED AND REPLACED L/H OVERWING SLIDE BATTERY PACK IAW B767 AMM 33-51-07. OPS CHECK NORMAL. NOTE: AIRCRAFT WAS IN MAINTENANCE CHECK AT THE TIME THE ISSUE WAS FOUND. FAA PMI HAS BEEN NOTIFIED.
Part: ENGINE — POWER LOSS (LEFT) · airframe 71,934 hrs · 28,327 cycles
ON DESCENT L/H ENGINE LOST PNEUMATIC PRESSURE AFTER THAT ENGINE FAILURE TO ACCELERATE. FOUND FUEL CONTROL APPROACH SOLENOID FAULTY, ACCOMPLISH TEST OF THE PNEUMATIC HIGH PRESSURE CONTROL FOUND OK, ACCOMPLISHED FULL GAS PATH BORESCOPE FOUND NO INTERNAL DAMAGE
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
1 SMALL EMERG EXIT LIGHT AFT OF CARGO DOOR, EXTERIOR INOP. RELAMPED SMALL EMERGENCY LIGHT AFT OF REAR CARGO DOOR IAW AMM 33-31-06. OPS CHECK OK
Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 71,822 hrs · 28,258 cycles
AT TOP OF DECENT LH ENGINE COMPRESSOR STALLED 4 TIMES. OIL PRESSURE DROPPED TO 13 PSI NO TEMPERATURE EXCEEDANCE SHUT DOWN PER QRH. SERVICED # 1 ENG OIL IAW B767 AMM 12-13-01. PERFORMED LEAK DETECTION IAW B767 AMM 79-00-00. NO LEAK NOTED. PERFORMED # 1 ENG IDLE RUN IAW B767 AMM 71-00-00. OIL PRESSURE INDICTED NORMAL