N450JE
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.
3 reports on file, 2011-01-25 – 2015-02-12.
Part: ACTUATOR — UNWANTED DEPLOY (ZONE 400) · airframe 10,738 hrs · 3,654 cycles
AT ABOUT 1200 FT ON CLIMB OUT, CREW NOTICED AURAL WARNING & THE CAS SHOWED A RED L REV UNLOCKED INDICATION.
Part: BLEED BAND — DEBONDED (ENGINE) · airframe 9,839 hrs · 3,345 cycles
GRADUAL DECREASE IN POWER TO RIGHT ENGINE. FOUND BLEED BAND DEBONDED.
Part: ELECTRONIC UNIT — INTERMITTENT (ZONE 500) · airframe 8,130 hrs · 2,759 cycles
IMMEDIATELY AFTER REACHING CRUISING ALTITUDE OF FL410, THE CREW NOTICED THE LT AUTOTHROTTLE ADVANCING FOLLOWED IMMEDIATELY BY A MASTER CAUTION CHIME/LIGHT. CAS MESSAGES OF LT FUEL PRESS LOW (RED CAPTION), LT MAIN FUEL FAIL (AMBER), LT ALT FUEL FAIL (AMBER). THE AUTOTHROTTLE ADVANCING WAS THE ENGINE STARVING FOR FUEL. THE PIC RETARDED THE ENGINE AND RETURNED TO DEPARTURE AIRPORT AND DECLARED AN EMERGENCY AS A PRECAUTION. AS THE ACFT DESCENDED, THE INDICATIONS CLEARED THEMSELVES AND AN UNEVENTFUL LANDING WAS MADE. THE MALFUNCTION OCCURRED ABOUT 21 MINUTES INTO THE FLIGHT UPON REACHING CRUISING ALTITUDE (FL410). TROUBLESHOOTING IN COOPERATION WITH THE MFG TECH DETERMINED THAT POWER WAS LOST TO BOTH LT WING BOOST PUMPS AND THAT THE LIKELY COMPONENT WAS AN INLINE FILTER (ELECTROMAGNETIC INTERFERENCE) AS IT IS THE ONLY PLACE WHERE BOTH SYSTEMS (MAIN AND ALT) ARE IN THE SAME LOCATION. THE SYS IS DESIGNED TO SELF FEED BELOW FL270 WHICH IS WHY THE MESSAGES EXTINGUISHED ON DESCENT. REPLACING THE FILTER PN 1159SCP011-13 AND PERFORMING A TEST FLIGHT PROVED A SUCCESSFUL RECTIFICATION.