N706XJ
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, 2014-04-18 – 2017-01-05.
Part: LINE — CHAFED (NR 1 ENGINE) · airframe 9,491 hrs · 5,665 cycles
WHILE CONDUCTING A FLEET WIDE FIRE LOOP INTERFERENCE INSPECTION, THE FOLLOWING ITEMS WERE FOUND ON ENGINE NR 1. REPLACED OIL LINES (P/N 23056412 AND 23065390), DUE TO CHAFFING BEYOND LIMITS. NO DEFECTS WERE NOTED ON THE NR 2 ENGINE.
Part: TUBE — BENT (LT WING) · airframe 7,540 hrs · 4,756 cycles
WITH THE WING ANTI-ICE SYS ACTIVATED IN FLIGHT, THE INBD TEMPERATURE SENSORS WOULD TRIGGER THE LT & RT WING ANTI-ICE HOT CAS MSG. RAN THE ANTI-ICE SYS MONITORED THE TEMP SENSORS THROUGH THE IMT WITH NO ABNORMALITIES NOTED. BLEED LEAK MSGS WILL MOST LIKELY NOT SHOW UP DUE TO REDUCED POWER & RUN TIME LIMITATIONS. THE INBOARD LEADING EDGES FROM THE WING STRUCTURE TO INSPECT FOR BLEED LEAKS. WITH THE LE REMOVED & ON THE WORK BENCH, TECHNICIANS USED SHOP AIR TO PRESSURIZE THE LE & FOUND LARGE LEAKS AT THE LANDING LIGHT PICCOLO BELL MOUTH TUBE. UPON DISASSEMBLY OF THE LE IT WAS DISCOVERED THE ANTI-ICE WELDED TUBE ASSEMBLY PART NR HAD BECOME BENT RESULTING IN A REDUCED RADIUS, THUS MAKING THE TUBE ASSEMBLY SHORTER & ALLOWING THE SEALING D RING TO DETERIORATE & SUBSEQUENTLY LEAK HEATED AIR ONTO THE TEMPERATURE SENSORS. IT IS UNKNOWN HOW THE TUBE BECOMES BENT, IT IS SUSPECTED THE DAMAGE OCCURS DURING THE LAST INSTALLATION OF THE LES. THIS CONDITION HAS BEEN FOUND ON TWO DIFFERENT ACFT.
Part: ACTUATOR — FAILED (PITCH FEEL) · airframe 7,192 hrs · 4,576 cycles
WHILE EN ROUTE TO TEB, THE FLIGHT CREW RECEIVED A PITCH FEEL FAIL CAUTION MSG. THE DECISION TO DIVERT INTO OPF WAS MADE FOLLOWED BY AN UNEVENTFUL LANDING. TECHNICIANS FROM SERVICE CTR WERE DISPATCHED TO INSPECT & REPAIR THE ACFT. IT WAS DETERMINED THAT A PITCH FEEL ACTUATOR WAS FAULTY. THE NR 1 & 2 PITCH FEEL ACTUATORS, PN 9914558-10, WERE REPLACED & THE ACFT WAS RELEASED FOR A MAINTENANCE CHECK FLIGHT.