N674DJ

RAYTHEON AIRCRAFT COMPANY 400A · 1999 · Fixed-wing multi-engine · 2 engines · 10 seats · Valid Registration

Registered owner: FALCON 7 LLC, DE (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.

2 reports on file, 2011-04-14 – 2011-04-20.

WARNING INDICATION · 2011-04-20 Matched by certificate designator
ATA 2742

Part: ACTUATOR — DEFECTIVE (HORIZONTAL STAB) · airframe 3,810 hrs · 2,912 cycles

THE HORIZ STABILIZER ACTUATOR FAILED 3.5 HOURS AFTER INSTALLATION. THE CREW REPORTED THAT DURING PREFLIGHT PREPARATIONS THE EMERGENCY/AUTOPILOT MODE OF THE HORIZONTAL STABILIZER ACTUATOR FAILED. THIS ACTUATOR PN 45AS61023-143, SN ET0050 WAS INSTALLED AFTER FAILURE OF SN ET0049 NORMAL FUNCTION MODE ONE DAY BEFORE. BOTH ACTUATORS (S/N ET0050 AND ET0049) WERE O/H. THE HORIZ STABILIZER ACTUATOR SYS WAS TROUBLESHOT AND INTERMITTENT RESISTANCE READINGS WERE FOUND IN THE EMERGENCY/AUTOPILOT MODE OF ACTUATOR MOTOR (ACTUATOR SN ET0050). THE ACTUATOR SN ET0050 WAS REPLACED BY S/N ET0042 AND THE ACFT WAS RETURNED TO SERVICE WITHOUT FURTHER PROBLEMS.

Source: SDR 9JLA2093
OTHER · 2011-04-14 Matched by certificate designator
ATA 2742

Part: ACTUATOR — DEFECTIVE (HORIZONTAL STAB) · airframe 3,806 hrs · 2,910 cycles

THE HORIZ STABILIZER ACTUATOR WAS DUE FOR O/H AND WAS REPLACED WITH AN O/H HORIZ STABILIZER ACTUATOR OF A DIFFERENT SN (ET0049). THE UNIT WAS INSTALLED BY A REPAIR STATION. GROUND FUNTIONAL/OPS AND THE OPS CHECK FLIGHT CHECKS WERE SATISFACTORY. DURING THE FIRST FLIGHT FOLLOWING THE OPS CHECK FLIGHT THE CREW WAS UNABLE TO OPERATE THE NORMAL PITCH TRIM FOLLOWING AUTOPILOT DISENGAEMENT ON APPROACH. THE CREW SWITCHED TO EMERGENCY PITCH TRIM MODE AND MADE AN UNEVENTFUL LANDING. A CONTINUITY CHECK OF THE ACTUATOR FOUND THE NORMAL MOTOR BRAKE WINDINGS TO BE OPEN. A REPLACEMENT ACTUATOR SN ET0050 WAS INSTALLED AND THE ACFT WAS RELEASED FOR FLIGHT.

Source: SDR 9JLA2091