N340PX
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.
9 reports on file, 1997-01-09 – 1997-09-16.
Part: CHIP DETECTOR — DIRTY (RT ENGINE)
RIGHT CHIP DETECTOR LIGHT CAME ON EN ROUTE. DID AIR RETURN TO MEM. CLEANED CHIP DETECTOR ON RIGHT ENGINE. (M)
Part: CTOT PANEL — MALFUNCTIONED (SINGLE)
ON TAKEOFF LEFT TORQUE INDICATION WOULD NOT SET AND ERRATIC INDICATIONS THEREAFTER. REMOVED AND REPLACED CTOT PANEL. PERFORMED FUNCTIONAL CHECK OF CTOT, NO FURTHER DEFECTS NOTED. (M)
Part: TURBINE — WORN (LT ENGINE)
TROUBLESHOT LEFT ENGINE OIL CONSUMPTION ON OVERSERVICEABLE LIMITS. REMOVED AND REPLACED LEFT POWER TURBINE IAW AMM 71-00-05. PERFORMED ON WING BREAK IN AND GROUND POWER ASSURANCE RUNS. OPS AND LEAK CHECK GOOD. REMOVED LEFT ENGINE FROM OVERSERVICEABLE LIMITS. AIRCRAFT OK FOR SERVICE. (M)
Part: CTOT — FAILED (LEFT ENGINE)
LEFT ENGINE CTOT WOULD NOT COME UP ON TAKEOFF (2 ATTEMPTS). DEFERRED AND PLACARD PER MEL. (X)
Part: RADAR TUBE — FAILED (RT COCKPIT)
RETURNED TO GATE DUE TO WEATHER RADAR BEING DEFERRED. REMOVED AND REPLACED RIGHT RADAR AND LEFT EFIS TUBE. (M)
Part: 4.5 BIAS TRIMMER — FAILED (LT ENGINE)
LEFT ITT FLUCTUATES PLUS/MINUS 50 IN CRUISE. CHANGED 4.5 BIAS TRIMMER. (M)
Part: PITCH TRIM — MALFUNCTIONED (ELEVATOR)
MAIN PITCH TRIM FAILED IN FLIGHT DECLARED EMERGENCY. UNABLE TO VERIFY PROBLEM. TESTED AND INSPECTED TRIM AND RELATED SYSTEMS WITH NO DEFECTS NOTED. (M)
Part: PROP GEAR BOX — LOW OIL (RT ENGINE)
RIGHT OIL PRESSURE CWP LIGHT. RIGHT PROPELLER GEAR BOX OIL PRESSURE IS IN LOWER YELLOW ARC AND OIL TEMP IN UPPER YELLOW ARC. SERVICED RT PROPELLER GEAR BOX WITH 1.5 QUARTS OF OIL. (M)
Part: HYD SWIVEL — FAILED (RT MLG)
LOST HYDRAULIC FLUID TAKEOFF. INSTALLED NEW SWIVEL ON MAIN GEAR DOWNLOCK ACTUATOR, SERVICED HYDRAULIC RESEVOIR WITH 5606, TEST FLIGHT REQUIRED. (M)