The 6600 Automated Tester is ideal for use on aircraft with SmartProbe™ capable of measuring AOA using Air Data. The tester has one Static output (Ps1), one Pitot output (Pt) and a third output (Ps2) which can be used to simulate either AOA or AOS. Using the small and light-weight Remote unit a user can operate the tester from the cockpit and test the entire pitot and static system of the aircraft. The tester includes built-in vacuum and pressure pumps and emergency manual bleed-down valves. The high accuracy of this unit meets all RVSM requirements. Calibration is required only once a year.
Pressure function
Range:
0.1 to 42 inHg
Resolution:
0.001 inHg
Accuracy:
±0.002 inHg
Units:
inHg, mbar
Altitude function
Range:
-4000 ft. to 60,000 ft.
Resolution:
1 foot
Accuracy:
± 2 ft. @ 0 ft.
± 6 ft. @ 35,000 ft.
± 12 ft. @ 50,000 ft.
Units:
Feet, Meters
Climb function
Range:
0 ft/min to ±25,000 ft/min
Resolution:
1 ft/min
Accuracy:
±1% of rate of climb
Units:
Feet/min, Meters/sec
PITOT OUTPUT
Pressure Function
Range:
0.1 to 60 inHg
Resolution:
0.001 inHg
Accuracy:
±0.003 inHg
Pt Units:
inHg, mbar, EPR
Qc Units:
inHg, mbar
Airspeed Function
Range:
0 to 650 knots
Resolution:
0.1 knots
Accuracy:
± 0.5 knots @ 50 knots
± 0.25 knots @ 100 knots
± 0.05 knots @ 650 knots
Units:
knots, Mach, km/hr, mph
Rate of change:
0 to 500 knots/min