Pitot-static tester 6300L

pressurefor altimetersaeronautical

The 6300L RVSM Automated Tester is designed to connect directly to an aircraft’s Pitot and Static system. Using the small and light-weight Remote unit a user can operate the tester from the cockpit and use it to test the entire pitot and static system of the aircraft, including altimeters, climb indicators, airspeed / Mach indicators, air data computers, and auto-pilots. The tester includes built-in vacuum and pressure pumps and emergency manual bleed-down valves. The operator simply connects power, and the pitot and static hoses, to make the unit operational. Also, it needs to be calibrated only once a year. The use of “Profiles” makes it possible for the operator to run through a test using only a single key on the Remote unit. Also, all commands can be performed through the RS232 interface. STATIC OUTPUT 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 Mach Function Range: 0.0 to 3.0 Mach Resolution: 0.001 Mach Accuracy: ±0.001 above 0.2 Mach