Aircraft Pitot Tube Leakage Tester

Description

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Pressure/Altitude/Airspeed Specification

Parameter Operating Range Resolution Accuracy
Pt Sensor -30 to 60 inHg 0.001 0.025% F.S
Ps Sensor -30 to 60 inHg 0.001 0.025% F.S
Barometric Sensor 22 – 35 inHgA 0.001 0.025% Reading
Altitude (Ps) -2000 to 50,000 ft 1 ft
3 ft @ 1000 ft
7 ft @ 10,000 ft
50 ft @ 40,000 ft
Airspeed (Pt) 50 to 650 knots 0.1 knots ±0.5 knots
Other Specification
Temperature Compensation 15 – 45 °C to rated accuracy
Selectable Engineering Units Knots, Feet, mbar, psi, inHg, hpa, mbarA, psiA, inHgA, hpaA
Display Type L.C.D Graphic Module, 128×4 dots
Display Information Line1(Pt) and Line2 (Ps)
Line 1 and Line 2 display both Feet reading
Pressure Generation Built-in electric pressure pump(self-generate), 30 psig
Vacuum Generation Built-in electric vacuum pump(self-generate), 95% vacuum
Relief Valve Protection Internal 10inHg between Pt and Ps line
Pressure Outlet x2 1/8”FNPT. Eaton quick connect B1K11 (1/4” FNPT)
Eaton quick connect plug B2K16 (1/8” FNPT)
Switch Input
Non Voltage Input, N.O or N.C type Display “OPEN” or “CLOSE” switch status
General Specification
Warm up time 5 minutes
Size 390x310x170 mm (Nanuk 915 case)
Weight 7.5 kg
Power 14.8Vdc @ 4AH Li-ion Battery
Charge / operating hours 4 hours per charge, 10 hours continuously use
Local Factory Warranty 1 year (including parts and labor)

Note: Pt (address 1), Ps (address 2), Baro (address 3)

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