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TM 1-4920-458-13&P
Section II. Equipment Description
SECTION CONTENTS
PARA
PAGE
FUNCTION
1-6
1-3
INPUT POWER
1-7
1-3
LOCATION AND DESCRIPTION OF MAJOR COMPONENTS
1-8
1-4
EQUIPMENT DATA
1-9
1-6
1-6.
FUNCTION
The Pitot and Static Systems Tester is a pneumatic testing system that simulates aircraft airspeed from 0-400 knots;
altitude from -1000 to 35,000 feet; and rate of climb from ±6000 feet per minute. Pitot and Static Systems Tester can
also be tested for leakage. The control panel of the Tester contains the three (3) appropriate aircraft instruments: Rate
of Climb, Altimeter, and Airspeed Indicator.
1-7.
INPUT POWER
The Tester contains three power cables and one cable adapter to permit operation from the following power sources:
28 + 4, -6 volts DC
115 volts AC ± 10 percent, 50 to 500 cycles, single phase.
115 volts AC ± 10 percent, 50 to 500 cycles, three phase.
1-3
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