4A-6 Developed for Training Purposes Leerjet 35/36
February 2007
CAE SimuFlite
The left No. 1 and right No. 2 static sources supply the pilot’s alt
imiter, airspeed indicator, and VSI. The right No. 1 and left No.
2 static sources supply the copilot’s altimeter, airspeed indica-
tor, and VSI. These static sources also supply the ADU, 0.74
Mach switch, and optional equipment.
Electrically controlled isolation valves in the pilot’s and copilot’s
static source supply lines can be closed to isolate parts of the
static system.
An unheated static port and an alternate static source supply
the pressurization module.
Additional Instrumentation
Airspeed/Mach Indicator
Pitot/static inputs operate the pilot’s and copilot’s identical air-
speed indicators. The instruments utilize a single rotating nee-
dle and dual scales for accurate Mach and airspeed indication.
The indicator face consists of a circular airspeed scale reading
0 to 400 kts, a movable circular Mach scale reading 0.4 to 0.9
Mach, an airspeed/Mach pointer, and a maximum allowable
marker (barber pole).
On S/N 35-506 and subsequent; 36-054 and subsequent; or
aircraft with AAK 83-2, the airspeed/Mach indicators also con-
tain airspeed and altitude switches used by the stick puller, stall
warning system, and overspeed warning system.
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