Leerjet 35/36 Developed for Training Purposes 4A-5
February 2007
Avionics
Pitot/Static System
On aircraft with an FC-200 autopilot, an electrically heated
pitot probe on the left and right nose supplies pitot pressure to
the flight instruments and airspeed warning systems. The left
pitot probe only supplies the pilot’s airspeed indicator. The right
pitot probe supplies the copilot’s airspeed indicator, Mach trim,
Mach warning and overspeed, switches, and air data sensor.
The left forward and right center static ports supply the pilot’s
altimeter and airspeed indicator. A selectable alternate static
source supplies these instruments if the normal static source
fails.
The left aft and right forward static ports supply the copilot’s
altimeter, airspeed indicator, and vertical speed indicator (VSI).
These static sources also supply the Mach trim, Mach warning
and overspeed warning, altitude pressure, and airspeed
switches.
The unheated right aft static port and a static port in the nose
compartment supply the pressurization module assembly.
Two shoulder static ports forward of the windshield supply
static pressure to autopilot air data sensor.
On aircraft with a typical RVSM
1
FC-530 autopilot, an elec-
trically heated pitot/static probe on the left and right nose sup-
plies pitot and static pressure to the pilot’s and copilot’s pitot/
static systems. The left pitot/static probe supplies the pilot’s air-
speed indicator. The right pitot/static probe supplies the copi-
lot’s airspeed indicator, air data unit (ADU), and the 0.74 Mach
switch.
1.RVSM installations vary. Consult your AFM for specific informa-
tion.
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