Learjet 35 - Page 343

Leerjet 35/36 Developed for Training Purposes 4H-13
February 1998
Ice and Rain Protection
Ice and Rain Protection Data
Power Source 28V DC
Bleed air
Distribution 28V DC
P
t2 Probe
Pitot-static
Stall warning vanes
Bleed air
Nacelle inlet and engine
Windshield
Wing and horizontal stabilizer
leading edges
Methyl alcohol (Methanol)
Pilot’s windshield
Radome
Control BAT/BAT 2 switches
L/R NAC HEAT switches
L/R PITOT HEAT switches
STAB/WING HEAT switch
WING INSPECTION ON/OFF pushbutton
On S/N 35-002 to 081, 083 to 086 and
36-002 to 022 without AAK 76-7
WSHLD AUTO/MAN switch
IN-NORMAL/OUT-DEFOG knob
On S/N 35-082, 087 to 106, 108 to 112;
36-023 to 031; prior aircraft with AAK 76-7
WSHLD AUTO/MAN switch
IN NORMAL/OUT-DEFOG knob