Leerjet 35/36 Developed for Training Purposes 6-13
February 1998
Servicing
To blend anti-ice additive:
Prist Blender . . . . . . . . . . . . . . . . . . . . ATTACH TO NOZZLE
. . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . .(Figure 6-2)
Fuel Nozzle . . . . . . . . . . . . . . . . . . .REGULATE FLOW RATE
Flow rate should be between 30 and 50 gallons per minute.
Prist Blender . . . . . . . .DIRECT FLOW INTO FUEL STREAM
Prist Blender . . . . . . . . . . . . . . . . . . . . . . . . . . STOP FLOW
Fuel Nozzle . . . . . . . . . . . . . . . . . . . . . . STOP FUEL FLOW
Figure 6-2. Attaching Refueling Nozzle
CAUTION: Ensure additive is directed into the fuel stream.
Ensure the additive flow begins after the fuel flow starts. Stop
the additive flow before the fuel flow stops. Do not allow con-
centrated additive to contact interior of fuel tank or aircraft
painted surfaces.
BLENDER TUBE (MUST BE ATTACHED
SO THAT ADDITIVE DISCHARGES
INTO THE FUEL STREAM)
REFUELING
MAT
RING
ANTI-ICING ADDITIVE PHF-204
HI-FLO PRIST (20 FL. OZ. CAN)
FUEL NOZZLE
TRIGGER
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