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Motor installation other than the Evolution
®
62GX:
The measurement from the firewall to the drive washer should
measure 7
1
/
inches (191mm). Make any necessary adjustments to
2
achieve this measurement.
Î The sample model required 1 lb (454g) of lead weight
in the nose to balance with the Evolution 62cc engine. Other
engine choices will vary the amount of balance weight required.
187. Thread a ball end eight turns on the 8
/
inch (225mm)
7
8
throttle pushrod.
188. Slide a silicone retainer on the clevis, then thread the clevis
on the pushrod.
189. Mount the throttle servo in the fuselage with the output facing
the front of the fuselage. Make sure to prepare the servo and
mounting holes as outlined previously.
190. Slide the pushrod into position. Attach the ball end to the
carburetor arm using an M3 x 10 socket head cap screw, M3
locknut and M3 washer. Use a 2.5mm hex wrench and pliers
to tighten the hardware.
Î It may be necessary to enlarge the hole in
the carburetor arm using a 1/8-inch (3mm) drill bit.
Use caution when drilling the carburetor arm/
EN
191. Attach the clevis to the throttle servo arm following the
instructions provided with the engine. Check the operation
of the throttle using the radio system. Make any adjustments
necessary so the carburetor opens and closes fully without
binding the servo.
192. Place the receiver and ignition batteries in the fuselage as far
forward as possible. Make sure to secure the batteries and
protect them with foam so they don't move during flight.
193. Remove the covering from the fuselage side using a hobby
knife and #11 blade. Mount the switch using the hardware
provided with the switch.
Î The radio and ignition switch can also be installed in the
cockpit floor. Some event regulations may require the switches
be located so they can be accessed in an emergency.
Optional Choke Linkage
Thread a ball end on a piece of threaded rod. Attach the ball end to
the choke lever of the carburetor.
Drill a 1/8-inch (3mm) hole in the instrument panel for the choke
linkage. Bend the end of the link so it can be operated from inside
the fuselage.
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