THRUSH AIRCRAFT, INC – MODEL S2R-R1340
AIRCRAFT MAINTENANCE MANUAL
Effective: 01/01/08
1-7
switch located on the left side of the
cockpit. The rudder controls are
interconnected by springs to the aileron
system so that a wing may be lifted with
the rudder alone.
INSTRUMENTS
The standard instruments are located on
three separate panels: An upper panel, a
left panel, and a right panel. The left panel
contains a clock, oil temperature, hour
meter, fuel pressure, oil pressure and fuel
quantity gauges. The right panel contains
a voltmeter, ammeter, and circuit breakers.
The upper panel contains propeller
tachometer and a standard flight instrument
package.
ELECTRICAL SYSTEM
The standard 24 volts and 50 amp (70 for
dual control version) electrical system
consists of the starting system, the
wiper/washer system, the navigation lights
and the strobe lights. The navigation
lights, strobe lights, landing lights, working
lights and the air conditioner system are
optional. The electrical system obtains
power from a single 24-volt battery and
one alternator. An external power
receptacle is standard equipment and may
be used for connecting a 24-volt ground
power unit to the aircraft for engine starting
or maintenance. The ground start system
utilizes the master relay so that starting is
accomplished by engaging the starter
switch.
AIRCRAFT WEIGHT & BALANCE
Refer to S2R-R1340 Flight Manual for
detailed aircraft weight and balance
information.
