I A P 2 0 2 1 . 0 0 1 - A F M /
I R I S G 1 1 5 E / T U T O R T . 1
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FOR SIMULATION PURPOSES ONLY
Voltmeter / Volt Indicator / LO VOLT
The voltmeter/volt indicator indicates the voltage on the Essential busbar. The
LO VOLT caption on the CWP illuminates when the Essential busbar voltage is
less than 25 ± 0.5 volts.
Ammeter / Amp Indicator
An ammeter/amp indicator shows the flow from the battery or external
supply to the busbars; a negative charge shows battery discharge and a
positive charge shows the generator charging the battery.
GENERAL EQUIPMENT
The aircraft is fitted with conventional dual flying controls consisting of a
control column and rudder pedals at each crew position. The head of the
column is fitted with a press-to-transmit (PTT) switch.
The control surfaces are mass and aerodynamically balanced and comprise
of;
•
Ailerons.
Differential and Frise ailerons extend over the outer third of
each wing trailing edge.
•
Elevators.
Elevators extend over the whole width of the tailplane trailing
edge.
•
Rudder.
A rudder extends the full height of the fin.
Elevator Control
Fore and aft movement of a control column is transmitted to the elevators by
a system of push-pull rods. The left elevator has an adjustable geared trim
tab. Trim control is by a hand-wheel that protrudes through the upper surface
of the centre pedestal aft of the engine controls. An adjacent indicator
shows the amount of trim set.
