TOMARK Viper SD-4 RTC - Page 118

TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 31 Indication & Recording Systems
Page 118 Issue: 11.AUG 2016
The left panel contains
 flight instruments (primary barometric airspeed indicator and
altimeter and secondary 10” Dynon Skyview EFIS),
 a rotary ignition control switch,
 an engine start button,
 master switch,
 generator switch,
 instrument switch,
 EMS alarm light,
 a battery charging warning light,
 electric fuel pump indicator light,
 engine starter indicator and
 a fresh air nozzle.
The central panel contains
 communication instruments (radio and transponder,
 GPS AvMap EKPV), and
 section switches/circuit breakers.
The magnetic compass is located above the panel.
The right panel contains
 a 10” Dynon Skyview for the monitoring of the engine parameters,
 a carburettor heat control button,
 a cylinder heat button,
 a cockpit heating control button,
 an on-board electric socket and
 an air nozzle.
The vertical part of the control panel contains sockets to connect
headset cable plugs.
The horizontal part of the control panel contains
 the 3 position FUEL LANE selector,
 the flaps control,
 the hydraulic brakes control lever,
 the engine throttle lever and
 the choke control button.