Airplane Description DA 62 AFM
Major Instruments and Controls
1 Electric master switch 17 Circuit breakers*
2 Avionic master switch 18 Standby attitude module
3 Engine master switches 19 Rudder pedal switches
4 Start button 20 USB charging ports
5 Pitot-/Static-/Stall warning heat
switch
21 Emergency compass
6 Alternator switches 22 ELT control unit
7 ECU test buttons 23 Primary flight display (PFD)
8 VOTER switches 24 Audio amplifier/intercom/marker
beacon receiver
9 Rotary buttons for instrument
lighting and flood light
25 Multi function display (MFD)
10 Light switches 26 De-Ice control panel
11 - 27 Autopilot control unit (part of MFD)
12 Flap selector switch 28 Alt air lever
13 Landing gear switch 29 Landing gear emergency
extension lever
14 Alternate static valve 30 Oxygen pressure indicator
15 Microphone socket 31 -
16 Ventilation nozzles 32 Fuel pump switches
*) Designations and abbreviations used to identify the circuit breakers are explained in
Section 1.5 - DEFINITIONS AND ABBREVIATIONS.
NOTE
The figure above shows the typical DA 62 installation position
for the equipment. The actual installation may vary due to
the approved equipment version.
Page 7 - 12 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
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