Airplane Description DA 42 AFM
Page 7 - 12 Rev. 8 15-Dec-2017 Doc. No. 7.01.05-E
Major Instruments and Controls
1 Electric Master switch 17 Circuit breakers*
2 Avionic Master switch 18 Backup airspeed indicator
3 Engine Master switches 19 Backup artificial horizon
4 Start switch 20 Backup altimeter
5 Pitot-/Stall Warning Heat switch 21 Emergency compass
6 Alternator switches 22 ELT control unit
7 ECU Test buttons 23 Primary Flight Display (PFD)
8 ECU Swap 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 Emergency switch 27 Autopilot control unit
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 Oxygen control knob
16 Ventilation nozzles
*) Designations and abbreviations used to identify the circuit breakers are explained in
Section 1.5 - DEFINITIONS AND ABBREVIATIONS.
NOTE
The Figure on the previous page shows the typical DA 42
installation position for the equipment. The actual installation
may vary due to the approved equipment version.
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