Diamond Aircraft DA 40 NG, Airplane Flight Manual

Page: 271 / 326

DA 40 NG AFM
Airplane
Description
Doc. # 6.01.15-E Rev. 3 01-Jul-2014 Page 7 - 11
Major Instruments and Controls
1 Electric Master key switch 21 ELT control unit
2 Fuel Transfer switch 22 Accessory power socket
3 Pitot Heat switch
4 Avionics Master switch 24 Primary Flight Display (PFD)
5 Essential Bus switch 25 Audio amplifier / Intercom /
Marker beacon receiver
6 Fuel pumps switch 26 Multi Function Display (MFD)
7 ECU Test button 27 Airspeed Indicator
8 ECU Voter switch 28 Attitude Gyro (artificial horizon)
9 Engine Master switch**
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29 Altimeter
10 Rotary buttons for instrument
lighting and flood light
30 Vertical Speed Indicator (VSI)
11 Light switches 31 Directional Gyro
12 Emergency switch**
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32 Turn & Bank indicator
13 Circuit breakers
*
33 Intercom
14 Flap selector switch 34 Annunciator panel
15 Alternate static valve 35 Main Engine Display (MED)
16 Ventilation nozzles 36 Secondary Engine Display (SED)
17 Backup airspeed indicator 37 Chronometer with OAT Indicator
18 Backup artificial horizon 38 COM/NAV
19 Backup altimeter 39 Transponder
20 Emergency compass
*) Designations and abbreviations used to identify the circuit breakers are explained in
Section 1.5 - DEFINITIONS AND ABBREVIATIONS of the AFM.
**) The Emergency switch and optionally the Engine Master switch are guarded. Lift the
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guard prior to actuate the toggle. After switching, lower the Engine Master switch guard
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with the toggle in the desired position. Do not lower the Emergency switch guard with
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the toggle in ON position.
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