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) A control panel in the center console. This panel has a forward cover and an aft cover. The forward
cover has the cabin heat control levers and parking brake lever. The aft cover has the engine
control and emergency fuel valve.
See the related Chapter or Section for data about the controls. For example, see Section 76-01 for
data on the engine controls.
% The instrument and avionic equipment installed in the airplane can be chosen by the customer. The
% following Figures show two examples of instrument panel assemblies:
% ) D4D-3110-00-00 (Basic certification, VFR, Figure 1)
% ) D4D-3118-00-00 (OÄM 40-TBD, IFR, Figure 2)
% Note: The instruments and avionic equipment cannot be installed in any arbitrary
% combination. The airplane manufacturer must be contacted before removing or
% installing equipment, with the exception of replacing a unit by an identical unit.
AIRCRAFT
Indicating Systems DA 40 Series
AMM
Page 2
20 Sep 2007 31-11-00 Doc # 6.02.01
Rev. 5
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% Figure 1: D4D-3110-00-00
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% Figure 2: D4D-3118-00-00
AIRCRAFT
DA 40 Series
AMM
Indicating Systems
Doc # 6.02.01
Rev. 5 31-11-00 Page 3
20 Sep 2007
% LEGEND
% 1 Electric Master switch 22 Intercom
% 2 Engine Master switch 23 COM / NAV / GPS
% 3 Electrical switches 24 ELT control unit
% 4 ECU Test button 25 Compact Engine Display (CED)
% 5 ECU Swap switch 26 Auxiliary Engine Display (AED)
% 6 Rotary buttons for instrument lighting and
% flood light
27 Transponder
% 7 Flap selector switch 28 Stall warning horn
% 8 Microphone socket 29 not used
% 9 Circuit breakers 30 Autopilot control unit
% 10 Accessory power socket 31 Emergency switch
% 11 Alternate static valve 32 Slaving meter
% 12 Ventilation nozzles 33 Horizontal situation indicator (HSI)
% 13 Chronometer with OAT indicator 34 GPS Annunciation Unit
% 14 Turn & bank indicator 35 ADF indicator
% 15 Airspeed indicator 36 COM / NAV / GPS No. 2
% 16 not used 37 DME
% 17 Attitude gyro (artificial horizon) 38 ADF receiver
% 18 Altimeter 39 Remote DME switch
% 19 Vertical speed indicator (VSI) 40 'ECU Backup Unsafe'-light
% 20 Annunciator panel 41 'Clear WX 500'-button
% 21 Course deviation indicator (CDI)
AIRCRAFT
Indicating Systems DA 40 Series
AMM
Page 4
20 Sep 2007 31-11-00 Doc # 6.02.01
Rev. 5
2. Instrument Panel Description
A single piece of aluminum alloy makes the instrument panel. The panel has a vertical face with
instruments and a horizontal ‘shelf’ with electrical components. The shelf goes between the firewall
and the vertical face of the panel.
The left side of the panel has the usual flight instruments and some navigation indicators. This part can
be removed separately. The actual instruments installed depends on customer options. Refer to
Chapter 34 for data on these instruments.
The center part of the panel has the standard-size avionic equipment. It holds the trays for the GPS,
transponder, radios and other optional navigation avionics. Refer to Chapters 23 and 34 for data on
this equipment.
The right side of the panel contains the engine instruments. The engine data shows on two digital
instruments. Refer to Chapter 77 for data on these instruments.
The bottom left of the panel has the switch panel. The ELECTRIC MASTER key switch is a master
switch and starter switch (as in motor vehicles). Setting it to the ON position applies power to the bus
system. Refer to Chapter 24-01 for data on the electrical system.
The far left of the panel has the rheostat switches for lighting control. There is also a digital OAT
indicator and clock that can also show voltage.
The bottom part of the panel has the circuit-breakers. The circuit-breakers are grouped in bus order.
Refer to Section 24-61 for more data about the circuit-breakers and bus system.
The shelf part of the instrument panel holds relays, junction blocks, connectors and ground studs.
The instrument panel has a cover attached by screws.
AIRCRAFT
DA 40 Series
AMM
Indicating Systems
Doc # 6.02.01
Rev. 5 31-11-00 Page 5
20 Sep 2007
Left Side Plate
Right Side Plate
Front Bracket Center Bracket Rear Bracket
Top Bracket
Figure 2: Engine Control Assembly Structure
AIRCRAFT
Indicating Systems DA 40 Series
AMM
Page 6
20 Sep 2007 31-11-00 Doc # 6.02.01
Rev. 5
3. Center Console Description
The engine control assembly holds the parking brake and heating controls. It also holds the engine
　
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