% Figure 6: DA4-3120-00-00/1
% Figure 7: DA4-3121-00-00
%
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AMM
% Figure 9: DA4-3123-00-00 %
% Figure 10: DA4-3123-00-00/1 %
% Figure 11: DA4-3124-00-00 %
Page 6 Doc # 6.02.01 09 Jan 2003 Rev. 4
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Indicating Systems
AMM
% Figure 12: DA4-3126-00-00 %
% Figure 13: DA4-3129-00-00 %
% Figure 14: DA4-3130-00-00 %
Doc # 6.02.01 Page 7
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AMM
% Figure 15: DA4-3131-00-00 %
% Figure 16: DA4-3132-00-00 %
% Figure 17: DA4-3133-00-00 %
Page 8 Doc # 6.02.01 09 Jan 2003 Rev. 4
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AMM
% Figure 18: DA4-3134-00-00 %
% Figure 19: DA4-3135-00-00 %
% Figure 20: DA4-3137-00-00 %
Doc # 6.02.01 Page 9
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Indicating Systems AMM
AIRCRAFT
% % % % % % % % % % % % % Figure 21: DA4-3138-00-00 % % % %
% % % % % % % % % % % % % % % % % Figure 22: DA4-3139-00-00 % % % % % % %
Page 10 Doc # 6.02.01 09 Jan 2003 Rev. 4
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AMM
% Figure 23: DA4-3140-00-00 % % % % % % % % % % % % % % % %
% % Figure 24: DA4-3141-00-00
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AMM
%
%
%
%
%
DA 40 Series
LEGEND
1 Electrical switches, ignition switch 16 Turn & bank indicator 31 Microphone socket
2 Circuit breakers 17 Slaving meter 32 Ventilation nozzles
3 Emergency switch 18 ADF indicator 33 Alternate static valve
4 Instrument lighting and flood light rotary buttons 19 Course deviation indicator (CDI) 34 ELT operating unit (RCPI)
5 Flap selector switch 20 Audio amplifier / intercom / marker beacon receiver 35 Directional Gyro
6 OAT indicator 21 GPS Annunciation Control Unit 36 Strike Finder Display
7 Fuel quantity indicator 22 GPS 37 Clear WX 500 Button
8 Engine instruments 23 Radio / VOR, No. 1 38 Ground COM 2 switch
9 Lights (Annunciator Panel) 24 Remote DME switch 39 AUX FUEL QTY switch
10 Chronometer 25 Radio / VOR, No. 2
11 Altimeter 26 DME
12 Vertical speed indicator 27 ADF receiver
13 Attitude gyro (horizon) 28 Autopilot control unit
14 Horizontal situation indicator (HSI) 29 Transponder
15 Airspeed indicator 30 Stall warning horn
Page 12 Doc # 6.02.01 09 Jan 2003 Rev. 4
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AMM
2. Description
A. Instrument Panel
% The Figures in Paragraph 1 show the instrument panels which are available for the DA 40 with the
% Lycoming engine installed. The airplane has an aluminum alloy instrument panel. The panel has cut-outs for instruments and switches. A large cut-out in the middle of the panel has the avionic equipment. Brackets between the shelf and the avionic equipment rack make the installation rigid.
The bottom of the panel bends up at 87o to make a shelf. The shelf has mountings for electrical equipment such as relays and multi-pin connectors. Each side of the shelf has a row of ground terminals. Large cut-out areas in the shelf allow cooling air to move past the instruments and out through holes in the instrument panel cover.
Doc # 6.02.01 Page 13
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AMM
AIRCRAFT
Heat and Brake
Throttle Friction Adjuster
Top Cover Plate
Bottom Cover Plate
Mixture
Floor
Panel
Parking
Brake
Throttle
Distributor Valve Control Cable
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