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for the related data:
) 31-10 The instrument and control panels for the DA 40 with the Lycoming engine installed.
) 31-11 The instrument and control panels for the DA 40 with the TAE 125 Diesel engine
installed.
) 31-20 Independent instrument s for all DA 40 variants.
) 31-50 The central warning system for the DA 40 with the Lycoming engine installed.
) 31-51 The central warning system for the DA 40 with the TAE 125 Diesel engine installed.
The DA 40 has these indicating systems:
) An instrument panel. The instrument panel is made in one piece with a shelf. The shelf goes
between the panel and the firewall.
) A control panel in the center console. This panel has the engine controls, fuel controls, cabin
heat control levers, parking brake and trim. It has a forward part and an aft part.
) Independent instruments. The airplane has an integrated electronic indicating system which
covers the engine instruments and fuel quantities. The airplane also has a digital chronometer
(optional), an optional engine operated hours meter and an outside air temperature (OAT)
indicator.
) Warning lights (red), caution lights (amber), and status lights (white).
This Section does not tell you about the indicators that belong to systems. See the related system for
data. For example, see Section 27-31 for data about the trim indicator.
Note: Equipment which is certified for installation in the DA 40 is listed in Section 6.5 of
the Airplane Flight Manual. Such equipment may be installed in accordance with
the Airplane Maintenance Manual.
Any equipment which is not listed in Section 6.5 of the Airplane Flight Manual is
called "Additional Equipment". The installation of Additional Equipment is a
modification which must be handled in accordance with national regulations or a
Service Bulletin.
AIRCRAFT
Indicating Systems DA 40 Series
AMM
Page 2
20 Sep 2007 31-00-00 Doc # 6.02.01
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AIRCRAFT
DA 40 Series
AMM
Indicating Systems
Doc # 6.02.01
Rev. 5 31-10-00 Page 1
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Section 31-10
Instrument and Control Panels - Lycoming Engine
1. General
The DA 40 with the Lycoming engine installed has these instrument and control panels:
) An instrument panel. The instrument panel is made in one piece with a shelf. The shelf goes
between the panel and the firewall.
) 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 controls and fuel shut-off valve.
See the related Chapter or Section for data about the controls. For example, see Section 76-00 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:
% ) DA4-3110-00-00 (Basic certification, VFR, Figure 1)
% ) DA4-3135-00-00 (OÄM 40-121, 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 31-10-00 Doc # 6.02.01
Rev. 5
Figure 1: DA4-3110-00-00
% Figure 2: DA4-3135-00-00
AIRCRAFT
DA 40 Series
AMM
Indicating Systems
Doc # 6.02.01
Rev. 5 31-10-00 Page 3
20 Sep 2007
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
AIRCRAFT
Indicating Systems DA 40 Series
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钻石40系列AMM 2(40)
