31-11-00
AMM
% % Figure 1: D4D-3110-00-00 %
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
LEGEND
1 Electric Master switch 16 Suction gauge
2 Engine Master switch 17 Attitude gyro (artificial horizon)
3 Electrical switches 18 Altimeter
4 ECU Test button 19 Vertical speed indicator (VSI)
5 ECU Swap switch 20 Annunciator panel
6 Rotary buttons for instrument lighting and flood light 21 Course deviation indicator (CDI)
7 Flap selector switch 22 Intercom
8 Microphone socket 23 COM / NAV / GPS
9 Circuit breakers 24 ELT control unit
10 Accessory power socket 25 Compact Engine Display (CED)
11 Alternate static valve 26 Auxiliary Engine Display (AED)
12 Ventilation nozzles 27 Transponder
13 Chronometer with OAT indicator 28 Stall warning horn
14 Turn & bank indicator 29 Directional gyro
15 Airspeed indicator
%
Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
31-11-00
Indicating Systems
AMM
% 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.
Doc # 6.02.01 Page 3
Rev. 4 09 Jan 2003
31-11-00
AMM
%
%
Top Bracket
% % Figure 2: Engine Control Assembly Structure %
31-11-00
Indicating Systems
AMM
% 3. Center Console Description
% The engine control assembly holds the parking brake and heating controls. It also holds the engine % power lever.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:钻石40飞机维护手册 DA 40 SERIES AMM 3(64)