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时间:2011-05-24 14:56来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

%) 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 instrument panel assemblies are available:
%) D4D-3110-00-00 (Figure 1)
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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 

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Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
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% 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.
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Top Bracket

% % Figure 2: Engine Control Assembly Structure %
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% 3. Center Console Description
% The engine control assembly holds the parking brake and heating controls. It also holds the engine % power lever.
 
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