钻石40飞机维护手册 DA 40 SERIES AMM 2(66)

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

(1)  Remove the engine cowlings.  Refer to Section 71-11. 
(2)  Disconnect the battery: S Disconnect the negative cable from the battery. S Disconnect the positive cable from the battery. 
(3)  Remove the cover from the relay junction box. 
(4)  Disconnect the electrical cables from the external power relay. 
(5)  Remove the nut and washers which attach the bus bar to the external power relay. 
(6)  Remove the 2 bolts which attach the external power relay to the relay box. 
(7)  Move the relay clear of the airplane. 

%

Page 202 Doc # 6.02.01 09 Jan 2003 Rev. 4
24-41-00
Electrical Power
AMM

%
%
%
%

%

%
%
%
%

%

%
%
%
%

%

% B. Install the External Power Relay %

Detail Steps/Work Items  Key Items/References 
(1)  Put the relay in position in the relay junction box. 
(2)  Install the 2 attaching bolts. 
(3)  Install the washers and nut that attach the bus bar to the relay. 
(4)  Connect the power and control cables to the external power relay.  Refer to Chapter 92 for the wiring diagrams. 
(5)  Install the cover to the relay box. 
(6)  Connect the positive cable to the battery.  Apply Dow Corning compound (DC4) to the battery terminal and the cable lug. 
(7)  Connect the negative cable to the battery.  Apply Dow Corning compound (DC4) to the battery terminal and the cable lug. 
(8)  Install the engine cowlings.  Refer to Section 71-11. 

%

Doc # 6.02.01 Page 203
Rev. 4 09 Jan 2003

24-41-00
AMM

% Intentionally left blank
24-41-00
Electrical Power
AMM

% Section 24-60 % DC Electrical Load Distribution - Lycoming Engine
1. General
% This Section tells you about the system which supplies DC electrical power for other systems for % airplanes with the Lycoming engine installed. The DC electrical load distribution system has these components: ) Main bus. ) Avionic bus. ) Essential bus (optional). ) Essential avionic bus (only when the electrical system has an essential bus). ) Battery bus. ) Hot bus. ) Battery relay. ) Avionic master relay. ) Essential avionics relay (only when the electrical system has an essential bus). ) Switches. ) Circuit-breakers. Refer to Section 24-30 for the DC generation system.
Doc # 6.02.01 Page 1
Rev. 4 09 Jan 2003

24-60-00
Electrical Power
AMM

AVIONIC

VOLTAGE REGULATOR
MAIN BUS

BUS

Figure 1: DC Electrical Load Distribution without Essential Bus (simplified)
Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
24-60-00
Electrical Power
AMM

2. Description
A. Main Bus and Essential Bus
(1) Electrical System without Essential Bus
The alternator supplies the main bus through the alternator circuit-breaker. The battery supplies the main bus through the battery relay and the battery circuit-breaker. The battery supplies a positive voltage to the coil of the battery relay. The ALT/BAT switch connects the other side of the coil to ground.
The main bus supplies the airplane electrical systems through circuit-breakers.
(2) Electrical System with Essential Bus
The alternator supplies the main bus through the alternator circuit-breaker. The battery supplies the essential bus through the battery relay and the battery circuit-breaker. The battery supplies a positive voltage to the coil of the battery relay. The ALT/BAT switch connects the other side of the coil to ground.
The essential bus supplies the following electrical consumers through circuit-breakers:
) NAV/COM 1.
) Transponder (XPDR).
　
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 2(66)