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(2)  Connect the electrical cables to the switch.  Refer to Chapter 92 for the Wiring Diagrams. 
(3)  Install the instrument panel cover.  Refer to Section 25-10. 
(4)  Connect the battery.  Refer to Section 24-31. Connect the positive cable first. 
(5)  Install the top engine cowling.  Refer to Section 71-10. 
(6)  Do a functional test of the switch: S Set the ALT/BAT switch to ON. S Set the switch that you have installed to ON. S Set the switch that you have installed to OFF. S Set the ALT/BAT switch to OFF.  The system must operate correctly. The system must switch off. 

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Electrical Power
AMM

% Section 24-61 % DC Electrical Load Distribution - TAE 125 Diesel Engine % 1. General
% This Section tells you about the system which supplies DC electrical power for other systems. The % DC electrical load distribution system has these components:
%) Main bus. %) Relay junction box bus. %) ECU bus. %) Avionic bus. %) Essential bus. %) Essential avionic bus. %) Hot battery bus. %) Battery relay. %) Power relay. %) Avionics master relay. %) Essential avionics relay. %) Essential tie relay. %) Switches. %) Circuit-breakers. %) Fuses.
% Figure 1 shows the electrical system bus structure diagram of the electrical distribution system. Figure % 2 shows the layout of the switches and circuit-breakers in the instrument panel.
% This Section gives you the trouble-shooting and maintenance practices for the electrical distribution % system. Refer to Section 24-01 for the full system description and operation.
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%
%

INSTRUMENT PANEL ENGINE COMPARTMENT

Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
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DA 40 Series
Electrical Power
AMM AIRCRAFT
% 
CAUTION 
WARNING WHITE WIRE 
%  S 4 5 6 U C T I O N  START DOORS LOW VOLTS ENGINE FUEL TRANS GLOW ECU A ECU B TRIM FAIL LOW FUEL ALTERNATOR PITOT  ISO M U T E OFF VOLUME VOLUMESQUELCH SQUELCH PILOT CO-PILOT PWR/XMT ALL 
INSTRUMENT  GARMIN  RNG GNS 430 

C
COS
WPT
KHPN
C
ON
PWR
136.975 RPM
PUSHVOL
KHPN
SQ
%

0
D MENU
118.000 DIS
9
1
V
4.85
VLOC n
VOL PUSH
m CLR ENT
160
ID
TKE
V 117.95
OFF
40
NAV
000o
8
2
AIRSPEED 108.00
DEFAULT
NAV GPS
ALT
TO
COM
Oil Pressure Cooling TempGSFLOOD 140 VLOC
GPS
VLOC
TERM
mb IN.Hg
165 k
CALIBRATED
TOON 28.7 t
PUSH
PUSH Oil Temp Gearbox Temp
C/V GPS NAV
CRSR
20,000 FEET
120 KNOTS 7360
CDI OBS MSG FPL PROC
%
100
OFF
ECU
80 64
5
OBSTO LOAD
SWAP ECU
D.C.
0
%
ELEC.
TEST
24
10 Water Level
9
1
15
5
L Fuel Quantity R Fuel Quantity
UP VERTICAL SPEED
8
2
100 FEET PER MINUTE
ALT
L Fuel Temp (oC) R Fuel Temp (oC)
20
33
IN.Hg
mb
0
CALIBRATED TO
15
28.7O.A.T. VOLTS
20
20,000 FEET
TURN COORDINATOR
Ampere Volt
73
DOWNL
R
5
%

15 64
UT LT
2 MIN.
Fuel Flow
10
5
6
FT ET NO PITCH PUSH
INFORMATION
SELECT CONTROL
DAVTRON
%
　
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