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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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Electrical Power 
AMM
% 
%
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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