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panel on the co-pilot's side.
Engage the appropriate bolt in the
groove on the left side of the tray.
(5) Install the screw on the right side of the battery
tray.
(6) Connect the electrical plug on the right side of the
battery tray.
Ensure correct polarity.
(7) Remove the instrument panel cover. Refer to Section 25-10.
(8) Measure the voltage on the back side of the
EMERGENCY switch.
If the voltage is below 42 volts, it is
probable that the wiring is defective.
Repair wiring.
(9) Install the instrument panel cover. Refer to Section 25-10.
AIRCRAFT
DA 40 Series
AMM
Electrical Power
Doc # 6.02.01
Rev. 5 24-32-00 Page 203
20 Sep 2007
% 3. Remove/Install the Batteries in the Emergency Battery Pack (Lithium Manganese Batteries
% installed)
% A. Remove the Batteries in the Emergency Battery Pack (Lithium Manganese Batteries
% installed)
%
% Detail Steps/Work Items Key Items/References
% (1) Remove the instrument panel cover. Refer to Section 25-10 of the AMM.
(2) Disconnect the electrical plug of the battery
% package.
%
% (3) Remove the screw on the left side which holds
% the battery package.
Hold the battery package and the
mounting bracket.
(4) Remove the battery package and the mounting
% bracket clear of the airplane.
%
% CAUTION: THE BATTERIES CANNOT BE RE-CHARGED. DO NOT TRY TO RE%
CHARGE THE BATTERIES. IF YOU TRY TO RE-CHARGE THE
% BATTERIES, THEY CAN EXPLODE OR LEAK.
% CAUTION: DISPOSE OF THE BATTERIES PROPERLY (ASK YOUR BATTERY
% DEALER FOR ADVISE). BATTERIES CONTAIN POISONS WHICH
% HARM THE ENVIRONMENT. DO NOT THROW THE USED BATTERIES
% INTO THE GARBAGE. DO NOT EXPOSE BATTERIES TO FIRE. DO
% NOT DISMANTLE BATTERIES.
AIRCRAFT
Electrical Power DA 40 Series
AMM
Page 204
20 Sep 2007 24-32-00 Doc # 6.02.01
Rev. 5
% B. Install the Batteries in the Emergency Battery Pack (Lithium Manganese Batteries
% installed)
% CAUTION: USE ONLY A NEW BATTERY PACKAGE. REFER TO THE EQUIPMENT
% LIST IN THE AIRPLANE FLIGHT MANUAL, SECTION 6.5, FOR THE
% CORRECT BATTERY PACKAGE PART NUMBER.
% CAUTION: DO NOT SHORT-CIRCUIT THE BATTERY PACKAGE.
%
% Detail Steps/Work Items Key Items/References
% (1) Measure the voltage of the battery pack. On the connector for the electrical plug.
% If the voltage is less than 36 volts, then
% the battery package is used. Use a
% new battery package.
(2) Put the battery package in place behind the
% instrument panel on the co-pilot's side.
%
(3) Put the mounting bracket in place on the left side
% of the battery package.
%
(4) Install the screw on the left side of the battery
% package.
%
% (5) Connect the electrical plug of the battery
% package.
Ensure correct polarity.
% (6) Measure the voltage on the back side of the
% EMERGENCY switch.
If the voltage is below 36 volts, it is
probable that the wiring is defective.
% Repair wiring.
% (7) Install the instrument panel cover. Refer to Section 25-10 of the AMM.
AIRCRAFT
DA 40 Series
AMM
Electrical Power
Doc # 6.02.01
Rev. 5 24-33-00 Page 1
20 Sep 2007
Section 24-33
DC Generation - TAE 125 Diesel Engine
1. General
The DC generation system for the DA 40 with the TAE 125 Diesel engine has these components:
) Alternator.
) Alternator current sensor.
) Alternator fuse.
% ) Voltage regulator (integral with the alternator. If TR-MÄM-40-151 is carried out, an external
% regulator is used).
) Alternator excitation battery.
This Section gives you only the simplified description, trouble-shooting and maintenance practices
for the generating system. Refer to Section 24-01 for the full system description and operation.
AIRCRAFT
Electrical Power DA 40 Series
AMM
Page 2
20 Sep 2007 24-33-00 Doc # 6.02.01
Rev. 5
5A
5A
5A
5A
100A
Alternator
Main Battery
Alternator Excitation Battery
Battery Relay
OFF
ON
START
START
PWR
Power Relay
ECU A
ECU B
MAIN
TIE
ECU ALT
10
25
25
25
30
5
OFF
ON
Key Switch
Engine
Switch
FIREWALL
INSTRUMENT PANEL ENGINE COMPARTMENT
MAIN
BUS
ECU
BUS
RELAY
JUNCTION
BOX
BUS
Circuit-Breaker with Name and Rating
(Name as on the Placard)
Fuse with Rating
LEGEND
Current Sensor
Figure 1: Electrical Generation System Simplified Schematic Diagram
　
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