2.
Description............................................1
3.
Operation.............................................3
Trouble-Shooting
1. General ............................................101
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Engine Driven Fuel Pump Drain ..........201
3.
Remove/Install the Fuel Flow Divider Drain.................202
4.
Remove/Install the Induction Manifold Drain ................203
% Section 71-71 % Engine Drains - TAE 125 Diesel Engine % 1. General ..............................................1
Page 8 Doc # 6.02.01 09 Jan 2003 Rev. 4
71-CONTENTS
Power Plant
AMM
CHAPTER 71
POWER PLANT
% Section 71-00
% Power Plant - Lycoming Engine
% 1. General
This Chapter tells you about the power plant installed in the DA 40. It tells you about the components that make the power plant. It also tells you how to remove/install the power plant.
For data on the engine test after installation refer to the Lycoming Operator's Manual for the IO-360-M1A engine. Refer to the DA 40 Airplane Flight Manual for engine start/stop procedures.
Refer to these Chapters for data about other engine systems:
) Chapter 72 Refer to the Lycoming Operator's Manual for data on the engine.
) Chapter 73 Engine fuel and control. Refer to the Lycoming Operator's Manual for data on the fuel injection system.
) Chapter 74 Ignition system power supply and installation of high-tension cables. Refer to the Slick Maintenance Manual for more data on the magnetos. Refer to the Lycoming Operator's Manual for data on the spark plugs.
) Chapter 76 Engine controls.
) Chapter 77 Engine indicating.
) Chapter 78 Exhaust system.
) Chapter 79 Oil system components installed in the airframe. Refer to the Lycoming Operator's Manual for data on the engine oil system.
) Chapter 80 Starter system control and installation. Refer to the Lycoming Operator's Manual/Sky-Tec Manual for data on the lightweight geared starter.
Note: Equipment which is certified for installation in the DA 40 is listed in Section 6.5 of the Airplane Flight Manual. Such equipment may be installed in accordance with the Airplane Maintenance Manual.
Any equipment which is not listed in Section 6.5 of the Airplane Flight Manual is called "Additional Equipment". The installation of Additional Equipment is a modification which must be handled in accordance with national regulations or a Service Bulletin.
Doc # 6.02.01 Page 1
Rev. 4 09 Jan 2003
71-00-00
AIRCRAFT AMM
%
%
%
%
%
%
%
Top Cowling
%
%
%
%
%
%
%
%
%
%
%
Electrical Harness
% % % Engine Mounting Frame % % % % % % %
Engine Air Intake
%
%
%
Engine Drains
% % Bottom Cowling %
Oil Cooler Air Intake
% % % % Engine Cooling Air Intake % % Figure 1: Power Plant
Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
71-00-00
Power Plant
AMM