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AIRCRAFT
Turbines DA 40 Series
AMM
Page 2
20 Sep 2007 81-CONTENTS Doc # 6.02.01
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AIRCRAFT
DA 40 Series
AMM
Turbines
Doc # 6.02.01
Rev. 5 81-00-00 Page 1
20 Sep 2007
CHAPTER 81
TURBINES
1. General
This Chapter tells you about the turbo-charging system of the TAE 125 Diesel engine.
2. Description
The air intake system has an air filter located on the right of the engine compartment, just forward of
the firewall. The filter attaches to the bottom of an alternate air valve. The alternate air valve also has
an inlet direct from the engine compartment. A flap in the valve can select either filtered air or warm,
unfiltered air. Refer to Section 71-61 for more data on the air filter and alternate air valve.
The outlet from the alternate air valve connects to the turbo-charger. The turbo-charger compresses
the air. This makes the air hot. The outlet from the turbo-charger connects to an intercooler.
The intercooler is located on the right of the engine. It attaches to the engine mounting frame.
% The outlet from the intercooler connects to the engine inlet manifold.
AIRCRAFT
Turbines DA 40 Series
AMM
Page 2
20 Sep 2007 81-00-00 Doc # 6.02.01
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AIRCRAFT
DA 40 Series
AMM
Turbines
Doc # 6.02.01
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20 Sep 2007
Maintenance Practices
1. General
This Section tells you how to remove/install the intercooler.
CAUTION: YOU CANNOT DO MAINTENANCE ON THE TURBO-CHARGER.
CAUTION: DO NOT TRY TO ADJUST THE WASTE GATE CONTROL PUSH ROD.
ANY ADJUSTMENT WILL AFFECT THE CHARACTERISTICS OF THE
ELECTRONIC CONTROL SYSTEM.
Refer to Section 71-61 for maintenance data on the air filter and alternate air valve.
2. Remove/Install the Intercooler
A. Remove the Intercooler
Detail Steps/Work Items Key Items/References
WARNING: YOU MUST MAKE SURE THAT THE ENGINE IS SAFE BEFORE YOU
DO WORK ON THE ENGINE. IF THE PROPELLER TURNS IT CAN
CAUSE INJURY TO PERSONS.
(1) Make sure that the engine is safe:
S Set the ELECTRIC MASTER key switch to
OFF.
S Set the ENGINE MASTER switch to OFF.
S Set the power lever to IDLE.
(2) Remove the engine cowlings. Refer to Section 71-11.
% (3) Release the worm-drive clamps that attach the
% hose from the turbo-charger.
At the intercooler.
% (4) Release the worm-drive clamps that attach the
% hose to the engine inlet manifold.
At the intercooler.
%
(5) Remove the bolt, nuts and washers and vibration
% mount attaching the intercooler to the engine
% mounting frame.
% (6) Remove the intercooler from the airplane.
AIRCRAFT
Turbines DA 40 Series
AMM
Page 202
20 Sep 2007 81-00-00 Doc # 6.02.01
Rev. 5
Engine Air Intake Manifold
Intercooler
Intercooler Bottom Attachments
Intercooler Top Attachment
Turbo-Charger
Wiggins Clamp
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
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%
% Figure 1: Intercooler Installation
AIRCRAFT
DA 40 Series
AMM
Turbines
Doc # 6.02.01
Rev. 5 81-00-00 Page 203
20 Sep 2007
B. Install the Intercooler
Detail Steps/Work Items Key Items/References
WARNING: YOU MUST MAKE SURE THAT THE ENGINE IS SAFE BEFORE YOU
DO WORK ON THE ENGINE. IF THE PROPELLER TURNS IT CAN
CAUSE INJURY TO PERSONS.
(1) Make sure that the engine is safe:
S Set the ELECTRIC MASTER key switch to
OFF.
S Set the ENGINE MASTER switch to OFF.
S Set the power lever to IDLE.
(2) Put the intercooler in position on the engine
mount.
S Move the inlet and outlet pipes into position in
the related flexible hoses.
Refer to Figure 1.
% (3) Install the attaching bolts, washers, nuts and
% vibration mount.
(4) Tighten the worm-drive clamps that attach the
hose from the turbo-charger.
At the intercooler.
(5) Tighten the worm-drive clamps that attach the
hose to the engine inlet manifold.
At the intercooler.
% (6) Install the engine cowlings. Refer to Section 71-11.
% (7) Do an engine run-up. Refer to Section 71-01.
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Turbines DA 40 Series
AMM
Page 204
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AIRCRAFT
DA 40 Series
AMM
Wiring Diagrams
Doc # 6.02.01
Rev. 5 92-TITLE Page 1
20 Sep 2007
CHAPTER 92
　
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本文鏈接地址：鉆石40系列AMM 3(106)