曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

20 Sep 2007
3. Remove/Install the Front Exhaust Pipe
WARNING: MAKE SURE THAT THE EXHAUST SYSTEM IS COOL BEFORE YOU
TOUCH IT. THE EXHAUST SYSTEM CAN BE VERY HOT, THIS CAN
CAUSE INJURY TO PERSONS.
A. Remove the Front Exhaust Pipe
Detail Steps/Work Items Key Items/References
% WARNING: MAKE SURE THE ENGINE IS SAFE BEFORE YOU DO ANY WORK
ON THE EXHAUST SYSTEM. IF THE ENGINE STARTS THE
PROPELLER CAN CAUSE INJURY OR DEATH. (1)
(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 3 springs at the spherical coupling. Refer to Figure 1.
% (4) Release the bolt attaching the front bracket. Not installed if MÄM 40-138 conducted.
(5) Release the 3 nuts and washers from the flange
at the turbo-charger.
(6) Remove the front exhaust pipe from the airplane.
AIRCRAFT
Exhaust DA 40 Series
AMM
Page 204
20 Sep 2007 78-01-00 Doc # 6.02.01
Rev. 5
B. Install the Front Exhaust Pipe
Detail Steps/Work Items Key Items/References
% WARNING: MAKE SURE THE ENGINE IS SAFE BEFORE YOU DO ANY WORK
ON THE EXHAUST SYSTEM. IF THE ENGINE STARTS THE
PROPELLER CAN CAUSE INJURY OR DEATH.
(1) Put the front exhaust pipe in position on the
turbo-charger.
Refer to Figure 1. Apply anti-seize
compound (Loctite 8151 or equivalent)
to the conical seat.
(2) Install the 3 nuts and washers that attach the
flange to the turbo-charger.
% (3) Install the bolt for the front bracket. Not installed if MÄM 40-138 conducted.
(4) Engage the rear pipe part of the spherical
coupling with the ball of the front part.
Apply anti-seize compound (Loctite
8151 or equivalent) to the spherical
coupling.
(5) Install the 3 springs at the spherical coupling.
(6) Do a ground run-up. Look for leaks at the
spherical joint and turbo-charger joint.
Refer to Section 71-01.
(7) Install the engine cowlings. Refer to Section 71-11.
AIRCRAFT
DA 40 Series
AMM
Oil System
Doc # 6.02.01
Rev. 5 79-TITLE Page 1
20 Sep 2007
CHAPTER 79
OIL SYSTEM
AIRCRAFT
Oil System DA 40 Series
AMM
Page 2
20 Sep 2007 79-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Oil System
Doc # 6.02.01
Rev. 5 79-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 79
OIL SYSTEM
Section 79-00
Oil System - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description/Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Oil Cooler . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
Section 79-01
Oil System - TAE 125 Diesel Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Engine Oil System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Oil Radiator . . . . . . . . . . . . . . . . . . . . . . . . . . 201
AIRCRAFT
Oil System DA 40 Series
AMM
Page 2
20 Sep 2007 79-CONTENTS Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Oil System
Doc # 6.02.01
Rev. 5 79-00-00 Page 1
20 Sep 2007
CHAPTER 79
OIL SYSTEM
Section 79-00
Oil System - Lycoming Engine
1. General
The IO-360-M1A installed in the DA 40 has the usual wet-sump oil system. The oil system has an oil
cooler. The oil cooler attaches to brackets on the engine-mounting-frame. The oil system also has a
temperature indicator. The indicator is part of the integrated-engine-instrument-display. For more data
about the indication system refer to Section 77-40.
For more data on the oil system refer to the Lycoming Maintenance Manual.
2. Description/Operation
Figure 1 shows the schematic diagram for the oil system.
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40系列AMM 3(96)