• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2010-06-29 14:11来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(3) Disconnect the two electrical connectors
from the rear of the (EGT) indicator.
(4) Remove the two nuts and washers from the
(EGT) indicator attachment bracket. At the
rear of the instrument panel.
Hold the (EGT) indicator while you remove
the attachment bracket.
(5) Remove the (EGT) indicator from the front
of the instrument panel.
B. Install the (EGT) Indicator
Detail Steps/Work Items Key Items
(1) Position the (EGT) indicator into the
instrument panel at the front.
(2) Install the (EGT) indicator attachment
bracket at the rear of the instrument panel:
− Put the bracket onto the two studs.
− Attach the two washers and the two nuts
to the studs.
− Tighten the two nuts.
Make sure the (EGT) indicator is
positioned correctly before you attach the
bracket.
(3) Connect the two electrical connectors to the
rear of the (EGT) indicator.
(4) Install the instrument panel cover. Refer to Chapter 25-10
(5) Do an engine run up test. Look specially for
correct (EGT) indications.
Refer to the Teledyne Continental Motors
Maintenance Manual for (EGT) data. For
the engine run procedures refer to the
DA20-C1 Flight Manual.
DA20-C1 AMM
Engine Indicating
Doc # DA 201-C1
Rev. 9 77-00-00 Page 207
29 Apr 2004
7. Remove/Install The Cylinder Head Temperature Indicator
A. Remove The Cylinder Head Temperature Indicator
Detail Steps/Work Items Key Items
(1) Disconnect the airplane battery. Refer to Chapter 24-31
(2) Remove the instrument panel cover. Refer to Chapter 25-10
(3) Disconnect the two electrical connectors
from the rear of the (CHT) indicator.
(4) Remove the locking ring from the (CHT)
indicator. At the rear of the instrument
panel.
Hold the (CHT) indicator while you remove
the locking ring.
(5) Remove the (CHT) indicator from the front of
the instrument panel.
B. Install The Cylinder Head Temperature Indicator
Detail Steps/Work Items Key Items
(1) Position the (CHT) indicator into the
instrument panel at the front.
(2) Install the (CHT) indicator to the rear of the
instrument panel:
− Put the locking ring onto the (CHT)
indicator.
− Turn the locking ring clockwise until the
(CHT) indicator is tight in position.
Make sure the (CHT) indicator is
positioned correctly before you attach the
locking ring.
(3) Connect the two electrical connectors to the
rear of the (CHT) indicator.
(4) Install the instrument panel cover. Refer to Chapter 25-10
(5) Do an engine run up test. Look specially for
correct (CHT) indications.
Refer to the Teledyne Continental Motors
Maintenance Manual for (CHT) data. For
the engine run procedures refer to the
DA20-C1 Flight Manual.
Engine Indicating
DA20-C1 AMM
Page 208
19 Dec 1997 77-00-00 Doc # DA 201-C1
Rev. 0
Intentionally left blank
DA20-C1 AMM
Exhaust
Doc # DA201-C1
Rev. 0 78-TITLE Page 1
19 Dec 1997
CHAPTER 78
EXHAUST
Exhaust
DA20-C1 AMM
Page 2
19 Dec 1997 78-TITLE Doc # DA201-C1
Rev. 0
Intentionally left blank
DA20-C1 AMM
Exhaust
Doc # DA201-C1
Rev. 0 78-CONTENTS Page 1
19 Dec 1997
TABLE OF CONTENTS
CHAPTER 78-00 EXHAUST.....................................................................................................................1
1. General .............................................................................................................................1
2. Description ........................................................................................................................1
TROUBLE SHOOTING...............................................................................................................101
1. General .........................................................................................................................101
MAINTENANCE PRACTICES ....................................................................................................201
1. General .........................................................................................................................201
2. Remove/Install The Exhaust.........................................................................................201
Exhaust
DA20-C1 AMM
Page 2
19 Dec 1997 78-CONTENTS Doc # DA201-C1
Rev. 0
Intentionally left blank
DA20-C1 AMM
Exhaust
Doc # DA201-C1
Rev. 9 78-00-00 Page 1
29 Apr 2004
CHAPTER 78-00
EXHAUST
1. General
This Chapter tells you about the engine exhaust system. It also tells you about the muffler and the
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:钻石20系列AMM 2(106)