• 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

Air
DA20-C1 AMM
Page 208
23 Jun 2004 75-00-00 Doc # DA201-C1
Rev. 10
Detail Steps/Work Items Key Items
(9) Put these items through the aft baffle.
− Throttle control cable
− Mixture control cable
Remove the blanks and install:
− The fuel pressure hose to the fuel
manifold valve. Tighten the connection.
− The fuel drain pipe to the manifold.
Tighten the connection.
− The oil breather hose to the oil
separator. Attach the worm drive clamp
and tighten.
Torque to 15.2 - 16.9 Nm (135 - 150 in lbs)
Torque to 5.6 - 7.3 Nm (50 - 65 in lbs)
(10) Put the ignition cables through the rear
baffle.
(11) Install the two cable shields to the aft baffle.
Tighten the nuts and bolts.
(12) Install the throttle control cable to the support
bracket at the top of the plenum assembly:
− Position the throttle control cable
correctly in the support bracket.
− Install the two bolts washers and nuts.
− Tighten the two nuts.
(13) Install the eye end of the throttle control
cable onto the throttle lever:
− Put one washer under the head of the
bolt.
− Put the bolt through the eye end of the
control cable.
− Put one washer onto the bolt on the
other side of the eye end.
− Attach the bolt to the throttle lever.
− Put one washer on the bolt.
− Attach the nut to the bolt.
Tighten the assembly.
Refer to Chapter 76.
(14) For aircraft with a standard fuel pump:
Install the mixture control cable support
bracket to the apron:
− Attach the screw and washer. Tighten
the screw.
DA20-C1 AMM
Air
Doc # DA201-C1
Rev. 10 75-00-00 Page 209
23 Jun 2004
Detail Steps/Work Items Key Items
For aircraft with an altitude compensating
fuel pump:
Install the mixture control cable into the
support bracket at the front of the engine.
− Insert the end of the mixture control
cable through the hole in the apron.
− Slide the notch in the control cable into
the slot of the support bracket.
− Install the keeper onto the cable and
slide it into place.
− Install the screws, washers and nuts to
secure the keeper to the bracket.
− Tighten the assembly.
(15) Install the mixture control cable to the
mixture control lever on the fuel pump:
For aircraft with a standard fuel pump:
− Put the bolt through the lever from the
engine side.
− Put one washer onto the bolt.
− Put the control cable wire through the
hole in the bolt.
− Put one washer onto the bolt.
− Attach the nut to the bolt.
For aircraft with an altitude compensating
fuel pump:
− Install the jam nut and rod end onto the
mixture control cable.
− Put the thin washer under the head of
the bolt.
− Insert the bolt into the mixture lever from
the inboard side.
− Put one washer onto the bolt on the
other side of the lever.
− Put the rod end onto the bolt.
− Put one washer onto the bolt.
− Put the large diameter washer onto the
bolt.
− Attach the nut to the bolt.
Tighten the assembly.
Refer to Chapter 76.
Air
DA20-C1 AMM
Page 210
23 Jun 2004 75-00-00 Doc # DA201-C1
Rev. 10
(16) For aircraft with a standard fuel pump:
Put the mixture control cable in the support
bracket at the top of the engine. Attach the
cable to the bracket with a ty-wrap.
For aircraft with an altitude compensating
fuel pump:
Secure the mixture control cable to the #2
cylinder induction tube using a cable tie.
(17) Do a throttle control freedom and range of
movement check.
Refer to Chapter 76.
(18) Do a mixture control freedom and range of
movement check.
Refer to Chapter 76.
(18a) Bleed the engine fuel system. Refer to Chapter 73.
(19) Install the ignition leads to the spark plugs.
Tighten the “B” nuts.
Torque 12.4-13.5 Nm (110-120 in lbs)
(20) Install the top and bottom engine cowlings. Refer to Chapter 71-10
(21) Do an engine operational test. − For the engine run procedures, refer to
the DA20-C1 Flight Manual.
− For the operational test refer to TCM
Maintenance Manual Chapter 23
− Refer to the operational checklist in this
manual Chapter 05-20 for difference in
static RPM settings.
(22) Examine the engine for oil/fuel leaks.
DA20-C1 AMM
Engine Controls
Doc # DA201-C1
Rev. 0 76-TITLE Page 1
 
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(92)