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时间:2011-05-24 15:01来源:蓝天飞行翻译 作者:航空
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

(6)  Connect the small flexible pipe for the manifold pressure sensor.  On the outlet pipe to the engine inlet manifold. 
(7)  Attach the coolant expansion tank to the intercooler with 2 bolts, washers and nuts. 

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DA 40 Series

Detail Steps/Work Items  Key Items/References 
(8)  Only if a new intercooler is installed: S Remove air temperature sensor from old intercooler. S Install air temperature sensor to new intercooler.  Discard seal. Use a new seal. 
(9)  Connect the electrical connections at the manifold temperature sensor.  On the outlet pipe to the engine inlet manifold. 
(10)  Refill coolant in coolant expansion tank.  Refer to Section 75-01. 
(11)  Install the engine cowlings.  Refer to Section 71-11. 
(12)  Do an engine run-up.  Refer to Section 71-01. 

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CHAPTER 92
WIRING DIAGRAMS

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TABLE OF CONTENTS
CHAPTER 92
WIRING DIAGRAMS

1. General ..............................................1

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CHAPTER 92
WIRING DIAGRAMS

1. General
This Chapter contains the wiring diagrams for each system. The wiring diagrams use the ATA % Chapter/Section numbering system. Wiring diagrams that drawing numbers start with DA4- are for the % DA 40 with Lycoming engine and wiring diagrams that drawing numbers that start with D4D- are for % the DA 40 with the Diesel engine and listed at the end of the table.
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Title  Drawing No.  Rev. No.  No. of Sheets 
Autopilot, KAP 140  DA4-9222-10-02  D  1 
Autopilot, KAP 140, Garmin Interface  DA4-9222-10-03  C  1 
PM 1000, KX 125 NAV/COM  DA4-9223-10-01  F  2 
PM 1000, KX 125 NAV/COM, KI 208  DA4-9223-10-02  C  2 
PM 1000, KX 155A NAV/COM  DA4-9223-10-03  B  2 
KMA 28 audio panel  DA4-9223-50-01  E  2 
GMA 340 audio panel  DA4-9223-50-02  C  2 
GMA 340 audio panel, ground COM 2 switch  DA4-9223-50-02/1  - 2 
KMA 28 audio panel, with ANR power  DA4-9223-50-03  - 2 
Electrical system  DA4-9224-30-01  K  2 
Electrical system, ground COM 2  DA4-9224-30-01/1  - 2 
Emergency power package  DA4-9225-60-01  C  1 
Flaps  DA4-9227-50-01  G  1 
Fuel system pump  DA4-9228-20-01  E  1 
Pitot heat, S/N's through 40.039  DA4-9230-30-01  E  1 
Pitot heat, S/N's 40.040 & subsequent  DA4-9230-30-01  F  1 
Hourmeter  DA4-9231-20-02  D  1 
O.A.T.  DA4-9231-20-03  C  1 
Caution & warning (DAI annunciator panel)  DA4-9231-50-01  C  1 
Caution & warning (White Wire ann. panel)  DA4-9231-50-02  D  1 

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本文链接地址:钻石40飞机维护手册 DA 40 SERIES AMM 6(28)