曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

down. If there was too much bounce in
the DEFROST position, then move the
flap up.
(8) Set the distribution control lever in the cockpit
to DEFROST.
There should be 'bounce' of about
3 mm (1/8 in) between the back of the
lever and the cockpit stop.
Note: If you cannot get bounce at both ends of the range of movement, adjust the
cable to give bounce at the DEFROST end.
(9) Do items 8 and 9 as necessary to get the correct
adjustment.
(10) Install the top cover plate to the engine control
assembly.
Refer to Section 31-11.
AIRCRAFT
DA 40 Series
AMM
Auto Flight
Doc # 6.02.01
Rev. 5 22-TITLE Page 1
20 Sep 2007
CHAPTER 22
AUTO FLIGHT
AIRCRAFT
Auto Flight DA 40 Series
AMM
Page 2
20 Sep 2007 22-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Auto Flight
Doc # 6.02.01
Rev. 5 22-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 22
AUTO FLIGHT
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 22-10
Autopilot
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Flight Control Computer . . . . . . . . . . . . . . . . . 201
3. Remove/Install the Roll Servo . . . . . . . . . . . . . . . . . . . . . . . . . . . . 203
4. Remove/Install the Roll Servo Clutch . . . . . . . . . . . . . . . . . . . . . . 204
5. Remove/Install the Pitch Servo . . . . . . . . . . . . . . . . . . . . . . . . . . . 206
6. Remove/Install the Pitch Servo Clutch . . . . . . . . . . . . . . . . . . . . . 207
7. Remove/Install the Pitch Trim Servo . . . . . . . . . . . . . . . . . . . . . . . 209
8. Remove/Install the Pitch Trim Servo Clutch . . . . . . . . . . . . . . . . . 210
9. Adjust the Bridle Cable Tension . . . . . . . . . . . . . . . . . . . . . . . . . . 211
10. Adjust the Clutch Torques . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 212
11. Mechanical Check of the Autopilot System . . . . . . . . . . . . . . . . . . 213
AIRCRAFT
Auto Flight DA 40 Series
AMM
Page 2
20 Sep 2007 22-CONTENTS Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Auto Flight
Doc # 6.02.01
Rev. 5 22-00-00 Page 1
20 Sep 2007
CHAPTER 22
AUTO FLIGHT
1. General
This Chapter tells you about the components which enable the automatic control of the flight of the
airplane.
Refer to these Sections for data about the systems:
Section 22-10 Autopilot.
AIRCRAFT
Auto Flight DA 40 Series
AMM
Page 2
20 Sep 2007 22-00-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Auto Flight
Doc # 6.02.01
Rev. 5 22-10-00 Page 1
20 Sep 2007
Section 22-10
Autopilot
1. General
This Section tells you about the autopilot system that can be installed in the DA 40.
2. Description
The KAP 140 autopilot system is a digital flight control system that provides roll, pitch, and pitch trim
steering with optional altitude preselect. The system has the following components (refer to Fig. 1):
) KC 140 flight control computer (FCC).
) KCM 100 configuration module.
% ) Turn and bank coordinator with autopilot pick-off.
) KCS 55A gyro compass system. Refer to Section 34-28 for details about the gyro compass
system.
% ) Directional Gyro
) KS 271C roll servo.
) KS 270C pitch servo.
) KS 272C pitch trim servo.
) KM 275 and KM 277 servo mounts.
Heading input must be supplied for the KAP 140 autopilot by the KCS 55A gyro compass system.
% Refer to Section 34-28 for details about the gyro compass system. Alternatively a Directional Gyro
% connected to the suction system (DA 40 D only) may be installed.
% When the altitude preselect/vertical speed system option is installed, the airplane may be equipped
with the KEA 130A encoding altimeter.
The KAP 140 roll axis features includes wing leveler, heading select, and VOR/LOC intercept and
tracking. The KAP 140 can also be coupled to the GPS and the RNAV receivers. Roll rate information
is derived from the turn coordinator.
Pitch axis features include vertical speed, glideslope and altitude hold along with the optional altitude
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40系列AMM 1(83)