canadair
chauenQer
OPERATING MANUAL
SECTION 4
AUTOMATIC FLIGHT CONTROL SYSTEM
TABLE OF CONTENTS
S u b j e c t ZiSi
GENERAL 1
FLIGHT DIRECTOR SYSTEM 1
AIR DATA SYSTEM 2
AUTOPILOT SYSTEM '-
STABILITY AUGMENTATION SYSTEM ?
Yaw Damping
Mach Trim
FLIGHT DIRECTOR COMPONENTS 7
Attitude Director Indicator
Horizontal Situation Indicator
Remote Heading and Course Select Controller
Flight Director Mode Selector
Flight Director Computer $
Rate Gyro
Vertical Gyro
Directional Gyro
Instrument Comparator
Touch Control Steering
AIR DATA COMPONENTS 3
Air Data Computer
P i l o t ' s Altimeter 9
P i l o t f s Vertical Speed Indicator
P i l o t ' s Mach/Airspeed Indicator
TAS/SAT/TAT Indicator
VNAV Computer/Controller
RIGHT COMPARTMENT DISPLAYS 9
Attitude Director Indicator
Attitude Sphere
Aircraft Symbol 12
Roll Attitude Pointer
Eyelid Display
Pitch and Roll Command Bar
Flight Director Warning Flag
Glideslope Pointer
Glideslope Warning Flag
4 - CONTENTS
Page 1
Oct 03/83
cacnhaatiiiaeinr Qer
OPERATING MANUAL
Subject Page
FLIGHT COMPARTMENT DISPLAYS
Radio Altitude Bar 12
Expanded Localizer Pointer 13
Inclinometer
Attitude Test Switch
Speed Command Display
Rate-of-Turn
Rate-of-Turn Warning Flag
Attitude Warning Flag
Localizer Warning Flag 14
Speed Command Warning Flag
Mode Annunciators
Radio Altitude Display
Decision Height Set Knob and Dim Control
Radio Altitude Test Switch
Decision Height Display 15
Horizontal Situation Indicator
Aircraft Symbol
Heading Dial
Heading Bug
Heading Flag
Course Select Pointer 18
Course Display
Course Deviation Bar
Course Deviation Dots
Vertical Deviation Pointer
Vertical Warning Flag
Distance Display
NAV Mode Annunciator 19
RNAV Mode Annunciator
Alert Annunciator
Vertical Mode Annunciator
Bearing Pointer
Bearing Select Pushbuttons and Annunciators
True Heading Annunciator
Navigation Warning Flag 20
Compass Sync Annunciator
Navigation Source Annunciators
To-From Annunciator
Instrument Remote Controller
Pilot's Altimeter
Altitude Alert 23
Failure Warning Flag
Pilot's Vertical Speed Indicator
Pilot's Mach/Airspeed Indicator
TAS/SAT/TAT Indicator
VNAV Computer/Controller
Altitude Preselect
Altitude Alert 24
4 -
Page
Oct
canadair
chauenQer
OPERATING MANUAL
Subject fii?
FLIGHT COMPARTMENT DISPLAYS
Vertical Navigation Computation 24
Vertical Path Flying 29
Vertical Input Cancelling
Instrument Comparator
SYSTEM CONTROLS 29
Flight Director Mode Selector
Heading Select Mode 30
Navigation Mode
VOR Mode
VOR Approach Mode 33
RNAV Mode
Localizer Mode
Back Course Mode
Localizer Approach Mode 34
Pitch Hold Mode
Altitude Hold Mode
Indicated Airspeed Hold Mode 36
Vertical Speed Hold Mode
Mach Hold Mode
Standby Mode
Altitude Preselect Mode 37
VNAV Mode
Go-Around Mode
Touch Control Steering
Autopilot Controller 33
Yaw Damper Engage
Autopilot Engage
Turn Knob
Pitch Hold
Couple 41
Soft Ride
FAILURE MONITORING AND STATUS ANNUNCIATION 41
Failure Warnings
Autopilot Self-Test 43
4 -
Page
Oct
canadsir
chanentjer
OPERATING MANUAL
LIST OF ILLUSTRATIONS
Figure
Number Title Page
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
AFCS Flight Compartment Contro"
Stability Augmentation Control
Attitude Director Indicator (2
Horizontal Situation Indicator
Instrument Remote Controller
Altimeter
Vertical Speed Indicator
Mach/Airspeed Indicator
TAS/SAT/TAT Indicator
VNAV Computer/Controller
Instrument Comparator
Flight Director Mode Selector
Control Wheel
Throttle Actuating Lever
Autopilot Controller
Warning and Disengage Lights
Autopilot Status Panel
Is and Indicators
Panel
Sheets)
(2 Sheets)
3/4
6
10
16
21
22
25
25
27
28
31
32
35
39
40
42
44
canaaair
chauencier
OPERATING MANUAL
SECTION 4
AUTOMATIC FLIGHT CONTROL SYSTEM
GENERAL (Figure 1)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：Bombardier-Challenger_00-Automatic_Flight_Control_System
