For Training Purposes Only
Sept 04
2-5
P I L O T T R A I N I N G G U I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
Air data source identification
Lateral and vertical path deviations
Attitude source identification
Distance to station
NAV source identification
Tuned-to-NAV and To/From status
Course error
Inner, middle and outer marker data
Heading error
Radio altitude and flags
The source of other guidance information is selected via the source identifier received
from selected PFD symbol generator. The data received includes:
IRS:
Roll angle
Normal acceleration
Pitch angle
Ground speed
Roll rate
True track angle
Pitch rate
Flight path angle
Yaw rate
Magnetic heading
Longitudinal acceleration
True heading
Lateral acceleration
Inertial vertical speed
ADC:
Baro-corrected altitude
True airspeed
Pressure altitude
Dynamic pressure
Vertical speed
VMO
Mach
MMO
Calibrated airspeed
FMS:
Lateral steering command and flags VNAV submode selection flags
VNAV targets
FWC:
Preselected altitude
Display Controller (DC):
Speed references
