BOMBARDIER Primus 2000XP Pilot Training Manual page 7

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