Table 5–2 defines the air data units of measure and their data range for
this aircraft.
Display
Altitude
Pressure Altitude,
Baro Corrected Altitude
Altitude Rate
Preselect Altitude
Baro Set
Baro Set
Airspeed/
Indicated Airspeed
Mach
Mach
Vertical
Vertical Airspeed,
Airspeed
Vertical Speed Target
Air Data Display Parameters and Ranges
A28–1146–134
REV 1 Jan/03
PRIMUS
Parameter
Table 5–2
R
1000 Integrated Avionics System
Units
Data Range
feet
–1000 to 60,000
ft/min.
–20,000 to +20,000
feet
0 to 60,000
inHg
16 to 32
hPa
541 to 1083
knots
40 to 450
Mach
0.380 to 1.0
ft/min.
–9999 to +9999
System Limits
5-9/(5-10 blank)