Honeywell PRIMUS 1000 Pilot's Manual page 187

Mode
Pitch Sync TCS Switch on
Wheel
ALT Hold Micro Air Data
Computer
VS Hold Micro Air Data
Computer,
Accelerometer
SPD Hold, Micro Air Data
FLC Computer
(DGC for FLC)
ALT Preselect Micro Air Data
Computer/
Altitude
Preselect on
MFD
NOTE: FLC, on climb (airspeed) and descent (vertical speed) is controlled by the
respective IAS and V/S error and pitch/pitch rate limit values.
System Performance/Operating Limits
A28--1146--112--00
Control or
Sensor
Pitch Attitude
Command
ALT Hold Engage
Range
ALT Hold Engage
Error
Pitch Limit
Pitch Rate Limit
VERT Speed Engage
Range
VERT Speed Hold
Engage Error
Pitch Limit (see note)
Pitch Rate Limit (see
note)
SPD Engage Range
SPD Hold Engage
Error
Pitch Limit
Pitch Rate Limit
Preselect Capture
Range
Max. VS for Capture
Max. Gravitational
Force During Capture
Maneuver
Pitch Limit
Pitch Rate Limit
Table 7--1
PRIMUSr1000 Integrated Avionics System
Parameter
±20_max.
0 to 37,000 ft
±20 ft
±20_
f (TAS)
0 to ±6,000 ft/min
±30 ft/min
±20_
f (TAS) 0.3 g' s max
80 to 330 kts
±2 knots
±20_
f (TAS)
0 to 37,000 ft
±6000 ft/min.
±0.275g
±20_
f (TAS)
Value
System Limits
7-7