Honeywell PRIMUS 1000 Pilot's Manual page 163

Integrated avionics system for the citation encore
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R
PRIMUS
1000 Integrated Avionics System
Control or
Sensor
Mode
ALT
Micro Air Data
Preselect
Computer/
Altitude
Preselect on
MFD, AHRS,
IAC
VNAV
MADC, MFD,
NAV Menu,
IAC, FMS,
VOR/DME
System Performance and Operating Limits
System Limits
5-8
Parameter
Preselect Capture
Range
Max. VS for Capture
Max. Gravitational
Force During Capture
Maneuver
Pitch Command Limit
Pitch Rate Limit
Singlepoint VNAV
(Inoperative in the Encore)
Altitude Range Path
Angle Range
Elevation Range
Bias Range
Pitch Limit
Pitch Rate Limit
Pitch Limit
Pitch Rate Limit
FMS VNAV Steering Command
Pitch Limit
Pitch Rate Limit
Table 5–1
Value
–900 to 45,000 ft
±6000 ft/min.
±0.275g
±15_
f (TAS)
–900 to 45,000 ft.
±6_, one vertical waypoint
0 to 10,000 ft.
±99.9 NM from VOR, FMS
±15_
300/(TAS 2_/sec max/min)
±20_
f (TAS)
±20_
f (TAS)
A28–1146–134
REV 1 Jan/03

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