Honeywell PRIMUS 1000 - Climb to Initial Altitude

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-54
CLIMB TO INITIAL ALTITUDE
The aircraft is on climb, approaching 250 knots in HDG select and IAS
hold modes, as shown in figure 4--28. The AP and YD are engaged.
Altitude select is armedandtheamber altitude preselect digits indicate
that the aircraft is between 1000 and 250 feet from the 7000--foot
selected altitude. Vertical speed is 1500 feet per minute. The altitude
trend vector indicates climb. Flight director commands are satisfied.
3030
3030
AD--50922--R1@
Climb to Initial Altitude
Figure 4--28