SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Electronic Flight Instrument System (EFIS)
4-16
Climb to Initial Altitude
Figure 4--7 shows a display with the aircraft on climbout at 200 kts in
heading (HDG) and pitch attitude hold mode (not annunciated) with the
autopilot (AP) engaged. The flight director commands are satisfied.
AD--58059@
Climb To Initial Altitude
Figure 4--7