Honeywell SPZ-8000 Maintenance Manual page 677

At
point @ all altitudes
will be displayed as flight levels
in the FMS except for descent predictions less than 18,000
feet. Altitudes greater than 18,000 feet are displayed as
flight levels even when the aircraft is on the ground.
If the
baro correction is not changed to 29.92, the message CHECK BARO
SET will be displayed in the CDU scratchpad. This message is
displayed under the following conditions:
In a climb, if the baro set is not 29.92 and the aircraft
altitude equals the transition altitude (18,000 feet in this
example) plus 3000 feet, or the aircraft levels off between
the transition altitude plus 3000 feet above the transition
altitude.
In
a descent, if the baro set is 29.92 and the aircraft
altitude equals the transition altitude minus 3000 feet, or
the aircraft levels off between the transition altitude minus
3000 feet below the transition altitude.
At point ~ a constraint speed of 320 knots is entered on the
active flight plan page adjacent to WPT2, but since 320 is
larger than the entered 300 knots entered in PERF INIT, the
speed constraint is ignored and 300 remains as the speed target
(refer to rule 1).
At point ~ a constraint speed of 280 knots is entered
adjacent to WPT3. The active speed target changes to 280 knots
(refer to rule 2).
At point ~ the active speed target changes back to the
initialization climb speed of 300 knots when the waypoint is
sequenced (refer to rule 3).
The
speed target
will automatically change to a Mach target
(0.75 M) at the appropriate point or if selected on the GP-820
Flight Guidance Controller via the IAS/MACH pushbutton.
At point ~ the aircraft levels off at the cruise altitude of
45,000 feet and the speed target automatically changes to the
cruise speed of 0.78 M as entered in the performance
initialization.
22-14-00
Page
298.219
Apr 15/93
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