Honeywell SPZ-8000 Maintenance Manual page 666

Digital automatic flight control system for gulfstream iv
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The
speed
target
is
MAINTENANCE
MANUAL
GULFSTREAM IV
changed
to the descent
speed, provided
the
preselector
is
dialed
down, just prior
to the TOD if a
deceleration is required or at the TOD if no deceleration is
required. For any descent greater than 6500 feet, any
descent within 100 miles of the TOD, or
any descent past the
TOD, the
speed target is changed to the descent speed (at
the beginning of the descent).
Descents
started
more than
100 miles prior to the
TOD and descents with less than 6500
feet altitude change are considered cruise descents, and the
speed target remains at the cruise
speed.
During descent, the speed target is the descent speed
schedule selected during initialization, and the transition
to CAS is accomplished automatically. This speed schedule
is observed during any intermediate
level off.
.
If a speed/altitude limit is entered, the speed target is
changed to the limit minus 10 knots prior to the limiting
altitude to allow for deceleration,
provided the preselector
is set below the limiting altitude.
c
When the aircraft is within 20
NM flight plan distance from
the destination and less than 10,000 feet above the
destination elevation, the speed target is changed to the
placard speed for 10-degree flaps minus 10 knots.
This
allows
for
the
pilot
to
start
extending
the
flaps
when
required.
.
As the gear and flaps are extended, the
speed
target
is
changed
to the placard
minus
10 knots
for the next
expected
flap selection.
When
landing
flaps
are selected,
(39
degrees),
the speed
target
is set to Vref
plus
10 knots.
Typically,
the speed
would
change
to 240 knots
at 20 NM, 210
knots when
10-degree
flaps
are selected,
160 knots when
20-degree flaps are selected, and some value between 133-158
knots when 39-degree flaps are selected.
.
Vref
displayed
on the
display
controller
and on the
PFD is
calculated
by the
FMS and is always based on current weight
and configuration.
This Vref is accurate and valid even
below the 45,000 pound minimum landing weight.
.
If go-around
is selected,
the
speed
target
is changed
as
described
for climb.
22-14-00
Page 298.213
Apr 15/93
Use or disclosure
of informationon
this page is subject
to the restrictions
onthe
title page ofthis
document.

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