Piper Turbo Saratoga PA-32-301T Pilot's Manual page 269

PIPER AIRCRAFT CORPORATION SECTION 9
PA-32-301T, TURBO
SARATOGA
SUPPLEMENTS
c.
At the F.A.F. inbound,
return
to pitch mode
for
control of
descent and
reduce
power.
d.
At the M.D.A. select altitude hold mode and add power for
level flight. Monitor altimeter
to assure accurate altitude
control
is being provided by the autopilot.
e.
Go-Around
-
For missed approach
select desired pitch at-
titude with pitch command
disc and disengage altitude
hold
mode. This will initiate the
pitch
up
attitude change.
Immediately add takeoff
power
and monitor altimeter and
rate
of climb
for
positive climb
indication.
After climb
is
established,
retract
flaps.
Adjust
attitude as
necessary
for
desired
airspeed and select
HDG
mode for
turn
from the
VOR final approach
course.
(2)
1LS
-
Front
Course
Approach With Glide Slope Capture.
(Optional)
a.
Track inbound
to
LOM as described in
Section 4 (f)
or
(g)
above and
in altitude
hold mode.
b. Inbound to LOM slow to 90
-
95 KlAS and lower flaps
as
desired.
c.
Automatic glide slope capture will occur at glide slope
intercept if the following
conditions
are met:
1.
Coupler in LOC-Normal
mode.
2. Altitude hold
mode engaged (altitude
rocker
on
console).
3.
Under glide slope
for
more
than 20 seconds.
4.
Localizer
radio
frequency
selected on NAV receiver.
d. At
glide slope intercept immediately reduce power to main-
tain approximately
90-95
KIAS
on
final
approach.
Glide
slope capture is indicated by lighting of the green glide
slope engage annunciator
lamp
and by a slight pitch down
of the aircraft.
e.
Monitor
localizer
and glide slope raw
data
throughout
approach.
Adjust power as necessary to maintain
correct
final approach airspeed.
All power changes should
be
of
small magnitude
and smoothly applied for
best
tracking
performance. Do not change aircraft configuration
during
approach
while autopilot
is engaged.
ISSUED:
APRIL 4, 1980
REPORT: VB-1070
REVISED:
MAY
16, 1980
9-45