Download Print this page

Piper CHEROKEE ARCHER II Pilot Operating Handbook page 158

Hide thumbs Also See for CHEROKEE ARCHER II:

Advertisement

PIPER
AIRCRAFT CORPORATION
PA-28-181, CHEROKEE ARCHER
TI
SECTION
9
SUPPLEMENTS
SI.JPPLEMENT
2
AUTOFLME
II
AUTOPILOT INSTALLATION
SECTION
I
. GENERAL
This supplement
supplies
information
necessary
for
the operation
of
the airplane when the optional
AutoFlite
II
Autopilot is
installed. The
information
contained
within this
srpplement is
to
be used "as
described"
in coniunction with the
complete handbook.
This supplement
has been
"FAA
Approved"
as
a
perrnanent
part of this handbook
and must remain
in
this handbook at all times when the optional
AutoFlite
II
Autopilot
is installed.
SECTION
2.
LIMITATIONS
(a)
Autopilot
use
prohibited
above 149
KIAS.
(b)
Autopilot "OFF"
during takeoff and landing.
SECTION
3.
EMERGENCY PROCEDURES
(a)
In
case
of malfunction
DEPRESS
and
hold Disconnect switch
on
pilot's control
wheel.
(b)
RocLcr
svitch
on inrtnrmcnt
prnel'OFF."
(c)
Unit may
be overpowered
manudly.
(d)
In
climb, cnrise
or &rccnt
configrration
e
rnelfunction
with a
3 rcond
delay
in
recovery
initiation may
res.rlt
in
45o brnk and 180' dtihrde
loss.
Me"ximum
altitude
loss nrcasured
at
149
KIAS in
a
descent.
(e)
[n
approach configuration a malfunction
with a
I
second delay
in
recovery
initiaton
results
in
I
8'
bank and 10' altihrde
loss.
SECTION
4.
NORMAL
PROCEDURES
(a)
EnSrgerncnt
(
I
)
Rockcr Switch on
bilnrment pael '
ON.
(2)
Disconnect Switch on
left
hand
side
of pilot's control
wheel
-
RELEASED.
(b)
Disengagement
(
I
)
Depress
Disconnect Switch on
pilot's control
wheel
(or)
(2)
Rocker Switch on instrument panel
-
OFF.
(c)
Heading
Changes
(l)
Depress
Disconnect Switch, make Heading
Change, release
Disconnect Switch.
(2)
Move
Trim Knob on irutnrment for
Drift
Correction from
a
constant heading.
(3)
Move
Tum
Command
Knob on instnrme'nt for right or left
banked turns'
REPIORT: VB.79O
9-7
ISSUED: JLJNE 18, 1976

Advertisement

loading