Piper Turbo Saratoga PA-32-301T Pilot's Manual page 327

PIPER AIRCRAFT CORPORATION
SECTION 9
PA-32-301T, TURBO SARATOGA SUPPLEMENTS
Figure 7-9
(cont)
5.
COURSE BEARING
POINTER
-
Indicates selected VOR course
or
localizer
course on compass card (l0). The selected
VOR
radial
or localizer
heading remains
set on
the
compass
card when the
compass
card
(10)
rotates.
6. TO FROM
INDICATOR FLAG
-
Indicates
direction of VOR
station relative to selected course.
7.
DUAL GLIDE SLOPE POINTERS
-
Indicate on glide slope scale
(8)
aircraft displacement
from glide slope beam center. Glide slope
pointers in view
indicate a usable glide slope signalis being received.
The glide slope
pointers
will bias out of view
if
the glide slope signal
is lost.
8.
GLIDE SLOPE SCALES
-
Indicate
displacement from glide slope
beam
center.
A
glide slope deviation bar displacement of
2 dots,
represents
full scale
(0.7°)
deviation
above or below
glide
slope
beam centerline.
9. HEADING
SELECTOR KNOB
( )
-
Positions heading bug
(14)
on compass
card (IO) by rotating the heading selector knob.
The
Bug rotates with the compass card.
10. COMPASS CARD
-
Rotates
to display heading of airplane with
reference
to
lubber line
(3)
on HSI.
1I. COURSE SELECTOR KNOB
-
Positions
course bearing pointer
(5)
on the compass card
(10)
by rotating
the course selector knob.
12. COURSE DEVIATION BAR (D-BAR)
-
The center portion of
omni bearing pointer moves laterally
to
pictorially indicate the
relationship of aircraft to the selected course. It
indic¼tes degrees
of
angular
displacement from
VOR radials
and
localizer
beams,
or
displacement in
nautical miles from
RNAV
courses,
13. COURSE
DEVIATION SCALE
-
A coursedeviationbardisplace-
ment of
5 dots
represents
full scale (VOR
=
±l0°,
LOO=
±2 I/2°,
RNAV
=
5NM, RNAV APR
=
1 1
4NM)
deviation from beam
centerline.
14. HEADING BUG
-
Moved by
( )
knob
(9)
to
select desired
heading.
ISSUED: AUGUST 6, 1982 REPORT: VB-1070
9-103