Table of Contents
Advertisement
SECTION
9
- SUPPLEMENTS
SUPPLEMENT
15
-
FAA
APPROVED
All angle
intercepts compatible
with radar vectors may
be
accomþlished
by selecting ROL mode
PRIOR
to
pressing
the
REV
button. The
HDG bug must
still be
positioned
to
the
localizer FRONT COURSE INBOUND heading
to
the
localizer FRONT COURSE INBOUNP
¡cftdin$
to
provide course
da-tLlrn
to the autopilot
when
using a
DG.
a) lf the D-Bar is greater than 2 to
3
dots: the
autopilot
'
will annunciate REVnnu; when the
computed capture
point is
reached
the ARM
annunciator
will go out
and
ine
selected
back
course
will be
automatically
captured and tracked.
b) lf the D-Bar is less than 2 to
3
dots: the HDG
mode
'
will
disengage upon selecting REV mode;
the
REV
annunciator
-
will
illuminate
and
the
capture/track
sequence will automatically begin.
b.
When equipped
with
HSI:
1) BARO
Setting (if installed) -- CHECK.
2)
Course Bearing pointer
--
SET
to the
ILS front
course
inbound heading.
3)
Heading Selector Knob
-
SET
BUG
to
provide
desired
intercept angle and engage HDG mode'
4)
REV
Mode
Selector Button -- PRESS.
CESSNA
MODEL 182S
NOTE
When REV
is
selected,
the
autopilot
will flash HDG for
5
the
HDG bug
to
the
heading.
lf
heading
utton
selection,
a
45'
intercept angle will then be automatically established
based
on
the position
of
the
bug.
NOTE
s15-30
Dec 31/99
Advertisement
Chapters
Table of Contents
