Cessna T182 1982 Pilot Operating Handbook page 230

19
PILOT'S OPERATING HANDBOOK CESSNA 300A AUTOPILOT
SUPPLEMENT (TYPE AF-395A)
4. Heading Selector Knob -- ROT ATE bug to selected course (VOR or
localizer - inbound or outbound as appropriate).
5. Directional Gyro --SET for magnetic heading.
6. NAV INT Button -- PUSH.
7. HI SENS Button -- PUSH for localizer and "close-in" omni inter ­
cepts.
8. BACK CRS Button -- PUSH only
if
intercepting localizer front
course outbound or back course inbound.
CAUTION
With BACK CRS button pushed in and localizer frequency
selected, the CDI on selected nav radio will be reversed
even when the autopilot switch is OFF.
9. PULL-TURN Knob -- PUSH.
NOTE
Airplane will automatically turn to a 45
0
intercept angle.
NAV TRACKING (VOR/LOC):
1.
NA V TRK Button -- PUSH when CDI centers (within one dot) and
airplane is within
± 100
of course heading.
2. HI SENS Button -- Disengage for en route omni tracking (leave
engaged for localizer).
NOTE
Optional ARC function, if installed, should not be used for
autopilot operation.
If
airplane should deviate off course,
pull out PULL TURN knob and readjust airplane rudder
trim for straight flight on the turn coordinator. Push in
PULL TURN knob to reintercept course.
If
deviation
persists, progressively make slight adjustments of auto­
pilot TRIM control or heading bug on the directional gyro,
towards the course as required to maintain track.
SECTION 5
PERFORMANCE
There is no change to the airplane performance when this avionic
equipment is installed.
21 August 1981
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