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CESSNA 200A AUTOPILOT
PILOT'S OPERATING HANDBOOK
(TYPE AF-295B)
SUPPLEMENT
6.
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.
7.
PULL-TURN Knob -- Turn airplane parallel to desired course.
NOTE
Airplane must be turned until heading is within ±5° of
desired course.
8.
PULL TURN Knob -- CENTER and PUSH in. The airplane should
then turn toward desired course at 45° ±10° intercept angle (if the
CDI needle is in full deflection).
NOTE
If more than 15 miles from the station or more than 3
minutes from intercept, use a manual intercept procedure.
NAV TRACKING (VOR/LOC):
1.
NAV TRK Button -- PUSH when CDI centers and airplane is within
±5° of course heading.
2.
HI SENS BUTTON -- DISENGAGE for enroute omni tracking
(leave ENGAGED for localizer).
3.
Autopilot TRIM Control -- READJUST as required to maintain
track.
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 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.
6
1 July 1979
.2
PILOT'S OPERATING HANDBOOK
CESSNA 300 ADF
SUPPLEMENT
(TYPE R-546E)
SUPPLEMENT
CESSNA 300 ADF
(Type R-546E)
SECTION .
GENERAL
The Cessna 300 ADF is a panel-mounted, digitally tuned automatic
direction finder. It is designed to provide continuous 1 kHz digital tuning
in the frequency range of 200 kHz to 1,699 kHz and eliminates the need for
mechanical band switching. The system is comprised of a receiver, a
bearing indicator, a loop antenna, and a sense antenna. Operating controls
and displays for the Cessna 300 ADF are shown and described in Figure 1.
The audio system used in conjunction with this radio for speaker-phone
selection is shown and described in Section 7 of this handbook.
The Cessna 300 ADF can be used for position plotting and homing
procedures, and for aural reception of amplitude-modulated (AM) signals.
With the function selector knob at ADF, the Cessna 300 ADF provides a
visual indication, on the bearing indicator, of the bearing to the transmit-
ting station relative to the nose of the airplane. This is done by combining
signals from the sense antenna with signals from the loop antenna.
With the function selector knob at REC, the Cessna 300 ADF uses only
the sense antenna and operates as a conventional low-frequency receiver.
The Cessna 300 ADF is designed to receive transmission from the
following radio facilities: commercial AM broadcast stations, low-
frequency range stations, non-directional radio beacons,
ILS
compass
locators.
SECTION 2
LIMITATIONS
There is no change to the airplane limitations when this avionic
equipment is installed.
1 July 1979
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