Cessna 172S Nav III User Manual

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CESSNA SECTION 9 - SUPPLEMENTS
SUPPLEMENT 3
MODEL 172S NAV III
GENERAL (Continued)
BENDIXlKING KAP 140 2 AXIS AUTOPILOT WITH ALTITUDE
PRESELECT, OPERATING CONTROLS AND INDICATORS
1
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KIIPl40
2 3 4
18
5
16 23
22
6
7
8 9
Figure S3-2
KAP 140 WITH ALTITUDE PRESELECT
21 20
19
1. PITCH AXIS (P) ANNUNCIATOR - When illuminated,
indicates failure of pitch axis and will either disengage the
autopilot or not allow engagement of the pitch axis.
In
turbulent air, will illuminate during abnormal
verticaVaccelerations.
2. AUTOPILOT ENGAGE/DISENGAGE (AP) BUTTON - When
pressed
and held (approx. 0.25 seconds), engages autopilot
if all preflight self-test conditions are met. The autopilot will
engage
in the basic roll (ROL) mode which functions as a
wing leveler and the pitch axis vertical speed
(VS) mode. The
commanded vertical speed will
be displayed in the upper
right corner of autopilot display area. The captured
VS will
be the vertical speed present
at the moment the AP button is
pressed. The button may also be used to disengage the
autopilot.
3. ROLL AXIS (RI ANNUNCIATOR - When illuminated,
indicates failure
of the roll axis and disengages the autopilot.
(Continued Next Page)
FAA APPROVED
172SPHAUS-S3-00
U.S. S3-9

Cessna 172S Nav III Specifications

General

Brand	Cessna
Model	172S Nav III
Category	Aircrafts
Language	English