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SECTION 9
SUPPLEMENT 7
PIPER AIRCRAFT CORPORATION
PA-28R-201, ARROW
The following conditions will cause the Autopilot to automatically
disengage:
A. Power failure.
B. Internal Flight Control System failure.
C. With the KCS 55A Compass System, a loss of compass valid
(displaying HOG flag) disengages the Autopilot when a mode using
heading information is engaged. With the HDG flag present, the
Autopilot may be re-engaged in the basic wings level mode along
with any vertical mode.
O. Roll rates in excess of 16° per second will cause the autopilot to
disengage except when the CWS switch is held depressed.
E. Pitch rates in excess of 6° per second will cause the autopilot to
disengage except when the CWS switch is held depressed.
1
15
2
3
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4
5
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13
12
11
7
KC 192 AUTOPILOT & FLIGHT DIRECTOR COMPUTER
Figure 7-1
6
(
(
I.
KFC 150 SYSTEM KC 192 AUTOPILOT COMPUTER -
Complete Flight Director and Autopilot computer includes
(
system mode annunciators and system controls.
2.
MODE ANNUNCIATORS - Illuminates when a mode is selected
by
the corresponding mode selector button (PUSH ON - PUSH
OFF).
REPORT: VB-IJ65
ISSUED: SEPTEMBER 15, 1988
9-66,
II of 28
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