1A. THE
KA
285 ANNUNCIATOR PANEL
provides the same functions as the KAP 315
with the exception of the
ALT
ARM light.
I
2A.
THE KI
256
3-INCH VACUUMlELECTRlC
FLIGHT COMMAND INDICATOR disdavs
.~
the following information:
Pitch and roll attitude
Pitch and roll commands
Decision height (DH)
3A. THE KI 525A PICTORIAL NAVIGATION
INDICATOR displays slaved gyro magnetic
heading information and operates similarly
to the KPI 552.
6.
KEA
346
SERVOED ALTIMETER provides
barometric corrected altitude information to
the KAS 297 Altitude Selector and encoding
for an ATC transponder.
5.
THE OPTIONAL KC
291
YAW MODE
CONTROLLER can be installed alongside
the KC 290 Mode Controller. In this config-
uration the yaw axis is wired
so
that it
automatically engages when the Autopilot is
engaged. Disengagement of the yaw damper
is accomplished by using the control wheel
mounted disengage switch or the KC 291
engageldjsengage switch.
The Yaw Damper only is engaged
or disengaged using the KC 291. The Yaw
Damper engage status is annunciated on
7.
THE
KAS
297
ALTITUDE SELECTOR
the KC 291.
permits the pilot to preselect a desired altitude
Some airplanes are certified with the in climb or descent. The system provides
yaw damper on at all times when the autopilot automatic capture and hold upon reaching
is
engaged. (Refer
to
Flight Manual Supple- that altitude. Altitude alerting is also provided
ment to determine your type of installation.) as required by FAR 91.51.
A
L'
IRH
SELECTED ALTITUDE
v
SET
A
"..An
10
To Next Page
