P/N 11934-S24
3 of 6
Cirrus Design
Section 9
SR20
Supplements
Section 2 - Limitations
1.
The Sandel Avionics SN3308 Navigation Display Pilot's Guide,
SPN 90106-PG-C or later revision, must be immediately available
to the flight crew when navigation is predicated on use of the
Sandel SN3308 Navigation Display.
2.
The “CRC Self Test Failed” message must not appear on power-
up if flight operations are predicated on the use of the SN3308
Navigation Display.
3.
If flight into IMC is anticipated, the airplane must be flown from the
left seat.
Section 3 - Emergency Procedures
1.
If the SN3308 Navigation Display fails to operate, use the
magnetic compass as the heading source.
2.
If the remote directional gyro fails or becomes inoperative, the
compass rose color will change from white to amber and the flux
gate will provide the heading. The heading display will respond
much more slowly than normal.
3.
If the fluxgate fails, the SN3308 Navigation Display compass rose
color will change from white to amber and the heading numbers
will disappear. The display can be used to determine relative
heading for turns; however, the magnetic compass must be used
to determine absolute heading.
4.
The SN3308 Navigation Display is powered through redundant 5-
amp circuit breakers. HSI/PFD #1 circuit breaker is on the
Essential Bus and HSI/PFD #2 circuit breaker is on Main Bus 2.
Either circuit is capable of powering the Navigation Display.
5.
Refer to the Sandel Avionics SN3308 navigation Display Pilot’s
Guide
for error messages and alerts.
Section 4 - Normal Procedures
Activate Navigation Display
1.
Battery Master Switch................................................................ON
2.
Avionics Power Switch ...............................................................ON
Original: 01-07-03
Содержание SR20
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