Beechcraft Baron G58 Pilot Operating Handbook page 183

Model G58
c. TEST Softkey . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
1) Test Pattern. . . . . . . . . . . . . . . . VERIFY ON MFD
2) [TRAFFIC] . . . . . . . . . . . . . . . . . VERIFY ON PFD
d. Verify Voice Message . . . . . "Traffic Advisory System
e. ALT MODE. . . . . . . . . . . . . . . . . . SET AS DESIRED
f. Small FMS Knob . . . SELECT DESIRED MAP PAGE
12. TAWS (if desired) (if installed) . . . . . . . . . . . . . . . .TEST
a. Large FMS Knob (if reqd.) . . . SELECT MAP GROUP
b. Small FMS Knob . . . . . . SELECT THE TAWS PAGE
c. Press the MENU Key
d. Small FMS Knob . . . . . . . . . . SELECT "Test TAWS"
e. Press ENT Key
f. Verify a white [TAWS TEST] is displayed on the PFD.
g. Verify the TAWS page turns black, a yellow [TAWS
TEST] is displayed in the center of the page and a
white [TAWS TEST] is displayed in the lower right
corner.
h. Verify "TAWS SYSTEM TEST, OK" is heard at the
end of the test.
13. Standby Attitude Indicator. . . . . . . . . . . . . . . . . . CHECK
a. Standby Battery . . . . . . . . . . . . CHECK IF DESIRED
b. STBY PWR LED . . . . . . . . . . . . . . . EXTINGUISHED
c. Flag . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULLED
d. PULL-TO-CAGE Knob . . . . . . . . . . PULL TO ERECT
The indicator may be damaged if the PULL-TO-
CAGE knob is released with a snap.
April, 2008
(see OTHER NORMAL PROCEDURES)
Section 4
Normal Procedures
Test Passed"
(release knob slowly)
4-17