Beechcraft Baron G58 Pilot Operating Handbook page 185

Model G58
11. Electric Elevator Trim . . . . . . . . . . . . . . . . . . . . . CHECK
a. Left and Right Segments . . . . . . . . . . . . . . ACTUATE
(verify there is no trim movement. Red PTRM illumi-
nated on PFD if actuated for >4 sec.)
b. Left and Right Segments . . . ACTUATE TOGETHER
c. AP DISC Switch . . . . . . . . . . . . . . . . ACTUATE WITH
12. Trim. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
a. Aileron and Rudder . . . . . . . . . . . . . . . . . . NEUTRAL
b. Elevator . . . . . . . . . . . . SET WITHIN GREEN BAND
13. Flaps . . . . . CHECK OPERATION, SET FOR TAKEOFF
14. Flight Controls. . . .CHECK FREEDOM OF MOVEMENT
15. Doors and Windows . . . . . . . . . . . . . . . . . . . . . SECURE
• Cabin Door Lock Indicator. . . . . . . . . . CHECK CLOSED
16. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
17. Fuel Boost Pump . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
(if ambient temperature is 32°C or above, use LOW
pressure boost)
18. Alerts/Messages . . EXTINGUISHED OR CONSIDERED
19. PFD Attitude and Heading . . . . . . . . . . . . . . . .NORMAL
20. GPS Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . VALID
21. Standby Attitude Indicator. . . . . .ERECT AND NORMAL
22. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
April, 2008
(verify proper trim movement)
AND PROPER DIRECTION OF TRAVEL
(feel for detent; confirm visually)
('LOI' not annunciated on HSI)
Normal Procedures
INDIVIDUALLY
TRIM IN MOTION
(verify trim motion stops)
Section 4
4-19