Beechcraft Baron G58 Pilot Operating Handbook page 181

Model G58
5. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN
6. Fuel Boost Pump . . . . . HI UNTIL FUEL FLOW PEAKS
7. Throttle . . . . . . . . . . . . . . . . . . . . .CLOSE; THEN OPEN
8. Magneto/Start Switch . . . . . . . . . . . . . . . . . . . . . START
9. Fuel Boost Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . HI
(Momentarily after starting to purge the system)
10. Fuel Boost Pump . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
BEFORE TAXI
1. Throttles . . . . . . . . . . . . . . . . . . . . . . . 900 to 1000 RPM
2. Oil Pressure and Temperature . . . . . . . . . . . . . . CHECK
Engine oil and oil pressure must be in green
band prior to engine run-up above 1200 RPM.
3. Avionics Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
4. Autopilot Preflight Test . . . . . . . . . . . . . . . . COMPLETE
a. Red AFCS Message . . . . . . . ILLUMINATED WHILE
b. Red AFCS Message . . . . . . . . . . . . EXTINGUISHED
c. White PFT Message . . . . . . . . . . . . . ILLUMINATED
d. White PFT Message . . . . . . . . . . . . EXTINGUISHED
e. Autopilot Disconnect Tone . . . . . . . . . . . . . .SOUNDS
5. MFD . . . . . . . AVIATION DATABASE ACKNOWLEDGE
6. PFD and MFD . . . . . . . DISPLAYED IN NORMAL MODE
7. AHRS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALIGNED
April, 2008
APPROXIMATELY 1/2 INCH
(Release to BOTH when engine starts)
(press ENT to continue)
Section 4
Normal Procedures
THEN OFF
AHRS ALIGNS
(~ 5 Seconds)
4-15