Beechcraft Baron G58 Pilot Operating Handbook page 184

Section 4
Normal Procedures
14. Standby Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . SET
15. Brakes . . . . . . . . . . . . . . . . . . . .RELEASE AND CHECK
BEFORE TAKEOFF (RUNUP)
1. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
2. Seat Belts and Shoulder Harnesses . . . . . . . .CONFIRM
3. Engine Instruments . . . CHECK WITHIN OPER. LIMITS
4. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2200 RPM
6. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . EXERCISE
7. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM
8. Magnetos. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Variance between individual magnetos should not
exceed 50 RPM
b. Maximum drop should not exceed 150 RPM
9. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1500 RPM
10. Propellers . . . . . . . . . . . . . . . . . .FEATHERING CHECK
a. Move the propeller controls past the detent
b. Do not allow an RPM drop of more than 300 RPM on
either engine.
Failure to observe the RPM limits during the
FEATHERING CHECK will impose high stresses
on the propeller mechanisms, blade shanks and
engines.
4-18
Never taxi with a flat shock strut
(to obtain 200 to 300 RPM drop)
Model G58
BUCKLED
April, 2008