Beechcraft Baron 58 - Preflight Inspection; Cockpit; Right Fuselage; Empennage

Refer to all applicable Beech Supplements and
STC Supplements for flight phase procedures for
optional equipment installed in the airplane.
I
Section IV
Normal Procedures
NOTE
BEECHCRAFT Baron 58
Serial TH 773 and After
PREFLIGHT INSPECTIO"N
1. COCKPIT:
a. Control Lock - REMOVE AN D
STOW
b. Parking Brake - SET
c. All Switches - OFF
d.
Trim Tabs - SET TO ZERO
2. RIGHT FUSELAGE:
a. Load
Distribution - CHECK AND SECURED
b.
Utility Door - SECURE
c.
Static Port - UNOBSTRUCTED
d.
Emergency Locator Transmitter - ARMED
3. EMPENNAGE:
a. Control Surfaces, Tabs and Deice
Boots - CHECK
CONDITION, SECURITY,
AND ATTACHMENT
b. Tail Cone, Tail Light, and Rudder Beacon - CHECK
c. Tie
Down - REMOVE
d. Cabin
Air Inlet - CHECK
4-4
August, 1984