Beechcraft Baron 58 - Left Fuselage; Left Wing Trailing Edge; Left Wing Leading Edge

BEECHCRAFT Baron 58
Serial TH-773
and After
Section IV
Normal Procedures
4. LEFT FUSELAGE:
a. Cabin Air Outlet - CHECK
b. Static Port - UNOBSTRUCTED
c. All Antennas and Lower Beacon - CHECK
5. LEFT WING TRAILING EDGE:
a.
Fuel Sump Aft of Wheel Well - DRAIN
b. Fuel Vents w CHECK
c.
Flaps - CHECK GENERAL CONDITION
d. Aileron - CHECK CO~DITION AND FREEDOM OF
MOVEMENT, TAB NEUTRAL WHEN AILERON
NEUTRAL
6. LEFT WING LEADING EDGE
a. Lights and Deice Boot - CHECK FOR CONDITION
b. Stall Warning Vane - CHECK FREEDOM OF
MOVEMENT
c. Fuel - CHECK QUANTITY AND CAP(S) SECURE. AL-
WAYS CHECK WING TIP TANK FIRST (IF IN-
STALLED);
DO NOT REMOVE INBOARD CAP IF
FUEL IS VISIBLE IN TIP TANK.
d. Wing Tip Tank (if installed) Sump - DRAIN
e. Fuel Sight Gage - CHECK
f. Tie Down, Chocks - REMOVE
g. Engine ou . CHECK QUANTITY, CAP AND DOOR
SECURE
h. Engine Cowling and Doors - CHECK CONDITION
AND SECURITY
i. Landing Light (if installed) - CHECK
j. Engine
Air Intake - REMOVE COVER AND EX-
AMINE FOR OBSTRUCTIONS
August, 1984
4-4A