Beechcraft Baron 58 - Nose Section; Right Wing Leading Edge

BEECHCRAFT Baron 58
Serial
TH-773 and After
Section IV
Normal Procedures
k. Propeller - EXAMINE FOR NICKS, SECURITY
AND OIL LEAKS
I. Cowl Flap - CHECK
m. Wheel Well Doors, Tire, Brake Line and Shock
Strut - CHECK
n. Landing Gear Uplock Roller - CHECK
o. Fuel Drains - DRAIN
7. NOSE SECTION
a. Wheel Well Doors, Tire and Shock Strut - CHECK
b. Pitot(s) - REMOVE COVER, EXAMINE FOR
OBSTRUCTIONS
c. Taxi Light - CHECK (if installed)
d. Heater
Air Inlets - CLEAR
e. Oxygen - CHECK
f. Baggage Door - SECURE
8. RIGHT WING LEADING EDGE
a. Wheel Well Doors, Tire, Brake Line, and Shock
Strut - CHECK
b. Landing Gear Uplock Roller - CHECK
c. Cowl Flap - CHECK
d. Fuel Drains - DRAIN
e. Engine Oil - CHECK QUANTITY, CAP AND DOOR
SECURE
f. Engine Cowling and Doors - CHECK CONDITION
AND SECURITY
g. Landing Ught (if installed) - CHECK
h. Propeller - EXAMINE FOR NICKS, SECURITY,
AND OIL LEAKS
i. Engine Air Intake - REMOVE COVER AND
EXAMINE FOR OBSTRUCTIONS
j. Fuel Sight Gage - CHECK
k.
Fuel· CHECK QUANTITY AND CAP(S)
SECURE. ALWAYS CHECK WING TIP TANK
FIRST
(IF INSTALLED); DO NOT REMOVE
INBOARD CAP IF FUEL IS VISIBLE IN TIP
TANK.
August, 1984 4-5