Beechcraft Baron 58 - Page 71

~I
FUGHTINSTRUMENTS
enm
111m
::l·m
Altimeter
1
1 1 1
!!?O
Airspeed Indicator
1
1 1 1
-I:::t
:::to
Magnetic Compass
1
1
1
1
.....
::u
Attitude Indicator
0
0
1
1
.....
»
w."
Turn and Slip Indicator 0
0
1
1
III
-I
Directional Gyro
0 0
1
1
:1m
Q.III
Clock
0
0
1 1
» ..
Outside Air Temperature Indicator
1 1
1
1
;:tg
!t UI
FUEL EQUIPMENT
CD
Engine Driven Fuel Pump
2
2 2
2
Electrically Driven Aux Fuel Pump
2 2
2
2
Fuel Quantity Indicator
2
2
2
2
Fuel Flow Indicator
1
1
1
1
Fuel selector Valve
2
2 2
2
ICE AND RAIN PROTECTION
Emergency Static Air System
0
0
(If Installed)
r-
Pilot Heater
0 0
1
1
3·
en
_.111
Heated Fuel Vent 0
0
2
2
"0
III
..
~II
..
_.
-·0
o
:I
...,
;l=