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SOLOY TURBINE PAC
SECTION 7
POHS CESSNA T206H/206H
AIRPLANE & SYSTEMS
DESCRIPTION
7-4
F.A.A. Approved
May 23, 2003
FIGURE 7-1. INSTRUMENT PANEL (Sheet 1 of 2)
1
Transmission Oil Pressure
36
Propeller Controls
2
Suction Gage
37
Power Control
3
Fuel Quantity
38
Rudder Trim
4
Ammeter
39
Engine Alternate Air Control
5
Digital Clock and O.A.T.
40
Alternate Static Air Control
6
Fuel Flow and Temperature
41
Optional Continuous Ignition Switch
7
Turn Coordinator
42
Fuel Cut Off Control
8
Airspeed Indicator
43
Hand Microphone
9
Heading
44
12 Volt Power Port
10
Attitude
45
Engine Inlet Anti-ice Control
11
Spare
46
Fuel Selector
12
Vertical Speed
47
Radio and Panel Dimming Control
13
Altimeter
48
Glareshield/Pedestal Dimming Control
14
Optional Floatplane Gear
49
Elevator Trim
15
Nav 1/Nav 2
50
Optional Cowl Landing Lights Switch
16
Avionics Stack
51
Optional Cowl Landing Lights C.B.
17
Nav/GPS Selector
52
Optional Prop De-ice Switch
18
Optional Prop De-ice
53
Spare Circuit Breaker or Switch
19
Annunciator Panel
54
Optional Floatplane Circuit Breakers
20
Engine Oil Pressure/Temperature
55
Engine Start Circuit Breaker
21
Np Tachometer
56
Auto Feather Annunciator Light C.B.
22
N
1
Tachometer
57
Generator Field Circuit Breaker
23
T.O.T. Indicator
58
Avionics Master Switch
24
Torque Indicator
59
Hand Brake
25
Annunciator Lights
60
Circuit Breakers and Switch/Breakers
26
ELT Remote Switch/Annunciator
61
Spare Circuit Breaker or Switch
27
Hour Meter
62
Optional Continuous Ignition C.B.
28
Optional Avionics
63
Overspeed Warning Circuit Breaker
29
Avionics Circuit Breaker Panel
64
Generator Switch
30
Glove Box
65
Battery Switch
31
Auxiliary Cabin Air
66
Start/Motor Switch
32
Cabin Defrost
67
Generator Reset Switch
33
Cabin Air
68
Auto Feather Test Button
34
Cabin Heat
69
Reset Generator Circuit Breaker
35
Wing Flap Switch/Position Indicator
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