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Diagram,
electrical system, 2-4
exterior inspection, 1-2
fuel system, 2-2
instrument panel, 1-8
loading arrangements, 4-5
maximum glide, 6-10
principal dimensions, ii
radio selector switches, 7-4
taxiing, 2-11
Dimensions, Principal, ii
Disorientation In Clouds, 3-4
emergency let-downs through
clouds, 3-5
executing 180
clouds, 3-5
recovery from spiral dive, 3-6
Ditching, 3-4
Economy Mixture Indicator, 2-15,
7-11
operating instructions, 2-15
Electrical Power Supply System
Malfunctions, 3-1
excessive rate of charge, 3-1
insufficient rate of charge, 3-2
Electrical System, 2-3
ammeter, 2-5
circuit breaker s and fuses, 2-5
ground service plug receptacle,
7-1
master switch, 2-3
over-voltage sensor and
warning light, 2-5
schematic, 2-4
Emergency Landing without Engine
Power, 3-3
Emergency Let-Downs Through
Clouds, 3-5
Index-2
o
Q
turn in
E
Emergency Locator Transmitter
(ELT), 3-8
ELT operation, 3-9
Empty Weight, inside front cover
Engine,
before starting, 1-4
instrument markings, 4-2
oil, inside back cover
operation limitations, 4-2
starting, 1-4, 2-9
Enroute Climb, 1-5, 2-13
maximum performance, 1-6
normal, 1- 5
Equipment, Cold Weather, 7-1
Excessive Rate of Electrical
Charge, 3-1
Executing 180
Q
3-5
Exterior Inspection Diagram, 1-2
Exterior Lighting, 2-6
File, Aircraft, 5-5
Fires, 3-6
electrical fire in flight, 3-7
engine fire during start on
ground, 3-6
engine fire in flight, 3-7
Flight in Icing Conditions, 3-7
Flyable Storage, 5- 5
Forced Landings, 3-3
ditChing, 3-4
emergency landing without
engine power, 3-3
precautionary landing with
engine power, 3-3
Fuel System, 2-1
capacity, inside back cover
fuel grade, inside back cover
fuel quantity indicator s, 4-3
long range fuel tanks, 2-3
quick-drain valve kit, 7-12
Turn in Clouds,
F
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