D
E m e r g e n c y L o c a t o r Tr a n s m i t t e r
(ELT), 3-10
ELT operation, 3-10
Empty Weight, inside front cover
Engine,
Diagram,
electrical system, 2-5
ELT control panel, 3-11
exterior inspection, 1-2
fuel system, 2-2
instrument panel, 1-8
loading arrangements, 4-7
maximum glide, 6-10
principal dimensions, ii
radio selector switches, 7-4
taxiing, 2-12
Dimensions, Principal, ii
Disorientation In Clouds, 3-5
emergency let - d o wns through
clouds, 3-5
executing 180° turn in
clouds, 3-5
recovery from spiral dive, 3-6
etching, 3-3
before starting, 1-4
instrument markii^s, 4-3
magneto check, 2-13
oil, inside back cover
operation limitations, 4-3
rough operation or loss of
power, 3-7
starting, 1-4, 2-10, 2-20
warm-up, 2-11
Engine Failure, 3-1
af t e r t a k e - o ff , 3 - 1
during flight, 3-1
Enroute Climb, 2-15
maximum performance, 1-6
normal, 1-5
Equipment, Cold Weather, 7-1
Excessive Rate of Electrical
Charge, 3-9
Executing 180° Turn in Clouds,
E
3-5
Economy Mixture Indicator, 7-7
operating instructions, 2-17
Electrical Power Supply System
Malfunctions, 3-8
excessive rate of charge, 3-9
insufficient rate of charge, 3-9
Electrical System, 2-4
ammeter, 2-4
circuit breakers and fuses, 2-6
ground service plug receptacle,
7-1
ma s te r s w i t c h , 2 - 4
over-voltage sensor and
war nin g lig h t, 2 -4
schematic, 2-5
Emergency Landing Without Engine
Power, 3-2
'mergency Let-Downs Through
Clouds, 3-5
Exterior Inspection Diagram, 1-2
Exterior Lighting, 2-6
F
Flap Settings, Wing, 2-14
File, Aircraft, 5-5
Fires, 3-3
electrical fire in flight, 3-4
engine fire during start on
ground, 3-3
engine fire in flight, 3-4
Flight in Icing Conditions, 3-6
Flyable Storage, 5-6
Forced Landings, 3-2
ditching, 3-3
emergency landing without
engine power, 3-2
Index-2
To Next Page
Loading...
