Garmin Cessna Caravan G1000, Дополнение к руководству

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 22 of 65
2.5 ENGINE INSTRUMENT MARKINGS
Engine instrument markings and their color code significance are shown in the
table below.
NOTE
When an indication lies in the upper or lower prohibited range, the legend for
that display will change to the color of the prohibited range and will flash.
Indication
Red arc or
bar
=
Lower
prohibited
range
Yellow
arc or
bar
=
Caution
range
Green arc
or bar
=
Normal
operating
range
Yellow
arc or bar
=
Caution
range
Red arc or
bar
=
Upper
prohibited
range
Manifold
Pressure
In. – Hg
*Note 2*
-- -- 13 – 30 -- --
RPM -- --
500 –
2700
--
>2700
*Note 3*
Oil Temp
°
F
-- -- 149 – 230 231 - 245 >245
Cylinder Head
Temp
°
F
-- -- 150 – 475
476 –
500
>500
Fuel Press PSI
(DA 40)
*
Note 4 *
0 – 14 -- 14 – 35 -- >35
Oil Press
PSI
0 – 25 25 - 55 56 – 95 96 - 97 >97
Fuel flow
Gal/hr
-- -- 1 – 20 -- >20
Voltage
Volts
0 – 24.1 24.1 – 25 25.1 – 30 30.1 – 32 >32
Amperage
Amps
-- -- 2 – 75 -- --
Fuel quantity
US gal
Standard
Tanks
0 -- <0 – 17 -- --
Fuel quantity
US gal
Long Range
Tanks
0 --
<0 – 16
19 – 24
-- --