Page 2-6
EASA Approved
Initial issue
Power Plant Instrument Markings
Digital power plant instrument SkyView SV D1000 for monitoring of engine parameters complemented with analogue
engine speed indicator and fuel pressure indicator are marked with following color code significance:
Dynon SkyView
SV-D1000
Unit
Red Line
Minimum Limit
Green Arc
Normal Operating
Yellow Arc
Caution Range
Red Line
Maximum Limit
Engine speed
rpm
–
1400
–
5500
0
–
1400
5500
–
5800
5800
Manifold pressure
inHg
–
0.0
–
28.0
28.0
–
29.5
29.5
Coolant temperature
o
C
–
50
–
120
–
120
Oil temperature
o
C
50
90
–
110
50
–
90
110
–
130
130
Oil pressure
bar
0.8
2.0
–
5.0
0.8
–
2.0
5.0
–
7.0
7.0
Exhaust gas
temperature
o
C
–
200
–
880
–
880
Fuel pressure
bar
0.15
0.15
–
0.50
–
0.50
Fuel flow meter
l/h
–
0.0
–
30.0
–
over 30.0
Fuel level
l
0 - 16
16
–
45
45+
–
–
CAUTION
Illumination of the fuel reserve warning lamp signals that
in the appropriate tank is 16 liters / 4.23 U. S. gal of fuel remaining,
of which 3.5 liters / 0.92 U. S. gal is unusable fuel! This fuel is
sufficient for half-hour flight at maximum continuous power!
Taxi Power
Use the minimum power settings for taxiing.
Power settings for taxiing on flat, smooth, hard surfaces is idle (min. 1400 rpm). Power settings for grassy, inclined,
soft surfaces or when start motion is slightly above idle (1400 rpm).
Содержание WT9 Dynamic LSA / Club
Страница 2: ...This page is left blank intentionally...
Страница 4: ...Page B Initial issue This page is left blank intentionally...
Страница 8: ...Page F Initial issue Chapter Page Date Chapter Page Date...
Страница 10: ...Page H Initial issue This page is left blank intentionally...
Страница 20: ...Page 1 4 Initial issue Three View Drawing Fig 1 1 Three view drawing...
Страница 94: ...Page 4 28 Initial issue This page is left blank intentionally...
Страница 109: ...Initial issue EASA Approved Page 5 15 Fig 5 2 Crosswind U S Standard Units...
Страница 110: ...Page 5 16 EASA Approved Initial issue This page is left blank intentionally...
Страница 119: ...Initial issue EASA Approved Page 6 9 Fig 6 2 Operating Weight CG limit Metric Units...
Страница 120: ...Page 6 10 EASA Approved Initial issue Fig 6 3 Operating Weight CG limit U S Standard Units...
Страница 122: ...Page 6 12 EASA Approved Initial issue Fig 6 4 Check of flight weight moment limits Example Metric Units...
Страница 125: ...Initial issue EASA Approved Page 6 15 Fig 6 5 Weights and moments of variable masses chart Metric Units...
Страница 127: ...Initial issue EASA Approved Page 6 17 Fig 6 6 Weights and moments of variable masses chart U S Standard Units...
Страница 134: ...Page 6 24 EASA Approved Initial issue This page is left blank intentionally...
Страница 148: ...Page 7 14 Initial issue Fig 7 5 Arrangement screen 1 Fig 7 6 Arrangement screen 2...
Страница 149: ...Initial issue Page 7 15 Fig 7 7 Arrangement screen 3 Fig 7 8 Arrangement screen 4...
Страница 150: ...Page 7 16 Initial issue Fig 7 9 Arrangement screen 5 Fig 7 10 Arrangement screen 6...
Страница 162: ...Page 7 28 Initial issue Fig 7 16 Arrangement screen 1 Fig 7 17 Arrangement screen 2...
Страница 163: ...Initial issue Page 7 29 Fig 7 18 Arrangement screen 3 Fig 7 19 Arrangement screen 4...
Страница 164: ...Page 7 30 Initial issue Fig 7 20 Arrangement screen 5 Fig 7 21 Arrangement screen 6...
Страница 165: ...Initial issue Page 7 31 Fig 7 22 Arrangement screen 7 Fig 7 23 Arrangement screen 8...
Страница 173: ...Initial issue Page 7 39 Fig 7 29 Air outlets for cockpit venting Fig 7 30 Windshield demist knob...
Страница 178: ...Page 7 44 Initial issue This page is left blank intentionally...
Страница 188: ...Page 8 10 Initial issue Fig 8 5 Fuel draining...
Страница 198: ...Page 8 20 Initial issue This page is left blank intentionally...
Страница 204: ...Page 9 6 Initial issue This page is left blank intentionally...