Page 4-14
Initial issue
4.9
Before Takeoff
Before takeoff the engine should be properly warmed. The engine oil temperature must reach min.
50 °C.
Then
the ignition and engine ground tests may be performed as follows:
Ignition and Engine Ground Tests
a.
CARBUR. PREHEATING
Check
CLOSED
b.
Brake
MAX
Ignition and engine ground tests:
c.
THROTTLE
4000 rpm
d.
IGNITION
Switch OFF first ignition circuit, then back ON;
Switch OFF second ignition circuit, then back ON;
Engine speed drop with only one ignition circuit must not exceed 300 rpm;
Max. difference of engine speed by use of either circuit A or B is 115 rpm
e.
THROTTLE
Short MAX
f.
Engine speed
Check, 52
00 rpm ±200 rpm
g.
Engine parameters
Check
h.
CARBUR. PREHEATING
OPEN, check carburetor preheating function (engine speed drop min. 100 rpm);
Then CLOSE
i.
THROTTLE
IDLE, check min. 1400 rpm
WARNING
Before engine full-power ground test ensure that the propeller
area is clear!
WARNING
Position the aircraft so that the prop wash will not hurt any
persons, or cause any damage! Never perform a ground test
against any buildings or obstacles!
CAUTION
The engine full-power ground test should be performed
with the aircraft heading upwind. Do not perform the engine
full-power ground test on a gravel surface. The propeller may
sucks the gravel and damage the blades!
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...