Initial issue
Page 4-21
Short Field Landing
Landing approach is conducted at a small glide slope angle due to the long distance of the float before touchdown.
a.
Wing flaps
FLAPS 2
, extend gradually, check locked
b.
Airspeed
110
–
115 IAS / 59
–
62 KIAS
c.
TRIM
As required
d.
THROTTLE
IDLE
e.
Flare
Begin approximately 7 - 10 ft / 2 - 3 m above ground
f.
Touchdown
Perform on the main wheels first; the nose wheel should be lowered smoothly
to the runway as airspeed is diminished
g.
Directional control
Maintain with rudder control
h.
Wing flaps
FLAPS 0
i.
Brake
Apply heavily
j.
After landing
Perform according to Chapter 4.16
NOTE
For maximum brake effectiveness, retract the flaps, hold
the control stick full backward and apply max. braking without
skidding.
Soft Field Landing
a.
Wing flaps
FLAPS 2
, extend gradually, check locked
b.
Airspeed
120
–
130 IAS / 65
–
70 KIAS
c.
TRIM
As required
d.
THROTTLE
IDLE
e.
Flare
Begin approximately 7 - 10 ft (2 - 3 m) above ground
f.
Touchdown
Perform as gently as possible on the main wheels first; the nose wheel should be
lowered smoothly to the runway as airspeed is diminished
g.
Directional control
Maintain with rudder control
h.
Brake
Apply gently
i.
After landing
Perform according to Chapter 4.16
Summary of Contents for WT9 Dynamic LSA / Club
Page 2: ...This page is left blank intentionally...
Page 4: ...Page B Initial issue This page is left blank intentionally...
Page 8: ...Page F Initial issue Chapter Page Date Chapter Page Date...
Page 10: ...Page H Initial issue This page is left blank intentionally...
Page 20: ...Page 1 4 Initial issue Three View Drawing Fig 1 1 Three view drawing...
Page 94: ...Page 4 28 Initial issue This page is left blank intentionally...
Page 109: ...Initial issue EASA Approved Page 5 15 Fig 5 2 Crosswind U S Standard Units...
Page 110: ...Page 5 16 EASA Approved Initial issue This page is left blank intentionally...
Page 119: ...Initial issue EASA Approved Page 6 9 Fig 6 2 Operating Weight CG limit Metric Units...
Page 120: ...Page 6 10 EASA Approved Initial issue Fig 6 3 Operating Weight CG limit U S Standard Units...
Page 134: ...Page 6 24 EASA Approved Initial issue This page is left blank intentionally...
Page 148: ...Page 7 14 Initial issue Fig 7 5 Arrangement screen 1 Fig 7 6 Arrangement screen 2...
Page 149: ...Initial issue Page 7 15 Fig 7 7 Arrangement screen 3 Fig 7 8 Arrangement screen 4...
Page 150: ...Page 7 16 Initial issue Fig 7 9 Arrangement screen 5 Fig 7 10 Arrangement screen 6...
Page 162: ...Page 7 28 Initial issue Fig 7 16 Arrangement screen 1 Fig 7 17 Arrangement screen 2...
Page 163: ...Initial issue Page 7 29 Fig 7 18 Arrangement screen 3 Fig 7 19 Arrangement screen 4...
Page 164: ...Page 7 30 Initial issue Fig 7 20 Arrangement screen 5 Fig 7 21 Arrangement screen 6...
Page 165: ...Initial issue Page 7 31 Fig 7 22 Arrangement screen 7 Fig 7 23 Arrangement screen 8...
Page 178: ...Page 7 44 Initial issue This page is left blank intentionally...
Page 188: ...Page 8 10 Initial issue Fig 8 5 Fuel draining...
Page 198: ...Page 8 20 Initial issue This page is left blank intentionally...
Page 204: ...Page 9 6 Initial issue This page is left blank intentionally...