Page 8-4
Initial issue
Parking
It is advisable to park the aircraft inside a hangar or eventually inside a weather-proof space with stable temperature,
good ventilation, low humidity and a dust-free environment. The parking place should be protected against possible
damage caused by sun radiation, humidity and wind. Sunbeams reflected through the canopy can generate spot
heating and damage the cockpit area and the upholstery (Fig. 8-1).
For short term parking, the aircraft must be orientated in headwind direction, the parking brake must be engaged, the
wing flaps must be in the retracted position, pitch trim fully forward and the wheels must be chocked.
For extended and unattended parking, as well as in unpredictable wind conditions, in areas where a danger of
propwash from another aircraft or helicopter is present, the aircraft must be tied down to the ground or placed in a
hangar.
For parking, head the aircraft into the wind if possible.
WARNING
Parking the aircraft with canopy open and tail directed towards
the sun can cause damage in the cockpit area!
a.
Wing flaps
Check
FLAPS 0
b.
MASTER SWITCH
ON
c.
TRIM
Fully forward
d.
MASTER SWITCH
OFF
e.
IGNITION
Check OFF both circuits
f.
BRAKE
PARK
g.
Canopy
Close, lock and cover with the cloth dust-cover, as necessary
h.
Tie-down
As required (see Chapter 8.2.3)
Fig. 8-1 Canopy sunbeams reflection
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...