Niviuk ICEPEAK 3 22, Руководство пользователя

Страница: 8 / 22

8
4.2 POssIBle CONFIGUrATIONs
We recommend that training to master these manoeuvres be carried out
under the supervision of a competent school.
Asymmetric collapse
In spite of the high stability of the profile of the ICEPEAK 3, heavy
turbulent conditions may cause part of the wing to collapse asymmetrically.
This usually happens when the pilot has not foreseen this possible reaction
of the wing. When the wing is about to experience an asymmetric collapse
the brake lines and the harness will transmit a loss of pressure to the pilot.
To prevent the collapse from happening, pull the brake line corresponding
to the compromised side of the wing, this will increase the angle of
incidence. If the collapse does happen the ICEPEAK 3 will not react
violently, the turn tendency is very gradual and it is easily controlled. Lean
your body towards the side that is still flying in order to counteract the turn
and maintain a straight course, if necessary slightly slow down the same
side but do not brake it excessively as this may induce a stall. The collapse
will normally open by itself but if that does not happen, pull completely on
the brake line on the side which has collapsed. Do this with a smooth and
firm movement. You may have to repeat this operation to encourage the
re-opening. When the collapse has been solved, remember to allow the wing
recover its flying speed.
Symmetric collapse
In normal flying conditions the design of the ICEPEAK 3 ensures that a
symmetric collapse is quite improbable. The profile of the wing has been
designed to widely tolerate extreme changes in the angle of incidence. A
symmetric collapse may occur in heavy turbulent conditions, on entry or
exit of strong thermals or lack of adapting the use of the accelerator to the
prevailing air conditions. Symmetrical collapses usually re-inflate without
the glider turning but you can symmetrically apply the brake lines with
a quick deep pump to quicken the re-inflation. Release the brake lines
immediately to recover optimum flight speed.
ICePeAK 3 is a competition glider, and as such the brake travel is not
excessive, any reaction to a control input is immediate. Any corrective
action such as pumping the brakes must be carried out quickly so not to
induce a full stall.
Negative spin
This configuration is out of the normal flight behaviour of the iCePeaK 3.
Certain circumstances however, may provoke this configuration such as
trying to turn when the wing is flying at very low speed (while heavily braking).
it is not easy to give any recommendations about this situation since it varies
depending on the circumstances. remember that you should restore the
relative air speed over the wing. To achieve this, progressively reduce the
pressure on the brake lines and let the wing gain speed. The normal reaction
would be a lateral surge with a turn tendency no greater than 360º before
restoring to normal flight conditions.
Parachutal stall
If it does occur, the feeling would be that the wing would not have any
forward motion, you would feel a sense of instability and a lack of pressure
on the brake lines, although the canopy would appear to be correctly
inflated. The correct reaction would be to release the pressure on the brake
lines and push the A lines forward or rather lean your body to any side
WITHOUT PULLING ON THE BRAKE LINES.
Deep stall
The possibility of the ICEPEAK 3 falling into this configuration during
normal flight is very unlikely. This could happen if you are flying at a
very low speed, whilst over steering in a number of manoeuvres and in
turbulent conditions. To provoke a deep stall you have to take the wing
to minimum flight speed by symmetrically pulling the brake lines, when
you reach this point, continue pulling until you reach 100% and then
hold. The glider will first fall behind you and then situate itself above you,
rocking slightly, depending on how the manoeuvre was carried out. When
you start to provoke a stall, be positive and do not doubt an instant. Do
not release the brake lines when half way through the manoeuvre. This