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speed of rotation and descent with small changes of interior and exterior brake, and
more or less weight shift. It is possible to achieve descent rates of 10-15m/s or more in
this manoeuvre.

It is dangerous to induce spiral dives close to the ground due to the extreme centrifugal
forces which can cause fainting and, in some cases, blackouts or blurred vision..If you are
at all susceptible to any of these conditions, or are feeling at all unwell for any reason,
then you should not induce a spiral dive for this reason.

The exit from this manoeuvre should be performed gradually and progressively, finishing
in a nice controlled gentle turn to re-stabilise the wing. To do this, the pilot has to gra-
dually ease off the inside brake, and reduce weight shift, then gently apply a little out-
side brake to ease the glider out of the spiral. The pilot must be very careful not to exit
a spiral (especially if well developed) too briskly, as this could result in a steep climb out
(with the wing far behind the pilot and in a very vulnerable position, with little internal
pressure, no airspeed and prone to collapses) followed by a sharp dive which may need
damping to prevent a collapse.

It is NOT recommended to induce a spiral dive at the same time as applying any thrust
or power from the engine, as this could result in instability.

-- b-line stall

To induce a ‘B-line” stall, first take hold of both ‘B’ risers (left and right) one
in each hand (left and right respectively) FIRMLY at the maillons. Then, pull the
B-risers down together to approximately the level of the karabiners, BEING
VERY CAREFUL TO DO THIS SYMMETRICALLY so as to not induce a spin. This will
“B-stall” the glider, by deforming the aerofoil section of the wing in such a way
as to stop the airflow going over it as normal, effectively ‘breaking’ the aero-
foil effect. If done correctly, the glider will now enter into a “B-line stall”,
which is a kind of “parachutal” stall, stopping the glider flying and rendering
one’s trajectory effectively straight down through the air (BUT DRIFTING WITH
THE WIND). Once in the “B-line” stall one can control the descent rate to a
degree by pulling down more or less on the B-risers and it is possible (in still
air) to achieve descent rates from 5-11 m/s. BE CAREFUL, AS PULLING DOWN
TOO FAR ON THE B-LINES CAN CAUSE THE GLIDER TO BECOME UNSTABLE, SO
THIS SHOULD BE AVOIDED.

To exit from the B-line stall correctly, and minimise the chance of any instabi-
lity, the pilot should keep a firm hold of the B-risers and raise them until there
remains 10cm of travel of the B-risers and then release them completely,
taking care to do this SIMULTANEOUSLY. If the B-line is entered, or released,
asymmetrically, it is possible to enter a spin, and so this should always be avoi-
ded. Once the B-risers have been released in the correct manner the glider will
return to normal flight spontaneously with a small dive as it regains “healthy”
airspeed.

Summary of Contents for Kinetik 25

Page 1: ...K I N E T I K m a n u a l...

Page 2: ......

Page 3: ...3 Windtech w w w w i n d t e c h e s K I N E T I K 2 5 2 7 3 0 flight manual...

Page 4: ...n and take off 10 flying in turbulence 12 asymmetrical tuck collapse 12 front symmetrical tuck collapse 13 asymmetric stall spin 13 landing 14 weather to fly 14 emergency procedures quick descent tech...

Page 5: ...arefully read this manual in order to be aware of any limitations performances take off and flight characteristics landing procedures emergency situation and maintenance We always appreciate your feed...

Page 6: ...ng conditions so that you know when it is safe to fly and WHEN IT IS NOT SAFE TO FLY This manual cannot be used for operational purposes The flight log registration card must be filled and stamped by...

Page 7: ...or riser system to help overcome the various complexities that powered flight entails The risers are shorter than usual 42cm to allow for the different flying position and help minimise the effects of...

Page 8: ...ing trim position the actual speed will depend a lot on wing loading in which the trimmers are set to compen sate for the pitching back effect caused by the push of the motor bringing the wing into a...

Page 9: ...t is above the stipulated weight range this will result in a higher minimum speed and faster landing speed and the stall speed of the glider will also be higher powered flight The concept of performan...

Page 10: ...isers acce lerator throttle in one s hand etc makes this usually the most difficult part of a para motoring flight One has to bear in mind that a failed launch could result in the lines getting caught...

Page 11: ...rachute make sure that this is also correctly set up and that nothing will either cause your parachute to deploy accidentally or prevent it from deplo ying correctly should you need to do so in an eme...

Page 12: ...d in the following paragraphs along with a description of what to expect and the recovery techniques recommended asymmetrical tuck collapse An asymmetric collapse is a longitudinal lengthwise collapse...

Page 13: ...it is best to make sure that the trim mers are in the normal position as it is clear that you are flying in a turbulent area asymmetric stall spin It is extremely difficult to accidentally provoke a...

Page 14: ...eed being care ful to fly actively in case of turbulence and in some cases you may have to keep some brake pressure to give a more positive angle of attack and therefore reduce the chance of a collaps...

Page 15: ...symmetrically You should be applying NO brake as you could stall the wing in this way Steering is done by weigh shift To recover release the outer A lines the KINETIK will return to normal flight The...

Page 16: ...line stall first take hold of both B risers left and right one in each hand left and right respectively FIRMLY at the maillons Then pull the B risers down together to approximately the level of the k...

Page 17: ...ll bottom lines This is very important to maintain the flying and safety characteristics of the wing The rest of the lines must also be checked and change them if they have deteriorated Test some of t...

Page 18: ...18...

Page 19: ...kg Weight in fly kg Certification D H V Standard Risers Certification CEN Paramotor Risers 25 25 85 22 8 11 52 9 55 5 13 4 2 82 0 63 52 6 94 6 47 52 72 70 120 1 2 paramotor 27 27 6 24 3 11 9 9 86 5 13...

Page 20: ...20...

Page 21: ...63 5 65 72 216 5 134 209 134 62 5 62 5 63 504 5 61 209 470 212 5 67 5 134 134 67 61 60 209 502 212 5 212 5 212 5 209 492 5 209 209 502 5 216 5 219 3 4 5 6 8 7 9 10 13 209 488 209 213 496 5 209 212 14...

Page 22: ...68 5 60 134 5 60 207 5 200 200 200 64 5 128 128 60 58 60 203 5 57 128 64 128 480 5 58 54 186 5 466 5 200 200 208 5 200 471 203 5 481 203 5 207 207 5 475 4 5 203 5 6 7 8 9 11 10 18 200 190 5 203 5 203...

Page 23: ...58 58 58 124 467 5 56 5 193 5 455 197 62 5 124 124 56 5 62 55 5 193 5 465 197 197 197 193 5 456 193 5 193 5 465 5 201 202 3 4 5 6 8 7 9 10 14 193 5 452 193 5 197 460 193 5 196 15 184 5 193 5 451 476 5...

Page 24: ...24 flight log size date site duration flight details K K I I N N E E T T I I K K...

Page 25: ......

Page 26: ...POWERED BY WINDTECH francisco rodr guez 7 33201 g i j n spain p o box 269 33280 p 34 985 357 696 fax 34 985 340 778 email info windtech es web www windtech es K I N E T I K...

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