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12

> flying in turbulence

Only an experienced and proficient pilot should ever fly in any kind of turbulent condi-
tions. The pilot has to fly ‘actively’ (to maintain correct air speed and glider attitude) in
effect ‘absorbing’ turbulence with the controls and weight shift to keep the glider over-
head and help prevent any deflations and always to be extremely careful not to stall the
wing, through bad pilot input or use of motor, especially through overuse of thrust and/or
the controls.

Always remember that by applying thrust this pushes the pilot forwards relative to the
wing, increasing the angle of attack and wing loading, at least momentarily. This in effect
shortens the available brake travel (speed range) of the glider, making it stall at a higher
brake position. For this reason, under power it is not recommended to use more than 70%
of the brake travel and to generally use less brake than you would when not under thrust,
especially as you increase power. If the pilot encounters an area of turbulence just as
they apply power (they are pushed forward by the power of the engine and the angle of
attack of the wing therefore increases), one should be extremely careful as the control
and flight behaviour of the wing is very different whilst under power.

In turbulent conditions, it is possible for your wing to suffer from either an “asymmetric”
or “symmetric” collapse. Also known as “tucks”, these are described 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 of a part of the wing (say
20 – 70%) which is normally caused by turbulence (although it is also possible to indu-
ce collapses through poor pilot input). In un-powered flight, any tucks or collapses on
the Kinetik should sort themselves out automatically within 90 degrees. If you have a
collapse whilst under power, you should always ease off the thrust gradually, as the
thrust of the motor can considerably complicate the wing’s reactions and recovery beha-
viour. In any case, the pilot should know how to first prevent and, failing this, to deal
with, an asymmetric collapse. They should also be familiar with the required recovery
procedures and techniques to return the glider to normal flight, with the minimum loss
of height or directional control.

If you have an asymmetric collapse, remember: “Course, then Correction”. First try to
maintain a SAFE course, WITHOUT STALLING THE WING BY OVER-CORRECTING, by first
weight shift towards the (still inflated) flying side of the wing (this will give a better wing
loading and augment the internal pressure of the wing) and apply around 20-40% brake
on the open side of the wing to try to minimise the turn induced by the collapse.
Remember that you should have gradually reduced the power of the engine.

BE CAREFUL when trying to stop the turn of the glider after a collapse not to use too
much brake and so stall the flying part of the wing, as this could cause more problems

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...

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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...

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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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