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13

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 con-
trol 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 induce
collapses through poor pilot input). In un-powered flight, any tucks or collapses on the

EVO 

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 behaviour. In any
case, and setting timmers to neutral position, 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
than the collapse itself. Once you have maintained a safe course, and minimized the turn
induced by the collapse, you can apply CORRECTION to re-inflate the collapsed side of
the wing by giving smooth but firm pumps on the brake on the collapsed side, holding
down the brake until the glider re-inflates. Do not give small ‘panicky’ dabs of brake to
the collapsed side of the wing as this does not really help and will make the wing take
much longer to re-inflate. Once the wing re-inflates be careful not to hold down the
brake too much, for too long, as this could stall the wing, or induce a spin.

-- front/symmetrical tuck collapse 

SET TRIMMERS TO NEUTRAL POSITION

T

his is when the whole leading edge of the wing, from the centre to the tips, collapses.

It is possible to have a front tuck on exit from a strong thermal, when using the speed
system or trimmers in turbulent conditions, hitting a (wind) shear layer, etc. Generally,
this situation does not require any pilot intervention as the glider will re-inflate quickly,

Summary of Contents for EVO 23

Page 1: ...E V O 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 E V O 2 3 2 5 2 7 3 0 flight manual...

Page 4: ...11 flying in turbulence 12 asymmetrical tuck collapse 13 front symmetrical tuck collapse 13 asymmetric stall spin 14 landing 14 weather to fly 15 emergency procedures quick descent techniques 15 big e...

Page 5: ...ly 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 feedback s...

Page 6: ...lying course and gain a good understanding of the concepts of flight both powered and un pow ered It is also impera tive that you gain a good understanding of the weather and flying conditions so that...

Page 7: ...onger nylon of to prevent airofoil deformation even after several years of intensive use Rib cell wall reinforcements are made of Dacron 310 180 gr Line attachment points are made of polyester lines T...

Page 8: ...cy and stability across the whole speed range When the trimmers are pulled fully ON pulled all the way through the ratchet so that the rear risers are effectively pulled down to their shortest positio...

Page 9: ...stem The following is rough guide line as to how much to apply With around 10 km h of head wind best glide is obtained with 25 accelerator applied With around 15 25 km h of head wind best glide is obt...

Page 10: ...t that the pilot choos es a motor that is most suited to the pilot s weight abilities and intended uses in flight etc When one takes into consideration all of the factors one will arrive at one set of...

Page 11: ...h carefully preparing their equipment and doing all of the required pre flight checks using a clear and complete checklist Always allow ample security margins to make room for any error especially dur...

Page 12: ...y overhead in the correct flying position a quick BUT THOROUGH visual check to make 100 sure that everything is in order ensuring that the wing lines risers etc are all in perfect order before committ...

Page 13: ...f 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 flyi...

Page 14: ...stall rotating back wards negative whilst the still flying outside wing rotates forwards positive around the pilot In this case to return to normal flight the pilot has to raise the inside brake to r...

Page 15: ...walls of the glid er in this way weather to fly SET TRIMMERS TO NEUTRAL POSITION If in doubt about the weather and flying conditions do not launch Before going flying you should check the weather fore...

Page 16: ...he accelerator as well one gets a very good descent rate whilst keeping an acceptable speed spiral dive SET TRIMMERS TO NEUTRAL POSITION The Spiral Dive is obtained by maintaining the glider in a stee...

Page 17: ...IFTING WITH THE WIND Once in the B line stall one can con trol 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...

Page 18: ...The rest of the lines must also be checked and change them if they have deteriorated Test some of the lines that are not changed for minimum 40 of the rated strength If the line fails you should repla...

Page 19: ...ly kg Certification EN Paramotor Risers 25 25 85 22 8 11 52 9 55 5 13 4 2 82 0 63 52 6 94 52 72 70 130 paramotor 27 27 6 24 3 11 9 9 86 5 13 4 2 91 0 65 52 7 17 67 87 85 145 paramotor 30 30 15 26 6 12...

Page 20: ...20...

Page 21: ...ed Fast flight in smooth air A 43 cm B 43 cm C 43 cm D 43 cm A 34 cm B 36 5 cm C 43 cm D 43 cm A 43 cm B 43 cm C 52 cm D 60 cm A 34 cm B 36 5 cm C 52 cm D 60 cm B A A C D C B A A D C D A A B C B A A D...

Page 22: ...194 187 56 56 56 451 5 54 187 439 5 190 60 5 54 60 53 187 449 190 190 190 187 440 5 187 187 450 194 195 3 4 5 6 8 7 9 10 14 187 436 187 190 444 187 189 5 15 187 187 435 441 5 187 16 17 177 5 19 18 13...

Page 23: ...201 194 124 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 19...

Page 24: ...00 200 200 64 5 128 128 60 58 60 203 5 57 5 128 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 5 202 5 200 465 5 178...

Page 25: ...09 134 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 15 198 199 209 487 513...

Page 26: ...26 flight log s si iz ze e d da at te e s si it te e d du ur ra at ti io on n f fl li ig gh ht t d de et ta ai il ls s E V O...

Page 27: ......

Page 28: ...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 E V O...

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