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a variety of different materials. A correct folding method is very important 
to extend the useful life of your paraglider. It should be concertina-packed, 
with the leading edge reinforcements flat and the Nitinol flexible rods 
stacked up on top of each other. This method will keep the profile in its 
original shape and protect the integrity of the wing over time.

The wing should then be folded in three sections while taking care of not 
to bend or twist the SLE. There is no need for compression during the 
procedure; doing so may damage the fabric, including the risers and lines.

4. IN FLIGHT

4.1 FLYING IN TURBULENCE

The IKUMA P has an excellent profile design made to withstand various 
weather conditions, hence enabling the pilot to take advantage of its 
stability for greater piloting efficiency. It behaves impeccably in passive 
flight mode, thus offering a high level of safety in turbulent conditions. 
Nonetheless, the pilot always has to fly according to the prevailing 
weather conditions, and the pilot is the ultimate safety factor.

We recommend that the pilot to anticipate every move, understands the 
air mass and flies actively to make appropriate corrections with the right 
input amount. Over-steering is dangerous, all actions must be undertaken 
in a timely manner, amplitude and duration. The ultimate piloting goal 
is to keep the speed of the glider going. AIR SPEED = SAFETY. Do not 
hesitate to ask questions and get advice from qualify certified personnel 
if in doubt.

4.2 POSSIBLE CONFIGURATIONS

To become familiar with manoeuvres described below, we recommend 
practising within the environment of a competent training company

Asymmetric collapse

In spite of the IKUMA P’s profile stability, strong turbulent air may cause 
the wing to collapse asymmetrically if the pilot was unable to predict 
the glider’s reactions in specific circumstances. When the wing is about 
to experience an asymmetric collapse, the brake lines will slacken and 
transmit a tension loss affecting the harness stability. To prevent the 
collapse from happening, pull the toggle corresponding to the affected 
side of the wing. It will increase the incidence of the wing (angle of attack). 
If the collapse does happen, the IKUMA P will not react violently, the 
turning tendency is gradual and easily controlled. Weight-shift toward 
the flying and opposite side of the collapse to keep the wing  flying 
straight while applying a light brake pressure to that side if necessary, 
to slow it down. The collapsed side of the wing should then recover and 
reopen by itself. If it does not, then pull the brake toggle on the collapsed 
side decisively and quickly all the way down before bringing it back up 
immediately. You may have to repeat this pumping action to provoke the 
re-opening of the deflated glider side. Do not over-brake or slow down 
the flying side of the wing (the causes the risk of a stall for having too high 
an angle of attack). Once the collapsed side is open, re-centre your body 
under the wing to regain the default flying speed.

Frontal collapse

In normal flying conditions and due to the IKUMA P design, asymmetrical 
collapses are unlikely to take place. The wing’s profile has great buffering 
abilities when dealing with extreme incidence changes. A frontal collapse 
may occur in strong turbulent conditions, entering or exiting powerful 
thermals or when lacking experience using the accelerator/ speed-bar 
with untimely inadequate input. Frontal collapses usually re-inflate without 
the glider turning, but a symmetrically applied quick braking action with a 
quick deep pump will accelerate the re-inflation if necessary. Release the 
brake lines immediately to return to default glider air speed.

Negative spin

A negative spin does not conform to the IKUMA P’s normal flight 
behaviour. Certain circumstances however, may provoke this configuration 

Summary of Contents for IKUMA P

Page 1: ...USER MANUAL IKUMA P...

Page 2: ...o off the beaten track even before taking off Reduced weight and volume mean you can take this new Easy Performance wing wherever you want to go We are confident that you will enjoy flying this wing a...

Page 3: ...8 3 7 FOLDING INSTRUCTIONS 9 4 IN FLIGHT 9 4 1 FLYING IN TURBULENCE 9 4 2 POSSIBLE CONFIGURATIONS 9 4 3 USING THE ACCELERATOR 11 4 4 FLYING WITHOUT BRAKE LINES 11 4 5 LINE KNOT S IN FLIGHT 11 5 LOSING...

Page 4: ...eful information to the pilot it situates itself into the centre of the thermal or it follows the ascending air flow Its air intakes have been replaced so the application of the RAM Air Intake turns t...

Page 5: ...d The IKS1000 is designed and dimensioned as a connection system between the risers and the lines It has a breaking load of 1055 kg which greatly exceeds that of the classic 3mm 550 kg maillon but wit...

Page 6: ...Niviuk Gliders go through an extremely thorough and efficient final inspection Every line is checked and measured once the final assembly is concluded Each wing is then individually inflated for the...

Page 7: ...ruction manual and the certification test report outlining the chest strap length adjustments used during these tests 2 5 SPEED SYSTEM ASSEMBLY The acceleration mechanism of the IKUMA P works when you...

Page 8: ...wing fully open the lines untangled and properly laid out on the ground to ensure that all is in working order Be certain the weather conditions are suited for your flying skill level 3 5 WING INFLATI...

Page 9: ...r s reactions in specific circumstances When the wing is about to experience an asymmetric collapse the brake lines will slacken and transmit a tension loss affecting the harness stability To prevent...

Page 10: ...urned to its default overhead flying location To resume normal flight conditions progressively and symmetrically release the brake line tension to regain air speed When the wing reaches the overhead p...

Page 11: ...ith the ground This braking method is not as effective as using the brake lines and hence the wing will land with a higher ground speed 4 5 LINE KNOT S IN FLIGHT The best way to avoid knots and tangle...

Page 12: ...f the wing can easily be maintained by weight shifting the harness exactly the same as you would with big ears We recommend the application of the speed bar whilst using this technique To exit the man...

Page 13: ...eleration and dive depending on how the manoeuvre was carried out Practise these movements at sufficient altitude and with moderation 5 5 SLOW DESCENT TECHNIQUE This technique allows descent without s...

Page 14: ...should while still conforming to the certification criteria 7 4 REPAIRS If the wing is damaged you can temporarily repair it by using the ripstop material found in the repair kit so long as no stitche...

Page 15: ...15 liability coverage is for its product line only Niviuk cannot be held responsible for your actions Fly at your own risk...

Page 16: ...6 4 26 4 26 4 26 FLATTENING 15 15 15 15 CORD MAXIMUM m 2 33 2 44 2 52 2 62 MINIMUM m 0 54 0 56 0 58 0 61 AVERAGE m 1 92 2 01 2 07 2 16 LINES TOTAL METERS m 220 230 238 247 HEIGHT m 6 67 6 98 7 2 7 49...

Page 17: ...RON D P GERMANY RIB REINFORCEMENT LTN 0 8 STICK SPORTWARE CO CHINA THREAD SERAFIL 60 AMAN GERMANY SUSPENSION LINES FABRIC CODE SUPPLIER UPPER CASCADES DC 040 LIROS GMHB GERMANY UPPER CASCADES DC 060 L...

Page 18: ...18 10 3 RISERS LAYOUT...

Page 19: ...19 10 4 LINE PLAN...

Page 20: ...6186 10 5535 5471 5496 6145 11 5364 5353 5381 RISERS LENGTH m m A B B C 480 480 480 480 STANDARD 360 380 400 480 ACCELERATED LINES HEIGHT m m A B C D br 1 6517 6427 6538 6614 7308 2 6397 6309 6379 64...

Page 21: ...6720 10 6013 5943 5970 6678 11 5827 5815 5846 RISERS LENGTH m m A B B C 480 480 480 480 STANDARD 360 380 400 480 ACCELERATED LINES HEIGHT m m A B C D br 1 7039 6943 7062 7146 7880 2 6913 6819 6893 69...

Page 22: ...3 A 4 A 5 A 6 A 7 A 8 A 9 A 10 B 11 A 12 A 13 A 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_1056 2016 Date of issue DMY 13 05...

Page 23: ...46 1 B 2 A 3 A 4 A 5 A 6 A 7 A 8 A 9 A 10 B 11 A 12 A 13 A 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_1058 2016 Date of issu...

Page 24: ...The importance of small details niviuk com...

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