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When accelerating the wing, the profile becomes more sensitive to 
turbulence and closer to a possible frontal collapse. If a loss in internal 
wing pressure is felt, tension on the speed-bar should be reduced to a 
minimum and a slight pull on the brake lines is recommended to increase 
the wing’s incidence angle. Remember to re-establish the air speed after 
correcting the angle of attack.

It is NOT recommended to accelerate near obstacles or in very turbulent 
conditions. If necessary, constantly adjust the movements and pressure 
on the speed-bar whilst doing the same to the brake lines. This balance is 
considered to be ‘active piloting’.

4.4 FLYING WITHOUT BRAKE LINES

If, for any reason at all, the PEAK 5’s brake lines become disabled in 
flight, it will become necessary to pilot the wing with the C-risers and 
weight shifting until landing. These risers steer easily because are not 
under significant tension. You will have to be careful and not handle them 
too heavily in case this causes a stall or negative spin.  The wing must 
be flown at full speed (not accelerated) during the landing approach, and 
the C-risers will have to be pulled symmetrically all the way down shortly 
before contact with 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 FLIG

The best way to avoid knots and tangles is to thoroughly inspect the lines as 
part of a systematic pre-flight check. If a knot is spotted during the take off 
phase, immediately abort the launch sequence and stop.

If inadvertently taking off with a knotted line, the glider drift will need to be 
compensated by weight-shifting to the opposite side  and applying a slight 
brake pull to that side. Gently pull the brake line to see if the knot can be 
undone or try to locate the problem line. Try pulling it to see if the knot can 

be undone. Beware of trying to clear a knotted line or untangle a line in flight 
when close to the terrain. If the knot is too tight and cannot be undone, 
carefully and safely fly to the nearest landing zone. Be careful: do not pull too 
hard on the brake handles because there will be an increased risk of stalling 
the wing or entering a negative spin. Before attempting to clear a knot, make 
sure there are no other pilots flying in the vicinity.

5. LOSING ALTITUDE

Knowledge of different descent techniques could become vital in 
certain situations. The most suitable descent method will depend on the 
particular situation.

To become familiar with the manoeuvres described below, we 
recommend practising within the environment of a licensed training outfit.

5.1 BIG EARS

The “Big ears” is a moderate descent technique, able to increase the sink 
rate to –3 or –4 m/s and reduces the ground speed by 3 to 5 km/h. The 
angle of attack and effective wing-loading will also increase due to the 
smaller surface area of the wing.

Standard technique

To perform the ‘Big ears’ manoeuvre, take the outermost line on each 
A-riser and simultaneously, smoothly pull them outward and downward. 
The wingtips will fold in. 
To re-establish forward speed and the correct angle of attack, accelerate 
once the ears are pulled. 
Keep the ears pulled in until you have lost the desired altitude.
Let go of the lines to re-inflate the tips automatically. If they do not, try 
progressively pulling one brake then the other. We recommend inflating 
the wing tips asymmetrically, without major change to the angle of 
attack, especially when flying near the ground or flying in turbulence.

Содержание PEAK 5

Страница 1: ...PEAK 5 User s manual...

Страница 2: ...glider and will soon discover the meaning of our motto The importance of small details This is the user manual and we recommend you read it carefully The NIVIUK Gliders Team USER S MANUAL NIVIUK Glid...

Страница 3: ...0 3 7 PACKING 10 4 IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 10 4 3 ACCELERATED FLIGHT 13 4 4 FLYING WITHOUT BRAKE LINES 13 4 5 KNOT S IN FLIGHT 13 5 LOSING ALTITUD 13 5 1 B...

Страница 4: ...ents of the test pilot The report contains all the necessary information on how the paraglider reacts during each of the tested manoeuvres It is important to note that different size wings will react...

Страница 5: ...TNT a revolutionary technique using titanium Using Nitinol in the internal construction provides a more uniform profile and reduces the weight to gain efficiency in flight Nitinol provides the highes...

Страница 6: ...ine diameter has been calculated depending on the workload and aims to achieve the required best performance with the least drag The sheath protects the line cores from UV rays and abrasions The lines...

Страница 7: ...IKS or carabiners are properly fastened and securely locked PLEASE NOTE The PEAK 5 features risers of different lengths Size 21 uses risers of unequal lengths In all other models the risers are equal...

Страница 8: ...will fly at maximum speed but the glide will be adversely affected Released speed bar the A and B risers are aligned Full speed bar Size 21 13 cm Sizes 22 24 and 26 14 cm Please note The use of the s...

Страница 9: ...is advisable to fly with the original setting for a period of time to get used to the actual behaviour of the PEAK 5 In case it is necessary to modify the brake length loosen the knot slide the line...

Страница 10: ...ect the integrity of the wing over time Make sure the reinforcements are not bent or folded It should not be folded too tightly to avoid damage to the cloth and or lines At Niviuk we have designed the...

Страница 11: ...g light brake pressure to that side if necessary Normally the collapsed side of the wing should then recover and reopen by itself If it does not try to weight shift towards the collapsed side If this...

Страница 12: ...handles down to bring the wing back up and release them immediately while the glider is still in transition to reposition itself overhead Cravat A cravat may happen after an asymmetric collapse when...

Страница 13: ...ed by weight shifting to the opposite side and applying a slight brake pull to that side Gently pull the brake line to see if the knot can be undone or try to locate the problem line Try pulling it to...

Страница 14: ...ears This new rapid descent technique was first discovered by our Niviuk team pilots in 2009 while flying a competition prototype wing which because of its line plan and high aspect ratio would not al...

Страница 15: ...ly experience an asymmetrical acceleration and dive depending on how the manoeuvre was carried out Practise these manoeuvres at sufficient altitude and carefully 5 5 SLOW DESCENT TECHNIQUE This techni...

Страница 16: ...f your wing is wet from contact with water place it in a dry area air it and keep it away from direct sunlight Direct sunlight may damage the wing s materials and cause premature aging After landing d...

Страница 17: ...d from another wing of the same type Each trim setting is individual to each wing and is determined after measurements and subsequent analysis by specialist personnel Trim adjustments must be within 1...

Страница 18: ...tification The following are not considered to be modifications a replacement of damaged parts b trim correction c repairs d partial or total line replacement The above must all be carried out accordi...

Страница 19: ...0 211 2 1 3 2 1 3 2 1 3 2 1 3 2 1 A A B A A B A A B A A B mm 130 140 140 140 Kg 70 85 80 98 92 110 105 125 Kg 5 5 3 5 5 5 8 D D D D 10 TECHNICAL DATA 10 1 TECHNICAL DATA 20 CELLS Number ASPECT RATIO F...

Страница 20: ...OS GMHB GERMANY UPPER CASCADES DC 35 LIROS GMHB GERMANY UPPER CASCADES A 8000 U 50 EDELRID GERMANY UPPER CASCADES A 8000 U 70 EDELRID GERMANY MIDDLE CASCADES DC 35 LIROS GMHB GERMANY MIDDLE CASCADES A...

Страница 21: ...10 3 RISERS PLAN 22...

Страница 22: ...10 4 SUSPENSION PLAN 23...

Страница 23: ...00 500 360 405 500 A B C D BR 1 7238 7203 7223 7309 7562 2 7145 7107 7111 7197 7301 3 7120 7082 7088 7173 7194 4 7149 7115 7146 7224 7242 5 7055 7022 7024 7091 7054 6 6923 6892 6897 6959 6863 7 6848 6...

Страница 24: ...00 500 360 405 500 A B C D BR 1 8067 8030 8052 8147 8490 2 7966 7926 7931 8027 8201 3 7941 7901 7909 8003 8083 4 7977 7942 7976 8063 8139 5 7874 7839 7843 7918 7931 6 7731 7697 7704 7773 7719 7 7648 7...

Страница 25: ...C 5 A 6 A 7 A 8 A 9 D 10 D 11 A 12 A 13 A 14 D 15 A 16 A 17 A 18 B 19 0 20 A 21 A 22 A 23 0 Classification D In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1611 2019...

Страница 26: ...B 4 C 5 A 6 A 7 A 8 A 9 D 10 D 11 A 12 A 13 C 14 D 15 A 16 A 17 A 18 B 19 0 20 B 21 B 22 A 23 0 Classification D In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1673 2...

Страница 27: ...niviuk com...

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