Jan 10, 2014 - 90 kg. 116 kg. 3. 3. 3. C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique required. A. A. A. A. A.
6. Pitch stability operating controls during accelerated flight - 4.4.6 Collapse occurs 7. Roll stability and damping - 4.4.7 Oscillations 8. Stability in gentle spirals - 4.4.8 Tendency to return to straight flight 9. Behaviour exiting a fully developed spiral dive - 4.4.9 Initial response of glider (first 180°) Tendency to return to straight flight Turn angle to recover normal flight 10. Symmetric front collapse - 4.4.10 trim speed ~ 30%
Folding lines used Entry Recovery
trim speed > 50%
Dive forward angle on exit Cascade occurs Entry Recovery
accelerated > 50%
Dive forward angle on exit Cascade occurs Entry Recovery Dive forward angle on exit Cascade occurs
Keeping course
Entering a turn of less than 90°
11. Exiting deep stall (parachutal stall) - 4.4.11 Deep stall achieved
Yes
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Dive forward angle on exit Change of course Cascade occurs
0° - 30° Changing course less than 45° No
A A A
0° - 30° Changing course less than 45° No
A A A
Flight Test Report -
Musterprüfnummer:
Yes
EAPR-GS-0346/15
Seite 1 von 2
12. High angle of attack recovery - 4.4.12 Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Cascade occurs
No
A
No
A
30° - 60° No collapse No Less than 45° Most lines tight
B A A A A
30° - 60° No collapse No Less than 45° Most lines tight
B A A A A
13. Recovery from a developed full stall - 4.4.13 Dive forward angle on exit Collapse Cascade occurs (other than collapse) Rocking backward Line tension 14. Asymmetric collapse (trim speed) - 4.4.14 No
Change of course until re-inflation
< 90°
Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
trim speed, max 75% collapse
Change of course until re-inflation
accelerated, max 50% collapse
Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
accelerated, max 75% collapse
Re-inflation behavior
trim speed, max 50% collapse
Folding lines used
No
A
< 90°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A A
Dive or roll angle
0° - 15°
Dive or roll angle
15° - 45°
A
B
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A A
A
< 90°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A A
90° - 180°
< 90°
Dive or roll angle
Dive or roll angle
15° - 45°
15° - 45°
Dive or roll angle
Dive or roll angle
15° - 45°
15° - 45°
B
A
C
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A A
< 90°
Dive or roll angle
45° - 60°
Dive or roll angle
45° - 60°
C
15. Directional control with a maintained asymmetric collapse - 4.4.15 Able to keep course straight
Yes
A
Yes
A
180° turn away from the collapsed side possible in 10 sec
Yes
A
Yes
A
Amount of control range between turn and stall or spin
More than 50% of the symmetric control travel
A
More than 50% of the symmetric control travel
A
No
A
No
A
No
A
No
A
Spin rotation angle after release
Stops spinning in 90° to 180°
C
Stops spinning in 90° to 180°
C
Cascade occurs
No
A
No
A
16. Trim speed spin tendency - 4.4.16 Spin occurs 17. Low speed spin tendency - 4.4.17 Spin occurs 18. Recovery from a developed spin - 4.4.18
19. B-line-stall - 4.4.19 Change of course before release
Changing course less than 45°
A
Changing course less than 45°
A
Behaviour before release
Remains stable with straight span
A
Remains stable without straight span
C
Recovery
Spontaneous in 3 to 5 sec
B
Spontaneous in less than 3 sec
A
Dive forward angle on exit Cascade occurs
0° - 30° No
A A
30° - 60° No
A A
20. Big ears - 4.4.20 Entry procedure
Special device required
A
Special device required
A
Behaviour during big ears
Stable flight Recovery through pilot action in less than a further 3 sec 0° - 30°
A
Stable flight
A
B
Spontaneous in less than 3 sec
A
A
0° bis 30°
A
Entry procedure
Special device required
A
Special device required
A
Behaviour during big ears
Stable flight Recovery through pilot action in less than a further 3 sec 0° - 30°
A
Stable flight
A
B
Spontaneous in less than 3 sec
A
A
0° bis 30°
A
Stable flight
A
Stable flight
A
180° turn achievable in 20 sec
Yes
A
Yes
A
Stall or spin occurs
No
A
No
A
Recovery Dive forward angle on exit 21. Big Ears in accelerated flight - 4.4.21
Recovery Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears 23. Alternative means of directional control - 4.4.22
23. Any other flight procedure and/or configuration described in the user's manual - 4.4.23
NA NA NA
Procedure works as descibed Procedure suitable for novice pilots Cascade occurs
78 kg. 100 kg. 3. 3. 3. C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique required. A. A. A. A. A. A. B. B. A. A. A.
Flight test report: PG_0844.2014 / page 1 of 3. 1. Inflation/Take-off. A. Rising behaviour. Smooth, easy and constant rising A Smooth, easy and constant rising. A.
The data and statements contained within this manual may be changed without ... part of these documents may be copied or transmitted for any purpose in any .... DESIGN AND CONSTRUCTION. ..... Attaching the tow-line release system . ...... minimise th
full of holes in the process. Besides they exude a dark and strong colourant that ..... mobility of the wing and the ease of learning the basic flight techniques have.
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Extreme flight maneuvers. Behaviors in extreme flying conditions. Although the UP Trango is an extremely stable design, it is possible that it could enter an ...
5.2.1. Big Ears. 5.2.2. B-line Stall. 5.2.3. Spiral Dive. 5.3. SIV manoeuvres ... The Avax XC3 is a high-performance wing, a top 'Serial Class' competition glider, ... This manual provides information which will help you fly safely and keep your wing
and engineering in Pasadena, California, and promptly created ..... A Risers: Red. A3 Risers (for Big .... rucksack, compression bag and -strap, repair materials ...
Cut out this card and mail it to UP within 14 days of purchase, or register your new UP Kibo via www.up-paragliders.com>Service>UP>Product. Registration.
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Full frontal collapse . ..... online via www.up-paragliders.com>service>product registration. Your completed ... your local dealer or feel free to contact us here at UP directly. Have fun with your ... Please read this owner's manual thoroughly .....
If you have any questions regarding your paraglider or auxiliary equipment please ask your local ... and then went on to become fascinated by the emerging ...
Nov 9, 2016 - 90 kg. 116 kg. 2. 2. 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique required. A. A. A. A. A.
0. 5. Pitch stability exiting accelerated flight. A. Dive forward angle on exit. Dive forward less than 30°. A Dive forward less than 30°. A. Collapse occurs. No. A No.
akute Gefahr für die Struktur des UP. Lhotse dar. Allerdings beschleunigen häufige Material-Ãberbelastungen den. Alterungsprozess erheblich. Schirme,.
The data and statements contained within this manual may be changed without prior notice. ...... paragliders characterised by maximum safety, performance and quality in every ... the entire specific and general flying ..... textile industry. .... ext
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The data and statements contained within this manual may be changed ... part of these documents may be copied or transmitted for any purpose in any ...... PACKING AND CHECKING OF THE RESCUE SYSTEM. .... the very high standards we set ourselves. ....
May 7, 2015 - Recovery. Cascade occurs. Rocking back less than 45°. Rocking back less than 45°. Recovery through pilot action in less than a further. 3 sec.
The data and statements contained within this manual may be changed ... part of these documents may be copied or transmitted for any purpose in any ...... across the globe for designing and building the finest paragliders available â ... your local
