85 kg. 106 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. A. A. A. A. A. A.
1. Inflation / take-off - 4.4.1 Smooth, easy and constant rising, no pilot correction required No
A
Smooth, easy and constant rising, no pilot correction required No
No
A
No
A
Trim speed more than 30km/h
Yes
A
Yes
A
Speed range using the controls larger than 10km/h
Yes
A
Yes
A
Minimum speed
Less than 25 km/h
A
Less than 25 km/h
A
Rising behavior Special take off technique required
A
A A
2. Landing - 4.4.2 Special landing technique required 3. Speeds in straight flight - 4.4.3
4. Control movement - 4.4.4 Max. weight in flight up to 80kg
-
-
Max. weight in flight 80 to 100kg
-
-
Max. weight in flight greater than 100kg
A
Increasing
A A
Dive forward less than 30° No
A A
No
A
No
A
Reducing
A
Reducing
A
Spontaneous exit
A
Spontaneous exit
A
No immediate reaction Spontaneous exit Less than 720°, spontaneous recovery
B A A
No immediate reaction Spontaneous exit 720° to 1080°, spontaneous recovery
B A B
No Rocking back less than 45°
A
No Rocking back less than 45°
A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
0° - 30° Entering a turn of less than 90° No Rocking back less than 45°
A A A
0° - 30° Keeping course No Rocking back less than 45°
A A A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
30° - 60° Keeping course No Rocking back less than 45°
B A A
0° - 30° Keeping course No Rocking back less than 45°
A A A
Spontaneous in less than 3 sec
A
Spontaneous in 3 to 5 sec
B
30° - 60° No
B A
0° - 30° No
A A
>65 cm
Increasing
>65 cm
A
5. Pitch stability exiting accelerated flight - 4.4.5 Dive forward less than 30° No
Dive forward angle on exit Collapse occurs
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
Keeping course
11. Exiting deep stall (parachutal stall) - 4.4.11 Yes
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 -
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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
0° - 30° No collapse No Less than 45° Most lines tight
A 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
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 Dive or roll angle
15° - 45°
Dive or roll angle
0° - 15°
A
B
< 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
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°
A
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
90° - 180°
Dive or roll angle
15° - 45°
Dive or roll angle
15° - 45°
B
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 less than 90°
A
Stops spinning in less than 90°
A
Cascade occurs
No
A
No
A
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 with straight span
A
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Dive forward angle on exit Cascade occurs
30° - 60° No
A A
30° - 60° No
A 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
20. Big ears - 4.4.20 Entry procedure
Standard technique
A
Special device required
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Dive forward angle on exit
0° - 30°
A
0° bis 30°
A
Entry procedure
Standard technique
A
Special device required
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears
0° - 30°
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
21. Big Ears in accelerated flight - 4.4.21
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
12,56. 12,96 aspect ratio. 5,1 projected wing area, sq.m. 15,2. 19,43. 21,11. 22,81. 24,48. 26,16 ... lines, because it might lead to unpredictability in flying and make the paraglider dangerous in ..... Increasing, Greater than 55 cm. A not availabl
When using accelerator you will have a maximum speed of 48 km/h. When you .... Speed range using the controls larger than 10 km/h. Yes .... www.sc.com.ua.
Windtech assumes that the purchasing pilot has the appropriate pilot's licence, has taken a ... This glider has successfully passed the EN shock test with a weight equal to the .... pleasure. With qualified instruction you will actually learn faster,
manual carefully in order to be aware of any general limitations, performance characte- ristics, take off and ... You are the best feedback and support for future products, and please remember that we ... By no means is this a substitute of a trainin
The Atis 2 has been certified in Category B, having met all the requirements ... This Atis 2 is not a beginners paraglider due to its glide ratio of more than 8.5 and ...
tilt and the rotation speed by releasing the external brake. When you need to turn fast, you should swing Mystic-2 in the opposite direction and then pull as hard ...
Dauerhafte Lagerung bei sehr hoher Temperatur (z.B. im Auto im. Hochsommer) ist zu vermeiden. Bei längerer Lagerung sollte der Gleitschirm zudem nicht ...
However we like to mention that we don`t take any liability for possi- ... many happy landings with your U-Turn OBSESSION 2. The Research and Development team at U-Turn can proudly look back at many success- ful years in the ...... descent because a
SOL KANGAROO 2 and wish you many enjoyable hours of flying! If you have any questions, doubts,suggestions or constructive criticism regarding any SOL ...
However we like to mention that we don`t take any liability for possi- ... many happy landings with your U-Turn OBSESSION 2. The Research and Development team at U-Turn can proudly look back at many success- ful years in the ...... descent because a
31. O M E G A 4 2 5 / 2 8. A. 1. A. 2. A. 3. A. 4. A. 5. A. 6. A. 7. A. 11. A. 1. 2. A. 1. 3. A. 1. 4. A. 1. 5. A. 1. 6. A. 1. 7. A. 1. 8. A. 8. A. 9. A. 1. 0. B. 1. B. 2. B. 3. B. 4. B. 5.
You are the best feedback and support for future products, and please ... must be filled and stamped by the dealer & returned to Windtech in order to claim on ... paragliding is a high risk activity-especially without taking the appropriate ... The Z
or near other airspace users. Warning: â¢. Do not use the speed system in any extreme maneuvers. â¢. Be careful! Pic tur e : 1. Speed system. 2. Control Handle. 3.
42. XIV. Contact. 43. XV. Top 5 XC tips. 44. Introduction. Welcome. Welcome to the Triple Seven Team! We are excited that you have chosen to fly the ROOK2, ...
must be filled and stamped by the dealer & returned to Windtech in order to claim on ... paragliding is a high risk activity-especially without taking the appropriate ... Best glide in nil wind, and still air, is obtained at âtrimâ speed- that is
Apr 8, 2003 - The Dragon²'s construction and development. 5. ... It is our pleasure to welcome you to the world of Independence .... The best way to train for.
Nur so haben wir genügend Einfluss auf wichtige Faktoren, wie z.B. auf die ..... Werden im Sackflug die Bremsen betätigt, so geht der Schirm in einen Fullstall über! .... B2 329,9. Liros PPSL 275 yellow. BM1 258,8. Liros PPSL 160 yellow.
Le CESIM (Centre d'Etudes de Sécurité Internationale et de Maîtrise des armements) a été créé ... approches scientifiques pluridisciplinaires et rigoureuses. L'accent est mis ... Département Aires Culturelles et Politiques, Bâtiment Albert Camus ' t.
DOBERMANN 2's characteristics, but it cannot be viewed as an instructional handbook and does not offer the instruction required to pilot this type of wing.