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.
Immediate reduction of rate in turn Spontaneous exit 720° to 1080°, spontaneous recovery
A A B
Immediate reduction of rate in turn Spontaneous exit 720° to 1080°, spontaneous recovery
A A B
No Rocking back less than 45°
A
No Rocking back less than 45°
A
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
0° - 30° Entering a turn of less than 90° No Rocking back less than 45°
A A A
Keeping course 0° - 30° No Rocking back less than 45°
A A A
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
30° - 60° Entering a turn of less than 90° No Rocking back less than 45°
B A A
0° - 30° Entering a turn of less than 90° No Rocking back greater than 45°
A A C
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
30° - 60° No
C A
0° - 30° No
A A
Dive forward less than 30° No
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
Entering a turn of 90° to 180°
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
30° - 60° Changing course less than 45° No
B A A
30° - 60° Changing course less than 45° No
B A A
Flight Test Report -
Musterprüfnummer:
Yes
EAPR-GS-0378/15
Seite 1 von 2
12. High angle of attack recovery - 4.4.12 Recovery
Spontaneous in 3 to 5 sec
C
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
15° - 45°
Dive or roll angle
0° - 15°
A
C
< 90°
Inflates in less than 3 sec from start of pilot action
C
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A 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
90° - 180°
90° - 180°
Dive or roll angle
Dive or roll angle
45° - 60°
15° - 45°
Dive or roll angle
Dive or roll angle
45° - 60°
15° - 45°
C
A
C
< 90°
Inflates in less than 3 sec from start of pilot action
C
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
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
25% to 50% of the symmetric control travel
C
25% to 50% of the symmetric control travel
C
No
A
No
A
No
A
No
A
Spin rotation angle after release
Stops spinning in less than 90°
A
Stops spinning in 90° to 180°
C
Cascade occurs
No
A
No
A
Change of course before release
Changing course 45° or more
C
Changing course less than 45°
A
Behaviour before release
Remains stable without straight span
C
Remains stable without straight span
C
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
0° - 30° 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
Recovery
Spontaneous in 3 to 5 sec
B
B
Dive forward angle on exit
0° - 30°
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
A
A
21. Big Ears in accelerated flight - 4.4.21 Entry procedure
Standard technique
A
Special device required
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
A
Spontaneous in 3 to 5 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
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
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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.
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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.
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.
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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 ... 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
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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.
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