100 kg. 128 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.
Smooth, easy and constant rising, no pilot correction required
A
Smooth, easy and constant rising, no pilot correction required
A
Special take off technique required
No
A
No
A
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
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 720° to 1080°, spontaneous recovery
B A B
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° Keeping course No Rocking back less than 45°
A A A
30° - 60° Keeping course No Rocking back less than 45°
B A A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
0° - 30° Keeping course 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 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 -
Musterprüfnummer:
EAPR-GS-0577/17
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
15° - 45°
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
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
0° - 30° 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 Recovery through pilot action in less than a further 3 sec 0° - 30°
A B
B
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
Entry procedure
Standard technique
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 B
B
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
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
A
A
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
A
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
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.
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.
Feb 11, 2015 - 105 kg. 129 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.
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.
Villleneuve. Glider model. Optic 22. Classification. B. Trimmer no. Test pilot Fukuoka Seiko. Dupont Philippe. Harness Sup'Air - Altiplume S. Sup' Air - Access S.
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.
A. 3. Speed in straight flight. A. Trim speed more than 30 km/h. Yes. A Yes. A. Speed range using the controls larger than 10 km/h. Yes. A Yes. A. Minimum speed.
no. Test pilot Thurnheer Claude. Berruex Gilles. Harness Niviuk Gliders - Hamak M. Gin Gliders - Gingo 2 L. Total weight in flight (kg) 110. 140. Flight test report: ...
A No. A. Cascade occurs. No. A No. A. With 50% collapse and accelerator. Change of course until re-inflation / Maximum dive forward or roll angle not available.
Classification. C. Trimmer no. Test pilot Thurnheer Claude. Zoller Alain. Harness Niviuk Gliders - Hamak 2 light Sup'Air - Altiplume L. Total weight in flight (kg) 75.
Inflation/Take-off. A. Rising behaviour. Smooth, easy and constant rising A Smooth, easy and constant rising. A. Special take off technique required. No. A No. A.
Minimum speed. Less than 25 km/h. A Less than 25 km/h. A. 4. Control movement. A. Max. weight in flight up to 80 kg. Symmetric control pressure / travel.
Sep 20, 2016 - 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off ... Atmus 2 L. Pilot's take off weight ... 0° bis 30°. A.
Oct 7, 2016 - 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Landing - 4.4.2. EAPR .... 0° bis 30°.
2. Landing - 4.4.2. EAPR-Testequipment. Eapr-Test Equipment. Testpilot ... 0° bis 30°. A. Spontaneous in less than 3 sec. Unstable flight. A. A. Most lines tight.
Jul 19, 2016 - 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Landing - 4.4.2 ... 0° bis 30°. A.
2. 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight .... 0° bis 30°. Special device required. Behaviour during big ears. Behaviour ...
Nov 29, 2016 - 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Landing - 4.4.2. EAPR- ... 0° bis 30°. A.
2. 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight .... Stable flight. A. 0° bis 30°. Standard technique. Behaviour during big ears.
Sep 30, 2016 - 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Landing - 4.4.2 .... 0° bis 30°. Standard ...
I elected to use the cool calm air of the following morning for the test flight, spending the remaining part of the day on some runway runs. The first thing I noticed, ...
Flight test report: PG_0704.2013 / page 1 of 3. 1. Inflation/Take-off. A. Rising behaviour. Smooth, easy and constant rising A Smooth, easy and constant rising. A.