Flight test report for paraglider Amicus 27 - Skyman
85 kg. 105 kg. 1. 1. 1. A. 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
Immediate reduction of rate in turn Spontaneous exit Less than 720°, spontaneous recovery
A A A
Immediate reduction of rate in turn Spontaneous exit Less than 720°, spontaneous recovery
A A A
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
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
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
0° - 30° No
A 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
Entering a turn of less than 90°
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-0415/15
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
0° - 30° No collapse No Less than 45° Most lines tight
A 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
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
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°
< 90°
Dive or roll angle
Dive or roll angle
15° - 45°
15° - 45°
Dive or roll angle
Dive or roll angle
15° - 45°
0° - 15°
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°
Dive or roll angle
15° - 45°
Dive or roll angle
15° - 45°
A
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
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
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
Jun 25, 2015 - 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. A. A. A. A. A. A.
102 kg. 124 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.
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. A. A. A. A. A. A. A. A. A. A.
Sep 14, 2007 - A Yes. A. Minimum speed. Less than 25 km/h. A Less than 25 km/h. A. 4. Control movement. Max. weight in flight up to 80 kg. Symmetric control ...
Flight test report: PG_0645.2012 / page 1 of 3. 1. Inflation/Take-off. A. Rising behaviour. Smooth, easy and constant rising A Smooth, easy and constant rising. A.
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.
Apr 18, 2007 - Sink rate after two turns. Up to 12m/s. A More than 14 m/s. B. 10. Symmetric front collapse. Entry. Rocking back less than 45°. A Rocking back ...
Oct 10, 2016 - C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off ... Smooth, easy and constant rising, no pilot ...
Oct 11, 2016 - 2. 3. 3. C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off ... Landing - 4.4.2. EAPR- ... 0° bis 30°. A.
Spontaneous in less than 3 sec. 25 km/h to 30 km/h. Special landing technique required. Speed range using the controls larger than 10km/h. Smooth, easy and ...
Nov 8, 2006 - 89259-700 Jaraguà do Sul, S.C. Brasil. Representive None. Classification B. Type of glider Prymus 2 S. Trimmer not available. Test Pilot Seiko ...
Nov 8, 2006 - Rua Walter Marquardt, 1180 cp 370. Place of test. Villeneuve. 89259-700 Jaraguà do Sul, S.C. Brasil. Representive None. Classification B.
B. Sink rate after two turns. Up to 12 m/s. A More than 14 m/s. B. 10. Symmetric front collapse. A. Entry. Rocking back less than 45°. A Rocking back less than 45°.
Date of flight test. 24. 04. 2009. Representative None. Place of test. Villeneuve. Glider model. Sprint S. Classification. B. Trimmer no. Test pilot Thurnheer Claude.
Special take off technique required. No. A No. A. 2. Landing. A. Special landing technique required. No. A No. A. 3. Speed in straight flight. A. Trim speed more ...
86-031 Osielsko. Poland. Date of flight test. 02. 12. ... Niviuk Gliders - Hamak 2 M. Total weight in flight (kg) 70. 95 ... 12 m/s to 14 m/s. A More than 14 m/s. B. 10.
Flight test report: PG_0351.2010 / page 1 of 3. 1. Inflation/Take-off. A. Rising behaviour. Smooth, easy and constant rising A Smooth, easy and constant rising. A.
Flight test report: EN. Manufacturer. Niviuk Gliders / Air Games. S.L.. Certification number. PG_0491.2011. Address. C. Del Ter, 6 â Nave D. 17165 La Cellera de ...
25. 04. 2008. Representative Alloix Pierre-Yves. Place of test. Villeneuve. Glider model. Magic 5 M. Classification. D. Trimmer no. Test pilot Thurnheer Claude.
Symmetric control pressure / travel not available. 0 not available. 0. 5. Pitch stability exiting accelerated flight. A. Dive forward angle on exit not available. 0.
May 30, 2007 - Total weight in flight 65 kg. 85 kg. Min weight. Max weight. 1. Inflation/Take-off. Rising behaviour. Smooth, easy and constant rising. A Smooth ...
