C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight ... Easy rising, ... C. 6. Pitch stability operating controls during accelerated flight - 4.4.6.
1. Inflation / take-off - 4.4.1 Easy rising, some pilot correction is required No
A
Easy rising, some pilot correction is 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
25 km/h to 30 km/h
B
25 km/h to 30 km/h
B
Rising behavior Special take off technique required
B
B 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
C
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° 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 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
0° - 30° Entering a turn of less than 90° 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° No
B A
0° - 30° No
A A
50cm - 65cm
Increasing
50cm - 65cm
C
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°
Entering a turn of less than 90°
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
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:
EAPR-GS-411/15
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
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
15° - 45°
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
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
15° - 45°
15° - 45°
Dive or roll angle
Dive or roll angle
45° - 60°
15° - 45°
C
A
C
< 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
180° - 360°
Dive or roll angle
15° - 45°
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
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 90° to 180°
C
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 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
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
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 Recovery through pilot action in less than a further 3 sec 0° - 30°
A
Stable flight
A
B
Spontaneous in 3 to 5 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
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
Dive forward angle on exit. B. B. A. A. A. C. Dive forward angle on exit. B. D. A. A. B. B. A. A. A. A. Spontaneous ... Easy rising, some pilot correction is required.
Pitch stability operating controls during accelerated flight - 4.1.6. Spontaneous exit .... Any other flight procedure and/or configuration described in the user's manual - 4.1.24. No. Yes. A. No. 0. 0. 0. seY ces 02 ni elbaveihca nrut °081. A.
FTR - Flight Test Report. Dieser Prüfbericht darf ohne schriftliche Zustimmung der EAPR nicht, auch nicht auszugsweise, vervielfältigt werden. Anselm Rauh.
993-391-Pica-L. Achensee. EAPR GmbH - Marktstr. 11. D-87730 Bad Grönenbach - Germany. Maximum take off weight. 95 kg. Type testing No. Max. weight in ...
serial number. Chili 4 S. Pilot's take off weight. 2. Landing - 4.4.2. EAPR leicht. EAPR-Testequipment. Less than 25 km/h. Special landing technique required.
Dec 9, 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 .... Spontaneous in 3 to 5 sec. A. 0° bis 30°. A. Spontaneous in less than 3 sec.
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.
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 ...
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.
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 ...
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°.
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 ...
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.
