Landing - 4.4.2. EAPR-Testequipment. EAPR Light. Less than 25 km/h. Special landing technique required. Speed range using the controls larger than 10km/h.
Immediate reduction of rate in turn Spontaneous exit Less than 720°, spontaneous recovery
A A A
No immediate reaction Spontaneous exit Less than 720°, spontaneous recovery
B 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° Entering a turn of less than 90° 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° Keeping course No Rocking back less than 45°
B A A
30° - 60° Keeping course No Rocking back less than 45°
B A A
Spontaneous in less than 3 sec
A
Spontaneous in 3 to 5 sec
B
30° - 60° No
B A
30° - 60° No
B A
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-0501/16
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
0° - 15°
Dive or roll angle
15° - 45°
A
A
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°
< 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
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
Standard technique
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 less than 3 sec
A
A
0° bis 30°
A
Entry procedure
Standard technique
A
Standard technique
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
Recovery Dive forward angle on exit 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
Delta 2 S. Classification. C. Trimmer no. Test pilot Dupont Philippe. Thurnheer Claude ... Smooth, easy and constant rising A Smooth, easy and constant rising. A.
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Delta 2 S. Classification. C. Trimmer no. Test pilot Dupont Philippe. Thurnheer Claude ... Smooth, easy and constant rising A Smooth, easy and constant rising. A.
N. 22-074727.62 C. Eze ear 2. testif. /o A.Y. A 22, 24. eae. A Å¿ea 2. A a/e, A. 6. a 1.27% decea A 27 2. A. 2. %2% A. Z. - 2 -. 2 (26a %2 77 as a 2Z. / at 22 a Å¿at a z. /.
Roll stability and damping. A. Oscillations. Reducing. A Reducing. A. 8. Stability in gentle spirals. A. Tendency to return to straight flight. Spontaneous exit.
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Reichweite Test- und Warnfunktion. ⢠Extrem ...... 33200.1 Joystick, bi-directionally self-neutralizing ..... The built-in range test reduces transmission power to an.
Point(s). La méthode des 2 Point(s) est accessible à toutes et à tous. C'est un instrument de conscience facile à apprendre et à appliquer. Chacun a en soi les ...
Triton 2 S. Pilot's take off weight. 2. Landing - 4.1.2. Minimum speed. Yes. Trim speed more than 30km/h. Academy Test Equipment. EAPR- Testequipment. Yes.
Qar og lain bu lilurauoise. EN certification paragliders hnesses oues para-test.com. FAI Category 1 Cross-Country events. 2015 Edition | Revision 3.5 | 01 Sept ...
In accordance with EN standards 926-2:2005 & 926-1:2006: PG_0645.2012. Date of issue (DMY):. 28. 08. 2013. Manufacturer: Ozone Gliders. Model: Delta 2 ...
probablement que leurs chants et danses estoyent in- vocations du diable, pour ... bras qui se monstroit, en peu d'heures, nous arriverions vers le grand sagamo.
Qar og lain bu lilurauoise. EN certification paragliders hnesses oues para-test.com. FAI Category 1 Cross-Country events. 2015 Edition | Revision 3.5 | 01 Sept ...
Electrical data: Connection connector. Rated Operational Voltage (UB). 24 DC V. Electrical type. DC. Utilization category. DC 13. No-load supply current max.