European Academy of Parachute Rigging e.V - Luitpoldstr. 30 - D87700 Memmingen - Germany. Under approval of EPTA European Paraglider Testlaboratory ...
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 in a steeply banked turn - 4.4.9 Sink rate after two turns
Dive forward angle on exit Cascade occurs Entry Recovery Dive forward angle on exit Cascade occurs
Flight Test-Report
accelerated
Entry Recovery
trim speed
10. Symmetric front collapse - 4.4.10 Rocking back less than 45°
A
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 A
30° - 60° Keeping course No Rocking back less than 45°
B A A A
Spontaneous in less than 3 sec 0° - 30° No
Keeping course
A A
Rev. 1.0
Spontaneous in less than 3 sec 30° - 60° No
Keeping course
B A
Stand - 01.12.2008 Seite 1
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
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° - 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
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
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
B
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° Yes, no turn reversal No No
A C A A
12. High angle of attack recovery - 4.4.12
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
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 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
Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
< 90°
90° - 180°
accelerated, max 50% collapse
Re-inflation behavior
90° - 180°
accelerated, max 75% collapse
Change of course until re-inflation
trim speed, max 50% collapse
14. Asymmetric collapse (trim speed) - 4.4.14
90° - 180°
Dive or roll angle
Dive or roll angle
Dive or roll angle
Dive or roll angle
0° - 15°
15° - 45°
15° - 45°
15° - 45°
Dive or roll angle
Dive or roll angle
Dive or roll angle
Dive or roll angle
15° - 45°
45° - 60°
15° - 45°
45° - 60°
B
C
B
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
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
Entry procedure
Special device required
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 less than 3 sec
A
A
0° bis 30°
A
Entry procedure
Special device required
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 less than 3 sec
A
A
0° bis 30°
A
Stable flight
A
Stable flight
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
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
Flight Test-Report
Rev. 1.0
Stand - 01.12.2008 Seite 2
22. Behaviour exiting a steep spiral - 4.4.22 Tendency to return to straight flight
Spontaneous exit
A
Spontaneous exit
A
Turn angle to recover normal flight
Less than 720°, spontaneous recovery
A
Less than 720°, spontaneous recovery
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 - 4.4.23
24. Any other flight procedure and/or configuration described in the user's manual - 4.4.24 Procedure works as descibed Procedure suitable for novice pilots Cascade occurs
NA NA NA
NA NA NA
25. Remarks of testpilot: 0 0 0 0 0
Copyright Ralf Antz 2009
Flight Test-Report
0 0 0 0 0
This Flight Test Report was generated automatically and is valid without signature
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