7273-14-15-ITV-Annapurna-L ML - independence paragliding
100 kg. 125 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. A. A. A. B. A. A. A.
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
Spontaneous in 3 to 5 sec 30° - 60° No
Keeping course
B A
Rev. 1.0
Spontaneous in 3 to 5 sec 0° - 30° No
Entering a turn of less than 90°
A A
Stand - 01.12.2008 Seite 1
11. Exiting deep stall (parachutal stall) - 4.4.11 Deep stall achieved
Yes
Recovery
Spontaneous in less than 3 sec
Dive forward angle on exit Change of course Cascade occurs
30° - 60° Changing course less than 45° No
Recovery Cascade occurs
Yes
A
Spontaneous in less than 3 sec
A
B A A
30° - 60° Changing course less than 45° No
B A A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
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
C
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° Yes, no turn reversal No No
A C A A
Less than 360° No No No
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
C
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° Yes, no turn reversal No No
A C 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 50% collapse
Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
trim speed, max 75% collapse
Re-inflation behavior
< 90°
90° - 180°
< 90°
accelerated, max 75% collapse
Change of course until re-inflation
accelerated, 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
15° - 45°
45° - 60°
15° - 45°
45° - 60°
Dive or roll angle
Dive or roll angle
Dive or roll angle
Dive or roll angle
15° - 45°
15° - 45°
15° - 45°
15° - 45°
B
B
B
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
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 less than 90°
A
Cascade occurs
No
A
No
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 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
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
A
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
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
A
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
Stable flight
A
Stable flight
A
20. Big ears - 4.4.20
Recovery Dive forward angle on exit
B
B 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
Flight Test-Report
Rev. 1.0
B
B A
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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No. Entry. Recovery. Cascade occurs. Dive forward angle on exit. Rocking back less than 45° trim s peed. Entry. Cascade occurs. 0° - 30°. Keeping course a cce.
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