Smooth, easy and constant rising. Evaluation. Yes. Minimum take off weight serial number. Sigma 9-29. Schruns. Achensee. Maximum take off weight. Location.
6. Pitch stability operating controls during accelerated flight - 4.1.6 Collapse occurs 7. Roll stability and damping - 4.1.7 Oscillations 8. Stability in gentle spirals - 4.1.8 Tendency to return to straight flight 9. Behaviour in a steeply banked turn - 4.1.9 Sink rate after two turns 10. Symmetric front collapse - 4.1.10 trim speed
Entry Recovery
accelerated
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) - 4.1.11
Flight Test Report -
Musterprüfnummer:
EAPR-GS-0179/14
Seite 1 von 3
Deep stall achieved
Yes
Recovery
Spontaneous in less than 3 sec
A
Yes 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
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
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°
A
Spontaneous re-inflation
A
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
12. High angle of attack recovery - 4.1.12
13. Recovery from a developed full stall - 4.1.13 Dive forward angle on exit Collapse Cascade occurs (other than collapse) Rocking backward Line tension 14. Asymmetric collapse (trim speed) - 4.1.14 trim speed, max 50% collapse
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 Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
accelerated, max 50% collapse
Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
accelerated, max 75% collapse
Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
< 90°
< 90°
< 90°
Dive or roll angle
Dive or roll angle
Dive or roll angle
0° - 15°
15° - 45°
15° - 45°
Spontaneous re-inflation Less than 360° No No No 90° - 180°
Dive or roll angle
15° - 45°
Dive or roll angle
Dive or roll angle
Dive or roll angle
Dive or roll angle
0° - 15°
15° - 45°
15° - 45°
45° - 60°
A
B
A
C
15. Directional control with a maintained asymmetric collapse - 4.1.15 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 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 without straight span
C
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
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
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 - 4.1.16 Spin occurs 17. Low speed spin tendency - 4.1.17 Spin occurs 18. Recovery from a developed spin - 4.1.18
19. B-line-stall - 4.1.19
20. Big ears - 4.1.20
21. Big Ears in accelerated flight - 4.1.21
Recovery Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears 22. Behaviour exiting a steep spiral - 4.1.22
Flight Test Report -
Musterprüfnummer:
EAPR-GS-0179/14
Seite 2 von 3
Tendency to return to straight flight
Spontaneous exit
A
Spontaneous exit
A
Turn angle to recover normal flight
720° to 1080°, spontaneous recovery
C
720° to 1080°, spontaneous recovery
C
180° turn achievable in 20 sec
Yes
A
Yes
A
Stall or spin occurs
No
A
No
A
23. Alternative means of directional control - 4.1.23
24. Any other flight procedure and/or configuration described in the user's manual - 4.1.24 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 2014
Flight Test Report -
0 0 0 0 0
This Flight Test Report was generated automatically and is valid without signature
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