C. C. Dive forward angle on exit. B. B. A. A. Location. Achensee. FTR - Flight Test Report. Dieser Prüfbericht ... Smooth, easy and constant rising. Rising behavior.
2. Landing - 4.1.2 Special landing technique required 3. Speeds in straight flight - 4.1.3
4. Control movement - 4.1.4 Max. weight in flight up to 80kg
-
-
Max. weight in flight 80 to 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
More than 14m/s
B
More than 14m/s
B
Increasing
Max. weight in flight greater than 100kg
50cm - 65cm
A
>65 cm
5. Pitch stability exiting accelerated flight - 4.1.5 Dive forward less than 30° No
Dive forward angle on exit Collapse occurs
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
Rocking back less than 45°
A
Rocking back less than 45°
A
Spontaneous in less than 3 sec
A
Spontaneous in 3 to 5 sec
B
0° - 30° Keeping course No Rocking back greater than 45°
A A C
Entering a turn of less than 90° 30° - 60° No Rocking back greater than 45°
B A C
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
30° - 60° No
B A
30° - 60° No
B A
Keeping course
Entering a turn of less than 90°
11. Exiting deep stall (parachutal stall) - 4.1.11
Flight Test Report -
Musterprüfnummer:
Seite 1 von 3
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
60° - 90° No collapse No Less than 45° Most lines tight
C A A A A
A
< 90°
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°
Dive or roll angle
15° - 45°
Dive or roll angle
A
15° - 45°
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° No No No
A A A A
Less than 360° No No No
A A A A
C
< 90°
A
Spontaneous re-inflation
A
A A A A
Less than 360° No No No
A A A A
C
180° - 360°
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
180° - 360°
90° - 180°
Dive or roll angle
Dive or roll angle
15° - 45°
45° - 60°
Spontaneous re-inflation Less than 360° No No No 180° - 360°
Dive or roll angle
15° - 45°
Dive or roll angle
Dive or roll angle
Dive or roll angle
C
45° - 60°
A
15° - 45°
C
45° - 60°
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
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 90° to 180°
C
Stops spinning in 90° to 180°
C
Cascade occurs
No
A
No
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 Change of course before release
NA
NA
Behaviour before release
NA
NA
Recovery
NA
NA
Dive forward angle on exit Cascade occurs
NA NA
NA NA
20. Big ears - 4.1.20 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 3 to 5 sec
B
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
A
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
Stable flight
A
Stable flight
A
Recovery Dive forward angle on exit 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
B
B A
22. Behaviour exiting a steep spiral - 4.1.22
Flight Test Report -
Musterprüfnummer:
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
