AirDesign Volt 2-XS-OG-MK75kg_Sepp-UG60kgm - Para2000
C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Smooth, easy and constant rising, no pilot correction ...
No immediate reaction Spontaneous exit Less than 720°, spontaneous recovery
B 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 3 to 5 sec
B
0° - 30° Entering a turn of less than 90° No Rocking back less than 45°
A A A
30° - 60° Entering a turn of less than 90° No Rocking back less than 45°
B A A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
30° - 60° Entering a turn of less than 90° No Rocking back less than 45°
B A A
30° - 60° Entering a turn of less than 90° 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
C 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
Entering a turn of less than 90°
Entering a turn of 90° to 180°
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
Flight Test Report -
Musterprüfnummer:
EAPR-GS-0503/16
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
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
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° - 180°
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
15° - 45°
Dive or roll angle
15° - 45°
B
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
90° - 180°
90° - 180°
Dive or roll angle
Dive or roll angle
15° - 45°
15° - 45°
Dive or roll angle
Dive or roll angle
45° - 60°
15° - 45°
C
B
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
90° - 180°
Dive or roll angle
45° - 60°
Dive or roll angle
45° - 60°
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
25% to 50% of the symmetric control travel
C
25% to 50% of the symmetric control travel
C
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
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
Standard technique
A
Standard technique
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
A
Spontaneous in 3 to 5 sec
A
Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears
0° - 30°
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
21. Big Ears in accelerated flight - 4.4.21
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
on digital logic cards eliminating the distribution problems association with single-point regulation The devices are available in two standard transistor packages ...
A separate opcode (refer to Table 5-3 on page 10 for a complete list) is ...... All dimensions and tolerance conform to ASME Y 14.5M, 1994. 2. The surface finish ...
Description ... grammed, as well as reading or writing a continuous data stream. ... To allow for simple in-system reprogrammability, the AT45DB041B does not require ...... intellectual property right is granted by this document or in connection with
chiffre d'affaires de 2 434 keuros sur 9 mois (+110%). Villepinte, le 12 octobre 2015 â DRONE VOLT, leader français du drone professionnel, annonce le ...
answers to most electrical trouble- ... a wire as a water hose, there is pressure .... There are some simple resistance checks that you can perform to check the.
of 200 mA if adequate heat sinking is provided With the. TO-3 power package the available output current is greater than 1A. The regulators are essentially ...
fonctionnement, de la performance, des pièces, accessoires ou service, composez le ...... le protecteur en fil métallique situé sur la bouche d'évacuation. 2.
all threaded joints to protect against leakage. 5. Storage tank ... The pump motor is equipped with thermal overload protection. If .... O-Ring Gasket (-218). 1.
launch characteristics of the glider. The line .... As this is not a training manual we will not try to teach you launching techniques. ... The ZEFIRA has very good launch behaviour in no wind conditions. ..... then inflated with air for a flotation
1. Owner's Manual and Service Booklet. Serial Number: ... may be changed without prior notice. No part of these documents may be copied or transmitted for any purpose in any manner or by any means .... Speed system . ...... the very high standards we
Ill-adjusted steering lines may cause you to misinterpret the canopy's ..... PVC tube rigid plastic rod. The most soft handle is obtained when no insertion is used.