499-Independence-Geronimo 2 L 29 OG Anselm-UG95kg-MKm
2. 2. B. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique required. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A.
1. Inflation / take-off - 4.4.1 Smooth, easy and constant rising, no pilot correction required No
A
Smooth, easy and constant rising, no pilot correction required No
No
A
No
A
Trim speed more than 30km/h
Yes
A
Yes
A
Speed range using the controls larger than 10km/h
Yes
A
Yes
A
Minimum speed
Less than 25 km/h
A
Less than 25 km/h
A
Rising behavior Special take off technique required
A
A A
2. Landing - 4.4.2 Special landing technique required 3. Speeds in straight flight - 4.4.3
4. Control movement - 4.4.4 Max. weight in flight up to 80kg
-
-
Max. weight in flight 80 to 100kg
-
-
Max. weight in flight greater than 100kg
A
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
No immediate reaction Spontaneous exit Less than 720°, spontaneous recovery
B A A
Immediate reduction of rate in turn Spontaneous exit Less than 720°, spontaneous recovery
A 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 less than 3 sec
A
0° - 30° Entering a turn of less than 90° No Rocking back less than 45°
A A A
0° - 30° Keeping course No Rocking back less than 45°
A A A
Spontaneous in 3 to 5 sec
B
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
0° - 30° Keeping course No Rocking back less than 45°
A A A
Spontaneous in 3 to 5 sec
B
Spontaneous in less than 3 sec
A
30° - 60° No
B A
0° - 30° No
A A
>65 cm
Increasing
>65 cm
A
5. Pitch stability exiting accelerated flight - 4.4.5 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°
Keeping course
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
0° - 30° Changing course less than 45° No
A A A
Flight Test Report -
Musterprüfnummer:
EAPR-GS-0499/16
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
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
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°
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
0° - 15°
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°
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
15° - 45°
0° - 15°
B
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°
Dive or roll angle
15° - 45°
Dive or roll angle
15° - 45°
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
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
30° - 60° No
A A
0° - 30° 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
Special device required
A
Behaviour during big ears
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
B
B
Dive forward angle on exit
0° - 30°
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
Entry procedure
Standard technique
A
Special device required
A
Behaviour during big ears
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
A
B
A
A
21. Big Ears in accelerated flight - 4.4.21
A
0° - 30°
A
Stable flight Recovery through pilot action in less than a further 3 sec 0° bis 30°
Stable flight
A
Stable flight
A
180° turn achievable in 20 sec
Yes
A
Yes
A
Stall or spin occurs
No
A
No
A
Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears
A
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
Anne-Roger, b = 23 juillet 1743, m 30 juin 1767, à Joseph BERNIER. LACHAPELLE (7), Madeleine. [JEAN-BTE. 1676. 1763, (11 avril) Montréal. I. AMAURY (8) ...
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 ...
Dove compare questo simbolo esiste un elevato grado di pericolo e rischio per. I'incolumitä dell'operatore 0 altre persone. Ulilizzare tutle le precauzioni e ca ...
T. I. 3. 3. 0 .7. 7. R. D. 18.38. 333.71. 333.71. 290.72. LOT B. LOT C. DANA. PM 107/48. LOT E. L=383.32. P. O. U. R. R. O. Y. POURRO. Y. L= 14 .71. 3.92 AC.
il fut détruit lors de la prise de Jérusalem par les Babyloniens. 2è temple. 1ère phase : Le temple de Zorobabel (construit lors du retour des juifs de la captivité en ...
4.78 AC NT. 19.93 AC NT. 10.18 AC GR. 4.78 AC NT. 4.50 AC NT. 2.31 AC NT. PAR 3. PAR 4. 18.57 AC NT. 19.46 AC M/L. 18.33. 21.15. 30'. 30'. 6. 6. 1 .7. 1. 6.
Aug 15, 2009 - Summary of knowledge on Bradyporus dasypus (Illiger, 1800) .... (Buda Hills) at the end of the nineteenth century, but seems to have disappeared ... The first adults appear in early May, after 6 moults and can live up to Sep-.
Udarbejdet af: Lea Mariane Bang Nielsen, Mathilde Søndergaard Nielsen, Rikke Holm Berg, Signe Jæger Nielsen og Sisse ... Nogle er tydeligere end andre.
Place one cork square on each side of lavatory inside pedestal ring . 2. Measure .... Instructions pour I'installation Lavabo-Piédestal Untés. #22-504 ... Mettre un carré de liège de chaque côté du lavabo à l´intérieur du cercle de la colonne. 2.
Place one cork square on each side of lavatory inside pedestal ring . 2. Measure from floor for placement of top of hanger.(see drawing for specific pedestal.
portion of trap to tail piece). 7. Rehang lavatory, level and install anchor screws in holes provided at back of lavatory. 8. Install anchor screws in pedestal to floor.
du maintien de la paix et de la s6curitd internationales,. R6affirman! Ie r61e crucial et la responsabilit6 primordiare de l,organisation des Nations Unies dans le domaine du d6sarmement,. Reconnaissant qurune paix authentique et durable ne pourra 6t
Document 29. Pourquoi je suis ... Document additionnel. (1867 à nos ... Source: Marcel CHAPUT, Pourquoi je suis séparatiste, Montréal, Éditions du Jour, 1961.
communiquées la veille de la compétition, avant le début des poules, il est possible, pour compléter le tableau des 64, de permettre la qualification des tireurs qui sont classés après les poules de qualification du premier jour. Il n'y aura pas véri
Tartar of salmon and avocado, lime and coriander. Mozzarella, pea, broad bean, mint and lemon. Asparagus, poached duck egg, butter sauce. Grilled lambs ...