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航空機 Air Creation iFun XLのPDF パイロット・オペレーション・ハンドブックをオンラインで閲覧またはダウンロードできます。Air Creation iFun XL 18 ページ。

5.3

Flight Specifications

5.3.1

This wing is not designed for aerobatics.

It is imperative to respect the flight envelope !



Maximum Pitch attitudes 30° nose up, 30° nose down



Maximum Bank angle 60°



Aerobatics and deliberate spinning prohibited



V.N.E. (never to be exceeded): 81 mph (130 km/h)



Acceleration limits +4/-0g ; positive "g" at all times



Stalls authorized only in glide path with a progressive speed reduction

and throttle to idle position.

The instructions in paragraph 5.3.3 concerning stall exercises must be

followed.

Over these limits, stability problems, structural failure or irreversible "tumbling"

motions may occur.

Ideal handling will only be reached after about 10 flight hours and roll control will be

stiffer during the first flights.

5.3.2

Control bar:

Pushing the control bar forward causes the wing to pitch its nose up, which increases the

angle of attack (causing the aircraft to climb) – primary effect, and a decrease in air speed

– secondary effect.

Roll control is effected from lateral movement of the control frame, and follows weight

shift convention, i.e. bar right, aircraft rolls to the left.

A separate yaw control is not provided. Like other weight shift aircraft, yaw is provided

from the secondary effect of banking.

GDMUiFXL-evo-1G

Warning:

Version 0010