DG Flugzeugbau DG-800A, Руководство по обслуживанию, Страница: 101 / 163

Maintenance Manual DG-808C
Issued: May 2012 TN 800/41 5.2
Datum (BE): Wing leading edge at root rib
Levelling line: Aft fuselage boom slope 1000:37 (tail down)
Moment arms of pilots and equipment see flight manual sect. 6.9
Empty weight C.G. c
After the addition or deletion of equipment or accessories, repairs, painting, or
any change in the aircraft that could influence the weight and balance; a new
weight and balance must be carried out. Aircraft certified as Standard Category
must have the weight and balance carried out by a licensed Airframe Mechanic.
Empty weight C.G. range is determined by reference to the diagram in sect.
6.8.7 of the flight manual.
If the C.G. is out of limits, adjustments may be made by ballasting or by
relocating equipment or accessories.
The result has to be entered in the flight manual section 6.8.6 and in the aircraft
logs. If the min. cockpit load has changed, the new value is to be entered in the
cockpit placard.
Weight and balance must be carried out at least every four years.
C.G. shift due to extension of the engine
see flight manual section 6.9
b
x
W2
pattern 1000:37
W
BE