Aeroplanes DAR ltd.
Brief Flight Manual DAR – Solo
Page 4 of 25
LIMITATIONS AND SAFETY INFORMATION
Limitations
DAR Solo is an aircraft that falls in the LTF-UL Category.
It is designed to be used for any maneuvers as:
Normal flying maneuvers;
Stalls (except whip stalls); and
Lazy eights, chandelles, and steep turns, in which the angle
of bank is not more than 60 degrees.
The following limitations are imposed on the speeds and loading
of the airplane:
V
S1
= 55 km/h
V
SF
= 51 km/h
V
NE
= 150 km/h
V
A
=109 km/h
V
F
= 92 km/h
V
FE
=83 km/h
Max Wind Limits = 5 m/s
Engine Limitation = no negative loads more 3 sec
MTOW = 260 kg
Empty Weight = 140 kg
Load Limitation = +4/-2
