2008, october, 17
2-5 Weight and balance
2-5.1 Empty weight
Basic empty weight (kg)
Max. empty weight (kg)
X-air Hanuman Jabiru SP
276
284
X-air Hanuman Jabiru AP
289
306,5
X-air Hanuman 602T SP
263
281
X-air Hanuman 602T AP
276
303,5
X-air Hanuman 912 AP
296
306,5
X-air Hanuman 912 SP
280
284
X-air Hanuman 912S AP
296
305,5
X-air Hanuman 912S SP
284
284
2-5.2 Maximum weight at take-off
Like any aircraft, an ultralight has a maximum take off weight. This must never be
exceeded.
Maximum take off weights:
450 kg for the versions without parachute
472,5 kg for the versions with parachute
The builder will in no circumstances be held liable should these weight limitations be
exceeded whatever the origin or nature of the additional or accessory equipment carried on
the aircraft.
This manual includes all the information required for the use and maintenance of the
aircraft.
This manual is specific to the aircraft it describes, and must be read by all users, as stated
in Parts 1and 2 of June 17, 1986 ruling.
2-5.3 Balance
Calculation method of C. of G.:
Aircraft must be horizontal
Weighing operation must be made with three similar weighing machine located each under
each wheel of the plane
acceptable limit of C G = between 22 to 40,5mm forward from reference point
Reference point : axel of the base tube
Weight ( kg )
Front wheel
A
Main gear : left wheel
B
Main gear : right wheel
C
150 x A
CG = ------------- = ………..
(A+B+C)
Summary of Contents for X-AIR HANUMAN 602T AP
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