Aerospool WT-9 Dynamic - Page 14

WT-9 Dynamic Club S FLIGHT MANUAL Section 2 Page 2-5
2.7 Weight
Empty weight - with fixed undercarriage …..……...334,1 kg
Maximum take-off weight....……...............……. 472,5 kg
Maximum landing weight ……................……… 472,5 kg
Useful load ………........................................……138,4 kg
Maximum fuel weight ……............................…….... 91 kg
Maximum weight in Baggage Compartment…...... 10 kg
WARNING
Maintain maximum take off weight 472,5 kg
Depending on different countries rules
2.8 Centre of gravity
Position of C.G.:
Empty airplane.....................................12 ± 2% MAC
Position of C.G. in flight…..................20 ÷ 30% MAC
Rear centre of gravity limit is valid for en-route weight at maximum crew weight.
Forward centre of gravity limit is valid for minimum pilot weight and minimum
capacity of the fuel tanks.
Example to check the centre of gravity position is in Sect. 6.
2.9 Approved manoeuvres
WT-9 Dynamic Club S is certified in the Normal Category – Ultralight airplane. The
following manoeuvres are permited:
− Steep turns with the angle of bank up to 60°
°°
° - appropriate entry speed is 140 km/h.
− Lazy eighths - appropriate entry speed is 140 km/h.
− Combat turns - appropriate entry speed is 200 km/h.
Date: 15.1.2007 / Rev.: 4
„Appr“
WARNING
A flight shall not be commenced until the pilot-in-
command
is satisfied that the mass of the airplane and centre of
gravity location are such that the flight can be conducted
safely!
WARNING
Aerobatic manoeuvres and intentional spins are prohibited!