ATEC Atec Wheelchair ATEC 212 SOLO ROTAX 912 UL 사용자 설명서

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9.1. 
Introduction 
 
The weight, useful weight and centre of gravity information is described in this chapter. 
 
9.2. 
Empty Weight 
 
The weight of aircraft full equipped, without fuel and pilot. It is weighed as a total weight of 
all wheels weights.  
The empty weight of the ATEC 212 SOLO including ROTAX 912 UL 80 HP and standard 
equipment with / without rescue system is  
 
……………………………… kg 
 
9.3. 
Maximum take-off weight 
 
300 
315  kg 
 
Never exceed the maximum take-off weight  
 
9.4. 
Centre of gravity range 
 
The aircraft CG  including the pilot of 75 kg without fuel is  
 
32,6 % of MAC 
 
 The flight range of CG specified by manufacturer is  
 
28 – 36% of MAC 
 
Operation over this range is prohibited