h3. *Proposal From:*
Vladimir Silhan, Czech delegate
h3. *Proposal title:*
DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT
h3. *Existing text:*
*1.3 DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT*
1.3.1 A one or two seat powered aircraft whose minimum speed at Maximum Take Off Weight (MTOW) is less than 65 km/h, and having a MTOW of:
\- 300 kg for a landplane flown solo
\- 330 kg for an amphibian or a pure seaplane flown solo;
\- 450 kg for a landplane flown with two persons
\- 495 kg for an amphibian or a pure seaplane flown with two persons
_Note. These definitions also apply to foot-launched Microlight and Paramotor aircraft._
1.3.2 The MTOW described in 1.3.1 may be increased by 5% if the aircraft is equipped with a parachute system designed to bring the entire aircraft to the ground if it is deployed.
h3. *New text:*
{panel}
*1.3 DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT*
1.3.1 A one or two seat powered aircraft whose minimum speed at Maximum Take Off Weight (MTOW) is less than 65 km/h, and having a MTOW of:
\- 300 kg for a landplane -flown solo- {color:#ff0000}built and equipped for one pilot only{color}
\- 330 kg for an amphibian or a pure seaplane -flown solo- {color:#ff0000}built and equipped for one pilot only{color} ;
\- 450 kg for a landplane -flown with - {color:#ff0000}built and equipped for{color} two persons
\- 495 kg for an amphibian or a pure seaplane -flown with- {color:#ff0000}built and equipped for{color} {color:#000000}two{color} persons
_Note. These definitions also apply to foot-launched Microlight and Paramotor aircraft._
1.3.2 The MTOW described in 1.3.1 may be increased by 5% if the aircraft is equipped with a parachute system designed to bring the entire aircraft to the ground if it is deployed.
{panel}
h3. *Reason:*
Two-seater flown in solo isn’t one-seater.
Vladimir Silhan, Czech delegate
h3. *Proposal title:*
DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT
h3. *Existing text:*
*1.3 DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT*
1.3.1 A one or two seat powered aircraft whose minimum speed at Maximum Take Off Weight (MTOW) is less than 65 km/h, and having a MTOW of:
\- 300 kg for a landplane flown solo
\- 330 kg for an amphibian or a pure seaplane flown solo;
\- 450 kg for a landplane flown with two persons
\- 495 kg for an amphibian or a pure seaplane flown with two persons
_Note. These definitions also apply to foot-launched Microlight and Paramotor aircraft._
1.3.2 The MTOW described in 1.3.1 may be increased by 5% if the aircraft is equipped with a parachute system designed to bring the entire aircraft to the ground if it is deployed.
h3. *New text:*
{panel}
*1.3 DEFINITION OF A MICROLIGHT OR PARAMOTOR AIRCRAFT*
1.3.1 A one or two seat powered aircraft whose minimum speed at Maximum Take Off Weight (MTOW) is less than 65 km/h, and having a MTOW of:
\- 300 kg for a landplane -flown solo- {color:#ff0000}built and equipped for one pilot only{color}
\- 330 kg for an amphibian or a pure seaplane -flown solo- {color:#ff0000}built and equipped for one pilot only{color} ;
\- 450 kg for a landplane -flown with - {color:#ff0000}built and equipped for{color} two persons
\- 495 kg for an amphibian or a pure seaplane -flown with- {color:#ff0000}built and equipped for{color} {color:#000000}two{color} persons
_Note. These definitions also apply to foot-launched Microlight and Paramotor aircraft._
1.3.2 The MTOW described in 1.3.1 may be increased by 5% if the aircraft is equipped with a parachute system designed to bring the entire aircraft to the ground if it is deployed.
{panel}
h3. *Reason:*
Two-seater flown in solo isn’t one-seater.