Aircraft

Falcon-XP, 2-seat, tandem, land

Solo flight from front seat only.

 

Empty XP Center of Gravity Location

(inches aft of datum, “0” butt line canard Pin nose of fuselage)

Empty XP maximum weight           500lbs

Center of gravity location               101.5 inches

 

Maximum Forward Center of Gravity

(C of G location at gross max. wt. aircraft will maintain flight at minimum design IAS)

Front pilot maximum weight                            200lbs

Rear crew member maximum weight             210lbs

Fuel weight (at station 120)                              90lbs

XP empty weight maximum                             500lbs

maximum gross weight                                     1,000lbs

Center of gravity                                                 89.in (86.in with out fuel)

 

Maximum Aft Center of Gravity

(Main wing stall will not occur at any IAS within design flight envelope)

Front Pilot weight                           130lbs

Rear crew member                         none

Fuel weight                                      90lbs

XP empty weight                            500lbs

weight                                              720lbs

Center of gravity                           95.in

 

Note: Main wind stall may occur at any IAS when center of gravity is more than 98 inches of datum