Vision 4, Specifications (of course subject to change)

Dimensions
Overall

Length
Wing Span
Height (top of tail)

   24ft.
   30 ft.
   8.2 ft.

 

 

Powerplant

Horsepower


 

180 hp minimum. 320 hp max.

Fuselage
Dimensions

Cockpit Width:

  Front Seats
  Rear Seats
Cockpit Height
Cockpit Length

46 in.

46 in.
 46 in.
 47.5 in.
 106 in.

 

Weights

Spar Location
Empty Weights
Gross Weight
Useful Load
Fuel Capacity
Baggage

           30% of Chord
          1400 -1500 lbs.
          2700 lbs.
         900 - 1300 lbs.
          70 - 82 gal. 
           per CG allowance

Wing
Dimensions

Wing Area
Wing Aspect Ratio
MAC

Spar Locations

Airfoil
Dihedral
Tip
Wash Out
Wing Loading

134 sq.ft.
       7

55.4 inches
30% & 70%
  of chord
NACA63-214
3.5 degrees
  1.5 degrees

  20 lbs sq.ft.

 

Performance

Top Speed (sea level)
Cruise Speed (sea lvl)
Stall Speed (clean)
Stall Speed (ldng)
Range w/Reserve
Rate Of Climb
... Average wt.
... Gross wt.
Take Off Roll
..Ovr 50
ft. obstcle
Landing Roll
Ceiling

 

Flap
Dimensions

Flap Type
Flap Area / Wing

slotted
15%

 

Limitations

Limit Load Factor (+)
Design Limit Load (-)
G Loading
Va Maneuver Speed
Vf Flap Extension
Vne Never Exceed

4.5 G 
  3.0 G
   
Normal
 162 mph
 100 mph
 234 mph

Tail
Dimensions

 Horizontal Tail Span
Horz Stab Mean Chord
Horz. Tail Area
Vertical Tail Height

 


 

10 ft. 
2.74 ft.
27.4 sq.ft.
14.3 sq. Ft.

 

 

Landing Gear
and Wheels

Main Landing Gear
...Type
...Wheels
...Tires
...Brakes

Nose Landing Gear
...Type
...Wheel
...Tire


2 Piece
Cleveland 6 x 6
Goodyear 6:00x6

oe Act. Disk
     /Caliper
Free Castering
 
 5:00x5-13.5

Control
Movement

Elevator
Aileron
Rudder
Flaps

+30  -30 deg
+20  -20 deg
L30 - R30 deg
0-40 deg

 

Placarded
Airspeed
Limits

Green Arc
Yellow Arc
White Arc
Red Line

       to 162 mph IAS
162 to 234 mph IAS
       to 100 mph IAS
       234 mph  IAS