METRIC                                         IMPERIAL

Aerolite 103

Introducing the

Aerolite 103

to the Australian Sky

Empty Weight      107 Kgs

 Gross Weight 272 Kgs

  Length 16 ft. 3.25 in. 

  Wing Span 8.185 meters

  Wing Area 11.24 sq. meters  

 Wing Loading @ 450 Lbs. 3.72 lbs / sq. ft.  

 Wing Loading @ 500 Lbs. 4.13 lbs / sq. ft.  

 Wing Loading @ 550 Lbs. 4.54 lbs / sq. ft. 

 Wing Loading @ Max Gross Weight 4.96 lbs / sq. ft. 

  Design Load Limits @ Gross Weight +4 / -2  

 Engine Power Requirements 28 hp.-50 hp.  

 Propeller Max. Diameter 152 cms   

 Stall Speed, Flaps Extended 23 knots

Stall Speed, Clean 24 knots

 Cruise Speed (2) 49 - 55 knots   

 Top Speed 55 knots

 Rate Of Climb 500 - 1000 fpm   

 Sink Rate 350-400 fpm.  

 Roll Rate 45° to 45° bank / 2.5 seconds  

 Take Off Distance 100-200 ft.   

 Landing Distance 100-200 ft.  

 Fuel Capacity 19 litres

Endurance 1.5-2.5 hours   

Fuel Consumption 7.5 - 17 litres / hour   

Range 80-120 miles         

Limitations &   V-Speeds 

  Vne (never   exceed) 61 knots.   

Va   (design maneuvering speed) 43 knots.   

Vfe  (max   flaps extended) 60 knots  

 Vy  (best   rate of climb) 39 knots.   

Vx (best   angle of climb) 35 knots  

 Vs  (stall,   flaps retracted) 24 knots  

 Vs  (stall,   flaps extended) 23 knots

 Vr  (rotation   speed) 27 knots.  

 Max. Crosswind Component 13 knots

 Max. Wind Speed 22 knots. 

 Max. Bank Angle 45° 

 Max. Pitch Angle 30° 

Empty Weight      235 lbs 

 Gross Weight 600 lbs.  

  Length 16 ft. 3.25 in. 

  Wing Span 26 ft. 10.25 in. 

  Wing Area 121 sq. ft.  

 Wing Loading @ 450 Lbs. 3.72 lbs / sq. ft.  

 Wing Loading @ 500 Lbs. 4.13 lbs / sq. ft.  

 Wing Loading @ 550 Lbs. 4.54 lbs / sq. ft. 

 Wing Loading @ Max Gross Weight 4.96 lbs / sq. ft. 

  Design Load Limits @ Gross Weight +4 / -2  

 Engine Power Requirements 28 hp.-50 hp.  

 Propeller Max. Diameter 60 in   

 Stall Speed, Flaps Extended 26 mph

 Stall Speed, Clean 28 mph 

 Cruise Speed (2) 45-63 mph   

 Top Speed 63 mph 

 Rate Of Climb 500 - 1000 fpm   

 Sink Rate 350-400 fpm.  

 Roll Rate 45° to 45° bank / 2.5 seconds  

 Take Off Distance 100-200 ft.   

 Landing Distance 100-200 ft.  

 Fuel Capacity 5 U.S. Gallons   

Endurance 1.5-2.5 hours   

Fuel Consumption 2-4.5 US Gallons / hour   

Range 80-120 miles         

Limitations &   V-Speeds 

  Vne (never   exceed) 70 mph.   

Va   (design maneuvering speed) 50 mph.   

Vfe  (max   flaps extended) 70 mph.  

 Vy  (best   rate of climb) 45 mph.   

Vx (best   angle of climb) 40 mph.  

 Vs  (stall,   flaps retracted) 28 mph  

 Vs  (stall,   flaps extended) 26 mph 

 Vr  (rotation   speed) 30 mph.  

 Max. Crosswind Component 15 mph

 Max. Wind Speed 25 mph. 

 Max. Bank Angle 45° 

 Max. Pitch Angle 30° 

SPECIFICATIONS

STRENGTH

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Pics of the wing load and airframe load testing.