[عبدالسلام-1]

وهنا جميع المعلومات الخاصة بالطائرة كل جزء على حدا
Gross Weight 1,080 lb
Empty Weight (including water) 625 lb
Useful Load 455 lb

Weight of Wing 95 lb
Weight of Body 130 lb
Weight of Motor (Ford Model A) with Magneto 244 lb
Weight of Radiator 21 lb
Weight of Propeller 15 lb

Span 28 ft 2 in
Chord 5 ft
Wing Area (incl ailerons) 140 sq ft
Aileron Area (each) 6.2 sq ft
Aspect Ratio 5.67

Length (overall) 17 ft 6 in
Height (overall) 6 ft 6 in

Flying Speed 60 - 75 mph
Take-Off Speed 40 mph
Landing Speed 35 mph

Fuel Capacity 10 gals

Airfoil Pietenpol
Powerplant Model A (35 hp @ 1600 rpm)
Propeller (6'2" to 6'6") x (4'0 to 4'3")



Configuration: 1934 Improved Air Camper


Gross Weight 1,080 lb
Empty Weight (including water) 610 lb
Useful Load 470 lb

Span 29 ft
Chord 5 ft
Wing Area (incl ailerons) 145 sq ft
Aileron Area (each) 6.2 sq ft
Aspect Ratio 5.8

Length (overall) 17 ft 8 in
Height (overall) 6 ft 6 in

High Speed 90 mph
Landing Speed 40 mph

Climb Light Load (solo weight) 500 fpm
Climb Full Load (gross weight) 200 fpm

Fuel Capacity 10 gals

Airfoil Pietenpol
Powerplant Model A (40 hp @ 1650 rpm)
Propeller (6'2" to 6'6") x (4'0 to 4'3")