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Junior VI
The
plans built C.P. 1320 Saphire is a side by side two seat, low wing aircraft
designed by Giuseppe Vidor. Construction materials are wood &
fabric. The landing gear is a fixed trigear configuration.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
VW Engine 62 HP 50 to 65 HP
x
20 ft.
x
28.6 ft.
123.7 sq. ft.
2
530 lbs.
x
950 lbs.
x
375 miles
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performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
350 ft.
600 ft./min.
125 mph.
100 mph.
400 ft.
10,000 ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
135 mph.
38.5 mph.
x |
All specifications are based on manufacturer's
calculations
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