1986 PHANTOM X2 ULTRALIGHT
Phantom type ultralight aircrafts were designed by John Dempsy. It was produced in 1986 and built as high wing and two seater. It was designed as a training aircraft. The restoration of this aircraft was carried out under the supervision of an experienced technician by the young people who devoted themselves to aviation at Sivrihisar Aviation Center.
It was donated to M.S.Ö. Air & Space Museum in April 2019 by Mustafa YAVUZ.
Specifications:
EMPTY WEIGHT
MTOW
FUEL CAPACITY
MAXIMUM SPEED
CRUISING SPEED
RANGE
SERVICE CEILING
RATE OF CLIMB
WING SPAN
HEIGHT
LENGTH
474 lbs
974 lbs
10 gal
75 mph
68 mph
282 KM
4420 M (14,500 FT)
653 fpm
29’11’’
8’5’’
16’11’’
EMPTY WEIGHT 474 lbs
MTOW 442 KG
FUEL CAPACITY 10 gal
MAXIMUM SPEED 121 82 KM / H
CRUISING SPEED 110 82 KM / H
RANGE 282 KM
SERVICE CEILING 4420 M (14,500 FT)
RATE OF CLIMB 653 fpm
WING SPAN 29’11’’
HEIGHT 8’5’’
LENGTH 16’11’’
