The Y-12 is a twin-engine turboprop STOL general purpose aircraft.
The aircraft is a high-wing monoplane with a single tail and non retractable, tricycle landing gear.
The Y-12 can perform cargo and passenger transport.
It can also be modified for parachute jumping, air dropping, maritime survey, aerial photography, geological survey, forestry seeding, air ambulance, sightseeing and etc.
It can take-off and land on unprepared airstrips, grass and sandstone runways.
Specifications
Crew
2
Capacity
17 pax / 1,700 kg (3,748 lb) max payload
Length
14.86 m (48 ft 9 in)
Wingspan
17.235 m (56 ft 7 in)
Height
5.575 m (18 ft 3 in)
Wing area
34.27 m2 (368.9 sq ft)
Airfoil
LS-0417
Empty weight
2,840 kg (6,261 lb)
Max take-off weight
5,300 kg (11,684 lb)
Fuel capacity
1,616 l (427 US gal; 355 imp gal) / 1,230 kg (2,712 lb) max usable fuel weight