The Hindustan Turbo Trainer (HTT)-40 is an ab-initio trainer aircraft designed to meet primary training requirements. This fully aerobatic tandem seat turbo trainer will have an air-conditioned cockpit, modern avionics, hot refueling, quick pilot change over and zero-zero ejection seats. Built around a proven turbo prop engine, this aircraft is designed to have good low speed handling qualities for better training effectiveness. This aircraft will be certified to FAR-23 Standard.
The aircraft is fitted with Glass Cockpit and Indigenously developed Avionics viz Radio Communication, Standby Communication, VOR-ILS, TACAN, Radio Altimeter and Identification Friend or Foe (IFF) and Integrated Standby Instrument System (ISIS).
The HTT-40 is powered by Honeywell TPE331-12B Turboprop engine.
Salient Features:
Sturdy structure with a combination of light alloys and composites.
Single piece canopy giving both pilots good all-round vision
Glass cockpit
Maximum load factor +6/-3 g
Glide ratio of 12.3:1
Specification - Value
Internal fuel mass - 460 kg
Normal Training Configuration Mass - 2960 kg
Take-off Distance - 785 meter
Landing Distance - 987 meter
Time to Climb 3 km - 7.05 min
Service ceiling - 6 km
Endurance - 3.09 hrs
Max permissible Speed - 450 kmph @ 6g
Max level Speed - 407 kmph
Max Power - 1100 Shp
Roles
Basic flying training
Instrument Flying
Navigation
Night Flying
Close formation