HTT-40

General Description
Product Specifications
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Point of Contact for further follow up
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Product Manufacturer
Hindustan Aeronautics Limited (HAL)
Designing/Manufacturing agency
HAL
Product Description

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.

Features/Roles/Variants of the product
Sturdy structure with a combination of light alloys and composites.
Single piece canopy giving both pilots good all-round vision
Glass cockpit
Maximum speed 450 km/h
Maximum load factor +6/-3 g
Glide ratio of 12.3:1
Product Specification
Basic Information
Length - 10.061 meter
Height - 3.583 meter
Span - 11.0 meter
Basic Empty Mass - 2414 kg
Internal fuel mass - 460 kg
Maximum Take-off Mass - 3040 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
Range - 1009 km
Endurance - 3.09 hrs
Max permissible Speed - 450 kmph @ 6g
Max level Speed - 407 kmph
Max Power - 1100 Shp
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