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Products in Current Manufacturing Range
 
HAL-DORNIER 228


The 19 seater HAL - DO - 228 aircraft is a highly versatile multi-purpose light transport aircraft. It has been developed specifically to meet the manifold requirements of utility and commuter transport, third level services and air-taxi operations, coast guard duties and maritime surveillance.
 
External Dimensions
Wing span
16.97 m
Overall length
16.56 m
Overall height
4.86 m
Baggage Compartments
 
Front
Aft
Volume(m3) 0.89 2.60
Max load (kg) 120 210
Cabin
Pax seats
19
Length
7.08 m
Width
1.35 m
Height
1.55 m
Cargo cum pax door(wide)
1.60m x 1.34 m
Cargo door (normal)

1.28m x 1.34m
Power Plant
Engine Model
Garrett TPE 331-5-252D
Take-off power
2 x 715 SHP flat rated to ISA + 18oC
Propeller type Hartzell four-bladed
Propeller diameter
2.69 m
Fuel capacity
2350 ltrs (2250 kg)
Fuel consumption
213 kg/hr
Weights
Max. Take off Weight  
 
Maritime role

6400 kg
Commuter role

6200 kg
Max Landing Weight
5590 kg
Max Zero fuel Weight
5590 kg
Performance
short take-off and landing capabilities  
Max cruise speed 428 km/hr
Max range speed 333 km/hr
Rate of climb 9.7 m/s

Roles
  • Maritime surveillance
  • pollution prevention
  • Troop transport
  • Aerial survey
  • Search and Rescue
  • Commuter transport
  • Calibration of airport NAV-COM aids
  • Remote sensing applications
  • Casuality evacuation
  • Executive transport
  • Cargo & Logistics support


HPT-32


The HPT-32, an ab-initio, piston engine basic trainer aircraft with side-by-side seats has been completely designed, developed and manufactured by Hindustan Aeronautics Limited to cater to the stringent requirements of both military and civil users. Designed to meet the FAR-23 requirements, the aircraft has been type certified by both the civil and military airworthiness authorities of India.
 
Main Dimensions
Span
9.50 m
Length
7.72 m
Height
2.88 m
Wheel track
3.45 m
Propeller diameter
2.03 m
Propeller ground clearance
0.24 m
Weights
Max take-off-weight
1310 kg
Max landing weight
1310kg
Operating empty weight
906 kg
Max useable fuel
172 kg
Power Plant
Engine 260 hp Textron Lycoming engine driving a two bladed Hartzell propeller
Performance
Max speed at SL
264 kmph
Stall speed (clean)
115 kmph
Stall speed (with flaps)
110 kmph
Take-off distance to 15 m
450 kmph
Landing distance to 15 m
512 m
Rate of climb (SL, ISA + 15oC)
328 m/min
Range (3 Km altitude)
902 km
Endurance (3 km altitude)
5 hrs 15 min

Roles


  • Ab-initio training
  • Instrument flying
  • Navigation flying
  • Night flying
  • Formation flying
  • Liaison
  • Sports flying
 
 

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