
The Embraer-Mahindra C-390 Millennium has emerged as a strong contender for
the Indian Air Force's Medium Transport Aircraft (MTA) requirement, which aims
to replace the ageing An-32 transport fleet. The aircraft combines high
payload capacity, jet-powered performance and multi-role flexibility, making
it one of the most capable medium-lift transport platforms currently
available.
As part of its bid for the Indian Air Force requirement, Embraer and Mahindra
have identified Nagpur as the proposed location for a final assembly line in
India. The project remains subject to the C-390 being selected under the MTA
program. The proposed facility would support aircraft assembly, systems
integration, manufacturing engineering and the development of a domestic
aerospace supply chain.
The partnership is working closely with the Maharashtra Government to
establish the industrial infrastructure required for the programme. If
approved, the project would support India's self-reliance objectives by
integrating Indian aerospace firms into the global C-390 ecosystem and
expanding local manufacturing capabilities.
India represents a strategically important market for Embraer. The company
believes the Indian Air Force could ultimately require between 60 and 80 C-390
aircraft, making the programme one of the largest military transport aircraft
opportunities in the world.
A major advantage of the C-390 is its 26-ton maximum payload capacity,
allowing it to transport military equipment, vehicles, humanitarian supplies
and operational cargo. Its large cargo hold offers 169 cubic metres of
internal space, providing excellent flexibility for a wide range of missions.
The aircraft can carry up to 80 personnel in a troop transport configuration
and up to 64 paratroopers for airborne assault operations. Its spacious cabin
also enables the transport of military vehicles, with room for three to four
light vehicles or one to two heavy vehicles depending on mission requirements.
The C-390 is additionally capable of transporting a Black Hawk-sized
helicopter within its cargo hold, reducing deployment times and increasing
operational flexibility across long distances.
Powered by two IAE V2500-E5 turbofan engines, the aircraft can cruise at up to
470 knots, or approximately 870 km/h. This makes it significantly faster than
many traditional turboprop military transports, enabling quicker response
times during military and humanitarian missions.
When carrying a full 26-ton payload, the aircraft offers a range of 1,080
nautical miles. With a 23-ton payload, range increases to 1,470 nautical
miles. Ferry range extends to 3,370 nautical miles and can reach 4,570
nautical miles when fitted with internal auxiliary fuel tanks.
The aircraft has been designed to operate from semi-prepared, austere and
damaged runways, making it well suited to India's demanding operating
environment, including remote border regions, island territories and forward
locations.
Take-off performance is equally impressive. The aircraft requires
approximately 1,524 metres of runway with a 23-ton payload and only 1,165
metres with a 16-ton payload. Landing distance is listed at around 1,000
metres with a 26-ton payload.
The C-390 can rapidly be converted for medical evacuation missions. Depending
on the configuration, it can accommodate between 50 and 80 stretchers along
with medical attendants and specialised equipment.
In its KC-390 tanker configuration, the aircraft can conduct aerial refuelling
operations while also being capable of receiving fuel from another tanker
aircraft. This dual-role capability provides additional operational
flexibility and could reduce the need for separate refuelling platforms.
The aircraft is also suitable for search and rescue operations, humanitarian
assistance, disaster relief missions and aerial firefighting. Its modular
design allows rapid reconfiguration between different mission profiles.
Embraer has emphasised the aircraft's ability to operate in extreme climates,
including hot desert environments, dusty conditions, high-altitude regions and
very cold locations. Demonstrations have included operations from unpaved
runways and challenging environments such as Antarctica.
The C-390 measures 35.20 metres in length, stands 11.84 metres high and has a
wingspan of 35.05 metres. The aircraft can operate at altitudes up to 36,000
feet and carries up to 23.9 tons of usable fuel in its wing tanks. Avionics
include the Rockwell Collins Pro Line Fusion suite and the Gabbiano T-20
tactical radar.
Beyond performance, the aircraft offers modern fly-by-wire controls, lower
maintenance requirements, high mission availability rates and reduced
lifecycle costs. It currently serves with multiple air forces worldwide and
has secured orders from several NATO nations, highlighting growing
international confidence in the platform.
Should the Indian Air Force select the C-390 Millennium, the proposed Nagpur
facility would establish a major aerospace manufacturing hub in India while
strengthening indigenous capability across production, maintenance, training
and long-term support activities.
Key Specifications And Capabilities of The Embraer C-390 Millennium
| Category | Specification / Capability |
|---|---|
| Aircraft Type | Twin-engine, jet-powered military transport aircraft |
| Maximum Payload | 26 tonnes |
| Cargo Compartment Volume | 169 cubic metres |
| Troop Capacity | Up to 80 troops |
| Paratrooper Capacity | Up to 64 paratroopers |
| Vehicle & Equipment Carriage | Multiple light or heavy military vehicles, or a Black Hawk-class helicopter |
| Maximum Cruise Speed | Up to 470 knots, approximately 870 km/h |
| Range with 26-ton Payload | 1,080 nautical miles |
| Range with 23-ton Payload | 1,470 nautical miles |
| Ferry Range | Up to 4,570 nautical miles with additional internal fuel tanks |
| Airfield Operations | Can operate from semi-prepared, austere and damaged runways |
| Take-Off Distance | 1,524 metres with a 23-tons payload |
| Landing Distance | Approximately 1,000 metres with a 26-tons payload |
| Engines | Two IAE V2500-E5 turbofan engines |
| Engine Thrust | 31,330 pounds of thrust per engine |
| Maximum Operating Altitude | 36,000 feet |
| Usable Fuel Capacity | 23.9 tonnes |
| Flight Controls | Advanced fly-by-wire flight-control system |
| Avionics Suite | Rockwell Collins Pro Line Fusion cockpit and Gabbiano T-20 tactical radar |
| Mission Reconfiguration | Rapid mission reconfiguration capability |
| Operational Advantages | Reduced maintenance requirements, high operational availability and lower lifecycle costs |
| Mission Roles | Cargo transport; troop movement; airborne assault operations; paratroops deployment; medical evacuation; aerial refuelling; search and rescue; humanitarian assistance; disaster relief; and aerial firefighting |
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