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NAL Saras

By Wikipedia,
the free encyclopedia,

NAL Saras
NAL Saras taking off
Role Light transport aircraft
National origin India
Manufacturer National Aerospace Laboratories
Hindustan Aeronautics Limited
First flight 29 May 2004
Status Under Development
Number built 2
Unit cost 39 Crore Indian Rupees

The NAL Saras (Sanskrit: सरस्: "Crane") is the first Indian multi-purpose civilian aircraft in the Light Transport Aircraft category designed by the National Aerospace Laboratory (NAL).

Design and development

The project began in 1991 as a collaboration with Russia (Myasishchev had a similar project called the Duet), but financial trouble led the Russians to drop out early in the project. The project almost came to a halt when it was hit by US-imposed sanctions in 1998, after India's nuclear tests in Pokhran.

The first Saras (PT1) completed its maiden flight at the HAL airport in Bangalore on 29 May 2004.

While the designed empty weight of the aircraft is around 4,125 kg, the first prototype weighed in around 5,118 kg. This issue is sought to be addressed by including composite wings and tail by the third prototype. This also resulted in the originally chosen 850 hp PT6A-66 Pratt and Whitney engine being replaced by a 1,200 hp engine of the same PT6A family in the second prototype.

According to NAL, besides providing a higher lift, the new engine will also meet the more stringent FAR-25 climb gradient requirements under conditions of one engine failure. Apparently, the basic structure and the landing gear have enough margins to handle this increased all-up weight.

The second prototype (PT2) first flew on 20 April 2007. The third prototype is expected to fly by June 2009, with the modifications for weight reduction. The first prototype aircraft was on flying display at the 2005 Aero India airshow.

The total sanctioned cost of the project is at Rs 139 crores (30 Million USD).

Saras is one of the few aircraft to make use of a pusher propeller configuration. The basic configuration resembles very closely the platform of the Embraer/FMA CBA 123 Vector which never went into production.

The initial certification plan will include the two prototypes ( to be flown by the Airborne Systems Testing Establishment (ASTE) for a total period of 500 hours before certification from the Directorate General of Civil Aviation (DGCA).

Currently, work is progressing in all aspects towards building the weight optimized Production Standard Aircraft (PSA), with a targeted weight reduction of 500 kg. PSA is expected to have its first flight in the year 2009.

Saras-PT1 of the aircraft will be modified and converted to a Saras-PT3 by fitting the higher thrust Pratt and Whitney engines.

An extended version of Saras is planned. Commercial production of the aircraft is now expected by 2010.

Operational history

The manufacturer has stated that the Indian Air Force intends to place an order for up to 45 aircraft.

Incidents and accidents

Air Crash of Saras-PT2

On March 6, 2009, 2 Indian Air Force test pilots, Wing Commander Praveen and Wing Commander Dipesh Shah along with a Flight Test Engineer Squadron Leader Ilayaraja, were killed when the second prototype Saras aircraft crashed and caught fire in an open field near Bidadi, about 30 km from Bangalore.The airframe of Saras-PT2 was built with lighter composites to reduce its overall weight by about 400 kg from its first prototype, which was overweight by about 900 kg. The aircraft is powered by two Canadian Pratt & Whitney turbo-prop engines.

Specifications (Saras)

General characteristics


External links

Text from Wikipedia is available under the Creative Commons Attribution/Share-Alike License; additional terms may apply.

Published in July 2009.

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