ADOUR MK 811 Jaguar Aircraft is powered by two Adour MK 804 / MK 811 Engines. MK 811 Engines are manufactured from 1981 under licence from RR/TM [ Rolls Royce Turbomeca ].
Adour MK 804 Engines are also overhauled and repaired under the above licence.
Adour Engine is a bypass Jet Engine of modular construction. The Adour has two-stage low pressure and five-stage high pressure axial flow Compressors which are driven by separate, single stage high pressure and low pressure Turbines connected through co-axial shafts, with low pressure shaft passing through high pressure shaft.
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| Main Characteristics |
| Intake Diameter (m) | 0.564 |
| Length (m) | 2.90 |
| Weight (kg) | 794 |
| Thrust | 2500 (dry)
3737 (wet) |
Specific Fuel Consumption
(kg / kg-hr) | 0.80 |
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GARRETT 331 - 5
The Garrett TPE 331-5 Turbo prop Engine is being manufactured, overhauled and repaired for various Customers under licence from Garrett Engine Division of Honey Well Company [earlier Allied Signal Aerospace Company, USA] since 1988 and belongs to one of the most popular series of small Turbo prop Engines powering a large number of Commuter and Corporate Aircraft such as Dornier DO-228.
It has a single shaft Centrifugal Compressor Engine rated at 715 shaft horse power at 1591 RPM output speed. Being a reverse flow Gas Turbine with a small frontal area, it has better dry specifics and easier airframe integration. Apart from its simplicity of design and superior performance, the engine features a propeller control system, anti-icing and foreign object damage resistance, reverse thrust and negative torque sensing facilities. The division is also an authorised service centre for Garrett TPE 331-5 series engines up to - 12.
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| Main Characteristics |
| Maximum Diameter (m) | 0.7 |
| Length (m) | 1.11 |
| Weight (kg) | 164 |
| Power | 715 |
Specific Fuel Consumption
(kg / shp-hr) | 0.268 |
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Artouste III B
 Artouste III B Engine powers both Cheetah and Chetak Helicopters. Manufacture of the Engine commenced in 1962 under licence from Turbomeca, France.
The Engine has side air intake, one axial and one centrifugal compressor connected to a three-stage Turbine. The power output is 550 SHP at 33500 RPM. The reduction Gearbox in the front transfers the power to Helicopter. More than 665 Engines have been manufactured and 2950 Engines overhauled and repaired for various Customers.
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| Main Characteristics |
| Maximum Diameter (m) | 0.50 |
| Length (m) | 1.815 |
| Weight (kg) | 182 |
| Power | 550 |
Specific Fuel Consumption
(kg / shp-hr) | 0.346 |
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| Potential For Overhaul and Repair |
DART 533 - 2 AND 536 - 2T
 The Dart series of Engines were manufactured since 1966 under licence from Rolls Royce, UK. At present, these Engines are being repaired and overhauled. Two Dart Engines power HS-748 aircraft.
This engine has two-stage Centrifugal Compressors, three- stage Turbine and utilises water methanol injection to increase the shaft Horse Power.
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| Main Characteristics |
| Maximum Diameter (m) | 0.960 |
| Length (m) | 2.490 |
| Weight (kg) | 628.6 |
Power (shp)
533-2
536-2T |
1835 (dry)
1990 (wet)
1835
2040 (wet) |
Specific Fuel Consumption
(kg / shp-hr) | 0.348 |
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ORPHEUS 70105
 Orpheus 70105, indigenously modified by HAL, is a derivative of Orpheus 701 at lower rating and is the Power Plant for Kiran MK II Aircraft indigenously designed by HAL.
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| Main Characteristics |
| Maximum Diameter (m) | 0.822 |
| Length (m) | 2.290 |
| Weight (kg) | 420 |
| Thrust (kg) | 1875 |
Specific Fuel Consumption
(kg / shp-hr) | 0.348 |
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AVON
 Avon is a Turbo Jet Engine designed and developed by Rolls Royce and is being overhauled / repaired under licence at HAL from 1959. Avon MK 1 is used in Canberra Trainer Aircraft. Avon MK 109 is used in Canberra Bomber and Avon MK 203 / 207 power the Hunter Fighter.
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| Main Characteristics |
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Avon
MK 1
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Avon
MK 109
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Avon
MK 203/207
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| Maximum Diameter (m) | 1.07 | 1.09 | 1.05 |
| Length (m) | 2.58 | 3.53 | 3.12 |
| Weight (kg) | 1006 | 1180 | 1310 |
| Thrust (kg) | 2955 | 3363 | 4613 |
Specific Fuel Consumption
(kg / kg-hr) | 0.94 | 0.95 | 0.88 |
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ADOUR MK 804 E
 The Adour MK 804 Engine is being repaired and overhauled under licence from Rolls Royce, UK. This is similar in construction to the MK 811 engine.
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| Main Characteristics |
| Maximum Diameter (m) | 1.278 |
| Length (m) | 2.990 |
| Weight (kg) | 733 |
| Thrust (kg) | 2343 (dry)
3347 (wet) |
Specific Fuel Consumption
(kg / kg-hr) | 0.79 |
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Gnome 1400 - IT
 The Gnome 1400 - IT engines being repaired and overhauled under licence from Rolls Royce, UK and is the Power Plant for Seaking Helicopter.
It is a Turbo shaft single spool with 10-stage Axial Compressor, two-stage Turbine and free Power Turbine.
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| Main Characteristics |
| Maximum Diameter (m) | 0.574 |
| Length (m) | 1.376 |
| Weight (kg) | 168 |
| Power (shp) | 1535 |
Specific Fuel Consumption
(kg / shp-hr) | 0.276 |
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