ASU (Air Start Unit) MODELS
Air Starter Group 180-400 ppm
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GS180
Specifications
Nominal flow rate (*): 180 ppm
Chassis: trailer / self-propelled
Pneumatic characteristics (*): 42 psi
Diesel engine: Deutz
Dimensions: 4700 x 1940 x 2450 mm
Weight: 4300 kg
(*): at 15°C, at sea level
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GS280
Specifications
Nominal flow rate (*): 280 ppm
Chassis: trailer / self-propelled
Pneumatic characteristics (*): 42 psi
Diesel engine: Deutz
Dimensions: 4700 x 1940 x 2450 mm
Weight: 5100 kg
(*): at 15°C, at sea level
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GS400
Specifications
Nominal flow rate (*): 400 ppm
Chassis: trailer / self-propelled
Pneumatic characteristics (*): 42 psi
Diesel engine: Deutz
Dimensions: 5625 x 2300 x 3200 mm
Weight: 9200 kg
(*): at 15°C, at sea level
ASU
Variable speed Guinault ASUs ensure the pneumatic start-up of aircraft engines in the event of an APU failure. The range covers all existing aircraft. Aircraft start-up characteristics relating to the climatic environment are provided by the manufacturers in the aircraft operation manuals. The Guinault range covers requirements from 0 to 400 ppm.
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