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GENERAL DESCRIPTION: The rig consiala essentially o1 a. structure on which tttu indipendem air condition units are installed. The control for both units are groused on a common control panel localed in 1he rear side of the rig. The rig ie capable to deliver conditioned air (controlled temperature and humidity) 1o cool simultaneously the avionic bay of two aircraft during ground test of trie avionic equipment. POWER PLANT: Air conditioning nominal power 29W0kcal-'h for each unit Dehumidified air at a temperature of 17 ±2"C ;B5Qm2;h), AH<5g/kg tor each unit Tawing speed: B knVti AMBIENT...

Pneumatic fiir Starter and flir Conditioning System flS/Boostrap Diesel Engine Driuen

GENERAL DESCRIPTION: The unit combines a 1reon free (air cycle) air conditioning ayalem and a aneumalic starter unit. The unit is capable 1o deliver conditioned air at controlled temperalure and humidity to cool the avianic bay o1 aircraft during ground tests and to deliver compressed air POWER PLANT: Cummina QEB5.9 turbo diese engine, water cooled, rated outpul 116kW 2300-pr" AMBIENT CONDITION: S:or^ge temperalure: Caerating humidhy: Operating altitude: OPERATING CHARACTERISTICS, AIR CONDITIONING SYSTEM: Dehumidified air at a temperature of 15 ±2°C (flOQ kg/h at 1.25bar(a) > AH<5c 'kg...

flir Conditioning System for CiuiL Aircraft flircgcle/Boostrap Electric Engine Driuen

GENERAL DESCRIPTION: The unit ta fitted with a freon free (air cycle) air onndilioning eyatem. The unit is capable to deliver conditioned air (-controlled temperature and humidity) 1Q ccol 1he avionic bay o1 aircraft during ground tests. ELECTRICAL POWER: AMBIENT CONDITION: Operating temperature: S:or^ge temperalure: Operating humidhy: Operating altitude: OPERATING CHARACTERISTICS: Tawing speed: 25 kmfli

multi-Power Capability Unit for Ciuil Aircraft Diesel Engine Driuen The muHi-power capabilhiea unit has been designed to provide the aircraft wilh: Elevr CCL power: 28,5 V de, max current 120QA AMBIENT CONDITION