ENGINE COMPRESSOR WASHING STAND

MAIN FEATURES:
The A/C turbine engine compressor washing unit is realized on a steerable trailer equipped with four pneumatic wheels, towing through a tow-bar at the maximum speed of 30 Km/h.
Rear wheels are equipped with hand operated drum brake.
The unit is powered by an air compressor driven by a gasoline mono cylinder engine.
An auxiliary power outlet 12Vdc 5A is provided.

TECHNICAL CHARACTERISTICS:
•  Engine: Mono cylinder, with electrical and hand starter, nominal rotation speed 2840 RPM
•  Engine power: 5,5 CV
•  Compressor: Mono cylinder, maximum delivery 200 LPM at 10 bar, 50 Lt tank capacity, nominal rotation speed 1420 RPM
•  Priming: Belt with pulleys coupling. Transmission ratio 1:2
•  Delivery: 55 LPM at 20psi.
•  Work pressure: adjustable from 5 to 110 PSI
•  Safety relief valve: 4 safety valves: 8 bar valves (2) on compressor tank, 8 bar valve on each fluid tank.
•  Pressure gauge: 4 pressure gauges
   –  Compressed air inlet, Dia 100mm F.S. 160PSI, accuracy 0,6 %
   –  Fluid delivery pressure, Dia 100mm F.S. 160PSI, accuracy 0,6 %
   –  Reservoir compressed air pressure (1&2) Dia 63mm F.S 10bar
•  Filtering: β 50 > 100
•  Equipment: Two stainless steel tank 83 Lt. capacity each; output flexible hose Aeroquip FC 332-8, type in AQP, or equivalent MULTIFIT, length 10 m.
•  Structure: Steel and painted structure Mounted on four pneumatic wheels provided with rear parking brake, towing bar in accordance to STANAG 4101or 3510 standards.

ACCESSORIES:
Test stand textile cover, wood crate for transport; O&M manual, CoC, Test report, gauge calibration report.

REMARKS:
Suitable for AW109, AW139, AW189, AB212/412, CH47, EH101, NH90, HH3F, SH3D

ADOPTED BY:
Leonardo Company H.D., Airbus Helicopters, Italian Navy, Italian Army