The test system is developed to carry out pressurization tests on wing tanks as well as safety valve tests for the aircraft PC24.
It is possible to adapt the equipment for other aircraft types.
> Supply of the device is ensured by an external pressure source
> Two test pressure circuits with varying pressure ranges and a vacuum circuit are fitted to ensure testing of test objects
> An activated carbon filter is provided at the return pipe to ensure filtering of fuel vapors
> Control elements are well arranged on the control panel inside the case