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Hydraulic test stand

Specifications
Fluid typeMIL-H-5606 (air3520b, otan h515)
Operating temperature-14°F to +125°F
Dimensionss l × w × h22.5 × 22.5 × 57 in
Weight298 lb

Description and features

Typical aircraft application:

Servicing: any type aircraft

Main features:

  • Test stand is designed for the ground tests and checks of various aircraft components (landing gear, flaps, flight servo-controls…) and as decontaminate the fluid
  • A braking system actuated by means of a lockable lever provided on the tow-bar
  • The hydraulilc hoses
  • Pressure adjustable from 725 to 3000 psi
  • The stands is available in electric motor driven version or engine driven version. it can changing the “driving module”

Download the PDF document:

TDS BH2402.pdf (555.89Kb)

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