AEROSPACE RESEARCH AND TEST ESTABLISHMENT

• static and fatigue of aircraft airframes, their parts and structural components
  
• static strength test of non aircraft structures in cooperation with certified worksite for these tests
  
• strength tests of metallic and composite structures with ambient conditions influence
  
• residual static strength tests
  
• aircraft airframe and their parts rigidity tests
  
• static, fatigue, functional and drop tests of landing gears
  
• overpressure static tests
  
• stress and strain measurements, deformations and displacements measurements, stress and
  strain experimental analysis (strain gages, laser interferometry, photogrammetry, thermoelasticimetry, photostress analysis, brittle lacquers), NDT inspections
• special strength tests (for example Bird Strike test etc.)
  

• uniaxial electromechanical load machine TIRAtest 28500S (up to 500 kN)
  
• Aero 90 (24 channels) and Aero ST (10 channels) servo-hydraulic fully digitally controlled load systems
  
• Fatigue and static load machines (MTS, Instron Schenck, Tira, Inova, Amsler up to 500 kN
  
• 6 channel and 12 channel IST Schenck Hydropuls servo-hydraulic digitally controlled load systems
  
• hydraulic IHS load system (up to 200 kN)
  
• 20 channel electro hydraulic MTS load systems
  
• 100 hydraulic load actuators (range 1 – 1000 kN) hydraulic oil supply station (working pressure 210 MPa, total capacity 1440 lpm)
  
• load grid areas 30mx30m and 30mx60m, unified system of test load fixtures (upper grid assembly)
  
• modular climatic chamber with two Testair climatic units(max.- temperature 80±1°C, max. relative humidity 90±5% for conditioning
  
• AMD-01, 02 length changes measure system
  
• Electro-hydraulic pneumatic overpressure system
  
• multichannel data acquisition and stress and strain measure systems (Vishay, Schlumberger, HBM, BMC, DAQ National Instruments)
  
• contactless systems for stress and strain and deformation measurements (Dantec Dynamics ESPI, GOM ARAMIS 3D HS, SPATE 4000 etc.)
  

STANDARD SPECIFICATIONS:

• aeronautical airworthiness requirements EASA CS
  (JAR), FAR, CAGI, MIL
  
  

APPROVAL CERTIFICATES:

• Civil Aviation Authority of the Czech Republic (ÚCL) certificate No. L-3-014/5 according to CAA.TI-012-3/99
  
• ISO 9001:2008 quality certificate

• companies involved in design, development, manufacture, operation and maintenance of aircraft and their parts
  
• companies involved in developing transport and manipulating engineering
  
• development and research establishments