Selected references

• 
  Airbus A380 Major airframe
  fatigue test
  Structural tests on full-scale airframe tests
  • All airbus basic types (A300 to A340-600 completed; A380, A400M on-going, A350 in preparation)
  • Commuter aircrafts (PC-12)
  • General aviation aircraft (Extra 400; Grob G180 at the manufacturer’s site)
  • Military aircraft (Tornado, Eurofighter Typhoon, Swiss F/A-18 at RUAG, Pilatus PC-21)
• Structural component tests
• Airbus A380 engine pylon attachment and spoiler
• Pilatus PC-21 landing gear drop test
• Airbus A380 vertical tail plane component
• Tornado main landing gear door
• Structural analysis
  • NDT inspections on test articles (Airbus A380) and in-service aircraft (Tornado)
  • Damage documentation (DamDoc) during full-scale fatigue tests (Airbus A380)
  • Structural damage analysis on in-service aircraft (Tornado)
  • Complex FEM analyses for the optimisation of structural tests (integration of Airbus A380 full-scale fatigue test article into test rig)
  • Technical/scientific structural advice during the development and operation of aircraft (Eurofighter Typhoon)
• 
  Airbus A400 Major airframe
  fatigue test
  Structural monitoring
  Fatigue life monitoring of the following aircraft types:
  • PA200 Tornado
  • F-4F Phantom
  • C-160 Transall
  • BR-1150 Breguet Atlantic
  • Alpha-Jet
  • Mig 29
  • Eurofighter Typhoon
  • CH-53
• Flight tests
  • Grob G180 flight testing (measurement concepts, instrumentation, telemetry, special equipment)
  • Saab Gripen Hot-and-high testing in Granada (telemetry, infrastructure)
  • New development CH53 AFCS amplified measuring system for parameter identification flights
  • Saab 2000 special version testing in Granada
  • Performance improvement kit Dornier 228 (measuring system, telemetry)