CONSTRAINTS IN CRAGER

• Operation related

  • WAT Climb Gradient > 2.4 %
  • Main Cruise Throttle < 100%
  • Max. Rate of Descent < 500 fpm (Unpressurised a/c)
  • Sideline Noise value < 94 EPNdB @ 450 m
    

• Derived parameters

  • Static Margin = 5% MAC
  • Calculated MTOW = Assumed MTOW
  • Calculated Fuel mass = Assumed Fuel mass
  • Main Stage Length = Climb + Cruise + Descent
  • Notional Stage Length = Climb + Cruise + Descent

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