Icing
The Clean Aircraft Concept
Every performance parameter in the flight computer assumes a perfectly clean aerodynamic profile. There is no mathematical allowance for frost.
Aerodynamic Verification
Targeting reticle confirms a clean-surface lock while laminar streamlines illustrate the undisturbed airflow over the airfoil that the flight computer models.
Regulatory Basis
Aeronautical Mandate
Regulations dictate zero takeoff tolerance for frost, ice, snow, or slush adhering to any critical surface.
Performance Model
Design Assumption
Climb rates, stall speeds, and control authority computations are strictly based on clean wings.
Legal Framework
Shared Accountability
Flight Crew, Flight Operations Officers (FOO), and Ground Handlers share equal legal accountability in verifying compliance.