Applied knowledge of aircraft engineering.
Adequate knowledge applied to engineering of:
- Calculation methods for aircraft design and project;
- Cetification basis and aircraft maintenance;
- Operational use of aircrafts.
Knowledge of concurrent engineering methods and manufacturing processes.
Knowledge of operating environment and aircraft design envelopes.
Knowledge of design variables related to flight and ground performance.
Application of preliminary design methods to establish the main aircraft design variables:
- maximum weight;
- thrust-to-weight ratio;
- wing loading.
Knowledge of methods to determine payload-range diagrams.
Knowledge of aircraft configuration and design constraints for its components: wing, fuselage, tails, etc.
Knowledge of main structural loads conditions, in accordance with certification rules.
Knowledge of specific characteristics of supersonic and fighter aircrafts.