
Engine displacement and airframe mass must maximize payload capacity while ensuring STOL capabilities under high density altitude conditions.
High-tensile aluminum or titanium airframes must undergo non-destructive testing to verify long-term resistance to aerodynamic stresses and vibration.
Selection depends on Mean Time Between Failure data and standardized TBO intervals to minimize unscheduled maintenance and operational risks.
Digital EFIS systems must provide real-time engine monitoring and backup analog instrumentation to prevent total situational awareness loss.
