What climb gradient must a multi-engine aircraft achieve on runway 19 from KPSO if one engine is inoperative?

To determine the required climb gradient for a multi-engine aircraft with one engine inoperative, several factors must be considered, such as the aircraft's performance specifications and the specific conditions at the airport. The climb gradient is expressed in feet of altitude gained per nautical mile (NM) of horizontal distance covered.

When an aircraft loses an engine, it typically must achieve a minimum climb gradient to maintain safety and performance standards, especially during takeoff. This gradient ensures the aircraft can safely clear obstacles in the vicinity of the airport.

A climb gradient of 296 feet per nautical mile indicates that the aircraft would be capable of achieving a positive rate of climb even with one engine not functioning. This value is often specified in manufacturer performance data or the appropriate aeronautical regulations, taking into account the specific characteristics of the aircraft model, weight, and environmental conditions present at that time.

Understanding the required climb gradient is critical for flight safety, and ensuring compliance with these standards helps pilots make informed decisions during flight operations.