What is the maximum density altitude listed in the POH limitations for MAGGIE14LR?

The maximum density altitude listed in the Pilot's Operating Handbook (POH) limitations for the MAGGIE14LR is 14,000 feet. This figure is significant because it indicates the upper limit at which the helicopter can safely operate regarding engine performance, rotor efficiency, and overall aircraft performance characteristics. Density altitude affects the lift capabilities of the rotor blades; as the altitude increases, the air density decreases, which leads to a reduction in engine performance and the amount of lift generated by the rotor system.

Operating above this density altitude limit may result in insufficient power, longer takeoff distances, and an inability to climb effectively, which can jeopardize safety. This limitation helps pilots to make informed decisions regarding weight, balance, and environmental conditions to ensure safe flight operations.

In contrast, the other altitude options are not correct as they exceed the operational capabilities specified for the MAGGIE14LR, implying potential performance issues and safety risks if the helicopter were to be operated at those altitudes. Understanding these limits is essential for maintaining safety margins during flight.