A method includes displaying, on an electronic display, an electronic checklist. The method further includes determining whether the electronic checklist includes a checklist item associated with states of multiple components of a subsystem associated with the electronic checklist. The method further includes, based on determining that the electronic checklist includes the checklist item associated with the states of the multiple components, displaying, on the electronic display, a single option that is selectable to send control commands to the multiple components.

A method includes displaying, on an electronic display, an electronic checklist. The method further includes determining whether the electronic checklist includes a checklist item associated with states of multiple components of a subsystem associated with the electronic checklist. The method further includes, based on determining that the electronic checklist includes the checklist item associated with the states of the multiple components, displaying, on the electronic display, a single option that is selectable to send control commands to the multiple components.

A fuel jettison system for the inflight discharge of fuel from an aircraft, and an aircraft having such a fuel jettison system. Using a venturi effect, the fuel jettison system facilitates the inflight discharge of fuel from the aircraft during an inflight fuel jettison operation at a higher velocity that mitigates the effects of turbulence to thereby mitigate an occurrence of fuel jettison impingement on aerodynamic surfaces of the aircraft.

A fuel jettison system for the inflight discharge of fuel from an aircraft, and an aircraft having such a fuel jettison system. Using a venturi effect, the fuel jettison system facilitates the inflight discharge of fuel from the aircraft during an inflight fuel jettison operation at a higher velocity that mitigates the effects of turbulence to thereby mitigate an occurrence of fuel jettison impingement on aerodynamic surfaces of the aircraft.

A fuel jettison system for the inflight discharge of fuel from an aircraft, and an aircraft having such a fuel jettison system. Using a venturi effect, the fuel jettison system facilitates the inflight discharge of fuel from the aircraft during an inflight fuel jettison operation at a higher velocity that mitigates the effects of turbulence to thereby mitigate an occurrence of fuel jettison impingement on aerodynamic surfaces of the aircraft.

A fuel jettison system for the inflight discharge of fuel from an aircraft, and an aircraft having such a fuel jettison system. Using a venturi effect, the fuel jettison system facilitates the inflight discharge of fuel from the aircraft during an inflight fuel jettison operation at a higher velocity that mitigates the effects of turbulence to thereby mitigate an occurrence of fuel jettison impingement on aerodynamic surfaces of the aircraft.

A seaplane float frame apparatus with extra fuel storage, and a method of installing, comprising: 1) a middle section housing at least one auxiliary fuel storage tank; and 2) two opposing side panels affixed to the middle section, extending outward from about 45-60-degrees from the parallel, each of the two opposing side panels comprising a bottom flat edge fit-able to a float (e.g., carbon composite). The middle section further comprises a fuel pump and a fuel line attached to the auxiliary fuel storage tank(s) and to a main fuel tank within an airplane fuselage-engine. Electrical components enable the pilot, or automatedly as needed, to pump fuel from the frame's tanks. The two opposing side panels comprise triangular shaped cutouts to reduce the float frame's weight and drag, and a built-in steps, a bar, and non-skid coating on the floats to assist in climbing safely into/out of the cockpit.

A seaplane float frame apparatus with extra fuel storage, and a method of installing, comprising: 1) a middle section housing at least one auxiliary fuel storage tank; and 2) two opposing side panels affixed to the middle section, extending outward from about 45-60-degrees from the parallel, each of the two opposing side panels comprising a bottom flat edge fit-able to a float (e.g., carbon composite). The middle section further comprises a fuel pump and a fuel line attached to the auxiliary fuel storage tank(s) and to a main fuel tank within an airplane fuselage-engine. Electrical components enable the pilot, or automatedly as needed, to pump fuel from the frame's tanks. The two opposing side panels comprise triangular shaped cutouts to reduce the float frame's weight and drag, and a built-in steps, a bar, and non-skid coating on the floats to assist in climbing safely into/out of the cockpit.

A seaplane float frame apparatus with extra fuel storage, and a method of installing, comprising: 1) a middle section housing at least one auxiliary fuel storage tank; and 2) two opposing side panels affixed to the middle section, extending outward from about 45-60-degrees from the parallel, each of the two opposing side panels comprising a bottom flat edge fit-able to a float (e.g., carbon composite). The middle section further comprises a fuel pump and a fuel line attached to the auxiliary fuel storage tank(s) and to a main fuel tank within an airplane fuselage-engine. Electrical components enable the pilot, or automatedly as needed, to pump fuel from the frame's tanks. The two opposing side panels comprise triangular shaped cutouts to reduce the float frame's weight and drag, and a built-in steps, a bar, and non-skid coating on the floats to assist in climbing safely into/out of the cockpit.

A seaplane float frame apparatus with extra fuel storage, and a method of installing, comprising: 1) a middle section housing at least one auxiliary fuel storage tank; and 2) two opposing side panels affixed to the middle section, extending outward from about 45-60-degrees from the parallel, each of the two opposing side panels comprising a bottom flat edge fit-able to a float (e.g., carbon composite). The middle section further comprises a fuel pump and a fuel line attached to the auxiliary fuel storage tank(s) and to a main fuel tank within an airplane fuselage-engine. Electrical components enable the pilot, or automatedly as needed, to pump fuel from the frame's tanks. The two opposing side panels comprise triangular shaped cutouts to reduce the float frame's weight and drag, and a built-in steps, a bar, and non-skid coating on the floats to assist in climbing safely into/out of the cockpit.