Aircraft Landing-gear Step

FIG. 1 a bottom perspective view of the aircraft landing-gear step.

FIG. 2 is a front elevational view of the landing-gear step as configured in FIG. 1 .

FIG. 3 is a rear elevational view of the landing-gear step as configured in FIG. 1 .

FIG. 4 is a left side elevational view of the landing-gear step as configured in FIG. 1 .

FIG. 5 is a right side elevational view of the landing-gear step as configured in FIG. 1 .

FIG. 6 is a top plan view of the landing-gear step as configured in FIG. 1 .

FIG. 7 is a bottom plan view of the landing-gear step as configured in FIG. 1 .

FIG. 8 is a top perspective view of the aircraft landing-gear step shown in an environment of use.

FIG. 9 is an oblique view of the left landing-gear step, the door being configured in a closed position.

FIG. 10 is a front elevational view of the landing-gear step as configured in FIG. 9 .

FIG. 11 is a rear elevational view of the landing-gear step as configured in FIG. 9 .

FIG. 12 is a left side elevational view of the landing-gear step as configured FIG. 9 .

FIG. 13 is a right side elevational view of the landing-gear step as configured in FIG. 9 .

FIG. 14 is a top plan view of the landing-gear step as configured in FIG. 9 .

FIG. 15 is a bottom plan view of the landing-gear step as configured in FIG. 9 ; and,

FIG. 16 is an oblique view of the landing-gear step as configured in FIG. 9 .

The broken lines shown in FIGS. 1 - 7 and 9 - 15 illustrate portions of the aircraft landing-gear step that form no part of the claimed design; the additional broken lines shown in FIGS. 8 and 16 are for purposes of illustrating environmental subject matter only and forms no part thereof. The right side not shown is understood to be a mirror image of the left side shown in FIGS. 1 - 8 and 9 - 16 .