Power step for an aircraft
FIG. 1 is a front perspective view of a power step for an aircraft showing my new design;
FIG. 2 is a front perspective view thereof in open condition, the broken line showing of environmental structure being for illustrative purposes only and forms no part of the claimed design;
FIG. 3 is a left end elevation view of FIG. 1;
FIG. 4 is a right end elevation view of FIG. 1;
FIG. 5 is a rear perspective view of FIG. 1;
FIG. 6 is a front perspective view taken from the opposite end of that shown in FIG. 1;
FIG. 7 is a top perspective view of FIG. 1;
FIG. 8 is a right end elevation view of FIG. 2;
FIG. 9 is a left end elevation view of FIG. 2;
FIG. 10 is a rear perspective view of FIG. 2;
FIG. 11 is a front perspective view taken from the opposite end of that shown in FIG. 2;
FIG. 12 is a bottom perspective view of FIG. 2.
3778011 | December 1973 | Cannon |
4440364 | April 3, 1984 | Cone et al. |
Type: Grant
Filed: Nov 13, 1984
Date of Patent: Jan 13, 1987
Assignee: Power Steps (Kennedale, TX)
Inventor: Keith T. Short (Bedford, TX)
Primary Examiner: James M. Gandy
Assistant Examiner: Kay H. Chin
Attorney: Charles D. Gunter, Jr.
Application Number: 6/670,569