Power step for an aircraft

Description

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.

Referenced Cited
U.S. Patent Documents
3778011 December 1973 Cannon
4440364 April 3, 1984 Cone et al.
Patent History
Patent number: D287714
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
Classifications
Current U.S. Class: Element Or Attachment (9) (D12/345); D12/157