Passenger aircraft
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FIG. 1 is a top plan view of a first embodiment showing our ornamental design for a passenger aircraft;
FIG. 2 is a right side elevational view thereof with the landing gear extended;
FIG. 3 is a left side elevational view thereof with the landing gear extended;
FIG. 4 is a bottom plan view thereof with the landing gear extended;
FIG. 5 is a rear elevational view thereof with the landing gear extended, the rear view of the subsequently described second embodiment being identical thereto;
FIG. 6 is a front elevational view thereof with the landing gear extended, the front view of the subsequently described second embodiment being identical thereto;
FIF. 7 is a rear elevational view thereof with the landing gear retracted, the rear view of the subsequently described second embodiment being identical thereto;
FIG. 8 is a front elevational view thereof with the landing rear retracted, the front view of the subsequently described second embodiment being identical thereto;
FIG. 9 is a right side elevational view of the first embodiment of the present invention with the landing rear retracted;
FIG. 10 is a left side elevational view of the first embodiment of the present invention with the landing gear retracted;
FIG. 11 is a top plan view of a second embodiment of our ornamental design for a passenger aircraft;
FIG. 12 is a right side elevational view of the second embodiment with the landing gear extended;
FIG. 13 is a left side elevational view of the second embodiment with the landing gear extended;
FIG. 14 is a bottom plan view of the second embodiment with the landing gear extended;
FIG. 15 is a rear elevational view of the second embodiment with the landing gear extended;
FIG. 16 is a rear elevational view of the second embodiment with the landing gear retracted;
FIG. 17 is a right side elevational view of the second embodiment with the landing gear retracted;
FIG. 18 is a left side elevational view of the second embodiment with the land gear retracted; and,
FIG. 19 is a bottom plan view of the second embodiment with the landing gear retracted.
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Type: Grant
Filed: Jan 30, 1995
Date of Patent: May 14, 1996
Assignee: Starkraft, Inc. (Ft. Scott, KS)
Inventors: Roger E. Kraft (Ft. Scott, KS), Jeffrey D. Ackland (Shawnee, KS), Harold E. Kraft (Ft. Scott, KS), Martin Hollmann (Monterrey, CA)
Primary Examiner: Kay H. Chin
Law Firm: Hovey, Williams Timmons & Collins
Application Number: 0/34,229
