FIG. 1 is a perspective view of a trim for aircraft panels.
FIG. 2 is a partial, enlarged view of FIG. 1.
FIG. 3 is a front view of the trim for aircraft panels of FIG. 1.
FIG. 4 is a rear view of the trim for aircraft panels of FIG. 1.
FIG. 5 is a left side view of the trim for aircraft panels of FIG. 1.
FIG. 6 is a right side view of the trim for aircraft panels of FIG. 1.
FIG. 7 is a top view of the trim for aircraft panels of FIG. 1.
FIG. 8 is a bottom view of the trim for aircraft panels of FIG. 1.
FIG. 9 is a left side, bottom perspective view of the trim for aircraft panels of FIG. 1.
FIG. 10 is a partial, enlarged view of FIG. 9.
FIG. 11 is a right side, bottom perspective view of the trim for aircraft panels of FIG. 1.
FIG. 12 is a partial, enlarged view of FIG. 11.
FIG. 13 is a rear perspective view of the trim for aircraft panels of FIG. 1.
FIG. 14 is a partial, enlarged view of FIG. 13.
FIG. 15 is a top perspective view of the trim for aircraft panels of FIG. 1.
FIG. 16 is a bottom perspective view of the trim for aircraft panels of FIG. 1.
FIG. 17 is a perspective view of the trim for aircraft panels of FIG. 1 shown coupled to panels of an aircraft
FIG. 18 is a partial, enlarged view of FIG. 17.
FIG. 19 is a rear view of FIG. 17.
FIG. 20 is a bottom perspective view of FIG. 17; and,
FIG. 21 is an enlarged top partial view of FIG. 17.
The breaks in the drawings illustrate no specific length. The breaks indicate that the trim for aircraft panels can have varies lengths without departing from the scope of this invention. The features shown in broken lines form no part of the claimed design. The features shown in broken lines are for illustrative purposes only or show environment.