-print ' Pad[', \
- mm2mils100(WingInner + WingWidth/2), \
- mm2mils100(PadCenter - WingHeight/2 + WingWidth/2), \
- mm2mils100(WingInner + WingWidth/2), \
- mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \
- mm2mils100(WingWidth), \
- (MinClearance*2), \
- mm2mils100(WingWidth)+(MaskDelta*2), \
- '"tab5" "G" 0x0100]'
-
-print ' Pad[', \
- mm2mils100(-WingInner - WingWidth/2), \
- mm2mils100(PadCenter - WingHeight/2 + WingWidth/2), \
- mm2mils100(-WingInner - WingWidth/2), \
- mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \
- mm2mils100(WingWidth), \
- (MinClearance*2), \
- mm2mils100(WingWidth)+(MaskDelta*2), \
- '"tab6" "G" 0x0100]'
-
-# box around actual connector size, with line at PCB edge
-#
-#print ' ElementLine[',\
-# mm2mils100(-BoxWidth/2), \
-# mm2mils100(0), \
-# mm2mils100(-BoxWidth/2), \
-# mm2mils100(BoxHeight), \
-# '1000 ]'
-#
-#print ' ElementLine[',\
-# mm2mils100(BoxWidth/2), \
-# mm2mils100(0), \
-# mm2mils100(BoxWidth/2), \
-# mm2mils100(BoxHeight), \
-# '1000 ]'
-#
-#print ' ElementLine[',\
-# mm2mils100(-BoxWidth/2), \
-# mm2mils100(0), \
-# mm2mils100(BoxWidth/2), \
-# mm2mils100(0), \
-# '1000 ]'
-#
-#print ' ElementLine[',\
-# mm2mils100(-BoxWidth/2), \
-# mm2mils100(BoxHeight), \
-# mm2mils100(BoxWidth/2), \
-# mm2mils100(BoxHeight), \
-# '1000 ]'
-#
-#print ' ElementLine[',\
-# mm2mils100(-EdgeWidth/2), \
-# mm2mils100(EdgeHeight), \
-# mm2mils100(-BoxWidth/2), \
-# mm2mils100(EdgeHeight), \
-# '1000 ]'
-#
-#print ' ElementLine[',\
-# mm2mils100(BoxWidth/2), \
-# mm2mils100(EdgeHeight), \
-# mm2mils100(EdgeWidth/2), \
-# mm2mils100(EdgeHeight), \
-# '1000 ]'
-#
-print ")"
+print(' Pad[', \
+ mm2mils100(WingInner + WingWidth/2), \
+ mm2mils100(PadCenter - WingHeight/2 + WingWidth/2), \
+ mm2mils100(WingInner + WingWidth/2), \
+ mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \
+ mm2mils100(WingWidth), \
+ (MinClearance*2), \
+ mm2mils100(WingWidth)+(MaskDelta*2), \
+ '"tab5" "G" 0x0100]')
+
+print(' Pad[', \
+ mm2mils100(-WingInner - WingWidth/2), \
+ mm2mils100(PadCenter - WingHeight/2 + WingWidth/2), \
+ mm2mils100(-WingInner - WingWidth/2), \
+ mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \
+ mm2mils100(WingWidth), \
+ (MinClearance*2), \
+ mm2mils100(WingWidth)+(MaskDelta*2), \
+ '"tab6" "G" 0x0100]')
+
+print(")")