diff --git a/Makefile b/Makefile
index 135f172..0f9a7c7 100644
--- a/Makefile
+++ b/Makefile
@@ -7,6 +7,7 @@ ifeq ($(UNAME), Darwin)
 endif
 
 AIRFOILS = ag24.dat m1-il.dat
+TAIL = t-tail
 
 b: build/allparts.svg
 
@@ -15,15 +16,15 @@ build:
 
 build/assembly.scad: src/*.rs $(AIRFOILS)
 	mkdir -p build
-	cargo run t-tail assembly
+	cargo run $(TAIL) assembly
 
 build/part%.scad: src/*.rs $(AIRFOILS)
 	mkdir -p build
-	cargo run parts t-tail
+	cargo run parts $(TAIL)
 
 build/allparts.scad: src/*.rs $(AIRFOILS)
 	mkdir -p build
-	cargo run sheet t-tail
+	cargo run sheet $(TAIL)
 
 e393.dat:
 	curl http://airfoiltools.com/airfoil/seligdatfile?airfoil=e393-il -o e393.dat
@@ -59,11 +60,11 @@ build/%.dxf:  build/%.scad
 build/%.dwg:  build/%.svg
 	svg2dwg -no-gui -no-dock-icon -o $@ $<
 
-.PHONY: svgs dxfs clean b
-svgs: build/%.scad
+.PHONY: svgs dxfs clean b v-tail
+svgs: build/part%.scad
 	ls build/part*.scad | sed 's/scad/svg/' | xargs make
 
-dxfs: build/%.scad
+dxfs: build/part%.scad
 	ls build/part*.scad | sed 's/scad/dxf/' | xargs make
  
 clean:
@@ -74,12 +75,18 @@ clean:
 vis: build/assembly-clear.scad
 	openscad build/assembly-clear.scad
 
+v-tail: src/*.rs $(AIRFOILS)
+	cargo run v-tail assembly sheet parts
+
+t-tail: src/*.rs $(AIRFOILS)
+	cargo run t-tail assembly sheet parts
+
 build/testwing-clear.scad: build/testwing.scad
 	sed 's/color("clear-red")/color([1.0,1.0,0.0,0.9])/g' $< > $@
 	sed 's/color("clear-blue")/color([0.0,1.0,1.0,1.0])/g' -i $@
 
 build/assembly-clear.scad: build/assembly.scad
-	cargo run --features assembly t-tail film
+	cargo run --features assembly $(TAIL) film
 	sed 's/color("clear-red")/color([1.0,0.0,0.0,0.5])/g' $< > $@
 	sed 's/color("clear-blue")/color([0.0,1.0,0.0,0.9])/g' -i $@
 	sed 's/color("clear-blue")/color([0.0,0.0,1.0,0.9])/g' -i $@
diff --git a/src/main.rs b/src/main.rs
index ac0c177..32d65f2 100644
--- a/src/main.rs
+++ b/src/main.rs
@@ -161,6 +161,8 @@ fn v_tail(
     ruddervator.add_child(struts.visualization);
     ruddervator.add_child(spar.visualization);
     ruddervator = scad!(Translate(vec3(0.0, FUSELAGE_GAP, 0.0)); ruddervator);
+    parts.append(struts.parts.clone().as_mut());
+    parts.append(spar.parts.clone().as_mut());
     parts.append(struts.parts.as_mut());
     parts.append(spar.parts.as_mut());
     ruddervators.add_child(scad!(Mirror(vec3(0.0, 1.0, 0.0)); ruddervator.clone()));