diff --git a/empennage_design/src/taw/conventional/low/lowConventionalEmpennageDesignPlot.cpp b/empennage_design/src/taw/conventional/low/lowConventionalEmpennageDesignPlot.cpp
index 8f074b052526045ca7b46ce017fcb116c605bb8d..952e9c0361373af1cb7e32f14cb3d1a23a37f835 100644
--- a/empennage_design/src/taw/conventional/low/lowConventionalEmpennageDesignPlot.cpp
+++ b/empennage_design/src/taw/conventional/low/lowConventionalEmpennageDesignPlot.cpp
@@ -110,6 +110,10 @@ fs::path Conventional::plot_stabilizer_planform(
     const geom2::MultisectionSurface<geom2::AirfoilSection>& surface,
     const std::vector<geom2::MultisectionSurface<geom2::PolygonSection>>& spars,
     const std::vector<geom2::MultisectionSurface<geom2::PolygonSection>>& devices) {
+  /* Plot active */
+  if (!rtIO->plotOn) {
+    return "";
+  }
   auto coordinates_xy = geom2::transform::outline_2d(surface, geom2::Direction_3(0, 0, 1));
   std::deque<double> spanwise;
   std::deque<double> chordwise;
@@ -185,7 +189,7 @@ fs::path Conventional::plot_stabilizer_planform(
     ax->xlabel("y [m]");
     ax->ylabel("x [m]");
   }
-  
+
   ax->limits_mode(matplot::manual);
   ax->axis(matplot::equal);
   if (is_vertical) {
@@ -208,6 +212,10 @@ fs::path Conventional::plot_stabilizer_planform(
 
 fs::path Conventional::plot_thickness_and_twist_distribution(
     const geom2::MultisectionSurface<geom2::AirfoilSection>& surface) {
+  /* Plot active */
+  if (rtIO->plotOn) {
+    return "";
+  }
   std::vector<double> eta;
   std::vector<double> thickness_to_chord_ratio;
   std::vector<double> twist;
@@ -250,6 +258,10 @@ fs::path Conventional::plot_thickness_and_twist_distribution(
  * \return fs::path
  */
 std::vector<fs::path> Conventional::plot_airfoils(const geom2::MultisectionSurface<geom2::AirfoilSection>& surface) {
+  /* Plot active */
+  if (!rtIO->plotOn) {
+    return {""};
+  }
   std::map<std::string, std::vector<geom2::Point_2>> airfoils_data{};
   std::vector<fs::path> airfoil_plots_path;
 
@@ -295,4 +307,4 @@ std::vector<fs::path> Conventional::plot_airfoils(const geom2::MultisectionSurfa
 }
 
 }  // namespace low
-}  // namespace taw
\ No newline at end of file
+}  // namespace taw