diff --git a/sw/logalizer/flight_gear.h b/sw/logalizer/flight_gear.h
index 5aef329600..95d0542fe8 100644
--- a/sw/logalizer/flight_gear.h
+++ b/sw/logalizer/flight_gear.h
@@ -109,7 +109,7 @@ struct FGNetCtrls {
 };
 
 
-#define FG_NET_FDM_VERSION 23
+#define FG_NET_FDM_VERSION 24
 #define FG_NET_FDM_MAX_ENGINES 4
 #define FG_NET_FDM_MAX_WHEELS  3
 #define FG_NET_FDM_MAX_TANKS   4
@@ -141,12 +141,9 @@ struct FGNetFDM {
   float v_north;              // north velocity in local/body frame, fps
   float v_east;               // east velocity in local/body frame, fps
   float v_down;               // down/vertical velocity in local/body frame, fps
-  float v_wind_body_north;    // north velocity in local/body frame
-                              // relative to local airmass, fps
-  float v_wind_body_east;     // east velocity in local/body frame
-                              // relative to local airmass, fps
-  float v_wind_body_down;     // down/vertical velocity in local/body
-                              // frame relative to local airmass, fps
+  float v_body_u;             // ECEF velocity in body frame
+  float v_body_v;             // ECEF velocity in body frame
+  float v_body_w;             // ECEF velocity in body frame
 
   // Accelerations
   float A_X_pilot;            // X accel in body frame ft/sec^2
@@ -163,6 +160,7 @@ struct FGNetFDM {
   uint32_t eng_state[FG_NET_FDM_MAX_ENGINES];// Engine state (off, cranking, running)
   float rpm[FG_NET_FDM_MAX_ENGINES];       // Engine RPM rev/min
   float fuel_flow[FG_NET_FDM_MAX_ENGINES]; // Fuel flow gallons/hr
+  float fuel_px[FG_NET_FDM_MAX_ENGINES];      // Fuel pressure psi
   float egt[FG_NET_FDM_MAX_ENGINES];       // Exhuast gas temp deg F
   float cht[FG_NET_FDM_MAX_ENGINES];       // Cylinder head temp deg F
   float mp_osi[FG_NET_FDM_MAX_ENGINES];    // Manifold pressure
diff --git a/sw/simulator/flight_gear.h b/sw/simulator/flight_gear.h
index 6951926a4e..ce9639950e 100644
--- a/sw/simulator/flight_gear.h
+++ b/sw/simulator/flight_gear.h
@@ -122,9 +122,9 @@ struct FGNetFDM {
   float v_north;              // north velocity in local/body frame, fps
   float v_east;               // east velocity in local/body frame, fps
   float v_down;               // down/vertical velocity in local/body frame, fps
-  float v_body_u;    // ECEF velocity in body frame
-  float v_body_v;    // ECEF velocity in body frame
-  float v_body_w;    // ECEF velocity in body frame
+  float v_body_u;             // ECEF velocity in body frame
+  float v_body_v;             // ECEF velocity in body frame
+  float v_body_w;             // ECEF velocity in body frame
 
   // Accelerations
   float A_X_pilot;            // X accel in body frame ft/sec^2
@@ -137,17 +137,17 @@ struct FGNetFDM {
   // Pressure
 
   // Engine status
-  uint32_t num_engines;	     // Number of valid engines
-  uint32_t eng_state[FG_NET_FDM_MAX_ENGINES];// Engine state (off, cranking, running)
-  float rpm[FG_NET_FDM_MAX_ENGINES];	     // Engine RPM rev/min
-  float fuel_flow[FG_NET_FDM_MAX_ENGINES]; // Fuel flow gallons/hr
-  float fuel_px[FG_NET_FDM_MAX_ENGINES];   // Fuel pressure psi
-  float egt[FG_NET_FDM_MAX_ENGINES];	     // Exhuast gas temp deg F
-  float cht[FG_NET_FDM_MAX_ENGINES];	     // Cylinder head temp deg F
-  float mp_osi[FG_NET_FDM_MAX_ENGINES];    // Manifold pressure
-  float tit[FG_NET_FDM_MAX_ENGINES];	     // Turbine Inlet Temperature
-  float oil_temp[FG_NET_FDM_MAX_ENGINES];  // Oil temp deg F
-  float oil_px[FG_NET_FDM_MAX_ENGINES];    // Oil pressure psi
+  uint32_t num_engines;                       // Number of valid engines
+  uint32_t eng_state[FG_NET_FDM_MAX_ENGINES]; // Engine state (off, cranking, running)
+  float rpm[FG_NET_FDM_MAX_ENGINES];          // Engine RPM rev/min
+  float fuel_flow[FG_NET_FDM_MAX_ENGINES];    // Fuel flow gallons/hr
+  float fuel_px[FG_NET_FDM_MAX_ENGINES];      // Fuel pressure psi
+  float egt[FG_NET_FDM_MAX_ENGINES];          // Exhuast gas temp deg F
+  float cht[FG_NET_FDM_MAX_ENGINES];          // Cylinder head temp deg F
+  float mp_osi[FG_NET_FDM_MAX_ENGINES];       // Manifold pressure
+  float tit[FG_NET_FDM_MAX_ENGINES];          // Turbine Inlet Temperature
+  float oil_temp[FG_NET_FDM_MAX_ENGINES];     // Oil temp deg F
+  float oil_px[FG_NET_FDM_MAX_ENGINES];       // Oil pressure psi
 
   // Consumables
   uint32_t num_tanks;         // Max number of fuel tanks