diff --git a/addons/aircraft/CfgVehicles.hpp b/addons/aircraft/CfgVehicles.hpp
index f5f496505e..8f3be35873 100644
--- a/addons/aircraft/CfgVehicles.hpp
+++ b/addons/aircraft/CfgVehicles.hpp
@@ -223,25 +223,16 @@ class CfgVehicles {
     class Plane_CAS_01_base_F: Plane_Base_F {
         lockDetectionSystem = 12;
         incomingMissileDetectionSystem = 16;
-        class Turrets;
-
-        #include <flightmodel_thunderbolt.hpp>
     };
 
     class Plane_CAS_02_base_F: Plane_Base_F {
         lockDetectionSystem = 12;
         incomingMissileDetectionSystem = 16;
-        class Turrets;
-
-        #include <flightmodel_yak.hpp>
     };
 
     class Plane_Fighter_03_base_F: Plane_Base_F {
         lockDetectionSystem = 12;
         incomingMissileDetectionSystem = 16;
-        class Turrets;
-
-        #include <flightmodel_alca.hpp>
     };
 
     class UAV_01_base_F: Helicopter_Base_F {
diff --git a/addons/aircraft/flightmodel_alca.hpp b/addons/aircraft/flightmodel_alca.hpp
deleted file mode 100644
index afe74ef9fd..0000000000
--- a/addons/aircraft/flightmodel_alca.hpp
+++ /dev/null
@@ -1,23 +0,0 @@
-acceleration = 300;
-maxSpeed = 936;
-irScanRangeMin = 500;
-irScanRangeMax = 5000;
-aileronSensitivity = 0.64;
-elevatorSensitivity = 0.682;
-rudderInfluence = 0.001;
-aileronControlsSensitivityCoef = 3;
-elevatorControlsSensitivity = 2;
-rudderControlsSensitivityoef = 4;
-elevatorCoef[] = {0.6, 0.73, 0.62, 0.52, 0.39, 0.33, 0.28};
-aileronCoef[] = {0.5, 0.68, 0.75, 0.86, 0.92, 0.96, 1};
-rudderCoef[] = {0.9, 0.75, 0.58, 0.45, 0.38, 0.35, 0.3};
-envelope[] = {0, 0.06, 1.2, 3, 3.6, 3.75, 3.65, 3.45, 3.3, 2.8, 2.4, 1.9, 1.5};
-angleOfIndicence = 0.0523599;  //determines velocity vector behaviour,  how quickly it catches up with where your nose is pointing,  I think
-draconicForceXCoef = 7.5;  //max angle of attack,  lower value gives higher aoa
-draconicForceYCoef = 0.2198;  //Something to do with bleed off of speed,  low values seem to increase bleed off
-draconicForceZCoef = 5.12;  //????
-draconicTorqueXCoef = 0.18;  //resistance to elevator input,  also impacts speed degradation
-draconicTorqueYCoef = 0.000017;
-thrustCoef[] = {1.3, 1.27, 1.24, 1.2, 1.17, 1.15, 1.13, 1.1, 1.06, 1, 0.94, 0.72, 0.51, 0.4, 0.25, 0};
-gunAimDown = 0.029;
-flapsFrictionCoef = 0.32;
diff --git a/addons/aircraft/flightmodel_thunderbolt.hpp b/addons/aircraft/flightmodel_thunderbolt.hpp
deleted file mode 100644
index 0f99f5ef91..0000000000
--- a/addons/aircraft/flightmodel_thunderbolt.hpp
+++ /dev/null
@@ -1,21 +0,0 @@
-maxSpeed = 736;
-aileronSensitivity = 0.85;
-elevatorSensitivity = 0.75;
-rudderInfluence = 0.001;
-aileronControlsSensitivityCoef = 3;
-elevatorControlsSensitivity = 2;
-rudderControlsSensitivityoef = 4;
-elevatorCoef[] = {0.7, 0.75, 0.75, 0.65, 0.55, 0.45, 0.35};
-aileronCoef[] = {0.6, 0.85, 0.88, 0.92, 0.95, 0.97, 1};
-rudderCoef[] = {0.8, 0.75, 0.65, 0.5, 0.4, 0.33, 0.3};
-flapsFrictionCoef = 0.35;
-angleOfIndicence = 0.0523599;
-draconicForceXCoef = 9.5;
-draconicForceYCoef = 0.56;
-draconicForceZCoef = 0.1;
-draconicTorqueXCoef = 0.58;
-draconicTorqueYCoef = 0.00013;
-envelope[] = {0, 0, 0.75, 2.4, 3.6, 3.8, 3.7, 3.2, 2.2, 1.7, 0.9};
-thrustCoef[] = {1, 1.2, 1.3, 1.25, 1.06, 1.01, 1, 0.92, 0.75, 0.65, 0.5, 0.25, 0};
-acceleration = 265;
-landingSpeed = 220;
diff --git a/addons/aircraft/flightmodel_yak.hpp b/addons/aircraft/flightmodel_yak.hpp
deleted file mode 100644
index 9ba4c40c76..0000000000
--- a/addons/aircraft/flightmodel_yak.hpp
+++ /dev/null
@@ -1,20 +0,0 @@
-maxSpeed = 1059;
-acceleration = 300;
-aileronSensitivity = 0.635;
-elevatorSensitivity = 0.814;
-rudderInfluence = 0.001;
-aileronControlsSensitivityCoef = 3;
-elevatorControlsSensitivity = 2;
-rudderControlsSensitivityoef = 4;
-elevatorCoef[] = {0.6, 0.76, 0.7, 0.65, 0.58, 0.47, 0.43};
-aileronCoef[] = {0.5, 0.85, 0.87, 0.89, 0.92, 0.95, 1};
-rudderCoef[] = {0.8, 0.7, 0.6, 0.5, 0.4, 0.32, 0.27};
-angleOfIndicence = 0.0523599;
-draconicForceXCoef = 7.6;
-draconicForceYCoef = 0.75;
-draconicForceZCoef = 0.085;
-draconicTorqueXCoef = 0.815;
-draconicTorqueYCoef = 0.000152;
-envelope[] = {0, 0.446, 1.5, 3.9, 5.2, 4.8, 4.2, 3.5, 2, 1, 0.5};
-thrustCoef[] = {1, 1.2, 1.7, 1.7, 1.65, 1.54, 1.32, 1.1, 0.95, 0.75, 0.5, 0.35, 0};
-flapsFrictionCoef = 0.32;