diff --git a/firmware/controllers/algo/fuel_math.cpp b/firmware/controllers/algo/fuel_math.cpp
index 5b4365850b..7ef4e9bd10 100644
--- a/firmware/controllers/algo/fuel_math.cpp
+++ b/firmware/controllers/algo/fuel_math.cpp
@@ -86,7 +86,7 @@ floatms_t getBaseFuel(int rpm DECLARE_ENGINE_PARAMETER_S) {
 	return ENGINE(engineState.tpsAccelEnrich) + ENGINE(engineState.baseFuel);
 }
 
-float getinjectionOffset(int rpm DECLARE_ENGINE_PARAMETER_S) {
+float getinjectionOffset(float rpm DECLARE_ENGINE_PARAMETER_S) {
 	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_F);
 	return fuelPhaseMap.getValue(rpm, engineLoad);
 }
diff --git a/firmware/controllers/algo/fuel_math.h b/firmware/controllers/algo/fuel_math.h
index fafe0d496d..ff51bbd39b 100644
--- a/firmware/controllers/algo/fuel_math.h
+++ b/firmware/controllers/algo/fuel_math.h
@@ -27,7 +27,7 @@ floatms_t getRealMafFuel(float airMass, int rpm DECLARE_ENGINE_PARAMETER_S);
 floatms_t getBaseTableFuel(engine_configuration_s *engineConfiguration, int rpm, float engineLoad);
 float getBaroCorrection(DECLARE_ENGINE_PARAMETER_F);
 
-float getinjectionOffset(int rpm DECLARE_ENGINE_PARAMETER_S);
+float getinjectionOffset(float rpm DECLARE_ENGINE_PARAMETER_S);
 float getIatCorrection(float iat DECLARE_ENGINE_PARAMETER_S);
 floatms_t getInjectorLag(float vBatt DECLARE_ENGINE_PARAMETER_S);
 float getCltCorrection(float clt DECLARE_ENGINE_PARAMETER_S);
diff --git a/firmware/controllers/core/table_helper.cpp b/firmware/controllers/core/table_helper.cpp
index 955a0954fc..acf6bc70ad 100644
--- a/firmware/controllers/core/table_helper.cpp
+++ b/firmware/controllers/core/table_helper.cpp
@@ -22,7 +22,7 @@ void setTableBin2(float array[], int size, float l, float r, float precision) {
 
 void setRpmBin(float array[], int size, float idleRpm, float topRpm) {
 	array[0] = idleRpm - 150;
-	int rpmStep = efiRound((topRpm - idleRpm) / (size - 2), 50) - 150;
+	int rpmStep = (int)(efiRound((topRpm - idleRpm) / (size - 2), 50) - 150);
 	for (int i = 1; i < size - 1;i++)
 		array[i] = idleRpm + rpmStep * (i - 1);
 	array[size - 1] = topRpm;