diff --git a/firmware/controllers/algo/airmass/lua_airmass.h b/firmware/controllers/algo/airmass/lua_airmass.h
new file mode 100644
index 0000000000..3250ebde64
--- /dev/null
+++ b/firmware/controllers/algo/airmass/lua_airmass.h
@@ -0,0 +1,17 @@
+#pragma once
+
+#include "airmass.h"
+
+class LuaAirmass final : public AirmassModelBase {
+public:
+	AirmassResult getAirmass(int /*rpm*/) override {
+		return m_airmass;
+	}
+
+	void setAirmass(AirmassResult airmass) {
+		m_airmass = airmass;
+	}
+
+private:
+	AirmassResult m_airmass;
+};
diff --git a/firmware/controllers/algo/fuel_math.cpp b/firmware/controllers/algo/fuel_math.cpp
index be1d3293fa..0b85bd0482 100644
--- a/firmware/controllers/algo/fuel_math.cpp
+++ b/firmware/controllers/algo/fuel_math.cpp
@@ -38,6 +38,7 @@
 #include "perf_trace.h"
 #include "sensor.h"
 #include "speed_density_base.h"
+#include "lua_hooks.h"
 
 EXTERN_ENGINE;
 
@@ -170,6 +171,9 @@ AirmassModelBase* getAirmassModel(engine_load_mode_e mode DECLARE_ENGINE_PARAMET
 		case LM_SPEED_DENSITY: return &sdAirmass;
 		case LM_REAL_MAF: return &mafAirmass;
 		case LM_ALPHA_N: return &alphaNAirmass;
+#if EFI_LUA
+		case LM_LUA: return &(getLuaAirmassModel());
+#endif
 #if EFI_UNIT_TEST
 		case LM_MOCK: return engine->mockAirmassModel;
 #endif
diff --git a/firmware/controllers/algo/rusefi_enums.h b/firmware/controllers/algo/rusefi_enums.h
index f94d33ad6b..32e5c10135 100644
--- a/firmware/controllers/algo/rusefi_enums.h
+++ b/firmware/controllers/algo/rusefi_enums.h
@@ -501,6 +501,8 @@ typedef enum {
 
 	LM_ALPHA_N = 5,
 
+	LM_LUA = 6,
+
 	// This mode is for unit testing only, so that tests don't have to rely on a particular real airmass mode
 	LM_MOCK = 100,
 
diff --git a/firmware/controllers/lua/lua_hooks.cpp b/firmware/controllers/lua/lua_hooks.cpp
index 3007716af0..fd8df50c4f 100644
--- a/firmware/controllers/lua/lua_hooks.cpp
+++ b/firmware/controllers/lua/lua_hooks.cpp
@@ -7,6 +7,9 @@
 #include "adc_inputs.h"
 #include "efilib.h"
 #include "tunerstudio_outputs.h"
+#include "fuel_math.h"
+#include "airmass.h"
+#include "lua_airmass.h"
 #include "pwm_generator_logic.h"
 
 // Some functions lean on existing FSIO implementation
@@ -64,6 +67,12 @@ static int lua_table3d(lua_State* l) {
 	return 1;
 }
 
+static LuaAirmass luaAirmass;
+
+AirmassModelBase& getLuaAirmassModel() {
+	return luaAirmass;
+}
+
 #if !EFI_UNIT_TEST
 static SimplePwm pwms[LUA_PWM_COUNT];
 static OutputPin pins[LUA_PWM_COUNT];
@@ -177,6 +186,42 @@ static int lua_setDebug(lua_State* l) {
 	return 0;
 }
 
+static auto lua_getAirmassResolveMode(lua_State* l) {
+	if (lua_gettop(l) == 0) {
+		// zero args, return configured mode
+		return CONFIG(fuelAlgorithm);
+	} else {
+		return static_cast<engine_load_mode_e>(luaL_checkinteger(l, 1));
+	}
+}
+
+static int lua_getAirmass(lua_State* l) {
+	auto airmassMode = lua_getAirmassResolveMode(l);
+	auto airmass = getAirmassModel(airmassMode);
+
+	if (!airmass) {
+		return luaL_error(l, "null airmass");
+	}
+
+	auto rpm = Sensor::get(SensorType::Rpm).value_or(0);
+	auto result = airmass->getAirmass(rpm).CylinderAirmass;
+
+	lua_pushnumber(l, result);
+	return 1;
+}
+
+static int lua_setAirmass(lua_State* l) {
+	float airmass = luaL_checknumber(l, 1);
+	float engineLoadPercent = luaL_checknumber(l, 2);
+
+	airmass = clampF(0, airmass, 10);
+	engineLoadPercent = clampF(0, engineLoadPercent, 1000);
+
+	luaAirmass.setAirmass({airmass, engineLoadPercent});
+
+	return 0;
+}
+
 static int lua_stopEngine(lua_State*) {
 	doScheduleStopEngine();
 
@@ -199,6 +244,8 @@ void configureRusefiLuaHooks(lua_State* l) {
 	lua_register(l, "getFan", lua_fan);
 	lua_register(l, "getDigital", lua_getDigital);
 	lua_register(l, "setDebug", lua_setDebug);
+	lua_register(l, "getAirmass", lua_getAirmass);
+	lua_register(l, "setAirmass", lua_setAirmass);
 
 	lua_register(l, "stopEngine", lua_stopEngine);
 #endif
diff --git a/firmware/controllers/lua/lua_hooks.h b/firmware/controllers/lua/lua_hooks.h
index ca2bca57c6..6e2f6dde8c 100644
--- a/firmware/controllers/lua/lua_hooks.h
+++ b/firmware/controllers/lua/lua_hooks.h
@@ -1,4 +1,8 @@
 #pragma once
 
+struct lua_State;
 void configureRusefiLuaHooks(lua_State*);
 void luaDeInitPins();
+
+struct AirmassModelBase;
+AirmassModelBase& getLuaAirmassModel();
diff --git a/firmware/integration/rusefi_config.txt b/firmware/integration/rusefi_config.txt
index 2ba2e4de2e..147818d4a7 100644
--- a/firmware/integration/rusefi_config.txt
+++ b/firmware/integration/rusefi_config.txt
@@ -616,7 +616,7 @@ end_struct
 int sensorSnifferRpmThreshold;+Disable sensor sniffer above this rpm;"RPM", 1, 0, 0, 30000, 0
 	int rpmHardLimit;set rpm_hard_limit X;"rpm", 1, 0, 0, 20000, 2
 
-#define engine_load_mode_e_enum "INVALID", "INVALID", "INVALID", "Speed Density", "MAF Air Charge", "Alpha-N", "INVALID"
+#define engine_load_mode_e_enum "INVALID", "INVALID", "INVALID", "Speed Density", "MAF Air Charge", "Alpha-N", "Lua"
 
 
 custom engine_load_mode_e 4 bits, U32, @OFFSET@, [0:2], @@engine_load_mode_e_enum@@