diff --git a/sw/airborne/firmwares/rotorcraft/guidance/guidance_indi_hybrid.c b/sw/airborne/firmwares/rotorcraft/guidance/guidance_indi_hybrid.c
index 0d38d8c57e..a5ad216dd8 100644
--- a/sw/airborne/firmwares/rotorcraft/guidance/guidance_indi_hybrid.c
+++ b/sw/airborne/firmwares/rotorcraft/guidance/guidance_indi_hybrid.c
@@ -558,7 +558,7 @@ struct StabilizationSetpoint guidance_indi_run(struct FloatVect3 *accel_sp, floa
   float thrust_vect[3];
 #if GUIDANCE_INDI_HYBRID_U > 3
   thrust_vect[0] = du_gih[3];
-  if (thrust_vect[0] > MAX_PUSHER_INCREMENT*guidance_indi_thrust_x_eff) {
+  if (thrust_vect[0] > GUIDANCE_INDI_MAX_PUSHER_INCREMENT*guidance_indi_thrust_x_eff) {
     thrust_vect[0] = GUIDANCE_INDI_MAX_PUSHER_INCREMENT*guidance_indi_thrust_x_eff;
   }
 #else