diff --git a/ROMFS/px4fmu_common/init.d/2100_standard_plane b/ROMFS/px4fmu_common/init.d/2100_standard_plane
index 13ce1359ec..eb5323d695 100644
--- a/ROMFS/px4fmu_common/init.d/2100_standard_plane
+++ b/ROMFS/px4fmu_common/init.d/2100_standard_plane
@@ -7,8 +7,8 @@
 #
 # @output MAIN1 aileron
 # @output MAIN2 elevator
-# @output MAIN3 rudder
-# @output MAIN4 throttle
+# @output MAIN3 throttle
+# @output MAIN4 rudder
 # @output MAIN5 flaps
 # @output MAIN6 gear
 #
diff --git a/ROMFS/px4fmu_common/mixers/AETRFG.main.mix b/ROMFS/px4fmu_common/mixers/AETRFG.main.mix
index 9ae1d7302b..47de4ed3e0 100644
--- a/ROMFS/px4fmu_common/mixers/AETRFG.main.mix
+++ b/ROMFS/px4fmu_common/mixers/AETRFG.main.mix
@@ -7,7 +7,7 @@ assumes the aileron servo(s) are connected to output 0, the elevator to
 output 1, the throttle to output 2 and the rudder to output 3.
 
 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
-(roll), 1 (pitch), 2 (yaw), 3 (thrust), 4 (flaps), 7 (landing gear)
+(roll), 1 (pitch), 2 (thrust), 3 (yaw), 4 (flaps), 7 (landing gear)
 
 CH1: Aileron mixer
 -------------