cdata =
{

	A4E_AIRCRAFTNAME                  		= _('A-4E-C'),

	A4E_PROJECTPAGE          				= _('https://08jne01.github.io/community-a4e-c/'),

	A4E_TRIMSPEED_PITCH_LABEL          		= _('Trim Speed: Elevator (Pitch)'),
	A4E_TRIMSPEED_ROLL_LABEL           		= _('Trim Speed: Aileron (Roll)'),
	A4E_TRIMSPEED_RUDDER_LABEL         		= _('Trim Speed: Rudder (Yaw)'),
	A4E_TRIM_SPEED_SLIDER_HELP        		= _('Trim speeds also affect "Trim Reset (Hold)" - Default: 100%'),

	A4E_THROTTLE_RATE_LABEL	        		= _('Throttle Increment'),
	A4E_THROTTLE_RATE_HELP	        		= _('Percentage change applied by "Throttle Position - Increment/Decrement" - Default: 1.0%'),

	A4E_THROTTLE_ACCELERATION_LABEL	    	= _('Custom Throttle Rate'),
	A4E_THROTTLE_ACCELERATION_HELP	       	= _('Determines the accelleration rate for "Custom Throttle Rate" inputs - Default: 50%'),

--	A4E_CATLAUNCHMODE_LABEL           		= _('Catapult Launch Mode'),
--	A4E_CATLAUNCHMODE_HELP            		= _('Launch the catapult when throttle at MIL POWER.'),
--	A4E_CATLAUNCHMODE_HELP2           		= _('Launch the catapult with the Pilot Salute command'),

--	A4E_CATAPULT_ALIGNMENT_CHECK_TEXT 		= _('Bypass Catapult Alignment Check'),
--	A4E_CATAPULT_ALIGNMENT_CHECK_HELP 		= _('Check if aircraft is aligned with a catapult before allowing catapult hook up.'),

--	A4E_EXPERIMENTAL_EFM_CHECK_TEXT	  		= _('Enable the experimental EFM'),
--	A4E_EXPERIMENTAL_EFM_CHECK_HELP   		= _('Should the A-4E-C use the experimental external flight model or the simple flight model.'),

	A4E_COCKPIT_SHAKE_SLIDER_LABEL 	  		= _('Cockpit Shake'),
	A4E_COCKPIT_SHAKE_SLIDER_HELP	  		= _('Amount of cockpit and head position shake effect - Default: 100%'),

	A4E_COCKPIT_CSS_LABEL			  		= _('FFB CSS Mode Deflection'),
	A4E_COCKPIT_CSS_HELP			  		= _('Force Feedback Stick deflection point at which AFCS engages Control Stick Steering - Default: 15%'),

	A4E_WHEEL_BRAKE_ASSIST_CHECK_LABEL 		= _('Simple Braking (Rudder-Assisted)'),
	A4E_WHEEL_BRAKE_ASSIST_CHECK_TOOLTIP 	= _('Simple Braking Enabled'),
	A4E_WHEEL_BRAKE_ASSIST_CHECK_HELP  		= _('When enabled, "Wheel Brake" applies Left and Right Wheelbrakes in proportion to rudder input'),

	A4E_OLD_RADAR_CHECK_LABEL 				= _('AN/APG-53A Radar Legacy Mode'),
	A4E_OLD_RADAR_CHECK_TOOLTIP 			= _('AN/APG-53A Radar Legacy Mode Enabled'),
	A4E_OLD_RADAR_CHECK_HELP 				= _('Enables low-definition ground radar (performance mode)'),

	A4E_CUSTOM_FCS_PITCH_PRESSURE_LABEL		= _('Pitch Deflection'),
	A4E_CUSTOM_FCS_PITCH_RELEASE_LABEL		= _('Pitch Recentering'),
	A4E_CUSTOM_FCS_ROLL_PRESSURE_LABEL		= _('Roll Deflection'),
	A4E_CUSTOM_FCS_ROLL_RELEASE_LABEL		= _('Roll Recentering'),
	A4E_CUSTOM_FCS_RUDDER_PRESSURE_LABEL	= _('Rudder Deflection'),
	A4E_CUSTOM_FCS_RUDDER_RELEASE_LABEL		= _('Rudder Recentering'),
	A4E_CUSTOM_FCS_HELP1					= _('Flight Control sensetivity for Aircraft Pitch, Roll, and Rudder button inputs.'),
	A4E_CUSTOM_FCS_HELP2					= _('Set Recentering to 0 for a non-centering input.'),
	A4E_CUSTOM_FCS_HELP3					= _('- Defaults:   - Pitch: D.50, R.0   - Roll: D.50, R.100   - Rudder: D.50, R.100'),

}
