RSickenberg · January 10, 2025 11:57
diff --git a/032.02.txt b/032.02.txt
 03.01 Takeoff
 01 Determine the field-length-limited take-off mass and take-off speeds given defactored distance, configuration, pressure altitude, temperature and headwind/tailwind component.
 02 Determine the accelerate-go distance and accelerate-stop distance data.
 03 Determine the ground-roll distance and take-off distance from graphs.
 04 Determine the all-engine-out and critical-engine-out take-off climb data.
 05 Determine take-off flight path for a MEP aeroplane of given mass and given airfield conditions and calculate the obstacle clearance based on the take-off flight path.
 06 Determine the minimum headwind or maximum tailwind component required for take-off for a given mass and given airfield conditions.
 07 Given take-off run available (TORA), TODA and ASDA, slope and surface conditions, calculate the defactored distance to be used for commercial air transport using the appropriate take-off graphs
 08 Calculate the minimum TORA or TODA for commercial air transport given the defactored take-off distance or run, runway surface and slope.

 03.02 Climb
 01 Determine rate of climb.
 02 Calculate obstacle clearance climb data.
 03 Determine the still-air and flight-path gradients for given IAS, altitude, temperature, aeroplane weight and, if relevant, wind component.

 03.04 Landing
 01 Determine the field-length-limited landing mass and landing speeds given defactored distance, configuration, pressure altitude, temperature and headwind or tailwind component.
 02 Determine landing climb data in the event of balked landing
 03 Determine landing distance and ground-roll distance for given flap position, aeroplane weight and airfield data.
 04 Calculate, given the landing distance available (LDA), slope and surface type and condition, the defactored distance to be used for commercial air transport using the appropriate landing graphs.
 05 Calculate the minimum landing distance (LD) that must be available for commercial air transport given the defactored landing distance, runway surface and slope.
	03.01 Takeoff
	01 Determine the field-length-limited take-off mass and take-off speeds given defactored distance, configuration, pressure altitude, temperature and headwind/tailwind component.
	02 Determine the accelerate-go distance and accelerate-stop distance data.
	03 Determine the ground-roll distance and take-off distance from graphs.
	04 Determine the all-engine-out and critical-engine-out take-off climb data.
	05 Determine take-off flight path for a MEP aeroplane of given mass and given airfield conditions and calculate the obstacle clearance based on the take-off flight path.
	06 Determine the minimum headwind or maximum tailwind component required for take-off for a given mass and given airfield conditions.
	07 Given take-off run available (TORA), TODA and ASDA, slope and surface conditions, calculate the defactored distance to be used for commercial air transport using the appropriate take-off graphs
	08 Calculate the minimum TORA or TODA for commercial air transport given the defactored take-off distance or run, runway surface and slope.

	03.02 Climb
	01 Determine rate of climb.
	02 Calculate obstacle clearance climb data.
	03 Determine the still-air and flight-path gradients for given IAS, altitude, temperature, aeroplane weight and, if relevant, wind component.

	03.04 Landing
	01 Determine the field-length-limited landing mass and landing speeds given defactored distance, configuration, pressure altitude, temperature and headwind or tailwind component.
	02 Determine landing climb data in the event of balked landing
	03 Determine landing distance and ground-roll distance for given flap position, aeroplane weight and airfield data.
	04 Calculate, given the landing distance available (LDA), slope and surface type and condition, the defactored distance to be used for commercial air transport using the appropriate landing graphs.
	05 Calculate the minimum landing distance (LD) that must be available for commercial air transport given the defactored landing distance, runway surface and slope.