Last Updated on 4 years by teboo
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032 03 03 00 Use of aeroplane performance data
032 03 03 01 Take-off
(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.
Syllabus BK Syllabus details and associated Learning Objectives
(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 NTOFP for a MEP aeroplane of given mass and given airfield conditions, and calculate the obstacle clearance based on the NTOFP.
(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.
032 03 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.
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032 03 03 04 Landing
Syllabus BK Syllabus details and associated Learning Objectives
(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.