Last Updated on 4 years by teboo
032 05 01 00 Take-off
032 05 01 01 Take-off (performance data)
(01) Determine from given graphs the field-lenght-limited take-off mass (FLLTOM) and describe situations in which this limitation could be most restrictive for take-off.
(02) Determine from given graphs the climb-limited take-off mass and describe situations in which this limitation could be most restrictive for take-off.
Syllabus BK Syllabus details and associated Learning Objectives
(03) Determine from given graphs the obstacle-limited mass and describe situations in which this limitation could be most restrictive for take-off.
(04) Determine from given graphs the tyre-speed-limited take-off mass.
(05) Determine from given graphs the maximum brake-energy-limited take-off mass.
(06) Determine the take-off V speeds for the actual take-off mass.
(07) Determine the maximum take-off mass using given RTOM tables.
(08) Using RTOM tables, determine the take-off V speeds for the actual take-off weight using appropriate corrections.
(09) Determine the assumed/flex temperature and take-off V speeds using the RTOM tables.
(10) Calculate the break cooling time following a rejected take-off given appropriate data.
032 05 02 00 Drift-down and stabilising altitude
032 05 02 01 Drift-down and stabilising altitude (performance data)
(01) Determine the one-engine-out net stabilising altitude (level-off altitude) from given graphs/tables.
(02) Determine the maximum mass at which the net stabilising altitude with one-engine-out clears the highest relevant obstacle by the required clearance margin.
(03) Determine, using drift-down graphs, fuel used, time and distance travelled in a descent from a cruise flight level to a given altitude.
Syllabus BK Syllabus details and associated Learning Objectives
032 05 03 00 Landing
032 05 03 01 Landing (performance data)
(01) Determine the field length required for landing with a given landing mass from the aeroplane performance data sheets.
(02) Determine the landing and approach climb-limited landing mass from the aeroplane performance data sheets.
(03) “Calculate the maximum allowable landing mass as the lowest of:
— approach-climb- and landing-climb-limited landing mass;
— landing-field-length-limited landing mass;
— structural-limited landing mass.”
(04) Determine the brake cooling time for different landing masses using the aeroplane performance data sheets.