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ATPL - 032.05 LO
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| 01.01 Takeoff (Performance Data) | |
| 01 Determine from given graphs the field-length-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. | |
| 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 brake cooling time following a rejected take-off given appropriate data. | |
| 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. | |
| 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. |
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