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032 02 00 00 CS-23/EU-OPS PERFORMANCE CLASS B — THEORY
032 02 01 00 Airworthiness requirements
032 02 01 01 Airworthiness requirements and definitions
(01) X “Define the following speeds:
— stall speeds VS, VS0 and VS1;
— rotation speed VR;
— speed at 50 ft above the take-off surface level;
— reference landing speed VREF.”
(02) Describe the limitations on VR, on the speed at 50 ft above the take- off surface and on VREF, and given the appropriate stall speed, estimate the values based on these limitations for a single-engine, class B aeroplane.
(03) Describe the limitations on VR, on the speed at 50 ft above the take- off surface and on VREF, and given the appropriate stall speed, estimate the values based on these limitations for a multi-engine, class B aeroplane.
(04) X Describe the European Union airworthiness requirements according to CS-23 relating to aeroplane performance (CS-23 SUBPART A — GENERAL, PERFORMANCE, CS 23.45 to CS 23.78 inclusive).
Syllabus BK Syllabus details and associated Learning Objectives
(05) Define and identify the critical engine of a multi-engine propeller aeroplane.
(06) Explain the effect of an engine failure on the power required, the total drag (thrust required) and climb performance of a multi-engine aeroplane.
(07) Explain the effect of engine failure on the minimum control speed of a multi-engine aeroplane under given conditions (temperature and pressure altitude).
032 02 02 00 Intentionally left blank
032 02 03 00 Take-off and landing
032 02 03 01 Take-off and landing (definitions and effects)
(01) X “Define the following distances and masses:
— take-off distance;
— landing distance;
— ground-roll distance;
— maximum allowed take-off mass;
— maximum allowed landing mass.”
(02) Explain the effect of flap-setting on the take-off, landing and ground- roll distances.
(03) “Explain the effects of the following runway (RWY) variables on take- off distances:
— RWY slope;
— RWY surface conditions: dry, wet and contaminated;
— RWY elevation.”
Syllabus BK Syllabus details and associated Learning Objectives
(04) For both fixed-pitch and constant-speed propeller aeroplanes, explain the effect of airspeed on thrust during the take-off run.
(05) Describe the effects of brake release before take-off power is set on the TOD and ASD.
(06) Explain the effect of wind on take-off and landing distances, and determine the actual headwind/tailwind component given the runway direction, wind speed and direction, by use of wind component graphs, mathematical calculations, and rule of thumb.
(07) Explain why an aeroplane has maximum crosswind limit(s) and determine the crosswind component given the runway direction, wind speed and direction, by use of wind component graphs, mathematical calculations, and rule of thumb.
(08) Explain the percentage of accountability for headwind and tailwind components during take-off and landing calculations.
(09) Explain the effect of runway conditions on the landing distance.
(10) Explain the effects of pressure altitude and temperature on the take- off distance, take-off climb, landing distance and approach climb.
(11) Describe the landing airborne distance and ground-roll distance and estimate the effect on the landing distance when the aeroplane is too fast or too high at the screen.
(12) Describe the net take-off flight path (NTOFP) for a multi-engine, class B aeroplane.
(13) Describe the dimensions of the NTOFP accountability area (domain).
032 02 04 00 Climb, cruise and descent
Syllabus BK Syllabus details and associated Learning Objectives
032 02 04 01 Climb, cruise and descent (requirements and calculations)
(01) Describe the climb and en-route requirements according to the applicable operational requirements.
(02) For a single-engine aeroplane, calculate the expected obstacle clearance (in visual meteorological conditions (VMC)) given gross climb performance, obstacle height and distance from reference zero.
(03) For a single-engine aeroplane, calculate the net glide gradient and net glide distance, given aeroplane altitude, terrain elevation, gross gradient or lift/drag ratio (L/D ratio), and headwind or tailwind component.