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ATPL Performance Questions in English

Practise Performance

In the conventional still-air aerodynamic model, with constant propulsion efficiency or specific fuel consumption and with neither optimum restricted by speed limits, the speed for maximum endurance: 4 Answers On a long distance flight the gross mass decreases continuously as a consequence of the fuel consumption. The result is: 4 Answers When landing on a wet runway within the aircraft limitations and with adequate landing performance, which technique best helps manage the risk of hydroplaning? 4 Answers Refer to Performance Manual MEP1 Figure 3.1 Normal Procedure Given: OAT 24 °C; Pressure Altitude: 3000'; RWY 12L; Wind 080/12 KT; Take-off Mass: 3800 lbs. Other conditions as associated in the header of the graph. What is the take-off distance over a 50 ft obstacle? 4 Answers Under the standard Part-CAT dry-runway dispatch rule for a performance class A turboprop aeroplane, with no reduced landing distance approval and no steep approach, which statement is correct? 4 Answers The approach climb requirement has been established to ensure: 4 Answers According to CS-25 the landing reference speed VREF may not be less than: 4 Answers Is there any difference between the vertical speed versus forward speed curves for two identical aeroplanes having different masses? (assume zero thrust and wind) 4 Answers Under the standard Part-CAT dry-runway dispatch rule for a performance class A turboprop aeroplane, with no reduced landing distance approval, compare the required LDA at destination and at an alternate for the same landing mass and conditions. It is: 4 Answers For standard dry-runway performance class A turbojet dispatch, without reduced landing distance approval, what fraction of the LDA is the maximum permitted unfactored AFM landing distance from 50 ft? 4 Answers

Other exam subjects ATPL - Airline Transport Pilot Licence