32-02. PERFORMANCE CLASS B – SINGLE-ENGINE AEROPLANES
All questions: 51
In mode TRAINING show all questions of the discipline with correct answers presentation. To go to the next question, click the “Next”.
Questions for exams: 30
In mode Exam correct answers are not shown, after choosing the answer, transition to the next question occurs automatically.
1. (Refer to figure 032-13)
Using the Range Profile Diagram, for the single engine aeroplane, determine the range, with 45 minutes reserve, in the following conditions, given:
OAT: ISA
Pressure altitude: 4.000 ft
Power: Full throttle (25,0 in/Hg and 2.100 RPM)

2. On a reciprocating single-engined aeroplane, to maintain a given angle of attack, configuration and altitude at higher gross mass:
3. According to the information in a light aircraft manual, which gives two power settings for cruise, 65% and 75%. If you fly at 75% instead of 65%:
4. The landing reference speed VREF has, in accordance with international requirements, the following margins above stall speed in landing configuration:
5. What margin above the stall speed is provided by the landing reference speed VREF?