Page 769 - PPL-engelsk 2025
P. 769

Aircraft general knowledge




                Here tou see a schematic

                diagram      showing      the

                function  of  the  air  speed

                indicator.






                The (total) dynamic pressure comes in via the pitot tube.

                The more pressure, the more the spiral tube will expand. This causes, via rods

                and the triangle, a movement of the pointer.


                In the instrument housing itself there is static pressure, so the airspeed indicator

                shows the difference between total pressure and static pressure – namely the

                dynamic pressure.




                8.12.5.1     The airspeed indicator

                Here  you  can  see  the  airspeed  indicator

                pointer itself. As can be seen, there are color

                divisions on the speedometer.


                The white area is the flap area.


                The lowest speed is the stall speed with full
                weight and with the engine idling. The highest

                speed is the max. speed with flaps.


                The green arc is the normal area.


                The lowest value is the stall speed at full weight with the engine idling, and

                without using flaps. The dividing line between the green and yellow areas is
                called VNO.


                Yellow area. Caution must be exercised.


                Red line indicates the maximum permitted speed VNE.




             Flyveteori PPL(A)(UL)/LAPL             Henning Andersen, Midtjysk Flyveskole© 2025               769
   764   765   766   767   768   769   770   771   772   773   774