Quiz ATPL | Pagina 17

When determining the maximum landing mass of an turbojet powered aeroplane during the planning phase what factor must be used on the landing distance available (dry runway)	4 risposte
The landing reference speed VREF has, in accordance with CS 25, the following margins above reference stall speed in landing configuration:	4 risposte
According to PART-CAT, which one of the following statements concerning the landing distance for a turbojet aeroplane is correct?	4 risposte
What is the minimum field length required for the worst wind situation, landing a twin jet aeroplane with the anti-skid inoperative?Elevation: 2000 ftQNH: 1013 hPaLanding mass: 50 000 kgFlaps: as required for minimum landing distance Runway condition: dryWind:Maximum allowable tailwind: 15 kt Maximum allowable headwind: 50 kt	4 risposte
If a flight is performed with a higher 'Cost Index' at a given mass which of the following will occur?	4 risposte
Which statement is correct for a descent without engine thrust at maximum lift to drag ratio speed?	4 risposte
The maximum mass for landing could be limited by	4 risposte
The landing field length required for turbojet aeroplanes at the destination (wet condition) is the demonstrated landing distance plus:	4 risposte
The landing field length required for jet aeroplanes at the alternate (wet condition) is the demonstrated landing distance plus	4 risposte
What is the most important aspect of the 'backside of the power curve'?	4 risposte

ATPL - Airline Transport Pilot license - Performance Pagina 17