Welcome!

This website offers free access to 75% of the official exam questions.

Want to prepare even better and access all the available questions? Download our mobile app now and get the complete database to maximize your chances of passing the exam!

Check out the mobile app here

Don’t miss the chance to have all the material always at your fingertips, wherever you are, even offline and without any kind of advertising!

Exam Questions
Training
Exam simulation
PDF Exam
Contact Us
Are you a school?
iOS & Android »
EN
IT
ES
DE
FR

Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone > Performance - ATPL - Airline Transport Pilot license

Quiz Performance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Performance, no time limit

Change Subject New Test

1 - Two identical turbojet aeroplane (whose specific fuel consumptions are considered to be equal) are at holding speed at the same altitude.The mass of the first aircraft is 130000 kg and its hourly fuel consumption is 4300 kg/h. The mass of the second aircraft is 115000 kg and its hourly fuel consumption is: 4044 kg / h 3365 kg / h 3804 kg / h 3578 kg / h

2 - At reference or use or Performance Manual MEP 1 Figure 3.2 Given:OAT: 25°CPressure Altitude: 3000 ft RWY: 24LWind: 310°/20ktsTake off Mass: 4400 lbs Heavy Duty Brakes installed.Other conditions as associated in the header of the graph.What is the Accelerate and Stop Distance under the conditions given? 3750 ft 3350 ft 4000 ft 4300 ft

3 - A higher outside air temperature (OAT): Increases the climb limited take-off mass Increases the field length limited take-off mass Decreases the take-off distance Decreases the brake energy limited take-off mass

4 - The net flight path gradient after take-off compared to the actual climb gradient is: Smaller Depends on type of aircraft and may be smaller or larger respectively Equal Larger

5 - In straight horizontal steady flight, at speeds below that for minimum drag: A lower speed requires a higher thrust. The aeroplane cannot be controlled manually. A higher speed, but still below that for minimum drag, requires a higher thrust. The aeroplane can be controlled only in level flight.

6 - The take-off runway performance requirements for transport category aeroplanes are based upon: All engines operating only One engine inoperative only Failure of the critical engine or all engines operating whichever requirement gives the greater distance Failure of the critical engine only

7 - The force exactly opposing and balance lift in a glide descent is: Thrust x sin(angle of descent) Weight x sin(angle of descent) Weight x cos(angle of descent) Thrust x cos(angle of descent)

8 - In accordance to CS 25 which of the following listed speeds are used for determination of V2min: VMCG, V2 VSR, VMCA V1, VR VLOF, VMC

9 - A runway is contaminated by a 0.5 cm layer of wet snow. The take-off is nevertheless authorized by a light-twin's flight manual.The take-off distance in relation to a dry runway will be: Unchanged Decreased Increased Very significantly decreased

10 - Density altitude is the: Altitude read directly from the altimeter Altitude reference to the standard datum plane Height above the surface Pressure altitude corrected for 'non standard' temperature

Change Subject New Test

slide-home/multia.png

Subscribe to Newsletter

QuizVds.it - Facebook - Contact Us - Donation - Cookie Policy - Privacy Policy - Terms and Conditions - Partner