×

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, FAA Drone > Mass and Balance - ATPL - Airline Transport Pilot license

Quiz Mass and Balance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Mass and Balance, no time limit

Change Subject New Test

1 - The maximum quantity of fuel that can be loaded into an aircraft's tanks is given as 2200 l. If the fuel density (specific gravity) is given as 0.79 the mass of fuel which may be loaded is: 1738 kg 1798 kg 2098 kg 2785 kg

2 - In cruise flight, a centre of gravity moving aft will: Decrease longitudinal static stability Not change the manoeuvrability Have no effect on longitudinal static stability Increase longitudinal static stability

3 - From the data contained in the attached appendix, the maximum allowable take - off mass and traffic load is respectively: 61600 kg and 12150 kg 60425 kg and 10975 kg 66770 kg and 17320 kg 68038 kg and 18588 kg[see Annex]

4 - Which is true of the aircraft basic empty mass? It is a component of dry operating mass. It is the actual take-off mass, less traffic load. It is dry operating mass minus traffic load. It is dry operating mass minus fuel load.

5 - The maximum certificated take - off mass is: A take - off limiting mass which is governed by the gradient of climb after reaching V2 . A take - off limiting mass which is affected by the aerodrome altitude and temperature. Limited by the runway take off distance available. It is tabulated in the Flight Manual. A structural limit which may not be exceeded for any take - off.

6 - In order to provide an adequate 'buffet boundary' at the commencement of the cruise a speed of 1.3 Vs is used.At a mass of 120000 kg this is a CAS of 180 KT.If the mass of the aeroplane is increased to 135000 kg the value of 1.3 Vs will be: Increased to 191 KT, drag will increase and air distance per kg of fuel will decrease. Increased to 202 KT but, since the same angle of attack is used, drag and range will remain the same. Increased to 191 KT, drag will decrease and air distance per kg of fuel will increase. Unaffected as Vs always occurs at the same angle of attack.

7 - An aeroplane is performance limited to a landing mass of 54230 kg. The Dry Operating Mass is 35000 kg and the zero fuel mass is 52080 kg. If the take-off mass is 64280 kg the useful load is 29280 kg. 10080 kg. 12200 kg. 17080 kg

8 - The loaded centre of gravity (cg) of an aeroplane is 713 mm aft of datum. The mean aerodynamic chord lies between station 524 mm aft and 1706 mm aft. The cg expressed as% MAC (mean aerodynamic chord) is: 60 % 41 % 10 % 16 %

9 - The Maximum Certificated Taxi (or Ramp) Mass is that mass to which an aeroplane may be loaded prior to engine start. It is: A value which varies with airfield temperature and altitude. Corrections are listed in the Flight Manual. A value which varies only with airfield altitude. Standard corrections are listed in the Flight Manual. A fixed value which is listed in the Flight Manual. A value which is only affected by the outside air temperature. Corrections are calculated from data given in the Flight Manual.

10 - . The mass of an item multiplied by it's distance from the datum is it's Moment Force Moment arm Centre of gravity

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