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

Home > Exam Quiz Archive > Quiz PPL(A) English - Exam test Private Pilot License > Performance and flight planning Page 7

PPL(A) - Private Pilot License - Performance and flight planning Page 7

Questions Performance and flight planning - Private Pilot (Aircraft) Page 7

Given the following information, what range can be achieved? Outside air temperature: 22° C Pressure altitude: 2000 ft Power: 55 % See annex (PFP-013) (1,00 P.) Siehe Anlage 12	4 Answers
Given the following conditions, the TAS equals... Outside air temperature: 10° C Pressure altitude: 6000 ft Power: 65 % See annex (PFP-014) (1,00 P.) Siehe Anlage 13	4 Answers
Given the following conditions, the TAS equals... Outside air temperature: -2° C Pressure altitude: 8000 ft Power: 75 % See annex (PFP-014) (1,00 P.) Siehe Anlage 13	4 Answers
Which maximum rate of climb can the aircraft reach at 9000 ft pressure altitude and OAT 12° C? See annex (PFP-011) (1,00 P.) Siehe Anlage 11	4 Answers
Which is the maximum rate of climb for the aircraft at 6500 ft pressure altitude and an OAT of 0° C? See annex (PFP-011) (1,00 P.) Siehe Anlage 11	4 Answers
What is the true airspeed (TAS) [kt] and fuel consumption [l/h] for cruise flight with 60 % power in flight level 60 under the following conditions? Temperature: ISA - 20° C QNH: 980 hPa See annex (PFP-012) (2,00 P.) Siehe Anlage 10	4 Answers
What is the true airspeed (TAS) [kt] and fuel consumption [l/h] for cruise flight with 70 % power in flight level 60 under the following conditions? Temperature: ISA - 20° C QNH: 980 hPa See annex (PFP-012) (2,00 P.) Siehe Anlage 10	4 Answers
What is the fuel flow and the true airspeed for cruise flight with 60 % power in flight level 85 at an OAT of -25° C? See annex (PFP-014) (1,00 P.) Siehe Anlage 13	4 Answers
At which airspeed do you climb to flight level (FL) 75 after a departure from an airfield which is located at a pressure altitude of 3000 ft with an initial mass of 3000 lbs? OAT at airfield: 25° C OAT in FL 75: 0° C See annex (PFP-023) (1,00 P.) Siehe Anlage 14	4 Answers
What is the required fuel to climb from FL 65 to FL 95 under the following conditions? Aircraft mass: 3000 lb. OAT in FL 65: -5° C OAT in FL 95: -15° C See annex (PFP-023) (1,00 P.) Siehe Anlage 14	4 Answers

PPL(A) - Private Pilot License Training!

5
6
7
8
9

slide-home/multia.png

Subscribe to the Newsletter

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