General Leave a reply0% General 1 / 201. Q112 The airspeed indicator is unservicable. The airplane may only be operated… A) when a GPS with speed indication is used during flight. B) if no maintenance organisation is around. C) when the airspeed indicator is fully functional again. D) if only airfield patterns are flown. 2 / 202. Q96 What is the meaning of the white arc on the airspeed indicator? A) Speed range not to exceed B) Speed range in smooth air C) Speed range in bumpy air D) Speed range for extended flaps 3 / 203. Q10 The load factor “n” describes the relationship between… A) thrust and drag. B) lift and weight. C) drag and lift. D) weight and thrust. 4 / 204. Q46 What devices can be affected by a failure of the electrical system in a helicopter? A) Radio equipment, navigation equipment and magnetic compass B) Airspeed indicator, altimeter and artificial horizon C) Radio equipment, navigation equipment and gyros D) Fuel quantity indication, radio equipment and altimeter 5 / 205. Q55 What is the direct influence by switching on the carburettor heating on fixed propeller engines during engine run-up? A) RPM increaes B) Angle of attack decreases C) RPM decreases D) Angle of attack increases 6 / 206. Q58 In which outside air temperature is icing most likely? 7 / 207. Q30 What is the purpose of the secondary flight controls? A) To constitute a backup system for the primary flight controls B) To improve the turn characteristics of an aircraft in the low speed regime during approach and landing C) To enable the pilot to control the aircraft’s movements about its three axes D) To improve the performance characteristics of an aircraft and relieve the pilot of excessive control forces 8 / 208. Q100 Which of the mentioned cockpit instruments is connected to the pitot tube? A) Altimeter B) Direct-reading compass C) Airspeed indicator D) Vertical speed indicator 9 / 209. Q27 What is the effect of pulling the control yoke or stick backwards? A) The aircraft’s tail will produce an increased downward force, causing the aircraft’s nose to drop B) The aircraft’s tail will produce an increased upward force, causing the aircraft’s nose to rise C) The aircraft’s tail will produce an increased downward force, causing the aircraft’s nose to rise D) The aircraft’s tail will produce an decreased upward force, causing the aircraft’s nose to drop 10 / 2010. Q14 Reasons for dents in the helicopter structure are… A) excessive engine rpm and cylinder defects. B) intense erosion or high wear. C) material defects or old colour. D) hard landing or excessive stress. 11 / 2011. Q70 During ignition check the ignition is switched to OFF for a short moment and subsequently back to BOTH. What happens to the RPM if the ignition system is properly grounded? A) The RPM decreases once switched to OFF and resumes the previous value when switched back to BOTH B) The RPM increases once switched to OFF and resumes a value below the previous one when switched back to BOTH C) The RPM decreases once switched to OFF and resumes a value below the previous one when switched back to BOTH D) The RPM increases once switched to OFF and resumes the previous value when switched back to BOTH 12 / 2012. Q61 What happens during oil filter clocking? A) The oil circulation will end after 15 minutes so that a proper engine run will not be guaranteed B) The oil circulation will end after 30 minutes so that a proper engine run will not be guaranteed C) A bypass valve opens thus enabling the circulation to continue, debris will not be filtered D) A bypass valve opens thus enabling the circulation to continue, debris will be filtered by an alternate filter 13 / 2013. Q126 What is the purpose of winglets? A) Increase of lift and turning manoeuvering capabilities. B) To increase efficiency of aspect ratio. C) Reduction of induced drag. D) Increase gliging performance at high speed. 14 / 2014. Q9 Which constructional elements give the wing its profile shape? A) Planking B) Rips C) Spar D) Tip 15 / 2015. Q82 A true altitude is… A) a height above ground level corrected for non-standard temperature. B) an altitude above mean sea level corrected for non-standard temperature. C) a height above ground level corrected for non-standard pressure. D) a pressure altitude corrected for non-standard temperature. 16 / 2016. Q107 What is a cause for the dip error on the direct-reading compass? A) Acceleration of the airplane B) Deviation in the cockpit C) Temperature variations D) Inclination of earth’s magnetic field lines 17 / 2017. Q63 Piston engines of helicopters have… A) two independent ignition systems. B) one electrical ignition system. C) two coupled ignition systems. D) one magneto ignition system. 18 / 2018. Q87 Which of the following options states the working principle of a vertical speed indicator? A) Measuring the vertical acceleration through the displacement of a gimbal-mounted mass B) Static air pressure is measured and compared against a vacuum C) Measuring the present static air pressure and comparing it to the static air pressure inside a reservoir D) Total air pressure is measured and compared to static pressure 19 / 2019. Q32 The trim wheel or lever in the cockpit is moved aft by the pilot. What effect does this action have on the trim tab and on the elevator? A) The trim tab moves down, the elevator moves down B) The trim tab moves up, the elevator moves down C) The trim tab moves up, the elevator moves up D) The trim tab moves down, the elevator moves up 20 / 2020. Q92 Which of the following factors could cause an erroneous airspeed indication? A) The boost pressure line is defective B) A circuit breaker was pulled C) The aircraft is covered with adhesive foils D) The earth wire is still attached Your score is 0%