Title DGCA MODULE 17 (02 OF 2017) QUESTION SET.pdf ✅

Visit our website to download all latest EASA / DGCA CAR 66 Module examination Question papers and study material – click here >> www.amequestionpaper.in WWW.AMEQUESTIONPAPER.IN DGCA MODULE 17 (02 OF 2017) QUESTION SET 1.The force that tends to pull the propeller blades out of the hub[EASA 1.9] a) centrifugal force b) thrust bending force c) CTF d) ATF 2. The purpose of drain hole in wooden propeller tipping [EASA, 2.3] a) to drain out the engine oil stuck in piston by centrifugal action b) to drain away moisture by centrifugal action c) to drain away anti-ice fluid by centrifugal force 3.Electrical de-icing converts [CAIP2, 871 & EASA 5.4] a) electrical energy to heat energy b) mechanical energy to heat energy c) heat energy to electrical energy 4.In deicing system electrical power transfers through[EASA 5.4] a) slip rings b) brush c) slip rings and brushes 5.Electrical de-icing systems are usually designed for [EASA 5.5] a) continuous application b) intermittent application c) none 6.Blade tracking is carried out in propeller to determine [EASA, 6.6] a) actual position of propeller blade b) relative position of propeller blades c) as in (b) and out of track propeller are easy to dynamically balance d) ATA 7.When a/c climbs and engine failure occurs, propeller [EASA, 2.9] a) blade angle increases to negative pitch to reduce drag b) blade angle decrease to negative pitch reduce drag c) blade angle neither decrease nor increase o reduce drag
Visit our website to download all latest EASA / DGCA CAR 66 Module examination Question papers and study material – click here >> www.amequestionpaper.in WWW.AMEQUESTIONPAPER.IN 8.Purpose of metal tipping in L.E. of wooden propeller to [EASA, 2.2] a) prevent formation of ice & snow b) protect blade from FOD caused by flying objects & aerodynamic smoothness c) reduce drag and increase efficiency 9.MTCS, ground adjustable propellers[EASA, 2.8] a) adjustable blade angle only in ground b) adjust blade angle only in flight c) adjust blade angle in both ground & flight 10.The purpose of reverse pitch in propeller[EASA, 2.10] a) blade angle is changed to reverse pitch to provide negative thrust b) blade angle is changed to forward pitch to provide positive thrust c) blade angle is not changed at all 11.In propeller governor, the purpose of pilot valve [EASA, 3.4-3.5] a) to control the propeller RPM b) to control the engine RPM c) to control both engine & propeller RPM 12.In feathering, the source of hydraulic pressure is from[EASA, 3.16] a) dedicated propeller- hydraulic system b) a/c hydraulic system c) engine lubrication system 13.During feathering of propellers[EASA, 2.9] a) hydraulic pressure moves blades toward low pitch b) hydraulic pressure moves blades toward high pitch c) hydraulic pressure moves blades toward reverse pitch 14.MTCS,station numbers[EASA, 1.5] a) are measured in centimeter b) are measured from center of hub c) are measured from center of propeller shank 15.Blade angle [EASA, 1.5] a) increases from root to tip b) decreases from root to tip c) decreases from tip to root
Visit our website to download all latest EASA / DGCA CAR 66 Module examination Question papers and study material – click here >> www.amequestionpaper.in WWW.AMEQUESTIONPAPER.IN 16.The primary function of front & rear cones when splined propeller shaft [EASA, 2.4] a) to center the propeller on the crankshaft b) to prevent the propeller from loosening 17.When flyweight overcome the speeder spring pressure it means[EASA, 3.7] a) propeller rotation under speed b) propeller rotation over speed c) engine rotation over speed d) engine rotation under speed 18.Autofeathering accomplises [EASA, 3.11] a) automatically b) manually by pilot c) both automatically & manually 19.When speeder spring force decreases, the blade angle will be [EASA, 3.7] a) increases b) decreases c) remain same d) none 20.If an propeller rotates in underspeed condition the blade angle will be[EASA,3.7] a) fine pitch b) coarse pitch c) smooth pitch d) bastard pitch 21.Hygroscopic covering on propeller while storing [EASA, 7.3] a) it makes a layer between blade & atmosphere b) it cannot moisture c) it absorbs moisture d) both (a) & (b) 22.Phosphate is used as anti-icing fluid in place of isopropyl alcohol due to[EASA, 5.3] a) expensive b) flammability
Visit our website to download all latest EASA / DGCA CAR 66 Module examination Question papers and study material – click here >> www.amequestionpaper.in WWW.AMEQUESTIONPAPER.IN c) corrosive d) all 23.Static balancing is done by [EASA, 6.9] a) suspension test stand b) knife-edge test stand c) no stand is required 24. Storage of propeller should be [EASA, 7.3] a) on tip suspension b) not on tip c) dip In oil 25.Nicks and abrasions are a) permeseable b) not permeseable 26.Hydraumatic propeller with engine shaft are used in[EASA, 3.13] a) feathering propellers b) non-feathering propeller c) fixed pitch propeller 27.Material of propeller [CAIP 2, 850] a) Aluminum b) Anodized aluminum c) Anodized Mg d) all 28.During preservation, the propeller should be checked for a) moisture & sunlight b) physical damage & corrosion c) internal damage d) both (a) & (b) 29.Static unbalance is due to [EASA, 6.9] a) when CG of the propeller doesn’t coinside with the axis of rotation b) when CG of the propeller or similar propeller elements do not follow in the same plane c) when CG of the propeller coinside with the axis of rotation