CLASS RATING ME (A) QUESTION BANK.docx

The critical engine inoperative? ================================ a. Increases the power required and the total drag due to the additional drag of the windmilling engine and the compensation of the yaw moment. b. Increases the power required and decreases the total drag due to the wi...

The critical engine inoperative? ================================ a. Increases the power required and the total drag due to the additional drag of the windmilling engine and the compensation of the yaw moment. b. Increases the power required and decreases the total drag due to the windmilling engine. c. Does not affect the aeroplane performance since it is independent of the power plant. d. Decreases the power required and increases the total drag due to the additional drag of the windmilling engine and the compensation of the yaw moment. Higher gross mass at the same altitude decreases the gradient and the rate of climb whereas? ============================================================================================ e. VX is increased and VY is decreased. f. VY and VX are decreased. g. VY and VX are not affected by a higher gross mass. h. VY and VX are increased. VX is? ====== i. The speed for best angle of flight path. j. The speed for best rate of climb. k. The speed for best angle of climb. l. The speed for best specific range. **The take-off distance required increases?** m. Due to lower gross mass at take-off. n. Due to downhill slope because of the smaller angle of attack. o. Due to slush on the runway. p. Due to head wind because of the drag augmentation. The flight manual of a light twin engine recommends two cruise power settings, 65 and 75%. The 75% power setting in relation to the 65% results in? =================================================================================================================================================== q. An increase in speed, fuel consumption and fuel-burn/distance. r. Same speed and fuel-burn/distance, but an increase in the fuel-burn per hour. s. Same speed and an increase of the fuel-burn per hour and fuel-burn/distance. t. An increase in speed and fuel-burn/distance, but an unchanged fuel-burn per hour. Which condition is most favourable handling-wise during take-off for a twin engine aircraft with the engines wing mounted, both being right hand props? ======================================================================================================================================================= u. A right engine failure, with a right quartering wind. v. A right engine failure, with a left quartering wind. w. A left engine failure, with a right quartering wind. x. A left engine failure, with a left quartering wind Which condition is least favourable handling-wise during take-off for a twin engine aircraft with the engines wing mounted, both being right hand props? ======================================================================================================================================================== y. A right engine failure, with a right quartering wind. z. A left engine failure, with a left quartering wind. a. A left engine failure, with a right quartering wind. b. A right engine failure, with a left quartering wind. With regard to a twin engine turbo prop with two clockwise props, the critical engine is? ========================================================================================= c. The right engine. d. At a positive angle of attack the right engine is critical. e. Both engines are critical. f. The left engine. A balanced field is contaminated with compacted snow what effect will it have on the TODA and ASDA? =================================================================================================== g. TODA increases ASDA decreases. h. TODA and ASDA increase. i. TODA increases and ASDA decreases. j. They will stay the same. A balanced field is contaminated with compacted snow what will happen to the TODR and the ASDR? =============================================================================================== k. TODR and ASDR increase. l. TODR increases and ASDR decreases. m. TODR decreases and ASDR increases. n. TODR stays constant and the ASDR increases. A balanced field is contaminated with compacted snow, what effect will it have on the TODA and ASDR? ==================================================================================================== o. THE TODR and ASDR will increase. p. THE TODA will decrease and the ASDR will increase. q. The TODA stays the same and the ASDR increases. r. The TODA and ASDR will increase. What is the effect on a TODA limited take-off and a ASDA limited take-off with an increased V1? =============================================================================================== s. TODA TOM increases, ASDA TOM decreases. t. TODA TOM decreases, ASDA TOM increases. u. TODA TOM increases, ASDA TOM increases. v. TODA TOM decreases, ASDA TOM decreases. Which of the following will decrease landing distance? ====================================================== w. Landing at a high altitude airfield. x. A tailwind y. Landing on a wet runway. z. Spoilers A balanced field take-off is? ============================= a. Where the OEI TODR = the AEO ASDR b. Where the OEI TODR = the OEI ASDR c. Where AEO TODR = AEO ASDR d. Where OEI TODA = OEI ASDA On take-off from an un-balanced field you have an available range of V1\'s. If a higher V1 is selected from the range than? =========================================================================================================================== e. Both TOD and ASD will decrease. f. Both TOD and ASD will increase. g. The ASDR will decrease. h. The all engine take-off distance will be unaffected. Which condition is most favourable handling-wise during take-off for a twin engine aircraft with the engines wing mounted, both being right hand props? ======================================================================================================================================================= i. A right engine failure, with a right quartering wind. j. A right engine failure, with a left quartering wind. k. A left engine failure, with a right quartering wind. l. A left engine failure, with a left quartering wind. Which condition is least favourable handling-wise during take-off for a twin engine aircraft with the engines wing mounted, both being right hand props? ======================================================================================================================================================== m. A right engine failure, with a right quartering wind. n. A left engine failure, with a left quartering wind. o. A left engine failure, with a right quartering wind. p. A right engine failure, with a left quartering wind. If the take-off mass of an aeroplane is brake energy limited a higher uphill slope would? ========================================================================================= q. Have no effect on the maximum mass for take-off. r. Decrease the maximum mass for take-off. s. Decrease the required take-off distance. t. Increase the maximum mass for take-off. Field length is balanced when? ============================== u. One engine acceleration from V1 to VLOF plus flare distance between VLOF and 35 feet are equal. v. All engine acceleration to V1 and braking distance for rejected take-off are equal. w. Calculated V2 is less than 110% VMCA and V1. x. Take-off distance available equals accelerate stop distance available. Which of the following statements is true regarding a balanced field-length? ============================================================================ y. A balanced take-off provides the lowest elevator input force requirement for rotation. z. For a balanced field-length the take-off run required always equals the take-off run available. a. A balanced field length provides the greatest margin between netand grosstake-off flight paths. b. A balanced-field length provides the minimum field-length available in the event of an engine failure. If V2 is increased what happens to CLTOM and the climb angle? ============================================================= c. Both decrease. d. CLTOM decreases and climb angle increases. e. CLTOM increases and climb angle decreases f. Both increase. Which of the following provides maximum obstacle clearance during climb? ======================================================================== g. The speed, at which the flaps may be selected one position further UP. h. The speed for maximum climb angle Vx. i. The speed for maximum rate of climb. j. 1.2Vs. Field length is balanced when? ============================== k. One engine acceleration from V1 to VLOF plus flare distance between VLOF and 35 feet are equal. l. All engine acceleration to V1 and braking distance for rejected take-off are equal. m. Calculated V2 is less than 110% VMCA and V1. n. Take-off distance available equals accelerate stop distance available. V1 for a balanced field is calculated when? =========================================== o. The speed is equal to V2. p. The take-off mass is field-length limited by the stopway to produce the maximum take-off mass. q. The acceleration/stop distance available is equal to the take-off distance available. r. The take-off mass is field-length limited by the clearway to produce the maximum take-off mass. A \'Balanced Field Length\' is said to exist where? =================================================== s. The clearway length does not equal the stopway length. t. The accelerate/stop distance available is equal to the take-off distance available. u. The take-off run available is equal to the take-off distance available. v. The accelerate/stop distance is equal to the take-off distance. For take-off obstacle clearance calculations, obstacles may be avoided? ======================================================================= w. By banking not more than 15° between 50 ft and 400 ft above the runway elevation. x. By standard turns - but only after passing 1500 ft. y. Only by using standard turns. z. By banking as much as needed if aeroplane is more than 50 ft above runway elevation. The net flight path gradient after take-off compared to the actual climb gradient is? ===================================================================================== a. Smaller. b. Depends on type of aircraft and may be smaller or larger respectively. c. Larger. d. Equal. According to CS23 what is the minimum VR speed for a Class B twin engine aeroplane; =================================================================================== e. 88 kts f. 90 kts g. 81 kts h. 96 kts 29. With regard to a twin engine turbo prop with two clockwise props, the critical engine is? ========================================================================================= i. The right engine. j. At a positive angle of attack the right engine is critical. k. Both engines are critical. l. The left engine. 30. Consider an engine failure of a twin-engine turboprop airplane. Which of the following statements about asymmetric effects of the propeller slipstream are correct? 1. A rolling moment towards the running engine will be induced. 2. Slipstream-induced lift will be lost on the side where the engine has failed. ==================================================================================================================================================================================================================================================================================================================== m. 3,4 n. 1,2 o. 2,3 p. 2,4 31. You are flying a twin-engine propeller airplane, where the engines are mounted on the wings. Which of the following conditions will result in the least asymmetric yaw and roll in case of an engine failure? ============================================================================================================================================================================================================= q. The failure of the right engine on a twin with counter-rotating propellers that rotate inwards. r. The failure of the right engine on a twin with counter-rotating propellers that rotate outwards. s. The failure of the left engine on a twin with two right-hand propellers. t. The failure of the left engine on a twin with counter-rotating propellers that rotate outwards. 32. How will CG affect asymmetric yaw? ================================== u. CG FWD will increase yaw v. CG AFT will reduce yaw w. It is not dependent on CG x. CG FWD will reduce yaw 33. A propeller is turning to the right when viewed from behind. The asymmetric blade effect in the climb at low speed will? ======================================================================================================================== y. Roll the aeroplane to the right. z. Roll the aeroplane to the left. a. Yaw the aeroplane to the right. b. Yaw the aeroplane to the left 34. Which statement about a propeller are correct or incorrect? 1. Asymmetric blade effect is unaffected when engine power is increased. 2. Asymmetric blade effect increases when the angle between the propeller axis and the airflow through the propeller disc increases? ========================================================================================================================================================================================================================================================================= c. 1\) is correct, 2) is incorrect. d. 1\) is correct, 2) is correct. e. 1\) is incorrect, 2) is incorrect f. 1\) is incorrect, 2) is correct. 35. When an aircraft is in asymmetric flight, which overall sideslip force will be created when only slipping towards the running engine? ===================================================================================================================================== g. Aft of the CG in the opposite direction as the rudder force h. Forward of the CG in the same direction as the rudder force i. Forward of the CG in the opposite direction as the rudder force j. Aft of the CG in the same direction as the rudder force 36. Which statement about a propeller are correct or incorrect? 1. Asymmetric blade effect reduces when engine power is increased. 2. Asymmetric blade effect is independent of the angle between the propeller axis and the airflow through the propeller disc? ============================================================================================================================================================================================================================================================ k. 1\) is correct, 2) is correct. l. 1\) is correct, 2) is incorrect. m. 1\) is incorrect, 2) is correct. n. 1\) is incorrect, 2) is incorrect. 37. For a tail wheel aircraft with a propeller turning to the right (when viewed from behind), at the start of the take-off run, asymmetric blade effect causes? ============================================================================================================================================================ o. Nose down pitch (tail up) p. Yaw to right. q. No effect. r. Yaw to left. 38. Which statement about a propeller are correct or incorrect? 1. Asymmetric blade effect increases when engine power is increased. 2. Asymmetric blade effect reduces when the angle between the propeller axis and the airflow through the propeller disc increases? =================================================================================================================================================================================================================================================================== s. 1\) is incorrect, 2) is correct. t. 1\) is incorrect, 2) is incorrect. u. 1\) is correct, 2) is incorrect. v. 1\) is correct, 2) is correct. 39. The asymmetric blade effect on a single engine aeroplane with a clockwise rotating propeller? ============================================================================================= w. Produces left yaw. x. Does not produce any yaw. y. Is also called the gyroscopic effect. z. Produces right yaw. 40. Asymmetric propeller blade effect is mainly induced by: ======================================================= a. Large angles of yaw. b. Large angles of climb. c. The inclination of the propeller axis to the relative airflow. d. High speed. 41. Which of the following have an effect on rudder force in asymmetric flight? 1. Rudder deflection 2. Thrust setting 3. CG 4. Mass 5. TAS 6. IAS? =============================================================================================================================================== e. 1,3,6 f. 2,3,4 g. 2,3,6 h. 4,5,6 42. In order to maintain straight and level flight when you have just lost your critical engine you must? ===================================================================================================== i. rudder and bank towards good engine. j. bank towards good engine and rudder towards dead engine. k. rudder and bank towards dead engine. l. bank towards dead engine and rudder towards good engine. 43. The calibrated airspeed during the take-off run at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the aeroplane using the rudder control alone, and the lateral control to the extent of keeping the wings level to enable the take-off to be safely continued using normal piloting skills, is called? ============================================================================================================================================================================================================================================================================================================================================================ m. V1 n. VMC o. V2 p. VMCG 44. Which of these statements about the equilibrium of forces and moments at VMCA are correct or incorrect? 1. Because VMCA must be determined for the case where the critical engine suddenly fails there is no need to obtain equilibrium of moments about the normal axis. 2. Equilibrium of forces along the lateral axis does not require any sideslip during a wings level condition? ======================================================================================================================================================================================================================================================================================================================================================================================= q. 1\) is correct, 2) is correct. r. 1\) is incorrect, 2) is incorrect. s. 1\) is correct, 2) is incorrect. t. 1\) is incorrect, 2) is correct. 45. If a twin-engine jet aeroplane commences a take-off on runway 27 and the current wind is 210°/15 kt, what is the critical jet engine in case of an engine failure during take-off run? ====================================================================================================================================================================================== u. The left engine is the critical engine. v. The right engine is the critical engine. w. There is no critical engine. x. Both engines are critical engines. 46. Which of the following statements are correct or incorrect? 1. When the critical engine fails during take- off the speed VMCL can be limiting. 2. Speed VMCL can be limited by the available maximum roll rate? =============================================================================================================================================================================================================== y. 1\) is incorrect, 2) is correct. z. 1\) is correct, 2) is correct. a. 1\) is incorrect, 2) is incorrect. b. 1\) is correct, 2) is incorrect. 47. Compare a MEP with inward counter rotating propellers encountering an engine failure, with a MEP with clockwise rotating propellers encountering a failure of the critical engine. Why is the MEP with counter rotating propellers easier to control after an engine failure? ============================================================================================================================================================================================================================================================================= c. The thrust line is closer to the longitudinal axis d. The thrust line is further from the longitudinal axis e. The thrust line is further from the lateral axis f. The thrust line is closer to the lateral axis 48. VMCA is the minimum speed at which directional control can be maintained when, amongst others: 1. maximum take-off thrust was set and is maintained on the remaining engines. 2. a sudden engine failure occurs on the most critical engine. 3. flaps are in any position. 4. the gear is either up or down. 5. The aeroplane is either in or out of ground effect. The combination that regroups all of correct statements is? =============================================================================================================================================================================================================================================================================================================================================================================================================================== g. 1,2,4 h. 2,3,5 i. 3, 4, 5 j. 1,2 49. A pilot suffers an engine failure and forgets to feather the propeller, what will happen? ========================================================================================= k. Glide distance is increased. l. Climb gradient is decreased. m. Airspeed is increased. n. Glide angle is not affected. 50. When the blades of a propeller are in the feathered position? ============================================================= o. The windmilling RPM is the maximum. p. The propeller produces an optimal windmilling RPM. q. The drag of the propeller is then minimal. r. The RPM is then just sufficient to lubricate the engine. 51. Which of the following are the effects of feathering a propeller in flight? 1. Drag and Yaw increase. ===================================================================================================== s. 1,4 t. 2,4 u. 1,2 v. 1,3 52. What happened when one of the engine\'s propellers are feathered on an MEP aircraft? ==================================================================================== w. The yawing effect reduces. x. The yawing effect disappears. y. The yawing effect increases. z. The yawing effect initially reduces but then increases due to the increased rudder input required by the pilot. 53. Which statements are correct or incorrect? 1. Stall speeds are determined with the CG at the forward limit. 2. Minimum control speeds are determined with the CG at the aft limit? ================================================================================================================================================================================== a. 1\) is correct, 2) is correct. b. 1\) is correct, 2) is incorrect. c. 1\) is incorrect, 2) is incorrect. d. 1\) is incorrect, 2) is correct. 54. Which of the following statements are correct or incorrect? 1. VMCL is the minimum control speed in the landing configuration. 2. The speed VMCL is always limited by maximum rudder deflection? ================================================================================================================================================================================================ e. 1\) is incorrect, 2) is incorrect. f. 1\) is correct, 2) is correct. g. 1\) is incorrect, 2) is correct. h. 1\) is correct, 2) is incorrect. 55. Which statement about minimum control speed is correct? ======================================================= i. VMCL is determined by maximum rudder only. j. The nose wheel steering control may be used to determine VMCG k. Crosswind is taken into account to determine VMCG l. VMCA depends on the airport density altitude, and the location of the engine on the aeroplane (aft fuselage or wing). 56. Minimum control speeds are established when conducting flight tests. Vmcg has to be established with a CG position at the (1) location and (2) the use of nose wheel steering? ============================================================================================================================================================================== m. \(1) most unfavorable; (2) without n. \(1) most unfavorable; (2) with o. \(1) forward; (2) with p. \(1) forward; (2) without 57. In a straight steady climb the thrust must be? ============================================== q. Equal to the drag. r. Greater than drag because more lift has to be produced. s. Greater than the drag because it must also balance a component of weight. t. Lower than the drag because it is assisted by a component of weight.