Tecnam P2006T Knowledge Test Bank PDF

TECNAM P2006T KNOWLEDGE TEST BANK (100 ITEMS) 1. Which of the following is the engine manufacturer and model of P2006T? a. Rotax-912 b. Bombardier-Rotax 912 S3 c. Lycoming IO-250-C4B5 d. None of the above 2. What is the maximum power of P2006? a. 73.5 kW (98.6...

TECNAM P2006T KNOWLEDGE TEST BANK (100 ITEMS) 1. Which of the following is the engine manufacturer and model of P2006T? a. Rotax-912 b. Bombardier-Rotax 912 S3 c. Lycoming IO-250-C4B5 d. None of the above 2. What is the maximum power of P2006? a. 73.5 kW (98.6hp) @ 5800 rpm – 5 minutes maximum b. 73.5 kW (98.6hp)@ 5800 rpm – 10 minutes maximum c. 73.5 kW (98.6hp) @ 5000 rpm – 5 minutes maximum d. None of the above 3. Which of the following the propeller manufacturer and model of P2006T. a. Rotor Dowtyxxxx b. Hartzell E2Y c. MT Propeller MTV-21-A-C-F/CF178-05 d. None of the above 4. What type of propeller is installed on the P2006T? a. Fixed pitch b. Variable pitch-hydraulically controlled c. None of the above d. A & B 5. Which of the following is the manufacturer and model of the propeller governor of P2006T? a. Mt Propeller P-875-12 hydraulic b. Lycoming governor c. None of the above d. A & B 6. What are the approved fuel for the P2006T a. AVGAS 100LL only b. Jet- A1 and Jet B c. MOGAS ASTM D4814 and AVGAS 100LL (ASTM D910) d. MOGAS ASTM D4814, EN 228 Super/Super Plus (min RON 95) and AVGAS 100LL(ASTM D910) e. Kerosene 7. What is the fuel capacity of each wing tank? a. 100 liters (26.42 US gallons) b. 98 liters (25.55 US gallons) c. 120 liters (28.55 US gallons) d. None of the above 8. What is the total tanks capacity? a. 200 liters (52.8 US gallons) b. 250 liters (60 US gallons) 9. What is the overall usable fuel? a. 200 liters (52.8 US gallons) b. 194.4 liters (51.25 US gallons) c. 205 liters (53 US gallons) d. None of the above 10. What is the overall unusable fuel? a. 6.0 liters b. 5.6 liters c. 5.0 liters d. 4.5 liters 11. What is the maximum and minimum oil capacity per tank? a. Max. 3.0 liters – min 2.0 liters (per tank) b. Max. 4.0 liters – min 3.0 liters (per tank c. Max. 3.0 liters – min 2.0 liters (both tanks) d. None of the above 12. What type of lubrication system P2006 engine has? a. Forced type with external reservoir b. Sump type c. A & B are both correct d. None of the above 13. What is the type of cooling system the P2006 has? a. Ram-air cooled cylinders b. Liquid cooled cylinder heads(closed and pressurized circuit) c. Liquid cooled cylinders only d. Both A and B are correct. 14. What is the never exceed speed (Vne) in KIAS? a. 167 KIAS b. 168 KIAS c. 160 KIAS d. 150 KIAS 15. What is the design manoeuvring (Va) speed? a. 120 KIAS b. 118 KIAS c. 125 KIAS d. 121 KIAS 16. What is the maximum Landing Gear extended (Vle) speed? a. 93 KIAS b. 95 KIAS c. 98 KIAS d. 90 KIAS 17. What is the maximum Landing Gear operating (Vlo) speed? a. 93 KIAS b. 95 KIAS c. 98 KIAS d. 90 KIAS 18. What is the maximum flaps extended speed (Vfe) FULL? a. 119 KIAS b. 93 KIAS c. 117 KCAS d. 120 KCAS 19. What is the maximum flaps extended speed (Vfe) T.O.? a. 119 KIAS b. 93 KIAS c. 117 KCAS d. 120 KCAS 20. What is the aircraft minimum control speed (Vmc) with one engine inoperative? a. 62 KIAS b. 70 KIAS c. 75 KIAS d. 40 KIAS 21. What does the red line on the airspeed indicator marking denotes? a. 62 KIAS, Vmc b. 70 KIAS, Vmc c. 75 KIAS, Vmc d. 50 KIAS, Vmc 22. What does the blue line on the airspeed indicator marking denotes? a. Best rate-of-climb speed with one engine inoperative at sea level b. Speed range where manoeuvres must be conducted with caution and only in smooth air c. Minimum aircraft control speed with one engine inoperative and flaps set to T.O. d. Normal aircraft operating range speed 23. What is the maximum power and max rpm in maximum T.O.? a. Max power 73.5kW(98.6hp), 2388, time maximum(minutes) 5 b. Max power 74.0kW(99.0hp),2400, no time limit c. Max. Cont. 69.0kW(92.5hp), 2265, no time limit d. Both A and C are correct 24. What is the maximum CHT? a. 140 degree Centigrade b. 135 degree Centigrade c. 145 degree Centigrade d. 130 degree Centigrade 25. What is the maximum continuous power and rpm of the 912 S3? a. 69kW (92.5hp), 2265 rpm b. Max power 74.0kW(99.0hp),2400, no time limit c. Max power 73.5kW(98.6hp), 2388, time maximum(minutes) 5 d. Max. Cont. 69.0kW(92.5hp), 2265, time maximum (minutes) 5 26. What is the oil temperature normal operating range? a. 90 deg C/110 deg C b. 50 deg C/130 deg C c. 110 deg C/150 deg C d. 60 deg F/100 deg F 27. What is the minimum and maximum oil temperature? a. 90 deg C/110 deg C b. 50 deg C/130 deg C c. 110 deg C/150 deg C d. 60 deg F/100 deg F 28. What is the minimum oil pressure (below 1400 rpm prop) a. 0.8 Bar/12 psi b. 2 - 5 Bar/29 – 73 psi c. 7 Bar/102 psi d. None of the above 29. What is the normal oil pressure (above 1400 rpm prop) a. 0.8 Bar/12 psi b. 2 - 5 Bar/29 – 73 psi c. 7 Bar/102 psi d. None of the above 30. What is the maximum oil pressure (above 1400 rpm prop) a. 0.8 Bar/12 psi b. 2 - 5 Bar/29 – 73 psi c. 7 Bar/102 psi d. None of the above 31. What is the engine starting allowable temperature range? a. OAT Min -25 deg Centigrade, OAT Max +50 deg C b. OAT Min -25 deg Centigrade, OAT Max +50 deg C c. OAT Min -10 deg Centigrade, OAT Max +70 deg C d. OAT Min -50 deg Centigrade, OAT Max +50 deg C 32. What is the minimum fuel pressure? a. 0.15 Bar/2.2 psi b. 0.40 Bar/5.8 psi c. 0.50 Bar/6.0 psi d. 0.10 Bar/1.8 psi 33. What is the maximum fuel pressure? a. 0.15 Bar/2.2 psi b. 0.40 Bar/5.8 psi c. 0.50 Bar/6.0 psi d. 0.10 Bar/1.8 psi 34. What is the maximum operating altitude of the P2006T? a. 15000 feet MSL b. 14000 feet MSL c. 20000 feet MSL d. FL250 pressure altitude 35. What does the red warning LH OVERVOLT signifies? a. Right engine – coolant liquid low level b. Left engine electric system overvoltage c. Right engine electric system overvoltage d. Left engine compartment: fire detected 36. What does the red warning RH ENGINE FIRE means? a. Right engine – coolant liquid low level b. Left engine electric system overvoltage c. Right engine electric system overvoltage d. Right engine compartment: fire detected 37. What is the maximum takeoff weight of P2006T? a. 1180 kg or 2601 lb. b. 1200 kg or 2701 lb. c. 1145 kg or 2524 lb. d. None of the above 38. What is the maximum landing weight of P2006T? a. 1180 kg or 2601 lb. b. 1200 kg or 2701 lb. c. 1145 kg or 2524 lb d. None of the above 39. What is the maximum zero wing fuel weight of P2006T? a. 1180 kg or 2601 lb. b. 1200 kg or 2701 lb. c. 1145 kg or 2524 lb. d. None of the above 40. Which of the following is not an approved maneuver for this aircraft? a. Any manoeuvre pertaining to “normal” flight b. Stalls (except whip stalls) c. Lazy eights d. Chandelle e. Spins and turns with angle of bank more than 60 degrees 41. What is the maneuvers load factor limits with flaps retracted? a. +3.8 g and – 1.78 g b. +4.0 g and – 2.00 g c. +3.5 g and – 1.78 g d. Both A and B are correct 42. What is the maneuvers load factor limits with flaps extended? a. +3.8 g and – 1.78 g b. +4.0 g and – 2.00 g c. +3.5 g and – 1.78 g d. +2 and 0 g 43. What is the minimum crew and maximum number of occupants? a. Minimum crew of 1 pilot and maximum occupants of 4 people (including the pilot) b. Minimum crew of 2 pilots and maximum occupants of 4 people(including the pilots) c. Minimum crew of 1 pilot and maximum occupants of 3 people (including the pilot) d. Minimum crew of 1 pilot and maximum occupants of 3 people (excluding the pilot) 44. What is the maximum allowable load of the baggage compartment? a. 80 kg/176 lb b. 90 kg/180 lb c. 70 kg/170 lb d. 75 kg/173 lb 45. What is the low pressure limit allowed for the landing gear emergency accumulator? a. 20 Bar b. 30 Bar c. 10 Bar d. 25 Bar 46. What is the forward CG limit for all weights? a. 0.415 m (31% MAC) aft of datum b. 0.221 m (16.5% MAC) aft of datum c. 0.415 m (31% MAC) forward of datum d. 0.221 m (16.5% MAC) forward of datum 47. What is the aft limit CG limit for all weights? a. 0.415 m (31% MAC) aft of datum b. 0.221 m (16.5% MAC) aft of datum c. 0.415 m (31% MAC) forward of datum d. 0.221 m (16.5% MAC) forward of datum 48. What does an amber caution LH GENERATOR signifies? a. RH generator failure b. Left Hand generator failure c. Left engine – electrical fuel pump ON d. Pitot heating system ON 49. What does a green advisory LG Down and Locked means? a. Landing lights are ON b. Landing gear is retracted c. Landing gear extended and locked d. Landing gear doors not locked 50. What does a red warning RH LOW COOLANT signifies? a. Right engine – coolant liquid low level b. Left engine – coolant liquid low level c. Right engine – coolant normal level d. Left engine – coolant above normal level 51. What color will illuminate on the annunciator panel to indicate that pertinent device is turned ON? a. green b. amber c. red 52. What color will illuminate on the annunciator panel to indicate no-hazard situations which have to be considered and which require a proper crew action? a. green b. amber c. red 53. What color will illuminate on the annunciator panel to indicate emergency conditions? a. green b. amber c. red 54. What is the rotation speed with flaps set to T/O (MTOW is 1180kg)? a. 64 KIAS b. 73 KIAS c. 80 KIAS d. 90 KIAS 55. What is the best-angle-of-climb speed(Vx), flaps 0(MTOW is 1180kg)? a. 64 KIAS b. 73 KIAS c. 80 KIAS d. 90 KIAS 56. What is the best-rate-of-climb speed(Vy), flaps 0(MTOW is 1180kg)? a. 64 KIAS b. 73 KIAS c. 80 KIAS d. 90 KIAS 57. What is the approach speed with flaps T/O(MTOW is 1180kg)? a. 64 KIAS b. 73 KIAS c. 80 KIAS d. 90 KIAS 58. What is the final approach speed, flaps FULL(MTOW is 1180kg)? a. 64 KIAS b. 73 KIAS c. 70 KIAS d. 90 KIAS 59. What is the recommended safe simulated OEI speed(Vsse)? a. 70 KIAS b. 64 KIAS c. 90 KIAS d. 80 KIAS 60. Refer to figure 2. What is the stall speed with flaps 0, bank angle 0 a. 66 KIAS b. 64 KIAS c. 56 KIAS d. 53 KIAS 61. What is the maximum demonstrated crosswind of P2006T? a. 18 Kts b. 17 kts c. 15 kts d. 20 kts 62. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 30 deg and wind speed is 20 knots? a. Headwind = 17.5 Kts ; Crosswind = 10 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts  c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above 63. Refer to Figure 4. What will be the take-off rate of climb at a weight of 930 kg, sea level, at a temperature of 25 deg Celsius? a. 1206 fpm b. 1372 fpm c. 864 fpm d. 1451 fpm 64. Refer to Figure 4. What will be take-off rate of climb and climb speed (Vy)at a weight of 1080 kg, at a pressure altitude of 2000 feet, standard atmosphere? a. 946 fpm, 79 KIAS b. 933 fpm, 82 KIAS c. 1068 fpm, 82 KIAS d. 1315 fpm, 82 KIAS 65. Refer to Figure 4. What will be take-off rate of climb and climb speed (Vy) at a weight of 1180 kg, at a pressure altitude of 4000 feet, 25 deg Celsius temperature? a. 701 fpm, 79 KIAS b. 946 fpm, 79 KIAS c. 1315 fpm, 82 KIAS d. 1068 fpm, 82 KIAS 66. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, sea level pressure altitude at a temperature of 25 degree Celsius? a. 171 fpm, 80 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 67. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, 2000 pressure altitude at a temperature of 25 degree Celsius? a. 171 fpm, 80 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 68. What is the normal landing gear tires pressure? a. Nose tire 1.7/24 Psi, main landing gear tires 2.3 Bar/33 Psi b. Nose tire 2.0/28 Psi, main landing gear tires 2.5 Bar/35 Psi c. Nose tire 1.5/23 Psi, main landing gear tires 2.0 Bar/32 Psi d. Nose tire 1.8/25 Psi, main landing gear tires 2.2 Bar/32.5 Psi 69. Emergency procedures memory items: Enumerate the emergency procedures in an engine failure during takeoff run-(before rotation: abort take off) a. 1. Throttle Lever BOTH IDLE 2. Rudder Keep heading control 3. Brakes As required b. 1. Rudder Keep heading control 2. Throttle Lever BOTH IDLE 3. Brakes As required 70. Emergency procedures: Enumerate the emergency procedures in Engine Securing applicable to shutdown in flight a. 1. Throttle Lever IDLE 2. Ignition BOTH OFF 3. Propeller Lever FEATHER 4. Fuel Selector OFF 5. Electric fuel pump OFF 71. Emergency procedures memory items: Engine failure during climb a. 1. Autopilot OFF 2. Heading Keep control using rudder and ailerons 3. Attitude Reduce as appropriate to keep airspeed over 62 KIAS 72. Emergency procedures memory items: Engine failure in flight a. 1. Autopilot OFF 2. Heading Keep control using rudder and ailerons 3. Attitude Adjust as appropriate to keep airspeed over 62 KIAS 73. Emergency procedures memory items: Engine fire on the ground a. 1. Fuel selectors BOTH OFF 2. Ignitions ALL OFF 3. Electric fuel pumps BOTH OFF 4. Cabin heat and defrost OFF 5. MASTER SWITCH OFF 6. Parking Brake ENGAGED 7. Aircraft evacuation carry out immediately b. 1. Fuel selectors BOTH OFF 2. Ignitions ALL OFF 3. Electric fuel pumps BOTH OFF 4. Cabin heat and defrost OFF 5. MASTER SWITCH OFF 6. Parking Brake ENGAGED 7. Aircraft evacuation carry out immediately 74. Emergency procedures memory items: If decision is taken to continue the takeoff after an engine failure. a. 1. Operating engine throttle Lever FULL POWER 2. Operating engine propeller Lever FULL FORWARD 3. Heading Keep control using rudder and ailerons 4. Attitude Reduce as appropriate to keep airspeed over 62 KIAS 5. Inoperative engine Propeller lever FEATHER 6. Landing gear control lever UP 7. Airspeed Vxse/Vyse as required 8. Flaps 0 degree  b. 1. Landing gear control lever UP 2. Operating engine propeller Lever FULL FORWARD 3. Heading Keep control using rudder and ailerons 4. Attitude Reduce as appropriate to keep airspeed over 62 KIAS 5. Inoperative engine Propeller lever FEATHER 6. Landing gear control lever UP 7. Airspeed Vxse/Vyse as required 8. Operating engine throttle Lever FULL POWER 8. Flaps 0 degree 75. What is capacity of each wing tank? a. 100 liters b. 200 liters c. 300 liters d. 120 liters 76. What is the maximum CHT for the Engine Model Rotax 912 S3? a. 140 deg C b. 135 deg C c. 130 deg C 77. What is the minimum and maximum oil temperature for the Rotax 912 S3? a. 50 deg C/130 deg C b. 60 deg C/150 deg C c. 45 deg C/125 deg C 78. What is the minimum oil pressure for the Rotax 912 S3 engine? a..9 Bar/13 psi (below 1400 rpm prop) b..8 Bar/12 psi (below 1400 rpm prop) c..7 Bar/11 psi (below 1400 rpm prop) 79. What is the normal oil pressure for the Rotax 912 S3 engine? a. 7 Bar/102 psi (above 1400 rpm prop) b. 2 -5 Bar/29 -73 psi (above 1400 rpm prop) c. 0.8 Bar/12 psi (below 1400 rpm prop) 80. What is the minimum and maximum fuel pressure? a. Minimum 0.15 Bar/2.2 psi; Maximum 0.40 Bar/5.8 psi b. Minimum 0.10 Bar/2.2 psi; Maximum 0.50 Bar/5.8 psi c. Minimum 0.17 Bar/2.2 psi; Maximum 0.60 Bar/5.9 psi 81. What is the maximum operating altitude of the P2006T? a. 14,000 feet MSL b. 18,000 feet MSL c. 12,000 feet MSL 82. The following are approved maneuvers for the P2006T except a. Stalls b. Lazy eights c. Chandelle d. Spins 83. The following are approved maneuvers for the P2006T except a. Stalls b. Lazy eights c. Chandelle d. Turns with angle of bank of more 60 degrees 84. What is the minimum and maximum oil capacity of the P2006T engine? a. Max 3.0 liters – min 2.0 liters (per tank) b. Max 2.5 liters – min 2.2 liters (per tank) c. Max 3.5 liters – min 2.5 liters (per tank) 85. What is the voltmeter’s normal operating range? a. 12 – 14 Volt b. 10 – 12 Volt c. 14 – 16 Vol 86. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1080 kg, 4000 feet pressure altitude at a temperature of 25 degree Celsius? a. 80 fpm, 79 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 87. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, 4000 feet pressure altitude at a temperature of 0 degree Celsius? a. 111 fpm, 79 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 88. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, 1000 feet pressure altitude at a temperature of 25 degree Celsius? a. 134 fpm, 80 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 89. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, sea level pressure altitude at a temperature of 25 degree Celsius? a. 171 fpm, 80 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 90. Refer to Figure 5. What is the one-engine rate of climb and Climb speed(Vyse) at a weight of 1180 kg, 3000 pressure altitude at a temperature of 25 degree Celsius? a. 60 fpm, 79 KIAS b. 134 fpm, 80 KIAS c. 97 fpm, 80 KIAS d. 60 fpm, 80 KIAS 91. Refer to figure 2. What is the stall speed with flaps T/O, bank angle 15 a. 57 KIAS b. 64 KIAS c. 56 KIAS d. 53 KIAS 92. Refer to figure 2. What is the stall speed with flaps full, bank angle 30 a. 66 KIAS b. 64 KIAS c. 58 KIAS d. 53 KIAS 93. Refer to figure 2. What is the stall speed in KIAS with flaps 0, bank angle 60 a. 66 KIAS b. 64 KIAS c. 56 KIAS d. 93 KIAS 94. Refer to figure 2. What is the stall speed with flaps 0, bank angle 45 a. 77 KIAS b. 64 KIAS c. 56 KIAS d. 53 KIAS 95. Refer to figure 2. What is the stall speed with flaps full, bank angle 30 a. 58 KIAS b. 64 KIAS c. 56 KIAS d. 53 KIAS 96. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 90 deg and wind speed is 10 knots? a. Headwind = 0 Kts ; Crosswind = 10 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above 97. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 45 deg and wind speed is 20 knots? a. Headwind = 14 Kts ; Crosswind = 14 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above 98. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 20 deg and wind speed is 20 knots? a. Headwind = 18 Kts ; Crosswind = 7 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above 99. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 0 deg and wind speed is 20 knots? a. Headwind = 20 Kts ; Crosswind = 0 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above 100. Refer to Figure 3. What is the headwind and crosswind component if the wind direction(wind respect to aircraft longitudinal axis) is 30 deg and wind speed is 20 knots? a. Headwind = 17.5 Kts ; Crosswind = 10 Kts b. Headwind = 18 Kts ; Crosswind = 12 Kts c. Headwind = 20 Kts ; Crosswind = 16 Kts d. None of the above Figure 2 Figure 4 Figure 5