Tecnam P 2006T 85 Questions PDF

Questions Tecnam P 2006T Tecnam P2006T 1. Choose the INCORRECT statement a) The model number of the engine is 912 S3 b) The type of engine is four cylinder horizontally...

Questions Tecnam P 2006T Tecnam P2006T 1. Choose the INCORRECT statement a) The model number of the engine is 912 S3 b) The type of engine is four cylinder horizontally opposed c) The cylinder and cylinder heads are air cooled d) All are correct 2. The travel limit of the trailing edge of stabilator is a) Up 20° Down 17° c) Up 2° Down 19° b) Up 4° Down 15° d) Up 20° Down 20° 3. Choose the INCORRECT statement regarding propeller a) The diameter of propeller is 1780 mm b) It has three blades made of wood/composite with aluminum hub c) It is hydraulically controlled variable pitch propeller d) The manufacturer of propeller is MT propeller 4. The approved type of fuel for Tecnam P2006T is: a) MOGAS ASTM D4814(Check if DGCA has approved MOGAS) b) MOGAS EN228 Super/ Super plus c) AVGAS 100LL (ASTM D910) d) All of the above 5. VYSE refers to: a) Single engine control speed b) Minimum control speed c) Best Angle of Climb speed in case of one engine inoperative d) Best Rate of Climb speed in case of one engine inoperative 6. TOD a) Is the distance measured from actual start to wheel lift off point b) Is the distance measured from start to 15m obstacle clearance c) Is the distance measured from lift off to 15m obstacle clearance d) None of the above 7. VNO VLE VMC (in KIAS) a) 167 135 93 b) 135 118 93 c) 135 93 62 d) 135 118 62 8. Maximum full flaps extended speed is: 1 Questions Tecnam P 2006T a) 62 KIAS c) 119 KIAS b) 93 KIAS d) 118 KIAS 9. The significance of blue line in ASI is: a) Minimum Control Speed with one engine inoperative b) Best AOC Speed with one engine inoperative c) Best ROC Speed with one engine inoperative d) Rotation Speed 10. Mark the correct one: a) Maximum CHT is 135 F b) Normal range for oil pressure is 29-73 PSI c) Maximum oil pressure is 107 PSI d) None is correct 11. Rear seat must be kept in _______ and _______ position during taxi, take off, landing and emergency landing a) Lowest and full aft c) Highest and full forward b) Lowest and full forward d) Highest and full aft 12. Choose the correct one: a) The low pressure limit for landing gear hydraulic system is 20 bar. b) As in (a) and if during preflight inspection the value is below 20 bar, the system must be recharged by means of override button c) As in (a) and if during preflight inspection the value is below 20 bar, the pilot should wait for the system to come within limit for one minute. 13. To by pass the door locking system for emergency exit a) Push and hold red tab down b) Pull and hold red tab down c) As in (a) and open door with handle d) As in (b) and open door with handle 14. For main door exit a) Verify propeller stopped before opening door b) Exit towards back of aircraft c) Exit towards front of aircraft d) Both a and c 15. The color of lights on annuciator panel indicates: a) Green to indicate that pertinent device is turned on 2 Questions Tecnam P 2006T b) Amber to indicate on hazard situation which have to be considered and which requires a proper crew action c) Red to indicate emergency condition d) All are correct 16. The procedure for engine securing during flight is: a) Throttle IDLE, Ignition- Both off, Propeller- Feather, Fuel Selector – OFF, Fuel Pump – OFF b) Throttle IDLE, Mixture- IDLE cut off, Ignition- OFF, Propeller- Feather, Fuel Pump OFF c) Throttle IDLE, Mixture Idle cut off, Propeller- Feather, Fuel Selector OFF 17. In case of propeller over-speeding in flight, procedure is: a) Throttle Lever – Reduce Power to minimum practical Propeller Lever – Reduce as practical RPM indicator – Check b) Throttle Lever – Reduce Power to minimum practical Propeller Lever – Feather RPM indicator – Check c) Throttle Lever – Reduce Power to idle Propeller Lever – Feather RPM indicator – Check 18. Choose the correct statement a) Flaps up take requires take off distance increased by about 20% b) Carburetor heating selected ON will cause engine RPM reduction of about 100 rpm causing sensible available power decrease c) If flaps control fails, consider higher stall speed and increased landing distance by about 25% d) All are correct 19. Choose the correct statement: a) The ineffectiveness of one engine results in asymmetric traction which tends to yaw and bank the aircraft towards the inoperative engine. b) As in (a) and In this condition, it is essential to maintain the direction of the flight compensating the lower traction and counteracting the yawing effects by means of rudder pedals c) As in (b) and to improve directional control, it is advisable to bank the aircraft of about 10° to the side inoperative engine d) All are correct 20. Which statement is correct regarding magneto check? a) Magneto check on this aircraft is carried out at 1650 RPM b) Maximum RPM differencefrom Both to R/L should not exceed 150 RPM c) The differential RPM drop between R and L should not be over 75 RPM 3 Questions Tecnam P 2006T d) All are correct 21. Maximum demonstrated cross wind is _____ a) 17 kts b) 15 kts c) 20 kts d) 35 kts 22. Mark the INCORRECT statement: a) Each wing consists of light alloy torque box which carries all the wing bending, shear and torque loads b) Fuselage is constituted by light alloy semi monocoque structure wrapped around by stressed skin panel c) Radome and stern fairing are made up of light alloy d) All are correct 23. Rudder is made up of a) Light alloy c) Steel Alloy b) Aluminum alloy d) Composite material 24. The secondary flight controls consists of _____ a) One axis trim system b) As in (a) and flap system c) Two axis trim system d) As in (c) and flap system 25. Rudder trim tab is operated ________ a) Manually via control wheel b) Electrically via switch c) Can be adjusted on ground only 26. Emergency light is a five leds light located a) Over the LH instrument panel b) In the overhead panel c) Over RH instrument panel 27. The lubrication system of the engine is a) Dry sump b) Wet sump c) Dry sump with oil pump with integrated pressure regulator d) Wet sump with oil pump 28. The fuel gascolator is located beneath engine nacelle a) Between fuel tank and electric pump b) Before electric pump 4 Questions Tecnam P 2006T c) After electric pump d) Before engine driven pump 29. Mark correct statement regarding fuel system a) Each fuel tank has a capacity of 100 liters b) As in (a) and is equipped with a vent valve c) As in (a) and a sump fitted with drain valve d) All are correct 30. The landing gear retraction system is: a) Hydraulic type c) Electro-hydraulic type b) Electric type d) Mechanical type 31. Emergency operation of landing gear extension is done by means of: a) Hydraulic jacks b) Gravity only c) Hydraulic accumulator which discharge pressurized oil in jacks 32. A warning horn alerts pilots when: a) Landing Gear control knob is in UP position b) As in (a) and both the throttle levers are at idle and/or flaps are in LAND position c) As in (a) and at least one of the throttle is at idle and /or flaps are in LAND position 33. The cabin heat control knobs are positioned on : a) Lower side of LH instrument panel b) Lower side of RH instrument panel c) Central console d) Upper side of LH instrument panel 34. Maximum baggage weight allowed is ______ a) 120 kg b) 80 kg c) 130 lbs d) 80 lbs 35. Each generator is rated at: a) 12 VDC, 20 amp c) 14.2-14.8 VDC, 20 amp b) 14.2-14.8 VDC, 40 amp d) 12 VDC, 40 amp 36. During normal operations, two generators operate in _____ a) Parallel b) Series c) independent 37. Cockpit lights are supplied by a) Battery bus c) Generator bus b) LH Avionics bus d) RH Avionics bus 5 Questions Tecnam P 2006T 38. Mark the correct statement: a) When aircraft is moved on ground, either manually or by towing, Master switch must be turned on until aircraft is parked b) Do not turn the nose wheel above 20° either side of center c) Mooring is strongly recommended when wind is more than 15 knots and aircraft is completely refueled d) All are correct 39. A fully charged battery can supply electric power for at least a) 15 min b) 30 min c) 10 min d) 45 min 40. In case nose landing gear UP position is reported, touchdown should be made at a speed: a) Below 93 KIAS b) At 62 KIAS c) As low as 50 KIAS with flaps d) At 70-90 KIAS 41. Power loading of Tecnam P2006T at MTOW 1180 kg is a) 16.37 lb/hp c) 13.26 lb/hp b) 13.84 lb/hp d) 17.1 lb/hp 42. Normal operation range of Oil temperature is: a) 80-100° C c) 90-110°C b) 90-100°C d) 110-130°C 43. The wingspan for Tecnam P2006T is: a) 28.5 ft c) 35.1 ft b) 37.4 ft d) 40.5 ft 44. The overall unusable fuel is: a) 5.6 liters c) 3.5 liters b) 5.0 liters d) 4.0 liters 45. Cooling system of Tecnam P2006T aircraft is: a) Ram-air cooled cylinders, liquid cooled cylinder head (closed and pressurized circuit) b) Ram-air cooled cylinders, liquid cooled cylinder head (closed and un-pressurized circuit) c) Liquid cooled cylinders, liquid cooled cylinder head (closed and un-pressurized circuit) d) Liquid cooled cylinders, liquid cooled cylinder head (closed and pressurized circuit) 46. Find the correct statement: 6 Questions Tecnam P 2006T a) Left fuel selector manages the left engine feeding, allowing fuel supply from the left fuel tank or from the right one (crossfeed). b) Right fuel selector manages the right engine feeding, allowing fuel supply from the right fuel tank or from the left one (crossfeed). c) Each selector can be set in OFF position only pulling and simultaneously rotating the lever: this avoids an unintentional operation. d) All of the above are correct 47. Maximum continuous propeller rpm/engine rpm for maximum power are: a) 2265/5800 b) 2388/5800 c) 2265/5500 d) 2388/5500 48. Find the incorrect statement: a) Strobe lights are located on the winglets and on top of vertical fin. b) Taxi and landing lights are located on the left wing leading edge. c) NAV lights, a total three in number are provided to avoid collision on ground and in the air d) All above lights have dedicated switches located on the right instrument panel. 49. Maximum continuous rpm/engine rpm for maximum power is: a) Fuel quantity indicators and fuel pressure indicators for each engine are located on the LH instrument panel. b) Fuel quantity indicators and fuel pressure indicators for each engine are located on the LH and RH instrument panel respectively. c) Fuel quantity indicators and fuel pressure indicators for each engine are displayed on MFD. d) Fuel quantity indicators and fuel pressure indicators for each engine are located on the RH instrument panel. 50. Indicate the correct statement about the fuel system of Tecnam P2006T: a) Each wing tank is equipped with a vent valve which is located on the upper wing skin. b) Each wing tank is equipped with a vent valve which is located on the lower wing skin. c) The fuel system in normal operation relies on electric pumps, one for each tank d) The fuel system in normal operation relies on an engine operated pump apart from an electric pump for safety. 51. In Tecnam P2006T Gascolator is: a) An air intake booster located on the inlet manifold. b) Installed to provide better scavenging of exhaust gasses c) A sediment filter bowl d) None of the above 7 Questions Tecnam P 2006T 52. Landing gear retraction system in Tecnam P2006T is: a) Electro-hydraulic type powered by non-reversible pump which is electrically controlled b) Electro-hydraulic type powered by reversible pump which is electrically controlled. c) Electro-hydraulic type powered by reversible pump which is mechanically controlled d) None of the above 53. Aural warning to avoid accidental “gear up” landing depends on the landing configuration in terms of: a) Flaps, throttle levers and landing gear position b) Throttle levers and landing gear position only c) Flaps and throttle levers only d) Landing gear position only 54. An alternate static source is located: a) Under the left wing b) In the cockpit, on the control wheel c) In the cockpit central pedestal 55. The P2006T engine is characterized by: a) 4 cylinders horizontally opposed with 1352 c.c. of overall displacement b) 4 cylinders horizontally opposed with 1211 c.c. of overall displacement c) 4 cylinders horizontally opposed with 2200 c.c. of overall displacement d) 4 cylinder horizontally inline with 1211 c.c. of overall displacement 56. Which type of oil is approved for the engines? a) Aviation Grade Mineral Oil (Red Can) b) Aviation Grade Syntetic Oil (Blue Can) c) API Classification "SG" or higher 57. Which type of fire extinguisher equipped the P2006T? a) Carbon Dioxide b) Halon 1211 c) Dry Powder 58. The P2006T flap indicator displays: a) 4 positions related to 0°, take off (T/O), 15°and landing (FULL) b) 2 positions related to takeoff (T/O) and landing (FULL) c) 3 positions related to 0°, takeoff (T/O) and landing (FULL) 59. What does RPM indicator indicates? a) Propeller revolution b) Engine revolution c) Propeller pitch 60. Each main gear is a single axle unit characterized by: a) An oleo-pneumatic shock absorber b) Two oleo-pneumatic shock absorbers 8 Questions Tecnam P 2006T c) A rubber pad shock absorber d) None of the above 61. P2006T static air sources are located: a) At the top of the fuselage b) At both sides of the fuselage c) At the left side of the fuselage d) At the right side of the fuselage 62. What is ambient temperature limitation of the Tecnam P2006T a) -22 degree Celsius to 45 degree Celsius b) -25 degree Fahrenheit to 50 Fahrenheit c) -25 degree Celsius to 45 degree Celsius d) -25 degree Celsius to 50 degree Celsius 63. Maximum operating altitude of Tecnam P2006T is a) 14000 ft MSL b) 13500 ft MSL c) 14500 ft MSL d) 15000 ft MSL 64. What is the procedure for emergency landing gear operation? a) Remove access panel on the co-pilot side floor and turn the upper right hand control lever 90 degrees counter clockwise, wait for 20 seconds and turn the left hand lever 90 degrees counterclockwise. b) Remove access panel on the pilot side floor and turn the upper right hand control lever 90 degrees counter clockwise, wait for 20 seconds and turn the left hand lever 90 degrees counterclockwise. c) Remove access panel on the co-pilot side floor and turn the upper right hand control lever 90° counter clockwise, wait for 20 seconds and turn the left hand lever 180° counterclockwise. d) Remove access panel on the pilot side floor and turn the upper right hand control lever 90 degrees counter clockwise, wait for 20 seconds and turn the left hand lever 180 degrees counterclockwise. 65. Consider the following statements regarding propeller check: a) Propeller check is carried out at 1650 rpm b) Propeller must be checked from minimum to maximum three times. c) Both a and b are correct d) Neither a nor b is correct 66. Standard empty weight is a) Weight of the aircraft with full fluids & oil and full fuel b) Weight of the aircraft with engine fluids and oil at operating level c) Weight of aircraft without fuel and engine fluids d) None of the above 67. Maximum oil capacity for Tecnam P2006T : a) 2 liters c) 3 liters in total 9 Questions Tecnam P 2006T b) 3 liters in each tank d) 6 liters in each tank 68. The range of green arc of ASI is a) 53-93 b) 66-135 c) 66-80 d) 62-167 69. The flight time above 12500 ft without supplement oxygen is limited to a) 10 min b) 30 min c) 30 sec d) 5 min 70. Minimum limit for fuel pressure (in psi) is: a) 2.2 b) 0.8 c) 2.0 d) 5.8 71. Normal operating range of voltmeter is: a) 10-12 V b) 11-14 V c) 12-14 V d) 5-10V 72. Excessive oil pressure leads to _________ a) High pitch propeller configuration b) Low pitch propeller configuration c) As in (a) and with consequent propeller feathering d) As in (b) and with consequent propeller overspeeding 73. Yellow arc of propeller rpm: a) 2265-2388 b) 580-2265 c) 2365-2588 d) None 74. An excessive oil pressure value can be counteracted by a) Decreasing propeller rpm c) decreasing engine rpm b) Increasing propeller rpm d) increasing engine rpm 75. Flight into known icing conditions________ a) Permitted with carb heat BOTH ON b) Permitted with pitot ON c) Both a and b d) is prohibited 76. The immediate action after engine failure in flight: a) Operating engine fuel pump ON, operating engine fuel selector CROSSFEED b) Autopilot- OFF, heading- keep control using rudder and aileron, attitude- adjust to keep airspeed over 62 KIAS c) Land as soon as possible d) None of the above 77. An unwanted landing gear extension with at least one leg moving downward, may be caused by hydraulic fluid loss and it is signaled by : a) Significant aerodynamic noise increase b) Light and counteractable nose down pitch moment c) Red TRANS light turned on d) All of the above 78. Best angle of climb speed for MTOW 1230 kg is : a) 72 KIAS b) 84 KIAS c) 90 KIAS d) 65 KIAS 10 Questions Tecnam P 2006T 79. For starting of cold engine : a) Throttle – Fully closed, Chokes- Fully closed. Soon after starting, advance throttle to approx 800 rpm b) Throttle – fully open, chokes – fully open. Soon after starting, reduce throttle to 800 rpm and slowly close choke. Keep engine at 900 rpm for warm up c) Throttle- fully closed, chokes- fully opened. Soon after starting, reduce throttle to 800 rpm and slowly close choke. Keep engine at 900 rpm for warm up 80. For flooded engine (after engine start) a) Keep chokes closed, open throttle fully and start engine then quickly reduce throttle to idle b) Keep chokes open, open throttle fully and start engine c) Keep chokes closed, throttle fully closed and start engine, then advance throttle to 900 rpm 81. Engine should be warmed up to minimum oil temperature of _____ at ______ a) 60°C ; 1000 rpm c) 50°C ; 900 rpm b) 50°C ; 1200 rpm d) 60°C ; 1200 rpm 82. Maximum take off power must be limited to ____ a) 5 min b) 10 min c) no limit d) 2 min 83. The aircraft has a trim tab on _____ aileron and is __________ a) Left ; operated electrically via switch b) Left ; adjustable on ground only c) Right ; operated mechanically via control wheel d) Right ; adjustable on ground only 84. There are ______ outlet(s) in Tecnam P2006T for entering of ram air for ventilation a) One b) two c) three d) four 85. The battery bus is energized from _________ a) Battery c) LH or RH generator b) Both generator d) both a and c 11