Tecnam P92-js Aircraft Flight Manual Exam

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    Engine has:

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    • 8 cylinders
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Tecnam P92-js Aircraft Flight Manual Exam - Quiz
About This Quiz

For those of you who would like to know more about and all things aircrafts plus things that led to various events in the aircraft filed, this is for you. If you are prepared to test your knowledge try it out.


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  • 2. 

    Vne

    • Can be exceeded in smooth air

    • Can not be exceeded

    • Can be exceeded in a dive

    • Can not be exceeded in turbulent air

    Correct Answer
    A. Can not be exceeded
    Explanation
    The correct answer is "Can not be exceeded". Vne refers to the never exceed speed, which is the maximum speed that should not be exceeded under any circumstances. This speed is determined by the aircraft manufacturer and is based on factors such as structural limitations and safety considerations. Exceeding Vne can lead to structural damage or loss of control of the aircraft, so it is important for pilots to adhere to this speed limit.

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  • 3. 

    Maximum demonstrated crosswind component for the aircraft is:

    • 13 knots

    • 15 knots

    • 16 knots

    • 18 knots

    Correct Answer
    A. 15 knots
    Explanation
    The maximum demonstrated crosswind component for the aircraft is 15 knots. This means that the aircraft has been tested and proven to be able to safely handle crosswinds up to this speed. Any crosswind exceeding this limit may pose a risk to the aircraft's stability and control during takeoff or landing. It is important for pilots to be aware of the maximum demonstrated crosswind component for their aircraft in order to make informed decisions and ensure the safety of the flight.

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  • 4. 

    Cylinders in the engine are arranged in:

    • Radial

    • V-shape

    • In-line

    • Horizontally opposed

    Correct Answer
    A. Horizontally opposed
    Explanation
    The cylinders in an engine can be arranged in different configurations. In a horizontally opposed arrangement, the cylinders are positioned opposite each other, with the crankshaft located in the middle. This configuration helps to achieve a lower center of gravity and better balance in the engine, resulting in smoother operation and improved handling. It is commonly used in aircraft engines and some high-performance cars.

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  • 5. 

    Maximum baggage mass is:

    • 10kg

    • 20kg

    • 30kg

    • 40kg

    Correct Answer
    A. 20kg
    Explanation
    The maximum baggage mass allowed is 20kg. This means that passengers cannot exceed this weight limit when checking in their baggage. It is important to adhere to this limit to ensure safety and efficiency in handling luggage during travel. Exceeding the weight limit may result in additional charges or the need to remove items from the baggage.

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  • 6. 

    Minimum fuel pressure:

    • 1.0 psi

    • 14.0 psi

    • 2.2 psi

    • 5.0 psi

    Correct Answer
    A. 2.2 psi
    Explanation
    The minimum fuel pressure required is 2.2 psi. This means that the fuel system needs to maintain a pressure of at least 2.2 psi in order to properly function. If the pressure drops below this level, it can cause issues with fuel delivery and engine performance. Therefore, it is important to ensure that the fuel pressure is always above the minimum requirement.

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  • 7. 

    In case of irregular engine RPM you should first:

    • Check throttle position, turn on carburetor heat, turn on electric fuel pump

    • Land at the closest airport

    • Apply full power and climb

    • Try to restart the engine

    Correct Answer
    A. Check throttle position, turn on carburetor heat, turn on electric fuel pump
    Explanation
    In case of irregular engine RPM, checking the throttle position is important as it could be a possible cause for the issue. Turning on the carburetor heat helps to prevent ice formation which can affect engine performance. Turning on the electric fuel pump ensures a steady fuel supply to the engine. These steps are necessary to diagnose and address the problem before considering other options like landing or restarting the engine.

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  • 8. 

    Maximum continuous power is:

    • 92.5hp

    • 51.5hp

    • 100hp

    • 105.5hp

    Correct Answer
    A. 92.5hp
    Explanation
    The maximum continuous power is stated to be 92.5hp. This means that the engine or device can consistently produce a maximum power output of 92.5 horsepower without any interruptions or limitations.

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  • 9. 

    Total unusable fuel is:

    • 87.5 liters

    • 3.2 liters

    • 2 liters

    • 1.5 liters

    Correct Answer
    A. 3.2 liters
    Explanation
    The given answer of 3.2 liters is the total unusable fuel.

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  • 10. 

    Aircraft has:

    • 1.5 degree dihedral

    • 1.5 degree anhedral

    • No dihedral / anhedeal

    • 91.5 degree dihedral

    Correct Answer
    A. 1.5 degree dihedral
    Explanation
    The correct answer is 1.5 degree dihedral. Dihedral refers to the upward angle of the wings from the horizontal axis of the aircraft. A positive dihedral angle creates stability by allowing the aircraft to roll in response to disturbances, making it easier to control. In this case, the aircraft has a small dihedral angle of 1.5 degrees, indicating a slight upward angle of the wings.

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  • 11. 

    Engine model is:

    • 912 S2

    • 912

    • 912 UL

    • IO-240B

    Correct Answer
    A. 912 S2
    Explanation
    The correct answer is 912 S2 because it is the specific engine model mentioned in the given options. The other options, 912, 912 UL, and IO-240B, are not the exact engine models listed.

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  • 12. 

    Propeller is:

    • Made of composites

    • Made of wood

    • Made of aluminum

    • A variable pitch propeller

    Correct Answer
    A. Made of wood
    Explanation
    Wood is a common material used in the construction of propellers. It is lightweight, durable, and has excellent strength-to-weight ratio, making it suitable for propeller applications. Wood propellers are also known for their natural balance and ability to absorb vibrations, resulting in smoother operation. Additionally, wood propellers can be easily repaired or reshaped if damaged, making them a cost-effective choice.

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  • 13. 

    Maximum cylinder head temperature is:

    • 125° C

    • 135° C

    • 130° C

    • 140° C

    Correct Answer
    A. 135° C
    Explanation
    The maximum cylinder head temperature is 135° C. This means that the temperature of the cylinder head should not exceed 135° C in order to prevent any potential damage or malfunction. It is important to monitor and control the temperature to ensure the engine operates within safe limits.

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  • 14. 

    Maximum useful load (Standard aircraft)

    • Is 225kg

    • Is 192kg

    • Does not include fuel

    • Does not include baggage

    Correct Answer
    A. Is 225kg
    Explanation
    The maximum useful load for a standard aircraft is 225kg. This means that the aircraft can carry a maximum weight of 225kg, which includes passengers, cargo, and any other items on board. It does not include the weight of fuel or baggage.

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  • 15. 

    P92-JS maybe operated:

    • Under IFR

    • Only under VFR, day and night

    • Only under VFR, only day

    • Under IFR if IFR equipped

    Correct Answer
    A. Only under VFR, only day
    Explanation
    The correct answer is "only under VFR, only day." This means that the aircraft can only be operated under Visual Flight Rules (VFR) and only during daylight hours. It cannot be operated under Instrument Flight Rules (IFR) or at night.

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  • 16. 

    Maximum power (less than 5 minutes) of the engine is:

    • 98.6 hp

    • 121 hp

    • 88.5 hp

    • 100 hp

    Correct Answer
    A. 98.6 hp
    Explanation
    The maximum power of the engine is determined to be 98.6 hp.

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  • 17. 

    While flying at 1500ft you notice low engine oil pressure with increasing oil temperature. Your following action is to:

    • Reduce engine throttle to slow down to 70 KIAS and land as soon as possible

    • Increase speed to 100 KIAS in order to increase engine cooling and land as soon as possible

    • Land as soon as possible

    • Continue to your destination in the most direct manner

    Correct Answer
    A. Reduce engine throttle to slow down to 70 KIAS and land as soon as possible
    Explanation
    The correct answer is to reduce engine throttle to slow down to 70 KIAS and land as soon as possible. This is the appropriate action to take when experiencing low engine oil pressure and increasing oil temperature. By reducing the engine throttle, it helps alleviate the strain on the engine and reduces the risk of further damage. Slowing down to 70 KIAS also helps in maintaining control and stability during the landing. Landing as soon as possible is necessary to address the issue and prevent any potential engine failure or damage.

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  • 18. 

    Engine is manufacrured by:

    • Lycoming

    • Continental

    • Rotax GmbH

    • Bombardier-Rotax GmbH

    Correct Answer
    A. Bombardier-Rotax GmbH
    Explanation
    Bombardier-Rotax GmbH is the correct answer because it is a well-known manufacturer of engines. They have a strong reputation in the industry for producing high-quality engines. Lycoming, Continental, and Rotax GmbH are also engine manufacturers, but Bombardier-Rotax GmbH is the most suitable answer as it specifically mentions the joint venture between Bombardier and Rotax GmbH.

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  • 19. 

    Engine can be run at maximum continuous power for:

    • A maximum of 5 minutes

    • A maximum of 7 minutes

    • As long as oil temperature, cylinder head temperature and oil pressure remain bellow specific values

    • A maximum of 3 minute

    Correct Answer
    A. A maximum of 5 minutes
    Explanation
    The correct answer is "A maximum of 5 minutes." This means that the engine can only be run at maximum continuous power for a maximum duration of 5 minutes. It is important to adhere to this time limit to prevent any potential damage to the engine.

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  • 20. 

    Is case of engine fire in flight:

    • Fuel valves should be turned off and full throttle applied

    • You should land at the nearest airfield

    • Fire extinguisher should be used to fight the fire

    • Engine should be secured and best glide speed obtained

    Correct Answer
    A. Fuel valves should be turned off and full throttle applied
    Explanation
    In case of an engine fire in flight, the correct action to take is to turn off the fuel valves and apply full throttle. This is because turning off the fuel valves will cut off the fuel supply to the engine, which can help prevent the fire from spreading further. Applying full throttle can help to extinguish the fire by blowing it out with the force of the airflow. It is important to prioritize shutting off the fuel valves before attempting to fight the fire with a fire extinguisher or securing the engine. Landing at the nearest airfield and obtaining the best glide speed are also important steps to ensure a safe landing in case the fire cannot be fully extinguished.

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  • 21. 

    Colour of AVGAS 100LL is:

    • Blue

    • Red

    • Green

    • Straw

    Correct Answer
    A. Blue
    Explanation
    AVGAS 100LL is a type of aviation gasoline commonly used in piston engine aircraft. It is dyed blue to distinguish it from other types of fuel. The blue color helps to prevent accidental misfueling of aircraft with other types of fuel, such as jet fuel or diesel. This color coding system ensures that the correct type of fuel is used for each aircraft, promoting safety and preventing potential engine damage.

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  • 22. 

    Minimum suction pressure is:

    • 4 in. Hg

    • 0 in. Hg

    • 55 in Hg

    • 14 in Hg

    Correct Answer
    A. 4 in. Hg
    Explanation
    The minimum suction pressure is the lowest pressure at which a suction system can effectively operate. In this case, the correct answer is 4 in. Hg, indicating that the system can operate at a minimum pressure of 4 inches of mercury.

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  • 23. 

    Load factors for the aircraft are:

    • +3.8G / -1.9G

    • +4.4G / -1.76G

    • +6.0G / -3.0G

    • +2.5G / -1.5G

    Correct Answer
    A. +3.8G / -1.9G
    Explanation
    The given answer, +3.8G / -1.9G, represents the load factors for the aircraft. Load factor refers to the ratio of the total load supported by the aircraft to its weight. In this case, the aircraft can withstand a maximum positive load factor of 3.8G, which means it can support 3.8 times its own weight before reaching its structural limit. The maximum negative load factor is -1.9G, indicating that the aircraft can withstand 1.9 times its weight in the opposite direction. These load factors are important for determining the structural integrity and limits of the aircraft during flight maneuvers and turbulence.

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  • 24. 

    Maximum take-off mass is (Standard aircraft):

    • 550kg

    • 450kg

    • 500kg

    • 600kg

    Correct Answer
    A. 550kg
    Explanation
    The maximum take-off mass for a standard aircraft is 550kg. This means that the aircraft, including its fuel, passengers, and cargo, cannot exceed this weight when taking off. It is an important safety consideration as exceeding the maximum take-off mass can affect the aircraft's performance and ability to safely lift off the ground.

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  • 25. 

    Va in KIAS

    Correct Answer
    93
  • 26. 

    Maximum suction pressure is:

    • 1 in. Hg

    • 5.5 in. Hg

    • 55 in Hg

    • 14 in Hg

    Correct Answer
    A. 5.5 in. Hg
    Explanation
    The maximum suction pressure is determined by the capacity and power of the suction pump. In this case, the correct answer is 5.5 in. Hg, indicating that the pump can create a maximum suction pressure of 5.5 inches of mercury. This means that the pump is capable of generating enough vacuum to lift a column of mercury to a height of 5.5 inches.

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  • 27. 

    Maximum value for oil pressure:

    • 2 bar

    • 7 bar for less than 30 seconds

    • 10 bar

    • What ever the pilot thinks is safe

    Correct Answer
    A. 7 bar for less than 30 seconds
    Explanation
    The maximum value for oil pressure is 7 bar, but only for a duration of less than 30 seconds. This suggests that the engine can tolerate a higher oil pressure for a short period of time, but it is not safe to maintain this high pressure for longer durations. It is important for the pilot to monitor and regulate the oil pressure to ensure the safety and proper functioning of the engine.

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  • 28. 

    Aircraft has a:

    • Full JAA type certification

    • Is type certified under JAA as a VLA (very light aircraft)

    • Is type certified under JAA as a LSA (light sports aircraft)

    • Is type certified by the Latvian CAA

    Correct Answer
    A. Is type certified under JAA as a VLA (very light aircraft)
    Explanation
    The correct answer is "Is type certified under JAA as a VLA (very light aircraft)". This means that the aircraft has undergone the necessary certification process and meets the requirements set by the Joint Aviation Authorities (JAA) for being classified as a very light aircraft. This certification ensures that the aircraft is safe and suitable for operation as a VLA.

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  • 29. 

    Maximum fuel pressure:

    • 2.2 psi

    • 3.3 psi

    • 1.0 psi

    • 5.8 psi

    Correct Answer
    A. 5.8 psi
    Explanation
    The maximum fuel pressure is 5.8 psi. This means that the fuel system is designed to operate at a maximum pressure of 5.8 pounds per square inch. This information is important for ensuring that the fuel system is functioning properly and that the correct pressure is being maintained for efficient fuel delivery to the engine.

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  • 30. 

    Minimum oil temperature before take-off is:

    • 50° C

    • 60° C

    • 70° C

    • There is no minimum oil temperature for normal operation

    Correct Answer
    A. 50° C
    Explanation
    The minimum oil temperature before take-off is 50°C. This means that the oil temperature must be at least 50°C before the aircraft can safely take off. This is important because the oil helps lubricate and cool the engine, and if the oil is too cold, it may not be able to perform these functions effectively. Therefore, it is necessary to ensure that the oil temperature is at least 50°C before initiating take-off procedures.

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  • 31. 

    Engine is:

    • Liquid cooled

    • Air cooled

    • Cooled by air and cooling is aided by the use of cowl flaps

    • Liquid and air cooled

    Correct Answer
    A. Liquid and air cooled
    Explanation
    The engine is both liquid and air cooled. This means that it uses a combination of liquid coolant and airflow to regulate its temperature. The liquid coolant helps to absorb and dissipate heat from the engine, while the airflow provided by the use of cowl flaps aids in cooling the engine further. This combination of cooling methods allows for efficient temperature regulation and helps prevent overheating of the engine.

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  • 32. 

    Vfe in KIAS

    Correct Answer
    68
  • 33. 

    Vy in KIAS

    Correct Answer
    70
  • 34. 

    Best glide speed at 450 KG or with flaps extened to 15° is:

    • 60 KIAS

    • 66 KIAS

    • 68 KIAS

    • 63 KIAS

    Correct Answer
    A. 60 KIAS
    Explanation
    The best glide speed at 450 KG or with flaps extended to 15° is 60 KIAS. This means that when the aircraft is at this weight or with the flaps at this angle, the optimal speed for maintaining the longest glide distance is 60 knots indicated airspeed. This speed allows for the most efficient use of the available lift generated by the wings, maximizing the aircraft's glide range.

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  • 35. 

    In case of engine failure at the cruise altitude:

    • First assess the situation

    • First find a place to land

    • First pitch for speed 66 KIAS

    • First try to restart the engine

    Correct Answer
    A. First pitch for speed 66 KIAS
    Explanation
    In case of engine failure at the cruise altitude, the first action should be to pitch for speed at 66 KIAS. This means adjusting the aircraft's pitch to maintain a specific airspeed. By doing so, the pilot can ensure that the aircraft maintains a safe and controlled descent while maximizing glide distance. This allows the pilot to have more time to assess the situation, find a suitable place to land, and attempt to restart the engine if possible.

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  • 36. 

    In case of fuel pressure falling bellow 2.2 psi the initial action is

    • To turn on the electric fuel pump

    • Switch both fuel tanks on

    • Apply carburetor heat

    • Land at the closest airfield

    Correct Answer
    A. To turn on the electric fuel pump
    Explanation
    When the fuel pressure falls below 2.2 psi, the initial action should be to turn on the electric fuel pump. This is because the electric fuel pump helps to maintain the required fuel pressure for the engine to operate properly. By turning on the electric fuel pump, it can help to restore the fuel pressure and prevent any further issues with the engine. Switching both fuel tanks on, applying carburetor heat, and landing at the closest airfield may be necessary actions depending on the situation, but the first step should be to turn on the electric fuel pump.

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  • 37. 

    To restart the engine in flight:

    • Throttle should be half way in

    • Throttle should be all the way in

    • Airspeed should be above 70 KIAS

    • Throttle should be on fast idle

    Correct Answer
    A. Throttle should be half way in
    Explanation
    Restarting the engine in flight requires the throttle to be halfway in. This means that the throttle should be set at a position that is halfway between idle and full power. This allows for a controlled increase in power to restart the engine without causing any sudden changes in speed or altitude. It is important to maintain a stable airspeed above 70 KIAS (Knots Indicated Airspeed) to ensure proper airflow and prevent stalling during the engine restart. Setting the throttle to fast idle or all the way in would not be appropriate for restarting the engine in flight.

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  • 38. 

    Standard empty weight of the aircraft is:

    • 550 kg

    • 325 kg

    • 225 kg

    • 358 kg

    Correct Answer
    A. 325 kg
    Explanation
    The correct answer is 325 kg. This refers to the standard empty weight of the aircraft, which is the weight of the aircraft without any fuel, passengers, or cargo. It is an important measurement for determining the maximum weight capacity and performance of the aircraft.

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  • 39. 

    Vne in KIAS

    Correct Answer
    134
  • 40. 

    Tecnam P92 is a:

    • Single pilot aircraft

    • Multi pilot aircraft

    • May be operated as a multi pilot aircraft provided it is operated for public air transport

    • Requires a type rating

    Correct Answer
    A. Single pilot aircraft
    Explanation
    The correct answer is Single pilot aircraft. This means that the Tecnam P92 is designed to be operated by only one pilot. It does not require multiple pilots to operate the aircraft.

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  • 41. 

    Aircraft is certified:

    • In aerobatics category

    • In utility category

    • In normal category

    • In VLA category

    Correct Answer
    A. In normal category
    Explanation
    The correct answer is "In normal category". This means that the aircraft has met all the necessary requirements and standards to be certified for normal operations. It indicates that the aircraft is suitable for general aviation purposes and can be used for regular flights, without any specific restrictions or limitations.

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  • 42. 

    Vobs in KIAS

    Correct Answer
    56
  • 43. 

    In case you unintentionally fly into cloud (enter IMC)

    • You should turn, climb or decent out of the cloud while flying on instruments

    • Continue through the cloud only if the cloud is very small while flying on instruments

    • Make a 180° degree turn on instruments

    • Assess the situation

    Correct Answer
    A. Make a 180° degree turn on instruments
    Explanation
    If a pilot unintentionally flies into a cloud (enters IMC), the correct action to take is to make a 180° degree turn on instruments. This is because flying in IMC without the proper training and equipment can be extremely dangerous and increase the risk of spatial disorientation. By making a 180° degree turn, the pilot can quickly exit the cloud and regain visual reference to maintain safe flight. It is important to rely on instruments rather than visual cues in this situation to avoid disorientation and potential loss of control.

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  • 44. 

    Vr in KIAS

    Correct Answer
    47
  • 45. 

    Fuel capacity of each wing tank is (long range tanks):

    • 35 liters

    • 70 liters

    • 34 liters

    • 45 liters

    Correct Answer
    A. 35 liters
    Explanation
    The fuel capacity of each wing tank is 35 liters.

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  • 46. 

    Maximum propeller RPM (maximum time 5 minutes) is:

    • 5800 RPM

    • 2388 RPM

    • 2265 RPM

    • 5500 RPM

    Correct Answer
    A. 2388 RPM
  • 47. 

    Maximum oil temperature for normal operating is:

    • 110° C

    • 135° C

    • 140° C

    • 145° C

    Correct Answer
    A. 110° C
    Explanation
    The maximum oil temperature for normal operating is 110°C. This means that the oil should not exceed this temperature during regular operation. Exceeding this temperature could lead to damage or malfunction of the equipment or system that relies on the oil for lubrication or cooling. It is important to monitor and control the oil temperature to ensure the proper functioning and longevity of the machinery.

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  • 48. 

    Navigation lights must be operational and turned on:

    • From sunset to sunrise

    • From take-off to landing

    • When ever aircraft is moving

    • At pilot's discretion

    Correct Answer
    A. From sunset to sunrise
    Explanation
    Navigation lights are required to be operational and turned on from sunset to sunrise. This is to ensure that the aircraft is visible to other pilots and to prevent any potential collisions during periods of reduced visibility. By having the navigation lights on during this time, it helps to maintain safety in the airspace and allows for better situational awareness for all pilots involved.

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  • 49. 

    You may refuel

    • At least 95 octane MOGAS or AVGAS 100

    • At least 98 octane MOGAS or AVGAS 100LL

    • At least 95 octane MOGAS or AVGAS 100LL

    • At least 98 octane MOGAS or AVGAS 100

    Correct Answer
    A. At least 95 octane MOGAS or AVGAS 100LL

Quiz Review Timeline (Updated): Mar 21, 2023 +

Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.

  • Current Version
  • Mar 21, 2023
    Quiz Edited by
    ProProfs Editorial Team
  • Jan 21, 2011
    Quiz Created by
    CaptSpock
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