Tecnam P92-js Aircraft Flight Manual Exam

  • FAA
  • EASA
  • ICAO
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Quizzes Created: 4 | Total Attempts: 1,946
| Attempts: 523 | Questions: 75
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1. Engine has:

Explanation

The engine has 4 cylinders.

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About This Quiz
Flight Operations Quizzes & Trivia

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

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:

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:

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:

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:

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:

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:

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:

Explanation

The given answer of 3.2 liters is the total unusable fuel.

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10. Aircraft has:

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:

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:

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:

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)

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:

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:

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:

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:

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:

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:

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:

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:

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:

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):

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

Explanation

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26. Maximum suction pressure is:

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:

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:

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:

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:

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:

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

Explanation

not-available-via-ai

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33. Vy in KIAS

Explanation

not-available-via-ai

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

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:

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

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:

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:

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

Explanation

not-available-via-ai

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40. Tecnam P92 is a:

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:

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

Explanation

not-available-via-ai

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43. In case you unintentionally fly into cloud (enter IMC)

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

Explanation

not-available-via-ai

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

Explanation

The fuel capacity of each wing tank is 35 liters.

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46. Maximum propeller RPM (maximum time 5 minutes) is:

Explanation

not-available-via-ai

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47. Maximum oil temperature for normal operating is:

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:

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

Explanation

not-available-via-ai

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50. Vlo in KIAS

Explanation

not-available-via-ai

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51. Vgl at MTOM with flaps extended in KIAS

Explanation

not-available-via-ai

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52. Maximum engine operating temperature is:

Explanation

The maximum engine operating temperature is + 40° C. This means that the engine can safely operate at temperatures up to 40° C without causing any damage or performance issues. Operating the engine at temperatures higher than this could potentially lead to overheating and other problems. It is important to monitor the engine temperature and take appropriate measures to prevent it from exceeding the maximum operating temperature.

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53. Best glide speed at 550 KG and flaps extened to 15° is:

Explanation

The best glide speed at 550 KG and flaps extended to 15° is 60 KIAS. This means that when the aircraft is at this weight and the flaps are set to 15°, the most efficient speed to maintain for a glide is 60 knots indicated airspeed. This speed allows the aircraft to maximize its gliding distance and maintain control while descending without power.

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54. Maximum oil pressure allowed is

Explanation

The maximum oil pressure allowed for a cold start for a short period is 7 bars. This means that during a cold start, the oil pressure can temporarily reach up to 7 bars before it needs to stabilize. It is important to have a higher oil pressure during cold starts to ensure proper lubrication and protection of the engine components. However, this higher pressure is only permissible for a short period to prevent any potential damage to the engine.

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55. Minimum oil pressure for normal operating is

Explanation

The correct answer is 2 bar. This means that the minimum oil pressure required for normal operating is 2 bar. Oil pressure is important for lubricating and cooling the engine components, so maintaining the proper oil pressure is crucial for the engine's performance and longevity. A lower oil pressure can indicate a problem with the oil pump or a leak, while a higher oil pressure can indicate a blockage or restriction in the oil passages. Therefore, it is important to monitor and maintain the oil pressure within the recommended range to ensure the engine's proper functioning.

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56. Best glide speed at MTOM and clean configuration is:

Explanation

The best glide speed at maximum takeoff weight (MTOM) and in a clean configuration is 66 KIAS. This means that when the aircraft is at its maximum weight and all unnecessary drag-inducing components (such as landing gear or flaps) are retracted, the optimal glide speed for maintaining the longest distance and time in the air is 66 knots indicated airspeed (KIAS). This speed allows for the most efficient use of the aircraft's aerodynamic properties and minimizes the rate of descent.

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57. In case of an engine failure during take-off I should first:

Explanation

In case of an engine failure during take-off, the correct first action is to pitch for 60 KIAS (Knots Indicated Airspeed) and land in the front sector while avoiding obstacles. This means that the pilot should adjust the aircraft's pitch to maintain a speed of 60 knots indicated airspeed and aim to land in an area that is in front of the aircraft's current position. The pilot should also be cautious of any obstacles, such as buildings or trees, and try to avoid them while landing. This action prioritizes the safety of the aircraft and its occupants by ensuring a controlled landing in a suitable area.

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58. In case of an engine failure during take-off an attempt to return to the field:

Explanation

Attempting to return to the field in case of an engine failure during take-off poses a significantly higher risk of fatal and serious injuries compared to trying to land into the front sector. This means that the chances of sustaining a fatal injury are 10 times higher and the chances of sustaining a serious injury are 5 times higher when attempting to return to the field.

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59. Following an engine failure you are trying to restart the engine by:

Explanation

not-available-via-ai

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60. Minimum cylinder head temperature is:

Explanation

The given answer states that there is no minimum cylinder head temperature for normal operation. This means that the engine can operate within a range of temperatures without any specific minimum requirement for the cylinder head temperature. This is likely because the cylinder head temperature can vary depending on factors such as engine load, ambient temperature, and cooling system efficiency. As long as the temperature remains within a safe operating range, there is no specific minimum temperature that needs to be maintained for normal operation.

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61. From an altitude of 1000ft on P92 you can glide:

Explanation

From an altitude of 1000ft on P92, you can glide for a distance of 3NM. This means that the aircraft can maintain its altitude and cover a horizontal distance of 3 nautical miles without using the engine. Gliding is possible due to the aerodynamic properties of the aircraft and the pilot's skill in managing the descent.

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62. Engine oil cooling is based on:

Explanation

The correct answer is the dry sump system. In a dry sump system, the engine oil is stored in a separate reservoir rather than in the oil pan. This allows for better cooling of the oil as it is not in direct contact with the hot engine components. The oil is circulated through a series of coolers to dissipate heat more efficiently. This system is commonly used in high-performance and racing engines to prevent oil starvation and maintain consistent lubrication under high G-forces and extreme operating conditions.

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63. Vgl at MTOM in clean configuration in KIAS

Explanation

not-available-via-ai

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64. Vs1 in KIAS with 45° of bank.

Explanation

The given correct answer is 52. This suggests that Vs1, which is the stalling speed in a specific configuration, is being measured in knots indicated airspeed (KIAS) with a 45° bank angle. The stalling speed is the minimum speed at which an aircraft can maintain controlled flight without stalling. The bank angle of 45° indicates that the aircraft is turning at a steep angle. Therefore, the stalling speed in this scenario is 52 KIAS.

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65. Vs1 in KIAS

Explanation

not-available-via-ai

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66. It is a cold winter day at Spilve. ATIS reported weather is CAVOK with temperature of -15°C and dewpoint -23°C.

Explanation

The given information states that the temperature is -15°C and the dewpoint is -23°C. Carburetor icing occurs when the temperature is near or below freezing and there is moisture present in the air. In this case, the temperature is significantly below freezing, which reduces the likelihood of moisture being present in the air. Therefore, it is unlikely that carburetor icing will occur due to the low temperature.

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67. Aircraft you want to take for a crosscountry flight has just returned and you observe that the preflight inspection has already been done earlier during the day.

Explanation

Conducting a preflight inspection on the aircraft is not required because it has already been done earlier during the day. The preflight inspection is typically done before each flight to ensure the aircraft is in proper working condition and safe to fly. However, since it has already been done, there is no need to repeat the inspection before the crosscountry flight.

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68. Maximum continuous propeller RPM is

Explanation

The maximum continuous propeller RPM is 2265 RPM. This means that the propeller should not exceed this speed for a prolonged period of time. Going above this RPM could potentially cause damage to the propeller or other components of the system. It is important to adhere to the specified RPM limit to ensure the safe and efficient operation of the propeller.

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69. Aircraft preflight inspection:

Explanation

The correct answer is "Is valid for 24 hours". This means that the preflight inspection of an aircraft is considered valid for a period of 24 hours. After this time, the pilot must conduct another preflight inspection before the next flight. It is important for pilots to regularly inspect the aircraft to ensure its safety and airworthiness.

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70. Aircraft is approved for:

Explanation

The correct answer is "Can only be approved for spinning if an STC spin kit is installed." This means that the aircraft can be approved for spinning, but only if a specific modification called an STC spin kit is installed. Without this modification, the aircraft is not approved for spinning. The reason for this requirement is likely related to the forward center of gravity, which makes it difficult or unsafe for the aircraft to enter a spin without the additional equipment provided by the spin kit.

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71. Aircraft minimum equiptment required:

Explanation

The given list includes the minimum equipment required for an aircraft. These instruments are essential for safe flight operations. The altimeter is used to measure the altitude of the aircraft, the airspeed indicator measures the speed of the aircraft, and the heading indicator indicates the aircraft's direction. The fuel gauge, oil pressure indicator, oil temperature indicator, and cylinder head temperature indicator are crucial for monitoring the engine's performance and ensuring its proper functioning. The outside air temperature indicator helps in determining the temperature outside the aircraft. The tachometer measures the engine's revolutions per minute, and the chronometer is used for accurate timekeeping. The first aid kit and hand-held fire extinguisher are necessary for emergencies, and the life raft is essential for over-water flights.

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72. Which one is correct regarding aircraft spinning?

Explanation

In aircraft spinning, it is important to neutralize the rudder as the spin is halted. This means that the pilot should center the rudder pedals to prevent any further yawing motion once the spin has stopped. This is crucial for regaining control and stabilizing the aircraft. Applying opposite rudder or holding the stick neutrally in the middle until the spin has halted can prolong the spin and make it more difficult to recover. Full throttle is not necessary and the deflection of the ball opposite to the spin direction is a result of the spin, not a corrective action.

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73. Vx in KIAS

Explanation

not-available-via-ai

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74. Vno in KIAS

Explanation

not-available-via-ai

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75. On a typical summer day at low level you fly into a rain shower. What risks can it pose?

Explanation

Flying into a rain shower at low level can pose several risks. Reduced visibility can lead to spatial disorientation, making it difficult for pilots to accurately perceive their position and orientation. The effect of rain on laminar airflow on the wings can severely decrease aircraft performance. Additionally, there is an increased risk of carburetor icing, which can disrupt the engine's operation. The presence of wind shear and turbulence can also make the flight more challenging and potentially dangerous.

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Engine has:
Vne
Maximum demonstrated crosswind component for the aircraft is:
Cylinders in the engine are arranged in:
Maximum baggage mass is:
Minimum fuel pressure:
In case of irregular engine RPM you should first:
Maximum continuous power is:
Total unusable fuel is:
Aircraft has:
Engine model is:
Propeller is:
Maximum cylinder head temperature is:
Maximum useful load (Standard aircraft)
P92-JS maybe operated:
Maximum power (less than 5 minutes) of the engine is:
While flying at 1500ft you notice ...
Engine is manufacrured by:
Engine can be run at maximum continuous power for:
Is case of engine fire in flight:
Colour of AVGAS 100LL is:
Minimum suction pressure is:
Load factors for the aircraft are:
Maximum take-off mass is (Standard aircraft):
Va in KIAS
Maximum suction pressure is:
Maximum value for oil pressure:
Aircraft has a:
Maximum fuel pressure:
Minimum oil temperature before take-off is:
Engine is:
Vfe in KIAS
Vy in KIAS
Best glide speed at 450 KG or with flaps extened to 15° is:
In case of engine failure at the cruise altitude:
In case of fuel pressure falling bellow 2.2 psi the initial action is
To restart the engine in flight:
Standard empty weight of the aircraft is:
Vne in KIAS
Tecnam P92 is a:
Aircraft is certified:
Vobs in KIAS
In case you unintentionally fly into cloud (enter IMC)
Vr in KIAS
Fuel capacity of each wing tank is (long range tanks):
Maximum propeller RPM (maximum time 5 minutes) is:
Maximum oil temperature for normal operating is:
Navigation lights must be operational and turned on:
You may refuel
Vlo in KIAS
Vgl at MTOM with flaps extended in KIAS
Maximum engine operating temperature is:
Best glide speed at 550 KG and flaps extened to 15° is:
Maximum oil pressure allowed is
Minimum oil pressure for normal operating is
Best glide speed at MTOM and clean configuration is:
In case of an engine failure during take-off I should first:
In case of an engine failure during ...
Following an engine failure you are trying to restart the engine by:
Minimum cylinder head temperature is:
From an altitude of 1000ft on P92 you can glide:
Engine oil cooling is based on:
Vgl at MTOM in clean configuration in KIAS
Vs1 in KIAS with 45° of bank.
Vs1 in KIAS
It is a cold winter day at Spilve. ATIS ...
Aircraft you want to take for a crosscountry flight has just returned...
Maximum continuous propeller RPM is
Aircraft preflight inspection:
Aircraft is approved for:
Aircraft minimum equiptment required:
Which one is correct regarding aircraft spinning?
Vx in KIAS
Vno in KIAS
On a typical summer day at low level you fly into a rain shower. What...
Alert!

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