Embraer 190 - Aircraft Limitations

1. Maximum Altitude For Flap Extension is ________ ft. (no numbers or comas on the answer, e.g: "50000")

The maximum altitude for flap extension is 20000 ft.

Explanation

The maximum altitude for flap extension is 20000 ft.

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5. The maximum landing gear retraction speed is _____ KIAS.

The maximum landing gear retraction speed is 235 KIAS. This means that the landing gear should not be retracted at speeds higher than 235 knots indicated airspeed. Retracting the landing gear at higher speeds can cause damage to the gear and the aircraft. It is important for pilots to follow this limitation to ensure the safe operation of the aircraft.

Explanation

The maximum landing gear retraction speed is 235 KIAS. This means that the landing gear should not be retracted at speeds higher than 235 knots indicated airspeed. Retracting the landing gear at higher speeds can cause damage to the gear and the aircraft. It is important for pilots to follow this limitation to ensure the safe operation of the aircraft.

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8. Maximum APU operation altitude is ______ ft.

The maximum APU operation altitude is 33,000 ft or 33.000 ft. This means that the APU, or Auxiliary Power Unit, can operate at altitudes up to 33,000 ft. The APU is a small engine located on aircraft that provides power for functions such as starting the main engines, operating electrical systems, and providing air conditioning while the aircraft is on the ground or in flight.

Explanation

The maximum APU operation altitude is 33,000 ft or 33.000 ft. This means that the APU, or Auxiliary Power Unit, can operate at altitudes up to 33,000 ft. The APU is a small engine located on aircraft that provides power for functions such as starting the main engines, operating electrical systems, and providing air conditioning while the aircraft is on the ground or in flight.

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11. Maximum Engine N1 and N2 is _____ %

The maximum Engine N1 and N2 is 100%. This means that the engines are running at their full capacity and generating maximum power.

Explanation

The maximum Engine N1 and N2 is 100%. This means that the engines are running at their full capacity and generating maximum power.

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12. Minimum Oil Pressure is ____ psi.

The minimum oil pressure is 25 psi. This means that the oil pressure should never be lower than 25 pounds per square inch. Maintaining the minimum oil pressure is crucial for proper lubrication and cooling of the engine components. If the oil pressure drops below this level, it can lead to engine damage and failure. Therefore, it is important to monitor the oil pressure regularly and take necessary actions to maintain it at or above the minimum recommended level.

Explanation

The minimum oil pressure is 25 psi. This means that the oil pressure should never be lower than 25 pounds per square inch. Maintaining the minimum oil pressure is crucial for proper lubrication and cooling of the engine components. If the oil pressure drops below this level, it can lead to engine damage and failure. Therefore, it is important to monitor the oil pressure regularly and take necessary actions to maintain it at or above the minimum recommended level.

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13. The takeoff time limit is extended to ____ min with one engine inoperative for airplanes Post-Mod. SB 190-73-0004 or equivalent factory incorporated modification.

The takeoff time limit is extended to 10 minutes with one engine inoperative for airplanes Post-Mod. SB 190-73-0004 or equivalent factory incorporated modification. This means that the airplane is allowed to continue with the takeoff procedure for up to 10 minutes even if one engine is not functioning properly. This extension is likely due to the modification made to the airplane, which improves its performance and allows for a longer takeoff time limit.

Explanation

The takeoff time limit is extended to 10 minutes with one engine inoperative for airplanes Post-Mod. SB 190-73-0004 or equivalent factory incorporated modification. This means that the airplane is allowed to continue with the takeoff procedure for up to 10 minutes even if one engine is not functioning properly. This extension is likely due to the modification made to the airplane, which improves its performance and allows for a longer takeoff time limit.

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14. The maximum landing gear extended and locked speed is _____ KIAS.

The maximum landing gear extended and locked speed is 265 KIAS. This means that the landing gear should be fully extended and locked in place before reaching a speed of 265 knots indicated airspeed. Going beyond this speed could potentially cause damage to the landing gear system.

Explanation

The maximum landing gear extended and locked speed is 265 KIAS. This means that the landing gear should be fully extended and locked in place before reaching a speed of 265 knots indicated airspeed. Going beyond this speed could potentially cause damage to the landing gear system.

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16. Maximum crosswind Dry Runway is _____ kt.

The maximum crosswind on a dry runway is 38 knots. This means that any crosswind with a speed of 38 knots or below is considered safe for landing and takeoff on a dry runway. Crosswinds can affect the stability and control of an aircraft during these maneuvers, so it is important to know the maximum allowable crosswind speed to ensure safe operations.

Explanation

The maximum crosswind on a dry runway is 38 knots. This means that any crosswind with a speed of 38 knots or below is considered safe for landing and takeoff on a dry runway. Crosswinds can affect the stability and control of an aircraft during these maneuvers, so it is important to know the maximum allowable crosswind speed to ensure safe operations.

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17. Maximum permitted imbalance between wing tanks is ______ kg

The maximum permitted imbalance between wing tanks is 360 kg. This means that there should not be more than a 360 kg difference in fuel quantity between the left and right wing tanks. This is important for maintaining the stability and balance of the aircraft during flight.

Explanation

The maximum permitted imbalance between wing tanks is 360 kg. This means that there should not be more than a 360 kg difference in fuel quantity between the left and right wing tanks. This is important for maintaining the stability and balance of the aircraft during flight.

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21. Maximum APU start altitude is ______ ft.

The maximum APU start altitude is 30,000 feet or 30,000. This means that the APU (Auxiliary Power Unit) can be started up to an altitude of 30,000 feet.

Explanation

The maximum APU start altitude is 30,000 feet or 30,000. This means that the APU (Auxiliary Power Unit) can be started up to an altitude of 30,000 feet.

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26. Wich is the Max. Takeoff Weight (MTOW)?

51960 KG

51800 KG

44000 KG

40900 KG

The correct answer is 51800 KG. This refers to the maximum takeoff weight of an aircraft, which is the maximum weight at which the aircraft is allowed to take off. It includes the weight of the aircraft, fuel, passengers, cargo, and any other necessary equipment. The MTOW is an important factor in determining the performance and capabilities of the aircraft, as it affects factors such as the required runway length and the aircraft's range and payload capacity.

Explanation

The correct answer is 51800 KG. This refers to the maximum takeoff weight of an aircraft, which is the maximum weight at which the aircraft is allowed to take off. It includes the weight of the aircraft, fuel, passengers, cargo, and any other necessary equipment. The MTOW is an important factor in determining the performance and capabilities of the aircraft, as it affects factors such as the required runway length and the aircraft's range and payload capacity.

27. The maximum landing gear extension speed is _____ KIAS.

The maximum landing gear extension speed is 265 KIAS. This means that the landing gear should not be extended at speeds higher than 265 knots indicated airspeed. Going beyond this speed could potentially damage the landing gear or compromise the safety of the aircraft during landing. It is important for pilots to adhere to this limitation to ensure the proper functioning of the landing gear system.

Explanation

The maximum landing gear extension speed is 265 KIAS. This means that the landing gear should not be extended at speeds higher than 265 knots indicated airspeed. Going beyond this speed could potentially damage the landing gear or compromise the safety of the aircraft during landing. It is important for pilots to adhere to this limitation to ensure the proper functioning of the landing gear system.

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28. Maximum crosswind Wet Runway is _____ kt.

The maximum crosswind for a wet runway is 31 knots. This means that if the wind speed exceeds 31 knots and the runway is wet, it may be unsafe for aircraft to take off or land due to the strong crosswind. Crosswinds can cause the aircraft to drift off course during takeoff or landing, making it difficult for pilots to maintain control. Therefore, it is important for pilots to be aware of the maximum crosswind limitations for different runway conditions to ensure safe operations.

Explanation

The maximum crosswind for a wet runway is 31 knots. This means that if the wind speed exceeds 31 knots and the runway is wet, it may be unsafe for aircraft to take off or land due to the strong crosswind. Crosswinds can cause the aircraft to drift off course during takeoff or landing, making it difficult for pilots to maintain control. Therefore, it is important for pilots to be aware of the maximum crosswind limitations for different runway conditions to ensure safe operations.

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30. Cooling period after each starting attempt: Third Attempt _____ min OFF Third Attempt............................................................. 5 min OFF

The cooling period after each starting attempt is 5 minutes.

Explanation

The cooling period after each starting attempt is 5 minutes.

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32. Motoring Number Maximum Time Cool-Down Time Attempts 3 and 5 is ___ minutes.

The question is asking for the maximum time for cool-down between attempts 3 and 5. The given answer, 5 minutes, suggests that it takes 5 minutes for the system to cool down between these two attempts.

Explanation

The question is asking for the maximum time for cool-down between attempts 3 and 5. The given answer, 5 minutes, suggests that it takes 5 minutes for the system to cool down between these two attempts.

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33. TAS, TAT and SAT information are only valid above ___ KIAS.

TAS (True Airspeed), TAT (Total Air Temperature), and SAT (Static Air Temperature) information are only valid above 60 KIAS (Knots Indicated Airspeed). This means that the information provided by these instruments can be trusted and accurate when the aircraft is flying at a speed greater than 60 knots indicated airspeed.

Explanation

TAS (True Airspeed), TAT (Total Air Temperature), and SAT (Static Air Temperature) information are only valid above 60 KIAS (Knots Indicated Airspeed). This means that the information provided by these instruments can be trusted and accurate when the aircraft is flying at a speed greater than 60 knots indicated airspeed.

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34. Turbulence penetration airspeed below FL 100 is ______ KIAS.

The correct answer is 250 KIAS. This means that the turbulence penetration airspeed below FL 100 is 250 knots indicated airspeed.

Explanation

The correct answer is 250 KIAS. This means that the turbulence penetration airspeed below FL 100 is 250 knots indicated airspeed.

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35. Wich is the Max. Zero Fuel Weight (MZFW)?

51960 KG

51800 KG

44000 KG

40900 KG

The Max. Zero Fuel Weight (MZFW) refers to the maximum weight that an aircraft can have, excluding the weight of the fuel on board. In this case, the correct answer is 40900 KG, which means that the aircraft can carry a maximum weight of 40900 KG without any fuel. This weight includes the weight of passengers, cargo, and other equipment on board, but does not include the weight of the fuel.

Explanation

The Max. Zero Fuel Weight (MZFW) refers to the maximum weight that an aircraft can have, excluding the weight of the fuel on board. In this case, the correct answer is 40900 KG, which means that the aircraft can carry a maximum weight of 40900 KG without any fuel. This weight includes the weight of passengers, cargo, and other equipment on board, but does not include the weight of the fuel.

36. Maximum usable quantity per wing tank is ________ kg. is

The maximum usable quantity per wing tank is 6550 kg. This means that the wing tank can hold a maximum of 6550 kg of fuel.

Explanation

The maximum usable quantity per wing tank is 6550 kg. This means that the wing tank can hold a maximum of 6550 kg of fuel.

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39. STARTING DUTY CYCLE LIMITS, the maximum motoring time on ground is ___ seconds.

The maximum motoring time on ground is 90 seconds.

Explanation

The maximum motoring time on ground is 90 seconds.

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41. The LOW LEVEL indication will be announced when the fuel level is below ____ kg.

The LOW LEVEL indication will be announced when the fuel level is below 400 kg.

Explanation

The LOW LEVEL indication will be announced when the fuel level is below 400 kg.

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42. The Mmo is ___ M.

The correct answer for the missing word in the sentence "The Mmo is ___ M" is "0.82" or ".82".

Explanation

The correct answer for the missing word in the sentence "The Mmo is ___ M" is "0.82" or ".82".

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43. Turbulence penetration airspeed above FL 100 is ______ KIAS

The correct answer is 270. This means that the turbulence penetration airspeed above FL 100 is 270 knots indicated airspeed (KIAS).

Explanation

The correct answer is 270. This means that the turbulence penetration airspeed above FL 100 is 270 knots indicated airspeed (KIAS).

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45. Maximum crosswind Runway with Ice (no melting) _____ kt.

The given question is incomplete and does not provide enough information to generate a proper explanation.

Explanation

The given question is incomplete and does not provide enough information to generate a proper explanation.

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46. There ______ time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.

Is no

Is

There is no time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.

Explanation

There is no time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.

47. REGARDING TAKEOFF THRUST. The total thrust reduction must not exceed ___% of the full takeoff thrust.

The total thrust reduction during takeoff must not exceed 25% of the full takeoff thrust. This means that the engines should not be throttled back by more than 25% of their maximum power output during the initial phase of the takeoff. This limitation ensures that there is enough power available for the aircraft to safely accelerate and climb after takeoff. If the thrust reduction exceeds 25%, it could potentially compromise the aircraft's performance and safety.

Explanation

The total thrust reduction during takeoff must not exceed 25% of the full takeoff thrust. This means that the engines should not be throttled back by more than 25% of their maximum power output during the initial phase of the takeoff. This limitation ensures that there is enough power available for the aircraft to safely accelerate and climb after takeoff. If the thrust reduction exceeds 25%, it could potentially compromise the aircraft's performance and safety.

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49. APU Cooling period after each starting attempt: First and Second Attempts is ____ seconds OFF

The APU cooling period after each starting attempt is 60 seconds off. This means that after the first and second attempts to start the APU, it will be turned off for a period of 60 seconds before another starting attempt can be made.

Explanation

The APU cooling period after each starting attempt is 60 seconds off. This means that after the first and second attempts to start the APU, it will be turned off for a period of 60 seconds before another starting attempt can be made.

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52. The Vmo up to FL 080 is ____ KIAS.

The Vmo (Maximum Operating Speed) up to FL 080 is 300 KIAS (Knots Indicated Airspeed). This means that the maximum speed at which an aircraft can safely operate below Flight Level 080 is 300 knots indicated airspeed. Going beyond this speed could exceed the structural limitations of the aircraft and pose a safety risk.

Explanation

The Vmo (Maximum Operating Speed) up to FL 080 is 300 KIAS (Knots Indicated Airspeed). This means that the maximum speed at which an aircraft can safely operate below Flight Level 080 is 300 knots indicated airspeed. Going beyond this speed could exceed the structural limitations of the aircraft and pose a safety risk.

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53. Maximum crosswind Runway with Compacted Snow is _____ kt.

The maximum crosswind for a runway with compacted snow is 20 knots. This means that pilots should not attempt to land or take off if the crosswind exceeds this limit. Crosswinds can make it difficult for pilots to maintain control of the aircraft during these critical phases of flight, so it is important to adhere to the maximum crosswind limits to ensure the safety of the aircraft and its passengers.

Explanation

The maximum crosswind for a runway with compacted snow is 20 knots. This means that pilots should not attempt to land or take off if the crosswind exceeds this limit. Crosswinds can make it difficult for pilots to maintain control of the aircraft during these critical phases of flight, so it is important to adhere to the maximum crosswind limits to ensure the safety of the aircraft and its passengers.

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54. (For dry motoring duty cycles) Motoring number 1; maximum time ____ seconds with a cool down time of 5 minutes.

This statement is describing a specific duty cycle for dry motoring. It states that during motoring number 1, the maximum time allowed is a certain number of seconds, which is not specified. However, it does mention that there should be a cool down time of 5 minutes after this maximum time is reached. The correct answer to this question is 90, as it is the missing value in the statement.

Explanation

This statement is describing a specific duty cycle for dry motoring. It states that during motoring number 1, the maximum time allowed is a certain number of seconds, which is not specified. However, it does mention that there should be a cool down time of 5 minutes after this maximum time is reached. The correct answer to this question is 90, as it is the missing value in the statement.

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55. After five sequential motorings, cycle may be repeated following a ____ minute cool-down period.

After five sequential motorings, the cycle may be repeated following a 15-minute cool-down period.

Explanation

After five sequential motorings, the cycle may be repeated following a 15-minute cool-down period.

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57. One pack INOP maximum altitude is _________ .

The correct answer is 31.000,31000. This indicates that the maximum altitude for one pack INOP is 31,000 feet.

Explanation

The correct answer is 31.000,31000. This indicates that the maximum altitude for one pack INOP is 31,000 feet.

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58. Wich is the Max. Landing Weight (MLW)?

51960 KG

51800 KG

44000 KG

40900 KG

The correct answer is 44000 KG. Max. Landing Weight (MLW) refers to the maximum weight at which an aircraft is allowed to land safely. It is an important parameter that pilots must adhere to in order to ensure the structural integrity and safety of the aircraft during landing. In this case, the MLW is 44000 KG, indicating that the aircraft should not exceed this weight when landing.

Explanation

The correct answer is 44000 KG. Max. Landing Weight (MLW) refers to the maximum weight at which an aircraft is allowed to land safely. It is an important parameter that pilots must adhere to in order to ensure the structural integrity and safety of the aircraft during landing. In this case, the MLW is 44000 KG, indicating that the aircraft should not exceed this weight when landing.

59. Engine maximum In flight start temperature is _____ ºC.

The given answer, 875°C, suggests that the maximum in-flight start temperature for the engine is 875°C. This means that the engine can safely start and operate at temperatures up to 875°C while the aircraft is in flight.

Explanation

The given answer, 875°C, suggests that the maximum in-flight start temperature for the engine is 875°C. This means that the engine can safely start and operate at temperatures up to 875°C while the aircraft is in flight.

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60. Turbulence penetration airspeed above crossover altitude ______ Mach.

The correct answer is 0.76 or .76. This means that the turbulence penetration airspeed above the crossover altitude is 0.76 Mach.

Explanation

The correct answer is 0.76 or .76. This means that the turbulence penetration airspeed above the crossover altitude is 0.76 Mach.

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61. Minimum width for 180º turn is _____ mts.

22

32

42

The minimum width for a 180° turn is 22 meters.

Explanation

The minimum width for a 180° turn is 22 meters.

62. Wich is the Max. Ramp Weight (MRW)?

51960 KG

51800 KG

44000 KG

40900 KG

The maximum ramp weight (MRW) refers to the maximum weight at which an aircraft can be safely parked or maneuvered on the ground. In this case, the correct answer is 51960 KG, indicating that this is the maximum weight that the aircraft can have while on the ground without causing any safety concerns.

Explanation

The maximum ramp weight (MRW) refers to the maximum weight at which an aircraft can be safely parked or maneuvered on the ground. In this case, the correct answer is 51960 KG, indicating that this is the maximum weight that the aircraft can have while on the ground without causing any safety concerns.

63. (For dry motoring duty cycles) Motoring number 2 to 5; maximum time ____ seconds with a cool down time of 5 minutes.

The maximum time for dry motoring duty cycles is 30 seconds, with a cool down time of 5 minutes. This means that the motor can be operated continuously for up to 30 seconds before it needs to cool down for 5 minutes.

Explanation

The maximum time for dry motoring duty cycles is 30 seconds, with a cool down time of 5 minutes. This means that the motor can be operated continuously for up to 30 seconds before it needs to cool down for 5 minutes.

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65. In flight, there is _______________ shutdown if EGT exceeds the limits.

Automatic

No automatic

In flight, there is no automatic shutdown if EGT exceeds the limits. This means that the engine will not automatically shut down if the EGT (Exhaust Gas Temperature) goes beyond the specified limits. The pilot or the flight crew will have to manually intervene and take appropriate action to address the issue.

Explanation

In flight, there is no automatic shutdown if EGT exceeds the limits. This means that the engine will not automatically shut down if the EGT (Exhaust Gas Temperature) goes beyond the specified limits. The pilot or the flight crew will have to manually intervene and take appropriate action to address the issue.

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67. Minimum APU start temperature is ______ ºC

The correct answer is -54 °C. This is the minimum APU start temperature, meaning that the APU (Auxiliary Power Unit) can safely start and operate at temperatures as low as -54 °C.

Explanation

The correct answer is -54 °C. This is the minimum APU start temperature, meaning that the APU (Auxiliary Power Unit) can safely start and operate at temperatures as low as -54 °C.

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69. Motoring Number Maximum Time Cool-Down Time Attempts 1 and 2 is ___ seconds

The given answer is 10 because it is stated that "Attempts 1 and 2 is ___ seconds" and the only number provided in the options is 10. Therefore, it can be inferred that the maximum time for attempts 1 and 2 is 10 seconds.

Explanation

The given answer is 10 because it is stated that "Attempts 1 and 2 is ___ seconds" and the only number provided in the options is 10. Therefore, it can be inferred that the maximum time for attempts 1 and 2 is 10 seconds.

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70. Maximum Takeoff and Landing Tailwind Component is _____ kt. is ________

The maximum takeoff and landing tailwind component is 15 knots.

Explanation

The maximum takeoff and landing tailwind component is 15 knots.

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71. PRESSURIZATION Maximum differential overpressure is ___ psi

The maximum differential overpressure is 8.8 psi. This means that the pressure difference between two points cannot exceed 8.8 pounds per square inch.

Explanation

The maximum differential overpressure is 8.8 psi. This means that the pressure difference between two points cannot exceed 8.8 pounds per square inch.

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73. The maximum and minimum glideslope angles are ________________ respectively.

3.25° and 2.5°

3.5° and 2.0°

The maximum and minimum glideslope angles are 3.25° and 2.5° respectively.

Explanation

The maximum and minimum glideslope angles are 3.25° and 2.5° respectively.

74. Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than _____ kt.

Static takeoff refers to taking off without rolling down the runway. Engine compressor stall is a condition where the airflow through the engine is disrupted, leading to a loss of engine power. Crosswind refers to the wind blowing perpendicular to the direction of takeoff. A crosswind component greater than 25 knots can increase the risk of engine compressor stall during a static takeoff. Therefore, it is not recommended to perform a static takeoff with a crosswind component greater than 25 knots.

Explanation

Static takeoff refers to taking off without rolling down the runway. Engine compressor stall is a condition where the airflow through the engine is disrupted, leading to a loss of engine power. Crosswind refers to the wind blowing perpendicular to the direction of takeoff. A crosswind component greater than 25 knots can increase the risk of engine compressor stall during a static takeoff. Therefore, it is not recommended to perform a static takeoff with a crosswind component greater than 25 knots.

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75. Minimum fuel tank temperature altitude is ______ ºC

The correct answer is -37. The minimum fuel tank temperature altitude is -37 degrees Celsius.

Explanation

The correct answer is -37. The minimum fuel tank temperature altitude is -37 degrees Celsius.

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76. Minimum Engine N2 is _____ %

The minimum Engine N2 is expressed as a percentage. The given answer options are 59.3 and 59. Since the question does not provide any additional information or context, it is not possible to determine the exact percentage. Therefore, both 59.3 and 59 could be considered correct answers.

Explanation

The minimum Engine N2 is expressed as a percentage. The given answer options are 59.3 and 59. Since the question does not provide any additional information or context, it is not possible to determine the exact percentage. Therefore, both 59.3 and 59 could be considered correct answers.

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