Embraer 190 - Aircraft Limitations

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

Explanation

The maximum altitude for flap extension is 20000 ft.

Submit
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About This Quiz
Embraer Quizzes & Trivia

LIMITATIONS QUESTIONS MADE FROM AOM VOL. 1
GOOD LUCK!
SANTIAGO STOCKER.

2. The maximum flap extended speed for flaps 1 is _____ KIAS.

Explanation

The maximum flap extended speed for flaps 1 is 230 KIAS.

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3. The maximum flap extended seep for flaps 3 is _____ KIAS.

Explanation

The maximum flap extended speed for flaps 3 is 200 KIAS.

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4. The maximum flap extended seep for flaps 4 is _____ KIAS.

Explanation

The maximum flap extended speed for flaps 4 is 180 KIAS.

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

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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6. The maximum flap extended seep for flaps 2 is _____ KIAS.

Explanation

The maximum flap extended speed for flaps 2 is 215 KIAS.

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7. The maximum flap extended seep for flaps FULL is _____ KIAS.

Explanation

not-available-via-ai

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8. Maximum APU operation altitude is ______ ft.

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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9. Maximum APU electrical generator altitude is ______ ft.

Explanation

The maximum APU electrical generator altitude is 33,000 feet.

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10. Maximum altitude to asist engine start is ______ ft.

Explanation

The maximum altitude to assist engine start is 21,000 feet.

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11. Maximum Engine N1 and N2 is _____ %

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.

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.

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.

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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15. Maximum Tire Ground Speed is _____ kt.

Explanation

not-available-via-ai

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16. Maximum crosswind Dry Runway is _____ kt.

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

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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18. AUTOPILOT Minimum Engagement Height is ___ ft

Explanation

The minimum engagement height for the autopilot is 400 feet.

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19. AUTOPILOT Minimum Use Height is ___ ft 

Explanation

The minimum use height for the autopilot is 50 feet.

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20. The maximum flap extended seep for flaps 5 is _____ KIAS.

Explanation

The maximum flap extended speed for flaps 5 is 180 KIAS.

Submit
21. Maximum APU start altitude is ______ ft.

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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22. Maximum APU bleed altitude n is ______ ft.

Explanation

The maximum APU bleed altitude is 15,000 feet or 15,000 ft.

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23. Maximum rotor APU speed is _____ %.

Explanation

The maximum rotor APU speed is 108%.

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24. STARTING DUTY CYCLE LIMITS, maximum motoring time in-flight is ___ seconds.

Explanation

The maximum motoring time in-flight is 120 seconds.

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25. The Vmo above FL 100 is ____ KIAS.

Explanation

not-available-via-ai

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

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.

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

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.

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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29. Maximum APU continuous temperature is _____ºC.

Explanation

The maximum APU continuous temperature is 717°C.

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

Explanation

The cooling period after each starting attempt is 5 minutes.

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31. Maximum Continuous      temperature is _____ºC.

Explanation

not-available-via-ai

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

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.

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.

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)?

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.

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

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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37. Maximum Oil Temperature Continuous is _____  ºC.

Explanation

The maximum oil temperature continuous is 155 °C.

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38. Normal and Maximum Takeoff and Go Around Temperature is limited to ____ minutes.   Temperature

Explanation

not-available-via-ai

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

Explanation

The maximum motoring time on ground is 90 seconds.

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40. Coupled go-around height loss may be ___ ft.

Explanation

Coupled go-around height loss may be 50 ft.

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

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 

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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44. Maximum crosswind Runway with Standing Water/Slush/Wet Snow/Dry Snow is _____ kt.

Explanation

not-available-via-ai

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

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. 

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.

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

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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48. Maximum Airspeed for Windshield Wiper Operation ___ KIAS

Explanation

not-available-via-ai

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

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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50. Engine maximum On Ground start temperature is _____ ºC.

Explanation

not-available-via-ai

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51. PRESSURIZATION Maximum differential pressure for Takeoff and Landing is ___ psi

Explanation

not-available-via-ai

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

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.

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.

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. 

Explanation

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

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56. The unusable quantity per tank is _____ kg.

Explanation

not-available-via-ai

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57. One pack INOP maximum altitude is  _________ .

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)?  

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.

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

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.

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.

Explanation

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

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

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.

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63. (For dry motoring duty cycles) Motoring number 2 to 5; maximum time ____ seconds with a cool down time of 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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64. The Vmo from FL 080 to FL 090 is ____ KIAS.

Explanation

not-available-via-ai

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

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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66. PRESSURIZATION Maximum differential negative pressure is ___ psi

Explanation

not-available-via-ai

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67. Minimum APU start temperature is ______ ºC

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.

Submit
68. Maximum APU start temperature is _____ºC.

Explanation

not-available-via-ai

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

Explanation

The maximum takeoff and landing tailwind component is 15 knots.

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71. PRESSURIZATION Maximum differential overpressure is ___ psi

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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72. PRESSURIZATION Maximum differential pressure is ___ psi  

Explanation

not-available-via-ai

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

Explanation

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

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

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

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 _____ %

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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77. Normal and Maximum Takeoff and Go Around temperature is _____ ºC.

Explanation

not-available-via-ai

Submit
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Maximum Altitude For Flap Extension is ________ ft. (no numbers or...
The maximum flap extended speed for flaps 1 is _____ KIAS.
The maximum flap extended seep for flaps 3 is _____ KIAS.
The maximum flap extended seep for flaps 4 is _____ KIAS.
The maximum landing gear retraction speed is _____ KIAS.
The maximum flap extended seep for flaps 2 is _____ KIAS.
The maximum flap extended seep for flaps FULL is _____ KIAS.
Maximum APU operation altitude is ______ ft.
Maximum APU electrical generator altitude is ______ ft.
Maximum altitude to asist engine start is ______ ft.
Maximum Engine N1 and N2 is _____ %
Minimum Oil Pressure is ____ psi.
The takeoff time limit is extended to ____ min with one engine...
The maximum landing gear extended and locked speed is _____ KIAS.
Maximum Tire Ground Speed is _____ kt.
Maximum crosswind Dry Runway is _____ kt.
Maximum permitted imbalance between wing tanks is ______ kg
AUTOPILOT Minimum Engagement Height is ___ ft
AUTOPILOT Minimum Use Height is ___ ft 
The maximum flap extended seep for flaps 5 is _____ KIAS.
Maximum APU start altitude is ______ ft.
Maximum APU bleed altitude n is ______ ft.
Maximum rotor APU speed is _____ %.
STARTING DUTY CYCLE LIMITS, maximum...
The Vmo above FL 100 is ____ KIAS.
Wich is the Max. Takeoff Weight (MTOW)?  
The maximum landing gear extension speed is _____ KIAS.
Maximum crosswind Wet Runway is _____ kt.
Maximum APU continuous temperature is _____ºC.
Cooling period after each starting attempt:...
Maximum Continuous      temperature is...
Motoring Number Maximum Time Cool-Down Time ...
TAS, TAT and SAT information are only valid above ___ KIAS.
Turbulence penetration airspeed below FL 100 is ______ KIAS.
Wich is the Max. Zero Fuel Weight (MZFW)?
Maximum usable quantity per wing tank is ________ kg.  is
Maximum Oil Temperature Continuous is _____  ºC.
Normal and Maximum Takeoff and Go Around Temperature is limited...
STARTING DUTY CYCLE LIMITS, the maximum motoring time on ground is ___...
Coupled go-around height loss may be ___ ft.
The LOW LEVEL indication will be announced when the fuel level is...
The Mmo is ___ M.
Turbulence penetration airspeed above FL 100 is ______ KIAS 
Maximum crosswind Runway with Standing Water/Slush/Wet Snow/Dry Snow...
Maximum crosswind Runway with Ice (no melting) _____ kt.
There ______ time limitation for operating the APU on ground or in...
REGARDING TAKEOFF THRUST....
Maximum Airspeed for Windshield Wiper Operation ___ KIAS
APU Cooling period after each starting attempt:...
Engine maximum On Ground start temperature is _____ ºC.
PRESSURIZATION ...
The Vmo up to FL 080 is ____ KIAS.
Maximum crosswind Runway with Compacted Snow is _____ kt.
(For dry motoring duty cycles) Motoring number 1; maximum...
After five sequential motorings, cycle may be repeated following a...
The unusable quantity per tank is _____ kg.
One pack INOP maximum altitude is  _________ .
Wich is the Max. Landing Weight (MLW)?  
Engine maximum In flight start temperature is _____ ºC.
Turbulence penetration airspeed above crossover altitude ______...
Minimum width for 180º turn is _____ mts.
Wich is the Max. Ramp Weight (MRW)?
(For dry motoring duty cycles) Motoring number 2 to 5; maximum...
The Vmo from FL 080 to FL 090 is ____ KIAS.
In flight, there is _______________ shutdown if EGT exceeds the...
PRESSURIZATION ...
Minimum APU start temperature is ______ ºC
Maximum APU start temperature is _____ºC.
Motoring Number Maximum Time Cool-Down Time ...
Maximum Takeoff and Landing Tailwind Component is _____ kt. ...
PRESSURIZATION ...
PRESSURIZATION ...
The maximum and minimum glideslope angles are ________________...
Due to engine compressor stall possibility, static takeoff is not...
Minimum fuel tank temperature altitude is ______ ºC
Minimum Engine N2 is _____ %
Normal and Maximum Takeoff and Go Around temperature is _____ ºC.
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