Embraer 190 - Aircraft Limitations
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Maximum Altitude For Flap Extension is ________ ft. (no numbers or comas on the answer, e.g: "50000")
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LIMITATIONS QUESTIONS MADE FROM AOM VOL. 1
GOOD LUCK!
SANTIAGO STOCKER.
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- 2.
The maximum flap extended speed for flaps 1 is _____ KIAS.
Explanation
The maximum flap extended speed for flaps 1 is 230 KIAS.Rate this question:
- 3.
The maximum flap extended seep for flaps 2 is _____ KIAS.
Explanation
The maximum flap extended speed for flaps 2 is 215 KIAS.Rate this question:
- 4.
The maximum flap extended seep for flaps 3 is _____ KIAS.
Explanation
The maximum flap extended speed for flaps 3 is 200 KIAS.Rate this question:
- 5.
The maximum flap extended seep for flaps 4 is _____ KIAS.
Explanation
The maximum flap extended speed for flaps 4 is 180 KIAS.Rate this question:
- 6.
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.Rate this question:
- 7.
The maximum flap extended seep for flaps FULL is _____ KIAS.
- 8.
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.Rate this question:
- 9.
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.Rate this question:
- 10.
Maximum APU electrical generator altitude is ______ ft.
Explanation
The maximum APU electrical generator altitude is 33,000 feet.Rate this question:
- 11.
Maximum altitude to asist engine start is ______ ft.
Explanation
The maximum altitude to assist engine start is 21,000 feet.Rate this question:
- 12.
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.Rate this question:
- 13.
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.Rate this question:
- 14.
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.Rate this question:
- 15.
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.Rate this question:
- 16.
Maximum Tire Ground Speed is _____ kt.
- 17.
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.Rate this question:
- 18.
AUTOPILOT Minimum Engagement Height is ___ ft
Explanation
The minimum engagement height for the autopilot is 400 feet.Rate this question:
- 19.
AUTOPILOT Minimum Use Height is ___ ft
Explanation
The minimum use height for the autopilot is 50 feet.Rate this question:
- 20.
The maximum flap extended seep for flaps 5 is _____ KIAS.
Explanation
The maximum flap extended speed for flaps 5 is 180 KIAS.Rate this question:
- 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.Rate this question:
- 22.
Maximum APU bleed altitude n is ______ ft.
Explanation
The maximum APU bleed altitude is 15,000 feet or 15,000 ft.Rate this question:
- 23.
Maximum rotor APU speed is _____ %.
Explanation
The maximum rotor APU speed is 108%.Rate this question:
- 24.
STARTING DUTY CYCLE LIMITS, maximum motoring time in-flight is ___ seconds.
Explanation
The maximum motoring time in-flight is 120 seconds.Rate this question:
- 25.
The Vmo above FL 100 is ____ KIAS.
- 26.
Wich is the Max. Takeoff Weight (MTOW)?
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51960 KG
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51800 KG
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44000 KG
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40900 KG
Correct Answer
A. 51800 KGExplanation
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.Rate this question:
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- 27.
The maximum landing gear extension speed is _____ KIAS.
Correct Answer
265Explanation
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.Rate this question:
- 28.
Maximum crosswind Wet Runway is _____ kt.
Correct Answer
31Explanation
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.Rate this question:
- 29.
Maximum APU continuous temperature is _____ºC.
Correct Answer
717Explanation
The maximum APU continuous temperature is 717°C.Rate this question:
- 30.
Cooling period after each starting attempt: Third Attempt _____ min OFF Third Attempt............................................................. 5 min OFF
Correct Answer
5Explanation
The cooling period after each starting attempt is 5 minutes.Rate this question:
- 31.
Maximum Continuous temperature is _____ºC.
Correct Answer
960 - 32.
Maximum Oil Temperature Continuous is _____ ºC.
Correct Answer
155Explanation
The maximum oil temperature continuous is 155 °C.Rate this question:
- 33.
Motoring Number Maximum Time Cool-Down Time Attempts 3 and 5 is ___ minutes.
Correct Answer
5Explanation
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.Rate this question:
- 34.
TAS, TAT and SAT information are only valid above ___ KIAS.
Correct Answer
60Explanation
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.Rate this question:
- 35.
Turbulence penetration airspeed below FL 100 is ______ KIAS.
Correct Answer
250Explanation
The correct answer is 250 KIAS. This means that the turbulence penetration airspeed below FL 100 is 250 knots indicated airspeed.Rate this question:
- 36.
Wich is the Max. Zero Fuel Weight (MZFW)?
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51960 KG
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51800 KG
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44000 KG
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40900 KG
Correct Answer
A. 40900 KGExplanation
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.Rate this question:
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- 37.
Maximum usable quantity per wing tank is ________ kg. is
Correct Answer
6550Explanation
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.Rate this question:
- 38.
Normal and Maximum Takeoff and Go Around Temperature is limited to ____ minutes. Temperature
Correct Answer
5 - 39.
STARTING DUTY CYCLE LIMITS, the maximum motoring time on ground is ___ seconds.
Correct Answer
90Explanation
The maximum motoring time on ground is 90 seconds.Rate this question:
- 40.
Coupled go-around height loss may be ___ ft.
Correct Answer
50Explanation
Coupled go-around height loss may be 50 ft.Rate this question:
- 41.
The LOW LEVEL indication will be announced when the fuel level is below ____ kg.
Correct Answer
400Explanation
The LOW LEVEL indication will be announced when the fuel level is below 400 kg.Rate this question:
- 42.
The Mmo is ___ M.
Correct Answer
0.82
.82Explanation
The correct answer for the missing word in the sentence "The Mmo is ___ M" is "0.82" or ".82".Rate this question:
- 43.
Turbulence penetration airspeed above FL 100 is ______ KIAS
Correct Answer
270Explanation
The correct answer is 270. This means that the turbulence penetration airspeed above FL 100 is 270 knots indicated airspeed (KIAS).Rate this question:
- 44.
Maximum crosswind Runway with Standing Water/Slush/Wet Snow/Dry Snow is _____ kt.
Correct Answer
18 - 45.
Maximum crosswind Runway with Ice (no melting) _____ kt.
Correct Answer
12Explanation
The given question is incomplete and does not provide enough information to generate a proper explanation.Rate this question:
- 46.
There ______ time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.
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Is no
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Is
Correct Answer
A. Is noExplanation
There is no time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.Rate this question:
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- 47.
REGARDING TAKEOFF THRUST. The total thrust reduction must not exceed ___% of the full takeoff thrust.
Correct Answer
25Explanation
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.Rate this question:
- 48.
Maximum Airspeed for Windshield Wiper Operation ___ KIAS
Correct Answer
253 - 49.
APU Cooling period after each starting attempt: First and Second Attempts is ____ seconds OFF
Correct Answer
60Explanation
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.Rate this question:
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Mar 22, 2023Quiz Edited by
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Jun 15, 2011Quiz Created by
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