Test Multi-engine โผ 100 ข้อ By ICEBEAR BAC55

On takeoff the first power reduction normally is delayed until reaching?

• VMC.

• VA.

• VYSE.

• A safe maneuvering altitude and airspeed.

When a go-around from a final approach becomes necessary the first steps should be to?

• Increase the power accelerate to VXSE then retract the landing gear.

• Increase the power accelerate to VYSE then retract the landing gear.

• Increase the power raise the flaps to the take off setting and then retract the landing gear.

• Increase the power retract the landing gear the proceed as radar vectors.

The purpose of counterweights on propeller of multi-engine aircraft is to?

• Aid in feathering operations.

• More effectively balance a three-bladed propeller.

• Increase VMC and decrease induce drag.

• Help synchronize the propellers by stabilizing r.p.m.

A maximum zero fuel weight is established for some multi-engine airplanes to

• Decrease aft CG and provides a slight increase in performance.

• Increase the payload.

• Limit the ratio of loads between the fuselage and wings.

• Limit the landing weight so the gear is not overstressed.

In high angle of attack maneuvers the left-turning tendency of a conventional multi-engine airplane generally is more pronounced than that of a single-engine airplane because?

• Most multi-engine airplanes have three-bladed propellers.

• Gyroscopic forces are doubled with the addition of another engine and propeller.

• The more powerful engines normally utilized are displaced from the lateral axis.

• Two engine use more fuel than one so accurate power setting are important in multi-engine airplanes.

In which direction does engine torque tend to roll a conventional twin-engine airplane?

• Toward the engine with the lowest power setting.

• Toward the engine with the highest power setting.

• The same direction as engine and propeller rotation.

• The opposite direction of engine and propeller rotation.

The multi-engine absolute ceiling is point where?

• VX and VY converge.

• VMC and VSO converge.

• Rate of climb is 50 f.p.m.

• Critical altitude is reached.

What is the advantage of banking toward the operating engine during engine-out operations?

• Induce drag decreases and VMC increase.

• Turns toward the operation engine.

• The direction in which you apply the rudder to maintain your heading can help you identity the failed engine.

• This technique reduces the amount of rudder deflection required to maintain directional control.

During engine-out operations greater caution is required when?

• Climbing.

• Descending.

• Turning toward the good engine.

• Turning away from the good engine.

If an engine failure occurs at the multi-engine service ceiling the air plane will descend initially to the

• Go/no-go altitude.

• Turbocharger critical altitude.

• Single-engine service ceiling.

• Single-engine absolute ceiling.