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6-2

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del Test:
6-2

Descripción:
for study

Fecha de Creación: 2014/05/17

Categoría: Otros

Número Preguntas: 39

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When an altimeter is changed from 30.11" Hg to 29.96" Hg, in which direction will the indicated altitude change and by what value?. Altimeter will indicate 15 feet lower. Altimeter will indicate 150 feet lower. Altimeter will indicate 15 feet higher.

En route at FL290, the altimeter is set correctly, but not reset to the local altimeter setting of 30.57" Hg during descent. If the field elevation is 650 feet and the altimeter is functioning properly, what is the approximate indication upon landing?. 715 feet. 1,300 feet. Sea level.

En route at FL290, your altimeter is set correctly, but you fail to reset it to the local altimeter setting of 30.26" Hg during descent. If the field elevation is 134 feet and your altimeter is functioning properly, what will it indicate after landing?. 100 feet MSL. 474 feet MSL. 206 feet below MSL.

Which of the following defines the type of altitude used when maintaining FL210?. Indicated. Pressure. Calibrated.

What is the procedure for setting the altimeter when assigned an IFR altitude of 18,000 feet or higher on a direct flight off airways?. Set the altimeter to 29.92" Hg before takeoff. Set the altimeter to the current altimeter setting until reaching the assigned altitude, then set to 29.92" Hg. Set the altimeter to the current reported setting for climb out and 29.92" Hg upon reaching 18,000 feet.

While you are flying at FL250, you hear ATC give an altimeter setting of 28.92" Hg in your area. At what pressure altitude are you flying?. 24,000 feet. 25,000 feet. 26,000 feet.

If you are departing from an airport where you cannot obtain an altimeter setting, you should set your altimeter. On 29.92" Hg. On the current airport barometric pressure, if known. To the airport elevation.

The local altimeter setting should be used by all pilots in a particular area, primarily to provide for. The cancellation of altimeter error due to nonstandard temperatures aloft. Better vertical separation of aircraft. More accurate terrain clearance in mountainous areas.

How should you preflight check the altimeter prior to an IFR flight?. Setthealtimeterto29.92"Hg.Withcurrenttemperatureandthealtimeterindication,determinethetruealtitude to compare with the field elevation. Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting. Setthealtimetertothecurrentaltimetersetting.Theindicationshouldbewithin75feetoftheactualelevation for acceptable accuracy.

How should you preflight check the altimeter prior to an IFR flight?. Setthealtimetertothecurrenttemperature.Withcurrenttemperatureandthealtimeterindication,determine the calibrated altitude to compare with the field elevation. Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting. Setthealtimetertothecurrentaltimetersetting.Theindicationshouldbewithin75feetoftheactualelevation for acceptable accuracy.

One characteristic that a properly functioning gyro depends upon for operation is the. Ability to resist precession 9° to any applied force. Resistance to deflection of the spinning wheel or disc. Deflecting force developed from the angular velocity of the spinning wheel.

If a 180° steep turn is made to the right and the aircraft is rolled out to straight-and-level flight by visual references, the attitude indicator. Should immediately show straight-and-level flight. Will show a slight skid and climb to the right. May show a slight climb and turn.

As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using a. Full bar width on the attitude indicator. Half bar width on the attitude indicator. Two bar width on the attitude indicator.

Which condition during taxi is an indication that an attitude indicator is unreliable?. The horizon bar tilts more than 5° while making taxi turns. The horizon bar vibrates during warmup. The horizon bar does not align itself with the miniature airplane after warmup.

What pretakeoff check should be made of the attitude indicator in preparation for an IFR flight?. The horizon bar does not vibrate during warmup. The miniature airplane should erect and become stable within 5 minutes. The horizon bar should erect and become stable within 5 minutes.

During normal coordinated turns, what error due to precession should you observe when rolling out to straight-and-level flight from a 180° steep turn to the right?. A straight-and-level coordinated flight indication. The miniature aircraft would show a slight turn indication to the left. The miniature aircraft would show a slight descent and wings-level attitude.

Errors in both pitch and bank indication on an attitude indicator are usually at a maximum as the aircraft rolls out of a. 180° turn. 270° turn. 360° turn.

When an aircraft is accelerated, some attitude indicators will precess and incorrectly indicate a. Climb. Descent. Right turn.

When an aircraft is decelerated, some attitude indicators will precess and incorrectly indicate a. Lefft turn. Climb. Descent.

While cruising at 160 knots, you wish to establish a climb at 130 knots. When entering the climb (full panel), it is proper to make the initial pitch change by increasing back elevator pressure until the. Attitude indicator, airspeed, and vertical speed indicate a climb. Vertical speed indication reaches the predetermined rate of climb. Attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb.

While cruising at 190 knots, you wish to establish a climb at 160 knots. When entering the climb (full panel), it would be proper to make the initial pitch change by increasing back elevator pressure until the. Attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb. Attitude indicator, airspeed, and vertical speed indicate a climb. Airspeed indication reaches 160 knots.

Prior to starting an engine, you should check the turn – and – slip indicator to determine if the. Needle indication properly corresponds to the angle of the wings or rotors with the horizon. Needle is approximately centered and the tube is full of fluid. Ball will move freely from one end of the tube of other when the aircraft is rocked.

What indication should be observed on a turn coordinator during a left turn while taxiing?. The miniature aircraft will show a turn to the left and the ball remains centered. The miniature aircraft will show a turn to the left and the ball moves to the right. Both the miniature aircraft and the ball will remain centered.

What indications should you observe on the turn-and-slip indicator during taxi?. The ball moves freely opposite the turn, and the needle deflects in the direction of the turn. The needle deflects in the direction of the turn, but the ball remains centered. The ball deflects opposite the turn, but the needle remains centered.

What does the miniature aircraft of the turn coordinator directly display?. Rate of roll and rate of turn. Angle of bank and rate of turn. Angle of bank.

What indications are displayed by the miniature aircraft of a turn coordinator?. Rate of roll and rate of turn. Direct indication of bank angle and pitch attitude. Indirect indication of bank angle and pitch attitude.

What indication is presented by the miniature aircraft of the turn coordinator?. Indirect indication of the bank attitude. Direct indication of the bank attitude and the quality of the turn. Quality of the turn.

Which instrument indicates the quality of a turn?. Attitude indicator. Heading indicator or magnetic compass. Ball of the turn coordinator.

What force causes an airplane to turn?. Rudder pressure or force around the vertical axis. Vertical lift component. Horizontal lift component.

The rate of turn at any airspeed is dependent upon. The horizontal lift component. The vertical lift component. Centrifugal force.

When airspeed is decreased in a turn, what must be done to maintain level flight?. Decrease the angle of bank and/or increase the angle of attack. Increase the angle of bank and/or decrease the angle of attack. Increase the angle of attack.

During a skidding turn to the right, what is the relationship between the component of lift, centrifugal force, and load factor?. Centrifugal force is less than horizontal lift and the load factor is increased. Centrifugal force is grater than horizontal lift and the load factor is increased. Centrifugal force and horizontal lift are equal and the load factor is decreased.

What is the relationship between centrifugal force and the horizontal lift component in a coordinated turn?. Horizontal lift exceeds centrifugal force. Horizontal lift and centrifugal force are equal. Centrifugal force exceeds horizontal lift.

When airspeed is increased in a turn, what must be done to maintain a constant altitude?. Decrease the angle of bank. Increase the angle of bank and/or decrease the angle of attack. Decrease the angle of attack.

During standard-rate turns, which instrument is considered primary for bank?. Heading indicator. Turn and slip indicator or turn coordinator. Attitude indicator.

If a half-standard rate turn is maintained, how long would it take to turn 360°?. 1 minute. 2 minutes. 4 minutes.

If a standard rate turn is maintained, how long would it take to turn 180°?. 1 minute. 2 minutes. 3 minutes.

If a half-standard rate turn is maintained, how much time would be required to turn clockwise from a heading of 090° to a heading of 180°?. 30 seconds. 1 minute. 1 minute 3 seconds.

During a constant-bank level turn, what effect would an increase in airspeed have on the rate and radius of turn?. Rate of turn would increase, and radius of turn would increase. Rate of turn would decrease, and radius of turn would decrease. Rate of turn would decrease, and radius of turn would increase.

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