2 Chapter

Who is responsible for determining that the altimeter system has been checked and found to meet 14 CFR part 91 requirements for a particular instrument flight?. Owner. Operator. Pilot in command.

Your aircraft had the static pressure system and altimeter tested and inspected on January 5, o f this year, and was found t o comply with FAA standards. These systems must be reinspected and approved for use i n controlled airspace under IFR by. January 5, next year. January 5, 2 years hence. January 31, 2 years hence.

An aircraft altimeter system test and inspection must be accomplished within. 12 calendar months. 18 calendar months. 24 calendar months.

A n aircraft operated under 1 4 CFR part 91 IF is required to have which of the following?. Radar altimeter. Dual VOR system. Gyroscopic direction indicator.

You check the flight instruments while taxiing and find that the vertical speed indicator (VSI) indicates a descent o f 100 feet per minute. In this case, you. must return to the parking area and have the instrument corrected b y an authorized instrument repairman. may take off and use 100 feet descent as the zero indication. may not take off until the instrument is corrected by either the pilot o r a mechanic.

Under what condition i s pressure altitude and density altitude the same value?. At standard temperature. When the altimeter setting is 29.92 inches Hg. When indicated, and pressure altitudes are the same value on the altimeter.

Under which condition will pressure altitude be equal to true altitude?. When the atmospheric pressure i s 29.92 inches Hg. When standard atmospheric conditions exist. When indicated altitude i s equal t o the pressure altitude.

Which condition would cause the altimeter t o indicate a lower altitude than actually flown (true altitude)?. Air temperature lower than standard. Atmospheric pressure lower than standard. Air temperature warmer than standard.

When an altimeter i s changed from 30.11 inches Hg to 29.96 inches Hg, in which direction will the indicated altitude change and b y what value?. Altimeter will indicate 15 feet lower. Altimeter will indicate 150 feet lower. Altimeter will indicate 150 feet higher.

Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92 inches Hg?. In warmer than standard air temperature. In colder than standard air temperature. When density altitude i s higher than indicated altitude.

Which o f the following defines the type o f altitude used when maintaining F L 210?. Indicated. Pressure. Calibrated.

Altimeter setting i s the value to which the scale o f the pressure altimeter i s set so the altimeter indicates. true altitude at field elevation. pressure altitude a t field elevation. pressure altitude at sea level.

(Refer t o figures 2 7 and 28.) What CAS must be used to maintain the filed TAS at the flight planned altitude if the outside air temperature i s -5°C?. 134 KCAS. 139 KCAS. 142 KCAS.

(Refer to figure 3 2 o n page 2-8.) What CAS must be used t o maintain the filed TAS at the flight planned altitude i f the outside air temperature is +8°C?. 154 KCAS. 157 KCAS. 163 KCAS.

(Refer to figure 38. What CAS must be used to maintain the filed TAS at the flight planned altitude i f the outside air temperature i s +05°C?. 129 KCAS. 133 KCAS. 139 KCAS.

(Refer to figure 44 on page 2-10.) What CAS must be used t o maintain the filed TAS at the flight planned altitude if the outside air temperature i s + 5 °C?. 147 KCAS. 150 KCAS. 154 KCAS.

(Refer t o figure 50.) What CAS must be used t o maintain the filed TAS at the flight planned altitude? (Temperature 0°C). 136 KCAS. 140 KCAS. 147 KCAS.

(Refer to figure 69 on page 2-12.) What CAS should b e used t o maintain the filed TAS i f the outside air temperature is +05°C?. 119 KCAS. 124 KCAS. 126 KCAS.

(Refer t o figure 74.) What CAS should be used to maintain the filed TAS a t the flight planned altitude if the outside air temperature is +5°C. 129 KCAS. 133 KCAS. 139 KCAS.

How should you preflight check the altimeter prior t o an IF flight?. Set the altimeter to 29.92 inches Hg. With current temperature and the altimeter indication, determine the true altitude to compare with the field elevation. Set the altimeter first with 29.92 inches Hg and then the current altimeter setting. The change in altitude should correspond to the change i n setting. Set the altimeter t o the current altimeter setting. The indication should be within 75 feet o f the actual elevation for acceptable accuracy.

What is the procedure for setting the altimeter when assigned an IFR altitude of 18,000 feet o r higher o n a direct flight off airways?. Set the altimeter t o 29.92 inches Hg before take-off. Set the altimeter to the current altimeter setting until reaching the assigned altitude, then set to 29.92 inches Hg. Set the altimeter to the current reported setting for climbout and 29.92 inches Hg upon reaching 18,000 feet.

En route at FL 290, the altimeter i s set correctly, but not reset to the local altimeter setting of 30.57 inches Hg during descent. If the field elevation i s 650 feet and the altimeter is functioning properly, what is the approximate indication upon landing?. 715 feet. 1,300 feet. Sea level.

How can you obtain the pressure altitude on flights below 18,000 feet?. 24,000 feet. 25,000 feet. 26,000 feet.

How can you obtain the pressure altitude on flights below 18,000 feet?. Set your altimeter to 29.92 inches Hg. Use your computer t o change the indicated altitude t o pressure altitude. Contact an FSS and ask for the pressure altitude.

How can you determine the pressure altitude a t a n airport without a tower or FSS?. Set the altimeter t o 29.92 inches Hg and read the altitude indicated. Set the altimeter to the current altimeter setting of a station within 100 miles and correct this indicated altitude with local temperature. Use your computer and correct the field elevation for temperature.

Which altitude i s indicated when the altimeter is set t o 29.92 inches Hg. Density. Pressure. Standard.

if you are departing from an airport where you canno ›btain an altimeter setting, you should set you altimeter. on 29.92 inches Hg. on the current airport barometric pressure, if known. to the airport elevation.

En route at F L 290, your altimeter i s set correctly, but you fail to reset i t to the local altimeter setting of 30.26 inches H g during descent. If the field elevation i s 134 feet and your altimeter i s functioning properly, what will it indicate after landing?. 100 feet MSL. 474 feet MSL. 206 feet below MSL.

How does a pilot normally obtain the current altimeter setting during an IF flight i n Class E airspace below 18,000 feet?. The pilot should contact ARTCC at least every 100 NM and request the altimeter setting. FSS's along the route broadcast the weather information at 15 minutes past the hour. ATC periodically advises the pilot o f the proper altimeter setting.

(Refer to figure 83) Which altimeter depicts 12,000 feet?. 2. 3. 4.

(Refer to figure 84) Which altimeter depicts 8,000 feet?. 1. 2. 3.

If both the ram air input and drain hole of the pitot system are blocked, what airspeed indication can be expected?. No variation o f indicated airspeed i n level flight even if large power changes are made. Decrease o f indicated airspeed during a climb. Constant indicated airspeed during a descent.

If both the ram air input and the drain hole of the pitot system are blocked, what reaction should you observe o n the airspeed indicator when power is applied and a climb is initiated out o f severe icing conditions?. The indicated airspeed would show a continuous deceleration while climbing. The airspeed would drop to, and remain at, zero. N o change until an actual climb rate i s established then indicated airspeed will increase.

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 t o the left and the ball moves t o the right. Both the miniature aircraft and the ball will remain centered.

On the taxi check, the magnetic compass should. swing opposite to the direction o f turn when turning from north. exhibit the same number o f degrees of dip as the latitude. swing freely and indicate known headings.

Which condition during taxi is a n indication that an attitude indicator i s unreliable?. The horizon bar tilts more then 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 does the miniature aircraft o f the turn coordinator directly display?. Rate of roll and rate of turn. Angle of bank and rate of turn. Angle of bank.

What pre-takeoff 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 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 i s increased. Centrifugal force is greater than horizontal lift and the load factor is increased. Centrifugal force and horizontal lift are equal and the load factor is decreased.

What indications are displayed by the miniature air- craft o f a turn coordinator?. Rate o f roll and rate o f turn. Direct indication o f bank angle and pitch atti- tude. Indirect indication o f bank angle and pitch atti- tude.

What indication should a pilot observe if an airspeed indicator ram air input and drain hole are blocked?. The airspeed indicator will react as an altimeter. The airspeed indicator will show a decrease with an increase in altitude. No airspeed indicator change will occur during climbs or descents.

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

During normal operation o f a vacuum-driven attitude indicator, what attitude indication should you see when rolling out from a 180° skidding turn to straight- and-level coordinated flight?. A straight-and-level coordinated flight indication. A nose-high indication relative to level flight. The miniature aircraft shows a turn in the direction opposite the skid.

During normal coordinated turns, what error due t o precession should you observe when rolling out t o 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 t o the left. The miniature aircraft would show a slight descent and wings-level attitude.

What information does a Mach meter present?. The ratio of aircraft true airspeed to the speed of sound. The ratio of aircraft indicated airspeed to the speed of sound. The ratio o f aircraft equivalent airspeed, corrected for installation error, t o the speed o f sound.

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

What force causes an airplane t o turn?. Rudder pressure o r force around the vertical axis. Vertical lift component. Horizontal lift component.

What should be the indication on the magnetic compass as you roll into a standard rate turn t o the left from a n east heading in the Northern Hemisphere?. The compass will initially indicate a turn to the right. The compass will remain o n east for a short time, then gradually catch up to the magnetic heading of the aircraft. The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth.

What would b e the indication o n the VSI during entry into a 500 FPM actual descent from level flight if the static ports were iced over. The indication would be i n reverse o f the actual rate of descent (500 FPM climb. The initial indication would be a climb, then descent at a rate i n excess o f 500 FPM. The VSI pointer would remain at zero regardless o f the actual rate o f descent.

How should you preflight check the altimeter prior to an IFR flight?. Set the altimeter to the current temperature. With current temperature and the altimeter indication, determine the calibrated altitude t o compare with the field elevation. Set the altimeter first with 29.92" H g and then the current altimeter setting. The change i n alti- tude should correspond to the change i n setting. Set the altimeter to the current altimeter setting. The indication should be within 75 feet o f the actual elevation for acceptable accuracy.

Which practical test should be made on the electric gyro instruments prior to starting an engine?. Check that the electrical connections are secure on the back of the instruments. Check that the attitude o f the miniature aircraft is wings level before turning o n electrical power. Turn on the electrical power and listen for any unusual or irregular mechanical noise.

Prior to starting an engine, you should check the turn-and-slip indicator to determine if the. needle indication properly corresponds to the angle o f the wings o r 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 to the other when the aircraft i s rocked.

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 centere. The ball deflects opposite the turn, but the needle remains centered.

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

What pretakeoff check should be made o f a vacuum- driven heading indicator in preparation for an IFR flight?. After 5 minutes, set the indicator t o the magnetic heading o f the aircraft and check for proper alignment after taxi turns. After 5 minutes, check that the heading indicator card aligns itself with the magnetic heading o f the aircraft. Determine that the heading indicator does not precess more than 2 ° in 5 minutes of ground operation.

What should be the indication on the magnetic com- pass as you roll into a standard rate turn to the right from an easterly heading in the Northern Hemisphere?. The compass will initially indicate a turn t o the left. The compass will remain on east for a short time, then gradually catch up t o the magnetic heading o f the aircraft. The compass will indicate the approximate cor- rect magnetic heading if the roll into the turn i s smoot.

What should be the indication on the magnetic com- pass as you roll into a standard rate turn to the right from a south heading i n the Northern Hemisphere?. The compass will indicate a turn t o the right, but a t a faster rate than is actually occurring. The compass will initially indicate a turn to the left. The compass will remain o n south for a short time, then gradually catch up t o the magnetic heading o f the aircraft.

On what headings will the magnetic compass read most accurately during a level 360° turn, with a bank o f approximately 15°?. 135° through 225°. 90° and 270º. 180° and 0°.

What causes the northerly turning error in a magnetic compass?. Coriolis force at the mid-latitudes. Centrifugal force acting on the compass card. The magnetic dip characteristic.

What should be the indication on the magnetic com- pass when you roll into a standard rate turn to the left from a south heading in the Northern Hemisphere?. The compass will indicate a turn to the left, but at a faster rate than is actually occurring. The compass will initially indicate a turn t o the right. The compass will remain on south for a short time, then gradually catch u p t o the magnetic heading of the aircraft.

What should be the indication o n the magnetic com- pass as you roll into a standard rate turn t o the right from a westerly heading i n the Northern Hemisphere. The compass will initially show a turn i n the opposite direction, then turn to a northerly indi- cation but lagging behind the actual heading of the aircraft. The compass will remain on a westerly heading for a short time, then gradually catch up t o the actual heading of the aircraft. The compass will indicate the approximate cor- rect magnetic heading if the roll into the turn i s smooth.

What should be the indication on the magnetic com- pass as you roll into a standard rate turn t o the right from a northerly heading in the Northern Hemisphere?. The compass will indicate a turn to the right, but at a faster rate than i s actually occurring. The compass will initially indicate a turn t o the left. The compass will remain on north for a short time, then gradually catch u p to the magnetic heading o f the aircraft.

What should be the indication on the magnetic com- pass a s you roll into a standard rate turn t o the left from a west heading in the Northern Hemisphere?. The compass will initially indicate a turn to the right. The compass will remain o n west for a short time, then gradually catch up to the magnetic heading of the aircraft. The compass will indicate the approximate cor- rect magnetic heading i f the roll into the turn is smooth.

What should b e the indication on the magnetic com- pass as you roll into a standard rate turn to the left from a north heading i n the Northern Hemisphere. The compass will indicate a turn to the left, but at a faster rate than is actually occurring. The compass will initially indicate a turn to the right. The compass will remain o n north for a short time, then gradually catch up to the magnetic heading of the aircraft.

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

I f 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 head- ing of 090° to a heading o f 180°. 30 seconds. 1 minute. 1 minute 30 seconds.

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

If a 180° steep turn is made to the right and the air- craft is rolled out t o straight-and-level flight b y visual references, the attitude indicator. should immediately show straight-and-level flight. will show a slight skid and climb t o the right. may show a slight climb and turn.

One characteristic that a properly functioning gyro depends upon for operation is the. ability to resist precession 90° to any applied force. resistance to deflection o f the spinning wheel o r disc. deflecting force developed from the angular velocity o f the spinning wheel.

If a standard rate turn i s maintained, how much time would be required to turn to the right from a heading o f 090° to a heading of 270°?. 1 minute. 2 minutes. 3 minutes.

If a standard rate turn i s maintained, how much time would be required to turn t o the left from a heading o f 090° to a heading of 300°?. 30 seconds. 40 seconds. 50 seconds.

If a half-standard rate turn i s maintained, how long would it take to turn 135°. 1 minute. 1 minute 20 seconds. 1 minute 30 seconds.

If, while in level flight, it becomes necessary to use a n alternate source of static pressure vented inside the airplane, which o f the following should the pilot expect?. The gyroscopic instruments t o become inoperative. The altimeter and airspeed indicator to become inoperative. The vertical speed t o momentarily show a climb.

During flight, i f the pitot-tube becomes clogged with ice, which o f the following instruments would b e affected?. The airspeed indicator only. The airspeed indicator and the altimeter. The airspeed indicator, altimeter, and Vertical Speed Indicator.

The local altimeter setting should be used by all pilots i n a particular area, primarily to provide for. he cancellation o f altimeter error due t o nonstan- dard temperatures aloft. better vertical separation o f aircraft. more accurate terrain clearance i n mountainous areas.

At an altitude o f 6,500 feet MSL, the current altimeter setting is 30.42 inches Hg. The pressure altitude would be approximately. 7,500 feet. 6,000 feet. 6,500 feet.

The pressure altitude at a given location is indicated on the altimeter after the altimeter is set to. the field elevation. 29.92 inches Hg. the current altimeter setting.

If the outside air temperature increases during a flight at constant power and at a constant indicated altitude, the true airspeed will. decrease and true altitude will increase. increase and true altitude will decrease. increase and true altitude will increase.

If severe turbulence is encountered during your IFR flight, the airplane should be slowed to the design maneuvering speed because the. maneuverability o f the airplane will be increased. amount of excess load that can be imposed on the wing will be decreased. airplane will stall a t a lower angle o f attack, giving an increased margin o f safety.

When an aircraft i s 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. left turn. climb. descent.

The displacement o f a turn coordinator during a coordinated turn will. indicate the angle of bank. remain constant for a given bank regardless of airspeed. increase as angle of bank increases.

Altimeter setting is the value to which the scale o f the pressure altimeter is set so the altimeter indicates. pressure altitude at sea leve. true altitude at field elevation. pressure altitude at field elevation.

Pressure altitude is the altitude read on your altimeter when the altimeter is adjusted to indicate height above. sea level. the standard datum plane. ground level.

The gyroscopic heading indicator is inoperative. What is the primary bank instrument in unaccelerated straight-and-level flight?. Magnetic compass. Attitude indicator. Miniature aircraft of turn coordinator.

When airspeed is decreased in a turn, what must b e 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 o f attack. Increase the angle o f attack.

What instruments are considered supporting bank instruments during a straight, stabilized climb at a constant rate?. Attitude indicator and turn coordinator. Heading indicator and attitude indicator. Heading indicator and turn coordinator.

What instruments are primary for pitch, bank, and power, respectively, when transitioning into a constant airspeed climb from straight-and-level flight?. Attitude indicator, heading indicator, and manifold pressure gauge or tachometer. Attitude indicator for both pitch and bank; airspeed indicator for power. Vertical speed, attitude indicator, and manifold pressure or tachometer.

What is the primary bank instrument once a standard rate turn is established?. Attitude indicator. Turn coordinator. Heading indicator.

What is the correct sequence in which to use the three skills used in instrument flying?. Aircraft control, cross-check, and instrument interpretation. Intrument interpretation, cross-check, and aircraft control. Cross-check, instrument interpretation, and aircraft control.

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

A s power is increased to enter a 500 feet per minute rate of climb i n straight flight, which instruments are primary for pitch, bank, and power respectively?. Attitude indicator, heading indicator, and manifold pressure gauge o r tachometer. VSI, attitude indicator, and airspeed indicator. Airspeed indicator, attitude indicator, and manifold pressure gauge o r tachometer.

What is the primary pitch instrument during a stabilized climbing left turn at cruise climb airspeed?. Attitude indicator. VSI. Airspeed indicator.

What is the primary pitch instrument when establishing a constant altitude standard rate turn?. Altimeter. VSI. Airspeed indicator.

What is the initial primary bank instrument when establishing a level standard rate turn?. Turn coordinator. Heading indicator. Attitude indicator.

What instruments) is(are) supporting bank instrument when entering a constant airspeed climb from straight- and-level flight?. Heading indicator. Attitude indicator and turn coordinator. Turn coordinator and heading indicator.

What are the three fundamental skills involved in attitude instrument flying?. Instrument interpretation, trim application, and aircraft control. Cross-check, instrument interpretation, and air- craft control. Cross-check, emphasis, and aircraft control.

What is the primary bank instrument while transitioning from straight-and-level flight t o a standard rate turn t o the left?. Attitude indicator. Heading indicator. Turn coordinator (miniature aircraft).

What is the third fundamental skill in attitude instrument flying?. Instrument cross-check. Power control. Aircraft control.

During standard-rate turns, which instrument i s con- sidered "primary" for bank?. Heading indicator. Turn and slip indicator or turn coordinator. Attitude indicator.

What is the first fundamental skill i n attitude instrument flying?. Aircraft control. Instrument cross-check. Instrument interpretation.

As power i s reduced to change airspeed from high to low cruise i n level flight, which instruments are primary for pitch, bank, and power, respectively?. Attitude indicator, heading indicator, and manifold pressure gauge o r tachometer. Altimeter, attitude indicator, and airspeed indicator. Altimeter, heading indicator, and manifold pressure gauge or tachometer.

Which instrument provides the most pertinent information (primary) for bank control in straight-and- level flight?. Turn-and-slip indicator. Attitude indicator. Heading indicator.

Which instruments are considered primary and supporting for bank, respectively, when establishing a level standard rate turn?. Turn coordinator and attitude indicator. Attitude indicator and turn coordinator. Turn coordinator and heading indicator.

While recovering from an unusual flight attitude without the aid of the attitude indicator, approximate level pitch attitude is reached when the. airspeed and altimeter stop their movement and the VSI reverses its trend. airspeed arrives a t cruising speed, the altimeter reverses its trend, and the vertical speed stops its movement. altimeter and vertical speed reverse their trend and the airspeed stops its movement.

Which instruments, in addition to the attitude indica- tor, are pitch instruments?. Altimeter and airspeed only. Altimeter and VSI only. Altimeter, airspeed indicator, and vertical speed indicator.

Which instrument provides the most pertinent informa- tion (primary) for pitch control in straight-and-level flight?. Attitude indicator. Airspeed indicator. Altimeter.

Which instruments are considered t o be supporting instruments for pitch during change o f airspeed i n a level turn?. Airspeed indicator and VSI. Altimeter and attitude indicator. Attitude indicator and VSI.

If an airplane is in a n unusual flight attitude and the attitude indicator has exceeded its limits, which instru- ments should be relied o n t o determine pitch attitude before starting recovery?. Turn indicator and VSI. Airspeed and altimeter. VSI and airspeed t o detect approaching VSI or VMO.

Which instrument i s considered primary for power as the airspeed reaches the desired value during change of airspeed in a level turn?. Airspeed indicator. Attitude indicator. Altimeter.

Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight attitude?. -Increase pitch attitude, reduce power, and level wings. Reduce power, correct the bank attitude, and raise the nose to a level attitude. Reduce power, raise the nose t o level attitude, and correct the bank attitude.

Which instruments should be used t o make a pitch correction when you have deviated from your assigned altitude?. Altimeter and VSI. Manifold pressure gauge and VSI. Attitude indicator, altimeter, and VSI.

When airspeed i s increased in a turn, what must b e done to maintain a constant altitude?. Decrease the angle o f bank. Increase the angle o f bank and/or decrease the angle o f attack. Decrease the angle o f attack.

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

Conditions that determine the pitch attitude required to maintain level flight are. airspeed, air density, wing design, and angle of attack. flightpath, wind velocity, and angle o f attack. relative wind, pressure altitude, and vertical lift component.

Approximately what percent o f the indicated vertical speed should be used to determine the number o f feet to lead the level-off from a climb t o a specific alti- tude?. 10 percent. 20 percent. 25 percent.

To level off from a descent to a specific altitude, the pilot should lead the level-off by approximately. 10 percent o f the vertical speed. 30 percent of the vertical speed. 50 percent of the vertical speed.

Rate o f turn can be increased and radius o f turn decreased by. decreasing airspeed and shallowing the bank. decreasing airspeed and increasing the bank. increasing airspeed and increasing the bank.

The primary reason the angle o f attack must be increased, to maintain a constant altitude during a coordinated turn, i s because the. thrust is acting in a different direction, causing a reduction in airspeed and loss o f lift. vertical component o f lift has decreased as the result of the bank. use o f ailerons has increased the drag.

For maintaining level flight at constant thrust, which instrument would be the least appropriate for deter- mining the need for a pitch change?. Altimeter. VSI. Attitude indicator.

To enter a constant-airspeed descent from level-cruis- ing flight, and maintain cruising airspeed, the pilot should. first adjust the pitch attitude to a descent using the attitude indicator as a reference, then adjust the power t o maintain the cruising airspeed. first reduce power, then adjust the pitch using the attitude indicator as a reference t o establish a specific rate on the VSI. simultaneously reduce power and adjust the pitch using the attitude indicator as a reference t o maintain the cruising airspeed.

To level off a t an airspeed higher than the descent speed, the addition of power should b e made, assum- ing a 500FM rate o f descent, at approximately. 50 t o 100 feet above the desired altitude. 100 to 150 feet above the desired altitude. 150 t o 200 feet above the desired altitude.

To level off from a descent maintaining the descending airspeed, the pilot should lead the desired altitude by approximately. 20 feet. 50 feet. 60 feet.

During recoveries from unusual attitudes, level flight is attained the instant. the horizon bar on the attitude indicator is exactly overlapped with the miniature airplane. a zero rate of climb i s indicated o n the VSI. the altimeter and airspeed needles stop prior t o reversing their direction o f movement.

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 b y increasing back elevator pressure until the. attitude indicator, airspeed, and vertical speed indicate a climb. vertical speed indication reaches the predeter- mined rate o f climb. attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb.

While cruising at 190 knots, you wish t o establish a climb a t 160 knots. When entering the climb (full panel), i t would be proper to make the initial pitch change b y 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.

(Refer to figure 145.) What i s the correct sequence for recovery from the unusual attitude indicated?. Reduce power, increase back elevator pressure, and level the wings. Reduce power, level the wings, bring pitch attitude to level flight. Level the wings, raise the nose o f the aircraft t o level flight attitude, and obtain desired airspeed.

(Refer to figure 146) Identify the system that has failed and determine a corrective action to return the airplane to straight-and-level flight. Static/pitot system i s blocked; lower the nose and level the wings to level-flight attitude by use of attitude indicator. Vacuum system has failed; reduce power, roll left t o level wings, and pitchup t o reduce airspeed. Electrical system has failed; reduce power, roll left to level wings, and raise the nose to reduce airspeed.

(Refer t o figure 147) Which is the correct sequence for recovery from the unusual attitude indicated?. Level wings, add power, lower nose, descend to original attitude, and heading. Add power, lower nose, level wings, return to original attitude and heading. Stop turn by raising right wing and add power a t the same time, lower the nose, and return to original attitude and heading.

(Refer t o figure 148) What is the flight attitude? One system which transmits information t o the instruments has malfunctioned. Climbing turn to left. Climbing turn to right. Level turn t o left.

(Refer to figure 149.) What is the flight attitude? One system which transmits information to the instruments has malfunctioned. Level turn to the right. Level turn to the left. Straight-and-level flight.

(Refer to figure 150.) What is the flight attitude? One instrument has malfunctioned. Climbing turn to the right. Climbing turn to the left. Descending turn to the right.

(Refer to figure 151.) What i s the flight attitude? One instrument has malfunctioned. Climbing turn to the right. Level turn t o the right. Level turn to the left.

When must an operational check o n the aircraft VOR equipment b e accomplished when used t o operate under IFR?. Within the preceding 10 days o r 10 hours of requirement.flight time. Within the preceding 30 days or 30 hours of flight time. Within the preceding 3 0 day.

Which data must b e recorded in the aircraft log or other appropriate log by a pilot making a VOR opera- tional check for IFR operations?. VOR name o r identification, date o f check, amount of bearing error, and signature. Place o f operational check, amount of bearing error, date o f check, and signature. Date o f check, VOR name or identification, place of operational check, and amount of bearing error.

What record shall be made i n the aircraft log or other permanent record by the pilot making the VOR opera- tional check?. The date, place, bearing error, and signature. The date, frequency o f VOR o r VOT, number of flight hours since last check, and signature. The date, place, bearing eror, aircraft total time, and signature.

Which checks and inspections of flight instruments or instrument systems must be accomplished before a n aircraft can b e flown under IFR?. VOR within 3 0 days, altimeter systems within 24 calendar months, and transponder within 24 calendar months. ELT test within 30 days, altimeter systems within 12 calendar months, and transponder within 24 calendar months. VOR within 24 calendar months, transponder within 24 calendar months, and altimeter system within 12 calendar months.

When making an airborne VOR check, what is the maximum allowable tolerance between the two indicators o f a dual VOR system (units independent of each other except the antenna)?. 4 ° between the two indicated bearings o f a VOR. Plus or minus 4° when set to identical radials of a VOR. 6° between the two indicated radials of a VOR.

What minimum navigation equipment is required for IFR flight?. VOR/LOC receiver, transponder, and DME. VOR receiver and, if i n ARTS III environment, a coded transponder equipped for altitude reporting. Navigation equipment appropriate to the ground facilities t o be used.

(Refer t o figure 30, GNATS ONE o n page 10-26.) During the arc portion of the instrument departure procedure (GNATS1.MOURN), a left crosswind i s encountered. Where should the bearing pointer of a n RMI b e referenced relative to the wingtip to compensate for wind drift and maintain the 15 DME are?. Behind the right wingtip reference point. On the right wingtip reference point. Behind the left wingtip reference point.

(Refer t o figures 30 on page 10-26 and 30A.) What is your position relative to GNATS intersection and the instrument departure routing?. On departure course and past GNATS. Right of departure course and past GNATS. Left of departure course and have not passed GNATS.

(Refer to figures 27 and 30 on pages 2-6 and 10-26.) To which maximum service volume distance from the OED VORTAC should you expect to receive adequate signal coverage for navigation at the flight planned altitude?. 100 NM. 80 NM. 40 NM.

(Refer to figures 3 5 o n page 6-2 and 37) What i s your position relative to the CONNY intersection on the BUJ.BUJ3 transition?. Left o f the TXK R-272 and approaching the BUJ R-059°. Left o f the TXK R-266 and past the BUJ R-065. ght o f the TKR-270 and approaching the BUJ R-245.

(Refer to figures 42A and 4 3 o n pages 7-6 and 2-57.) What is your position relative t o CHAAR intersection? The aircraft is level at 3,000 feet MSL. Right of the localizer course approaching CHAAR intersection and approaching the glide slope. Left of the localizer course approaching CHAAR intersection and below the glide slope. Right of the localizer course, past CHAAR intersection and above the glide slop.

(Refer t o figures 4 6 and 48 o n pages 10-41 and 2-57.) What is your position relative to the 9 DME ARC and the 206° radial of the instrument departure procedure?. On the 9 DME arc and approaching R-206. Outside the 9 DME are and past R-206. de the 9 DME are and approaching R-206.

(Refer to figures 5 2 and 5 4 on pages 10-45 and 2-58.) What i s the aircraft's position relative to the HABUT Intersection? (The VOR-2 i s tuned t o 116.5.). South of the localizer and past the GVO R-163. North of the localizer and approaching the GVO R-163. South of the localizer and approaching the GVO R-163.

(Refer to figure 55 on page 6-7.) As a guide i n making range corrections, how many degrees o f relative bearing change should be used for each one half mile deviation from the desired arc?. 2° t o 3°. 5° maximum. 10° to 20°.

(Refer to figure 58.) Which indications on the VOR receivers and DME at the Easterwood Field VOR receiver checkpoint would meet the regulatory requirement for this flight? No.1 VOR TO/FROM No. 2 VOR TO/FROM DME. 097°FROM 101°FROM 3.3. 097° T O 096° TO 3.2. 277°FROM 280° FROM 3.3.

(Refer t o figures 60A and 61 on page 2-60 and 2-61.) What i s your position relative to the PLATS intersection, glide slope, and the localizer course?. Past PLATS, below the glide slope, and right o f the localizer course. Approaching PLATS, above the glide slope, and left of the localizer course. Past PLATS, above the glide slope, and right of the localizer course.

(Refer t o figure 64 on page 2-62.) The course devia- tion indicator (CDI) are centered. Which indications on the No. 1 and No. 2 VOR receivers over the Lafayette Regional Airport would meet the require- ments for the VOR receiver check? No 1. VOR • TO/FROM No 2. VOR TO/FROM. 162° T O 346° FROM. 160° FROM 162° FROM. 341° FROM 330° FROM.

(Refer t o figures 65 and 66 on pages 5-4 and 2-63.) What is your position relative to GRICE intersection?. Right o f V552 and approaching GRICE intersection. Right o f V552 and past GRICE intersection. Left of V552 and approaching GRICE intersection.

(Refer t o figure 76 on page 10-55.) Which indication would be an acceptable accuracy check of both VOR receivers when the aircraft is located on the VOR receiver checkpoint at the Helena Regional Airport?. A. B. C.

(Refer to figures 78 o n page 10-57 and 79.) What is your position relative to the VOR COP southeast bound o n V86 between the BOZEMAN and LIVINGSTON VORTACs? The No. 1 VOR is tuned to 116.1 and the No. 2 VOR is tuned to 112.2. Past the LVM R-246 and west o f the BZN R-11. Approaching the LVM R-246 and west o f the BZN R-110. Past the LVM R-246 and east o f the BZN R-110.

What is the maximum tolerance allowed for an operational VOR equipment check when using a VOT?. Plus o r minus 4°. Plus o r minus 6°. Plus o r minus 8°.

When using VOT to make a VOR receiver check, the CDI should be centered and the OBS should indicate that the aircraft i s on the. 090 radial. 180 radial. 360 radial.

How should the pilot make a VOR receiver check when the aircraft i s located on the designated check- point o n the airport surface?. Set the OBS on 180° plus o r minus 4°; the CDI should center with a FROM indication. Set the OBS on the designated radial. The CDI must center within plus or minus 4 ° o f that radial with a FROM indication. With the aircraft headed directly toward the VOR and the OBS set to 000°, the CDI should center within plus or minus 4° of that radial with a TO indication.

When the CDI needle is centered during an airborne VOR check, the omnibearing selector and the TO/FROM indicator should read. within 4 ° o f the selected radial. within 6 ° o f the selected radial. 0º TO, only if you are due south o f the VOR.

(Refer to figure 81 on page 2-66.) When checking a dual VOR system by use o f a VOT, which illustration indicates the VOR's are satisfactory?. 1. 2. 4.

While airborne, what is the maximum permissible variation between the two indicated bearings when checking one VOR system against the other?. Plus o r minus 4 ° when set to identical radials of a VOR. 4° between the two indicated bearings t o a VOR. Plus o r minus 6° when set t o identical radials o f a VOR.

How should the pilot make a VOR receiver check when the aircraft is located on the designated checkpoint on the airport surface?. With the aircraft headed directly toward the VOR and the OBS set t o 000°, the CDI should center within plus or minus 4° of that radial with a TO indication. Set the OBS on the designated radial. The CDI must center within plus o r minus 4° of that radial with a FROM indication. Set the OBS o n 180° plus or minus 4°; the CDI should center with a FROM indication.

Refer to figure 82) Which i s an acceptable range o f accuracy when performing an operational check of dual VOR's using one system against the othe. 1. 2. 4.

Where can the VOT frequency for a particular airport be found?. On the IAP Chart and i n the Airport/Facility Directory. Only in the Airport/Facility Directory. In the Airport/Facility Directory and on the A/G Voice Communication Panel o f the En Route Low Altitude Chart.

Which indications are acceptable tolerances when checking both VOR receivers by use o f the VOT?. 360° T O and 003° TO, respectively. 001° FROM and 005° FROM, respectively. 176° T O and 003° FROM, respectively.

I n which publication can the VOR receiver ground checkpoints) for a particular airport be found?. Aeronautical Information Manual. E n Route Low Altitude Chart. Airport/Facility Directory.

Which is the maximum tolerance for the VOR indica- tion when the CDI is centered and the aircraft i s directly over the airborne checkpoint?. Plus or minus 6° of the designated radial. Plus 6° o r minus 4° o f the designated radial. Plus or minus 4 ° of the designated radial.

When making a n airborne VOR check, what i s the maximum allowable tolerance between the two indica- tors of a dual VOR system (units independent o f each other except the antenna). 4° between the two indicated radials o f a VOR. Plus or minus 4° when set t o identical radials of a VOR. 6º between the two indicated radials of a VOR.

Which distance i s displayed b y the DME indicator?. Slant range distance i n NM. Slant range distance i n SM. Line-of-sight direct distance from aircraft to VORTAC in SM.

Where does the DME indicator have the greatest error between ground distance to the VORTAC and dis- played distance?. High altitudes far from the VORTAC. High altitudes close t o the VORTAC. Low altitudes far from the VORTAC.

For operations off established airways at 17,000 feet MSL i n the contiguous U.S., (H) Class VORTAC facilities used t o define a direct route of flight should be n o farther apart than. 75 NM. 100 NM. 200 NM.

What indication should a pilot receive when a VOR station is undergoing maintenance and may be considered unreliable?. No coded identification, but possible navigation indications. Coded identification, but no navigation indications. A voice recording on the VOR frequency announcing that the VOR is out of service for maintenance.

A particular VOR station is undergoing routine maintenance. This is evidenced by. removal of the navigational feature. broadcasting a maintenance alert signal on the voice channel. removal o f the identification feature.

What i s the meaning o f a single coded identification received only once approximately every 3 0 seconds from a VORTAC?. The VOR and DME components are operative. VOR and DME components are both operative, but voice identification i s out o f service. The DME component is operative and the VOR component is inoperative.

Which DME indication should you receive when you are directly over a VORTAC site at approximately 6,000 feet AGL?. 0. 1. 1.3.

Which o f the following is required equipment for operating a n aircraft within Class B airspace?. A 4096 code transponder with automatic pres- sure altitude reporting equipment. A VOR receiver with DME. A 4096 code transponder.

A s a rule o f thumb, t o minimize DME slant range error, how far from the facility should you be t o consider the reading as accurate?. Two miles or more for each 1,000 feet of altitude above the facility. One or more miles for each 1,000 feet of altitude above the facility. No specific distance is specified since the reception i s line-of-sight.

A s a rule o f thumb, t o minimize DME slant range error, how far from the facility should you b e t o consider the reading as accurat. Two miles o r more for each 1,000 feet of altitude above the facility. One o r more miles for each 1,000 feet o f altitude above the facility. No specific distance is specified since the reception is line-of-sight.

(Refer to figure 8 7 o n page 5-8 and figure 88.) What is your position with reference to FALSE intersection (V222) if your VOR receivers indicate as shown?. South of V222 and east o f FALSE intersection. North o f V222 and east o f FALSE intersection. South o f V222 and west of FALSE intersection.

(Refer t o figures 89 and 90 o n pages 5-9, and 2-71.) What i s your relationship to the airway while en route from BCE VORTAC to HVE VORTAC on V8?. Left o f course o n V8. Left o f course on V382. Right o f course o n V8.

What angular deviation from a VOR course centerline is represented by a full-scale deflection o f the CDI?. 4º. 5º. 10º.

When using VOR for navigation, which o f the following should be considered as station passage?. The first movement o f the CDI as the airplane enters the zone of confusion. The moment the TO-FROM indicator becomes blan. The first positive, complete reversal o f the TO-FROM indicator.

Which of the following should b e considered as sta- tion passage when using VOR?. The first flickering of the TO-FROM indicator and CDI a s the station is approached. The first full-scale deflection o f the CDI. The first complete reversal o f the TO-FROM indicator.

When checking the sensitivity o f a VOR receiver, the number of degrees in course change as the OBS is rotated t o move the CDI from center t o the last dot on either side should be between. 5 ° and 6°. 8° and 10°. 10° and 12°.

A VOR receiver with normal five-dot course sensitivity shows a three-dot deflection a t 3 0 N M from the station. The aircraft would be displaced approximately how far from the course centerline?. 2 NM. 3 NM. 5 NM.

An aircraft which is located 30 miles from a VOR station and shows a 1/2 scale deflection on the CDI would be how far from the selected course centerline?. 1 1/2 miles. 2 1/2 miles. 3 1/2 miles.

What angular deviation from a VOR course centerline is represented by a 1/2 scale deflection of the CDI?. 2º. 4º. 5º.

After passing a VORTAC, the CDI shows 1/2 scale deflection t o the right. What is indicated if the deflection remains constant for a period of time?. The airplane is getting closer to the radial. The OBS i s erroneously set o n the reciprocal headin. The airplane i s flying away from the radial.

(Refer to figure 95 on page 2-74.) What is the lateral displacement o f the aircraft i n NM from the radial selected on the No. 1 NAV?. 5.0 NM. 7.5 NM. 10.0 NM.

(Refer to figure 95.) On which radial is the aircraft as indicated by the No. 1 NAV?. R-175. R-165. R-345.

(Refer to figure 95.) Which OBS selection on the No.1 NAV would center the CDI and change the TO/FROM indication to a TO?. 175°. 165°. 345°.

(Refer to figure 95.) What i s the lateral displacement in degrees from the desired radial on the No.2 NAV?. 1º. 2º. 4º.

(Refer t o figure 95.) Which OBS selection on the No. 2 NAV would center the CDI?. 174°. 166°. 335°.

(Refer to figure 95) Which OBS selection o n the No. 2 NAV would center the CDI and change the TO/FROM indication to a TO?. 166º. 346º. 354º.

(Refer t o figures 98 and 9 9 on pages 2-76 and 2-77.) To which aircraft position does HSI presentation "D" correspond?. 4. 15. 17.

(Refer to figures 98 and 9 9 on pages 2-76 and 2-77.) To which aircraft position does HSI presentation "E" correspond?. 5. 6. 15.

(Refer to figures 9 8 and 99.) To which aircraft position does HSI presentation "F" correspond?. 10. 14. 16.

(Refer to figures 9 8 and 99.) To which aircraft position does HSI presentation "A" correspond?. 1. 8. 11.

(Refer to figures 98 and 99.) To which aircraft posi- tion does HSI presentation "B" correspond?. 9. 13. 19.

(Refer to figures 98 and 99.) To which aircraft posi- tion does HSI presentation "C" correspond?. 6. 7. 12.

(Refer t o figure 101) What is the magnetic bearing TO the station?. 060º. 260º. 270º.

(Refer to figure 100) Which RMI illustration indicates the aircraft t o b e flying outbound on the magnetic bearing o f 235° FROM the station? (Wind 050° at 20 knots.). 2. 3. 4.

(Refer to figure 100.) What is the magnetic bearing T O the station as indicated b y illustration 4?. 285°. 055°. 235°.

(Refer t o figure 100.) Which RMI illustration indicates the aircraft i s southwest of the station and moving closer TO the station?. 1. 2. 3.

(Refer to figure 100 on page 2-79. Which RMI illustration indicates the aircraft is located on the 055° radial of the station and heading away from the station?. 1. 2. 3.

(Refer to instruments in figure 102.) On the basis of this information, the magnetic bearing T O the station would be. 175°. 255°. 355°.

(Refer to instruments in figure 102) On the basis o f this information, the magnetic bearing FROM the station would be. 175°. 255°. 355°.

(Refer to instruments in figure 103.) On the basis of this information, the magnetic bearing FROM the station would be. 030°. 060°. 240°.

(Refer to instruments in figure 103.) On the basis o f this information, the magnetic bearing TO the station would be. 060°. 240°. 270°.

(Refer to figure 104 on page 2-82.) If the radio magnetic indicator is tuned to a VOR, which illustration indicates the aircraft is on the 115° adial?. 1. 2. 3.

(Refer t o figure 104 on page 2-82.) I f the radio magnetic indicator is tuned t o a VOR, which illustration indicates the aircraft i s on the 335° radial?. 2. 3. 4.

(Refer to figure 104.) I f the radio magnetic indicator is tuned t o a VOR, which illustra- tion indicates the aircraft is o n the 315° radial?. 2. 3. 4.

(Refer to figure 104.) If the radio magnetic indicator is tuned to a VOR, which illustra- tion indicates the aircraft is on the 010° radial?. 1. 2. 3.

(Refer to figure 105 on page 2-84.) I f the magnetic heading shown for airplane 7 i s maintained, which ADF illustration would indicate the airplane is on the 120° magnetic bearing FROM the station?. 2. 4. 5.

(Refer t o figure 105 on page 2-84.) If the magnetic heading shown for airplane 5 is maintained, which ADF illustration would indicate the airplane i s o n the 210° magnetic bearing FROM the station?. 2. 3. 4.

(Refer to figure 105.) If the magnetic heading shown for airplane 3 is maintained, which ADF illustration would indicate the airplane i s on the 120° magnetic bearing TO the station?. 4. 5. 8.

(Refer to figure 105.) If the magnetic heading shown for airplane 1 is maintained, which ADF illustration would indicate the airplane i s on the 060° magnetic bearing T O the station?. 2. 4. 5.

(Refer to figure 105.) If the magnetic heading shown for airplane 2 is maintained, which ADF illustration would indicate the airplane is on the 255° magnetic bearing T O the station?. 2. 4. 5.

(Refer to figure 105 on page 2-84.) I f the magnetic heading shown for airplane 4 i s maintained, which ADF illustration would indicate the airplane i s on the 135° bearing TO the station?. 1. 4. 8.

(Refer to figure 105 on page 2-84.) I f the magnetic heading shown for airplane 6 i s maintained, which ADF illustration would indicate the airplane i s on the 255° magnetic bearing FROM the station?. 2. 4. 5.

(Refer t o figure 105 on page 2-84.) I f the magnetic heading shown for airplane 8 is maintained, which ADF illustration would indicate the airplane i s on the 090° magnetic bearing FROM the station?. 3. 4. 6.

(Refer to figure 105 on page 2-84.) If the magnetic heading shown for airplane 5 is maintained, which ADF illustration would indicate the airplane i s on the 240° magnetic bearing T O the station?. 2. 3. 4.

(Refer to figure 105 on page 2-84.) If the magnetic heading shown for airplane 8 i s maintained, which ADF illustration would indicate the airplane i s o n the 315° magnetic bearing T O the station?. 3. 4. 1.

(Refer to figure 106 on page 2-88.) The course selec- tor of each aircraft is set on 360 degrees. Which air- craft would have a FROM indication on the TO/FROM indicator and the CDI pointing t o left of center?. 1. 2. 3.

(Refer to figure 107) Where should the bearing point- er be located relative t o the wingtip reference to main- tain the 16 DME range i n a right-hand arc with a right crosswind component?. Behind the right wingtip reference for VOR-2. Ahead o f the right wingtip reference for VOR-2. Behind the right wingtip reference for VOR-1.

(Refer to figure 108) Where should the bearing point- er b e located relative t o the wingtip reference t o main- tain the 16 DME range i n a left-hand arc with a left crosswind component?. Ahead o f the left wingtip reference for the VOR-2. Ahead o f the right wingtip reference for the VOR-1. Behind the left wingtip reference for the VOR-2.

(Refer to figure 109 on page 2-90.) I n which general direction from the VORTAC is the aircraft located?. Northeast. Southeast. Southwest.

(Refer to figure 110 on page 2-90.) I n which direction from the VORTAC is the aircraft located?. Southwes. Northwest. Northeast.

(Refer t o figure 111 on page 2-91.) In which general direction from the VORTAC is the aircraft located?. Northeast. Southeast. Northwest.

For IFR operations off o f established airways below 18,000 feet, VOR navigational aids used to describe the "route o f flight" should be no more than. 80 NM apart. 40 NM apart. 70 NM apar.

(Refer t o figure 47 o n page 10-42.) When en route on V448 from YKM VORTAC to BTG VORTAC, what minimum navigation equipment i s required to identify ANGOO Intersection?. One VOR receiver. One VOR receiver and DME. Two VOR receivers.

When a VOR/DME i s collocated under frequency pairings and the VOR portion is inoperative, the DME identifier will repeat at an interval o f. 20 second intervals at 1020 Hz. 30 second intervals at 1350 Hz. second intervals a t 1350 Hz.

Full scale deflection of a CDI occurs when the course deviation bar or needle. deflects from left side o f the scale to right side of the scale. deflects from the center of the scale to either far side o f the scale. deflects from half scale left t o half scale right.

(Refer t o figure 128 on page 8-3.) How should a pilot determine when the DME a t Price/Carbon County Airport is inoperative?. The airborne DME will always indicate "O" mileage. The airborne DME will "search," but will not "lock on.". The airborne DME may appear normal, but there will be n o code tone.

(Refer to figure 143 on page 2-92.) The heading on a remote indicating compass is 120° and the magnetic compass indicates 110°. What action is required t o correctly align the heading indicator with the magnetic compass?. Select the free gyro mode and depress the counter-clockwise heading drive button. Select the slaved gyro mode and depress the clockwise heading drive button. Select the free gyro mode and depress the clock- wise heading drive button.

(Refer to figure 143) When the system is i n the free gyro mode, depressing the clockwise manual heading drive button will rotate the remote indicating compass card to the. right to eliminate left compass card error. right to eliminate right compass card error. left t o eliminate left compass card error.

(Refer t o figure 143.) The heading o n a remote indicat- ing compass i s 5° t o the left o f that desired. What action i s required t o move the desired heading under the heading reference?. Select the free gyro mode and depress the clockwise heading drive button. Select the slaved gyro mode and depress the clockwise heading drive button. Select the free gyro mode and depress the counter-clockwise heading drive button.

During IF operation using an approved GPS system for navigation,. no other navigation system is required. active monitoring o f an alternate navigation system i s always required. the aircraft must have an approved and opera- tional alternate navigation system appropriate for the route.