Chapter 2 - Principles of Instrument Flight ABC
What does the miniature aircraft of the turn coordinator directly display? A - Rate of roll and rate of turn B - Angle of bank and rate of turn C - Angle of bank
A - Rate of roll and rate of turn
Which condition would cause the altimeter to indicate a lower altitude than actually flown (true altitude)? A - Air temperature lower than standard B - Atmospheric pressure lower than standard C - Air temperature warmer than standard
C - Air temperature warmer than standard
If a 180 degree steep turn is made to the right and the aircraft is rolled out to straight and level flight by visual references, the attitude indicator A - should immediately show straight and level flight B - will show a slight skid and climb to the right C - may show a slight climb and turn
C - may show a slight climb and turn
If a standard rate turn is maintained, how long would it take to turn 180°? A - 1 minute B - 2 minutes C - 3 minutes
A - 1 minute
If a standard rate turn is maintained, how much time would be required to turn to the left from a heading of 090° to a heading of 270°? A - 1 minute B - 2 minutes C - 3 minutes
A - 1 minute
(Figure 144) Which illustration indicates a coordinated turn? A - 3 B - 1 C - 2
A - 3
What pretakeoff check should be made of a vacuum-driven heading indicator in preparation for an IFR flight? A - After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns B - After 5 minutes, checks that the heading indicator card aligns itself with the magnetic heading of the aircraft C - Determine that the heading indicator does not precess more than 2 degrees in 5 minutes of ground operation
A - After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns
Under what condition is pressure altitude and density altitude the same value? A - At standard temperature B - When the altimeter setting is 29.92 in. Hg C - When indicated and pressure altitudes are the same value on the altimeter
A - At standard temperature
When airspeed is decreased in a turn, what must be done to maintain level flight? A - Decrease the angle of bank and/or increase the angle of attack B - Increase the angle of bank and/or decrease the angle of attack C - Increase the angle of attack
A - Decrease the angle of bank and/or increase the angle of attack
(Figure 144) What changes in control displacement should be made so that turn-and-slip indicator #2 would display a coordinated standard-rate turn? A - Increase left rudder and increase rate of turn B - Increase left rudder and decrease rate of turn C - Decrease left rudder and decrease angle of bank
A - Increase left rudder and increase rate of turn
(Figure 144) What change in control displacement should be made so that turn-and-slip indicator #1 would display a coordinated standard-rate turn? A - Increase right rudder and increase rate of turn B - Decrease right rudder and increase angle of bank C - Increase right rudder and decrease rate of turn
A - Increase right rudder and increase rate of turn
What indication is presented by the miniature aircraft of the turn coordinator? A - Indirect indication of the bank attitude B - Direct indication of the bank attitude and the quality of the turn C - Quality of the turn
A - Indirect indication of the bank attitude
What indications are displayed by the miniature aircraft of a turn coordinator? A - Rate of roll and rate of turn B - Direct indication of bank angle and pitch attitude C - Indirect indication of bank angle and pitch attitude
A - Rate of roll and rate of turn
How can you determine the pressure altitude at an airport without a tower? A - Set the altimeter to 29.92 in. Hg and read the altitude indicated B - Set the altimeter to the current altimeter setting of a station within 100 miles and correct this indicated altitude with local temperature C - Use your computer and correct the field elevation for temperature
A - Set the altimeter to 29.92 in. Hg and read the altitude indicated
During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be affected? A - The airspeed indicator B - The airspeed indicator and the altimeter C - The airspeed indicator, altimeter, and vertical speed indicator
A - The airspeed indicator
What information is typically provided by the trend vector on the HSI of the PFD? A - The end of the trend vector shows what the airplane's heading will be in six seconds if the turn continues at the same rate B - The trend vector shows the bank angle necessary for a standard-rate turn C - The end of the trend vector shows what the airplane's heading will be in 1 minute if the airplane is turning at a standard rate
A - The end of the trend vector shows what the airplane's heading will be in six seconds if the turn continues at the same rate
Which condition during taxi is an indication that an attitude indicator is unreliable? A - The horizon bar tilts more than 5 degrees while making taxi turns B - The horizon bar vibrates during warmup C - The horizon bar does not align itself with the miniature airplane after warmup
A - The horizon bar tilts more than 5 degrees while making taxi turns
What information does a Mach meter present? A - The ratio of aircraft true airspeed to the speed of sound B - The ratio of aircraft indicated airspeed to the speed of sound C - The ratio of aircraft equivalent airspeed, corrected for installation error, to the speed of sound
A - The ratio of aircraft true airspeed to the speed of sound
Aircraft being operated under IFR are required to have, in addition to the equipment required for VFR and night, at least A - a slip skid indicator B - dual VOR receivers C - distance measuring equipment
A - a slip skid indicator
The ADC displays readings for the A - airspeed indicator, altimeter, and VSI B - Attitude relative to the horizon and heading C - airspeed indicator, attitude indicator, and altimeter
A - airspeed indicator, altimeter, and VSI
Conditions that determine the pitch attitude required to maintain level flight are A - airspeed, air density, wing design, and angle of attack B - flight path, wind velocity, and angle of attack C - relative wind, pressure altitude, and vertical lift component
A - airspeed, air density, wing design, and angle of attack
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 A - attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb B - attitude indicator, airspeed, and vertical speed indicate a climb C - airspeed indication reaches 160 knots
A - attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb
When the aircraft accelerates, the attitude indicator may precess and incorrectly indicate a A - climb B - descent C - right turn
A - climb
If both the ram air input and drain hole of the pitot system become blocked, the indicated airspeed will A - increase during a climb B - decrease during a climb C - remain constant regardless of altitude change
A - increase during a climb
If the pitot tube ram air pressure hole and drain hole become obstructed, the airspeed indicator will operate A - like an altimeter as the aircraft climbs and descends B - like a very sluggish airspeed indicator lagging all changes by minutes C - normally due to the static port pressure changes
A - like an altimeter as the aircraft climbs and descends
Below 18,000 feet pressure altitude may be obtained by A - setting the altimeter to 29.92 in. Hg B - setting the altimeter to the local altimeter setting C - requesting the current pressure altitude for the area
A - setting the altimeter to 29.92 in. Hg
The rate of turn at any airspeed is dependent upon A - the horizontal lift component B - centrifugal force C - the vertical lift component
A - the horizontal lift component
Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates A - true altitude at field elevation B - pressure altitude at field elevation C - pressure altitude at sea level
A - true altitude at field elevation
(Figure 144) Which illustration indicates a skidding turn? A - 2 B - 1 C - 3
B - 1
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°? A - 30 minutes B - 1 minute C - 1 minute 30 seconds
B - 1 minute
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? A - 24,000 feet B - 25,000 feet C - 26,000 feet
B - 25,000 feet
The pressure altitude at a given location is indicated on the altimeter after the altimeter is set to A - the field elevation B - 29.92 in. Hg C - the current altimeter setting
B - 29.92 in. Hg
At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42" Hg. The pressure altitude would be approximately A - 7,500 feet B - 6,000 feet C - 6,500 feet
B - 6,000 feet
On what headings will the magnetic compass read most accurately during a level 360° turn, with a bank of approximately 15°? A - 135 degrees through 225 degrees B - 90 degrees through 270 degrees C - 180 degrees and 0 degrees
B - 90 degrees through 270 degrees
If the AHRS or ADC detects a problem with the integrity of sensor information, what occurs? A - The system reverts to revisionary mode and PFD information is displayed on the MFD B - A red X is placed over the display of the affected instrument C - An alert message appears and you must determine the affected instrument(s) by comparing the indications of all instruments
B - A red X is placed over the display of the affected instrument
When an altimeter is changed from 30.11 inches Hg to 29.96 inches Hg, in which direction will the indicated altitude change and by what value? A - Altimeter will indicate 15 feet lower B - Altimeter will indicate 150 feet lower C - Altimeter will indicate 150 feet higher
B - Altimeter will indicate 150 feet lower
During a skidding turn to the right, what is the relationship between the component of lift, centrifugal force, and load factor? A - Centrifugal force is less than horizontal lift and the load factor is increased B - Centrifugal force is greater than horizontal lift and the load factor is increased C - Centrifugal force and horizontal lift are equal and the load factor is decreased
B - Centrifugal force is greater than horizontal lift and the load factor is increased
What are the three fundamental skills involved in attitude instrument flying? A - Instrument interpretation, trim application, and aircraft control B - Cross-check, instrument interpretation, and aircraft control C - Cross-check, emphasis, and aircraft control
B - Cross-check, instrument interpretation, and aircraft control
What is the relationship between centrifugal force and the horizontal lift component in a coordinated turn? A - Horizontal lift exceeds centrifugal force B - Horizontal lift and centrifugal force are equal C - Centrifugal force exceeds horizontal lift
B - Horizontal lift and centrifugal force are equal
Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92 in. Hg? A - In warmer than standard air temperature B - In colder than standard air temperature C - When density altitude is higher than indicated altitude
B - In colder than standard air temperature
When airspeed is increased in a turn, what must be done to maintain a constant altitude? A - Decrease the angle of bank B - Increase the angle of bank, and/or decrease the angle of attack C - Decrease the angle of attack
B - Increase the angle of bank, and/or decrease the angle of attack
What is the first fundamental skill in attitude instrument flying? A - Aircraft control B - Instrument cross-check C - Instrument interpretation
B - Instrument cross-check
Which altitude is indicated when the altimeter is set to 29.92 in. Hg? A - Density B - Pressure C - Standard
B - Pressure
Which of the following defines the type of altitude used when maintaining FL210? A - Indicated B - Pressure C - Calibrated
B - Pressure
What is the function of the Air Data Computer (ADC) for the PFD of an electronic flight display? A - The ADC determines the readings for the airspeed indicator, attitude indicator, and altimeter B - The ADC determines the readings for the airspeed indicator, altimeter, and vertical speed indicator C - The ADC monitors all PFD instruments to compare the data from different inputs and check information integrity
B - The ADC determines the readings for the airspeed indicator, altimeter, and vertical speed indicator
If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following variations in instrument indications should you expect? A - The altimeter will read lower than normal, airspeed lower than normal, and the VSI will momentarily show a descent B - The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb C - The altimeter will read lower than normal, airspeed greater than normal, and the VSI will momentarily show a climb and then a descent
B - The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a south heading in the Northern Hemisphere? A - The compass will initially indicate a turn to the right B - The compass will indicate a turn to the left, but at a faster rate than is actually occurring C - The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft
B - The compass will indicate a turn to the left, but at a faster rate than is actually occurring
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere? A - The compass will initially indicate a turn to the left B - The compass will indicate a turn to the right, but at a faster rate than is actually occurring C - The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft
B - The compass will indicate a turn to the right, but at a faster rate than is actually occurring
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a northerly heading in the Northern Hemisphere? A - The compass will remain on north for a short time, then gradually catch up to the magnetic heading of the aircraft B - The compass will initially indicate a turn to the left C - The compass will indicate a turn to the right, but at a faster rate than is actually occurring
B - The compass will initially indicate a turn to the left
What indication should be observed on a turn coordinator during a right turn while taxiing? A - The miniature aircraft will show a turn to the left and the ball remains centered B - The miniature aircraft will show a turn to the right and the ball moves to the left C - Both the miniature aircraft and the ball will remain centered
B - The miniature aircraft will show a turn to the right and the ball moves to the left
Under which condition will pressure altitude be equal to true altitude? A - When the atmospheric pressure is 29.92 in Hg B - When standard atmospheric conditions exist C - When indicated altitude is equal to the pressure altitude
B - When standard atmospheric conditions exist
During taxi, the VSI indicates a 100 FPM descent. How does this indication affect your flight? A - You may not operate under IFR until the VSI is repaired B - You may continue under IFR, using the 100 FPM descent as the "zero" indication C - You may operate under IFR, but only if the weather is VMC
B - You may continue under IFR, using the 100 FPM descent as the "zero" indication
A digital attitude indicator typically displays a A - roll scale with reference marks at 10, 25, 45, and 60 degrees B - a trapezoid slip/skid indicator located beneath the roll pointer C - turn-rate vector located on the roll scale to indicate standard-rate turns
B - a trapezoid slip/skid indicator located beneath the roll pointer
The local altimeter setting should be used by all pilots in a particular area, primarily to provide for A - the cancellation of altimeter error due to nonstandard temperature aloft B - better vertical separation of aircraft C - more accurate terrain clearance in mountainous areas
B - better vertical separation of aircraft
Rate of turn can be increased and radius of turn decreased by A - decreasing airspeed and shallowing the bank B - decreasing airspeed and increasing the bank C - increasing airspeed and increasing bank
B - decreasing airspeed and increasing the bank
Prior to starting an engine, you should check the turn-and-slip indicator to determine if the A - needle indication properly corresponds to the angle of the wings or rotors with the horizon B - needle is approximately centered and the tube is full of fluid C - ball will move freely from one end of the tube to the other when the aircraft is rocked
B - needle is approximately centered and the tube is full of fluid
One characteristic that a properly functioning gyro depends upon for operation is the A - ability to resist precession 90 degrees to any applied force B - resistance to deflection of the spinning wheel or disc C - deflecting force developed from the angular velocity of the spinning wheel
B - resistance to deflection of the spinning wheel or disc
Pressure altitude is the altitude read on your altimeter when the instrument is adjusted to indicate height above A - sea level B - the standard datum plane C - ground level
B - the standard datum plane
The primary reason the angle of attack must be increased, to maintain a constant altitude during a coordinated turn, is because the A - thrust is acting in a different direction B - vertical component of lift has decreased as the result of the bank C - use of ailerons has increased the drag
B - vertical component of lift has decreased as the result of the bank
If a half-standard rate turn is maintained, how long would it take to turn 135°? A - 1 minute B - 1 minute 20 seconds C - 1 minute 30 seconds
C - 1 minute 30 seconds
(Figure 144) Which illustration indicates a slipping turn? A - 1 B - 3 C - 2
C - 2
Enroute at FL290, your altimeter is set correctly, but you fail to reset it to the local altimeter setting of 30.26 in. Hg during descent. If the field elevation is 134 feet and your altimeter is functioning properly, what will it indicate after landing? A - 100 feet MSL B - 474 feet MSL C - 206 feet below MSL
C - 206 feet below MSL
An aircraft altimeter system test and inspection must be accomplished within A - 12 calendar months B - 18 calendar months C - 24 calendar months
C - 24 calendar months
If a half-standard rate turn is maintained, how long would it take to turn 360 degrees A - 1 minute B - 2 minutes C - 4 minutes
C - 4 minutes
If a standard rate turn is maintained, how much time would be required to turn to the left from a heading of 090° to a heading of 300°? A - 30 seconds B - 40 seconds C - 50 seconds
C - 50 seconds
Which are features that can be provided by a multifunction display (MFD)? A - A slip/skid indicator, instrument charts, and checklists B - Engine data, synthetic vision systems, and the vertical speed indicator C - A moving map, engine and system data, and communication frequencies
C - A moving map, engine and system data, and communication frequencies
A technically advanced aircraft (TAA) is defined as an airplane equipped with an electronically advanced avionics system, which includes: A - A multifunction display (MFD) with a moving map using VOR navigation to display the aircraft position B - A two-axis autopilot that contains it's own navigation and heading guidance system C - A primary flight display (PFD) with an airspeed indicator, turn coordinator, attitude indicator, heading indicator, altimeter, and vertical speed indicator
C - A primary flight display (PFD) with an airspeed indicator, turn coordinator, attitude indicator, heading indicator, altimeter, and vertical speed indicator
How does a pilot normally obtain the current altimeter setting during an IFR flight in Class E airspace below 18,000 feet? A - The pilot should contact ARTCC at least every 100 NM and request the altimeter setting B - Flight Service along the route broadcasts the weather information at 15 minutes past the hour C - ATC periodically advises the pilot of the proper altimeter setting
C - ATC periodically advises the pilot of the proper altimeter setting
What is the third fundamental skill in attitude instrument flying? A - Instrument cross-check B - Power control C - Aircraft control
C - Aircraft control
Which instruments should be used to make a pitch correction when you have deviated from your assigned altitude? A - Altimeter and VSI B - Manifold pressure gauge and VSI C - Attitude indicator, altimeter, and VSI
C - Attitude indicator, altimeter, and VSI
Which instrument indicates the quality of a turn? A - Attitude indicator B - Heading indicator or magnetic compass C - Ball of the turn coordinator
C - Ball of the turn coordinator
What is the correct sequence in which to use the three skills used in instrument flying? A - Aircraft control, cross-check, and instrument interpretation B - Instrument interpretation, cross-check, and aircraft control C - Cross-check, instrument interpretation, and aircraft control
C - Cross-check, instrument interpretation, and aircraft control
An aircraft operated under 14 CFR Part 91 IFR is required to have which of the following? A - Radar altimeter B - Dual VOR system C - Gyroscopic direction indicator
C - Gyroscopic direction indicator
What force causes an airplane to turn? A - Rudder pressure or force around the vertical axis B - Vertical lift component C - Horizontal lift component
C - Horizontal lift component
Your aircraft had the static pressure system and altimeter tested and inspected on January 5, of this year, and was found to comply with FAA standards. These systems must be reinspected and approved for use in controlled airspace under IFR by A - January 5, next year B - January 5, 2 years hence C - January 31, 2 years hence
C - January 31, 2 years hence
During a constant-bank level turn, what effect would an increase in airspeed have on the rate and radius of turn? A - Rate of turn would increase, and radius of turn would increase B - Rate of turn would decrease, and radius of turn would decrease C - Rate of turn would decrease, and radius of turn would increase
C - Rate of turn would decrease, and radius of turn would increase
Enroute at FL290, the altimeter is set correctly, but not reset to the local altimeter setting of 30.57 in. Hg during descent. If the field elevation is 650 feet and the altimeter is functioning properly, what is the approximate indication upon landing? A - 715 feet B - 1,300 feet C - Sea level
C - Sea level
How should you preflight check the altimeter prior to an IFR flight? A - Set the altimeter to 29.92 in. Hg with current temperature and the altimeter indication, determine the true altitude to compare with the field elevation B - Set the altimeter first with 29.92 in. Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting C - Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy
C - Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy
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? A - Set the altimeter to 29.92 in. Hg before takeoff B - Set the altimeter to the current altimeter setting until reaching the assigned altitude, then set to 29.92 in. Hg C - Set the altimeter to the current reported setting for climbout and 29.92 in. Hg upon reaching 18,000 feet
C - Set the altimeter to the current reported setting for climbout and 29.92 in. Hg upon reaching 18,000 feet
What would be the indication on the VSI during entry into a 500 FPM actual descent from level flight if the static ports were iced over? A - The indication would be in reverse of the actual rate of descent (500 FPM climb) B - The initial indication would be a climb, then descent at a rate in excess of 500 FPM C - The VSI pointer would remain at zero regardless of the actual rate of descent
C - The VSI pointer would remain at zero regardless of the actual rate of descent
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a westerly heading in the Northern Hemisphere? A - The compass will initially indicate a turn to the right B - The compass will remain on west for a short time, then gradually catch up to the magnetic heading of the aircraft C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from an east heading in the Northern Hemisphere? A - The compass will initially indicate a turn to the right B - The compass will remain on east for a short time, then gradually catch up to the magnetic heading of the aircraft C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a westerly heading in the Northern Hemisphere? A - The compass will remain on a westerly heading for a short time, then gradually catch up to the actual heading of the aircraft B - The compass will initially show a turn in the opposite direction, then turn to a northerly indication but lagging behind the actual heading of the aircraft C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from an easterly heading in the Northern Hemisphere? A - The compass will remain on east for a short time, then gradually catch up to the magnetic heading of the aircraft B - The compass will initially indicate a turn to the left C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
C - The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a northerly heading in the Northern Hemisphere? A - The compass will remain on north for a short time, then gradually catch up to the magnetic heading of the aircraft B - The compass will indicate a turn to the left, but at a faster rate than is actually occurring C - The compass will initially indicate a turn to the right
C - The compass will initially indicate a turn to the right
What pretakeoff check should be made of the attitude indicator in preparation for an IFR flight? A - The horizon bar does not vibrate during warmup B - The miniature airplane should erect and become stable within 5 minutes C - The horizon bar should erect and become stable within 5 minutes
C - The horizon bar should erect and become stable within 5 minutes
What causes the northerly turning error in a magnetic compass? A - Coriolis force at the mid-latitudes B - Centrifugal force acting on the compass card C - The magnetic dip characteristics
C - The magnetic dip characteristics
During normal operation of a vacuum-driven attitude indicator, what attitude indication should you see when rolling out from a 180 degree skidding turn to straight-and-level coordinated flight? A - A straight and level coordinated flight indication B - A nose high indication relative to level flight C - The miniature aircraft shows a turn in the direction opposite the skid
C - The miniature aircraft shows a turn in the direction opposite the skid
What is the function of the AHRS for the PFD of an electronic flight display? A - To provide airspeed, altitude, and vertical speed information B - To provide attitude, heading, and airspeed information C - To provide attitude, heading, rate of turn, and slip/skid information
C - To provide attitude, heading, rate of turn, and slip/skid information
Which practical test should be made on the electric gyro instruments prior to starting an engine? A - check that the electrical connections are secure on the back of the instrument B - Check that the attitude of the miniature aircraft is wings level before turning on electrical power C - Turn on the electrical power and listen for any unusual or irregular mechanical noise
C - Turn on the electrical power and listen for any unusual or irregular mechanical noise
Which is an action you should take after engaging the autopilot? A - Set the flight director command bars for the appropriate flight attitude B - Select the autopilot status page on the PFD to verify that the autopilot is receiving data from the AHRS and ADC C - Verify that the selected modes appear on the annunciator panel
C - Verify that the selected modes appear on the annunciator panel
To meet the requirements for flight under IFR, an aircraft must be equipped with certain operable instruments and equipment. One of those required is A - a radar altimeter B - a transponder with altitude reporting capability C - a clock with sweep second pointer or digital presentation
C - a clock with sweep second pointer or digital presentation
In addition to the attitude indicator, the pitch control instruments are the A - altimeter and airspeed indicator B - altimeter, turn coordinator, and VSI C - altimeter, airspeed indicator, and VSI
C - altimeter, airspeed indicator, and VSI
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 A - attitude indicator, airspeed, and vertical speed indicate a climb B - vertical speed indication reaches the predetermined rate of climb C - attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb
C - attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb
When an aircraft is decelerated, some attitude indicators will precess and incorrectly indicate a A - left turn B - climb C - descent
C - descent
As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using A - full bar width of attitude indication B - two bar width of attitude indication C - half bar width of attitude indication
C - half bar width of attitude indication
If the outside air temperature increases during a flight at constant power and at a constant indicated altitude, the true airspeed will A - decrease and true altitude will increase B - increase and true altitude will decrease C - increase and true altitude will increase
C - increase and true altitude will increase
The displacement of a turn coordinator during a coordinated turn will A - indicate the angle of bank B - remain constant for a given bank regardless of airspeed C - increase as angle of bank increases
C - increase as angle of bank increases
On the taxi check, the magnetic compass should A - swing opposite to the direction of turn when turning from north B - exhibit the same number of degrees of dip as the latitude C - swing freely and indicate known heading
C - swing freely and indicate known heading
If you are departing from an airport where you cannot obtain an altimeter setting, you should set your altimeter A - on 29.92 in. Hg B - on the current airport barometric pressure, if known C - to the airport elevation
C - to the airport elevation
