Term
| (Refer to figures 27 and 28) What CAS must be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is -5C? |
|
Definition
|
|
Term
| (Refer to figure 32) What CAS must be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is +8C? |
|
Definition
|
|
Term
| (Refer to figure 38) What CAS must be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is +05C? |
|
Definition
|
|
Term
| (Refer to figure 44) What CAS must be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is +5C? |
|
Definition
|
|
Term
| (Refer to figure 50) What CAS must be used to maintain the filed TAS at the flight planned altitude (temp 0C) |
|
Definition
|
|
Term
| (Refer to figure 69) What CAS should be used to maintain the filed TAS if the outside air temperature is +05C? |
|
Definition
|
|
Term
| (Refer to figure 74) What CAS should be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is +5C? |
|
Definition
|
|
Term
| What information does a Mach meter present? |
|
Definition
| the ratio of aircraft true airspeed to the speed of sound. |
|
|
Term
| (Refer to figure 56) What CAS should be used to obtain the filed TAS at the flight planned altitude if the outside air temperature is +5C? |
|
Definition
|
|
Term
| (Refer to figure 62) What CAS should be used to maintain the filed TAS at the flight planned altitude if the outside air temperature is +15C? |
|
Definition
|
|
Term
| Under what condition is pressure altitude and density altitude the same value? |
|
Definition
|
|
Term
| Under which condition wil pressure altitude be equal to true altitude? |
|
Definition
| When standard atmospheric conditions exist. |
|
|
Term
| Which condition would cause the altimeter to indicate a lower altitude than actually flown (true altitude)? |
|
Definition
| Air temperature warmer than standard |
|
|
Term
| Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92" Hg? |
|
Definition
| In colder than standard air temperature. |
|
|
Term
| Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates |
|
Definition
| true altitude at field elevation. |
|
|
Term
| How can you obtain the pressure altitude on flights below 18,000 ft? |
|
Definition
| Set your altimeter to 29.92" Hg |
|
|
Term
| How can you determine the pressure altitude on an airport without a tower or FSS? |
|
Definition
| Set the altimeter to 29.92" Hg and read the altitude indicated. |
|
|
Term
| Which altitude is indicated when the altimeter is set to 29.92" Hg? |
|
Definition
|
|
Term
| At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42" HG. The pressure altitude would be approximately |
|
Definition
|
|
Term
| The pressure altitude at a given location is indicated on the altimeter after the altimeter is set to |
|
Definition
|
|
Term
| If the outside air temperature increases during a flight at constant power and at a constant indicated altitude, the true airspeed will |
|
Definition
| increase and true altitude will increase. |
|
|
Term
| Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates |
|
Definition
| true altitude at field elevation. |
|
|
Term
| Pressure altitude is the altitude read on your altimeter when the instrument is adjusted to indicate height above |
|
Definition
|
|
Term
| 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? |
|
Definition
| Altimeter will indicate 150 ft lower |
|
|
Term
| En route at FL290, the altimeter is set correctly, but not rest to the local altimeter setting of 30.57" Hg during descent. If the field elevation is 650 ft and the altimeter is functioning properly, what is the approximate indication upon landing? |
|
Definition
|
|
Term
| 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 ft and your altimeter is functioning properly, what will it indicate after landing? |
|
Definition
|
|
Term
| Which of the following defines the type of altitude used when maintaining FL210? |
|
Definition
|
|
Term
| 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? |
|
Definition
| Set the altimeter to the current reported setting for climb-out and 29.92" Hg upon reaching 18,000 ft. |
|
|
Term
| 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? |
|
Definition
|
|
Term
| If you are departing from an airport where you cannot obtain an altimeter setting, you should set your altimeter |
|
Definition
|
|
Term
| How does a pilot normally obtain the current altimeter setting during an IFR flight in Class E airspace below 18,000 ft? |
|
Definition
| ATC periodically advises the pilot of the proper altimeter setting. |
|
|
Term
| The local altimeter setting should be used by all pilots in a particular area, primarly to provide for |
|
Definition
| better vertical separation of aircraft. |
|
|
Term
| How should you preflight check the altimeter prior to an IFR flight? |
|
Definition
| Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy. |
|
|
Term
| How should you preflight check the altimeter prior to an IFR flight? |
|
Definition
| Set the altimeter to the current setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy. |
|
|
Term
| (Refer to figure 83) Which altimeter depicts 12,000 ft? |
|
Definition
|
|
Term
| (Refer to figure 84) Which altimeter depicts 8,000 ft? |
|
Definition
|
|
Term
| You check the flight instruments while taxiing and find that the vertical speed indicator (VSI) indicates a descent of 100 ft per minute. In this case, you |
|
Definition
| may take off under IFR and use 100-foot descent as the zero indication. |
|
|
Term
| One characteristic that a properly functioning gyro depends upon for operation is the |
|
Definition
| resistance to deflection of the spinning wheel or disc. |
|
|
Term
| If a 180 steep turn is made to the right and the aircraft is rolled out to straight-and-level flight be visual references, the attitude indicator |
|
Definition
| may show a flight climb and turn |
|
|
Term
| As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using a |
|
Definition
| half bar width on the attitude indicator. |
|
|
Term
| Which condition during taxi is an indication that an attitude indicator is unreliable? |
|
Definition
| The horizon bar tilts more than 5 degrees while making taxi turns. |
|
|
Term
| What pretakeoff check should be made of the attitude indicator in preparation for an IFR flight? |
|
Definition
| The horizon bar should erect and become stable within 5 minutes |
|
|
Term
| During normal operation of 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? |
|
Definition
| The miniature aircraft shows a turn in the direction opposite the skid. |
|
|
Term
| 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? |
|
Definition
| The miniature aircraft would show a slight turn indication to the left. |
|
|
Term
| Errors in both pitch and bank indication on an attitude indicator are usually at a maximum as the aircraft rolls out of a |
|
Definition
|
|
Term
| When an aircraft is accelerated, some attitude indicators will precess and incorrectly indicate a |
|
Definition
|
|
Term
| When an aircraft is decelerated, some attitude indicators will precess and incorrectly indicate a |
|
Definition
|
|
Term
| 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 |
|
Definition
| attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb. |
|
|
Term
| 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 |
|
Definition
| attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb |
|
|
Term
| Which initial pitch attitude change on the attitude indicator should be made to correct altitude while at normal cruise in a helicopter? |
|
Definition
|
|
Term
| During the initial acceleration on an instrument takeoff in a helicopter, what flight attitude should be established on the attitude indicator? |
|
Definition
|
|
Term
| During a stabilized autorotation, approximately what flight attitude should be established on the attitude indicator? |
|
Definition
|
|
Term
| The primary reason the pitch attitude must be increased, to maintain a constant altitude during a coordinated turn, is because the |
|
Definition
| vertical component of lift has decreased as the result of the bank. |
|
|
Term
| Prior to starting an engine, you should check the turn-and-slip indicator to determine if the |
|
Definition
| needle is approximately centered and the tube is full of fluid. |
|
|
Term
| What indication should be observed on a turn coordinator during a left turn while taxiing? |
|
Definition
| The miniature aircraft will show a turn to the left and the ball moves to the right. |
|
|
Term
| What indications should you observe on the turn-and-slip indicator during taxi? |
|
Definition
| The ball moves freely opposite the turn, and the needle deflects in the direction of the turn. |
|
|
Term
| What indication should be observed on a turn coordinator during a right turn while taxiing? |
|
Definition
| The miniature aircraft will show a turn tot he right and the ball moves to the left. |
|
|
Term
| What does the miniature aircraft of the turn coordinator directly display? |
|
Definition
| Rate of roll and rate of turn |
|
|
Term
| What indications are displayed by the miniature aircraft of a turn coordinator? |
|
Definition
| Rate or roll and rate of turn. |
|
|
Term
| What indication is presented be the miniature aircraft of the turn coordinator? |
|
Definition
| Indirect indication of the bank attitude. |
|
|
Term
| Which instrument indicates the quality of a turn? |
|
Definition
| Ball of the turn coordinator |
|
|
Term
| What force causes the airplane to turn? |
|
Definition
| Horizontal component of lift. |
|
|
Term
| The rate of turn at any airspeed is dependent upon |
|
Definition
| the horizontal component of lift. |
|
|
Term
| When airspeed is decreased in a turn, what must be done to maintain level flight? |
|
Definition
| Decrease the angle of bank and/or increase the angle of attack |
|
|
Term
| During a skidding turn to the right, what is the relationship between the component of lift, centrifugal force, and load factor? |
|
Definition
| Centrifugal force is greater than horizontal lift and the load factor is increased. |
|
|
Term
| What is the relationship between centrifugal force and the horizontal component of lift in a coordinated turn? |
|
Definition
| Horizontal lift and centrifugal force are equal. |
|
|
Term
| When airspeed is increased in a turn, what must be done to maintain a constant altitude? |
|
Definition
| Increase the angle of bank and/or decrease the angle of attack |
|
|
Term
| During standard-rate turns, which instrument is considered "primary" for bank? |
|
Definition
| Turn and slip indicator or turn coordinator. |
|
|
Term
| If a half-standard rate turn is maintained, how long would it take to turn 360? |
|
Definition
|
|
Term
| If a standard rate turn is maintained, how long would it take to turn 180? |
|
Definition
|
|
Term
| 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? |
|
Definition
|
|
Term
| During a constant-bank level turn, what effect would an increase in airspeed have on the rate and radius of turn? |
|
Definition
| Rate of turn would decrease, and radius of turn would increase. |
|
|
Term
| If a standard rate turn is maintained, how much time would be required to turn to the right from a heading of 90 to a heading of 270? |
|
Definition
|
|
Term
| 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? |
|
Definition
|
|
Term
| If a half-stand rate turn is maintained, how long would it take to turn 135? |
|
Definition
|
|
Term
| Rate of turn can be increased and radius of turn decreased by |
|
Definition
| decreasing airspeed and increasing bank |
|
|
Term
| The primary reason the angle of attack must be increased, to maintain a constant altitude during a coordinated turn, is because the |
|
Definition
| vertical component of lift has decreased as the result of the bank. |
|
|
Term
| The displacement of a turn coordinator during a coordinated turn will |
|
Definition
| increase as angle of bank increases |
|
|
Term
| (Refer to figure 144) What changes in control displacement should be made so that "2" would result in a coordinated standard rate turn? |
|
Definition
| Increase left rudder and increase rate of turn. |
|
|
Term
| (Refer to figure 144) Which illustration indicates a coordinated turn? |
|
Definition
|
|
Term
| (Refer to figure 144) Which illustration indicates a skidding turn? |
|
Definition
|
|
Term
| (Refer to figure 144) What changes in control displacement should be made so that "1" would result in a coordinated standard rate turn? |
|
Definition
| Increase right rudder and increase rate of turn. |
|
|
Term
| (Refer to figure 144) Which illustration indicates a slipping turn? |
|
Definition
|
|
Term
| When airspeed is increased in a turn, what must be done to maintain a constant altitude? |
|
Definition
| Increase the angle of bank and/or decrease the pitch attitude. |
|
|
Term
| When airspeed is decreased in a turn, what must be done to maintain level flight? |
|
Definition
| Decrease the angle of bank and/or increase the pitch attitude. |
|
|
Term
| What force cases a helicopter to turn? |
|
Definition
| Horizontal lift component. |
|
|
Term
| What pretakeoff check should be made of a vacuum-driven heading indicator in preparation for an IFR flight? |
|
Definition
| After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns. |
|
|
Term
| On the taxi check, the magnetic compass should |
|
Definition
| swing freely and indicate known headings. |
|
|
Term
| 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? |
|
Definition
| The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. |
|
|
Term
| 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? |
|
Definition
| The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. |
|
|
Term
| 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? |
|
Definition
| The compass will indicate a turn tot he right, but at a faster rate than is actually occurring. |
|
|
Term
| On what headings will the magnetic compass read most accurately during a level 360 turn, with a bank of approximately 15? |
|
Definition
|
|
Term
| What causes the northerly turning error in a magnetic compass? |
|
Definition
| The magnetic dip characteristic. |
|
|
Term
| What should be the indication on the magnetic compass when you roll into a standard rate turn to the left from a south heading in the Northern Hemisphere? |
|
Definition
| the compass will indicate a turn to the left, but at a faster rate than is actually occurring. |
|
|
Term
| What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a west heading in the Northern Hemisphere? |
|
Definition
| The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. |
|
|
Term
| What should be the indication on the magnetic compass as you roll into a standard rate turn tot he left from a north heading in the Northern Hemisphere? |
|
Definition
| The compass will initially indicate a turn tot he right. |
|
|
Term
| (Refer to 143) The heading on a remote indicating compass is 120 and the magnetic compass indicates 110. What action is required to correctly align the heading indicator with the magnetic compass? |
|
Definition
| Select the free gyro mode and depress the clockwise heading drive button |
|
|
Term
| (Refer to figure 143) When the system is in the free gyro mode, depressing the clockwise manual heading drive button will rotate the remote indicating compass card to the |
|
Definition
| right to eliminate left compass card error. |
|
|
Term
| (Refer to figure 143) The heading on a remote indicating compass is 5 degree to the left of that desired. What action is required to move the desired heading under the heading reference? |
|
Definition
| Select the free gyro mode and depress the counter-clockwise heading drive button. |
|
|
Term
| Which practical test should be made on the electric gyro instruments prior to starting an engine? |
|
Definition
| Turn on the electrical power and listen for any unusual or irregular mechanical noise. |
|
|
Term
| If both the ram air input and drain hole of the pitot system are blocked, what airspeed indication can be expected? |
|
Definition
| No variation of indicated airspeed in level flight even if large power changes are made. |
|
|
Term
| If both the ram air input and the drain hole of the pitot system are blocked, what reaction should you observe on the airspeed indicator when power is applied and a climb is initiated out of severe icing conditions. |
|
Definition
| No change until an actual climb rate is established, then indicated airspeed will increase. |
|
|
Term
| What indication should a pilot observe if an airspeed indicator ram air input and drain hole are blocked? |
|
Definition
| The airspeed indicator will react as an altimeter. |
|
|
Term
| 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? |
|
Definition
| the VSI pointer would remain at zero regardless of the actual rate of descent. |
|
|
Term
| If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following should the pilot expect? |
|
Definition
| The vertical speed to momentarily show a climb. |
|
|
Term
| During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be affected? |
|
Definition
| The airspeed indicator only |
|
|
Term
| 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 the pilot expect? |
|
Definition
| The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb. |
|
|
Term
| (Refer to figure 146) Identify the system that has failed and determine a corrective action to return the airplane to straight-and-level flight? |
|
Definition
| Static/pitot system is blocked; lower the nose and level the wings to level-flight attitude by use of attitude indicator. |
|
|
Term
| (Refer to figure 150) What is the flight attitude? One instrument has malfunctioned. |
|
Definition
| Climbing turn to the right. |
|
|
Term
| (Refer to figure 148) What is the flight attitude? One system which transmits information to the instruments has malfunctioned. |
|
Definition
| Climbing turn to the right. |
|
|
Term
| (Refer to figure 149) What is the flight attitude? One system which transmits information to the instruments has malfunctioned. |
|
Definition
| Straight-and-level flight. |
|
|
Term
| (Refer to figure 151) What is the flight attitude? One instrument has malfunctioned. |
|
Definition
|
|
Term
| What is the correct sequence in which to use the three skills used in instrument flying? |
|
Definition
| Cross-check, instrument interpretation, and aircraft control |
|
|
Term
| What are the three fundamental skills involved in attitude instrument flying? |
|
Definition
| Cross-check, instrument interpretation, and aircraft control. |
|
|
Term
| what is the first fundamental skill i attitude instrument flying? |
|
Definition
|
|
Term
| What effect will a change in wind direction have upon maintaining a 3 degree glide slop at a constant true airspeed? |
|
Definition
| When ground speed increases, rate of descent must increase. |
|
|
Term
| The rate of descent required to stay on the ILS glide slope |
|
Definition
| must be decreased if the ground speed is decreased. |
|
|
Term
| To remain on the ILS glidepath, the rate of descent must be |
|
Definition
| increased if the ground speed is increased. |
|
|
Term
| The rate of descent on the glide slope is dependent upon |
|
Definition
|
|
Term
| The glide slope and localizer are centered, but the airspeed is too fast. What should be adjusted initially? |
|
Definition
|
|
Term
| During a precision radar or ILS approach, the rate of descent required to remain on the glide slope will |
|
Definition
| increase as the ground speed increases. |
|
|
Term
| what is the third fundamental skill in attitude instrument flying? |
|
Definition
|
|
Term
| The gyroscopic heading indicator is inoperative. What is the primary bank instrument in unaccelerated straight-and-level flight? |
|
Definition
|
|
Term
| What instruments are considered supporting bank instruments during a straight, stabilized climb at a constant rate? |
|
Definition
| Attitude indicator and turn coordinator. |
|
|
Term
| What instruments are primary for pitch, bank, and power, respectively, when transitioning into a constant airspeed climb from straight-and-level flight? |
|
Definition
| Attitude indicator, heading indicator, and manifold pressure gauge or tachometer. |
|
|
Term
| What is the primary bank instrument once a standard rate turn is established? |
|
Definition
|
|
Term
| As power is increased to enter a 500 feet per minute rate of climb in straight flight, which instruments are primary for pitch, bank, and power respectively? |
|
Definition
| Attitude indicator, heading indictor, and manifold pressure gauge or tachometer. |
|
|
Term
| What is the primary pitch instrument during a stabilized climbing left turn at cruise climb airspeed? |
|
Definition
|
|
Term
| What is the primary pitch instrument when establishing a constant altitude standard rate turn? |
|
Definition
|
|
Term
| As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using |
|
Definition
| less than a full bar width on the attitude indicator. |
|
|
Term
| What is the initial primary bank instrument when establishing a level standard rate turn? |
|
Definition
|
|
Term
| What is the primary bank instrument while transitioning from straight-and-level flight to a standard rate turn to the left? |
|
Definition
|
|
Term
| As power is reduced to change airspeed from high to low cruise in level flight, which instruments are primary for pitch, bank, and power, respectively? |
|
Definition
| Altimeter, heading indicator, and manifold pressure gauge or tachometer. |
|
|
Term
| Which instrument provides the most pertinent information (primary) for bank control in straight-and-level flight? |
|
Definition
|
|
Term
| Which instrument are considered to be supporting instruments for pitch during change of airspeed in a level turn? |
|
Definition
| Attitude indicator and VSI |
|
|
Term
| Which instrument is considered primary for power as the airspeed reaches the desired value during change of airspeed in a level turn? |
|
Definition
|
|
Term
| Which instruments should be used to make a pitch correction when you have deviated from your assigned altitude? |
|
Definition
| Attitude indicator, altimeter, and VSI |
|
|
Term
| Conditions that determine the pitch attitude required to maintain level flight are |
|
Definition
| airspeed, air density, wing design, and angle of attack. |
|
|
Term
| Approximately what percent of the indicated vertical speed should be used to determine the number of feet to lead the level-off from a climb to a specific altitude? |
|
Definition
|
|
Term
| To level off from a descent to a specific altitude, the pilot should lead the level-off by approximately |
|
Definition
| 10 percent of the vertical speed. |
|
|
Term
| For maintaining level flight at constant thrust, which instrument would be the least appropriate for determining the need for a pitch change? |
|
Definition
|
|
Term
| To enter a constant-airspeed descent from level-cruising flight, and maintain cruising airspeed, the pilot should |
|
Definition
| simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed. |
|
|
Term
| To level off at an airspeed higher than the descent speed, the addition of power should be made, assuming a 500 FPM rate of descent, at approximately |
|
Definition
| 100 to 150 feet above the desired altitude. |
|
|
Term
| What instrument(s) is(are) supporting bank instrument when entering a constant airspeed climb from straight-and-level flight? |
|
Definition
| Attitude indicator and turn coordinator |
|
|
Term
| As power is increased to enter a 500 feet per minute rate of climb in straight flight, which instruments are primary for pitch, bank, and power respectively? |
|
Definition
| Airspeed indicator, heading indicator, and manifold pressure gauge or tachometer. |
|
|
Term
| What is the primary pitch instrument during a stabilized autorotation? |
|
Definition
|
|
Term
| While recovering from an unusual flight attitude without the aid of the attitude indicator, approximate level pitch attitude is reached when the |
|
Definition
| airspeed and altimeter stop their movement and the VSI reverse its trend. |
|
|
Term
| During recoveries from unusual attitudes, level flight is attained the instant |
|
Definition
| the altimeter and airspeed needles stop prior to reversing their direction of movement. |
|
|
Term
| (Refer to figure 145) What is the correct sequence for recovery from the unusual attitude indicated? |
|
Definition
| Reduce power, level the wings, bring pitch attitude to level flight. |
|
|
Term
| (Refer to figure 147) Which is the correct sequence for recovery from the unusual attitude indicated? |
|
Definition
| Add power, lower nose, level wings, return to original attitude and heading. |
|
|
Term
| If an airplane is in an unusual flight atittude and the attitude indicator has exceeded its limits, which instruments should be relied on to determine pitch attitude before starting recovery? |
|
Definition
|
|
Term
| Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight attitude? |
|
Definition
| Reduce power, correct the bank attitude, and raise the nose to a level attitude. |
|
|
Term
| If a helicopter is in an unusual flight attitude and the attitude indicator has exceeded its liits, which instruments should be relied on to determine pitch attitude before starting recovery? |
|
Definition
| Airspeed, VSI and alitmeter |
|
|
Term
| Which is the correct sequence for recovery form a spiraling, nose low, increasing airspeed, unusual flight attitude? |
|
Definition
| Correct the bank attitude, raise the nose to a level attitude and reduce power. |
|
|