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Título del Test: jojojo4 Descripción: maria y juan Autor: mptm Fecha de Creación: 23/02/2016 Categoría: Otros Número Preguntas: 100

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401. when airspeed is increased in a turn, what must be done to maintain a constant altitude? decrease the angle of bank. increase the angle of bank and/ or decrease the angle of attack. 402. during standard-rate turns, which instrument is considered primary for bank? turn and slip indicator or turn coordinator. attitude indicator. 403. if a half-standard rate turn is maintained, how long would it take to turn 360°? 2 minutes. 4 minutes. 404. if a standard rate turn is maintained, how long would it take to turn 180°? 1 minute. 2 minutes. 405. 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°? 1 minute 3 seconds. 1 minute. 406 During a constant-bank level turn, what effect would an increase in airspeed have on the rate and radius of turn? Rate of turn would decrease, and radius of turn would increase. Rate of turn would increase, and radius of turn would increase. 407 If a standard rate turn is maintained, how much time would be required to turn to the right from a heading of 090° to a heading of 270°? 3 minutes. 1 minute. 408 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°? 40 seconds. 50 seconds. 409 If a half-standard rate turn is maintained, how long would it take to turn 135°? 1 minute 20 seconds. 1 minute 30 seconds. 410 Rate of turn can be increased and radius of turn decreased by Decreasing airspeed and increasing the bank. Decreasing airspeed and shallowing the bank. 411 The displacement of a turn coordinator during a coordinated turn will Remain constant for a given bank regardless of airspeed. Increase as angle of bank increases. 412 (Refer to Figure 8.) What changes in control displacement should be made so that “2” would result in a coordinated standard rate turn? Increase left rudder and increase rate of turn. Increase left rudder and decrease rate of turn. 413 (Refer to Figure 8.) Which illustration indicates a coordinated turn? 3 1 . 414 (Refer to Figure 8.) Which illustration indicates a skidding turn? 1 2. 415 (Refer to Figure 8.) What changes in control displacement should be made so that “1” would result in a coordinated standard rate turn? Increase right rudder and increase rate of turn. Increase right rudder and decrease rate of turn. 416 (Refer to Figure 8.) Which illustration indicates a slipping turn? 2 3. 417 What pretakeoff check should be made of a vacuum-driven heading indicator in preparation for an IFR flight? After 5 minutes, check that the heading indicator card aligns itself with the magnetic heading of the aircraft. After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns. 418 On the taxi check, the magnetic compass should Swing opposite to the direction of turn when turning from north. Swing freely and indicate known headings. 419 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? The compass will initially indicate a turn to the right. The compass will indicate the aproximate correct mgnetic heading if the roll into the turn is smooth. 420 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? The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. The compass will initially indicate a turn to the left. 421 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? The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft. The compass will indicate a turn to the right, but at a faster rate than is actually occurring. 422 On what headings will the magnetic compass read most accurately during a level 360° turn, with a bank of approximately 15°? 90° and 270°. 180° and 0°. 423 What causes the northerly turning error in a magnetic compass? Coriolis force at the mid-latitudes. The magnetic dip characteristic. 424 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? The compass will indicate a turn to the left, but at a faster rate than is actually occurring. The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft. 425 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? The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. The compass will remain on a westerly heading for a short time, then gradually catch up to the actual heading of the aircraft. 426 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? The compass will initially indicate a turn to the left. The compass will indicate a turn to the right, but at a faster rate than is actually occurring. 427 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? The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. The compass will initially indicate a turn to the right. 428 What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a north 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 to the right. 429 Which practical test should be made on the electric gyro instruments prior to starting an engine? Turn on the electrical power and listen for any unusual or irregular mechanical noise. Check that the electrical connections are secure on the back of the instruments. 430 En route at FL290, your altimeter is set correctly, but you fail to reset it to the local altimeter setting of 30.26" Hg during descent. If the field elevation is 134 feet and your altimeter is functioning properly, what will it indicate after landing? 100 feet MSL. 206 feet below MSL. 431 If both the ram air input and drain hole of the pitot system are blocked, what airspeed indication can be expected? Constant indicated airspeed during a descent. No variation of indicated airspeed in level flight even if large power changes are made. 432 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? No change until an actual climb rate is established, then indicated airspeed will increase. The airspeed would drop to, and remain at, zero. 433 What indication should a pilot observe if an airspeed indicator ram air input and drain hole are blocked? The airspeed indicator will show a decrease with an increase in altitude. The airspeed indicator will react as an altimeter. 434 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? The VSI pointer would remain at zero regardless of the actual rate of descent. The indication would be in reverse of the actual rate of descent (500 FPM climb). 435 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? The altimeter and airspeed indicator to become inoperative. The vertical speed to momentarily show a climb. 436 During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be affected? The airspeed indicator only. The airspeed indicator, altimeter, and Vertical Speed Indicator. 437 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? The vertical speed to show a climb. The altimeter to read higher than normal. 438 (Refer to Figure 9.) Identify the system that has failed and determine a corrective action to return the airplane to straight-and-level flight. Static/pitot system is blocked, lower the nose and level the wings to level-flight attitude by use of attitude indicator. Electrical system has failed, reduce power, roll left to level wings, and raise the nose to reduce airspeed. 439 (Refer to Figure 10.) What is the flight attitude? One instrument has malfunctioned. Climbing turn to the right. Climbing turn to the left. 440 (Refer to Figure 11.) What is the flight attitude? One system which transmits information to the instruments has malfunctioned. Straight-and-level flight. Level turn to the right. 441 What is the correct sequence in which to use the three skills used in instrument flying? Cross-check, instrument interpretation, and aircraft control. Aircraft control, cross-check, and instrument interpretation. 442 What are the three fundamental skills involved in attitude instrument flying? Cross-check, emphasis, and aircraft control. Cross-check, instrument interpretation, and aircraft control. 443 What is the third fundamental skill in attitude instrument flying? Aircraft control. Power control. 444 What is the first fundamental skill in attitude instrument flying? Instrument cross-check. Instrument interpretation. 445 What effect will a change in wind direction have upon maintaining a 3° glide slope at a constant true airspeed? When ground speed increases, rate of descent must increase. When ground speed decreases, rate of descent must increase. 446 The rate of descent required to stay on the ILS glide slope Must be decreased if the ground speed is decreased. Must be increased if the ground speed is decreased. 447 To remain on the ILS glidepath, the rate of descent must be Increased if the ground speed is increased. Decreased if the ground speed is increased. 448 The rate of descent on the glide slope is dependent upon Ground speed. Calibrated airspeed. 449 The glide slope and localizer are centered, but the airspeed is too fast. Which should be adjusted initially? Power only. Pitch only. 450 During a precision radar or ILS approach, the rate of descent required to remain on the glide slope will Increase as the ground speed increases. Decrease as the ground speed increases. 451 The gyroscopic heading indicator is inoperative. What is the primary bank instrument in unaccelerated straight-and-level flight? Magnetic compass. Attitude indicator. 452 What instruments are considered supporting bank instruments during a straight, stabilized climb at a constant rate? Attitude indicator and turn coordinator. Heading indicator and turn coordinator. 453 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. 454 What is the primary bank instrument once a standard rate turn is established? Turn coordinator. Heading indicator. 455 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? Attitude indicator, heading indicator, and manifold pressure gauge or tachometer. Airspeed indicator, attitude indicator, and manifold pressure gauge or tachometer. 456 What is the primary pitch instrument during a stabilized climbing left turn at cruise climb airspeed? Attitude indicator Airspeed indicator. 457 What is the primary pitch instrument when establishing a constant altitude standard rate turn? Airspeed indicator. Altimeter. 458 As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using Less than half bar width on the attitude indicator. Less than a full bar width on the attitude indicator. 459 What is the initial primary bank instrument when establishing a level standard rate turn? Attitude indicator. Heading indicator. 460 What instrument(s) is(are) supporting bank instrument when entering a constant airspeed climb from straight-and-level flight? Attitude indicator and turn coordinator. Turn coordinator and heading indicator. 461 What is the primary bank instrument while transitioning from straight-and-level flight to a standard rate turn to the left? Attitude indicator. Heading indicator. 462 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? Altimeter, heading indicator, and manifold pressure gauge or tachometer. Altimeter, attitude indicator, and airspeed indicator. 463 Which instrument provides the most pertinent information (primary) for bank control in straight-and-level flight? Attitude indicator. Heading indicator. 464 Which instruments are considered primary and supporting for bank, respectively, when establishing a level standard rate turn? Attitude indicator and turn coordinator. Turn coordinator and attitude indicator. 465 Which instruments, in addition to the attitude indicator, are pitch instruments? Altimeter, airspeed indicator, and vertical speed indicator. Altimeter and airspeed only. 466 Which instrument provides the most pertinent information (primary) for pitch control in straight-and-level flight? Altimeter. Attitude indicator. 467 Which instruments are considered to be supporting instruments for pitch during change of airspeed in a level turn? Attitude indicator and VSI. Airspeed indicator and VSI. 468 Which instrument is considered primary for power as the airspeed reaches the desired value during change of airspeed in a level turn? Airspeed indicator. Attitude indicator. 469 Which instruments should be used to make a pitch correction when you have deviated from your assigned altitude? Attitude indicator, altimeter, and VSI. Manifold pressure gauge and VSI. 470 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 of attack. 471 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? 10 percent. 20 percent. 472 To level off from a descent to a specific altitude, the pilot should lead the level-off by approximately 10 percent of the vertical speed. 30 percent of the vertical speed. 473 For maintaining level flight at constant thrust, which instrument would be the least appropriate for determining the need for a pitch change? Attitude indicator. Altimeter. 474 To enter a constant-airspeed descent from level-cruising flight, and maintain cruising airspeed, the pilot should First reduce power, then adjust the pitch using the attitude indicator as a reference to establish a specific rate on the VSI. Simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed. 475 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 100 to 150 feet above the desired altitude. 50 to 100 feet above the desired altitude. 476 To level off from a descent maintaining the descending airspeed, the pilot should lead the desired altitude by approximately 50 feet. 60 feet. 477 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 at cruising speed, the altimeter reverses its trend, and the vertical speed stops its movement. 478 During recoveries from unusual attitudes, level flight is attained the instant The altimeter and airspeed needles stop prior to reversing their direction of movement. The horizon bar on the attitude indicator is exactly overlapped with the miniature airplane. 479 (Refer to Figure 12.) What is the correct sequence for recovery from the unusual attitude indicated? Reduce power, level the wings, bring pitch attitude to level flight. Reduce power, increase back elevator pressure, and level the wings. 480 (Refer to Figure 13.) Which is the correct sequence for recovery from the unusual attitude indicated? Add power, lower nose, level wings, return to original attitude and heading. Level wings, add power, lower nose, descend to original attitude, and heading. 481 If an airplane is in an unusual flight attitude and the attitude indicator has exceeded its limits, which instruments should be relied on to determine pitch attitude before starting recovery? Airspeed and altimeter. Turn indicator and VSI. 482 Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight attitude? Reduce power, correct the bank attitude, and raise the nose to a level attitude. Reduce power, raise the nose to level attitude, and correct the bank attitude. 483 In aircraft equipped with constant-speed propellers and normally-aspirated engines, which procedure should be used to avoid placing undue stress on the engine components? When power is being Increased, increase the RPM before increasing the manifold pressure. Increased or decreased, the RPM should be adjusted before the manifold pressure. 484 Which statement best describes the operating principle of a constant-speed propeller? The propeller control regulates the engine RPM, and in turn, the propeller RPM. A high blade angle, or increased pitch, reduces the propeller drag and allows more engine power for takeoffs. 485 Fuel/air ratio is the ratio between the Weight of fuel and weight of air entering the cylinder. Weight of fuel and weight of air entering the carburetor. 486 To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and Decreasing RPM by increasing propeller blade angle. Decreasing RPM by decreasing propeller blade angle. 487 To develop maximum power and thrust, a constant-speed propeller should be set to a blade angle that will produce a Small angle of attack and high RPM. Large angle of attack and high RPM. 488 For takeoff, the blade angle of a controllable-pitch propeller should be set at a Small angle of attack and high RPM. Large angle of attack and high RPM. 489 The reason for variations in geometric pitch (twisting) along a propeller blade is that it Permits a relatively constant angle of attack along its length when in cruising flight. Permits a relatively constant angle of incidence along its length when in cruising flight. 490 To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and Decreasing RPM by increasing propeller blade angle. Decreasing RPM by decreasing propeller blade angle. 491 A fixed-pitch propeller is designed for best efficiency only at a given combination of Airspeed and RPM. Airspeed and altitude. 492 Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel Remains constant while the density of air decreases. Remains constant while the volume of air decreases. 493 A flux value is found in: Directional Gyro systems and has no moving parts Fuel control units and is an internal component not governed from the flight deck. 494 The intake section of a jet engine is often considered part of the fuselage. The other four parts which are considered part of the engine are The compressor, combustion chamber, turbine and exhaust The Engine struts, compressor, combustion chamber and exhaust. 495 Hydraulic systems in modern aircraft are usually employed to Aid in moving heavy control surfaces or accessories. Aid in lowering the landing gear, moving the nose wheel steering and activating the passenger stairs. 496 Large transport category jet airplanes employ: Heated leading edges for de-icing / anti-icing. Silver colored deicing boots. 497 The most fuel efficient type engine for commercial passenger transport is Turboprop Turbofan with afterburners. 498 What type measurement is used to rate power on Jet or Fanjet engines Pounds of thrust Brake horse power. 499 Modern aircraft electrical systems normally consist of Engine generators delivering 115v AC including 400Hz and 24v DC systems Standard 350v 600 Hz AC with step-up transformers. 500 Aircraft hydraulic systems use: Hydraulic fluid Aviation grade engine oil as standard fluid.

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