41 H931 PVT (Refer to figure 4.) What is the maximum structural cruising speed? A) 100 MPH. B) 165 MPH. C) 208 MPH. 42 H931 PVT (Refer to figure 4.) Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration? A) Upper limit of the green arc. B) Upper limit of the white arc. C) Lower limit of the white arc. 43 H931 PVT (Refer to figure 4.) What is the maximum flaps-extended speed? A) 65 MPH. B) 100 MPH. C) 165 MPH. 44 H931 PVT (Refer to figure 4.) Which color identifies the power-off stalling speed in a specified configuration? A) Upper limit of the green arc. B) Upper limit of the white arc. C) Lower limit of the green arc. 45 H931 PVT (Refer to figure 4.) The maximum speed at which the airplane can be operated in smooth air is A) 100 MPH. B) 165 MPH. C) 208 MPH. 46 H931 PVT If a pilot changes the altimeter setting from 30.11 to 29.96, what is the approximate change in indication? A) Altimeter will indicate .15 inches Hg higher. B) Altimeter will indicate 150 feet higher. C) Altimeter will indicate 150 feet lower. 47 H931 PVT How do variations in temperature affect the altimeter? A) Pressure levels are raised on warm days and the indicated altitude is lower than true altitude. B) Higher temperatures expand the pressure levels and the indicated altitude is higher than true altitude. C) Lower temperatures lower the pressure levels and the indicated altitude is lower than true altitude. 48 H931 PVT Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates A) calibrated altitude at field elevation. B) absolute altitude at field elevation. C) true altitude at field elevation. 49 H931 PVT (Refer to figure 3.) Altimeter 1 indicates A) 500 feet. B) 1,500 feet. C) 10,500 feet. 50 H931 PVT If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs? A) 70-foot increase in indicated altitude. B) 70-foot increase in density altitude. C) 700-foot increase in indicated altitude. 51 H931 PVT Under what condition is indicated altitude the same as true altitude? A) If the altimeter has no mechanical error. B) When at sea level under standard conditions. C) When at 18,000 feet MSL with the altimeter set at 29.92. 52 H931 PVT What is pressure altitude? A) The indicated altitude corrected for position and installation error. B) The altitude indicated when the barometric pressure scale is set to 29.92. C) The indicated altitude corrected for nonstandard temperature and pressure. 53 H931 PVT What is true altitude? A) The vertical distance of the aircraft above sea level. B) The vertical distance of the aircraft above the surface. C) The height above the standard datum plane. 54 H931 PVT What is absolute altitude? A) The altitude read directly from the altimeter. B) The vertical distance of the aircraft above the surface. C) The height above the standard datum plane. 55 H931 PVT What is density altitude? A) The height above the standard datum plane. B) The pressure altitude corrected for nonstandard temperature. C) The altitude read directly from the altimeter. 56 H932 PVT (Refer to figure 7.) The proper adjustment to make on the attitude indicator during level flight is to align the A) horizon bar to the level-flight indication. B) horizon bar to the miniature airplane. C) miniature airplane to the horizon bar. 57 H932 PVT (Refer to figure 7.) How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated? A) By the direction of deflection of the banking scale (A). B) By the direction of deflection of the horizon bar (B). C) By the relationship of the miniature airplane (C) to the deflected horizon bar (B). 58 H933 PVT In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate A) a turn momentarily. B) correctly when on a north or south heading. C) a turn toward the south. 59 H933 PVT In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if A) a left turn is entered from a north heading. B) a right turn is entered from a north heading. C) an aircraft is accelerated while on a north heading. 60 H933 PVT Deviation in a magnetic compass is caused by the A) presence of flaws in the permanent magnets of the compass. B) difference in the location between true north and magnetic north. C) magnetic fields within the aircraft distorting the lines of magnetic force.

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