21 H919 PVT As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will A) decrease as the true airspeed decreases. B) decrease as the true airspeed increases. C) remain the same regardless of altitude. 22 H919 PVT The angle of attack at which an airplane wing stalls will A) increase if the CG is moved forward. B) change with an increase in gross weight. C) remain the same regardless of gross weight. 23 J11 PVT An ATC radar facility issues the following advisory to a pilot flying north in a calm wind: `TRAFFIC 9 O`CLOCK, 2 MILES, SOUTHBOUND...` Where should the pilot look for this traffic? A) South. B) North. C) West. 24 H945 PVT (Refer to figure 36.) What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions? Pressure altitude 8,000 ft Temperature 22 �‹C Manifold pressure 20.8 inches Hg Wind Calm A) 60.2 gallons. B) 70.1 gallons. C) 73.2 gallons. 25 H948 PVT (Refer to figure 36.) What fuel flow should a pilot expect at 11,000 feet on a standard day with 65 percent maximum continuous power? A) 10.6 gallons per hour. B) 11.2 gallons per hour. C) 11.8 gallons per hour. 26 H945 PVT (Refer to figure 8.) What is the effect of a temperature decrease and a pressure altitude increase on the density altitude from 90 �‹F and 1,250 feet pressure altitude to 55 �‹F and 1,750 feet pressure altitude? A) 1,300-foot decrease. B) 1,700-foot decrease. C) 1,700-foot increase. 27 H945 PVT (Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97. A) 1,341 feet MSL. B) 1,451 feet MSL. C) 1,562 feet MSL. 28 H946 PVT (Refer to figure 8.) What is the effect of a temperature increase from 30 to 50 �‹F on the density altitude if the pressure altitude remains at 3,000 feet MSL? A) 900-foot increase. B) 1,100-foot decrease. C) 1,300-foot increase. 29 H946 PVT (Refer to figure 38.) Determine the approximate total distance required to land over a 50-foot obstacle. OAT 90 �‹F Pressure altitude 4,000 ft Weight 2,800 lb Headwind component 10 kts A) 1,525 feet. B) 1,775 feet. C) 1,950 feet. 30 H946 PVT (Refer to figure 38.) Determine the total distance required to land. OAT 32 �‹F Pressure altitude 8,000 ft Weight 2,600 lb Headwind component 20 kts Obstacle 50 ft A) 850 feet. B) 1,400 feet. C) 1,750 feet. 31 H945 PVT (Refer to figure 8.) Determine the pressure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22 at standard temperature. A) 2,913 feet MSL. B) 2,991 feet MSL. C) 3,010 feet MSL. 32 H945 PVT (Refer to figure 8.) Determine the pressure altitude at an airport that is 3,563 feet MSL with an altimeter setting of 29.96. A) 3,527 feet MSL. B) 3,556 feet MSL. C) 3,639 feet MSL. 33 H946 PVT (Refer to figure 41.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT Std Pressure altitude 4,000 ft Takeoff weight 2,800 lb Headwind component Calm A) 1,500 feet. B) 1,750 feet. C) 2,000 feet. 34 J22 PVT When activated, an emergency locator transmitter (ELT) transmits on A) 118.0 and 118.8 MHz. B) 121.5 and 243.0 MHz. C) 123.0 and 119.0 MHz. 35 B11 PVT When must the battery in an emergency locator transmitter (ELT) be replaced (or recharged if the battery is rechargeable)? A) After one-half the battery's useful life. B) During each annual and 100-hour inspection. C) Every 24 calendar months. 36 J22 PVT When may an emergency locator transmitter (ELT) be tested? A) Anytime. B) At 15 and 45 minutes past the hour. C) During the first 5 minutes after the hour. 37 J22 PVT Which procedure is recommended to ensure that the emergency locator transmitter (ELT) has not been activated? A) Turn off the aircraft ELT after landing. B) Ask the airport tower if they are receiving an ELT signal. C) Monitor 121.5 before engine shutdown. 38 J11 PVT If Air Traffic Control advises that radar service is terminated when the pilot is departing Class C airspace, the transponder should be set to code A) 0000. B) 1200. C) 4096. 39 H926 PVT One of the main functions of flaps during approach and landing is to A) decrease the angle of descent without increasing the airspeed. B) permit a touchdown at a higher indicated airspeed. C) increase the angle of descent without increasing the airspeed. 40 H931 PVT What is an important airspeed limitation that is not color coded on airspeed indicators? A) Never-exceed speed. B) Maximum structural cruising speed. C) Maneuvering speed.

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