8. MISELLANEOUS PERFORMANCE

9321. Which is the correct symbol for design cruising speed?. VC. VS. VA.

8344. How can turbulent air cause an increase in stalling speed of an airfoil?. An abrupt change in relative wind. A decrease in angle of attack. Sudden decrease in load factor.

9129. If severe turbulence is encountered, which procedure is recommended?. Maintain a constant altitude. Maintain a constant attitude. Maintain constant airspeed and altitude.

9320. Which speed symbol indicates the maximum operating limit speed for an airplane?. VLE. VMO / MMO. VLO / MLO.

8668. (Refer to Figures 68 and 69.) What are the recommended IAS and EPR settings for holding under Operating Conditions O-1?. 219 knots and 1.83 EPR. 223 knots and 2.01 EPR. 217 knots and 1.81 EPR.

8669. (Refer to Figures 68 and 69.) What are the rec- ommended IAS and EPR settings for holding under Operating Conditions O-2?. 210 knots and 1.57 EPR. 210 knots and 1.51 EPR. 210 knots and 1.45 EPR.

8670. (Refer to Figures 68 and 69.) What are the rec- ommended IAS and EPR settings for holding under Operating Conditions O-3?. 217 knots and 1.50 EPR. 215 knots and 1.44 EPR. 216 knots and 1.40 EPR.

8671. (Refer to Figures 68 and 69.) What are the recommended IAS and EPR settings for holding under Operating Conditions O-4?. 223 knots and 1.33 EPR. 225 knots and 1.33 EPR. 220 knots and 1.28 EPR.

8672. (Refer to Figures 68 and 69.) What are the rec- ommended IAS and EPR settings for holding under Operating Conditions O-5?. 219 knots and 1.28 EPR. 214 knots and 1.26 EPR. 218 knots and 1.27 EPR.

8673. (Refer to Figures 68 and 69.) What is the approximate fuel consumed when holding under Operating Conditions O-1?. 1,625 pounds. 1,950 pounds. 2,440 pounds.

8674. (Refer to Figures 68 and 69.) What is the approximate fuel consumed when holding under Operating Conditions O-2?. 2,250 pounds. 2,500 pounds. 3,000 pounds.

8675. (Refer to Figures 68 and 69.) What is the approxi- mate fuel consumed when holding under Operating Conditions O-3?. 2,940 pounds. 2,520 pounds. 3,250 pounds.

8676. (Refer to Figures 68 and 69.) What is the approxi- mate fuel consumed when holding under Operating Conditions O-4?. 2,870 pounds. 2,230 pounds. 1,440 pounds.

8677. (Refer to Figures 68 and 69.) What is the approximate fuel consumed when holding under Operating Conditions O-5?. 2,950 pounds. 2,870 pounds. 2,400 pounds.

9943. (Refer to Figure 69.) Before departure, you learn that your destination airport’s arrivals are holding for 30 minutes on the arrival. In a two-engine aircraft, how many pounds of fuel would be required to hold at 10,000 feet with an EPR of 1.26 and an airplane weight of 85,000 pounds?. 1,155 pounds. 2,310 pounds. 4,620 pounds.

8727-1. (Refer to Figure 21.) You are taking off from a runway with a 330° magnetic course. Tower reported winds are 290° at 25 knots. The computed headwind component for takeoff is. 19 knots. 25 knots. 16 knots.

8727. (Refer to Figures 287 and 421.) The winds are reported as 220/15. You compute tailwind component, hoping for a Runway 33 takeoff. You compute the tail- wind to be. 14 knots. 10 knots. 5 knots.

8728. (Refer to Figure 422.) At a weight of 68,500 pounds with gear and flaps up, you find the reference stall speed to be. 148 knots. 145 knots. 142 knots.

8729. (Refer to Figure 459.) With a payload of 20,000 pounds, the still-air range is. 1,350 NM. 1,410 NM. 1,590 NM.

8730. (Refer to Figure 459.) For a supplemental charter, a still-air range of 2,250 NM is required. The payload for this nonstop trip is. 5,100 pounds. 5,900 pounds. 6,100 pounds.

8731. (Refer to Figure 417.) You find one air data computer listed on the MEL as inoperative, leaving one ADC operative during your preflight logbook inspection. This means the flight. must fly non-RVSM flight levels above FL330. can only fly between FL290. must remain below FL290 unless dispatch obtains a deviation from ATC.

8732. (Refer to Figure 438.) With an actual runway length of 6,400 feet with 8 flaps, a 1% downslope, a 200 foot clearway, and 4 knots of tailwind, the Reference A is. 2.12. 2.02. 1.94.

8733. (Refer to Figures 318 and 439.) With a reported temperature of 30°C with packs on and anti-ice off, the Reference B is. 28.2. 29.8. 30.7.

8734. (Refer to Figure 440, All Engines.) With a Reference A of 3.00 and Reference B of 28.5, the takeoff weight is limited to. 78,500 pounds. 76,500 pounds. 75,000 pounds.

9128. What action is appropriate when encountering the first ripple of reported clear air turbulence (CAT)?. Extend flaps to decrease wing loading. Extend gear to provide more drag and increase stability. Adjust airspeed to that recommended for rough air.

9937. (Refer to Figure 473.) What is the maximum permissible takeoff weight with an airfield altitude of 7,300 feet and an outside air temperature of 24°C?. 65,000 pounds. 62,400 pounds. 63,800 pounds.