11. CONGLOMERADO DE TABLAS

8717. (Refer to Figures 340, 451, and 452.) With a reported temperature of 20°C, flaps set at 8, engine bleeds closed, and a takeoff weight of 79,500 pounds, the takeoff safety speed is. 154 knots. 160 knots. 162 knots.

8718. (Refer to Figures 336, 451, and 452). With a reported temperature of 5°C, flaps set at 8, engine bleeds closed, and a takeoff weight off 82,000 pounds, the VR is. 150 knots. 147 knots. 158 knots.

8719. (Refer to Figures 340 and 450.) With a reported temperature of 35°C, flaps set at 8, and 5 knots of head- wind at a takeoff weight of 82,300 pounds, the V1MBE is. 174 knots. 169 knots. 154 knots.

8720. (Refer to Figures 342 and 450.) With a reported temperature of 40°C, flaps set at 20, and a 3 knot tailwind at a takeoff weight of 84,500, the V1MBE is. 160 knots. 143 knots. 166 knots.

(Refer to Figures 342, 451, and 452.) With a reported temperature of -10°C, flaps set at 8, cowl anti- ice on, and at a takeoff weight off 77,000 lbs, the VR and V2 speeds are. 143 and 153 knots. 153 and 143 knots. 123 and 133 knots.

8584. (Refer to Figure 465.) At a weight of 60,000 pounds with 35 flaps, the Reference Stall Speed is. 96 knots. 93 knots. 89 knots.

8585. (Refer to Figure 465.) What is the reference stall speed if you will be landing the aircraft at 55,000 pounds with 35° of flaps?. 92 knots. 97 knots. 102 knots.

8586. (Refer to Figure 470.) What are the V1 and VR speeds at 25°C at sea level for an aircraft weighing 54,500 lbs. and a maximum V1/VR ratio of .93?. 110 and 114 knots. 112 and 121 knots. 97 and 102 knots.

8587. (Refer to Figure 470.) What are the V1 and VR speeds at ISA+30°C and a field elevation of 4,500 feet for an aircraft weighing 64,000 lbs. and a maximum V1/VR ratio of .98?. 100 and 104 knots. 112 and 115 knots. 135 and 137 knots.

8618. Refer to Figures 46, 53, and 55.) What is the takeoff safety speed for Operating Conditions R-1?. 128 knots. 121 knots. 133 knots.

8619. (Refer to Figures 46, 53, and 55.) What is the rotation speed for Operating Conditions R-2?. 147 knots. 152 knots. 146 knots.

8620. (Refer to Figures 46, 53, and 55.) What are V1, VR, and V2 speeds for Operating Conditions R-3?. 143, 143, and 147 knots. 138, 138, and 142 knots. 136, 138, and 143 knots.

8621. (Refer to Figures 46, 53, and 55.) What are critical engine failure and takeoff safety speeds for Operating Conditions R-4?. 131 and 133 knots. 123 and 134 knots. 122 and 130 knots.

8622. (Refer to Figures 46, 53, and 55.) What are rota- tion and V2 bug speeds for Operating Conditions R-5?. 138 and 143 knots. 136 and 138 knots. 134 and 141 knots.

8642-4 (Refer to Figures 237 and 238.) Given the following conditions, what are the takeoff V speeds?. V1 133 kts, VR 140 kts, V2 145 kts. V1 140 kts, VR 140 kts, V2 145 kts. V1 138 kts, VR 141 kts, V2 145 kts.

8712. (Refer to Figures 363 and 429.) At a reported temperature of 10°C with cowl anti-ice on and packs on, the takeoff thrust setting is. 90.0%. 89.1%. 87.4%.

8713. (Refer to Figures 330 and 428.) At a reported temperature of 30°C with engine bleeds closed, the takeoff thrust setting is. 91.9%. 87.4%. 90.9%.

8714. (Refer to Figures 329 and 428.) At a reported temperature of 20°C with engine bleeds closed, the takeoff thrust setting is. 92.1%. 92.3%. 88.4%.

8715. (Refer to Figures 329 and 429.) At a reported temperature of -10°C with cowl anti-ice on and packs on, the takeoff thrust setting is. 87.0%. 87.2%. 87.7%.

8716. (Refer to Figures 332 and 428.) At a reported temperature of 5°C with engine bleeds off, the takeoff thrust setting is. 87.0%. 87.2%. 88.2%.

8613. (Refer to Figure 393.) (Note: Applicants may request a printed copy of the chart(s) or graph(s) for use while computing the answer. All printed pages must be returned to test proctor.) With an OAT of 10°C, inertial separator in bypass and cabin heater, you calculate maximum torque for climb to be. 1,795 ft-lbs. 1,695 ft-lbs. 1,615 ft-lbs.

9874. (Refer to Figures 46, 53, and 55.) What is the takeoff EPR for Operating Conditions R-1?. 2.04. 2.01. 2.035.

8614. (Refer to Figures 46, 53, and 55.) What is the takeoff EPR for Operating Conditions R-2?. 2.19. 2.18. 2.16.

8615. (Refer to Figures 46, 53, and 55.) What is the takeoff EPR for Operating Conditions R-3?. 2.01. 2.083. 2.04.

8616. (Refer to Figures 46, 53, and 55.) What is the takeoff EPR for Operating Conditions R-4?. 2.06. 2.105. 2.11.

8617. (Refer to Figures 46, 53, and 55.) What is the takeoff EPR for Operating Conditions R-5?. 1.98. 1.95. 1.96.

8400-1. (Refer to Figure 271.) For a takeoff from Runway 25L at LAX, what is the minimum climb gradient that ATC expects the aircraft to maintain?. 500 feet per minute climb. 200 feet per minute climb. 400 feet per minute climb.

8593. (Refer to Figures 273 and 475.) With a reported temperature of 32°C, and a weight of 58,000 pounds, the second segment takeoff gross climb gradient is. 0.057%. 0.062%. 0.034%.

8594. (Refer to Figures 273 and 474.) With a reported temperature of 45°C, and a weight of 52,000 pounds, the first segment takeoff gross climb gradient is. 0.048%. 0.044%. 0.0419%.

9935. (Refer to Figure 474.) What is the gross climb gradient with the following conditions? Outside air temperature......................................... 0°C Airfield altitude............................................. 4,000 feet Weight ................................................. 55,000 pounds. 0.052%. 0.020%. 0.074%.

8628. (Refer to Figures 56, 57, and 58.) What is the ground distance covered during en route climb for Operating Conditions V-1?. 145 NM. 137 NM. 134 NM.

8629. (Refer to Figures 56, 57, and 58.) What is the ground distance covered during en route climb for Operating Conditions V-2?. 84 NM. 65 NM. 69 NM.

8630. (Refer to Figures 56, 57, and 58.) What is the ground distance covered during en route climb for Operating Conditions V-3?. 95 NM. 79 NM. 57 NM.

8631. (Refer to Figures 56, 57, and 58.) What is the ground distance covered during en route climb for Operating Conditions V-4?. 63 NM. 53 NM. 65 NM.

8632. (Refer to Figures 56, 57, and 58.) What is the ground distance covered during en route climb for Operating Conditions V-5?. 70 NM. 52 NM. 61 NM.

8633. (Refer to Figures 56, 57, and 58.) How much fuel is burned during en route climb for Operating Conditions V-1?. 4,100 pounds. 3,600 pounds. 4,000 pounds.

8634. (Refer to Figures 56, 57, and 58.) How much fuel is burned during en route climb for Operating Conditions V-2?. 2,250 pounds. 2,600 pounds. 2,400 pounds.

8635. (Refer to Figures 56, 57, and 58.) What is the aircraft weight at the top of climb for Operating Conditions V-3?. 82,100 pounds. 82,500 pounds. 82,200 pounds.

8636. (Refer to Figures 56, 57, and 58.) What is the aircraft weight at the top of climb for Operating Conditions V-4?. 102,900 pounds. 102,600 pounds. 103,100 pounds.

8637. (Refer to Figures 56, 57, and 58.) What is the aircraft weight at the top of climb for Operating Conditions V-5?. 73,000 pounds. 72,900 pounds. 72,800 pounds.

8638. (Refer to Figures 59 and 60.) What is the max climb EPR for Operating Conditions T-1?. 1.82. 1.96. 2.04.

8639. (Refer to Figures 59 and 60.) What is the max continuous EPR for Operating Conditions T-2?. 2.10. 1.99. 2.02.

8640. (Refer to Figures 59 and 60.) What is the max cruise EPR for Operating Conditions T-3?. 2.11. 2.02. 1.90.

8641. (Refer to Figures 59 and 60.) What is the max climb EPR for Operating Conditions T-4?. 2.20. 2.07. 2.06.

8642-1. (Refer to Figures 59 and 60.) What is the max continuous EPR for Operating Conditions T-5?. 2.00. 2.04. 1.96.

8642-2. (Refer to Figure 231.) Given the following conditions, what is the takeoff climb limit? Airport OAT.......................................................... 38°C Airport Pressure Altitude ..................................... 14 ft. Flaps....................................................................... 15° Engine Bleed for packs .......................................... On Anti-ice ................................................................... Off. 136,000 lb. 137,500 lb. 139,000 lb.

9875. (Refer to Figures 48, 49, and 50.) What is the ground distance covered during en route climb for Operating Conditions W-1?. 104.0 NM. 99.2 NM. 109.7 NM.

9876. (Refer to Figures 48, 49, and 50.) What is the ground distance covered during en route climb for Operating Conditions W-2?. 85.8 NM. 87.8 NM. 79.4 NM.

9877. (Refer to Figures 48, 49, and 50.) What is the ground distance covered during en route climb for Operating Conditions W-3?. 86.4 NM. 84.2 NM. 85.1 NM.

8596. (Refer to Figures 48, 49, and 50.) What is the ground distance covered during en route climb for Operating Conditions W-4?. 58.4 NM. 61.4 NM. 60.3 NM.

8597. (Refer to Figures 48, 49, and 50.) What is the ground distance covered during en route climb for Operating Conditions W-5?. 68.0 NM. 73.9 NM. 66.4 NM.

8598. (Refer to Figures 48, 49, and 50.) What is the aircraft weight at the top of climb for Operating Conditions W-1?. 81,600 pounds. 81,400 pounds. 81,550 pounds.

8599. (Refer to Figures 48, 49, and 50.) What is the aircraft weight at the top of climb for Operating Conditions W-2?. 82,775 pounds. 83,650 pounds. 83,775 pounds.

8600. (Refer to Figures 48, 49, and 50.) What is the aircraft weight at the top of climb for Operating Conditions W-3?. 75,750 pounds. 75,900 pounds. 76,100 pounds.

8601. (Refer to Figures 48, 49, and 50.) What is the aircraft weight at the top of climb for Operating Conditions W-4?. 86,150 pounds. 86,260 pounds. 86,450 pounds.

8602. (Refer to Figures 48, 49, and 50.) What is the aircraft weight at the top of climb for Operating Conditions W-5?. 89,900 pounds. 90,000 pounds. 90,100 pounds.

8935. At what minimum speed (rounded off) could dynamic hydroplaning occur on main tires having a pressure of 121 PSI?. 90 knots. 99 knots. 110 knots.

8936. At what minimum speed will dynamic hydroplaning begin if a tire has an air pressure of 70 PSI?. 85 knots. 80 knots. 75 knots.

9792. Arriving over the runway 10 knots over VREF would add approximately how many feet to the dry landing distance?. 800 feet. 1,700 feet. 2,800 feet.

8742. (Refer to Figures 327 and 457.) With a weight of 69,000 pounds, flaps 45, calm winds, the VREF is. 136 knots. 133 knots. 129 knots.

8743. (Refer to Figure 460.) At a weight of 77,500 pounds, and a landing elevation below 5,000 feet, the VREF is. 139 knots. 141 knots. 143 knots.

8744. (Refer to Figures 331 and 461.) At a weight of 73,500 pounds, the expected landing field length is. 6,700 feet. 5,650 feet. 6,450 feet.

8745. (Refer to Figures 331 and 461.) What is the maximum landing weight which will permit stopping 2,000 feet short of the end of a 7,500-foot dry runway?. 32,200 pounds. 71,000 pounds. 72,500 pounds.

8746. (Refer to Figures 321 and 458.) With a reported temperature of 15°C, a 0.8% upslope, and calm winds, the maximum permissible quick turn-around landing weight is. 81,000 pounds. 81,600 pounds. 82,000 pounds.

8750. (Refer to Figure 461.) What is the maximum land- ing weight which will permit stopping 700 feet short of the end of a 5,600 foot runway at sea level?. 61,000 pounds. 59,000 pounds. 63,000 pounds.

8753. (Refer to Figures 273 and 457). What is the land- ing field length on a wet runway with a headwind of 7 knots and an aircraft weight of 83,000 pounds?. 6,600 feet. 7,200 feet. 5,900 feet.

8756. (Refer to Figures 331 and 457.) What approach speed and landing distance will be needed when land- ing at a weight of 75,000 pounds on a dry runway with calm winds?. 131 knots and 5,600 feet. 141 knots and 4,600 feet. 141 knots and 5,600 feet.

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

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.

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.

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.

8678. (Refer to Figure 70.) How many minutes of dump time is required to reach a weight of 144,500 pounds? Initial weight................................................ 180,500 lb Zero fuel weight.......................................... 125,500 lb. 13 minutes. 15 minutes. 16 minutes.

8679. (Refer to Figure 70.) How many minutes of dump time is required to reduce fuel load to 25,000 pounds? Initial weight.................................................179,500 lb Zero fuel weight.......................................... 136,500 lb. 10 minutes. 9 minutes. 8 minutes.

8680. (Refer to Figure 70.) How many minutes of dump time is required to reach a weight of 151,500 pounds? Initial weight.................................................181,500 lb Zero fuel weight.......................................... 126,000 lb. 15 minutes. 14 minutes. 13 minutes.

8681. (Refer to Figure 70.) How many minutes of dump time is required to reduce fuel load to 16,000 pounds (at 2,350 lbs/min)? Initial weight.................................................175,500 lb Zero fuel weight.......................................... 138,000 lb. 9 minutes. 10 minutes. 8 minutes.

8682. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-1?. 19,400 feet. 18,000 feet. 20,200 feet.

8683. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-2?. 14,700 feet. 17,500 feet. 18,300 feet.

8684. (Refer to Figures 71 and 72.) What is the approxi- mate level-off pressure altitude after drift-down under Operating Conditions D-3?. 22,200 feet. 19,800 feet. 21,600 feet.

8685. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-4?. 27,900 feet. 22,200 feet. 24,400 feet.

8686. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-5?. 8,800 feet. 9,600 feet. 13,000 feet.