NAV ASA COM
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Título del Test:
![]() NAV ASA COM Descripción: NAV ASA COM PL |



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GIVEN: Determine the time en route and fuel consumption. 1 hour 28 minutes and 73.2 pounds. 1 hour 38 minutes and 158 pounds. 1 hour 40 minutes and 175 pounds. An airplane descends to an airport under the following conditions: 10 minutes, 348°, 18 NM, 1.4 gallons. 10 minutes, 355°, 17 NM, 2.4 gallons. 12 minutes, 346°, 18 NM, 1.6 gallons. An airplane descends to an airport under the following conditions: 16 minutes, 168°, 30 NM, 2.9 gallons. 18 minutes, 164°, 34 NM, 3.2 gallons. 18 minutes, 168°, 34 NM, 2.9 gallons. An airplane descends to an airport under the following conditions: 9 minutes, 274°, 26 NM, 2.8 gallons. 13 minutes, 274°, 28 NM, 2.5 gallons. 13 minutes, 271°, 26 NM, 2.5 gallons. An airplane departs an airport under the follow ing conditions: 14 minutes, 234°, 26 NM, 3.9 gallons. 17 minutes, 224°, 36 NM, 3.7 gallons. 17 minutes, 242°, 31 NM, 3.5 gallons. An airplane departs an airport under the follow ing conditions: 14 minutes, 128°, 35 NM, 3.2 gallons. 16 minutes, 132°, 41 NM, 3.7 gallons. 16 minutes, 128°, 32 NM, 3.8 gallons. GIVEN: Pressure altitude............................................ 12,000 ft True air temperature .......................................... +50°F From the conditions given, the approximate density altitude is. 11,900 feet. 14,130 feet. 18,150 feet. GIVEN: Pressure altitude.............................................. 5,000 ft True air temperature .......................................... +30°C From the conditions given, the approximate density altitude is. 7,200 feet. 7,800 feet. 9,000 feet. GIVEN: Pressure altitude.............................................. 6,000 ft True air temperature .......................................... +30°F From the conditions given, the approximate density altitude is. 9,000 feet. 5,500 feet. 5,000 feet. GIVEN: Pressure altitude.............................................. 7,000 ft True air temperature .......................................... +15°C From the conditions given, the approximate density altitude is. 5,000 feet. 8,500 feet. 9,500 feet. GIVEN: True course ..........................................................105° True heading ........................................................085° True airspeed .....................................................95 kts Groundspeed ......................................................87 kts Determine the wind direction and speed. 020° and 32 knots. 030° and 38 knots. 200° and 32 knots. GIVEN: True course ..........................................................345° True heading ........................................................355° True airspeed .....................................................85 kts Groundspeed ......................................................95 kts Determine the wind direction and speed. 095° and 19 knots. 113° and 19 knots. 238° and 18 knots. GIVEN: Distance off course ............................................... 9 mi Distance flown .................................................... 95 mi Distance to fly ................................................... 125 mi To converge at the destination, the total correction angle would be. 4°. 6°. 10°. |




