1. Aviation Seminars1 #3259. 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.

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4. Aviation Seminars4 #3294. Determine the density altitude for these conditions:Altimeter setting 29.25, Runway tempture +81 F, Airport elevation 5,250 MSL. (See Figure 8) A-4600 feet MSL. B-5877 feet MSL. C-8,500 feet MSL.

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7. Aviation Seminars7 #3684.Determine the maximum wind velocity for a 45 degree crosswind if the maximum crosswind component for the airplane is 25 knots. Use fig 37. A- 25 knots. B- 29 knots. C- 35 knots.

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10. Aviation Seminars10 #3686. With a reported wind of north at 20 knots, which runway (6, 29, or 32) is acceptable for an airplane with a 13-knot max crosswind component? Fig 37. A- Runway 6. B- Runway 29. C- Runway 32.

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13. Aviation Seminars13 #3707. What is the approximate ground roll distance for takeoff under the following conditions?Use fig. 41. OAT 100 F. Pressure alt. 2,000 ft. Takeoff wt 2,750 lb. Headwind – Calm. A- 1,150 feet. B- 1,300 feet.C- 1,800 feet.

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16. Aviation Seminars16 #5451. At 55 % power – cruise (lean) & 47 gallons of fuel, how much flight time would be available with a night VFR fuel reserve remaining?See Fig#8 A- 3 hours 8 minutes. B- 3 hours 22 minutes. C- 3 hours 43 minutes.

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19. Aviation Seminars19 Comm. 3-42a #5620. What is the total takeoff distance over a 50-ft. obstacle?(See fig 32.) Temperature 50 F. Pressure altitude Sea Level. Weight 2,700 lb. WindCalm. A- 550 feet. B- 650 feet. C- 750 feet.

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22. Aviation Seminars22 #3682. Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36 deg F higher than standard. See fig 36. A- 19.8” Hg.B- 20.8” Hg.C- 21.0” Hg.

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25. Aviation Seminars25 #3692. Determine the approximate total distance to land over a 50-foot obstacle.See fig 38. OAT….90 F Pres.. Alt….4,000 ft. Weight..2,800 lb. Headwind…10 kts. A- 1,525 feet. B- 1,950 feet. C- 1,775 feet.

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28. Aviation Seminars28 #5483. Using the maximum rate of climb, how much time would be required to climb to a pressure altitude of 8,000 ft.? Use fig 13. Weight 4,000 lb.Airport press alt. 2,000 ft. Temp. 32 C. A- 7 minutes. B- 8.4 minutes. C- 11.2 minutes. Comm.

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