Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for...

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Aviation Seminars 1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated when the b arometric pressure scale is set to 2 9.92. C- The indicated altitude corrected for nonstandard temperature and pres sure.

Transcript of Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for...

Page 1: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

Aviation Seminars 1

#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.

Page 2: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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Page 4: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

Aviation Seminars 4

#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.

Page 5: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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Page 7: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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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Page 10: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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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Page 13: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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.

Page 14: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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.

Page 17: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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Page 19: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

Aviation Seminars 19 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.Wind Calm.A- 550 feet.B- 650 feet.C- 750 feet.

Page 20: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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Page 22: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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.

Page 23: Aviation Seminars1 #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated.

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#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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#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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