Transcript #3259. What is pressure altitude? A- The indicated altitude corrected for position and installation error. B- The altitude indicated when the barometric pressure scale.

#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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#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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#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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#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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#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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#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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#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.
3-42a
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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.
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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.
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