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Showing results 291 - 300 of 969 total.
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2.3.2.8.4.A.1
PAR PGL PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H314
In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate
A) a turn toward the south.
B) a turn momentarily.
*C) correctly when on a north or south heading.
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Modified: 3/5/2004 kip
Comments: 1
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2.3.2.8.5.A.1
PGL
Knowledge Code: H314
In the Northern Hemisphere, if a glider is accelerated or decelerated, the magnetic compass will normally indicate
A) a turn toward south while accelerating on a west heading.
*B) correctly only when on a north or south heading.
C) a turn toward north while decelerating on an east heading.
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Modified: 3/5/2004 kip
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2.3.2.8.6.A.1
PAR PGL PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H314
During flight, when are the indications of a magnetic compass accurate?
A) During turns if the bank does not exceed 18°.
B) As long as the airspeed is constant.
*C) Only in straight-and-level unaccelerated flight.
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Modified: 3/5/2004 kip
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2.3.2.8.7.A.1
PAR PGL RPA PAT
Knowledge Code: H940
An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be
A) stalling at higher-than-normal airspeed.
B) a longer takeoff run.
*C) difficulty in recovering from a stalled condition.
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Modified: 8/17/2004 kip
Comments: 2
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2.3.2.8.8.A.1
PAR PGL RPA PAT
Knowledge Code: H940
Loading an airplane to the most aft CG will cause the airplane to be
*A) less stable at all speeds.
B) less stable at slow speeds, but more stable at high speeds.
C) less stable at high speeds, but more stable at low speeds.
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Modified: 4/12/2007 HABpilot
Comments: 0
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2.3.2.8.9.A.1
PAR PGL PBG PBH PLA PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H942
If the outside air temperature (OAT) at a given altitude is warmer than standard, the density altitude is
A) equal to pressure altitude.
B) lower than pressure altitude.
*C) higher than pressure altitude.
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Modified: 4/28/2007 HABpilot
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2.3.2.9.0.A.1
PAR PGL PBG PBH PLA PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H945
Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?
A) Low temperature, low relative humidity, and low density altitude.
B) High temperature, low relative humidity, and low density altitude.
*C) High temperature, high relative humidity, and high density altitude.
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Modified: 4/28/2007 HABpilot
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2.3.2.9.1.A.1
PAR PGL PLA PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H945
What effect does high density altitude have on aircraft performance?
A) It increases engine performance.
*B) It reduces climb performance.
C) It increases takeoff performance.
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Modified: 4/28/2007 HABpilot
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2.3.2.9.2.A.1
PAR PGL PBG PBH PLA PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H946
(Refer to figure 8.) What is the effect of a temperature increase from 25 to 50 °F on the density altitude if the pressure altitude remains at 5,000 feet?
A) 1,200-foot increase.
B) 1,400-foot increase.
*C) 1,650-foot increase.
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Modified: 4/28/2007 HABpilot
Comments: 0
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2.3.2.9.3.A.1
PAR PBG PBH PLA PRG PRH RPA RPG RPH PAT PGT PHT
Knowledge Code: H945
(Refer to figure 8.) Determine the pressure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22 at standard temperature.
*A) 2,991 feet MSL.
B) 3,010 feet MSL.
C) 2,913 feet MSL.
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Modified: 8/18/2004 kip
Comments: 13
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Showing results 291 - 300 of 969 total.
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