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have been neutralized
A.-Negative static stability
B.-Positive static stability
C.-Negative dynamic stability
A X
433..(Refer to Figure 6-2) If the pilot has identified IDK on the
ILS/DME Rwy 36L straight-in land at CAPITAL, what height
above the airport does a Category B aircraft descend to in
IMC?
A.308 feet.
B.193 feet.
C.200 feet.
B X
434..[Refer to Figures 4-35 and 4-36.] What are descent fuel
and distance under Operating Conditions S-5?
A.1,420 pounds, 97 NAM.
B.1,440 pounds, 102 NAM.
C.1,390 pounds, 92 NAM.
A X
435..(Refer to Figure 2-3) On which radial is the aircraft as
indicated by the NO.1 NAV?
136
A.R-175
B.R-165
C.R-345
C X
436..[Refer to Figures 4-22 and 4-24.] What is the go-around
EPR for Operating Conditions L-1?
A.2.01 EPR.
B.2.03 EPR.
C.2.04 EPR.
B X
437..To avoid the wingtip vortices of a departing jet airplane
during takeoff, the pilot should
A. Lift off at a point well past the jet airplane's flight path.
B. Climb above and stay upwind of the jet airplane's flight
path.
C. Remain below the flight path of the jet airplane.
B X
438..What effect would a change in ambient temperature or air
density have on gas-turbine-engine performance?
A.As air density decreases, thrust increases.
B.As temperature increases, thrust increases.
C.As temperature increases, thrust decreases.
C X
137
439..If an ATC controller assigns a speed, which is too fast for
the aircraft's operating limitation under the existing
circumstance, what should the pilot do?
A. increase speed to the assigned speed.
B. increase speed to the maximum speed at that circumstance.
C. advise ATC of the speed that will be used and expect the
controller issue new speed.
C X
440..What is the principal advantage of a sweepback design
wing over a straight wing design?
A.The critical Mach number will increase significantly.
B.Sweepback will increase changes in the magnitude of force
coefficients due to compressibility.
C.Sweepback will accelerate the onset of compressibility
effect.
A X
441..[Refer to Figure 4-26.] How many feet will remain after
landing on a 6,000-foot wet runway with reversers
inoperative at 110,000 pounds gross weight?
A.2,100 feet.
B.2,650 feet.
C.3,000 feet.
C X
138
442..(Refer to Figure 2-3) What is the lateral displacement of
the aircraft in nautical miles from the radial selected on the
No.1 NAV?
A.5.0NM
B.7.5NM
C.10.0NM
A X
443..(Refer to Figure 6-6) Using an average ground speed of 140
knots, what minimum indicated rate of climb must be
maintained to meet the required climb gradient of 4.6% to
4,930 as specified on the SID?
A.690 feet/minute.
B.644 feet/minute.
C.600 feet/minute.
B X
444..In the SIGMET 8 of the Figure 3, which station predict the
dangerous weather at first
A. ZULS
B. ASSS
C. ZUUU
A X
445..Which would most likely result in hyperventilation?
A.A stressful situation causing anxiety.
139
B.The excessive consumption of alcohol.
C.An extremely slow rate of breathing and insufficient
oxygen.
A X
446..(Refer to Figure 6-4) What is the takeoff minimum for Rwy
17 at PUDONG that applies to an aircraft with 2 propelled
engines?
A.VIS 1,600m.
B.RVR 200m.
C.RVR 250m.
A X
447..Which condition is present when a local of air is stable?
A. The parcel of air resists convection.
B. The parcel of cannot be forced uphill.
C. As the parcel of air moves upward, its temperature becomes
warmer than the surrounding air.
A X
448..[Refer to Figure 4-25.] What is the transition distance
when landing on a dry runway at a gross weight of 125,000
pounds?
A.1,200 feet.
B.850 feet.
C.400 feet.
140
C X
449..What is the reason for variations in geometric pitch
along a propeller or rotor blade?
A.It permits a relatively constant angle of attack along its
length when in cruising flight.
B.It prevents the portion of the blade near the hub or root
from stalling during cruising flight.
C.It permits a relatively constant angle of incidence along
its length when in cruising flight.
A X
450..Which documents are required to be carried aboard each
flag air carrier flight?
A.Dispatch release, flight plan, and weight and balance
release.
B.Load manifest, flight plan, and flight release.
C.Dispatch release, load manifest, and flight plan.
C X
　
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