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B X
134..[Refer to Figures 4-28 and 4-29.] What approach speed
and ground roll will be needed when landing at a weight of
140,000 pounds if flaps are not used?
A.138 knots and 3,900 feet.
B.153 knots and 2,900 feet.
C.183 knots and 2,900 feet.
C X
135..[Refer to Figures 4-35 and 4-36.] What are descent fuel
and distance under Operating Conditions S-4?
A.1,490 pounds, 118 NAM.
B.1,400 pounds, 110 NAM.
C.1,430 pounds, 113 NAM.
C X
136..[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
137..[Refer to Figures 4-35 and 4-36.] What are descent time
and distance under Operating Conditions S-1?
A.24 minutes, 118 NAM.
B.26 minutes, 125 NAM.
C.25 minutes, 118 NAM.
B X
138..[Refer to Figures 4-35 and 4-36.] What are descent time
and distance under Operating Conditions S-2?
A.24 minutes, 109 NAM.
B.25 minutes, 125 NAM.
C.23 minutes, 118 NAM.
C X
139..[Refer to Figures 4-46, 4-47 and 4-48.] What are the fuel
requirements from Chicago Midway Airport to Greater Buffalo
Intl?
A.2,224 pounds.
B.1,987 pounds.
C.1,454 pounds.
A X
140..[Refer to Figures 4-49, 4-50,4-51,4-52,4-53, and 4-54.]
What is the ETE at .78 Mach?
A.1 hours 08 minutes.
B.1 hours 02 minutes.
C.1 hours 05 minutes.
A X
141..[Refer to Figures 4-49, 4-50,4-51,4-52,4-53, and 4-54.]
What is the ETE at .80 Mach?
A.1 hours 02 minutes.
B.1 hours 04 minutes.
C.1 hours 07 minutes.
C X
142..[Refer to Figures 4-50,4-51,4-52,4-53, and 4-54.] What
is the total fuel required at .78 Mach?
A.22,140 pounds.
B.22,556 pounds.
C.22,972 pounds.
B X
143..[Refer to Figures 4-50,4-51,4-52,4-53, and 4-54.] What
is the total fuel required at .80 Mach?
A.22,836 pounds.
B.22,420 pounds.
C.22,556 pounds.
B X
144..A commercial operator plans to ferry a large,
four-engine, reciprocating-engine-powered airplane from one
facility to another to repair an inoperative engine. Which
is an operational requirement for the three-engine flight?
A.The gross weight at takeoff may not exceed 75 percent of
the maximum certificated gross weight.
B.Weather conditions at the takeoff and destination airports
must be VFR.
C.The computed takeoff distance to reach V1 must not exceed
70 percent of the effective runway length.
B X
145..A definition of the term "viscous hydroplaning" is where
A.the airplane rides on standing water.
B.a film of moisture covers the painted or rubber-coated
portion of the runway.
C.the tires of the airplane are actually riding on a mixture
of steam and melted rubber.
B X
146..An outside air pressure decreases, thrust output will
A.increase due to greater efficiency of jet aircraft in thin
air.
B.remain the same since compression of inlet air will
compensate for any decrease in air pressure.
C.decrease due to higher density altitude.
C X
147..At what minimum speed (rounded off) could dynamic
hydroplaning occur on main tires having a pressure of 100 PSI?
A.90 knots.
B.96 knots.
C.110 knots.
A X
148..At what minimum speed (rounded off) could dynamic
hydroplaning occur on main tires having a pressure of 110 PSI?
A.90 knots.
B.95 knots.
C.100 knots.
B X
149..At what minimum speed (rounded off) could dynamic
hydroplaning occur on main tires having a pressure of 121 PSI?
A.90 knots.
B.96 knots.
C.110 knots.
B X
150..At what speed, with reference to L/DMAX, does maximum
range for a jet airplane occur?
A.A speed less than that for L/DMAX.
B.A speed equal to that for L/DMAX.
C.A speed greater than that for L/DMAX.
C X
151..At what speed, with reference to L/DMAX, does maximum
rate-of-climb for a jet airplane occur?
A.A speed greater than that for L/DMAX.
B.A speed equal to that for L/DMAX.
C.A speed less than that for L/DMAX.
B X
152..Compared to dynamic hydroplaning, at what speed does
viscous hydroplaning occur when landing on a smooth, wet
runway?
A.At approximately 2.0 times the speed that dynamic
hydroplaning occurs.
B.At a lower speed than dynamic hydroplaning.
C.At the same speed as dynamic hydroplaning.
B X
153..Equivalent shaft horsepower (ESHP) of a turboprop engine
is a measure of
A.turbine inlet temperature.
B.shaft horsepower and jet thrust.
C.propeller thrust only.
　
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