LearJet Training Resources
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Part 135 Training Resources
1.
You may not operate if water and/or slush accumulation on the runway
A.
equals 3/4"
B.
exceeds 1/4"
C.
exceeds 3/4"
D.
exceeds 1-3/4"
2.
If the Dry Part 91 Landing Distance is 2943'
A.
the part 135 landing distance will be 4905'
B.
the part 135 landing distance will be 9405'
C.
the part 135 landing distance will be 4509'
D.
the part 135 landing distance will be 4095'
3.
If the Dry Part 91 Landing Distance is 2943'
A.
the Wet Part 135 landing distance will be 6541'
B.
the Wet Part 135 landing distance will be 5461'
C.
the Wet Part 135 landing distance will be 4561'
D.
the Wet Part 135 landing distance will be 5641'
4.
The following requirements must be met to accept a LAHSO clearance:
A.
T
hrust reversers (if installed), anti skid, and spoilers are all operational.
B.
No MEL weight penalties which reduce the landing runway weight (increase the landing roll). Available landing distance is verified with the tower controller.
C.
Clear, dry runways.
D.
All of the above.
5.
In determining takeoff performance, weights, distances, and flight paths must be analyzed for the
A.
runway to be used at the time of takeoff.
B.
runway to be used, the elevation of the airport, the effective runway gradient, the ambient temperature and wind component at the time of takeoff.
C.
runway to be used, the elevation of the airport, the effective runway gradient, and wind component at the time of takeoff.
D.
runway to be used, the elevation of the airport, and the wind component at the time of takeoff.
6.
Go-around power or thrust setting means
A.
the thrust setting identified in the performance data.
B.
the power identified in the performance data.
C.
the maximum allowable in-flight power or thrust setting identified in the performance data.
D.
the maximum allowable in-flight power or thrust setting identified in the operations specifications.
7.
Alternate airports must be selected based on the weight anticipated at the time of arrival,
A.
so that the aircraft can be brought to a full stop landing within 60 percent of the effective length of the runway.
B.
so that the aircraft can be brought to a full stop landing within 50 percent of the effective length of the runway.
C.
so that the aircraft can be brought to a full stop landing within 115% of the effective length of the runway.
D.
so that the aircraft can be brought to a stop landing within 160 percent of the effective length of the runway.
8.
The second segment begins at
A.
the end of the runway.
B.
the end of the stopway and continues to a height above the runway of 15 feet.
C.
the end of the runway plus or minus 1,500 feet and V2 speed.
D.
the end of gear retraction and continues to a height above the runway of 1,500 feet and V2 speed.
9.
Flaps 10 Overspeed
A.
Provides the maximum hot-day, high altitude performance that balances accelerate-stop distance, brake energy, and V2 speeds. Lear 25 Flight Manual Page 4-28
B.
Provides maximum balance between accelerate-stop distance, accelerate-go distance, landing distance, missed approach speeds, brake energy, and V2 speeds.
C.
Provides high altitude performance, V1, Vr and V2 speeds.
D.
Provides hot-day, high altitude performance that balances accelerate-stop distance.
10.
A Runway is considered to be wet when it has a shiny appearance due to a thin layer of water on it, but without significant areas of standing water. A runway with greater than 0.125 inch (3 mm) of standing water
A.
would not be a contaminated runway
B.
would not affect the V1 speed
C.
would require that a new V1 speed be calculated
D.
would be a contaminated runway
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