ASA Postion / Warning sys Exam with verified detailed solutions
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1 (8934) - The purpose of antiskid generators is to - ✔✔C- measure wheel rotational
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speed and any speed changes.
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2 (8935) - In a brake antiskid system, when an approaching skid is sensed, an
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electrical signal is sent to the skid control valve which - ✔✔B- relieves the hydraulic
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pressure on the brake. || || ||
3 (8936) - An antiskid system is - ✔✔B- an electrohydraulic system.
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4 (8937) - Antiskid braking systems are generally armed by - ✔✔B- a switch in the
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cockpit.
5 (8938) - A typical takeoff warning indication system, in addition to throttle setting,
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monitors the position of which of the following? - ✔✔B- Elevators, speed brake, flaps,
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and stabilizer trim.
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6 (8939) - The primary purpose of a takeoff warning system is to alert the crew that a
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monitored flight control is not properly set prior to takeoff. The system is activated by
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- ✔✔C- a thrust lever.
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7 (8940) - (1) An airspeed indicator measures the differential between pitot and static
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air pressures surrounding the aircraft at any moment of flight.(2) An airspeed
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indicator measures the differential between pitot and cabin air pressures at any
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Regarding the above statements,moment of flight. - ✔✔C- only No. 1 is true.
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8 (8941) - The angle-of-attack detector operates from differential pressure when the
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airstream - ✔✔B- is not parallel to the true angle of attack of the aircraft.
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, 9 (8942) - (1) When an airplane is slowed below approximately 20 MPH, the antiskid
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system automatically deactivates to give the pilot full control of the brakes for
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maneuvering and parking.(2) An antiskid system consists basically of three
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components; wheel speed sensors, control box, and Regarding the above || || || || || || || || || ||
statements,control valves. - ✔✔C- both No. 1 and No. 2 are true. || || || || || || || || || || ||
10 (8943) - In an antiskid system, wheel skid is detected by - ✔✔A- an electrical
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sensor.
11 (8944) - Which of the following functions does a skid control system perform?1.
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Normal skid control.2. Normal braking.3. Fail safe protection.4. Locked wheel skid
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control.5. Touchdown protection.6. Takeoff protection. - ✔✔B- 1, 3, 4, 5.
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12 (8945) - In the air with the antiskid armed, current cannot flow to the antiskid
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control box because the landing gear - ✔✔A- squat switch is open.
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13 (8946) - At what point in the landing operation does normal skid control perform
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its function? - ✔✔A- When wheel rotation deceleration indicates an impending skid.
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14 (8947) - (1) An antiskid system is designed to apply enough force to operate just
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below the skid point.(2) A warning lamp lights in the cockpit when the antiskid
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system is turned off or if there is a system failure.Regarding the above statements, -
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✔✔C- both No. 1 and No. 2 are true.
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15 (8948) - When an airplane's primary flight control surfaces are set for a particular
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phase of flight, such as landing or takeoff, the corresponding control-surface indicating
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system will show - ✔✔C- trim position.
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1 (8934) - The purpose of antiskid generators is to - ✔✔C- measure wheel rotational
|| || || || || || || || || || || || || || ||
speed and any speed changes.
|| || || ||
2 (8935) - In a brake antiskid system, when an approaching skid is sensed, an
|| || || || || || || || || || || || || || ||
electrical signal is sent to the skid control valve which - ✔✔B- relieves the hydraulic
|| || || || || || || || || || || || || || ||
pressure on the brake. || || ||
3 (8936) - An antiskid system is - ✔✔B- an electrohydraulic system.
|| || || || || || || || || || ||
4 (8937) - Antiskid braking systems are generally armed by - ✔✔B- a switch in the
|| || || || || || || || || || || || || || || ||
cockpit.
5 (8938) - A typical takeoff warning indication system, in addition to throttle setting,
|| || || || || || || || || || || || || ||
monitors the position of which of the following? - ✔✔B- Elevators, speed brake, flaps,
|| || || || || || || || || || || || || ||
and stabilizer trim.
|| ||
6 (8939) - The primary purpose of a takeoff warning system is to alert the crew that a
|| || || || || || || || || || || || || || || || || ||
monitored flight control is not properly set prior to takeoff. The system is activated by
|| || || || || || || || || || || || || || ||
- ✔✔C- a thrust lever.
|| || || ||
7 (8940) - (1) An airspeed indicator measures the differential between pitot and static
|| || || || || || || || || || || || || ||
air pressures surrounding the aircraft at any moment of flight.(2) An airspeed
|| || || || || || || || || || || ||
indicator measures the differential between pitot and cabin air pressures at any
|| || || || || || || || || || || ||
Regarding the above statements,moment of flight. - ✔✔C- only No. 1 is true.
|| || || || || || || || || || || ||
8 (8941) - The angle-of-attack detector operates from differential pressure when the
|| || || || || || || || || || || ||
airstream - ✔✔B- is not parallel to the true angle of attack of the aircraft.
|| || || || || || || || || || || || || ||
, 9 (8942) - (1) When an airplane is slowed below approximately 20 MPH, the antiskid
|| || || || || || || || || || || || || || ||
system automatically deactivates to give the pilot full control of the brakes for
|| || || || || || || || || || || || ||
maneuvering and parking.(2) An antiskid system consists basically of three
|| || || || || || || || || ||
components; wheel speed sensors, control box, and Regarding the above || || || || || || || || || ||
statements,control valves. - ✔✔C- both No. 1 and No. 2 are true. || || || || || || || || || || ||
10 (8943) - In an antiskid system, wheel skid is detected by - ✔✔A- an electrical
|| || || || || || || || || || || || || || || ||
sensor.
11 (8944) - Which of the following functions does a skid control system perform?1.
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Normal skid control.2. Normal braking.3. Fail safe protection.4. Locked wheel skid
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control.5. Touchdown protection.6. Takeoff protection. - ✔✔B- 1, 3, 4, 5.
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12 (8945) - In the air with the antiskid armed, current cannot flow to the antiskid
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control box because the landing gear - ✔✔A- squat switch is open.
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13 (8946) - At what point in the landing operation does normal skid control perform
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its function? - ✔✔A- When wheel rotation deceleration indicates an impending skid.
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14 (8947) - (1) An antiskid system is designed to apply enough force to operate just
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below the skid point.(2) A warning lamp lights in the cockpit when the antiskid
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system is turned off or if there is a system failure.Regarding the above statements, -
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✔✔C- both No. 1 and No. 2 are true.
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15 (8948) - When an airplane's primary flight control surfaces are set for a particular
|| || || || || || || || || || || || || || ||
phase of flight, such as landing or takeoff, the corresponding control-surface indicating
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system will show - ✔✔C- trim position.
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