Position + Warning Systems Flashcards
What unit in an anti-skid system generates the anti-skid warning signal?
The control unit.
How is the pilot alerted that an anti-skid system has automatically returned to a manual brake system?
By a warning light.
What is the significance of an anti-skid warning?
The system is off or has failed.
By what usual means does the stall warning system in a small aircraft alert the pilot of an impending stall?
An audible alert, and/or warning light.
What devices are used to provide warnings for a retractable landing gear system?
A horn or other aural device, and a red warning light or lights
How can a pilot determine that the landing gear is down and locked?
A green light or lights, and/or another type of visual indicator.
Name at least two conditions that would activate a takeoff configuration warning system in a jet transport aircraft:
Incorrect leading or trailing edge flap position.
Stabilizer position.
Speed break not stowed.
What landing gear positions must be indicated by regulations?
Down and locked.
Up and locked.
Under what conditions will a landing gear aural warning sound?
When the throttle is retarded and landing gear is not down and locked.
How does a takeoff configuration warning differ from a landing gear warning?
Takeoff warnings are usually an intermittent horn while landing gear warnings are steady.
What is the function of a mock airspeed warning system?
To alert the pilot that the never-exceed air speed limit has been reached or exceeded.
What systems are commonly used to activate the landing gear warning systems?
The throttles (thrust levers).
Wing flaps.
Why do airplanes with bleed air anti-icing of the wing leading edge have an anti-ice overheat light?
To indicate an over temperature condition, usually as a result of a break in the bleed air ducts. 
What warning system may be required when a nickel cadmium battery is installed in an aircraft?
A battery temperature monitoring system.
At what time would a check of a landing gears warning system normally be made?
During a landing gear retraction test.