Term
| How is the landing gear system controlled and actuated? |
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Definition
| Electrically controlled and hydraulically actuated |
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Term
| How is the main gear held in the retracted position? |
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Definition
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Term
| Can you always mute the gear warning horn? |
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Definition
| No, if the flaps are beyond 25 degrees and the gear is not down and locked |
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Term
| The gear warning horn will sound when flaps are extended past how many degrees with all the gear not down and locked? |
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Definition
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Term
| After an emergency gear extension, what indication will you see on the gear position lights? |
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Definition
| Three green and two red lights as the main gear doors will remain open |
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Term
| Name five systems that will be affected when the airplane lands and closes a squat switch? |
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Definition
-Spoilers/spoilerons-usable on ground with AUG AIL light on
-Nose wheel steering
-Thrust reversers
-Takeoff trim light
-Mach trim test
-Generator load limit-320 Amps on ground
-Windshield heat-low limit thermostats (215 degrees F)
-Pressurization valves (outflow/safety) opens
-Hour meter |
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Term
| If all three green lights were burned out, how could you tell whether the gear is down and locked? |
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Definition
-Landing lights for each respective main gear
-Engine sync light will illuminate when the nose gear is locked down
-Red gear inboard door lights illuminated and went out
-nose unsafe illuminated and went out
-No horns with thrust levers at idle or flaps extended beyond 25 degrees |
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Term
| What is the normal charge on the emergency bottle? |
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Definition
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Term
| What is connected to the Right Landing Gear Squat Switch? |
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Definition
Right Stall
Inboard anti-skid
Gear |
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Term
| What is connected to the Left Landing Gear Squat Switch? |
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Definition
Left Stall
Outboard anit-skid
Gear |
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Term
| What is connected to the Squat Switch Relay Panel? |
|
Definition
-Nose wheel steering - disabled in flight
-Spoilers/spoilerons-monitor system disabled on ground, slows deployment rate in air
-Anti-skid: brakes disabled in flight
-Stall warning test-disabled in flight
-Cabin pressurization-outflow valve open on ground, CAB ALT(510) disabled on ground
-Takeoff trim light-disabled in flight
-Generator load limit (SN 148 and above)- single generator limiting on ground
-Mach trim test- disabled in flight, will reset system
-Mach overspeed/stick puller- not disabled in flight on FC200
-Windshield heat sensor- Hi/LO limits
-Hour meter- disabled on ground
-Thrust reversers- disabled in flight |
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