Flight Controls Flashcards
How many Flap Control Units (FCU’s) are provided?
3
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What are the basic functions of the FCU’s?
Primary control
Secondary control
Indication and annunciation
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How man groups of leading flaps are provided, and how are they normally powered?
3
Pneumatically
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What are the two groups of trailing edge flaps, and how are they powered?
2
Hydraulically 1 & 4
How are opposite trailing edge flaps connected?
Mechanically
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What protection features do FCU’s provide for trailing edge flaps in primary mode?
FCU’s shut down Primary and Secondary Modes for the failed group.
Describe the function of the FCU’s in primary mode
Drive LE Pneumatically
Drive TE Hydraulically
Detect Asymmetry
Load Relief
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Describe the function of the FCU’s in secondary mode
If primary fails, secondary activates in symmetrical groups.
Driven by electric motors.
TE Flaps can upgrade to HYD when pressure is restored or fully UP if in secondary for other reasons.
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What happens if a primary control failure occurs in either the inboard or midspan leading edge flap group?
Both groups switch to secondary
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What happens if a failure occurs in a leading-edge flap group on one wing?
Both switch to secondary after a short delay.
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What happens immediately if a trailing edge asymmetry is detected?
Primary mode is immediately shut down and secondary mode is not used for the failed group.
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What EICAS advisory message displays if all three FCU’s fail in their control function?
FLAPS CONTROL
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How does the Flap Alternate Control mode work?
FCU’s are bypassed for a simplified control system on electric motors with no protection.
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Is there any asymmetry protection in alternate mode?
No
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State the actions that occur when the Alternate (ALTN) Flaps Arm switch is pushed
FCU’s are bypassed.
Alternate Flaps selector is armed.
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