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┃ A~7-~'M" A321 ┃FLAPS AND SLATS ┃SEQ 001 ┃REV 35 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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CONFIGURATIONS
The FLAPS lever has five positions ~ O, 1,
Two configurations correspond to position
The pilot selects these as follows ~
*
2, 3 and FULL.
1 ~ Configuration 1 and Configuration 1 + E
AS ~< 100KT AS _> IOOK"I"
A/S > 210KT*
AS ~< 210KT AS ~ 210KT
When Configuration 1 + F is selected, the flaps retract to 0~ automatically at 210
knots (before the airspeed reaches VFE).
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.27.50 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I FLIFLAPSOANDOSLATS ┃SEQ 001 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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ALPHA/SPEED LOCK FUNCTION (SLATS)
This function inhibits slat retraction at high angles of attack and low speeds.
The SFCCs use corrected angle-of-attack (alpha) or airspeed information from the air data
inertial reference units (ADIRUs) to key the inhibition of slat retraction.
If alpha exceeds 8.6~ or the airspeed falls below 148 knots, retraction from position 1 to
position 0 is inhibited.
The inhibition is removed when alpha falls below 7.6~ or when the speed exceeds 154
knots.
This function is not active if :
- Alpha exceeds 8.6~ or the airspeed falls below 148 knots after the pilot has moved the
lever to 0.
- The aircraft is on the ground with its speed less than 60 knots.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I -Z A318 ┃FLIGHT CONTROLS ┃1.27.50 P 5 ┃
┃ ~ ~ ,, ~I~ A319 ┃ ┃ ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(113)
