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┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
The FADEC computes the thrust rating limit for each thrust lever position, as shown below.
If the thrust lever is set in a detent, the FADEC selects the rating limit corresponding to this
detent.
If the thrust lever is set between two detents, the FADEC selects the rating limit
corresponding to the higher detent.
RATING LIMITS :
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┳━━━━━━━━━━━┓
┃J ~=~-C A318 ┃ POWER PLANT ┃1.70.30 P 3 ┃
┃ a= a= ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 005 J ┃J REV 23 ┃
┃ A~7-~'M" A321 ┃THRUST CONTROL SYSTEM ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━┻━━━━━┻━━━━━┛
MANUAL MODE
The engines are in the manual mode provided the A/-rHR function is :
- not armed or
- armed and not active (thrust lever not in the A/-I-HR operating range and no alpha floor).
In these conditions, each engine is controlled by the position of its thrust lever.
The pilot controls thrust by moving the thrust lever between the IDLE and TOGA positions.
Each position of the thrust lever within these limits corresponds to an NI.
When the thrust lever is in a detent, the corresponding N1 is equal to the N1 rating limit
computed by the FADEC for that engine.
THRUST
┏━┳━━━━┳━━━━━━━━━━━┳━━┓
┃ ┃ ┃ ┃ F ┃
┃ ┃ ┣━━━┳━━━━━┳━╋━━┫
┃ ┃ u. ┃ ┃ ┃ ┃ ┃
┃ ┃ ┃ ┣━┳━┳━╋━╋━━┫
┃ ┃ z ┃ ┃ ┃ ┃ ┃ ┃ ┃
┃ ┃ b-i ┃ ┃ ┃ ┃ ┃ ┃ ┃
┃ ┃ I- ┃ ┃ ┃ ┃ ┃ ┃ ┃
┃ ┃ z ┃H ┃ ┃ ┃ ┃ ┃ ┃
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual5(157)
