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┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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FADEC POWER SUPPLY
LGCIU
* SUPPLIED FOR 5 MINUTES
CCM ALL
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┃J -~ A318 ┃ POWER PLANT ┃1.70.30 P 1 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 105 J ┃J REV 23 ┃
┃ A~7-~'M" A321 ┃THRUST CONTROL SYSTEM ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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A FADEC dedicated to each engine controls thrust.
The pilot uses the thrust levers to set the thrust in manual mode, and the FMGS sets the
thrust in automatic mode.
The FADEC prevents the thrust from exceeding the limit for the thrust lever position in both
manual and automatic modes.
\
The thrust levers can only be moved manually.
They move over a sector that is divided into four operating segments.
The sector has five positions defined by detents or stops.
Thrust lever position is transmitted to the FADEC, which computes and displays the thrust
rating limit and the N1 for that Thrust Lever Angle (TLA).
Note ~ There is no reverse idle detent. When the pilot moves the/ever out of the idle stop
by pulling up the reverse/ever on the front of the thrust lever, he selects reverse
idle.
CCM ALL
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┃ ┃ ┃1.70.30 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I THRUSTECONTROL SYSTEM ┃SEQ 005 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
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AIRBUS A320 Flight Crew Operating Manual5(156)