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You have seen all the different laws and protections.
May be you wonder how to recover if extreme conditions cause the aircraft to
leave the protected envelope? (e.g. You have been flipped over by a very severe
turbulence)
Here is the answer. If the limits of Normal laws are exceeded, Abnormal
attitude laws become active. This is a safety feature to ensure that the flight
control computers will never prevent the pilots recovering from an abnormal inflight
attitude.
The flight control laws operate in Alternate law without protections and
stabilities except for load factor protection.
After recovery, controls remain in Alternate law without protections but with
auto trim. There is no reversion to Direct law when the gear is extended.
After all theses emotions, you will now see the Normal operation modules...
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FLIGHT CONTROLS MENU Reconfiguration Laws 30/29
LLIISSTTOOFFSSUUBBJJEECCTTSS
EXIT
AUDIO GLOSSARY FCOM
RETURN
AALLTTEERRNNAATTEELLAAWWSS
DDIIRREECCTTLLAAWW
MMEECCHHAANNIICCAALLBBAACCKKUUPP
SSUUMMMMAARRYY
AABBNNOORRMMAALLAATTTTIITTUUDDEELLAAWW
FLIGHT CONTROLS MENU Summary 1/60
FLIGHT CONTROLS MENU
Summary 2/60
EECCAAMFF//CCTTLL ppaaggee ((SSuurrffaacceess))
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
AILERON & ELEVATOR INDICATION
SPOILER INDICATION
RUDDER INDICATION
FLIGHT CONTROLS MENU
Summary 3/60
The movements are
symbolized by a green
index moving in front
of a white scale.
The index becomes
amber in case of
failure of both
hydraulic actuators.
Neutral position in
clean configuration.
Neutral position
when flaps are
extended and of 5
degree aileron drop.
EECCAAMFF//CCTTLL ppaaggee ((SSuurrffaacceess))
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
AILERON & ELEVATOR INDICATION
RUDDER INDICATION
SPOILER INDICATION
FLIGHT CONTROLS MENU
Summary 4/60
EECCAAMFF//CCTTLL ppaaggee ((SSuurrffaacceess))
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
SPOILER INDICATION
Deployed by
more than 2.5
degrees.
Retracted.
Faulty when
deflected.
Faulty when
retracted or
inhibited.
AILERON & ELEVATOR INDICATION
RUDDER INDICATION
FLIGHT CONTROLS MENU
Summary 5/60
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
Normally displayed in green.
Rudder symbol and scale become amber in
case of low pressure in all hydraulic circuits.
Rudder travel limiters at high speed are
indicated by white dashes on the rudder scale.
EECCAAMFF//CCTTLL ppaaggee ((SSuurrffaacceess))
AILERON & ELEVATOR INDICATION
SPOILER INDICATION
RUDDER INDICATION
FLIGHT CONTROLS MENU
Summary 6/60
EECCAAMFF//CCTTLL ppaaggee ((CCoomppuutteerrss && TTrriim))
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
COMPUTER INDICATION
PITCH TRIM INDICATION
RUDDER TRIM INDICATION
FLIGHT CONTROLS MENU
Summary 7/60
Normally in
green.
Becomes amber
in case of
computer failure,
switched OFF or
both FCDC failed.
EECCAAMFF//CCTTLL ppaaggee ((CCoomppuutteerrss && TTrriim))
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
COMPUTER INDICATION
RUDDER TRIM INDICATION
PITCH TRIM INDICATION
FLIGHT CONTROLS MENU
Summary 8/60
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
EECCAAMFF//CCTTLL ppaaggee ((CCoomppuutteerrss && TTrriim))
RUDDER TRIM INDICATION
Normally blue.
Becomes amber
if rudder trim reset
has failed.
COMPUTER INDICATION
PITCH TRIM INDICATION
FLIGHT CONTROLS MENU
Summary 9/60
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
EECCAAMFF//CCTTLL ppaaggee ((CCoomppuutteerrss && TTrriim))
PITCH TRIM INDICATION
Normally in
white.
Becomes amber
if case of pitch
trim jam.
Normally in
green.
Becomes amber
in case of failure
of both hydraulic
actuators.
COMPUTER INDICATION
RUDDER TRIM INDICATION
FLIGHT CONTROLS MENU
Summary 10/60
EECCAAMFF//CCTTLL ppaaggee ((HHyyddrraauulliiccss)) SPOILER HYDRAULIC INDICATION
Seelleecctt aannyy yyeelllloow bbuuttttoonn ffoorr rreevviieew..
PITCH TRIM HYDRAULIC INDICATION
RUDDER HYDRAULIC INDICATION
AILERON & ELEVATOR HYD INDICATION
FLIGHT CONTROLS MENU
Summary 11/60
Normally in green.
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