R **ON A/C 151-199, 401-499,
(4) Rudder control The pedals mechanically control the rudder position. The maximum rudder deflection is plus or minus 30 deg limited by the TLU. The trim authority is plus or minus 25 deg and its deflection rate is 1 deg/s. The yaw orders from the roll normal law are sent to the yaw damper servo-actuators and added to the servocontrol mechanical input. Authority of these orders is given in the table below:
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-90-00Page 29 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------| V Cas (kts) | Less than or| 200 | 240 | 320 | 380 | | | equal to 140 | | | | | |----------------|--------------|-----------|-----------|-----------|---------| | | plus | plus | plus | plus | plus | | | or | or | or | or | or | | | minus | minus | minus | minus | minus | | Max. authority | 25 deg | 12 deg | 7.3 deg | 4 deg | 2.8 deg | -------------------------------------------------------------------------------The limitation of the rudder maximum deflection is given in the table
below (TLU activated): -------------------------------------------------------------------------------| V Cas (kts) | Less than | 200 | 240 | 320 | 380 | | | 140 | | | | | |----------------|--------------|-----------|-----------|-----------|---------| | | plus | plus | plus | plus | plus | | | or | or | or | or | or | | | minus | minus | minus | minus | minus | | Max. authority | 30 deg | 14.5 deg| 8.8 deg| 4.8 deg| 3.4 deg| -------------------------------------------------------------------------------
**ON A/C 301-399,
(4) Rudder control The pedals mechanically control the rudder position. The maximum rudder deflection is plus or minus 28 deg limited by the TLU. The trim authority is plus or minus 21 deg and its deflection rate is 1 deg/s. The yaw orders from the roll normal law are sent to the yaw damper servo-actuators and added to the servocontrol mechanical input. Authority of these orders is given in the table below:
-------------------------------------------------------------------------------| V Cas (kts) | Less than or| 200 | 240 | 320 | 380 | | | equal to 160 | | | | | |----------------|--------------|-----------|-----------|-----------|---------| | | plus | plus | plus | plus | plus | | | or | or | or | or | or | | | minus | minus | minus | minus | minus | | Max. authority | 21 deg | 10.8 deg | 6.6 deg | 3.6 deg | 2.4 deg | -------------------------------------------------------------------------------
The limitation of the rudder maximum deflection is given in the table below (TLU activated):
R 1EFF : 151-199, 301-399, 401-499, 1 27-90-00Page 30 1 1 Aug 01/05 1 1 1CES 1
R -------------------------------------------------------------------------------
R | V Cas (kts) | Less than | 200 | 240 | 320 | 380 |
R | | 160 | | | | |
R |----------------|--------------|-----------|-----------|-----------|---------|
R | | plus | plus | plus | plus | plus |
R | | or | or | or | or | or |
R | | minus | minus | minus | minus | minus |
R | Max. authority | 25 deg | 13 deg | 7.9 deg| 4.3 deg| 2.9 deg|
R -------------------------------------------------------------------------------
**ON A/C ALL
(5) Operation in normal conditions
The lateral laws are activated as described in the table.
Activation of flight/ground laws in lateral
-------------------------------------------------------------------------------
| | | NORMAL LAW | |
| PHASE | TRANSITION |-----------------------------| DISPLAY ON |
| | | GROUND LAW | FLIGHT LAW | PFD |
|---------------|------------|--------------|--------------|------------------|
| GROUND | | YES | | LATERAL |
| | | | DECREASED | | LOAD FACTOR |
| | | | AUTHORITY | | |
| | | | WITH INCREA-| | |
| | | | SED SPEED | | |
| | | | | | |
| | TAKE | | YAW DAMPING | | |
| | OFF | | | | |
| | | | | | |
| FLIGHT | FLIGHT AND | WASHED OUT | PHASED IN | SIDE SLIP |
| | | Theta > 8. | OVER 0.5s | OVER 0.5s | |
| | | | | | |
| | LANDING | | | | |
| | | | | | |
| GROUND | GROUND | PHASED IN | PHASED OUT | LATERAL LOAD |
| | | OVER 0.5s | OVER 0.5s | FACTOR |
| | | | | |
| | | YAW DAMPING | | |
-------------------------------------------------------------------------------
R **ON A/C 001-049, 052-099, 101-149, 201-299,
C. Speedbrake Function
(Ref. Fig. 011)
(1)
General The speedbrake function is ensured by the spoilers 2, 3 and 4 and the associated SECs. The speedbrake deflection order is dependent upon the speedbrake control lever position. Extension of the spoilers 2 is half the extension of the spoilers 3 and 4. The speedbrake order is combined with roll orders. In flight, when the aircraft speed is more than 315 knots or Mach
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