A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(12)

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 1. General
_______ To accomplish the computations of laws and control loops, the flight controls computers use data from following components:
 -2 side stick controllers used for pitch and roll manual control (ELAC and SEC)
 -1 speedbrake control transducer unit used for SPD-BRK function and GND-SPLR function preselection (SEC).
 -
6 transducer units used: . one for yaw damper jacks position monitoring (FAC) . one for rudder position detection for surface position indication on ECAM CRT . two for rudder pedal position indication to deliver this information to ELACs . two for elevator control

 -
6 pressure switches used for monitoring the pressure in the three hydraulic systems (Ref. ATA 29) (ELAC and SEC).

 -3 pressure transducers used for monitoring of the hydraulic system pressure (ELAC).
 -2 throttle control units. Then components-delivered signals to the FADECs for engine control and to the SECs for ground spoiler function.
 2. Component Location
__________________
 (Ref. Fig. 001, 002, 003, 004, 005, 006)

 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 (Ref. Fig. 007)
R **ON A/C 151-199, 401-499,
 (Ref. Fig. 007A)

 Component Location
 Figure 001
 1EFF :  ALL  1  27-92-00 Page 2 
1  1  Feb 01/98
 1  1
 1CES  1

 

R R  Component Location Figure 002
 1EFF : 1 1 1CES  ALL  1 111 27-92-00 Page 3 May 01/04

 

R  Component Location Figure 003
 1EFF : 1 1 1CES  ALL  1 111 27-92-00 Page 4 Aug 01/04

 

R  Component Location Figure 004
 1EFF : 1 1 1CES  ALL  1 111 27-92-00 Page 5 Aug 01/04

 

R  Component Location Figure 005
 1EFF : 1 1 1CES  ALL  1 111 27-92-00 Page 6 Aug 01/04

 

R  Component Location Figure 006 
R 1EFF : 1 1 1CES  ALL  1 111 27-92-00 Page 7 Aug 01/04

 

 Component Location
 Figure 007

R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-92-00Page 8 1301-399, 1May 01/05 1 1 1CES 1

 Component Location Figure 007A 
R 1EFF : 1 1 1CES  151-199, 401-499,  1 111 27-92-00 Page 9 Aug 01/05

 

R **ON A/C ALL
R -------------------------------------------------------------------------------R FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA R I I I I DOOR I REF. R -------------------------------------------------------------------------------
R 4CE1 SSTU-ROLL CTL, CAPT R 4CE2 SSTU-ROLL CTL, F/O R 4CE3 SSTU-PITCH CTL, CAPT R 4CE4 SSTU-PITCH CTL, F/O R 7CE XDCR UNIT-SPD BRK CTL R 25CE1 XDCR UNIT-PEDAL POS, L R 25CE2 XDCR UNIT-PEDAL POS, R R 2CC XCDR UNIT-YAW DAMPER POS R 42WV XDCR UNIT-RUDDER POS R 49CE1 XDCR UNIT-ELEVATOR POS,L R 49CE2 XDCR UNIT-ELEVATOR POS,R R 12CE1 ACCLRM-1 R 12CE2 ACCLRM-2 R 12CE3 ACCLRM-3 R 12CE4 ACCLRM-4 R 10CE1 PRESSURE SWITCH-HYDRAULIC R 10CE2 PRESSURE SWITCH-HYDRAULIC R 10CE3 PRESSURE SWITCH-HYDRAULIC R 8KS1 CTL UNIT-THROTTLE, ENG 1 R 8KS2 CTL UNIT-THROTTLE, ENG 2 R 23CE1 ANN-SIDE STICK PRIORITY, CAPT R 23CE2 ANN-SIDE STICK PRIORITY, F/O
193VU 211 27-92-41 182VU 212 27-92-41 193VU 211 27-92-41 182VU 212 27-92-41 11VU 210 27-92-14 121 27-92-15 122 27-92-15 325 27-26-17 325 27-25-17 27-92-13 27-92-13 131 27-92-16 132 27-92-16 131 27-92-16 132 27-92-16 140 27-92-17 140 27-92-17 140 27-92-17 210 73-92-19 210 73-92-19 131VU 211 27-92-00 130VU 212 27-92-00

 3. Operation
_________
 A. Side Stick Controller (Ref. Fig. 008, 009, 010, 011, 012) Two side stick controllers are used for pitch and roll manual control one on the captain lateral console, another one on the first officer lateral console. The two side sticks are electrically coupled. The arm rest is fixed on the seat. General concept is a fail safe concept i.e. mainly that a single failure provides:
 -Neither total loss of artificial feel
 -Nor undetected uncontrolled pilot order.
 The hand grip includes 2 switches:

 -A/P disconnect pushbutton is used for:
 A/P disconnection in A/P mode
 Priority logic between sticks in manual mode

 -Push-to-talk button.
 The red light of the ANN-SIDE STICK PRIORITY, CAPT (23CE1) or ANN-SIDE
 STICK PRIORITY, F/O (23CE2) comes on in front of the pilot who has lost
 the priority.
 The green light of the ANN-SIDE STICK PRIORITY, CAPT (23CE1) or ANN-SIDE
 STICK PRIORITY, F/O (23CE2) comes on in front of the pilot who has
 priority as long as the side stick which has not priority is not a zero.
　
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