CHAPTER 22
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AUTO FLIGHT
TABLE OF CONTENTS
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SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Guidance Computer) FCU (Flight Control Unit) 33 ALL MCDU (Multipurpose Control and 41 ALL Display Unit)
FAULT ISOLATION FUNCTION - PRINCIPLE 22-91-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Line Maintenance 1 ALL Characteristics of the AFS 1 ALL Maintenance System Safety 1 ALL Component Location 2 ALL System Description 2 ALL General 2 ALL Description 2 ALL FIDS operation 7 ALL FIDS Power Supply 31 ALL FIDS Interface 31 ALL ARINC Inputs/Outputs 31 ALL Discrete Inputs/Outputs 31 ALL FIDS - BITE Interface 32 ALL Interface with FMGC1 32 ALL Operation 34 ALL General 34 ALL List of LRUs Covered by the FIDS 39 ALL Safety Tests 41 ALL
FAULT ISOLATION FUNCTION - PRINCIPLE 22-91-00
ADJUSTMENT/TEST 501 ALL
Ground Scanning of the AFS 501 ALL
AFS FAULT ISOLATION 22-92-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL List of FAC Error Codes 1 ALL List of FMGC/FG Error Codes 4 ALL List of FMGC/FM Error Codes 8 ALL
AFS TEST (AFTER AFS LRU REMOVAL) 22-96-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Triggering of the AFS TEST 1 ALL Execution of the AFS TEST in the 2 ALL FIDS
CHAPTER 22
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AUTO FLIGHT
TABLE OF CONTENTS
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SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
Test Execution 2 ALL
Execution of the LRU TEST in the 5 ALL
FAC
Execution of the LRU TEST in the 6 ALL
FMGC
FG Level 6 ALL FM Level 6 ALL Overall Result Indication 6 ALL
Operation 7 ALL Power-up Tests Initialization and 7 001-049, 051-060 Cockpit Repercussions 101-101,
Computer FMGC 7 001-049, 051-060 101-101, Computer FAC 8 001-049, 051-060 101-101, Computer FCU 9 001-049, 051-060 101-101, Computer MCDU 10 001-049, 051-060 101-101,
AFS TEST 22-96-00
ADJUSTMENT/TEST 501 ALL
Operational Test of the AFS 501 ALL
LAND CAT III CAPABILITY TEST 22-97-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
System Description 1 ALL
Test Acceptation 1 ALL Test Principle 1 ALL Test Running 2 001-049, 051-099
101-105, 151-199 201-299, Test Running 2 106-149, 301-399 401-499,
LAND CAT III CAPABILITY TEST 22-97-00
ADJUSTMENT/TEST 501 ALL
Operational Test of the LAND CAT 501 ALL
III Capability
22-CONTENTS Page 22 Aug 01/05
CES AUTO FLIGHT - GENERAL - DESCRIPTION AND OPERATION
_________________________________________________
1. General
_______
The auto-flight system is made up of the following sub-systems:
A. Flight Management and Guidance System (FMGS)
The FMGS performs the functions given below :
-autopilot (AP)
-flight director (FD)
-autothrust (A/THR)
-flight management which includes navigation, performance and processing of displays.
B. Flight Augmentation (FAC)
The FAC performs the functions given below:
-yaw damper
-rudder travel limiting
-monitoring of the flight envelope and computations of maneuvering speed
-yaw autopilot order using power loops of yaw damper and rudder trim
-FAC 1: BITE function of the AFS.
1EFF : ALL 1 22-00-00Page 1 1 1 Feb 01/98 1 1 1CES 1 2. Component Location
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(Ref. Fig. 001, 002)
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------1CA1 FMGC-1 83VU 127 824 22-83-34 1CA2 FMGC-2 84VU 128 824 22-83-34 2CA FCU 13VU 211 831 22-81-12 3CA1 MCDU-1 11VU 211 831 22-82-12 3CA2 MCDU-2 11VU 211 831 22-82-12
**ON A/C 001-049, 051-061, 101-105,
12CA1 SOLENOID-PITCH & ROLL LOCK, CAPT 193VU 211 831 22-11-00 12CA2 SOLENOID-PITCH & ROLL LOCK, F/O 182VU 212 831 22-11-00 1CC1 FAC-1 83VU 127 824 22-66-34 1CC2 FAC-2 84VU 128 824 22-66-34 9CC CTL SW-RUDDER TRIM 110VU 211 831 22-62-11 8CC P/BSW-RUD TRIM/RESET 110VU 210 831 22-62-12 17CC IND-RUDDER TRIM 110VU 211 831 22-62-21 2CC XDCR UNIT-YAW DAMPER POS 325 325BL 27-26-17 3CC1 SERVO ACTR-YAW DAMPER, 1 325 325BL 27-26-51 3CC2 SERVO ACTR-YAW DAMPER, 2 325 325BR 27-26-51 4CC LIMITATION UNIT-RUDDER TRAVEL 325 325DL 27-23-51 10CC ACTUATOR-RUDDER TRIM 325 325AL 27-22-51 7CA1 P/BSW-A/THR INST DISC, CAPT 211VU 210 831 22-31-00 7CA2 P/BSW-A/THR INST DISC, F/O 210VU 210 831 22-31-00 12CC1 P/BSW-FLT CTL/FAC1 23VU 211 831 22-65-00 12CC2 P/BSW-FLT CTL/FAC2 24VU 212 831 22-65-00 4CA CARRY ON LOADER 212 831 22-71-00 47CE1 RELAY-TAKEOVER & PRIORITY 1 187VU 127 824 27-92-00 47CE2 RELAY-TAKEOVER & PRIORITY 2 188VU 128 824 27-92-00
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