A319/A320/A321
TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE
27 FLIGHT CONTROLS
This document must be used for training purpose only
Under no circumstances should this document be used as a reference.
It will not be updated.
All rights reserved.
No part of this manual may be reproduced in any form,
by photostat, microfilm, retrieval system, or any other means,
without the prior written permission of Airbus Industrie.
GENERAL
** System Presentation (1) ....................... 1
** Fly By Wire Philosophy (1) ................... 11
** System Control and Indicating (1) ........... 15
** E.F.C.S. Presentation (1) .................... 21
** Control Law Presentation (1)................. 25
** Side Stick OPS & Priority Indication (1).... 43
** ECAM Page Presentation (1) ................... 61
PITCH
** Pitch Control Normal D/O (3)................. 71
** Pitch Control Abnormal D/O (3)............... 77
** Elevator Servo Control Operation (3) ........ 83
** Elevator Components (3) ...................... 91
** THS Actuator Operation (3) ................... 95
** THS Components (3)............................ 99
ROLL/YAW
** Roll Control Normal D/O (3)................. 103
** Roll Control Abnormal Operation (3) ........ 107
** Yaw Control Normal D/O (3) .................. 111
** Yaw Control Abnormal D/O (3)................ 117
** Aileron Servo Control Operation (3) ........ 121
** Aileron Components (3) ...................... 127
** Spoiler Servo Control Operation (3) ........ 131
** Spoiler Components (3) ...................... 139
** Rudder Trim Actuator D/O (3)................ 143
** Rudder Servo Control Operation (3) ......... 147
** Rudder Limiter Operation (3)................ 155
** Yaw Damper Servo Actuator Operation (3).... 161
** Rudder Components (FWD) (3)................. 171
** Rudder Components (AFT) (3)................. 181
** Speed Brake & Ground Spoiler D/O (3) ....... 197
EFCS GENERAL
** Flight Control Warnings (3)................. 207
** EFCS Control Interface (3) .................. 211
** EFCS Monitor Interface (3) .................. 239
** EFCS Components (3) ......................... 243
SLATS AND FLAPS SYSTEM
** Slats/Flaps System Presentation (1) ........ 255
** Slats/Flaps CTL & POS Indication(1)320/319. 261
** Slats/Flaps CTL & POS Indication(1)(A321).. 277
** Slats/Flaps Control (3) ..................... 293
** Slats/Flaps Abnormal OPS (Locking) (3) ..... 301
** Slats/Flaps Abnormal OPS (Half Speed) (3).. 311
** Slat Mechanical Drive D/O (3)............... 319
** Flap Mechanical Drive D/O (3) (A320/A319).. 325
** Flap Mechanical Drive D/O (3) (A321) ....... 331
** Flaps Drive Stations D/O (3)................ 337
** Flaps Attachment FAIL Detect Principle(3).. 345
** Flap Transmission Components (3) ........... 349
** Slat Transmission Components (3) ........... 361
** Slats/Flaps Control & Monitoring CMPNTS(3). 373
** Flaps Power Control Unit Components (3).... 379
** Slats Power Control Unit Components (3).... 383
** Slats/Flaps Warnings (3) .................... 389
** SFCC Control Interfaces (3)................. 395
** SFCC Monitor Interfaces (3)................. 399
MAINTENANCE PRACTICES
SPECIFIC PAGES
** CFDS Specific Page Presentation (3) ...... 405
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY
ALL
27 FLIGHT CONTROLS
UF94200 TABLE OF CONTENTS Page
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY
ALL
27 FLIGHT CONTROLS
UF94200 TABLE OF CONTENTS Page
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27 - FLIGHT CONTROLS
27-00-00 SYSTEM PRESENTATION
CONTENTS:
Introduction
Pitch
Roll
Yaw
Speed Brakes
Ground Spoilers
High Lift
Aileron Droop
Computers
Safety Precautions
Maintenance Practices
Self Examination
TMUFCBA02 LEVEL 1
EFFECTIVITY 27-00-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 1
ALL
SYSTEM PRESENTATION
INTRODUCTION
The surfaces are made of composite materials except
the slats which are made of aluminium alloy.
All the flight control surfaces are:
- electrically controlled and
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