A319/A320/A321
TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE
32 LANDING GEAR
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
** System Controls & Indicating Present. (1).... 9
LANDING GEAR AND DOORS
** Retraction/Extension Presentation (1) ....... 13
** System Indications (1) ....................... 23
** System Warnings (3) .......................... 27
** System Normal Operation (3) .................. 31
** Free Fall Extension (3) ...................... 47
** Safety Precautions (2) ....................... 57
** Doors Ground Operation (2) ................... 65
** Doors Ground Opening D/O (3)................. 71
** LGCIU Control Signals (3) .................... 77
** LGCIU Monitoring Interfaces (3) ............. 81
** MLG Description (2) .......................... 87
** MLG Doors Description (2) .................... 97
** NLG Description (2) ......................... 101
** NLG Doors Description (2) ................... 105
** Landing Gear Components (2)................. 109
** Landing Gear Components (3)................. 115
WHEELS AND BRAKES
** Brake System Presentation (1)............... 137
** Brake System Description (3)................ 151
** Auto-Brake System D/O (3) ................... 155
** Anti-Skid Function (3) ...................... 159
** Brake Hydraulic System Operation (3) ....... 163
** Brake Temperature System Presentation (3).. 173
** Brake Cooling System Presentation (1) ...... 177
** ECAM Page Presentation (1) .................. 181
** System Warnings (3) ......................... 185
** Normal Braking Components (3)............... 187
** Alternate Braking Components (3) ........... 209
** Parking Brake Components (3)................ 227
** Wheel Components (3) ........................ 237
** Brake Temperature System Components (3).... 249
** Brake Cooling System Components (3) ........ 253
NOSE WHEEL STEERING
** System Presentation (1) ..................... 257
** System Description/Operation (3) ........... 261
** ECAM Page Presentation (1) .................. 267
** System Warnings (3) ......................... 271
** Components (2)............................... 273
** Components (3)............................... 277
BRAKING AND STEERING
** BSCU Control Interfaces (3)................. 285
** BSCU Architecture & Monitoring INTFC (3)... 289
TIRE PRESSURE INDICATING
** System Presentation (1) ..................... 295
** System Description/Operation (3) ........... 299
** System Warnings (3) ......................... 303
** Components (3)............................... 305
MAINTENANCE PRACTICES
** MLG Servicing (3)............................ 313
** MLG Shock Absorber Servicing (3) ........... 319
** Low PRESS Circuit Filling and Bleeding(3).. 337
** Wheel and Brake R/I (2) ..................... 341
** CFDS Specific Page Presentation (3) ........ 347
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY
ALL
32 LANDING GEAR
UF94200 TABLE OF CONTENTS Page
32 CONTENTS
Page i
Dec 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY
ALL
32 LANDING GEAR
UF94200 TABLE OF CONTENTS Page
32 CONTENTS
Page ii
Dec 31/00
THIS PAGE INTENTIONALLY LEFT BLANK
32 - LANDING GEAR
32-00-00 GENERAL SYSTEM PRESENTATION
CONTENTS:
Gear
Extension/Retraction
Brakes
Steering
Self Examination
TMULDG101 LEVEL 1
EFFECTIVITY 32-00-00 Page 1
Feb 29/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 1
ALL
LANDING GEAR GENERAL SYSTEM PRESENTATION
GEAR
The landing gear consists of a forward retracting nose
gear and two inboard retracting main gear legs.
Each gear has an oleopneumatic shock absorber and is
equipped with two wheels.
Each main wheel is fitted with anti-skid wheel brakes.
The two-wheel nose gear comprises an oleopneumatic
shock absorber and a nose wheel steering system.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：ATA 32 LANDING GEAR
