A319/A320/A321
TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE
07 JACKING

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.

** Jacking (2) .................................... 1
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 07 JACKING
UF94200
EFFECTIVITY
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07 JACKING
UF94200 TABLE OF CONTENTS Page
07 CONTENTS
Page i
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 07 JACKING
UF94200
EFFECTIVITY
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07 JACKING
UF94200 TABLE OF CONTENTS Page
07 CONTENTS
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07 - LIFTING AND SHORING
07-10-00 JACKING
CONTENTS:
General
Limitations
Precautions
Jacking Points
Levelling
TMUJACA01 LEVEL 1
EFFECTIVITY 07-10-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 07 JACKING
UF94200
EFFECTIVITY Page 1
ALL
JACKING
GENERAL
Three jacking points, when equipped with jacking pads,
are used to lift the aircraft. The forward point "A"
is located forward of the nose landing gear. The points
"B" and "B’" are located outboard of the engine pylon.
A safety jack positioned at the rear of the aircraft
prevents the aircraft from tipping up.
LIMITATIONS
The open air jacking operation is limited if the wind
velocity exceeds permissible values which depend on
aircraft gross weight and center of gravity position.
In any condition, the aircraft must be pointing upwind.
PRECAUTIONS
The three jacks have to be operated together. The
aircraft has to be lifted so that the landing gear can
be operated in the "Landing gear shock absorbers
deflated, flat tyres" configuration.
As soon as the jacking operation is finished, position
the safety jack as a tail stanchion.
JACKING POINTS
Jacking pads have to be used under the jacking points
to spread the loads.
LEVELLING
To ensure that excessive side loads are not placed on
the jacks and on the aircraft structure, a quick
levelling check must be carried out during the jacking
operation.
The aircraft attitude monitor is located in the
Refuel/Defuel control panel recess.
The "D4" position corresponds to a longitudinal angle
of 0o and a lateral angle of 0o
.
TMUJACA01-T01 LEVEL 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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JACKING
TMUJACA01-P01 LEVEL 1
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TMUJACA01 LEVEL 1
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