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ALL
A320 STRUCTURE GENERAL
PAINT SYSTEM
Before the final paint system, all aluminium parts are
primed.
The paint system used includes polyurethane primers
and paint on the external surfaces, and epoxy primers
and polyurethane paint on the internal surfaces.
Anti-slip paint is the overwing escape zones.
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EFFECTIVITY 51-00-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
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ALL
A320 STRUCTURE GENERAL
TMUST0101-P03 LEVEL 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 25
ALL
A320 STRUCTURE GENERAL
NO STEP AREAS
Wing and tailplane no step areas.
Protective mats are required on the horizontal
stabilizer as it is a carbon fiber structure.
JACKING POINTS
There are three jacking points provided.
Three jacking points are provided, one below each wing
outboard of the pylon and one in front of the nose
landing gear bay.
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EFFECTIVITY 51-00-00 Page 8
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 26
ALL
A320 STRUCTURE GENERAL
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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THIS PAGE INTENTIONALLY LEFT BLANK
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ALL
51 - STRUCTURE
51-00-00 A320 STRUCTURAL BREAKDOWN AND
ZONING
CONTENTS:
Reference Axes
ATA Chapters
Section Numbers
Station Numbers
Zone Numbers
TMUST0201 LEVEL 1
EFFECTIVITY 51-00-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 29
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
REFERENCE AXES
The structure elements are localized according to the
following reference axis.
Note : The reference (station 0) for all structural
measurements in the X axis is located 100 in.
(254 cm) forward of the aircraft nose.
Here is a typical fuselage contour in the Y and Z
planes. Section A-A at frame 55.
These are the major aircraft reference axis.
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 30
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 31
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
ATA CHAPTERS
The aircraft structure is divided according to the ATA
100 specifications.
SECTION NUMBERS
Each major part of the aircraft, corresponding to
production receives a section number. The fuselage
section base number is 10.
The fuselage is divided into various sections for
manufacturing reasons.
TMUST0201-T02 LEVEL 1
EFFECTIVITY 51-00-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 32
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
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ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
SECTION NUMBERS
The general wing section base number is 20.
The general tail plane section base number is 30.
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MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
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A320 STRUCTURAL BREAKDOWN AND ZONING
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
　
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