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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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01 - GENERAL
01-00-00 AIRCRAFT DIMENSIONS
CONTENTS:
Lateral View
Top View
Front View
Door Heights
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AIRCRAFT DIMENSIONS (LATERAL VIEW)
EFFECTIVITY 01-00-00 Page 2
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AIRCRAFT DIMENSIONS (TOP VIEW)
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AIRCRAFT DIMENSIONS (FRONT VIEW)
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AIRCRAFT DIMENSIONS (DOOR HEIGHTS)
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51 - STRUCTURE
51-00-00 - A320 STRUCTURE GENERAL
CONTENTS:
Metallic Materials
Composite Materials
Aircraft Drainage
Surface Pretreatment
Paint System
No Step Areas
Jacking Points
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A320 STRUCTURE GENERAL
METALLIC MATERIALS
The basic aircraft structure is made of aluminium
alloys with stainless steel and titanium alloys in
specific areas.
COMPOSITE MATERIALS
Composite materials are used for primary and secondary
structure.
Composite materials represents about 15% of the
aircraft structural weight. CFRP is mainly used for
primary structures, whilst AFRP and GFRP are only used
for secondary structures.
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A320 STRUCTURE GENERAL
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A320 STRUCTURE GENERAL
AIRCRAFT DRAINAGE
Wings and fuselage are equipped with different types
of drains.
Holes and gaps are provided to ensure natural drainage
of the fluid collection points. Drain holes are drilled
before application of pretreatments. Remote drains are
used when natural drainage is not possible.
SURFACE PRETREATMENT
The protection of the structure against corrosion is
achieved by means of appropriate surface pretreatment
of the metallic parts.
Aluminium Alloys :
The primary protection is generally a pure aluminium
cladding. The main pretreatment used is the unsealed
chromic acid anodizing (CAA).
Titanium Alloys :
Surface interfaying with aluminium alloy parts are
zinc sprayed. The other titanium alloy surfaces are
left bare.
Titanium fasteners are either sulphuric acid anodized
or aluminium coated.
Composite materials are left bare.
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MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
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A320 STRUCTURE GENERAL
TMUST0101-P02 LEVEL 1
EFFECTIVITY 51-00-00 Page 5
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MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
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中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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