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UF94200
EFFECTIVITY Page 35
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
SECTION NUMBERS
The engine sectionbase number is 40.
The landing gear section base number is 50.
The general belly fairing section base number is 60.
TMUST0201-T04 LEVEL 1
EFFECTIVITY 51-00-00 Page 8
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 36
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P04 LEVEL 1
EFFECTIVITY 51-00-00 Page 9
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 37
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
STATION NUMBERS
The station number is the distance in centimeters of
a cross section from a reference point.
The station/frame numbers shown correspond to the
section boundaries.
Here are the engine station numbers.
Note : For the vertical stabilizer the reference
station is z=0 at the VTZ axis.
TMUST0201-T05 LEVEL 1
EFFECTIVITY 51-00-00 Page 10
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 38
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P05 LEVEL 1
EFFECTIVITY 51-00-00 Page 11
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 39
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
STATION NUMBERS
Horizontal stabilizer station numbers.
Note : For the horizontal stabilizer the reference
station is y=0 at the A/C Y axis.
Wings station numbers.
Note : For wings the reference station is wing
reference axis (WY). WY is located at 1868 mm
(73.54 in) from A/C X axis.
TMUST0201-T06 LEVEL 1
EFFECTIVITY 51-00-00 Page 12
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 40
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P06 LEVEL 1
EFFECTIVITY 51-00-00 Page 13
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 41
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
ZONE NUMBERS
There are 8 major zones in the aircraft.
Each major zone is identified by the first digit of a
three digit number.
Fuselage and vertical stabilizer zones.
TMUST0201-T07 LEVEL 1
EFFECTIVITY 51-00-00 Page 14
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 42
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P07 LEVEL 1
EFFECTIVITY 51-00-00 Page 15
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 43
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
ZONE NUMBERS
Belly fairing zones.
Landing gear zones.
Wings and horizontal stabilizer zones.
TMUST0201-T08 LEVEL 1
EFFECTIVITY 51-00-00 Page 16
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 44
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P08 LEVEL 1
EFFECTIVITY 51-00-00 Page 17
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 45
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
ZONE NUMBERS
Nacelles and pylon zones.
Door zones.
TMUST0201-T09 LEVEL 1
EFFECTIVITY 51-00-00 Page 18
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 46
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
TMUST0201-P09 LEVEL 1
EFFECTIVITY 51-00-00 Page 19
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 01 GENERAL
UF94200
EFFECTIVITY Page 47
ALL
A320 STRUCTURAL BREAKDOWN AND ZONING
ZONE NUMBERS
Access doors and panels are identified by the number
of the zone in which the panel is located followed by
a two-letter suffix which locates it within the zone.
Here is an example of access panel doors on the left
wing lower surface.
　
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