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The vane inner platforms are axially retained by the inner face of the fan OGV inner shroud.
The vane outer platforms are bolted to the downstream fan inlet case.
A splitter fairing, which separates the primary and secondary airflows, is bolted onto the fan OGV inner shroud forward flange.
There are 2 unplugged holes on the inner shroud, between the 3 and 4 o’clock positions, to enable borescope inspection of the booster vane assemblies. One is located between the OGV’s at the stage 3 vane assembly and the other at the stage 5 vane assembly.
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BASIC ENGINE
ALL CFM56-5B ENGINES FOR A319-A320-A321
CFMI PROPRIETARY INFORMATION

CFM56-5B包H TRAINING  MANUAL
OUTLET OGV  OUTER PLATFORM
GUIDE INNER UNPLUGGED VANE SHROUD BORESCOPE HOLES
OGV FAIRING SPLITTER
INNER PLATFORM
FAN OUTLET GUIDE VANES
CTC-063-020-02
EFFECTIVITY  Page 23
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ALL CFM56-5B ENGINES FOR A319-A320-A321  BASIC ENGINE

CFMI PROPRIETARY INFORMATION
THIS PAGE INTENTIONALLY LEFT BLANK

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EFFECTIVITY
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BASIC ENGINE
ALL CFM56-5B ENGINES FOR A319-A320-A321
CFMI PROPRIETARY INFORMATION

 包 CFM56-5B TRAINING MANUAL
H
CORE ENGINE MAJOR MODULE

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EFFECTIVITY
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BASIC ENGINE
ALL CFM56-5B ENGINES FOR A319-A320-A321

CFMI PROPRIETARY INFORMATION
The core engine is a high pressure, high speed, gas generator that produces the power to drive the engine.
The core engine consists of the :
- The High Pressure Compressor (HPC) section.

- The Combustion section.

- The High Pressure Turbine (HPT) section & the Low
Pressure Turbine (LPT) stage 1 nozzle.

 

Fan discharge air is compressed in the HPC section and heated and expanded in the combustion section. It is then directed to the HPT section. Energy not extracted from the gas stream by the HPT is used to drive the LPT, fan rotors and booster.
The forward end of the core is supported by the No 3 ball and roller bearings and the aft end by the No 4 roller bearing.
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EFFECTIVITY
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BASIC ENGINE
ALL CFM56-5B ENGINES FOR A319-A320-A321
CFMI PROPRIETARY INFORMATION

包H
HIGH PRESSURE
COMPRESSOR STATOR

HIGH PRESSURE COMPRESSOR ROTOR
#3 BEARING
CTC-063-039-00
EFFECTIVITY
CFM56-5B
COMBUSTION CASE
COMBUSTION SECTION
HPC STATOR
HPC
SECTION

CORE ENGINE MAJOR MODULE
ALL CFM56-5B ENGINES FOR A319-A320-A321

TRAINING  MANUAL
HIGH PRESSURE TURBINE SECTION
STAGE 1 LPT NOZZLES
#4 BEARING
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