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COMPRESSOR SECTION (Cont)
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TM-55-2840-254-23-1 Engine Gas Turbine Model T55-L-712 Manual
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Combustion Section

TM 55-2840-254-23
L NO. 1 BEARING. Supported in bearing housing which is supported by inlet housing. Supports
forward end of compressor rotor assembly.
M NO. 2 BEARING. Supported in bearing housing which is supported by air diffuser assembly. Sup-
ports rear end of compressor rotor assembly.
N NO. 3 BEARING. Supported by power shaft bearing support which is supported by inlet housing.
Supports forward end of integral shaft assembly.
O NO. 6 AND 7 BEARINGS. Supported by output shaft support housing. Supports forward end of
output shaft.
1-18

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