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TM-55-2835-209-23 Gas Turbine Engine (Auxiliary Power Unit APU) Model T 62T 40 I Part Numbers 116305-100 and 116305-200 Manual | Next
INSPECTION OF COMBUSTOR CASE (AVIM) |
TM 55-2835-209-23
Section VI INSTALL COMBUSTION CHAMBER
3-6 INSTALL COMBUSTION CHAMBER (AVIM)
INITIAL SETUP
Personnel Required:
68B Aircraft Powerpl
68B Aircraft Powerpl
References:
Task 3-11
ant Inspector
ant Repairer
Equipment Conditions:
APU on Maintenance Stand (T1)
Install combustion chamber (1) on power
section assembly (2) aligning match
marks made during removal, on combustion
chamber (1) and airflow deflector (3).
FOLLOW-ON MAINTENANCE: Install combus-
tor case (Task 3-11).
3-15
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