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INSTALL COMBUSTOR CASE (AVIM) (CONT) | Up
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
removal |
TM 55-2835-209-23
Section XIV HOT SECTION INSPECTION (1000 HOUR)
3-14 HOT SECTION INSPECTION (1000 HOUR) (AVIM)
This task covers: a. Removal b. Installation
INITIAL SETUP
Tools:
Engine Repairman’s Tool Kit (T47)
References:
Tasks 3-2, 3-6, 4-11, 6-2, 6-12, 6-19
Personnel Required:
Equipment Conditions:
68B Aircraft Powerplant Repairer
APU on Maintenance Stand (T1)
Materials/Parts:
Antiseize Compound (D7)
Marking Pencil (D24)
REMOVAL
1.
Drain APU oil (Task 6-2).
2.
Replace fuel filter assembly (Task
4-11).
3.
Replace oil filter element (Task
6-12).
4.
Remove combustion chamber (Task
3-2).
5.
Match mark airflow deflector, tur-
bine nozzle and compressor airflow
deflector to compressor housing
using marking pencil (D24).
6.
Remove bolts (1) and washers (2).
Discard bolts.
3-34
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