TM 1-1520-238-23
4-489
4.149.
NO. 1 OR NO. 2 ENGINE LOAD DEMAND SPINDLE FORWARD CABLE REMOVAL
4.149.1. Description
This task covers:
Removal. Cleaning. Inspection.
4.149.2. Initial Setup
Tools:
Aircraft mechanic’s tool kit (item 376, App H)
Personnel Required:
67R
Attack Helicopter Repairer
Equipment Conditions:
Ref
Condition
1.57
Helicopter safed
2.2
Access panel L200 removed for No. 1 en-
gine or access panel R200 removed; doors
RN1, T250R, T250L, T290R, T290L, and
L325 opened for No. 2 engine
1.72
External power application – hydraulic (pri-
mary)
NOTE
This task is typical for No. 1 or No. 2 engine load demand spindle forward cable, except as noted.
M04-1187-9
NO. 1 ENGINE LDS CABLE
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M04-1187-10
NO. 2 ENGINE LDS CABLE
