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Page Title: REMOVE FORWARD LANDING GEAR TORQUE ARM
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INSPECT FORWARD  LANDING  GEAR
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TM-55-1520-240-23-3 CH-47D Heilcopter Manual
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REMOVE  FORWARD  LANDING GEAR  TORQUE  ARM (Continued)

TM  55-1520-240-23-3 3-17 REMOVE  FORWARD LANDING GEAR  TORQUE  ARM 3-17 INITIAL  SETUP Applicable Configurations: All Tools: Aircraft  Mechanic’s Tool  Kit, NSN  5180-00-323-4692 Tiedown  Chain Aircraft  Towbar,  AA1730-1251 Materials: Barrier  Material  (E81) Personnel  Required: Medium  Helicopter  Repairer  (2) References: Task  3-9 Task  3-77 Equipment  Condition: Battery Disconnected  (Task  1-39) Electrical  Power  Off Hydraulic  Power  Off Release  Air  Pressure  From  Both  Forward  Shock Struts  (Task  1-71) Helicopter  Jacked  at Forward  Fuselage  Point (Task 1-22) NOTE Procedure  is same  for  removing  left or  right  landing  gear  torque  arm.  Left torque  arm  is  shown  here. 1. Tie  up  shock strut (1)  from  shackle  to  axle  flange with  chain  (2).  Position  barrier  material between chain  (2)  and  shock  strut  (1). 3-55

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