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REPLACE  LCT ACTUATOR  MOTOR (Continued)
INSTALL  FORWARD  LCT ACTUATOR (Continued) - TM-55-1520-240-23-9_838

TM-55-1520-240-23-9 CH-47D Heilcopter Manual
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TM  55-1520-240-23-9 11-206 INSTALL FORWARD LCT  ACTUATOR 11-206 INITIAL  SETUP Applicable Configurations: All Tools: Aircraft  Mechanic’s Tool  Kit, NSN 5180-00-323-4692 Torque  Wrench,  100  to  750  Inch-Pounds Materials: Antiseize  Compound  (E75) Gloves  (E184.1) Parts: Cotter Pins Washers Personnel  Required: Medium  Helicopter Repairer (2) Inspector References: TM  55-1520-240-23P Task  1-13 Task  11-202 Equipment  Condition: LCT  Actuator  Fully  Retracted Do  not use  cadmium  plated  hardware or  tools  while  working  on  yoke assembly.   Titanium  yoke  could  be damaged. Do  not  use  chlorinated  solvents  for cleaning.   Titanium  yoke  could  be damaged  by this  solutIon. Bushings  must be  in  swashplate  and yoke  before  installing  bolts;  otherwise, damage  to  components will  result. NOTE Positive  retention  bolts  are  installed in  flight  control  connections.  These bolts are  self-retaining  and  require  a special nut  and  torque  (Task  1-13). 11-821







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