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Page Title: INSPECT LANDING GEAR AXLE
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INSTALL AFT LANDING GEAR WHEEL AND  TIRE  ASSEMBLY (Continued)
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TM-55-1520-240-23-3 CH-47D Heilcopter Manual
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REMOVE  FORWARD  LANDING GEAR  AXLE

TM  55-1520-240-23-3 3-13 INSPECT  LANDING  GEAR AXLE 3-13 INITIAL  SETUP Applicable Configurations: All Tools: Outside  Micrometer,  1  to  2  Inch Depth  Gage  0  to  0.125  Inch Materials: None Personnel  Required: Inspector References: TM  1-1520-253-23 Equipment  Condition: Off  Helicopter  Task NOTE Procedure  is  same  for all axles. Replace  axle  if criteria  is not met. 1. Check  axle  for  cracks  and  bends.   There  shall be  no  bends or cracks.   If a  crack  is  suspected on  the  surface  of  the  landing  gear axle,  refer to TM  1-1520-253-23. 2. Check  axle  for  corrosion. 3. Check  axle  for  wear.   Measure  axle  as  shown. Dimensions  shall  be  no  less  than  1.9960 inches diameter shown  at axle  housing  end, or 1.9988 inches diameter and 1.248  inches  diameter  at the  wheel  nut  end. 4. Check  axle  for scratches.  Accept  a  maximum  of four scratches up  to  0.015 inch  wide, 0.015  inch deep  and  1 inch  long.   Blend  smoothly  within 0.03 inch on  either  side  of  scratch. FOLLOW-ON MAINTENANCE: None END  OF  TASK 3-49

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