Order this information in Print

Order this information on CD-ROM

Download in PDF Format

     

Click here to make tpub.com your Home Page

Page Title: LANDING GEAR (Continued)
Back | Up | Next

Click here for a printable version

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Combat
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
USMC
   
Products
  Educational CD-ROM's
Printed Manuals
Downloadable Books
   

 

Back
LANDING GEAR (Continued)
Up
TM-55-1520-240-23-3 CH-47D Heilcopter Manual
Next
LANDING GEAR (Continued)

TM  55-1520-240-23-3 3-1 LANDING  GEAR (Continued) 3-1 PROXIMITY  SWITCHES Linkage  from  the  aft  landing  gear  upper  drag  link  is connected  to  a  target.  The  target  is set  so  the  proximity switch  is  open  when  the  helicopter is  in  flight.  When  the helicopter  is on  the  ground,  the  switch  is  closed.  The switches prevent  DASH  actuator  input  during  lift-off  to hover.  They  also  reduce  AFCS  sensitivity  50 percent until  lift-off.   The  right  switch  turns off  the  IFF  when  the helicopter  is on  the  ground. STATIC  LOCK  MECHANISM The  static  lock  mechanism  is  a  link  attached  to  aft landing  gear shock  strut.  It is  operated  by hand  to  lock the  shock  strut in  the  up  position  when  the  helicopter is  jacked. SWIVEL HOUSING AND  SPINDLE A  swivel  housing  is  supported  by the  two  drag  links  and shock strut of  each  aft landing  gear.  The  housing  allows the  spindle  and  wheel  to  swivel  360º.  A  centering  cam in  the  housing  centers  the  wheel  in  the  trailing  position for taxiing  or flight.   The  swivel  locking  pin  can  lock  the wheel  in  this position. 3-5

Privacy Statement - Press Release - Copyright Information. - Contact Us - Support Integrated Publishing