TM   55-3930-660-14 APPENDIX B LOADING  RESTRAINT  FACTORS The  loading  restraint  factors  (LRFs)  used  for  surface  and  air  modes  are  the  "G"  (acceleration  of  gravity) loading  factors  that  can  be  expected  in  military  transport.  The  tiedown  arrangements  shown  in  the  6K VRRTFL TGTM are based on the following: —restraint factors are applied independently in each direction. —restraint  load  (GVW  times  the  LRF)  was  resolved  into  resultant  lashing  loads,  allowing  for  tiedown angle. –lashing loads are less than safe working load (SWL) of the restraint (that is, wire rope). Highway: The Transportation Engineering Agency highway LRFs are: 0.7 in the forward direction (relative to the transporter). 0.3 in the aft and vertical directions. 0.1 in the lateral direction. Rail: The Association of American Railroads recommended rail LRFs are: 3.0 in the longitudinal direction (relative to the railcar). 2.0 in the lateral and vertical directions. Marine: The Military Sealift Command (MSC) design LRFs are: 1.2 in the lateral direction (relative to the ship). 0.7 in the longitudinal direction. 0.2 in the vertical direction. MSC LRFs are for severe conditions. Actual  marine  LRFs  vary.  Marine  tiedown  restraint  depends  on  the  size  of  ship  (decreasing  on  larger vessels),  the  expected  sea  state  to  be  encountered,  and  the  stow  location  on  a  given  ship.  Generally,  the restraint  required  will  increase  for  locations  high  and  forward  (or  aft)  in  the  ship.  The  most  severe conditions occur on exposed “weather decks,”  where strong wind and wet conditions add to the problem. A ship’s  crew  may  require  additional  lashing  on  exposed  decks.  Below-deck  locations  that  are  closer  to  the vessel’s  centers  of  gravity  and  rotation  will  experience  less  severe  motion.  The  blocking  and  tiedown procedures presented (fig 4–1) will allow for severe, below-deck conditions. Air: The USAF aircraft LRFs are: 3.0 in the forward direction (relative to the aircraft). 2.0 in the vertical direction. 1.5 in the aft and lateral directions. B-1

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