text: NAVWEPS 00-EOT-80 
  OPERATING STRENGTH LIMITATIONS 
  
  airplane may encounter depend in great part 
  on the mission type of the airplane. However, 
  the maximum maneuvering capability 
  is of 
  interest because of 
  relationship with 
  strength limits. 
  
  the 
  
  The flight load factor is defined as the pro- 
  lift and weight, 
  
  portion between airplane 
  where 
  
  n=L/W 
  n= load factor 
  L=lift, 
  W= weight, Ibs. 
  
  Ibs. 
  
  LOAD FACTORS. The 
  maximum lift attainable at any airspeed occurs 
  the use 
  when the airplane is at CLmU. With 
  of the basic lift equation, this maximum lift 
  is expressed as: 
  
  MANEUVERING 