NAVWEPS OD-BOT-80  APPLICATION OF AERODYNAMICS  TO SPECIFIC PROBLEMS OF FLYING  RUNWAY LENGTH EQUAL TO CRITICAL  FIELD LENGTH  TAKEOFF d:; ‘ ,  CLIMB SP  CRITICAL ENGINE  LACCELERATION  WITH 1  FAILURE SPEED  q  ENGINE INOPERATIVE  ACCELERATION  WITH ALL ENGINES  OPERATIVE  \  PROFILE  \  RUNWAY LENGTH  RUNWAY LENGTH LESS THAN CRITICAL  FIELD LENGTH  MINIMUM SPEED NECESSAR  TO CONTINUE TAKEOFF WITH  ONE ENGINE IN  REFUSAL SPEE  LERATION WITH  ONE ENGINE INOPERATIVE  ACCELERATION  DECELERATION  TH ALL ENGINES  OPERATIVE  Figure 6.13. Critical Field Len&  395 