NAVWEPS 00-801-80  APPLICATION OF AERODYNAMICS  TO SPECIFIC PROBLEMS OF FLYING  THRUST  REQ ’ D  AND  AVAILABLE  LBS.  THRUST AVAJLABLE WJTH ALL  ENGINES OPERATING  THRUST AVAILABLE WITH  NES OPERATING  THRUST  REO ’ U  AND  AVAILABLE  LB.%  I  VELOCITY, KNOTS  THRUST REP ’ D  THRUST REO ’ D CLEAN  LANDING CONFIGURATION  CONFIGURATION  WING LEVEL FLIGHT  ,  BUT TURNING FLIGHT  WING LEVEL FLIGHT  AVAILABLE DUE TO  ENGINE FAILURE  4  VELOCITY, KNOTS  Figure 6.8. Engine Failure on Multi-engine  Aircraft  378 