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