NAVWEPS 00-807-80 
AIRPLANE PERFORMANCE 
ALL CURVES APPROPRIATE 
FOR A PARTICULAR: 
r 
ALTITUDE 
M&N NUMBER 
BOUNDARY A& 
DECELEFlATlON 
BOUNDARY 
MAFfGIN 
w 
E I (IDLE) N-RPM (MA%) 
EXHAUST GAS 
TEMPERATURE 
RPM c 
PRESSURE . _ . _ _ - - - 
TEMPERATURE 
rAILPIPE TOTAL 
PRESSURE 
Figure 2.12. Engine Governing and Instrumentation 
122