NAVWEPS C&801-80 
AIRPLANE PERFORMANCE 
TYPICAL PROPELLER AIRCRAFT ALTlTUOE PERFORMANCE 
. RATE OF,CL!MB_, _- 
. 
tiAXlMUM LEVEL FLIGHT SPEED 
HIGH BLOWER CRITICAL ALTITUDE 
FEE0 FOR MA% R c 
LOW BLOWER CRITICAL ALTITUDE 
= y$y VELOCITY, KNOTS 
-e-*-- 
TROPOPAUSE 
t- 
\ MAXIMUM LEVEL 
\ 
\ FLIGHT SPEED 
-RATE OF CLIMB 
\ 
\ 
\ 
\ 
I I I I b 
-8 
VELOCITY, KNOTS 
POWER OFF DESCENT PERFORMANCE 
POWER 
REQUIRED 
HP 
MINIMUM POWER REP’D 
I VELOCITY, KNOTS 
Figure UP, Climb ad Desceni Pedormome 
lS7