TM 1-1510-224-10
RANGE PROFILE - FULL MAIN TANKS
ASSOCIATED CONDITIONS:
EXAMPLE:
WEIGHT.................15672 LBS BEFORE
STANDARD DAY (ISA)
PRESSURE ALTITUDE ............26,000 FT
ENGINE START
RANGE @:
FUEL .....................AVIATION KEROSENE
ZERO WIND
MAXIMUM CRUISE 0POWER...650 NM
FUEL DENSITY ......6.7 LBS/GAL
NORMAL CRUISE POWER.......661 NM
ICE VANES ............RETRACTED
MAXIMUM RANGE POWER .....700 NM
Figure 7A-82. Range Profile - Full Main Tanks
7A-132
