TM 1-1510-224-10
RANGE PROFILE - FULL MAIN & AUX TANKS
ASSOCIATED CONDITIONS:
EXAMPLE:
WEIGHT.................16.620 LBS BEFORE
STANDARD DAY (ISA)
PRESSURE ALTITUDE ............26.000 FT
ENGINE START
RANGE @:
FUEL .....................AVIATION KEROSENE
ZERO WIND
MAXIMUM CRUISE POWER.....1005 NM
FUEL DENSITY ......6.7 LBS/GAL
NORMAL CRUISE POWER.......1023 NM
ICE VANES ............RETRACTED
MAXIMUM RANGE POWER .....1075 NM
Figure 7A-84. Range Profile - Full Main and Aux Tanks
7A-134