TM 1-1510-224-10
RANGE PROFILE - MAXIMUM CRUISE POWER
ASSOCIATED CONDITIONS:
1700 RPM
EXAMPLE:
WEIGHT.................16.620 LBS BEFORE
PRESSURE ALTITUDE .........26.000 FT
ENGINE START
FUEL .................................... 2572 LBS
FUEL .....................AVIATION KEROSENE
STANDARD DAY (ISA)
RANGE.................................... 628 NM
FUEL DENSITY ......6.7 LBS/GAL
ZERO WIND
ICE VANES ............RETRACTED
Figure 7A-51. Range Profile - Maximum Cruise Power at 1700 RPM
7A-77
