TM 1-1510-224-10
RANGE PROFILE - MAXIMUM CRUISE POWER
ASSOCIATED CONDITIONS-
WEIGHT.................. *16.620 LBS BEFORE
ENGINE START
FUEL. ..................... AVIATION KEROSENE
FUEL DENSITY ....... 6.7 LBS/GAL
ICE VANES ............. RETRACTED
1700 RPM
STANDARD DAY (ISA)
ZERO WIND
EXAMPLE:
PRESSURE ALTITUDE ...... 26,000 FT
FUEL................................. 2572 LBS
RANGE ............................. 648 NM
Figure 7-51. Range Profile - Maximum Cruise Power at 1700 RPM
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