TM 1-1510-224-10
RANGE PROFILE - MAXIMUM RANGE POWER
ASSOCIATED CONDITIONS:
WEIGHT..............*16,620 LBS BEFORE
ENGINE START
FUEL ...................AVIATION KEROSENE
FUEL DENSITY ..6.7 LBS/GAL
ICE VANES .........RETRACTED
1500 RPM
STANDARD DAY (ISA)
ZERO WIND
EXAMPLE:
PRESSURE ALTITUDE.......... 26,000 FT
FUEL ...................................... 2572 LBS
RANGE................................... 686 NM
Figure 7-72. Range Profile - Maximum Range Power at 1500 RPM
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