TM 1-1510-224-10
RANGE PROFILE - NORMAL CRUISE POWER
ASSOCIATED CONDITIONS:
1500 RPM
EXAMPLE:
WEIGHT.................. *16,620 LBS BEFORE
PRESSURE ALTITUDE ..........26000 FT
ENGINE START
FUEL .................................... 2572 LBS
FUEL ...................... AVIATION KEROSENE
STANDARD DAY (ISA)
RANGE ................................... 637 NM
FUEL DENSITY ....... 6.7 LBS/GAL
ZERO WIND
ICE VANES ............. RETRACTED
Figure 7A-63. Range Profile - Normal Cruise Power at 1500 RPM
7A-97
