TM 1-1510-224-10
ENDURANCE PROFILE - LOITER POWER
ASSOCIATED CONDITIONS:
WEIGHT..............*16,620 LBS BEFORE
ENGINE START
FUEL ...................AVIATION KEROSENE
FUEL DENSITY ..7 LBS/GAL
ICE VANES .........RETRACTED
1700 RPM
STANDARD DAY (ISA)
EXAMPLE:
PRESSURE ALTITUDE.......... 26,000 FT
FUEL ...................................... 2572 LBS
ENDURANCE......................... 3.44 HRS
Figure 7-81. Endurance Profile - Loiter Power at 1700 RPM
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