TM 1-1510-224-10
ENDURANCE PROFILE - LOITER POWER
ASSOCIATED CONDITIONS:
1700 RPM
EXAMPLE:
WEIGHT.................16.620 LBS BEFORE
STANDARD DAY (ISA)
PRESSURE ALTITUDE ......26,000 FT
ENGINE START
FUEL .................................2572 LBS
FUEL .....................AVIATION KEROSENE
ENDURANCE.....................3.34 HRS
FUEL DENSITY ......6.7 LBS/GAL
ICE VANES ............RETRACTED
Figure 7A-81. Endurance Profile - Loiter Power at 1700 RPM
7A-131
