Figure 7-81. Endurance Profile - Loiter Power at 1700 RPM

Figure 7-80. Loiter Power at 1700 RPM - ISA +37C (Sheet 2 of 2)

Figure 7-82. Range Profile - Full Main Tanks

TM-1-1510-224-10 Army RC-12P Aircraft and Army RC-12Q Aircraft Manual
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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 7-131

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