Figure 7-122. Range Profile

Figure 7-121. Endurance Profile - Loiter Power IR

Figure 7-123. Endurance Profile - Full Main Tanks IR

TM-1-1510-223-10 Army RC-12 Aircraft Manual
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TM 1-1510-223-10 RANGE PROFILE - FULL MAIN TANKS STANDARD DAY (ISA) ZERO WIND ASSOCIATED CONDITIONS: WEIGHT...................................15,672 LBS BEFORE ENGINE START FUEL ......................................AVIATION KEROSENE FUEL DENSITY .......................6 7 LBS/GAL ICE VANES .............................RETRACTED NOTE: RANGE ALLOWS FOR START, TAXI, AND RUNUP; INCLUDES CRUISE CLIMB AND DESCENT; AND ALLOWS FOR 45 UINUTES RESERVE FUEL AT MAXIUUM RANGE POWER EXAMPLE PRESSURE ALTITUDE ........................26,000 FT RANGE @: MAXIMUU CRUISE POWER ..........594 NM NORUAL CRUISE POWER.............596 NU MAXIUUM RANGE POWER............626 NY Figure 7-122. Range Profile - Full Main Tanks Change 2 7-197

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