Figure 7-37. Cruise FAT 10 C, 8000 FT (sheet 2 of 2)

TM-55-1510-215-10 Army U-21G Aircraft Manual
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242

TM 55-1510-215-10

CRUISE

SINGLE ENGINE

U-21G

PRESSURE ALTITUDE 8000 FEET

T74-CP-700

FAT = 10 C

FLAPS 0 PERCENT FUEL JP-4 GEAR UP

Figure 7-37. Cruise FAT 10 C, 8000 FT (sheet 2 of 2)

Change 1 7-79

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