Figure 7-36. Cruise FAT 0C, 8000 Ft (sheet 2 of 2)

TM-55-1510-215-10 Army U-21G Aircraft Manual
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240

TM 55-1510-215-10

CRUISE

SINGLE ENGINE

U-21G

PRESSURE ALTITUDE 8000 FEET

T74-CP-700

FAT = 0C

FLAPS 0 PERCENT FUEL JP-4 GEAR UP

Figure 7-36. Cruise FAT 0C, 8000 Ft (sheet 2 of 2)

Change 1 7-77

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