Figure 7-53. Cruise FAT -50C, 20,000 Ft

TM-55-1510-215-10 Army U-21G Aircraft Manual
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261

TM 55-1510-215-10

CRUISE

TWIN ENGINE

U-21G

PRESSURE ALTITUDE 20,000 FEET

T74-CP-700

FAT = -50C

FLAPS 0 PERCENT FUEL JP-4 GEAR UP

Figure 7-53. Cruise FAT -50C, 20,000 Ft

7-98 Change 1

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