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Figure 7-69. Cruise FAT -30C, 25,000 Ft
Section XV. CLIMB/DESCENT
TM-55-1510-215-10 Army U-21G Aircraft Manual
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TM
55-1510-215-10
CRUISE
CRUISE
TWIN
ENGINE
U-21G
PRESSURE
ALTITUDE
25,000
FEET
T74-CP-700
FAT
=
-20
C
FLAPS
0
PERCENT
FUEL
JP-4
GEAR
UP
Figure
7-
70.
Cruise
FAT
-
20
C, 25,000 Ft
Change
1
7-115