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Section XI. SINGLE-ENGINE CLIMB
Section XII. OPERATION ENVELOPE
TM-55-1510-215-10 Army U-21G Aircraft Manual
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TM
55-1510-215-10
SINGLE
ENGINE
CLIMB
SINGLE-ENGINE
TAKE
OFF
CONFIGURATION
CLIMB
FLAPS
0
PERCENT
PROP
FEATHERED
U-21G
POWER
-
TAKEOFF
T74-CP-700
Figure
7-15.
Single-Engine
Climb
7-33