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Figure 7A-102. One Engine Inoperative Maximum Cruise Power, 1900 RPM, ISA + 37 C
figure 7A-104 Holding time
TM-1-1510-218-10 Army C12C Aircraft Army C12D Aircraft Army C12T Aircraft Manual
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TM 1-1510-218-10
7A-115
Figure 7A-103.
Pressurization
Controller Setting for Landing