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f. ENGINE ACCEPTANCE AT MAXIMUM CRUISE POWER
G. AVIONICS FLIGHT CHECKS.
TM-55-1510-222-MTF Army RC-12K Aircraft Manual
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TM 55-1510-222-MTF
*c. Free air temperature
d.
Propeller
RPM
*e.
Torque
*f. N
1
*g. TGT (must not exceed 810°C)
7. Repeat for opposite engine.
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