SINGLE-ENGINE GO-AROUND - TM-55-1510-221-CL

LOSS OF PRESSURIZATION (ABOVE 10, 000 FEET)

ENGINE FIRE IN FLIGHT (IDENTIFIED) - TM-55-1510-221-CL_30

TM-55-1510-221-CL Maintenance Test Flight Manual Army Model RD-12G
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TM 55-1510-221-CL 3. Propeller lever (operative engine) - HIGH RPM. SINGLE-ENGINE GO-AROUND 1. Power - Maximum allowable. 2. Gear - UP. 3. Flaps - As required. 4. Landing lights - OFF. 5. Power - As required. 6. Yaw damp - As required. PROPELLER FAILURE (OVER 2080 RPM) 1. Power lever (affected engine) - IDLE. 2. Propeller lever - FEATHER. 3. Condition lever - As required. 4. Propeller synchronization - OFF. 5. Engine cleanup - As required. FIRE ENGINE/NACELLE FIRE DURING START OR GROUND OPERATIONS 1. Propeller levers - FEATHER. 2. Condition levers - FUEL CUTOFF. 3. Fire pull handle - Pull. 4. Push to extinguish switch - Push. 5. Master switch - OFF. ENGINE FIRE IN FLIGHT (FIRE PULL HANDLE LIGHT ILLUMINATED) 1. Power lever - IDLE. E-8

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