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IGNITION   and   ENGINE START  switch  -  ON
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TM-1-1510-225-MTF Army Model C-12 Aircraft Manual
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Engine  restart

TM   1-1510-225-MTF PROCEDURE TROUBLESHOOTING REFERENCE LOW  SPEED  SYSTEMS  CHECK  (CONT) propeller  unfeathering  -  Check  as  fol- lows: (a) AUTOFEATHER switch - ARM. (b) Airspeed - 120 KIAS. (c) PROP levers - Set 2000 RPM. (d)  POWER  levers  -  Set  as  required to arm autofeather system. (e) CONDITION lever (engine to be feathered) - IDLE CUTOFF. *  (f) Record  the  time  from  fuel  cutoff until  propeller  is  feathered.  (Pro- peller  is  considered  to  be  feath- ered   when   the   blades   are   indi- vidually visible to the human eye, but the propeller is still rotating.) Time  to  feather  shall  not  exceed 10  seconds. NOTE For  proper  autofeather  operation,  propeller  must stop completely. (g) Engine cleanup. (1)   CONDITION   lever   -   FUEL CUTOFF. (2)   AUTO   IGNITION   switch   - OFF. (3)   AUTOFEATHER   switch   - OFF. (4) GEN switch - OFF. 2-58

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