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Pilot’s   alternate   static   air   source
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TM-1-1510-225-MTF Army Model C-12 Aircraft Manual
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Trim  and  rigging

TM   1-1510-225-MTF PROCEDURE TROUBLESHOOTING REFERENCE 16.   Engine   performance   at   maximum cruise   power   -   Perform   as   required (Chapter   4). *17. Engine ice vanes - Check operation as follows: (a)  LEFT  and  RIGHT  ACTUATOR switches - MAIN. (b)  LEFT  and  RIGHT  ENG  ANTI- ICE switches - ON. Check L and R  ENG  ANTI-ICE  annunciators illuminated. (c)   Torquemeters   -   Monitor   for approximately   a   10%   drop   in torque with ice vanes extended. (d)   LEFT   and   RIGHT   ENGINE ANTI-ICE switches - OFF. (e)   Torquemeters   -   Monitor   for   an increase in torque. (f)   MN   ENG   ANTI-ICE   circuit breakers - Pull. Check that L and R   ENG   ICE   FAIL   annunciator lights illuminate. (g)  LEFT  and  RIGHT  ACTUATOR switches   -    STANDBY.    Check that LEFT and RIGHT ENG ICE FAIL   annunciator   lights   extin- guish. (h)   LEFT   and   RIGHT   ENGINE ANTI-ICE switches - ON. Check that LEFT and RIGHT ENG ICE FAIL  annunciators  illuminate. (i)  LEFT  and  RIGHT  ENG  ANTI- ICE switches - OFF. (j) L and R MN ENG ANTI-ICE cir- cuit breakers - Reset. 2-49

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