Cessna 208B - Page 405

SECTION 7 CESSNA
AIRPLANE AND SYSTEMS DESCRIPTION MODEL
2088 (675 SHP)
ELECTRICAL SYSTEM (Continued)
M>>B,
TO ITANDs" ALTERNliTOi SYSTEM
TO STANDBY FLAP MOTOR
TO FUEL SELECTOR 0ll
WARN,NO SYSTEM
TO LEFT TURN AND BANK NDCITOR
TO ANNUNCIATOR PANEL
TO FIRS DETECTOR EISTIM
TO ITT 8NDICATOR
TO iYiL TOTALZER
TO LEFT FUEL OYANTTI NDlCATOR
70 FUEL FLOW ,ND,CA,r,rn
70 OIL TEMPERATURE OAmE
TO BLEEO AIR HEATER
TO LEFT ?#TOT HIATiil
TO WINDSYIELD ANTICE CONTROL
TO MAP LIGHTS
TO NAVOATlON LlGHTE
TO lNSTilUMENT LIQWTS
TO hlAONE LOMTS
TO WINO ICE OETECIOe LIGHT
TO l1ADlO AND FLOOD LEHTS
TO L.8. DRECTONAL EIRO
70 R H. ATTITUDE GYRO
TO TORQUE NO .
NOTE: A TORQUE INDICATOR
CIRCUIT BREAKER IS
INSTALLED ONLY ON
SOME CARGO VERSIONS.
2ea5mos
Figure 7-14. Typical Electrical System (Sheet 2 of 3)
1 7-86 U.S. Revision 23