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Textron Cessna Grand Caravan Ex 208B - Starting Engine (with External Power)

Textron Cessna Grand Caravan Ex 208B
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SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
STARTING ENGINE (With External Power)
CAUTION
The external power unit must be rated at 24.0 - 28.0
Volt with a minimum output of 800 amps and a
maximum output of 1700 amps.
1. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. Engine Indication System . . . . . . . . . . CHECK PARAMETERS
(verify no red X’s)
4. EXTERNAL POWER Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
5. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify 20 VOLTS minimum shown)
6. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
7. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. External Power Unit. . . . . . . . . . . . . . . . . . . ENGAGE; then ON
9. EXTERNAL POWER Switch . . . . . . . . . . . . . . . . . . . . . . . . BUS
CAUTION
Make sure the EMERGENCY POWER lever is in the
NORMAL position or an over-temperature condition will
result during engine start.
10. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
11. BCN Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
12. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
13. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify 24.0 to 28.5 volts shown)
14. EXTERNAL POWER Switch. . . . . . . . . . . . . . . . . . . STARTER
15. EMERGENCY POWER Lever. . . . . . . . . . . . . . . . . . . NORMAL
16. Red EMERG PWR LVR Annunciator . . . . . . . . . . . . . . CHECK
(verify annunciator is not shown)
17. Propeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
(verify that all people and equipment are at a safe distance from
the propeller)
(Continued Next Page)
208BPHCUS-004-26

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