Garmin Cessna Caravan G1000, Процедура оформления заказа

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G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90 Page 3-5
190-00682-00 Revision 5
3.2
Electrical Load Test Procedures
CAUTION - De-icing heat elements will be energized during this procedure. Ensure aircraft is safe for the
application of anti-ice heat.
1. Using a 28 VDC ground power cart apply external power to the aircraft. Set BAT , EXT PWR and
AVIONICS MASTER switches to ON . Allow all aircraft systems to complete initialization and operate
for 15 minutes.
2. Set the clamp-on meter to read DC amps. Follow meter manufacture instructions to zero the amp-
meter. Place meter around the ground power cart DC power cable.
3. Make or verify the following switch selections: Switches not listed are not required.
•
EXT PWR – OFF
•
AVIONICS MASTER PWR – OFF
•
BAT – OFF
•
GEN 1 – OFF
•
GEN 2 - OFF
•
LEFT /RIGHT ENG AUTO IGNITION – OFF
•
BUS SENSE – NORM
•
GEN TIES – NORM
•
LEFT/RIGHT ENGINE ANTI-ICE – OFF
•
AUTOFEATHER – OFF
•
LEFT/RIGHT LANDING LIGHTS – OFF
•
TAXI LIGHTS – OFF
•
ICE LIGHTS – OFF
•
NAV LIGHTS – OFF
•
RECOG LIGHTS – OFF
•
PILOT WSHLD ANTI-ICE – OFF
•
COPILOT WSHLD ANTI-ICE – OFF
•
PROP ANTI-ICE – OFF
•
LEFT/RIGHT FUEL VENT ICE PROTECTION – OFF
•
SURFACE DEICE – OFF
•
STALL WARN ICE PROTECTION – OFF
•
LEFT/RIGHT PITOT ICE PROTECTION – OFF
•
BEACON LIGHTS – OFF
•
STROBE LIGHTS – OFF
•
TAIL FLOOD LIGHT – OFF
•
PROP SYNC – OFF (extended)
•
STANDBY BATTERY – OFF (extended)
•
CABIN BAR – OFF