Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C
Page 24 of 95
If Neither Generator Will Reset:
7. Avoid IFR conditions if possible and LAND AT THE NEAREST SUITABLE AIRPORT.
8. Standby Battery Switch............................................................................... INDICATES ARM or ON
9. Non-essential equipment:
a. Left and Right BOOST PUMP……………………………………………………………….OFF
b. Left and Right TRANS. PUMP OVERRIDE………………………………………………..OFF
c. ENG AUTO IGNITION………………………………………………………………………..OFF
d. PROP ICE PROTECTION…………………………………………………………………...OFF
e. All Exterior Lights……………………………………………………………………………..OFF
f. Cabin Lights……………………………………………………………………………………OFF
g. VENT BLOWER…………………………………………………………………………….AUTO
h. CABIN TEMP MODE selector……………………………………………………………….OFF
i. INSTRUMENT EMERG LIGHTS……………………………………………….ON (if required)
j. INSTRUMENT INDIRECT lights……………………………………………….ON (if required)
10. The following equipment will be functional while the G1000 is powered from the aircraft’s battery
power, Avionics Master Power Switch is ON, and the [L GEN TIE OPEN] and [R GEN TIE OPEN]
annunciators are illuminated.
Pilot’s Attitude, Heading, Air Data, and Nav CDI
Copilot’s Attitude, Heading, Air Data, and Nav CDI
Engine Gauges
Com1, Pilot’s Audio Panel
GPS 1, GPS 2, VHF Nav1, VHF Nav2 (Nav2 Audio Inop)
MFD, Flight Director, Transponder 1
NOTE
Inoperative G1000 equipment items will be displayed in the ALERTS window on both PFDs.
The aircraft’s battery will continue to power the G1000 equipment for 30 minutes following
complete loss of normal electrical power generation. Once the aircraft’s battery can no longer
power the G1000, the standby battery will automatically power the standby attitude indicator,
altimeter vibrator, and the internal lighting of the three standby instruments for an additional 30
minutes.
11. Consider a Flaps UP Landing and Landing Gear Manual Extension to conserve battery power for
an instrument approach if needed.