BELL HELICOPTER BELL 430 - 30 SEC OEI; auxiliary fuel system; BUS INT; external power

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THIS IS AN UNCONTROLLED DOCUMENT.
THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.
THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE
FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.
PRODUCT DATA JANUARY 2003
caution, the engine 2 MGT and torque
scales change their limit. This caution does
not trigger the attention-getter. A flashing
down counter is also provided on the right
hand side of the No.2 MGT scale to indicate
the last ten seconds of the OEI event. In
the event that the ARINC 429 input
becomes invalid, the IIDS will trigger this
caution based on the parameter input.
“LDG GR UP”
This caution appears when the engine 2
FADEC/ECU sends its 30 second OEI
signal over the ARINC 429 data bus. This
advisory appears on the top left hand side
of the primary screen. In conjunction with
this caution the engine 1 MGT and torque
scale change their limit. This caution does
not trigger the attention-getter. A flashing
down counter is also provided on the left
hand side of the No.2 MGT scale to indicate
the last ten seconds of the OEI event. In
the event that the ARINC 429 input
becomes invalid, the IIDS will trigger this
caution based on the parameter input.
This advisory appears when the auxiliary
fuel system valve is open. This blue
advisory appears below the auxiliary fuel
quantity readout or as a white “A/FUEL OP”
in the W/C/A window when on the secondary
screen page 1 or on the start page.
This caution appears when the engine 1
FADEC/ECU sends its 30 second OEI
signal over the ARINC 429 data bus. This
advisory appear on the top left hand side
of the primary screen. In conjunction with
this caution the engine 1 MGT and torque
scale change their limit. This caution does
not trigger the attention-getter. A flashing
down counter is also provided on the left
hand side of the No.1 MGT scale to indicate
the last ten seconds of the OEI event. In
the event that the ARINC 429 input
becomes invalid, the IIDS will trigger this
caution based on the parameter input.
“30 SEC OEI” (Engine 1)
“30 SEC OEI” (Engine 2)
“OPEN” or “A/FUEL OP”
This white advisory appears when the
access door of the external power
receptacle is open. This advisory appears
in the W/C/A window only.
“EXT PWR”
This white advisory appears when the start
sequence of either engine is initiated. This
advisory appears in the W/C/A window only.
“START”
This advisory appears when the fuel tank
interconnect valve is fully open. This
advisory appears as a closed blue line
between the fuel quantity vertical scales
or as a white “FUEL INT” in the W/C/A
window when on the secondary screen page
2 or on the start page.
“FUEL INT”
This caution appears when the electrical
power bus interconnect relay is closed. This
caution appears between the generator
volt/amp digital readouts or as “BUS INT”
in the W/C/A window when on the secondary
screen page 1.
This amber caution appears when the
airspeed indication is below 55 kts and the
landing gear is up. (An audio warning horn
is also activated.) This caution appears only
in the W/C/A window.
“BUS INT”