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BELL HELICOPTER BELL 430 - alternate input source; start abort

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71
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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
“ALT”
This white advisory appears when either
MGT, Ng, Np or engine torque is operating
on its alternate input source (analog or
ARINC 429). This advisory appears at the
bottom of the related vertical scale. For
Ng, the continuous line below the digital
readouts changes to a dashed line since
the display does not allow for the advisory.
“A/RLT” (Engine 1)
“SRT ABT” (Engine 2)
This caution appears when engine 2
FADEC/ECU has initiated a start abort
sequence on engine 2. This caution appears
above engine 2 torque display on the
primary screen.
This caution appears when engine 1
FADEC/ECU has initiated a start abort
sequence on engine 1. This caution appears
above engine 1 torque display on the
primary screen.
This white advisory appears when engine
2 FADEC/ECU has detected a soft fault and
the PLA is below ground idle on engine 2.
This advisory appears only into the W/C/
A window.
“SRT ABT” (Engine 1) “M/ECU 2” (Engine 2)
This caution appears when engine 2
FADEC/ECU is performing an auto-relight
sequence by powering the ignition exciters
on engine 1. This caution appears above
engine 2 torque display on the primary
screen.
This white advisory appears when engine
1 FADEC/ECU has detected a soft fault and
the PLA is below ground idle on engine 1.
This advisory appears only into the W/C/
A window.
“A/RLT” (Engine 2)
“1 M/ECU” (Engine 1)
“FAIL
This caution appears when either MGT, Np,
Nr, mast torque or engine torque input(s)
are failed or unavailable. This caution
appears at the bottom of the related vertical
scale.
This caution appears when engine 1
FADEC/ECU is performing an auto-relight
sequence by powering the ignition exciters
on engine 1. This caution appears above
engine 1 torque display on the primary
screen.
This white advisory appears when engine
2 FADEC/ECU has recorded an OEI range
usage and the PLA is below ground idle
on engine 2. This advisory appears only
into the W/C/A window.
“M/OEI 2” (Engine 2)
This white advisory appears when engine
1 FADEC/ECU has recorded an OEI range
usage and the PLA is below ground idle
on engine 1. This advisory appears only
into the W/C/A window.
“1 M/OEI” (Engine 1)

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