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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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
“L W/S HOT”
This caution appears when the left over
temperature sensor detects an overheat
(54.5°C/130°F) condition in the left
windshield heater circuit. This caution
appears only into the W/C/A window.
“OVSPD” (Np engine 1)
This caution appears when an internal fault
within the IIDS has been detected by the
continuous BIT. This caution appears only
into the W/C/A window.
“IIDS”
This caution appears when an Ng
overspeed has been detected by the engine
2 FADEC/ECU Ng > 106%. This caution
appears above the engine 2 Ng digital
readout.
“OVSPD” (Ng engine 2)
“R W/S HOT” “OVSPD” (Ng engine 1)
This caution appears when the right over
temperature sensor detects an overheat
(54.5°C/130°F) condition in the right
windshield heater circuit. This caution
appears only into the W/C/A window
This caution appears when an Ng
overspeed has been detected by the engine
1 FADEC/ECU Ng > 106%. This caution
appears above the engine 1 Ng digital
readout.
“PARK BRK”
This caution appears when the parking
brake is on. This caution appears only in
the W/C/A window.
This white advisory appears when the float
system is armed after pressing the float
arm push-button switch on the center
pedestal. This advisory appears only into
the W/C/A window.
“FLTS ARM”
This caution appears when an Np
overspeed has been detected by the engine
1 FADEC/ECU Np > 115%. This caution
appears above the engine 1 Np digital
readout.
“C/HK ARM”
This white advisory appears when the cargo
hook system is armed after pressing the
cargo hook switch to the armed position.
This advisory appears only into the W/C/
A window.
“OVSPD” (Np engine 2)
This caution appears when an Np
overspeed has been detected by the engine
2 FADEC/ECU Ng > 115%. This caution
appears above the engine 2 Np digital
readout.
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