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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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
“INV 1” or “1 INV”
This caution appears when either inverter
1 has failed or 28vdc to the inverter 1 is
not present. This caution actually uses the
inverter 1 voltmeter label as annunciator
by turning it amber and flashing or as “1
INV” in the W/C/A window when on page 1
or the start page.
“INV 2” or “2 INV ”
This caution appears when either inverter
2 has failed or 28vdc to inverter 2 is not
present. This caution actually uses the
inverter 2 voltmeter label as the annunciator
by turning it amber and flashing or as “INV
2” in the W/C/A window when on page 1 or
on the start page.
“DR LOCK”
This caution appears unless all passenger
and baggage compartment doors are
locked. This caution appears only into the
W/C/A window.
“BATT RLY”
This caution appears when the battery relay
in not closed. This caution appears only
into the W/C/A window.
“1 A/ICE”
This white advisory appears when the
engine 1 anti-ice system is turned on. This
advisory appears only into the W/C/A
window.
“A/ICE 2”
This white advisory appears when the
engine 2 anti-ice system is turned on. This
advisory appears only into the W/C/A
window.
“AUTO TRIM”
This caution appears upon AFCS mistrim
command. This caution appears only into
the W/C/A window.
“SCAS”
This warning appears when the AFCS
failure is declared by the FCC. This warning
appears only into the W/C/S window.
“AP”
This warning appears when all the AFCS
trim actuators are failed. This warning
appears only into the W/C/A window.
“AFCS PIT”
This warning appears when the AFCS pitch
trim actuator has failed. This warning
appears only into the W/C/S window.
“AFCS ROL”
This warning appears when the AFCS roll
trim actuator has failed. This warning
appears only into the W/C/A window.
“AFCS YAW”
“AFCS DISC”
This warning appears when the AFCS yaw
trim actuator has failed. This warning
appears only into the W/C/S window.
This warning appears when the AFCS has
disengaged from the aircraft controls. This
warning appears only into the W/C/A
window.
“O/TRQ
This warning appear when the mast torque
has exceeded 100%. This annunciator
remains latched until reset through the
attention-getter. This warning appears
above the mast torque display on the
primary screen.
3. Speed sensor fault (dual)
4. Memory fault
5. Fuel flow sensor fault
6. PLA fault
This caution appears above the engine 2
torque display on the primary screen.
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