6 8
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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
c a u t i o n , t h e e n g i n e 2 M G T a n d t o r q u e
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
t h e e v e n t t h a t t h e A R I N C 4 2 9 i n p u t
becomes invalid, the IIDS will trigger this
caution based on the parameter input.
“LDG GR UP”
This caution appears when the engine 2
F A D E C / E C U s e n d s i t s 3 0 s e c o n d O E I
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
t h e e v e n t t h a t t h e A R I N C 4 2 9 i n p u t
becomes invalid, the IIDS will trigger this
caution based on the parameter input.
This advisory appears when the auxiliary
f u e l s y s t e m v a l v e i s o p e n . T h i s b l u e
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
F A D E C / E C U s e n d s i t s 3 0 s e c o n d O E I
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
t h e e v e n t t h a t t h e A R I N C 4 2 9 i n p u t
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”
T h i s w h i t e a d v i s o r y a p p e a r s w h e n t h e
a c c e s s d o o r o f t h e e x t e r n a l p o w e r
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
i n t e r c o n n e c t v a l v e i s f u l l y o p e n . T h i s
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.
T h i s a m b e r c a u t i o n a p p e a r s w h e n t h e
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”
Содержание BELL 430
Страница 1: ...Product Data ...