Hawker 800 XP, Pilot Training Manual

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HAWKER 800 XP PILOT TRAINING MANUAL
FlightSafety
international
Revision 1 4-4
FOR TRAINING PURPOSES ONLY
Annunciator Cause for Illumination
Indicated vane heater has failed.
Indicates left or right side window
has overheated.
Airframe ice has been detected.
Indicates loss of left or right pitot
heat.
I n d i c a t e s l o w - p r e s s u r e o u t p u t
from airframe deicing pump.
Indicates airframe deicing quan-
tity low.
Indicates one or both continuous
ignition circuits is energized.
L VANE
HTR FAIL
R VANE
HTR FAIL
SIDE SCRN
OVHT
ICE
DETECTED
PITOT HTR
FAIL
ANTICE
LO PRESS
ANTICE
LO QTY
IGN ON
Annunciator Cause for Illumination
Indicated fuel filter differential is
excessive, or fuel temperature in
the indicated engine fuel pumps is
above normal.
Any valve in the refuel system is
not in the closed position.
Auxiliary fuel transfer lever is in
the open position.
Wing fuel crossfeed transfer lever
is in crossfeed or transfer position.
Fuel pressure in the supply line to
the respective engine is low.
ENG 1
FUEL
ENG 2
FUEL
REFUEL
ON
AUX FUEL
TFR
WING FUEL
XFD/TFR
FUEL 1
LO PRESS
FUEL 2
LO PRESS
Annunciator Cause for Illumination
Indicated AC bus bar has failed.
Indicated inverter has failed.
The standby inverter is selected
on.
XS 1
FAIL
XS 2
FAIL
XE
FAIL
INV 1
FAIL
INV 2
FAIL
STBY INV
ON
Table 4-2. ICE PROTECTION (Cont)
Annunciator Cause for Illumination
Either battery temperature is out-
of-limits high.
(Nicad batteries only.)
Indicated battery is not charging
or emergency contactor is open.
Either battery temperature is high
(Nicad batteries only.)
Indicated generator has failed.
The PS1 to PS2 bus-tie contactor
is open.
BATT 1
OVHT
BATT 2
OVHT
BATT 1
CNTCTR
BATT 2
CNTCTR
BATT 1
HOT
BATT 2
HOT
GEN 1
FAIL
GEN 2
FAIL
BUS TIE
OPEN
Table 4-4. DC POWER
Table 4-3. FUEL Table 4-5. AC POWER