Hawker 900XP Flight System Overview
Hawker 900XP Flight System Overview
CRS 1
SPEED HDG ALT YD/AP DISC CRS2
VNAV 1/2 BANK CPL
PUSH PUSH PUSH
MWS PUSH PUSH
DIRECT IAS MWS
CANCEL DIRECT
F F
UP MACH SYNC
ENG REFS NAV/BRG RADAR GCS ENG REFS NAV/BRG RADAR GCS
S S
H
H
H
AUTO STANDBY AUTO
S EL TI
S EL TI HORIZON ECT LT
S
TD
ECT LT HORIZON
S
TD
M.456 29.92 IN WARN
200 UNARMED
240 E-BAT
ANNUN GLARESHIELD PUSH TO INHIB STALL IDENT 10 10 000 CANCEL ON CABIN CABIN PUSH TO INHIB GLARESHIELD
HIGH HIGH STALL IDENT
BRT PANEL 1 2 FAULT GPWS PANEL
STALL STALL
220 18800 DATUM DATUM
MWS
1 2 FAULT
STALL STALL
BAG
IDENT 1 IDENT 2 SSU FLAP TERR VLV A VLV B
VLV A VLV B 10 10 DIM IDENT 1 IDENT 2 FIRE
600 CABIN SQUAT OPEN OPEN
INHIB INHIB FLAP FAIL
DIM OPEN OPEN
CKPT 200 20 20 OVRD INHIB
TEMP INHIB INHIB INSTRUMENT PANEL
SPKR CKPIT CAB
INSTRUMENT PANEL 400 PANELS INST DISPLAYS
INHIB GS ALT
180 32 33 34 35 N 0
PANELS INST DISPLAYS CALLS
N
26 24
M .456 ELECT FUEL M .456 0 28
BI
340 OVHT
AL 000
CA
STD GEAR OVRD I STD
X1
30 340 33 30 340
T-F
FT
33 30 N ENT DOOR RUDDER N 33
AC
T
N APU ON N
FMS1 UNLOCKED BIAS G
FMS1 DTK 350 30 ICE PROT FUEL STALL FMS2
30 DBQ SELECTED XFD TFR IDENT PUSH G 30 MIN
DTK 350 CID DTK 350
E CABIN
CID 95.0NM AL0 3 CID CON
MX0 TROLLER
3
3
95.0NM AIR BRAKE A 95.0NM
TNU AN0SA R MAX
A
1.5 T-1.5A P.S.I. x 1000 T-1.5A 6
TFC > EMERG RATE
1.4 TFC > 2 2 TFC >
.6 TCAS 0FF 1 1 L R WHEEL
8
L R BRAKE
1.3 1000
0 0
1.2 FT/MIN
1 PRESS
OFF OFF
< ET 17:12 SUPPLY APR OVRD APR ARM < ET 17:12 10
.4 4 0
COM1 122.875 ATC1 1200 UTC 11:42 TAT 5 °C COM2 129.650 GS 275 TAS 250 SAT 0 °C ISA 0 °C COM1 122.875 ATC1 1200 UTC 11:42 TAT -15 °C COM2 129.650 2 D I F F P 30
3 2 1
.2 APR 50
BRT BRT APR BRT BRT
ARMED AL T
DIM DIM DIM DIM
OPEN
R0
Hawker 900XP
Collins Pro Line 21
TEST
1 1 1
1 2
WING/TAIL ANTICE DC
DC VOLTS AC VOLTS INV 1 INV 2
ICE DET L PUMP R PUMP GEN 1 BUS TIE GEN 2 NO SMKG
START START WARNING INDICATORS
A 3 5 5 5 7½ 2 1
4 6 8
AUTO ON ON CLOSE CLOSE CLOSE AUTO
0 20 100
2 10 80 120
10 30
1 2 3 4 5 6 7 8 9 10
XE FLT G/S OVHD OVHD PRESSN ICE 0 12 O 140
60
BUS INST PANELS INST PANEL VENTUR 1 DET A 14 F OFF
LTS LTS FAN 0
PROT LTS LTS F V
40
V
LH LH J 3 3 3 5 3 5 5 3 3 3
D.C. A.C.
PITOT AMPS PE B5
L R OVRD EMERG EMERG TRIP OPEN TRIP PS1 PS2 B4 B6 XS1 XS2 STOP STOP ON XE XS1 XS2 FLT BUS FLT FLT WING WING REFUEL
B 3 3 5 5 5 5 3 3 CABIN
ELECTRICAL
B2 B3 PANEL
FAIL FAIL FAIL ANNUN TIE
OPEN
ANNUN
DIM
ANNUN
DIM
OVER
FLOW
FUEL
XFD
CTL
B1 OFF
DIM TEST
FAN RH LH TFR
SCREEN HEAT PITOT/VANE HEAT ENG ANTICE ENG IGNITION ENG CMPTR ENG SYNC F/DK VLV MAIN AIR VLV
STALL STALL STALL STALL STALL STALL STBY ELEC CABIN CABIN PRESSN XFER
L ON R L ON R 1 ON 2 1 ON 2 1 AUTO 2 N1 FLOOD FLOOR ON OVRD DUCT TEMP CABIN TEMP OPEN 1 OPEN 2
IDENT IDENT VLV VLV WARN WARN INV PITCH
1 2 A B MOTOR MOTOR TRIM AUTO
LH RH OPEN OPEN
OPEN
+50 20 30
K 3 3 3 3 1 3 3 3 3
A S
O T
U F N2 0 100 10 40 LP
T AUTO AUTO O ON HORN GEAR GEAR GEAR SMOKE EMER HYD 1 ENTRY RUD
F 0 P INSTR LTS LTS WARN DET BRAKE LO DOOR BIAS
C 5 3 3 1 3 25 25 3 5
O 50
DIM STBY CTL PRESS PRESS
OF
OF
°C °C
F
CABIN LH
D U CT COOL HOT
FIRE FIRE DUCT MWS REFUEL STBY FUEL FUEL ENG 1 OFF OFF OFF OFF OVSPD PROT OFF CLOSE CLOSE OFF AUTO MANUAL CLOSE CLOSE
EXT BELL OVHT PWR CTL FUEL PUMP PUMP ANT ICE
SHOT 1 DET 1 PWR PUMP LH CTL ICE PROTECTION FUEL ENVIRONMENTAL
LH LH L 3 3 3 3 5 3 3 3 10 7½
EXTERIOR LIGHTS ICE AIR MAIN CABIN ORD AUX EMER HYD 2 AVN AVN
FIRE SEAT DET BRAKES AIR ALT SIGNS HYD BRAKE LO AUX AUX
D 5 5 1 3 25 25 3 3 5 ICE/LOGO STROBE NAV BEACON L LANDING R ENG 1 EXT ENG 2 EXT BELTS VLVS LO PRESS PRESS LH RH
LEVEL RH
1 ENG 1 ENG 2 1 ON
FIRE FIRE
FIRE MWS MWS REFUEL STBY FUEL FUEL LOW ENG 2 L T S S GAUGES & APU
EXT TEST PWR MSTR FUEL PUMP PUMP LIMIT ANT ICE O A H BELL CANCEL H
SHOT 2 2 VLV PUMP RH CTL TEMP G X O O
RH RH SENSOR O I T BELL BELL T M 3 3 3 3 3 3 3
2 CNCLD CNCLD 2 OFF
FUEL DUCT HYD BATT TKS OAT PE
OFF OFF OFF OFF OFF
EXT 1 EXT 2 QTY TEMP SPLY AMPS FLUID & LOW
E 3 3 3 15 5 2 2 5 3 5 FIRED FIRED LH PRESS CTL QTY FUEL VOLT
APU CONTROL
MAIN F/DECK CABIN PITOT STATIC A SCREEN B SCREEN RUD RUD WING
AIR AIR TEMP HEAT PLATE HEAT HEAT BIAS BIAS TAIL APU RPM %
VLV VLV CTL LH HEAT CTL CTL HEAT VLV ANTICE
1 MAN LH LH LH LH LH PUMP
0 20 40 60 80 100 120 N 3 3 3 3 3 3 15 7½ 10 2
RPM CCP1 CCP2
FUEL CABIN BRAKE FIRE FIRE CTL FWD PS2
LTS LTS 28 VDC
F 3 3 3 15 5 2 2 5 3 3 APU EGT °F X 100
QTY
RH
TEMP PRESS WARN EXT
EM LT
LOW
N 33 6 VOLT
PANEL A 6 3 0 3 6 9 12 15 APU BATT
MAIN RAM CABIN PITOT STATIC A SCREEN B SCREEN RUD RUD SQUAT MISC
AIR AIR TEMP HEAT PLATE HEAT HEAT BIAS BIAS SW 28 VDC SCRN OVERHEAT TEST EGT
VLV VLV CTL RH HEAT CTL CTL HEAT VLV LH
AUDIO 1
2 AUTO RH RH RH RH RH
"A" SCRN
GEN. LOAD P 1 3 5 ¾ ¾ 2 15 5 1 1
LIGHTS 5 1 7½ 3 3 2 A 0 .2 .4 .6 .8 1.0 1.2
AIRVIEW GALLEY CABIN COCKPIT COCKPIT TEMP CABIN CABIN FAN FAN
D.C. LOAD BLOWER BLOWER BLOWER
G 7½ 7½ 15 5 10 5 3 5 3 7½
AMP CTL COMM 1 ATC 1 NAV 1 DME 1 MASTER FLOOD
LH RH
FAN FAN
CTL
FAIL FAIL
LH RH
APU LIMITATIONS
STROBE BEACON LANDING TAXI NOSE CTR CHART INST INST LOGO
LH LH TAXI PED PANEL PANEL LH AUDIO 2 LIGHTS ESIS
OPERATING 0-30,000 FT
LH FLOOD EMERG
3 5 1 7½ 3 3 2 B 10 10 STARTING 0-20,000 FT Q 5 5 7½ 5 3 2 5 5 5 7½
CABIN STBY AMP CTL COMM 2 ATC 2 NAV 2 DME 2 10 10 LH RH LAV BAGGAGE AISLE VEST FLT G/S INST INST
PHONE COMM FAULT LOW OIL HIGH OIL
H 5 3 15 5 10 5 5 5 10 7½ 1 2 INST PANEL PANEL PANEL
SSU 1 SSU 2 PRESS TEMP
HF 1 EFIS 1 READING LTS RH RH LH
10 10 RH
NAV WING LANDING TAXI NOSE CONSOLE CONSOLE STORM TAS LOGO BLEED AIR APU CABIN
ICE RH RH TAXI DIM DIM PROBE RH 3 25 5 2 10 10 2 10 10 10 C VALVE FAIL GEN
RH RH LH INHIBIT
RESET
R 5 5 2 5 5 2 2 5 30 30
CVR HF 1 HF 1 L/H PFD 1 PFD 1 DCP 1 MFD 1 MFD 1 MFD 1 VANE CASE
R/T CPLR XFER HEATER PRI HEATER SEC HEAT TEST
RESET "B" SCRN BLEED AIR READY TO
RELAYS ON LOAD
UPPER UPPER AUX AUX AUX CONTROL CONTROL PCU CABIN CABIN
EFIS 2 LH RH VEST LH RH 1 2&3 MASTER MASTER
MAIN TEST LAMP TEST PS1 PS2
CABIN
2 2 1 2 10 10 2 10 10 7½ D
OVV TEST THRUST REVERSER
DATA SELCAL R/H PFD 2 PFD 2 DCP 2 MFD 2 MFD 2 IEC O XY
RADIO
ALT LOADER XFER HEATER HEATER S 5 1 3 5 1 3 1 5 5 25
GE
RELAYS
O FF
O XY
N NO
DCU 1 CDU 1 ADC 1 AHRS 1
GE
OI NORM NORM LH LH LH RH RH RH AURAL CMS CMS CABIN
O FF
L
THERAPUTIC OXYGEN
N NO
DEPLOY ANNUN STOW DEPLOY ANNUN STOW WARN CTL CTL AUDIO
7½ 5 5 2 2 3 3 3 2 2 2 2 E L
OI
GEN BLEED AIR 1 2 AMP
7½ 5 5 2 2 3 3 2 2 2 2 F
MASTER
IAPS 2 EGPWS RADAR PRI SEC CDU 2 GPS 2 PRI SEC PRI SEC START
SHUT
ON
115 VAC ESIS FSU 1 AVIONICS MASTER BYPASS MASTER VALVE VALVE VALVE VALVE
STOP
1 3 3 2 1 1 1 5 3 3 G OVER OVER OVER
FULL FULL FULL
OFF
FLOW PRESS FLOW
TRIM MSU MAIN SFD ADU CCP1 AHS FGC PRI SEC PE PS1 PS2
SYNCHRO 1 FAN SVO 1 PRESS TO TEST P TO T PRESS TO TEST
LEFT RIGHT
AVIONICS MASTER FEEDERS ON REFUEL
REFUEL
1 1 1 1 1 5 35 35 35 H ON APU
FIRE
AOA TRIM COCKPIT ELT CCP2 FGC PE PS1 PS2 OFF
SYNCHRO 2 SPEAKERS SVO 2
INHIBIT
OFF PUSH TO TEST
DEFUEL
OFF
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 OFF L
WING
R
FIRE
POWER MASTER VENTRAL
R0
Hawker 900XP
Collins Pro Line 21
SQ
ON OFF
STBY
OFF
PA HF 2 HF 2
OFF PA
OFF
EMERG
EMERG
NORM PHONE I/C AUTOCOM
BOOM-MIC NORM PHONE I/C AUTOCOM
V
O V BOOM-MIC
I O
C I
E C
SPKR- OFF OXY-MIC
E SPKR- OFF
TONE PHONE
TONE PHONE OXY-MIC
MENU DATA
ADV MENU DATA
MEM 2 ADV
S MEM 2
PU S
PU
H
H
EL MEM 3 ZOOM
ECT
S
EL
ECT MEM 3 ZOOM
S
UNIVERSAL SIGNAL LEVEL PASS FAIL
1/2
1/4 3/4
E F
DE-ICE
FLUID
INCREASE
GROUND
TEST
OXYGEN
DECREASE NORMAL
PASSENGER SUPPLY
EMERGENCY
PITOT ISOLATE
SUPPLY
O XY
PULL
GE
O FF
N NO
ISOLATE DEPRESS
TEST OI TO OPERATE
L
PULL TO OPERATE
PUSH FOR OFF ON L GEAR R GEAR NORMAL
R0