Date post: | 27-Mar-2018 |
Category: |
Documents |
Upload: | hoangnguyet |
View: | 230 times |
Download: | 3 times |
COPILOTAIR
I
IPULLON
CABIN /COCKPIT
AIRI
IPULL
INCR CKTDECR CAB
Level C Full Flight Simulator
© FlyRight February 18th, 2015
FOR TRAINING PURPOSES ONLY
NOSE UP
NOSE DOWN
PITCH
TR
IM
CHRONOMETER
NOSE UP
NOSE DOWN
PI
TC
H
TR
IM
CHRONOMETER
GSPTTG
ET
NAV DATA TIMERSET
S/S
CRSSEL
MAPARC
HSIARC
MAP
DHSET
TST
WX
PREACT
XFR
COURSE
YAWENG
SR
Collins
YAW
APENG
1/2 Ø
L R
DN
UP
SELECTED ALTITUDE
Collins
ADF
ACT
STO
TESTV
TONEADF
OFF
ANT
MEM
XFR
MEM
Collins
2
1ALT
V
ALTON
OFF
STBYATC
PRE
IDENT
TEST
Collins
MEM
XFR
MEM
NAV
ACT
STO
TESTV
HLDON
OFF
Collins
MEM
XFR
MEM
NAV
ACT
STO
TESTV
HLDON
OFF
Collins
COMSTO
TESTV
SQOFFON
ACT
MEM
XFR
MEM
OFF
Collins
COMSTO
TESTV
SQOFFON
ACT
MEM
XFR
MEM
OFF
NRST OBS
KASE
KASE
137
D
PROP SYNON
OFF
VG FASTERECT
RADIO CALL
N225TF
TAWSFLAPOVRD
TAWSCAUTION
TAWSINHIBIT
P/TEST
ALT
BARO
GYROSLAVING
+-
SLEW MODE
DG
COLLINS
Y D
VERTICALSPEED
1 2
3
3
21
0
.5
.5
DN
UP
INSTANTANEOUSFPM X 1000
EADI/EHSIDIM
ELAPSEDTIME
AUX POWEREFIS
ON
TEST
OFF
HORN
SILENCE
AUX TEST
AUXON
GYROSLAVING
+-
SLEW MODE
DG
COLLINS
VERTICALSPEED
1 2
3
3
21
0
.5
.5
DN
UP
INSTANTANEOUSFPM X 1000
54
6ALT
OFF
T O T E S T
PRESS
MASTERWARNINGPUSH TO RESET
MASTERCAUTION
PUSH TO RESET
MASTERCAUTION
PUSH TO RESET
MASTERWARNINGPUSH TO RESET
EXTINGUISHERPUSH
DISCH OK
EXTINGUISHERPUSH
DISCH OK
FRICTIONLOCK
FRICTIONLOCK
LEFT RIGHT
RUDDER TAB
5
3
1 0 1 3 5
5
3
1 0 1 3 5
AILERON TRIM
LEFT RIGHT
0
DN
PITCH
TRI
M
UP
FEATHER
PROP
TAKEOFFLANDING
ANDREVERSE
CONDITI
ON
HIGHRPM
INCR
CAUTION
POWER
LIFT
LIFT
IDLEGO AROUND
FLAP
COCKPIT VOICE RECORDER
TEST ERASE
HEADSET600 OHMS
TAWSWARN
P/TEST
BELOWG/S
P/CANCEL
TAWSWARN
P/TEST
BELOWG/S
P/CANCEL
INVERTER DOOR UNLOCKED ALT WARN R ENG FIRE
L FUEL PRESS ----------------- ----------------- R FUEL PRESS
L OIL PRESS A/P TRIM FAIL R OIL PRESS
----------------- L BL AIR FAIL A/P FAIL R BL AIR FAIL -----------------
L ENG FIRE
-----------------
----------------------------------
L DC GEN ---------- HYD FLUID LOW RVS NOT READY --------- R DC GEN
L CHIP DETECT ---------- ---------- DUCT OVERTEMP ---------- R CHIP DETECT
L ENG ICE FAIL ---------- BATT CHARGE EXT POWER ---------- R ENG ICE FAIL
L AUTOFEATHER ---------- ELEC TRIM OFF AIR COND N1 LOW ---------- R AUTOFEATHER
L ENG ANTI-ICE BRAKE DEICE ON LDG/TAXI LIGHT PASS OXY ON ELEC HEAT ON R ENG ANTI-ICE
L IGNITION ON L BL AIR OFF ---------- FUEL CROSSFEED R BL AIR OFF R IGNITION ON
BUSFEEDERS
PROPDEICE
IGNITORPOWER
STARTCONTROL
BUSFEEDERS ITT TORQUE PROP
TACHFUELFLOW
TURBINETACH
OIL PRESS
OILTEMP
FUEL SYSTEM
FIREWALLVALVE
STANDBYPUMP
QTYIND
PRESSWARN
AUXTRANS
FERCROSSFEED
PRESSWARN
QTYIND
AUXTRANS
FERSTANDBY
PUMPFIRE
WALLVALVE
ENGINE INSTRUMENTS
LEFT RIGHT
LEFT
RIGHT
OPEN
FIREWALLSHUTOFF
VALVE
CLOSED
NO 3 LEFTFLAP
LEFT LEFT NO 3
OPEN
FIREWALLSHUTOFF
VALVE
CLOSED
NO 4 RIGHT RIGHT RIGHT NO 4CONTROL GOV
MOTOR
PROPDEICE
CONTROL
PROP
50 25 20 5 5 5 50
50 25 5 5 5 5 50
5 5 5 5 5 5 5
5 10 5 5 5
5 5 5 5 5 5 5
5 5 5 5 10 5
CROSSFEED FLOWSTANDBY PUMPON
AUX TRANSFEROVERRIDE
OFF
FUEL QUANTITYMAIN
AUXILIARY
AUTO
NO
TRANSFER
SEE MANUAL FORFUEL CAPACITY
ENGINE ENGINE
LEFT RIGHT
STANDBY PUMPON
AUX TRANSFEROVERRIDE
OFF
AUTO
NO
TRANSFER
6
QTYLBS X 100
0
2
14
12
10
84
MAIN TANKONLY
6
QTYLBS X 100
0
2
14
12
10
84
MAIN TANKONLY
CABINPRESSDUMP
TEST
PRESS
ELEVTRIM
OFF
DEPRESSURIZE CABINBEFORE LANDINGWARNING
RUDDERBOOST
OFF
RATE
MIN
MAX
CABINALT
CABINALT
1000FEET
15 17 19 21
23
2
5
30 35
ACFT ALT1000 FT
2 3
4
5
6
7
8 9 10 11 13 -1 0 1
CABIN
NO SMOKE& FSB
OFF
COFFEE
FURNON
DI
M
OFF
OFFOFF FSB
ENVIRONMENTALMANUAL
TEMPVENT
BLOWER
BLEED AIR VALVESOPENLEFT RIGHT
INCR
DECR
HIGH
LO
AUTO
CABIN TEMP
ENVROFF
INSTR & ENVIR OFFAFT
BLOWERON
ELECHEAT
OFF OFF
INCR MANHEAT
CABIN TEMP MODE
OFF
AUTO
MANCOOL
OFFTEST SWITCHENG FIRE SYS
LEXTR
LDET
RSTALLWARNTEST
HOURS 1/10
0 0 0 0 7 8
FLIGHT50 80
0 100
CABIN AIR
°F
4 53 6
GYROSUCTION
INCHES OF MERCURY
35K 15K
10PSI
0 20
PNEUMATICPRESSURE
I I
I I I
I I I
I I I I I I I I I I I I I
MICNORMAL
OXYGENMASK
BRIGHT
OXYGENSUPPLY PRESSURE
0
5001000
1500
2000
USE NOOIL
PSIPROP AMPS
10 20
0 30
LDG GEAR CONTROL
HYD FLUIDSENSOR
TEST
DOWNLOCK REL
NOSE
L R
GEARDOWN
DN
HD LTTEST
LANDINGGEAR
RELAY
2
UP
LIGHTS
LANDING TAXI ICE NAV RECOG
LEFT RIGHT OFF
ENG AUTOIGNITION
ARM
RIGHTOFF
LEFT
IGNITION ANDENGINE START
STARTER ONLY
OFF
RIGHTLEFTON
ENGINE ANTI-ICERIGHT
ONLEFT
OFF
MAIN
ACTUATORSTANDBY
ARM
TEST
OFF
AUTOFEATHERTEST
OFF
PROP GOV
AVIONICSMASTER PWR
OFF
MICNORMAL
OXYGENMASK
INVERTERNO 1
NO 2
GENRESET
ON
OFFGEN 2GEN 1BATT
OFF
ON
OFF
PARKING BRAKE
MASTER SWITCH
ICE PROTECTION
OFF
LEFT RIGHT
WSHIELD ANTI-ICENORMAL
PILOT COPILOT
OFF
VENTFUELPROP
AUTO MANUAL
MANUAL
BRAKEDEICE
SURFACEDEICE
SINGLESTALLWARN PITOT
LEFT RIGHT
- OFF -
OFF
BEACON STROBE
TAILFLOOD
OFF
LIGHTS
PILOTAIR
I
IPULLON
DEFROSTAIR
I
IPULLON
GEARWARN HORN
SILENCE
HI
OXYGENPULL ONSYSTEM READY
PASSENGERMANUAL DROP OUT
OPERATIONAL LIMITATIONS
CAUTION
STALL WARNING IS INOPERATIVE WHEN MASTER SWITCH IS OFFSTANDBY COMPASS IS ERRATIC WHEN WINDSHIELD ANTI-ICE AND/OR AIR CONDITIONING IS ON
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITHTHE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS
NO ACROBATIC MANEUVERS INCLUDING SPINS ARE APPROVEDTHIS AIRPLANE IS APPROVED FOR VFR, IFR, & DAY & NIGHT OPERATION AND IN ICING CONDITIONS
WINDSHIELD WIPERSOFF
MASTERPANELLIGHTS
ON
OFF
ENGINEINSTRUMENT
LIGHTS
BRT OFF
AVIONICSPANELLIGHTS
BRT OFF
OVERHEADSUB PANEL& CONSOLE
LIGHTS
BRT OFF
SIDEPANELLIGHTS
BRT OFF
COPILOT GYROINSTRUMENT
LIGHTS
BRT OFF
COPILOTFLIGHTLIGHTS
BRT OFF
PILOTFLIGHTLIGHTS
BRT OFF
OVERHEADFLOODLIGHTS
BRT OFF
INSTRUMENTINDIRECT
LIGHTS
BRT OFF
PARK SLOW
FAST
DO NOT OPERATEON DRY GLASS
AIRSPEEDS (IAS)
MAX GEAR EXTENSION 181 KNOTS
MAX GEAR RETRACT 163 KNOTS
MAX GEAR EXTENDED 181 KNOTS
MAX APPROACH FLAP 200 KNOTS
MAX FULL DOWN FLAP 157 KNOTS
MAX MANEUVERING 181 KNOTS
% LOAD
020 40 60 80
100
PUSHFOR VOLTS
010 20
30DC VOLTS
% LOAD
020 40 60 80
100
PUSHFOR VOLTS
010 20
30DC VOLTS
FREQ
390 400 410
PUSHFOR VOLTS
100110 120
130AC VOLTS
420380
3 N 33
POS 0 30 60 90 120 150 180 210 240 2
70 3
00 33
0 360
STEER 0 29 59 90 121 151 182 211 242 2
71 3
00 3
29 3
59
COMPASS CORRECTIONCALIBRATE WITH
ENGINE ON
EFIS
TEST ADCTESTCMPST
NORMAL
POWER
OFF
Collins
HDGCOURSE
AIRBEECHCRAFT
ALTALERT
O
I
M
DH
KNOTS40
60
80
100
140160180
200
220
240
260280
300
120
0
2
3
5
4
6
1
PPH X 100
FUELFLOW
0
2
3
5
4
6
1
PPH X 100
FUELFLOW
PROP
RPM X 100
230
5
10
13
1415
161718
19
20
21
22PROP
RPM X 100
230
5
10
13
1415
161718
19
20
21
22
ITT
°C X 100
6
2
4
5
8
9
7
START 12
ITT
°C X 100
6
2
4
5
8
9
7
START 12
OIL
PSIC
50
100
200
150
0200
60
20
100
140OIL
PSIC
50
100
200
150
0200
60
20
100
140
4TURBINE
% RPM
20
4060
80
100
110 078.0
4TURBINE
% RPM
20
4060
80
100
110 078.0
24
0
2
1410
8
12
26
18
20
22
6
4
16
TORQUE
FT LB X100
82
24
0
2
1410
8
12
26
18
20
22
6
4
16
TORQUE
FT LB X100
82
2CABIN CLIMBTHDS FT PER MIN
4
6
421
1
.5
.5
0
CABINALT
0
540
30
35
2520
10
15
PSI
1
2
345
6
7
FLAPS
DOWN
UP
TAKEOFFAND
APPROACH
20
60
80
PILOT’S EMERGENCYSTATIC AIR SOURCE
NORMAL ALTERNATE
SEE FLIGHT MANUAL PERFORM-ANCE SECTION FORINSTR CAL ERRROR
UP
FLAPAPPROACH
DOWN
5
DN
0
UP
10
UP
FUELCUTOFF
REVERSEONLY WITH
ENGINESRUNNING
GROUNDFINE
REVERSE
LOWIDLE
HIGH IDLE
CH SEL PWR
NM HLD KT MIN ID
Collins
Beechcraft KingAir B200
WARNINGS WEATHERLIGHTS
ENVIRONMENTAL FLIGHT ELECTRICAL
PROP
ALERT
LEFTPRESSOXYGEN
NO 2RIGHT
NO 1LEFTOUTSIDEPITCHPILOTPILOTALT
POWERWARNLEFTSTALL
WARN
PLT FLTAVIONICS
COPLT FLT
AVIONICS
DETCHIPDETR
STBY ENGANTI-ICE
MN ENGANTI-ICE
FUELCONTROL
HEAT
LEFTLEFTLEFTFIRELEFT
INSTR
& ENGINSTR
BLEEDAIR
WARNLANDING
GEARANN FUEL
VENT
GENCONTROL
BUSFEEDERS
ALTMAIR DATA
BLEEDAIR
CONTROL
ENGINSTR
POWER
SYNC
LEFT
COPLT BOOSTENCD ALTM
RUDDERCOPLTTEMP
AIRTEMP
TRIMTURN &
SLIP
CONTROLCONTROL
RIGHTCONTROL
FEATHER RIGHTRIGHTRIGHTRIGHT
AUTO
LEFT
RIGHT
INDINDRIGHT
SURF
DEICE
WSHLD
WIPERRIGHT
AVIONICS
MASTER
NAVCOMMAVIONICS
NO. 2NO. 2NO. 2
COMPASS
NO. 2
CABINPILOTAURAL
AUDIOAUDIOWARN
COPILOT
AUDIO
MASTER
POWER
CIGAR
LIGHTER
RCDR
ANN
RADIO
EFISFANS
DME
TCAS
FSB &CABIN
CONSOLEINDIRECT
INSTRREADING
TAWS
SIDE PNL
NAVCOMMAVIONICS
NO. 1NO. 1NO. 1
COMPASS
NO. 1
ENGINES
FURNISHING
5 5 5 5 5 7½
5 5 5 5 7½
5 10 5 7½ 5
5 5 7½ 7½
5
1 2 5 2
5 5
7½
7½
7½
5 5 5
5 5 5
5 5
3 5 5
5 1 5
1 5
2 2
7½
2 7½
5 5
5 10
50
50
50
50
10
10
2 2
30 7½ 2 3
30 7½ 2 3
DSPLPILOTEADI
PRCSR
VOICE
7½ 25
BAT
DSPPILOTEHSI
EFISAUX
1 155
DMEXPNDR
NO. 1
NORMAL
2 7½3
NO. 1 SERVO
AP
10
STBY
SUB PNLOVHD&
NO SMK
ACC
10
RMI
NO. 2
2
ADF
2
RMI
NO. 1
2
FMS
2
FCS
2
POWER
NO. 2
XPNDR
NO. 2
3
AVIONICSGPS
3
ALTM
BRAKE
DEICE
5
PAGING
VOL
AUDIOSPKR
OFF
HOTINTPH
OFF
AUTOCOMM
OFF
AUDIOSPKR
OFF
INTPH
VOLVOICE
RANGE
BOTH
COMM NAV MKR BCN DME
1 2 1 2 1 2 1 2 ADF
COPILOT AUDIO OFF
AUTOCOMM
OFF
VOICE
RANGE
BOTH
AUDIOEMER
NORM
COMM-1
COMM-2
PA
VOL
COMM-1
COMM-2
PA
VOL
AUXARM
AUXON
OFF
HORN
SILENCE
ON
TEST
STBY HORIZ PWR
PILOT AUDIO OFF
COMM NAV MKR BCN DME
1 2 1 2 1 2 1 2 ADF
PUSHON / OFF
GNDCOMM
PWR
AUX TEST DIM
ANNPUSH BRT
ENCDALTM
1
2VOL VOL
DME1 2
VOL
MKR BCN 1 & 2HI
LO
ONSBYOFF
402015
105
3
ABOVENORMBELOW
PUSH FOR FLPUSH TO TST
FAILTCAS BENDIX/KING
TST FL
KNOTS40
60
80
100
140160180
200
220
240
260280
300
120
NAV APPR B/CHDG
VS IASALT
CollinsTRIM HDG ARM DIS ARM
TEST
ALT SEL
CLIMB
DSC
L ENVIR FAIL CABIN DOOR R ENVIR FAIL R OIL PRES LO
----------------- CARGO DOOR R AC BUS -----------------
L BL AIR FAIL A/P TRIM FAIL ARM EMER LITES A/P FAIL R BL AIR FAIL
----------------- ----------------- ----------------- ----------------- -----------------
L OIL PRES LO
L AC BUS
CABIN ALT HI ----------------- CABIN DIFF HI R FUEL PRES LOL FUEL PRES LO
L DC GEN L FUEL QTY STALL HEAT BATTERY CHARGE --------- R FUEL QTY
L FW VALVE L COL TANK LOW L GEN TIE OPEN BATT TIE OPEN R GEN TIE OPEN R COL TANK LOW
L ENG ICE FAIL ---------- HYD FLUID LOW ---------- ANN PWR SOURCE ----------
L FIRE LOOP L PITOT HEAT XFR VALVE FAIL ---------- ---------- R PITOT HEAT
L NO AUX XFR AUTOFTHER OFF ---------- ---------- ---------- AFX DISABLE
INBD WG DEICE YD/RB FAIL ---------- TAIL DEICE ---------- RUD BOOST OFF
R DC GEN
R FW VALVE
R ENG ICE FAIL
R FIRE LOOP
R NO AUX XFR
OUTBD WG DEICE
L AUTOFEATHER L IGNITION ON ---------- ---------- ---------- R IGNITION ON
L ENG ANTI-ICE ---------- ---------- MAN TIES CLOSE ---------- ----------
L ENVIR OFF RDR PWR ON FUEL TRANSFER TAXI LIGHT ---------- EXTERNAL POWER
R AUTOFEATHER
R ENG ANTI-ICE
R ENVIR OFF
FIRE PULLFIRE PULL
STBYPUMP
QTYIND
PRESSWARN
QTYWARN
TRANS PRESSWARN
QTYIND
QTYWARN
AUXTANKPUMP
STBYPUMP
LEFT RIGHT
15 5 5 5 5 5 5 5 5 5 15
FIREWALLVALVE
5
FIREWALLVALVE
10
AUXTANKPUMP
TRANSFERFLOW
STANDBY PUMPON
AUX PUMPON
OFF
FUEL QTYMAIN
AUX
AUTO
LEFT ENGINE RIGHT ENGINE STANDBY PUMPON
OFF
AUTO
AUX PUMPON
AUTO
AUTO
OFF
USABLE FUEL LEFT MAIN 1621 LBS
AUX 621 LBS SEE MANUALUSABLE FUEL RIGHT MAIN 1621 LBS
AUX 621 LBS SEE MANUAL
QUANTITYLBS X 100
0
2
1412108
4
MAIN TANKONLY
6
16
1820
QUANTITYLBS X 100
0
2
1412108
4
MAIN TANKONLY
6
16
1820
LDG GR CONTROL
DOWNLOCKREL
NOSE
L R
DN
LANDINGGEAR
RELAY
2
UP
ENGINE ANTI-ICERIGHT
ONLEFT
OFF
MAIN
ACTUATORSSTANDBY
ARM
TESTLOW PITCH
PROP TESTOVERSPEED
AVIONICS
OFF
EXTPWR
OFF
R GENL GENBATTOFF
ON MASTER SWITCH
ICE PROTECTION
OFF
LEFT RIGHT
WSHIELD ANTI-ICENORMAL
PILOT COPILOT
OFF
FUEL VENT
PROPAUTO MANUAL
MANUAL
SURFACEDEICE
SINGLE
STALLWARN
PILOTAIR
I
IPULLON
DEFROSTAIR
I
IPULLON
ON
OFF
XFR
ENG AUTO IGNITION
ARM
OFF
RIGHTLEFT
AC BUS
RIGHTLEFT
IGNITION ANDENGINE START
STARTER ONLY
OFF
RIGHTLEFTON
OXYGENPULL
ON
GEN TIESMAN CLOSE
OPEN
BUS SENSERESET
TEST
OFF
AUTOFEATHER
OFF CABINOXYGENPULLON
PITOTLEFT RIGHT
ALTSTATIC
WARNHORN
SILENCE
HDLLT
TEST
NORM
MAN
OFF
AUTO
MANCOOL
TESTP
T
ENVIRONMENTAL
MAN TEMPINCR
BLOWERSHI
BLEED AIR VALVESOPEN
LEFTINST & ENVIR OFF AUTO
CABIN TEMP
AUTO TEMP
HOURS 1/10
0 0 0 0 7 89 9 9 9 8 9
FLIGHT
4 53 6
VACUUMINCHES OF MERCURY
35K 15K
10PSI
0 20
PNEUMATICPRESSURE
I I
I I I
I I I
I I I I I I I I I I I I I
COPILOTAIR
I
IPULLON
CABINAIR
I
IPULLDECR
OFF
ENVIR
OFF
RIGHT
OVERSPEEDWARNING
TEST
STALLWARNING
TEST
ENG FIRE TESTEXT
TEST AOFF
LEFT RIGHTTEST B
LOOPOFF
AMPDETECT
CABIN TEMP
40 80
0 120°F
OXYGENPRESSURE
0
5001000
1500
2000PSIG
OXYGENPRESSURE
0
5001000
1500
2000PSIG
VENT AIR - PULL ON
3 N 33
L GEN L GEN
CTRBUS
VOLT SELECT
BATT
TPLBUS
EXTPWR
LHINV
RHINV
PROP AMPS
2030
10
40
0
L
2030
10
40
0
R
FREQ
390 400 410
PUSHFOR VOLTS
100110 120
130AC VOLTS
420380
20VOLT
BATT
AMP
30
DC
10
60+
0
-60
20 40 60 80
0 100DC % LOAD
20 40 60 80
0 100DC % LOAD
INSTRUMENT
EMERGENCYLIGHTS
OFF
PILOTFLIGHTLIGHTS
BRT OFF
I N C R
ENGINEINSTRUMENT
LIGHTSBRT OFF
I N C R
AVIONICSPANELLIGHTS
BRT OFF
I N C R
OVERHEADFLOODLIGHTS
BRT OFF
I N C R
INSTRUMENTINDIRECT
LIGHTSBRT OFF
I N C R
EDGELIGHTPANELLIGHTS
BRT OFF
I N C R
OVERHEADSIDEPANELSUBPANEL
&CONSOLE INDLIGHTS
BRT OFF
I N C R
PILOTFLIGHTLIGHTS
BRT OFF
I N C R
PARK SLOW
FAST
WINDSHIELD WIPEROFF
DO NOT OPERATEON DRY GLASS
COPILOTMIC
OXYGENMASK
NORMAL
PILOTMICOXYGEN
MASK
NORMAL
MASTERPANELLIGHTS
ON
OFF
THIS AIRPLANE MUYST BE OPRATED AS A COMMUTER CATEFORY AIRPLANE IN COMPLIANCEWITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS MARKINGS ANDMANUALS. NO ACROBATIC MANEUVERS INCLUDING SPINS ARE APPROVED.THIS AIRPLANE APPROVED FOR VFR, IFR, DAY & NIGHT OPERATIONS & IN ICING CONDITIONS
STALL WARNING IS INOPERATIVE WHEN MASTER SWITCH IS OFF.STANDBY COMPAS IS ERRATIC WHEN WINDSHIELD ANTI-ICE ORSOME COMBINATION OF EXTERIOR LIGHTS ARE ON. SEE AFM.
CAUTION
OPERATING LIMITATIONS
GEAR EXTENSION
GEAR RETRACT
GEAR EXTENDED
180
180
180
17 DEG FLAPS
35 DEG FLAPS
MANEUVERING
188
154
178
MAXIMUM SPEEDS - KIAS
CABINFULL
READING FULL
PARTIAL
CABIN LIGHTSANTI COLLISION
BEACON STROBETAIL
FLOODLANDING TAXI
LEFT RIGHT
ICE NAV RECOGEXTERIOR LIGHTS
POS 0 30 60 90 120 150 180 210 240 270 3
00 3
30 3
60
STEER 0 29 59 90 121 151 182 211 242 2
71 300
329
359
COMPASS CORRECTIONCALIBRATE WITH
ENGINE ON
WARNINGS
WEATHER
LIGHTS
ENVIRONMENTAL
FLIGHT
ELEC
ENGINES AVIONICSLEFT
CONTROL
LEFT PRESSTEMP
AVIONICSSTEREOCABINCKPT
LEFT-WSHLD
POWERWARN LEFTSTALL
WARN
WINGNAVAVIONICSINSTR
IGNITERPOWER
OILTEMP
OILPRESS
FUELFLOW
LEFTLEFTLEFTFIRELEFT
ANN
BLEEDAIR
WARN
LANDINGGEAR
ANN
EADI
BRIEFER
BLEEDAIR
CONTROL
MASTER
CONTROL
RIGHT
RIGHT RIGHTRIGHTRIGHTRIGHTINDIND RIGHT
SURF
DEICE
WSHLD
WIPER
INDIRECT ICE
7½ 5 5 5 5 7½
7½ 5 5 5 5 7½
5 5 5 5
5 55 7½
55 7½
5 57½
7½
2 5
½
5
55
510
AURAL
WARN
5
TORQUEMETER
LEFT
RIGHT
7½
7½
FIREDET
STARTCONTROL
RIGHT
AUTO
FEATHER
5
PROP
SYNC
5
ROTATE
ANTICOLLISION
LIGHTS
STROBE
10
5
NO.1
INVPWRSEL
NO.2
5
5
FURNBUS
CONT
7½
POWER
½
AUTO-PROP-MAN
DEICE
5
DEICE
5
FLAP
IND &CONTROL
5
COPLT
ENCDALTM
1
ELEV
TRIM
5
PLT
ENCDALTM
1
OVRSPD
SENSOR
5
BAT
STBY HRZN
15 2
AUX IND
VOICERCDR
PLTNAVCOMMAVIONICS
SPKRNO.1
7½ 2 225
TPL FEED NO.1
COPLT
SPKR
2
NAVCOMMAVIONICSCOMPASS
L GEN NO.2NO.2
3 7½ 23
NO.1
FLTGPS
PHONE
5 2
PLTALTMRADIOAVIONICSCOMPASS
R GEN AIRDATA
ALTM
25 2 53
NO.2
PA &COPLT
PHONE
5 2
AVIONICS
R GEN
3
DSP-PRCSR
7½
7½
EHSI
5
5
DSP
1
1
RMI
NO.1
2
2
DME
NO.2
2
2
ADF
NO.2
2
5
XPNDR
NO.2
3
3
NO.2 NO.1NO.1 NO.1
RMI DMEADF XPNDR
PLT
COPLT
FD
2
RUDDER
5
FD
2
SERVO
5
NO.1 BOOSTNO.2
RADAR
5
FLT DATA
2
RADAR
1
ATT
1
RCDR NO.1
ATT
1
NO.2
HF
5
TAWS
5
TCAS
5
PWR
NAV
1
FLT DATA
2
RMI
1
RMI
1
RCDR NO.1
NAV
1
NO.2
FLTPRFL
55
EFISAUX
15
ADVST BAT
HF
5
REC NO.1 NO.2
BAT
BAT
L GEN
R GEN
BAT
BAT
L GEN
R GEN
115 VAC
28 VAC
EADI/EHSIDIM
ELAPSEDTIME
GSPTTG
ET
NAV DATA TIMERSET
S/S
CRSSEL
MAPARC
HSIARC
MAP
DHSET
TST
WX
PREACT
XFR
COURSE
EFIS
COMPAREPRESS TO
RESET
DRIVEXFR
ALTALERT
VG FASTERECT
NAV APPR B/CHDG
VS IASALT
CollinsTRIM HDG ARM CLM
DIS ARM
TEST
KNOTS40
60
80
100
120
140160180
200
220
240
260280
300
EFIS POWER PUSH / SWPILOT COPLT
EADI EHSI
EFIS TEST
PLT
COPLT
DSPL PRCSR
ON
OFF
ON
OFF
ON
OFF
ON
OFF
PILOT COPLT
WARNINGDEPRESSURIZE CABIN
BEFORE LANDING
CABINPRESSURE
DUMP
TEST
PARKINGBRAKE
RATEINC
78 6
24 2022 18
CA
BIN
ALT-FT
CABIN
X1000
CONTROLLER
ACF
T
05
10
13
141516
17
18
PROP
RPM X 100
19
200
5
10
13
141516
17
18
PROP
RPM X 100
19
20
4TURBINE
% RPM
20
4060
80
100
110 086.0
4TURBINE
% RPM
20
4060
80
100
110 086.0
0
23
5
4
6
7 8
1
PPH X 100
FUELFLOW
0
23
5
4
6
7 8
1
PPH X 100
FUELFLOW
OIL
PSIC
50
100
200
150
0200
60
20
100
140 OIL
PSIC
50
100
200
150
0200
60
20
100
140
50 05
10
15
2025
30
35
40
45 TORQUE
FT LB X100
50 05
10
15
2025
30
35
40
45 TORQUE
FT LB X100
ITT
°C X 100
6
2
4
5
8
9
7
START 12
ITT
°C X 100
6
2
4
5
8
9
7
START 12
FLAPS
35°DOWN
0°
17°
2CABIN CLIMBTHDS FT PER MIN
4
6
421
1
.5
.5
0
CABINALT
2
34
0
530
35
25
20 10
15
1
5
6
PSI
KNOTS40
60
80
100
120
140160180
200
220
240
260280
300
UP 0°
17°
35°
FLAP
DOWN
AFT
3
0TAXI
FUEL CUTOFF
REVERSEONLY WITHENGINESRUNNING
REVERSE
GNDFINE
GNDCOMM
PWR
HOTINTPH
ANNPUSH BRT
XPNDNORMAL
ENCDALTM 1 HI
LOOVERRIDEALTM 2
AUDIOSPKR
OFF OFF
OFF
VOICE
BOTH
RANGE
HORN
SILENCE
ON
TEST
COMM-1
COMM-2
PA
COMM NAV MKR BCN DME
1 2 1 2 1 2 1 2 ADF
PILOT RADIO OFF
VOLUME
DME1 MKR BKN 1 & 2STBY HORIZ PWR
2
PUSHON / OFF
PA VOLUME
COMM-1
COMM-2
PA
COMM NAV MKR BCN DME
1 2 1 2 1 2 1 2 ADF
COPILOT RADIO OFF
VOICE
BOTH
RANGE
AVIONICS BYBeechcraft
AUXARM
AUX TEST
AUXON
OFF
AP / L
AP / R COPLT COPLT
NORM NORM
OFFALL ON NO. 1
ALL ON NO. 2NORMHDG
PLTCMPST
DSPPLT
DR XFRPLT
CO PLTCMPST
ALL ON NO. 1
ALL ON NO. 2
NORMATT
ADCTEST
ONSBYOFF
402015
105
3
ABOVENORMBELOW
PUSH FOR FLPUSH TO TST
FAILTCAS BENDIX/KING
TST FL
RUDDERBOOST
ELEVTRIM
OFFYAWCONTROL
TEST
OFF
EFIS
DRIVEXFR
COMPARE
PRESS TORESET
FLTRCDROFF
Raytheon 1900D Airliner
OXYGENOUTLET PRESSURE
PSIG
2030 40 50
60
70CABIN ALTITUDE
NAV APPR B/CHDG
VS IASALT
CollinsTRIM HDG ARM DIS ARM
TEST
OFF
RUD BOOSTYAW DAMP
LEFT
RIGHTCOPLT COPLT
NORM NORMOFF
ALL ON NO. 1
ALL ON NO. 2NORMHDG
PLTCMPST
DSPPLT
DR XFRPLT
CO PLTCMPST
ALL ON NO. 1
ALL ON NO. 2
NORMATT
RUDDERBOOST
YAWCONTROL
TEST
OFF
ELEVTRIM
OFF
YAWDAMP
PUSHON / OFF
YDENG
----------------- -----------------
F1
F2a
F2b
F3F4 This is the panel that willbe seen after all folding