King Air B200EFIS-85
COMPASS CORRECTION
210209
9089
STEERFO
R0359
3028
6059 RADIO ON
150151
120120
180179
CALIBRATE WITH 240
238
330
329
270
269
300
299
OPERATION LIMITATIONS :THE MARKING AND PLACARDS INSTALLED IN THIS AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE INTHE COMMUTER CATEGORY. OTHER OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THE AIRPLANE IN THIS CATEGORY ARE CONTAINED IN THE AIRPLANE FLIGHT MANUAL. NO ACROBATIC MANEUVERS INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR DAY & NIGHT OPERATION AND IN ICING CONDITIONS.
OFF
LIGHTSON
PANELMASTER
STALL WARNING IS INOPERATIVE WHEN MASTER SWITCH IS OFF. STANDBY COMPASS IS ERRATIC WHEN WINDSHIELD ANTI-ICE AND/OR AIR
CONDITIONER AND/OR HIGH VENT BLOWER AND/OR LANDING LIGHTS ARE ON.
OFF
GYROINSTR
COPILOTPILOTFLIGHTINSTROFF
ENGINEINSTROFF
DO NOT OPERATEON DRY GLASS
WINDSHIELD WIPER
PARKOFF
SLOW
FAST
FLOOD
PILOTOVHD
OFF
& SUBPANELOVHD PEDAVIONICS
OFFPANEL
OFF
SIDEPANEL
OFF
INSTR
OFFINDIRECT
WARNING
FLIGHTCOPILOT
OFFINSTR
MAX MANEUVERING 181 KNOTS
181 KNOTS163 KNOTS
200 KNOTS167 KNOTS
181 KNOTSMAX GEAR RETRACT
MAX FULL ON FLAPMAX APPROACH FLAPMAX GEAR EXTENDED
MAX GEAR EXTENSION
AIRSPEEDS (IAS)
3 N 33
BRTBRTBRTBRTBRTBRT
BRTBRT
BRT
PUSHFOR VOLTS
40 60
DC VOLTS0
020
100
80
10 20100
% LOAD
PUSHFOR VOLTS
40 60
DC VOLTS0
020
100
80
10 20100
% LOAD
PUSHFOR VOLTS
400410
AC VOLTS100
380390
130
420
110
120% FREQ
0
BATT AMPS 6060
R0
King Air B200EFIS-85
2
XFR
MEMMEM
1
2
MEM
XFR
MEM
TCA
MEM
XFR
MEM
XFR
MEM
XFR
MEMMEM
TO TEST
P
RESS
STARTER ONLYPARKING BRAKE
ENGINE STARTIGNITION AND
LEFT RIGHTON
OFF
AVIONICS
TESTOFF
ON
ACTUATORS
ENGINE ANTI-ICE
GOV
AUTOFEATHER
OFF
ARM
OFF
ON
OFF
ONGENRESET
LEFT
LEFT
PROP TEST PULLON
RIGHT
RIGHT
PILOTAIR
IGNITIONENG AUTO
ARM
MAIN
LEFT
WSHLD ANTI-ICE
PILOT
BRAKEDEICE
CYCLESINGLE
ONPULL
AIRDEFROST
HI
OFFLEFT
COPILOT
MANUAL
WARNSTALL
LEFT
RIGHT
PITOT
RELAY
RIGHT
GEARLANDING
OFF
PROP
LIGHTS
ICE PROTECTION
LANDING TAXI
RIGHT
ONORMAL AUTO
NAVICE RECOG
FUEL VENTMANUAL
RELTEST
SENSORHYD FLUID
TEST
OFF
LDG GEAR CONTROL
LOCKDOWN
UP
HD LT
DN
LIGHTSSTROBE
GEARDOWN
BEACON
FLOODTAIL
OFF
OFF
OFF
STANDBY
FF
2
NOSE
L R
OFF
CABIN/COCKPITAIR
PULL
OFF OFF
BLOWERON
AFT
HEATELEC
ENVIROMENTALVENT
BLOWER
AUTO
HIGH
BLEED AIR VALVES
PNEU & ENVIR OFF
RIGHTLEFTOPEN
ENVIROFF
DECRFSB
MANUALTEMP
INCR
LO
COOLMAN
CABIN TEMP MODE
CABIN TEMP
MANHEATINCR AUTO
OFF
ONPULL
COPILOTAIR
CABIN AIR
0 10080
° F50
9340
FLIGHT1/10HOURS 2000
SUPPLY PRESSURE
1500
0OXYGEN
1000500
0 20PRESSUREPNUEMATIC
10PSI
INCHES OF MERCURY
GYROSUCTION
643 5
L BL AIRFAIL
R BL AIRFAIL
140
-200
100
20
60
°C
0
200OIL
150
100
50
PSI
SYNCON
OFF
PROP
0
5
ALT
1000 FT
6
7 100 FT 32992
IN
4
HG
09
87
2
1
37
TEST
BARO
92 9.5
2
08 09
0
001
7 2
3
2X1 00 FT
RAD ALT10
TEST
2015
5 4
DH
1
.5
.5
M
0VERT SPEED
x1000 FPM
1 24
R
6
1 2
4
DH
TRANSPONDER
NAV 1
COMM 1
ADF
NAV 2
COMM 2
OFF
V
ONOFF
SQ COM
ACTTEST
STO
Collins
ALTON
OFFSTBY
Collins
PRE
ATC
TESTTEST
IDENT
HLD
V
ONOFF
Collins
ACT
NAV
TESTTEST
STO
TONEANT
OFF
ADF
Collins
ADF
ACT
ADF
TESTTEST
STO
HLD
VOFF
ON
Collins
Collins
ACT
NAV
TESTTEST
STO
SQOFF
VOFF
ON
ACT
COM
TEST
STO
Collins
1
x1000 FPM
VERT SPEED
1
M
.5
0
.5
2 R
4
6
2
4
ONERECT
VG FAST
RCL SKP CLR
PGE
EMG
TFC
RDRNAV
RMT
DATA
PWR INT
Collins
ID
PWR
WPT1 2 3
SEL
NM HLD KT MIN
CH
NO SMOKE& FSB
OFF
BRIGHT
MASTER POWER
140
-200
100
20
60
°C
0
200OIL
150
100
50
PSI
ITT
AFX
°C x 100
9
8
7 564
2
START
12
USE NO OIL
GYROSLAVING
0
SLEW MODE
DG
D C
L R
1812
27
33
DF
A
30
NAVNAV
2421
3
0
6 9
16
DF
A
COLLINS
ID
PWR
WPT1 2 3
SEL
NM HLD KT MIN
CH
GYROSLAVING
0
SLEW MODE
DG
D C
L R
1812
27
33
DF
A
30
NAVNAV
2421
3
0
6 9
16
DF
A
AIR SPEED
KNOTS
200180 160
220
240
260
280
300
80
140
100
120
6040
MASTERWARNING
MASTERCAUTION
TO RESET
EXTINGUISHERPUSH
DISCHARGED
EXTINGUISHERPUSH
DISCHARGED
HORNWARN
SILENCE
ITT
AFX
°C x 100
9
8
7 564
2
START
12
AUX
INTEGGPSDRIVE
MFD
FANFAIL
MPU EFD
FANFAIL
DPUAUX
DRIVEPUSH TORESET
COMPARE
GPSINTEG
USTB GCS TRU 1
100
50WX+TA-2.5
RDR G+2 030
33
BRG
H
O
ADF 1
24
21
30W
CID18.4HDIST MSG LIN
S15
12
CRS090
6E
MAG1
N 3
TGT 040
10
10
DH 2000
AP/LYD
ALTSGS
VS 550 HDG LOC1
- - -
20
20
Collins
Collins
VOR1
VOR2
2
AUDIOSPKR
AUDIOSPKR
INTPHSENS
INTPHSENS
SIDE-TONE
SIDE-TONE
OFF OFFOFF
DME
ENCDALTM
1
RANGE RANGE
VOICE VOICEAUDIOEMER
NORM
PAGINGBOTH
BOTH
INTPH
PUSHON/OFF
BRT
LO
HI
ANNPUSH
1 & 2MKR BCN
HOTINTPH
VOLVOL
VOL VOL
VOL
DIM
PWRCOMMGND
3,ALTITUDE SET
PUSH TO
CANCEL
00PUSH
0100
ALTALERT 0
1COMM
PILOT AUDIO OFF
MKR BCNNAV2 1 2 1 22 1
DMEADF
DME
COPILOT AUDIO OFF
2COMM1 1
MKR BCN2
NAV1 2 1 ADF2
COMM 2COMM 1 CABIN
VOL
COMM 1COMM 2
CABIN
VOL21
AUDIOCOMM
OFF
AUDIOCOMM
OFF
CMPST MFD NORMALDRIVE
NORMALHDG
AIR SPEED
KNOTS
200180 160
220
240
260
280
300
80
140
100
120
6040
F A S T
E R E C T
EFIS
L ENG FIRE
L FUEL PRESS
DOOR UNLOCKED
INVERTER ALT WARN
NNN33
30W
24
21 S15
12E
6
3
GS
HDGNAV
10 10
FFO
202010 10
PRESS
TO RESET
PRESS
MASTERWARNING
MASTERCAUTION
TO RESET
PRESS
TO RESET
PRESS
3FUEL FLOW
PPH X 100
6
45
2
0
1
3FUEL FLOW
PPH X 100
6
45
2
0
1
90
RPM0
100
10
8050
70
203040
60
PERCENT
90
RPM0
100
10
8050
70
203040
60
PERCENT
TCA
TCA
TCA
TCA
TCA
P/OVRDTERRINOPTERR
-PRESS-OVRDFLAPGPWS
TERR
-PRESS- CANCLDG/S
GPWSINOP
G/SP/CANCEL
GPWSP/TESTGPWS
OFF
OFF
FURNON
COFFEE
OFF
CABIN
STALLWARNTEST
INCR CKTDECR CAB
DET
L
R300PROP AMPS
OXYGENMASK
MICNORMAL
OXYGENMASK
MICNORMAL
NO 2
INVERTERNO 1
MASTER SWITCH
DOWN - OFF
GEN - UP TO RESET
BATT GEN 1 GEN 2
OFF
OFF
FTLB x 100
10141618
2220
12
024
68
2426
TORQUE
FTLB x 100
10141618
2220
12
024
68
2426
TORQUE
RPM x 100
PROP
10
0
1514161718
1920 13
5
2122
23
RPM x 100
PROP
10
0
1514161718
1920 13
5
2122
23
EFISAUX POWER
ON HORN
TEST SILENCE
R ENG FIRE
R FUEL PRESS
R0
King Air B200EFIS-85
MAP
PAGE ADV
ATC IDENT
MAP
PAGE ADVATC IDENT
PASSENGERPULL ONSYSTEM READY OXYGEN MANUAL DROP OUT
TP
AILERON TAB
5
31
P
5
LEFT
REVERSECAUTION
RUNNING
ONLY WITH
DN
DNENGINES
R
U
M0
LIFTIDLE
GROUNDFINELIFT
I
GO AROUND
GEAR HORNSILENCE
T
APPROACH
3
5
310
5
1
RUDDER TRIM
3
LEFT
1
DOWN
5
RIGHT
CUT OFF
RIGHT
FRICTIONLOCK
REVERSE
FLAP
UP
LOCKFRICTION
FEATHERFUEL
IO
IDLELOW
N
O
HC5
UPWER
IP
T
DN
PINCR
HIGH IDLE
AND
P
OR
REVERSE
TAKE OFF LANDING
C
NDI
O
HIGHRPM
FLAP
TI
RM
NOSE UP
NOSE DN
HC
TI
P
12
8
4
16
20
18
22
14
24 2
10U S A
6
GI
HT
DIM
LBRT
TIR
M
ST-SP
ADV
MODERST
SET
QUARTZ CHRONOMETER
LC ETZU FT DC
NOSE UP
NOSE DN
HC
TIP
60
ANDFLAPSAPPROACH
80DOWN
UP20
TAKEOFF
N
PSI
PRESS
5
20
THDS FT PER MINCABIN CLIMB
.5
12
.5
21
35
4
6630
25
7
4I
LTCABA
401
23
10DIFF
4
15
000
TF
5
0
0
1
0
GO AROUND
I AN X
M
RATE
M
CABINALT
ALTCABIN
1000FT
0
-115
1413
12
1716
35
2321
19
1
11 10 9 8
76
54
32
30
25ACFT ALT1000 FT
WARNING BEFORE LANDINGDEPRESSURIZE CABIN
A B C D E F GH I J K L M NO P Q R S T UV W X Y Z
1 2 33 4 56 7 8
PWRDIM
NEXT
PREV
TUNE
FUEL
DATA
MSG
PERF
BACK
MENU
LIST
VNAV
FPL
DTO
NAV
0 ±ENTER
UNIVERSAL
NORMAL
FPL MENU 1/2
CLEARANCE
PPOS TO WPT
DEPART
DELETE FPL
STORE FPL
XFILL FPL
RAIM PRED
ARRIVE
RETURN
ELEVTRIM
CABINPRESSDUMP
TEST
RUDDERBOOST
OFF
PRESS HEADSET
COCKPIT VOICE RECORDER
TEST ERASE
UNIVERSAL
Collins
TEST
TCASSTBY
OFF
AUTO ONLYTA
1/2Ø
ENGYAWENG
L
AP
R
DISYAW APDIS TAP A R E
DN
UP
SR
1/2Ø
TRIMTRIMSR Collins
HDG
DTANAV
CTLCRS CER
HSUP
TI
D
CRS
CRS
Collins
HDGU
YS
P
N C
SH
ET
CRS XFR
Collins
BRG
DH SET
DIM
ARCHSI MAP
TSTRA
RDR ACTCRS
SEL/RNG
PRECRS
ALT SELALT VS IAS DSC
TRIMYAW
ARM
NAV
ALT SELARM
HDG
HDGALT
TRIMDIS
NAV
APPR
GSDR
VSAPPR
ARM1/2Ø
B/C CLIMB
CLMGA
B/CIAS DSC
TEST
SR APAP DIS
Collins
5
FIREWALLVALVE
10
STANDYBYPUMP
5 5
QTYIND
5
PRESSWARN
5
CROSSFEED
5
PRESSWARN
5
QTYIND
5
AUXTRANS
FER
AUXTRANS
FER
10
STANDYBYPUMP
5
FIREWALLVALVE
OPEN
CLOSED
FIREWALLSHUT OFF
VALVE
FUEL SYSTEM
OPEN
CLOSED
FIREWALLSHUT OFF
VALVE
5
LEFT RIGHT
ENGINE INSTRUMENTSLEFT
5 55555
5 5 55555
RIGHT
ITT TORQUE PROPTACH
TURBINETACH
FUELFLOW
OILPRESS
OILTEMP
50 25 555
BUSFEEDERS
BUSFEEDERS
PROPDEICE
5020
50 25 555 5020
MOTORPROPDEICE
CONTROL PROP
IGNITORPOWER
STARTCONTROL
NO 4 RIGHT RIGHT RIGHT
LEFTNO 3
NO 4
NO 3
CONTROL
LEFT LEFT
GOV
FLAP
TCS TCS
STANDBY PUMPON
OFF
AUX TRANSFEROVERRIDE
AUTO
AUX TRANSFEROVERRIDE
AUTO
AUXILIARY
CROSSFEEDFLOW
ENGINE ENGINE
SEE MANUAL FORFUEL CAPACITY
LEFT RIGHT
0
2
4
68 10 12
14FUEL
20
1816
QTY
STANDBY PUMPON
OFF
TRANSFER
0
2
4
68 10 12
14FUEL
20
1816
PRESS
TO
T E S T
DIM
TRANSFER
PRESS
TO
T E S T
DIM
FUEL QUANTITYMAIN
OFF
LBS X 100QTY
LBS X 100
OXYGEN
CONTROL
PRESS
CONTROL
LEFT
BLEEDAIR
CONTROL
ALT
ALERT
PILOT
TURN &SLIP
PILOT
ALTMAIR DATA
COPLT
PITCH
TRIM
OUTSIDE
AIRTEMP
NO. 1
INVCONTROL
LEFT
GENCONTROL
NO. 1 RMI
NO. 2
DME
READINGAVIONICS
& ENG
INSTR
OVHD &
CONSOLE
NO SMK& FSB
CABIN RIGHT IND IND RIGHT
WSHLD
WIPER
AVIONICS
NO. 2
COMM
NO. 2
NAV
NO. 2
XPNDR
NO.2
AVIONICS
ANN
COPLT FLT
INSTR
INSTR
INDIRECT
PLT FLT
SIDE PNL
STALL
WARN
LEFT
BLEEDAIR
WARN
WARN
LANDINGGEAR
POWER
ANN
LEFT
FUELVENT
SURF
DE-ICE
AVIONICS
NO. 1
COMM
NO. 1
NAV
NO. 1
XPNDR
AUDIO
AUTO
FEATHER RIGHT RIGHT RIGHT RIGHT RIGHT RIGHT RIGHT
AVIONICS
WARN
PILOT
AUDIO
CABIN
AUDIO
PROP
SYNC
LEFT FIRE
DET
LEFT
ICEVANE
CONTROL
LEFT
FUELCONTROL
HEAT
LEFT
OILTEMP
LEFT
OILPRESS
LEFT
TORQUEMETER
LEFT
FUELFLOW
AVIONICS
MASTER
TEMP
CONTROL RIGHT COPLT
ENCD ALTM
RUDDER
BOOST NO .2 RIGHT NO. 2
RMI
NO. 1
DME
NO. 1
COMPASS
NO. 2
MASTER
POWER
CIGAR
LIGHTER
RADAR ADF RADIO
ALTM
FLIGHT
ENGINES AVIONICS
ELECTRICAL
WEATHERWARNINGSLIGHTS
ENVIRONMENTAL
FURNISHING
BUSFEEDERS
PILOTS STATICAIR SOURCE
NORMAL ALTERNATE
SEE FLIGHT MANUAL PERFORM- ANCE SECTION FOR
INSTR CAL ERROR
5
CHIPDET
5 5 5 71/2 5
5 5 5 571/2
5 52
5 52
5
71/21530 2
COPILOT
AUDIO
30 71/2 2 2
71/22230
2 103
5
HDG
PRCSR
5
3 2
AP
SERVO
FCS
POWER
EHSI
2
COMPASS
NO. 1
2 2
71/2 2 3
5 5 571/2
5 5 5 5
5 55
5 5
5 5 5 13
53 1
5 50 5010
50 505 10
10 5
5 5 71/25
5 55
5 5
5 10
L DC GEN
L ENG ICEFAIL
L ENGANTI-ICE
L IGNITION ON
L BL AIR OFF
BATTERY CHG
LDG/TAXI LIGHT
RVS NOT READY
DUCT OVERTEMP
EXT PWR
AIR COND N1 LOW
PASS OXY ON
FUEL CROSSFEED
R DC GEN
R IGNITION ON
OFF OFF
ADCTEST
EFISTEST
EFIS POWER
DSPI PRCSR MULTI FCTNPRCSR
O2 ARM MAN OVRD
HYD FLUIDLOW
R CHIPDETECT
L CHIPDETECT
R ENG ICEFAIL
R ENGANTI-ICE
R BL AIR OFF
R0