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