Pilot Training Manual
King Air 350i
COCKPIT FLOWS
C
ockpit flows are designed as a structured pattern or memory aid to quickly facilitate a specific sequence of
events. The following flows work specifically for FlyRight’s simulator and are offered only as a guideline.
While a flow may mirror a specific checklist it is not intended to be used as a substitute. Always back up each flow
with the appropriate manufacturer’s FAA approved checklist.
For Training Purposes Only
Revision: Original - July 10, 2013
18-23
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
COCKPIT PREFLIGHT
For Training Purposes Only
Revision: Original - July 10, 2013
18-24
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
COCKPIT PREFLIGHT
1.Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
2.Right Side Panel
Circuit Breaker Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN
Pilot Static air source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL
3.Copilot’s Left Subpanel
Bleed Air Vavles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENVIR OFF
Cabin Temp Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Cabin Blower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Cockpit Blower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
4.Reversionary Panel
Ground Comm . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
DG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
Remote Tune . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
Emerg Freq . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OUT
Tune Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
ADC Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
Pilot Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY
DG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
5.Pilot’s Right Subpanel
Landing Gear Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Landing Gear Relay Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN
Light Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Nav Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Ice Protection Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
6.Pilot’s Left Subpanel
Engine Anti-Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & MAIN
Avionics Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
External Power Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Bat Bus . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
7.Left Side Panel
Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN
8.Fuel Panel
Aux Transfer Override Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Standby Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Cross Feed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9.Overhead Panel
Interior Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Voltmeter Bus Select Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Bat 23 volts min, all other positions 0
For Training Purposes Only
Revision: Original - July 10, 2013
18-25
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE ENGINE STARTING
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
PILOT
INSTR
PNL
OFF
BRT
OFF
OVHD PED
& SUBPANEL
OFF
PILOT
DISPLAYS
BRT
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
2
+
40
60-
10
VOLTMETER
BUS SELECT
GR EXTENSION
184
GR RETRACT
166
GR EXTENDED
184
APPROACH FLAP
202
FULL DN FLAP
158
MANEUVERING
184
359
30
POS 0 29
STEER 0
0
2 270
27 300
1 3 330 3
60
00 3
29
OFF
3 N 33
9
60 9
59
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
4
0 120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
1/2 BANK
ALT
PUS
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
H
AVIONICS
MASTER
POWER
AUTOFEATHER
ARM
PILOT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
STARTER ONLY
MANUAL
TEST
OFF
PROP
MANUAL
PILOT
DISPLAY
STBY
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
RIGHT
RELAY
BEACON
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
GEAR
DOWN
BLOWER
STROBE
L
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
NOSE
HD LT
TEST
L DC GEN
L CHIP DETECT
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
7
HYD FLUID
SENSOR
TEST
UP
20
FLAPS
.5
TAKEOFF
AND
APPROACH
+
1 5K
ON
NORM
.5
1
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
4
6
BLOWER
AUTO
0
TEMP
INCR CMS
CABIN
35
K
3 4
5
6
8
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
OFF
0
ENVIR
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
TR
IM
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
INCR
EXT
LEFT
9
T
R
I
M
5
LIFT
15
SE
DN
NO
C
O
N
D
I
T
I
O
N
9
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
10
4
HIGH
RPM
IDLE
2000
RIGHT
2
3
5
20
9
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
I I I I I II
I
I I 10
0
INCHES OF MERCURY
5
PSI
7
30
4
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
2
INCR
COCKPIT
TAIL DEICE
CABIN CLIMB
1
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
2
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
0
60
80
DOWN
SE
AHRS
MFD SLEW
1
PFD
2
UP
DN
FUEL VENT
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
PARKING BRAKE
+
LDG GEAR CONTROL
OFF
ICE PROTECTION
AUTO
INPH
NORM
I I I I
II
MAIN
OPEN
RIGHT
OFF
ON
OFF
RECOG
AUTO
6
TEST
IGNITION AND
ENGINE START
LEFT
OFF
6
TEST
RIGHT
WSHLD ANTI-ICE
NORMAL
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
NORM
OFF
R GEN
BUS SENSE
RESET
LEFT
NAV
AUDIO
ALTN
OFF
L GEN
ON
OFF
OFF
ICE
OFF
BAT
ESIS
ON
TAXI
LIGHTS
1
EMER
OFF
DOWN-OFF
LANDING
LIGHTS
MASTER SWITCH
ATC
1
SLEW
NORM
RIGHT
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
IDENT
MKR
Collins
ON
OFF
LEFT
BAT BUS
BRT
DIM
DIM
DG
FREE
ARM
ENG
AUTO
IGN
OFF
OFF-RESET
VOICE
RANGE
PUS
AUTO
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
CH
CPL
PUSH
N
AP
H
SY
MA
YD
ALT
H
T
APPR
HDG
H
S/
UP
MASTER
CAUTION
DISCHARGED
PRESS TO RESET
HDG
PUS
EC
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
T
SPEED
IA
D
STEEP
APPR
ACTIVE
TES
L
VNAV
NAV
C
CRS1
FLC
DOWN
H
T
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
PRESS
T
VS
PUS
G/S
INHIB
ACTIVE
3
O
4
FD
IR
Collins
XMIT
PA
1
-------------
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
T
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
OFF
OFF
AUX TRANSFER
OVERRIDE
6
8
4
2
AUTO
5
12
MAIN TANK
ONLY
QTY
0
14
LBS X 100
OFF
6
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
LBS X 100
MAIN
LEFT
9
3
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
PILOT PFD
5
5
& DCP
RTU
ENG FIRE EXT
5
ENTRY
CROSS
FEED
5
10
EDCI
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
DBU
CDU2
RIGHT
QTY
IND
5
3
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BUS
DISP
5
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
5
5
PILOT
AUDIO
5
1
3
7½
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
RIGHT
FAN
AUDIO
CONT
AUDIO
LEFT
PROP
GOV
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
5
10
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
5
CONSOLE
INSTR
IND
CONTROL
GEN
INSTR
CABIN
AVIONICS
LEFT
7½
7½
5
5
7½
5
5
RESET
INDIRECT
LIGHTS
ANN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
DIFF
CABIN
ALT
RIGHT
NOSE
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
PILOT WSHLD
ANTI ICE
PROP
R GEN
WSHLD
HF
5
10
DEICE
CONTROL
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
5
1
PNL
COOLING
DC
ADC1
3
5
HIGH
CIGAR
TAWS
25
L GEN
LEFT
5
FURNISHING
5
SEC
AVIONICS
BUS
½
R GEN
RIGHT
HIGH
DC
FUEL
VENT
TCAS
2
SEC
POWER
1
5
COM3
½
SYNC
MN ENG
ANTI
ICE
CMU
CONTROL
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
5
AVIONICS
RIGHT
BUS
TIE
POWER
STAT
7½
AURAL
5
2
DATA
5
MASTER
CABIN
VOICE
WARN
SEC
ESC
1
WARN
COM1
NO SMK
DCU2
MENU
ADV
3
RCDR
CCP
5
7½
MENU
TEL
RTER
FSU
5
FIRE
DETR
RIGHT
2
ESIS
BAT
AVIONICS
TEL
XVCR
LEFT
5
OIL
PRESS
PLT FLT
LEFT
SEC
RELAY
5
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
LEFT
5
TORQUE
METER
5
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
LEFT
5
IGNITOR
POWER
FLAP
ELECTRICAL
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
7½
START
CONT
RIGHT
FLIGHT
SERVO
PILOT
FUEL SYSTEM
LIGHTS
CDU1
AUX
FUEL
XFER
LEFT
5
STALL
20
AUXILIARY
FIRE
WALL
VALVE
AUTO
FEATHER
FLAP
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
FGC1
AUTO
LEFT
ENGINE
WARN
LANDING
GEAR
10
2
FUEL QUANTITY
TEST
AUX TRANSFER
OVERRIDE
8
4
5
5
STANDBY PUMP
ON
1 0 1
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
STBY ENG
ANTI ICE
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
9
CABIN
PRESS
DUMP
9
TEST
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
ERASE
HEADSET
RUDDER
BOOST
9
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-26
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE ENGINE STARTING
1.Pilot’s Left Subpanel
Battery Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2.Overhead Panel
Panel Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Fasten Seat Belt Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3.Glareshield
Annunciator Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST, All lights test except Fire Warning
4.Firewall Valves
Firewall Fuel Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
Standby Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Firewall Fuel Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
Standby Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
5.Fuel Panel
Crossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK OPERATION
Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Fuel Quantity Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
6.Pilot’s Left Subpanel
ESIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Bus Tie . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE (For Fire Warning and Overspeed test)
7.Pilot’s Right Subpanel
Landing Gear Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Hydraulic Fluid Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
8.Copilot’s Left Subpanel
Overspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Stall Warning/Landing Gear Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Cabin Alt Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Engine Fire System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
9.Center Pedestal
Power Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
Propeller Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM
Condition Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL CUTOFF
Oxygen Supply . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL ON
Oxygen System Preflight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
CVR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Rudder Boost Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Cabin Pressure Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
For Training Purposes Only
Revision: Original - July 10, 2013
18-27
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
ENGINE START
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
T
O
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
H
AVIONICS
MASTER
POWER
L GEN
R GEN
MAIN
AUTOFEATHER
ARM
RIGHT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
STARTER ONLY
MANUAL
TEST
PARKING BRAKE
OFF
RECOG
PILOT
DISPLAY
STBY
AUTO
PROP
MANUAL
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
UP
DN
FUEL VENT
RIGHT
BEACON
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
2
GEAR
DOWN
BLOWER
STROBE
L
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
NOSE
HD LT
TEST
L DC GEN
L CHIP DETECT
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
+
1 5K
ON
NORM
TEST
UP
20
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
TEMP
INCR CMS
CABIN
K
35
3 4
5
6
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
OFF
0
ENVIR
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
INCR
EXT
LEFT
TR
IM
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
I I I I I II
I
I I 10
0
INCHES OF MERCURY
5
PSI
7
30
5
2
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
0
60
80
DOWN
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
FLAPS
SE
AHRS
MFD SLEW
1
PFD
2
LDG GEAR CONTROL
OFF
ICE PROTECTION
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
OFF
OFF
ON
PILOT
OPEN
TEST
IGNITION AND
ENGINE START
LEFT
NAV
AUTO
TEST
OFF
NORM
OFF
RIGHT
WSHLD ANTI-ICE
NORMAL
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
LEFT
OFF
ICE
INPH
NORM
I I I I
II
BAT
ESIS
ON
OFF
TAXI
AUDIO
ALTN
OFF
EMER
OFF
ON
LANDING
LIGHTS
DOWN-OFF
+
NORM
RIGHT
LIGHTS
MASTER SWITCH
ATC
1
SLEW
-
ON
OFF
LEFT
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
IDENT
MKR
Collins
DG
FREE
ARM
ENG
AUTO
IGN
BAT BUS
BRT
DIM
DIM
OFF
1
OFF
OFF-RESET
VOICE
RANGE
PUS
AUTO
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
H
EC
YD
ALT
PUS
H
STEEP
APPR
ACTIVE
IA
D
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
APPR
HDG
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
7½
10
BUS
TIE
POWER
STAT
3
PROP
GOV
2
DATA
1
RIGHT
SEC
ESC
PILOT
AUDIO
5
5
DCU2
MENU
ADV
5
LEFT
7½
MENU
5
RIGHT
2
ESIS
BUS
5
RELAY
5
MASTER
CABIN
5
LEFT
SEC
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
CABIN
PRESS
DUMP
TEST
ERASE
HEADSET
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-28
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
ENGINE START
1.Pilot’s Left Subpanel
Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2.Pilot’s Right Subpanel
Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
For Training Purposes Only
Revision: Original - July 10, 2013
18-29
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAXI
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
3
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
4
T
O
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
TERR
INHIB
ACTIVE
2
Collins
RADIO CALL
N6410M
STEEP
APPR
ACTIVE
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RANGE
TILT
PUS
H
H
AUTO
AVIONICS
MASTER
POWER
L GEN
R GEN
1
MAIN
PILOT
OPEN
AUTOFEATHER
ARM
RIGHT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
STARTER ONLY
MANUAL
TEST
PARKING BRAKE
OFF
RECOG
PILOT
DISPLAY
STBY
AUTO
PROP
MANUAL
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
UP
DN
FUEL VENT
RIGHT
BEACON
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
GEAR
DOWN
BLOWER
STROBE
L
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
NOSE
HD LT
TEST
L DC GEN
L CHIP DETECT
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
+
1 5K
ON
NORM
TEST
UP
20
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
TEMP
INCR CMS
CABIN
K
35
3 4
6
5
6
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
OFF
0
ENVIR
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
INCR
EXT
LEFT
TR
IM
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
I I I I I II
I
I I 10
0
INCHES OF MERCURY
5
PSI
7
30
5
2
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
0
60
80
DOWN
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
FLAPS
SE
AHRS
MFD SLEW
1
PFD
2
LDG GEAR CONTROL
OFF
ICE PROTECTION
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
OFF
ON
OFF
NAV
AUTO
TEST
IGNITION AND
ENGINE START
LEFT
OFF
TEST
NORM
OFF
RIGHT
WSHLD ANTI-ICE
NORMAL
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
LEFT
OFF
ICE
INPH
NORM
I I I I
II
BAT
ESIS
ON
OFF
TAXI
AUDIO
ALTN
OFF
EMER
OFF
ON
LANDING
LIGHTS
DOWN-OFF
+
NORM
RIGHT
LIGHTS
MASTER SWITCH
ATC
1
SLEW
-
ON
OFF
LEFT
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
MKR
Collins
DG
FREE
ARM
ENG
AUTO
IGN
BAT BUS
IDENT
DIM
DIM
OFF
1
OFF
OFF-RESET
BRT
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
VOICE
RANGE
PUS
AUTO
T I LT
DIM
SPKR
BOTH
BOTH
TILT
BRT
IDENT
ADF
AUTO
COMM
RADAR
GCS
Collins
NORM
NAV / BRG
1/2
GCS
VOICE
NORM
2
2
LEC
DME-H
5
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
H
EC
YD
ALT
PUS
H
IA
D
FLAP
OVRD
ACTIVE
APPR
HDG
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
MEM 1
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
STAT
7½
10
BUS
TIE
POWER
DATA
3
PROP
GOV
2
ESC
1
RIGHT
SEC
MENU
ADV
PILOT
AUDIO
5
5
DCU2
MENU
5
LEFT
7½
ESIS
BUS
5
RELAY
5
RIGHT
2
SEC
5
MASTER
CABIN
5
LEFT
7
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
CABIN
PRESS
DUMP
TEST
ERASE
HEADSET
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-30
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAXI
1.Pilot’s Left Subpanel
Electrical System Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE (first flight)
Bus Sense . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Gen Ties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2.GPWS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
3.Overhead Panel
Interior master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
4.Glareshield
Annunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
5.TCAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
6.Copilot’s Left Subpanel
Environmental Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET AS REQUIRED
7.Center Pedestal
FMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Verify, Initialize, Flight Plan, Perf Init
For Training Purposes Only
Revision: Original - July 10, 2013
18-31
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAKEOFF/RUN-UP
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
T
O
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
H
AVIONICS
MASTER
POWER
R GEN
MAIN
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
STARTER ONLY
MANUAL
TEST
PARKING BRAKE
+
PILOT
DISPLAY
STBY
OFF
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
LDG GEAR CONTROL
OFF
ICE PROTECTION
AUTO
PROP
MANUAL
5
STALL
WARN
DOWN
LOCK
REL
LEFT
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
UP
DN
FUEL VENT
RIGHT
GEAR
DOWN
BLOWER
STROBE
NOSE
HD LT
TEST
L
L DC GEN
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L CHIP DETECT
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
+
1 5K
ON
NORM
TEST
UP
20
FLAPS
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
TEMP
INCR CMS
CABIN
K
35
3 4
5
6
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
OFF
0
6
ENVIR
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
INCR
EXT
LEFT
TR
IM
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
3
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
3
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
I I I I I II
I
I I 10
0
INCHES OF MERCURY
5
PSI
7
30
5
2
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
0
60
80
DOWN
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
1
SE
AHRS
MFD SLEW
1
PFD
2
BEACON
AUTO
AUTOFEATHER
ARM
RIGHT
OFF
OFF
ON
PILOT
OPEN
TEST
IGNITION AND
ENGINE START
LEFT
OFF
TEST
NORM
OFF
WSHLD ANTI-ICE
NORMAL
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
RIGHT
INPH
NORM
I I I I
II
4
L GEN
LEFT
RECOG
AUDIO
ALTN
OFF
BAT
ESIS
ON
OFF
OFF
NAV
OFF
EMER
OFF
ON
ICE
TAXI
LIGHTS
DOWN-OFF
LANDING
LIGHTS
MASTER SWITCH
ATC
1
SLEW
NORM
RIGHT
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
IDENT
MKR
Collins
ON
OFF
LEFT
BAT BUS
BRT
DIM
DIM
DG
FREE
ARM
ENG
AUTO
IGN
OFF
OFF-RESET
VOICE
RANGE
PUS
AUTO
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
PUS
H
EC
YD
ALT
HDG
H
STEEP
APPR
ACTIVE
IA
D
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
APPR
2
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
7½
10
BUS
TIE
POWER
STAT
3
PROP
GOV
2
DATA
1
RIGHT
SEC
ESC
PILOT
AUDIO
5
5
DCU2
MENU
ADV
5
LEFT
7½
MENU
5
RIGHT
2
ESIS
BUS
5
RELAY
5
MASTER
CABIN
5
LEFT
SEC
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
2
7
6
3
5
23 2 5
21
17 19
15
4
1000
FT
7
ACFT ALT
1000 FT
-1
M
A
X
11
35
13
RATE
M
I
N
10
30
1
TEST
0
CABIN
PRESS
DUMP
ERASE
HEADSET
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-32
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAKEOFF/RUN-UP
1.Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
2.Autoilot/Yaw Damp/Electric Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST and SET
3.Center Pedestal
Prop Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY FORWARD
Condition Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOW IDLE
4.Engine Run-up
Auto-Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM
Engine Anti-Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Overspeed Governors/Rudder Boost . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Prop Pitch Solenoid/Primary Governor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXERCISE and CHECK
Autofeather . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST and ARM
Manual Propeller Feathering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5.Pilot’s Right Subpanel
Ice Protection Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST AS REQUIRED
6.Copilot’s Left Subpanel
Pneumatic System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
7.Center Pedestal
Cabin Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST and SET
For Training Purposes Only
Revision: Original - July 10, 2013
18-33
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAKEOFF FINAL ITEMS
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
O
T
6
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
AVIONICS
MASTER
POWER
AUTO
L GEN
R GEN
MAIN
OFF
STARTER ONLY
PILOT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
2
GOV
+
OFF
AUTO
PROP
MANUAL
FUEL VENT
3
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
RIGHT
PILOT
DISPLAY
STBY
UP
DN
BEACON
GEAR
DOWN
L
NORM
EMER
FREQ
TUNE
1
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
L DC GEN
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L CHIP DETECT
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
UP
20
FLAPS
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
LDG GEAR
WARN TEST
TEMP
INCR CMS
CABIN
K
35
3 4
ELEC
HEAT
6
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
INCR
EXT
LEFT
TR
IM
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
OFF
0
ENVIR
OFF
I I I I I II
I
I I 10
0
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
5
5
VACUUM
INCHES OF MERCURY
5
PSI
7
30
5
2
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
OVERSPEED
WARN TEST
MAN COOL
OFF
----------
CABIN
ALT
1 5K
ON
NORM
AUTO
AUTO
----------
0
60
80
DOWN
+
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
TEST
GND
COM
DG
FREE
SLEW
-
121.5
NORM
BLOWER
1
SE
ADC
2
NORM
STROBE
NOSE
HD LT
TEST
AHRS
MFD SLEW
1
PFD
2
LDG GEAR CONTROL
OFF
ICE PROTECTION
HI
COPILOT
SURFACE
DEICE
SINGLE
MANUAL
TEST
PARKING BRAKE
ATC
1
4
SLEW
-
RECOG
AUTO
AUTOFEATHER
ARM
RIGHT
OFF
OFF
ON
WSHLD ANTI-ICE
NORMAL
OPEN
TEST
IGNITION AND
ENGINE START
LEFT
RIGHT
OFF
NORM
OFF
TEST
2
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
LEFT
NAV
INPH
NORM
I I I I
II
BAT
ESIS
ON
OFF
OFF
ICE
AUDIO
ALTN
OFF
EMER
OFF
ON
TAXI
LIGHTS
DOWN-OFF
DG
FREE
NORM
RIGHT
LANDING
MKR
Collins
ON
OFF
LIGHTS
MASTER SWITCH
PROP
SYNC
2
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
IDENT
DIM
DIM
OFF
LEFT
BAT BUS
BRT
T I LT
BRT
ARM
ENG
AUTO
IGN
OFF
OFF-RESET
VOICE
RANGE
PUS
H
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
H
EC
YD
ALT
PUS
H
STEEP
APPR
ACTIVE
IA
D
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
APPR
HDG
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
7½
10
BUS
TIE
POWER
STAT
3
PROP
GOV
2
DATA
1
RIGHT
SEC
ESC
PILOT
AUDIO
5
5
DCU2
MENU
ADV
5
LEFT
7½
MENU
5
RIGHT
2
ESIS
BUS
5
RELAY
5
MASTER
CABIN
5
LEFT
SEC
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
CABIN
PRESS
DUMP
TEST
ERASE
HEADSET
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-34
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
BEFORE TAKEOFF FINAL ITEMS
1.Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
2.Pilot’s Left Subpanel
Engine Switches:
Auto-Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM/AS REQUIRED
Engine Anti-Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF/AS REQUIRED
Autofeather . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM
3.Pilot’s Right Subpanel
Light Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4.Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ALT
5.Environmental Panel
Bleed Air Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Envir Bleed Air Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO/LOW AS REQUIRED
6.Annunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONSIDERED
For Training Purposes Only
Revision: Original - July 10, 2013
18-35
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
AFTER TAKEOFF
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
T
O
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
2
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
H
AVIONICS
MASTER
POWER
R GEN
MAIN
AUTOFEATHER
ARM
RIGHT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
STARTER ONLY
MANUAL
TEST
PARKING BRAKE
PILOT
DISPLAY
STBY
OFF
AUTO
PROP
MANUAL
FUEL VENT
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
RIGHT
LANDING
GEAR
2
LEFT
OFF
RIGHT
1
UP
DN
BEACON
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
GEAR
DOWN
BLOWER
STROBE
L
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
NOSE
HD LT
TEST
L DC GEN
L CHIP DETECT
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
+
1 5K
ON
NORM
TEST
UP
20
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
TEMP
INCR CMS
CABIN
K
35
3 4
5
6
MODE
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
OFF
0
ENVIR
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
TR
IM
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
INCR
EXT
LEFT
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
3
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
CABIN ALT WARN
TEST
SILENCE
DECR
ENVIR
BLEED AIR
NORMAL
I I I I I II
I
I I 10
0
INCHES OF MERCURY
5
PSI
7
30
5
2
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
0
60
80
DOWN
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
FLAPS
SE
AHRS
MFD SLEW
1
PFD
2
LDG GEAR CONTROL
OFF
ICE PROTECTION
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
OFF
OFF
ON
PILOT
OPEN
TEST
IGNITION AND
ENGINE START
LEFT
+
AUTO
TEST
OFF
NORM
OFF
WSHLD ANTI-ICE
NORMAL
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
RIGHT
RECOG
INPH
NORM
I I I I
II
L GEN
LEFT
NAV
AUDIO
ALTN
OFF
BAT
ESIS
ON
OFF
OFF
ICE
OFF
EMER
OFF
ON
TAXI
LIGHTS
DOWN-OFF
LANDING
LIGHTS
MASTER SWITCH
ATC
1
SLEW
NORM
RIGHT
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
IDENT
MKR
Collins
ON
OFF
LEFT
BAT BUS
BRT
DIM
DIM
DG
FREE
ARM
ENG
AUTO
IGN
OFF
OFF-RESET
VOICE
RANGE
PUS
AUTO
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
H
EC
YD
ALT
PUS
H
STEEP
APPR
ACTIVE
IA
D
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
APPR
HDG
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
7½
10
BUS
TIE
POWER
STAT
3
PROP
GOV
2
DATA
1
RIGHT
SEC
ESC
PILOT
AUDIO
5
5
DCU2
MENU
ADV
5
LEFT
7½
MENU
5
RIGHT
2
ESIS
BUS
5
RELAY
5
MASTER
CABIN
5
LEFT
SEC
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
CABIN
PRESS
DUMP
TEST
ERASE
HEADSET
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-36
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
AFTER TAKEOFF
1.Pilot’s Right Subpanel
Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
Landing and Taxi Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2.Yaw Damp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3.Center Pedestal
Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
For Training Purposes Only
Revision: Original - July 10, 2013
18-37
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
AFTER LANDING
DO NOT OPERATE
ON DRY GLASS
WINDSHIELD WIPER
OFF
PARK
PILOT
OVHD
FLOOD
OFF
INSTR
INDIRECT
OFF
COPILOT
OVHD
FLOOD
OFF
BRT
BRT
BRT
ANNUN
PUSH-BRT
SLOW
DIM
FAST
MASTER
PANEL
LIGHTS
ON
OFF
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
BRT
BRT
OVHD PED
& SUBPANEL
OFF
CABIN
LIGHT
PAX
60
80
20
0
OFF
40
60
80
BRT
BRT
ENTRY
LIGHTS
WARNING
ON
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
FSB
L GEN R GEN
TPL FED
CTR
EXT
PWR
60
30
DC % LOAD 100
BRT
OFF
DIM
40
DC % LOAD 100
COPILOT
INSTR
PNL
OFF
INTERIOR
MASTER
ON
NO SMK
FSB
DC
20
COPILOT
DISPLAYS
BRT
OPERATIONAL LIMITATIONS
THE MARKINGS AND PLACARDS INSTALLED
IN THE AIRPLANE CONTAIN OPERATING
LIMITATIONS WHICH MUST BE COMPLIED
WITH WHEN OPERATING THIS AIRPLANE
IN THE COMMUTER CATEGORY. OTHER OPERATING
LIMITATIONS WHICH MUST BE COMPLIED WITH
WHEN OPERATING THIS AIRPLANE IN THE
CATEGORY ARE CONTAINED IN THE AIRPLANE
FLIGHT MANUAL. NO ACROBATIC MANEUVERS
INCLUDING SPINS ARE APPROVED. THIS
AIRPLANE APPROVED FOR VFR, IFR DAY AND
NIGHT OPERATIONS AND IN ICING CONDITIONS.
0
SIDE
PANEL
OFF
+
40
60-
10
VOLTMETER
BUS SELECT
FULL DN FLAP
158
MANEUVERING
184
COMPASS CORRECTION
CALIBRATE WITH
ENGINE ON
359
4
120
02 4
121 150 180 2111 2
151 182 2
-------------
DOOR UNLOCKED
-------------
-------------
-------------
CABIN ALT HI
CABIN DIFF HI
R FUEL PRES LO
-------------
-------------
-------------
R OIL PRES LO
L BLEED FAIL
-------------
R BLEED FAIL
-------------
PRESS
T
O
T
9
60 9
59
TES
EXTINGUISHER
PUSH
ENG FIRE
F/W VALVE
PUSH
CLOSED
VNAV
NAV
SPEED
1/2 BANK
MASTER
CAUTION
DISCHARGED
CH
T
CPL
PUSH
N
CA
FD
YD/AP DISC 
CRS2
NCE
EC
Collins
Collins
Collins
RADIO CALL
N6410M
2
1
VOL
VOR
BARO
***NM 30.03 in
STD
60
1
42
3
NORM
NAV
2
DME
2
REFS
PA
10
10
10
10
* * * KTS
REFS
MENU
ADV
SE
RADAR
TILT
H
H
AVIONICS
MASTER
POWER
L GEN
R GEN
MAIN
PILOT
BRAKE
DEICE
PROP TEST
GND IDLE
STOP
GOV
HI
COPILOT
SURFACE
DEICE
SINGLE
OFF
STARTER ONLY
MANUAL
TEST
PARKING BRAKE
ATC
1
SLEW
-
+
PILOT
DISPLAY
STBY
OFF
NORM
ADC
2
EMER
FREQ
TUNE
1
NORM
2
CDU
NORM
RTU
RMT TUNE
NORM
DISABLE
GND
COM
DG
FREE
SLEW
-
121.5
NORM
LDG GEAR CONTROL
OFF
ICE PROTECTION
AUTO
PROP
MANUAL
2
STALL
WARN
LEFT
OFF
UP
DN
FUEL VENT
DOWN
LOCK
REL
LEFT
PITOT
RIGHT
LANDING
GEAR
2
RIGHT
GEAR
DOWN
BLOWER
STROBE
L
L GEN TIE OPEN
HYD FLUID LOW
RVS NOT READY
R GEN TIE OPEN
R DC GEN
L NO FUEL XFR
BAT TIE OPEN
DUCT OVERTEMP
R NO FUEL XFR
R CHIP DETECT
L ENG ICE FAIL
L FUEL QTY
ELEC HEAT ON
EXT PWR
R FUEL QTY
R ENG ICE FAIL
L BL AIR OFF
AUTOFTHER OFF
----------
OXY NOT ARMED
RUD BOOST OFF
R BL AIR OFF
TAIL
FLOOD
NOSE
HD LT
TEST
L DC GEN
L CHIP DETECT
L PITOT HEAT
R
----------
----------
L ENG ANTI-ICE
FUEL CROSSFEED
WING DEICE
L BK DEICE ON
MAN TIES CLOSE
L PROP PITCH
CABIN ALTITUDE
LDG/TAXI LIGHT
L IGNITION ON
OFF
HYD FLUID
SENSOR
+
1 5K
ON
NORM
TEST
UP
20
.5
TAKEOFF
AND
APPROACH
.5
----------
R PITOT HEAT
R ENG ANTI-ICE
R IGNITION ON
R BK DEICE ON
6
BLOWER
4
AUTO
0
TEMP
INCR CMS
CABIN
K
35
3 4
6
DECR
ENVIR
BLEED AIR
NORMAL
BLEED AIR VALVES
LEFT OPEN RIGHT
LOW
PNEU & ENVIR OFF
CABIN DIFF
WARN TEST
OFF
ENG FIRE TEST
DET
50 80
°F
FLIGHT
INCR
EXT
LEFT
TR
IM
10
UP
CHRONOMETER
GO AROUND
GEAR HORN
SILENCE
UT
LT
ET
P
O
W
E
R
T
R
I
M
5
LIFT
10
SE
DN
NO
C
O
N
D
I
T
I
O
N
SE
UP
NO
LOW
IDLE
CHRONOMETER
UT
LT
ET
FUEL
CUTOFF
FEATHER
PSI
15
HIGH
RPM
IDLE
2000
RIGHT
2
3
4
20
P
R
O
P
INCR
E
L
E
V
A
T
O
R
UP
1500
OXYGEN
SUPPLY PRESSURE
H
C
T
I
P
D
N
DN
NO
1000
USE NO
OIL
00007 8
99998 9
1
6
25
TAKEOFF
LANDING
AND
REVERSE
500
0
HOURS 1/10
100
CABIN AIR
M
I
R
T
P
I
T
C
H
SE
20
OFF
HIGH IDLE
NO
PSI
PNEUMATIC
PRESSURE
OFF
0
ENVIR
OFF
I I I I I II
I
I I 10
0
CABIN ALT WARN
TEST
SILENCE
MODE
3
5
INCHES OF MERCURY
5
PSI
7
30
5
2
LDG GEAR
WARN TEST
VACUUM
ELEC
HEAT
INCR
R PROP PITCH
40
35
THDS FT PER MIN
1
INCR
COCKPIT
TAIL DEICE
2
1 CABIN CLIMB4
STALL
WARN TEST
OFF
MAN MAN TEMP
INCR
HEAT
OFF
----------
CABIN
ALT
OVERSPEED
WARN TEST
MAN COOL
AUTO
AUTO
----------
0
60
80
DOWN
ENVIRONMENTAL
TEMP
WINDOW
DEFOG
PROP GND SOL
PASS OXYGEN ON AIR COND N1 LOW
RELAY
FLAPS
SE
AHRS
MFD SLEW
1
PFD
2
BEACON
AUTO
AUTOFEATHER
ARM
RIGHT
OFF
OFF
ON
WSHLD ANTI-ICE
NORMAL
OPEN
TEST
IGNITION AND
ENGINE START
LEFT
RIGHT
OFF
NORM
OFF
TEST
1
ACTUATORS
STANDBY
GEN TIES
MAN CLOSE
BUS SENSE
RESET
LEFT
RECOG
INPH
NORM
I I I I
II
BAT
ESIS
ON
OFF
OFF
2
NAV
AUDIO
ALTN
OFF
EMER
OFF
ON
ICE
LIGHTS
DOWN-OFF
TAXI
LIGHTS
MASTER SWITCH
DG
FREE
NORM
RIGHT
LANDING
IDENT
MKR
Collins
ON
OFF
ENGINE ANTI-ICE
RIGHT
LEFT
ON
GEN
RESET
GEN-UP TO RESET
BRT
DIM
DIM
OFF
LEFT
BAT BUS
1
ARM
ENG
AUTO
IGN
OFF
OFF-RESET
VOICE
RANGE
PUS
AUTO
T I LT
BRT
PROP
SYNC
ON
ON
EXT
PWR
BOTH
BOTH
RANGE
PUS
AUTO
T I LT
DIM
SPKR
GCS
TILT
BRT
IDENT
ADF
AUTO
COMM
1/2
Collins
NORM
NAV / BRG
DME-H
GCS
VOICE
NORM
2
2
LEC
N6410M
AUDIO
ALTN
NAV
DME
H
SE
T
H
NAV / BRG
RADAR
INPH
1
DATA
PUS
BRT
Collins
MKR
SPKR
S
2
1
PA
21
IDENT
AUTO
COMM
COMM
M
DATA
PUS
LEC
ADF
1
NORM
* * * MIN
S
MENU
ADV
MIC
OXY
STD
40
10 20
I II
II
1
1
T
H
MIC
OXY
2
VOL
PUS
H
COMM
XMIT
PA
BARO
1500
80 098CRS
PUS
T
S
1
MASTER
WARNING
PRESS TO RESET
PUS
IR
D
SY
MA
AP
H
S/
UP
ALT
H
EC
YD
ALT
PUS
H
STEEP
APPR
ACTIVE
IA
D
TERR
INHIB
ACTIVE
FLAP
OVRD
ACTIVE
APPR
HDG
PUS
H
PUS
G/S
INHIB
ACTIVE
HDG
T
CRS1
FLC
DOWN
L
VS
C
FD
IR
Collins
T
202
PRESS TO RESET
XMIT
PA
1
-------------
184
PRESS TO RESET
PRESS TO RESET
2
L OIL PRES LO
ENG FIRE
F/W VALVE
PUSH
CLOSED
DISCHARGED
184
166
GR EXTENDED
APPROACH FLAP
0
2 270
27 300
1 3 330 3
60
00 3
29
30
POS 0 29
STEER 0
------------L FUEL PRES LO
EXTINGUISHER
PUSH
MASTER
CAUTION
MASTER
WARNING
0
GR EXTENSION
GR RETRACT
OFF
3 N 33
0
INSTRUMENT
EMERG LTS
ON
MAXIMUM
IAS KNOTS
30
PROP AMPS
0
0
AMP
20
10
BAT
BATT
20
VOLT
GROUND
FINE
FRICTION
LOCK
LIFT
U
P
CAUTION
REVERSE
ONLY WITH
ENGINES
RUNNING
UP
UP
FLAP
REVERSE
4
APPROACH
FRICTION
LOCK
0
0
DOWN
AILERON TRIM
DN
LEFT
0
1
1
5
5
1 0 1
3
5
ENGINE
3
5
CROSSFEED FLOW
ENGINE
STANDBY PUMP
ON
RIGHT
LEFT
3
3
FLAP
RUDDER TAB
RIGHT
WARNING
BUS
TPL FED
L GEN
R GEN
BAT
POWER
5
7½
5
5
ANN
BLEED
AIR
WARN
OIL
PRESS
WARN
5
5
5
IND
5
IND
OFF
OFF
AUX TRANSFER
OVERRIDE
6
2
AUTO
USABLE FUEL
1273 LB EACH MAIN
533 LB EACH AUX
SEE MANUAL
10
12
MAIN TANK
ONLY
QTY
0
MAIN TANK
ONLY
14
LBS X 100
12
QTY
0
FUEL QUANTITY
TEST
LBS X 100
MAIN
LEFT
AUTO
PULL ON
SYSTEM READY
14
OXYGEN
STANDBY
PUMP
AUX
FUEL
XFER
5
10
5
MFD
FGP
COPILOT PFD
5
5
5
& DCP
RTU
QTY
IND
5
PRESS
WARN
QTY
WARN
5
5
LEFT
ENG FIRE EXT
ENTRY
CROSS
FEED
10
EDCI
3
2
2
7½
7½
7½
7½
INSTR CNTL
CNTL
CNTL INSTR
BATTERY BUS
GND
AVNCS
5
5
5
LIGHTS
COM
5
5
CDU2
RIGHT
QTY
IND
5
DBU
5
5
PRESS
WARN
5
ESIS
& DCP
LEFT
QTY
WARN
5
COPILOT PEDESTAL
5
5
RIGHT
2
BAT
DISP
½
5
5
3
CONT
BUS
HEAT
GND
CNTL
BAT
EDC2
DCU2
2
15
2
2
SNSR
HDG
CHG
7½
RIGHT
RIGHT
1
PILOT
3
RIGHT
FAN
AUDIO
CONT
AUDIO
AVIONICS
BUS
FSU
XM WX
COM2
MFD
COPILOT
AUDIO
COPILOT
20
25
3
5
7½
10
1
3
SERVO
MOTOR
IND &
CONTROL
SIDE PNL
FSB &
BAGGAGE
TEST
L GEN
TPL FED
CONT
AUDIO
PROP
LH CB
PNL
AVIONICS
BUS
XM R
AHC1
AHC2
RTU
5
20
30
5
2
2
LIGHTS
OUTSIDE
AIR
PITCH
SUB PNL
OVHD &
COPLT FLT
READING
5
5
3
7½
5
5
TEMP
TRIM
CONSOLE
INSTR
INSTR
CABIN
CONTROL
7½
GEN
7½
5
BUS
TIE
POWER
BLEED
AIR
CONTROL
RIGHT
LEFT
5
5
5
7½
5
INDIRECT
LIGHTS
ANN
TEMP
5
PRESS
OXY
5
5
CONTROL
CABIN
ALT
NOSE
½
½
PILOT WSHLD
ANTI ICE
PROP
5
SEC
ADC1
AHC1
PILOT
PFD
PILOT
DCP
ATC1
NAV1
25
3
2
2
10
2
3
3
ADC2
AHC2
COPILOT
PFD
COPILOT
DCP
ATC2
NAV2
R GEN
WSHLD
HF
5
10
WIPER
COM
ANT
LEFT
SURF
SELCAL
PILOT
PFD
5
5
1
PNL
COOLING
DC
FUEL
VENT
STBY ENG
ANTI ICE
TCAS
2
SEC
TAWS
DEICE
CONTROL
5
COM3
L GEN
5
HIGH
CMU
AVIONICS
BUS
LEFT
5
DC
MN ENG
ANTI
ICE
POWER
RIGHT
HIGH
CIGAR
R GEN
CONTROL
1
5
FURNISHING
SYNC
WEATHER
EQMT
COOLING
FLT
INSTR
WARN
MASTER
5
AVIONICS
RESET
CABIN
DIFF
LH CB
PNL
CHIP
DETR
FGC2
7½
MEM 1
7½
10
BUS
TIE
POWER
STAT
3
PROP
GOV
2
DATA
1
RIGHT
SEC
ESC
PILOT
AUDIO
5
5
DCU2
MENU
ADV
5
LEFT
7½
MENU
5
RIGHT
2
ESIS
BUS
5
RELAY
5
MASTER
CABIN
5
LEFT
SEC
1
WARN
COM1
WARN
ENVIRONMENTAL
BUS
TPL FED
L GEN
R GEN
BAT
EMER
5
AVIONICS
3
RCDR
CCP
NO SMK
BUS TIE
ENGINE
INDICATION
DCUI
DCUI
7½
AURAL
TEL
RTER
FSU
5
ELECTRICAL
PILOT
FUEL SYSTEM
LIGHTS
CDU1
5
VOICE
TEL
XVCR
5
FIRE
DETR
RIGHT
7½
FIRE
WALL
VALVE
AVIONICS
LEFT
5
OIL
PRESS
PLT FLT
IND
PILOT PFD
LEFT
5
TORQUE
METER
5
SERVO
FIRE
STANDBY WALL
PUMP
VALVE
LEFT
5
IGNITOR
POWER
FLAP
AUXILIARY
AUX
FUEL
XFER
LEFT
7½
START
CONT
RIGHT
PASSENGER
MANUAL DROP OUT
RIGHT
LEFT
5
STALL
20
10
2
AUTO
FEATHER
FLAP
FLIGHT
FGC1
AUX TRANSFER
OVERRIDE
8
4
LEFT
5
OFF
6
8
4
LEFT
ENGINE
WARN
LANDING
GEAR
STANDBY PUMP
ON
2
2
10
2
3
3
MFD
LEFT
RADAR
DME1
CDU1
GPS1
7½
2
3
3
RADIO
DME2
CDU2
GPS2
5
10
10
7½
DEICE
HEATER
HEATER
IAPS
BRAKE
IEC
5
5
15
15
5
5
5
7½
CONTROL
LIGHTER
CONV1
CONV2
RIGHT
RIGHT
DEICE
COPILOT
PFD
RIGHT
10
7½
2
HEATER
IAPS
ALTM
CHART
MEM 2
H
PUS
T
SE
MEM3
LEC
ZOOM
PILOT’S STATIC
AIR SOURCE
NORMAL
COCKPIT VOICE RECORDER
ALTERNATE
SEE FLIGHT MANUAL PERFORMANCE SECTION FOR
INSTR CAL ERROR
TEST
HOLD 5 SEC
CABIN
PRESS
DUMP
TEST
ERASE
HEADSET
RUDDER
BOOST
P
R
E
S
S
OFF
CABIN
ALT
9
8
10
1000
FT
11
35
21
17 19
15
0
1
2
3
5
4
ACFT ALT
1000 FT
-1
M
A
X
13
RATE
M
I
N
23 2 5
6
7
30
CABIN
ALT
CABIN
WARNING DEPRESSURIZE
BEFORE LANDING
For Training Purposes Only
Revision: Original - July 10, 2013
18-38
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
AFTER LANDING
1.Pilot’s Left Subpanel
Engine Switches:
Auto-Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Anti-Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2.Pilot’s Right Subpanel
Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF/AS REQUIRED
Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3.Copilot’s Left Subpanel
Environmental Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET AS REQUIRED
4.Center Pedestal
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
For Training Purposes Only
Revision: Original - July 10, 2013
18-39
AS-18 Maneuvers and Procedures
Pilot Training Manual
King Air 350i
This page intentionally left blank.
For Training Purposes Only
Revision: Original - July 10, 2013
18-40
AS-18 Maneuvers and Procedures