King Air B200 Operating Handbook 2010 CAE Simuflite

8/10/2019 King Air B200 Operating Handbook 2010 CAE Simuflite

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King Air 200Operating Handbook


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King Air 200 Operating Handbook

Developed for Training Purposes Jan 06 P-1

Preflight ProceduresCAE SimuFlite

PREFLIGHT INSPECTION

NOTE: After the first flight of the day the Preflight Inspection can be

omitted except for those items indicated by a H. The fueltank caps and engine oil quantity/filler cap need not be

checked unless system(s) were serviced. External inspections

with flaps down may be conducted at intervals deemed appro-priate by the pilot.

CABIN/COCKPIT

Electric Toilet (if installed). . . . . . . . . . . . . . . . . . . . . . . . KNIFE VALVE OPEN

H Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Emergency Exit . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE AND UNLOCKED

Control Locks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE AND STOWED

Trim Tabs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET TO 0 UNITS

Condition Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL CUTOFF

Landing Gear Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DNParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Ignition and Engine Start. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENSURE OFF

Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON, CHECK 23 VOLTS MINIMUM

Fuel Quantity (main and auxiliary) . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

ELT (cockpit installations). . . . . . . . . . . . . . . . ARM [XMT] EXTINGUISHED

Gear Down Annunciators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ILLUMINATED

Flap Control (if desired). . . . . . . . . . . . . . . . . . . . . APPROACH, THEN DOWN

(check indicator)Airstair Door (B200) Circuitry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Airstair Door (B200C) Circuitry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Oxygen System Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . COMPLETE

H Battery. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

LEFT WING AND NACELLE

Cabin Door Seal, Step Extension Cable, Light Wire,Damper, and Handrails . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Cabin Windows. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

H Auxiliary Fuel Tank Cap. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Flaps (condition, asymmetry protection, and flap tracks) . . . . . . . . . CHECK

Oil Breather Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

H Brake Lines, Brake Wear, Brake Deice Lines (if installed) . . . . . . . . . CHECK

Fire Extinguisher (if installed). . . . . . . . . . . . . . . . . . . . . . CHECK PRESSURE

FIRE EXTINGUISHER PRESSURE VS. TEMPERATURE

continued on next page

F

C

-40

-40

-20

-29

0

-18

20

-7

40

4

60

16

80

27

100

38

120

49

PSI

Range

190

to

240

220

to

275

250

to

315

290

to

365

340

to

420

390

to

480

455

to

550

525

to

635

605

to

730

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P-2 Developed for Training Purposes Jan 06

Preflight Procedures CAE SimuFlite

continued from previous page

Inverter Cooling Louver. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Aileron and Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Flush Outboard Wing Fuel Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Static Wicks (4). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Navigation, Recognition, & Strobe Lights . . . . . . . . . . . . . . . . . . . . . . CHECK

H Main Fuel Tank Cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Stall Warning Vane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

H Tiedown. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

Outboard Deice Boot and Stall Strip . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Ice Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Heated Fuel Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Ram Scoop Fuel Vent. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Gravity Line Drain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Inverter Cooling Louvers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Wing Leading Edge Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAINH Landing Gear (doors, wheel well, strut, tires, brakes) . . . . . . . . . . . . .CHECK

H Chock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

Fuel Filter and Fuel Stainer Drains . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

H Engine Oil . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK QUANTITY, CAP SECURE

Engine Compartment Door (outbd) . . . . . . . . . . . . . SECURE, BLEED VALVE

EXHAUST CLEAR

Exhaust Stack (outbd) . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR CRACKS

Top Cowling Locks (outbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Nacelle Cooling Ram Air Inlets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

H Prop . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR NICKS, DEICE BOOT SECURE

Engine Intake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Top Cowling Locks (inbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Exhaust Stack (inbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR CRACKS

Generator Cooling Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Engine Compartment Door (inbd). . . . . . . . . . . . . . . SECURE, BLEED VALVEEXHAUST CLEAR

Heat Exchanger Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Hydraulic Landing Gear Service Door . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Inboard Deice Boot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Heat Exchanger Outlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Hydraulic Landing Gear Vent Lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Auxiliary Fuel Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Lower Antennas and Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK


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Developed for Training Purposes Jan 06 P-3

Preflight ProceduresCAE SimuFlite

NOSE

OAT Probe/Relief Tube Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKBrake Reservoir Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Left Avionics Access Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Air Conditioning Condenser Exhaust Duct . . . . . . . . . . . . . . . . . . . . . . CLEAR

Windshield and Wipers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Radome . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Pitot Masts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Landing and Taxi Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Nose Gear (shimmy damper, stop block, torque knee, strut, tire). . . .CHECK Chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

Nose Gear Doors and Wheel Well. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Air Conditioner Condenser Intake Duct . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Right Avionics Access Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

RIGHT WING AND NACELLE

Ejector Exhaust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARAuxiliary Fuel Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Battery Drain. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Battery Air Inlet (Airplane Prior to BB-1632,

BL-141, and BW-30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR, VALVE FREE

Heat Exchanger Outlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Inboard Deice Boot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Battery Exhaust (Airplanes Prior to BB-1632,

BL-141, and BW-30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Heat Exchanger Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Engine Oil . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK QUANTITY, CAP SECURE

Engine Compartment Door (inbd). . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

BLEED VALVE EXHAUST CLEAR

Exhaust Stack (inbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR CRACKS

Top Cowling Locks (inbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Nacelle Cooling Ram Air Inlets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Prop . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR NICKS, DEICE BOOT SECURE

Engine Intake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARTop Cowling Locks (outbd) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Exhaust Stack (outbd) . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR CRACKS

Generator Cooling Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Engine Compartment Door (outbd) . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

BLEED VALVE EXHAUST CLEAR

Fuel Filter and Fuel Strainer Drains . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAINS

Landing Gear (doors, strut, tires, wheel well) . . . . . . . . . . . . . . . . . . . .CHECK

Fire Extinguisher (if installed). . . . . . . . . . . . . . . . . . . . . . CHECK PRESSURE Chock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

Heated Fuel Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Ram Scoop Fuel Vent. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Gravity Line Drain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Inverter Cooling Louvers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Wing Leading Edge Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN



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P-4 Developed for Training Purposes Jan 06

Preflight Procedures CAE SimuFlite


External Power Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSED

Ice Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Outboard Deice Boot and Stall Strip . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Tiedown. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

Flush Outboard Wing Fuel Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Main Fuel Tank Cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Navigation, Recognition, and Strobe Lights . . . . . . . . . . . . . . . . . . . . .CHECK

Static Wicks (4). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKAileron and Bendable Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Flaps (condition, asymmetry protection, flap tracks,

limit switches, and position transmitter) . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Inverter Cooling Louver. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Brake Lines, Brake Wear, Brake Deice Lines (if installed) . . . . . . . . . .CHECK

Oil Breather Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Auxiliary Fuel Tank Cap. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Cabin Windows. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

RIGHT AFT FUSELAGE

Lower Antennas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Ventral Fin Drain Holes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Lower Aft Cabin Access Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Tiedown. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVED

Oxygen Service Access Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Static Ports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

ELT (aft fuselage installations) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED

Cabin Air Exhaust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Access Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

TAIL

Ventral Fin and Static Wick (1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

VOR Antennas (right and left). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKRudder, Rudder Tab, Stinger and Static Wicks (4) . . . . . . . . . . . . . . . .CHECK

Horizontal Stabilizer, Boots and Static Wicks

(right and left) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Elevator, Tab, and Static Wicks (3 each side) . . . . . . . . . . . . . . . . . . . .CHECK

Position Light, Tail Floodlights (if installed)

(left and right) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

LEFT AFT FUSELAGEAccess Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECURE

Static Ports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Oxygen Overpressure Discharge and

Aft Compartment Drain Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Relief Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR


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CAE SimuFlite

07-03

Normal Procedures

King Air 200 (early) Operating HandbookDeveloped for Training Mar 01 N1

The Following Weather Conditions May Be Conducive to SevereIn-Flight Icing: Visible rain at temperatures below 0C ambient air tempera-

ture. Droplets that splash or splatter on impact at temperatures below

0C ambient air temperature.

Procedures for Exiting the Severe Icing Environment

These procedures are applicable to all flight phases from takeoff tolanding. Monitor the ambient air temperature. While severe icingmay form at temperatures as cold as -18C, increased vigilance is

warranted at temperatures around freezing with visible moisturepresent. If the visual cues specified in the Limitations Section of the

AFM for identifying severe icing conditions are observed, accom-

plish the following: Immediately request priority handling from Air Traffic Control to

facilitate a route or an altitude change to exit the severe icingconditions in order to avoid extended exposure to flight condi-tions more severe than those for which the airplane has beencertificated.

Avoid abrupt and excessive maneuvering that may exacerbatecontrol difficulties.

Do not engage the autopilot. If the autopilot is engaged, hold the control wheel firmly and

disengage the autopilot. If an unusual roll response or un-commanded roll control move-

ment is observed, reduce the angle-of-attack. Do not extend flaps when holding in icing conditions. Operation

with flaps extended can result in a reduced wing angle-of-attack,with the possibility of ice forming on the upper surface further

aft on the wing than normal, possibly aft of the protected area. If the flaps are extended, do not retract them until the airframe

is clear of ice. Report these weather conditions to Air Traffic Control.

ICING CONDITIONS


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CAE SimuFlite Normal Procedures


PF . . . . . . Pilot Flying. The pilot responsible for controlling theaircraft. Performs tasks and responds to checklist

challenges.PNF . . . . . Pilot Not Flying. Reads checklist challenges. . . . . . . . Intermediate stop/fast turnaround.

PNF PF

Passenger Briefing (see N-10) . . . . . . . . . . COMPLETEDCabin Door/Cargo Door Circuitry Check . . . . . COMPLETED

Cabin Door/Cargo Door . . . . . . . . . . . . . . . LOCKED Load and Baggage . . . . . . . . . . . . . . . . . SECURED Weight and Balance . . . . . . . . . . . . . . . . CHECKED Emergency Exit . . . . . . . . CONFIRM SECURE/UNLOCKED Control Locks . . . . . . . . . . . . . . . . . . . REMOVED

Seats . . . . . . . . . . . . . . . . . . . . . . POSITIONED Fire Extinguisher . . . . . . . . . . . . . . . . . . CHECKED Seat Belts/Shoulder Harnesses . . . . . . . . . . . FASTENED Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . SET Sub Panel Switches . . . . . . . . . . . . . . . . . . . . SET Landing Gear Switch Handle . . . . . . . . . . . . . DOWN Power Levers . . . . . . . . . . . . . . . . . . . . . . IDLE Propeller Controls . . . . . . . . . . . . . . FULL FORWARD

Condition Levers . . . . . . . . . . . . . . . . . . . CUT-OFF Friction Locks . . . . . . . . . . . . . . . . . . AS DESIRED Pedestal Switches . . . . . . . . . . . . . . . . . . . . . SET Cabin Sign . . . . . . . . . . . . . . . . . . . . . . . BOTH Cabin Temp Mode . . . . . . . . . . . . . . . . . . . . OFF Vent Blower . . . . . . . . . . . . . . . . . . . . . . AUTO Aft Blower . . . . . . . . . . . . . . . . . . . . . . . . OFF

Radiant Heat . . . . . . . . . . . . . . . . . . . . . . . OFFPilots Static Air Source . . . . . . . . . . . . . . . NORMALFuel System (see N-11) . . . . . . . . . . . . . . . CHECKEDBattery . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Fuel Quantity (Main and Auxiliary) . . . . . . . . CHECKED DC Volts/Loadmeters . . . . . . . PRESS TO CHECK VOLTAGE Annunciator Lights . . . . . . . . . . . . . . . . . . . . TEST Landing Gear Handle Lights Test Switch . . . . PRESS TO TEST

Stall Warning . . . . . . . . . . . . . . . . . . . . . . TEST Fire Detectors and Fire Extinguishers . . . . . . . . . . . TEST Rotating Beacon . . . . . . . . . . . . . . . . . . . . . ON

Oxygen Supply Pressure . . . . . . . . . . . . . . . CHECKOxygen Supply Control Handle . . . . . . . . . . . . CHECKManual System . . . . . . . . . . . . . . . . . . PUSH OFF

Automatic System . . . . . . . . . . . PULL ON/SYS READYOxygen System Preflight (see N-11) . . . . . . . . COMPLETEMicrophone Switches . . . . . . . . . . . . . . . . NORMAL

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . IN

BEFORE STARTING ENGINES


10/174


11/174



PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Condition Lever . . . . . . . . . . . . . . . . . . FUEL CUT OFFIgnition/Engine Start . . . . . . . . STARTER ONLY/15 SEC MAXStarter Use . . . . . . . . . . . . . . . DO NOT EXCEED LIMITS

Starter Limitation 40 secs ON/60 secs OFF/40 secs ON/60 secs OFF/40 secs ON/30 mins OFF

Ignition/Engine Start . . . . . . . . . . . . . . . . . . . . OFF

Inverters . . . . . . . . . . . . . . . . . . . . . . . . . . ONDC Voltage and Loadmeters . . . . . . . . . . . . . . CHECKED

AC Voltage and Frequency . . . . . . . . . . . . . . CHECKEDAvionics Master . . . . . . . . . . . . . . . . . . . . . . . ONLights . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDCabin Temperature and Mode . . . . . . . . . . . AS REQUIREDInstruments . . . . . . . . . . . . . . . . CHECKED/NO FLAGSPropellers . . . . . . . . . . . . . . . . . . . . FULL FORWARDBrakes . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Autopilot (page N-14) . . . . . . . . . . . . . . . CHECKED Pressurization (page N-13) . . . . . . . . . . . CHECKED/SET Vacuum and Pneumatic Pressure (page N-13) . . . CHECKED

Primary, Overspeed Governors . . . . . . . . . . . . TESTEDand Rudder Boost (page N-15)Engine Ice Vanes (Cold Weather Ops N-17) . . . CONSIDERED

Autofeather (if installed) (page N-15) . . . . . . . . CHECKED Autofeather (if installed) . . . . . . . . . . . . . . . . . ARM Propeller Feathering (manual) . . . . . . . . . . . CHECKED Engine Controls Friction Locks . . . . . . . . . . . . . . . SET Flaps . . . . . . . . . . . . . . . . . . . . . CHECKED/SET Flight Controls . . . . . . . . . . FREE/CORRECT MOVEMENT

Elevator Trim (page N-14) . . . . . . . . . . . . . CHECKED Trim Tabs . . . . . . . . . . . . . . . . . . . CONFIRM SET Fuel Quantity . . . . . . . . . . . . . . . . . . . . CHECKED Flight Instruments . . . . . . . . . . . . . . . . . . CHECKED Engine Instruments . . . . . . . . . . . . . . . . . CHECKED

BEFORE TAKEOFF (RUNUP)

AFTER STARTING AND TAXIING

ENGINE CLEARING


12/174

CAE SimuFliteNormal Procedures

King Air 200 (early) Operating HandbookDeveloped for Training Mar 01N6

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Avionics and Radar . . . . . . . . . . . . . . . . CHECKEDBleed Air Valves . . . . . . . . . . . . . . . . . . . . OPEN

Annunciators . . . . . . . . . . . . . . . . . . CONSIDEREDTransponder . . . . . . . . . . . . . . . . . . . . . . . ONIce Protection . . . . . . . . . . . . . . . . . . AS REQUIREDPropeller Synchrophaser . . . . . . . . . . . . . . . . . OFF

Engine Auto-Ignition . . . . . . . . . . . . . . . . . ARMED

Ignition Annunciators . . . . . . . . . . . . . EXTINGUISHEDAutofeather Annunciators . . . . . . . . . . . . ILLUMINATEDITT/Torque . . . . . . . . . . . . . . . . . . . . . MONITOR

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . UP (VYSE MIN)

Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . ON

Climb Power . . . . . . . . . . . . . . . . . . . . . . . SETITT/Torque/N1 Limits . . . . . . . . . . . . . . . . MONITORPropeller . . . . . . . . . . . . . . . . . . . . . 1900 RPMPropeller Synchrophaser . . . . . . . . . . . . . . . . . ON

Autofeather . . . . . . . . . . . . . . . . . . . . . . . OFFEngine Instruments . . . . . . . . . . . . . . . . . MONITORCabin Sign . . . . . . . . . . . . . . . . . . . AS REQUIREDCabin Pressurization . . . . . . . . . . . . . . . . CHECKED

Aft Blower . . . . . . . . . . . . . . . . . . . AS REQUIREDExterior Lights . . . . . . . . . . . . . . . . . . . . . . . .Outside Check . . . . . . . . . . . . . . . . . . . COMPLETE

Cruise Power . . . . . . . . . . . SET/SEE TABLES & GRAPHSEngine Instruments . . . . . . . . . . . . . . . . . MONITORSystems . . . . . . . . . . . . . . . . . . . . . . MONITOR

Auxiliary Fuel Gages . . . . . . . . . . . . . . . MONITORPressurization . . . . . . . . . . . . . . . . . . . MONITORDestination Weather . . . . . . . . . . . . . . . . CONSIDER

Approach Procedure . . . . . . . . . . . . . . . . CONSIDERLanding Data . . . . . . . . . . . . . . . . . . . . REVIEW

CRUISE

CLIMB

TAKEOFF

BEFORE TAKEOFF


13/174



WEIGHT X 1,000 LBS

12.5 12 11 10 9VYSE 121 119 117 114 111

VREF 0 FLAPS 132 130 126 122 117

VREF 100% FLAPS 103 102 99 96 93

WT(LBS)X

1000

VREFVYSE

TEMPC

LANDING DISTANCE (FT)

PRESSURE ALTITUDE (FT)

SL 2000 4000 6000

12.5 40 3150 3300 3550 390020 2950 3150 3300 3550

103 0 2750 2950 3150 3300121 -20 2550 2750 2950 3150

12 40 2950 3150 3350 365020 2750 2950 3150 3350

102 0 2550 2750 2950 3150

119 -20 2450 2550 2750 2950

11 40 2750 2950 3150 340020 2550 2750 2950 3150

99 0 2350 2550 2750 2950117 -20 2250 2350 2550 2750

10 40 2600 2800 3000 320020 2400 2600 2800 3000

96 0 2200 2400 2600 2800114 -20 2100 2200 2400 2600

9 40 2450 2650 2850 305020 2250 2450 2650 2850

93 0 2050 2250 2450 2650111 -20 1950 2050 2250 2450

The data given is estimated and is based on zero wind conditions. For exact values,refer to POH, Performance.

Wind factor for VAP is 1/2 Wind Speed Component + Gust Factor (Max. 10 kts).

For other/associated conditions, refer to pages F-34/35.

Landing 100% Flaps


14/174

Normal Procedures


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Pressurization (see Table page N-7) . . . . . . . . . . . . . SETAltimeters . . . . . . . . . . . . . . . . . . . . . . . . . . SETCabin Sign . . . . . . . . . . . . . . . . . . . . AS REQUIREDIce Protection . . . . . . . . . . . . . . . . . . . AS REQUIREDExterior Lights . . . . . . . . . . . . . . . . . . . CONSIDEREDPower . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Approach Speeds . . . . . . . . . . . . . . . . . . . CONFIRMPressurization . . . . . . . . . . . . . . . . . . . . . CHECKEDCabin Sign . . . . . . . . . . . . . . . . . . . NO SMOKE/FSB

Autofeather Switch . . . . . . . . . . . . . . . . . . . . . ARMFlaps . . . . . . . . . . . . . . . . . . . . . . . . APPROACHPropeller Levers . . . . . . . . . . . . . . . . . FULL FORWARDLanding Gear . . . . . . . . . . . . . . . . . . . . . . DOWNLanding and Taxi Lights . . . . . . . . . . . . . . AS REQUIREDRadar . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY

When Landing Assured:Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . VREFFlaps . . . . . . . . . . . . . . . . . . . . . . . DOWN/100%

Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . OFF

When Landing Assured:Condition Levers . . . . . . . . . . . . . . . . . . . HI IDLEPropellers . . . . . . . . . . . . . . . . . . FULL FORWARDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . DOWN

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . VREF

Yaw Damp . . . . . . . . . . . . . . . . . . . . . . . . OFFPower Levers . . . . . . LIFT & REVERSE AFTER TOUCHDOWN

MAXIMUM REVERSE THRUST LANDING

NORMAL LANDING

APPROACH

DESCENT

CAE SimuFlite


15/174



PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Power . . . . . . . . . . . . . . . . . MAXIMUM ALLOWABLEAirspeed . . . . . . . . . . . . . . . . . . . . . . . 100 KTSWhen clear of obstacles:

Normal Climb Attitude . . . . . . . . . . . . . ESTABLISHEDFlaps . . . . . . . . . . . . . . . . . . . . . UP (VYSE MIN)

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . UP

Landing and Taxi Lights . . . . . . . . . . . . . . AS REQUIREDEngine Ice Vanes . . . . . . . . . . . . . . . . . . . . EXTEND

Monitor oil pressure and engine ITT.Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . OFFTransponder . . . . . . . . . . . . . . . . . . . . . . . . OFFRadar . . . . . . . . . . . . . . . . . . . . . . . . STBY/OFFEngine Auto-Ignition . . . . . . . . . . . . . . . . . . . . OFFElectrical Load . . . . . . . . . . . . . . . . . OBSERVE LIMITSTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

AFTER LANDING

BALKED LANDING


16/174


17/174



PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Firewall Valve CBs . . . . . . . . . . . . . . . . . . . . . PULLBoost Pump CBs . . . . . . . . . . . . . . . . . . . . . . PULLFirewall Shutoff Valves . . . . . . . . . . . . . . . . . . CLOSEStandby Pumps . . . . . . . . . . . . . . . . . . . . . . . ON

Listen for standby pump operation.Battery Switch . . . . . . . . . . . . . . . . . . . . . . . ON

L/R FUEL PRESS annunciators illuminate.Firewall Shutoff Valves . . . . . . . . . . . . . . . . . . OPEN

L/R FUEL PRESS annunciators extinguish.Standby Pumps . . . . . . . . . . . . . . . . . . . . . . . OFF

L/R FUEL PRESS annunciators illuminate.Crossfeed . . . . . . . . . . . . . . . . ALTERNATE LEFT/RIGHT

The FUEL CROSSFEED and respective L/R FUEL PRESSannunciators illuminate.

Crossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . OFFNo Transfer Lights . . . . . . . . . . . . . . . . PRESS TO TESTFirewall Valve and Boost Pump CBs . . . . . . . . . . . . RESET

Oxygen Pressure Gage . . . . . . . . . . . CHECK/SUFFICIENTPercent of Usable Capacity . . . . . . . . . . . . . DETERMINEOxygen Duration . . . . . . . . . . . . . . . . . . . COMPUTE

Duration with Full Bottle . . . . . . . . . . . . . . SEE TABLEDuration with Less than Full Bottle . . . . . . . . . COMPUTE Compute oxygen duration in minutes from the table by multi-

plying the full bottle duration by the percent of usable capacity. Pilot and copilot are each counted as two people with diluter

demand masks set at 100% or NORMAL mode.Mask Mic Operation . . . . . . . . . . . . . . . . . . . CHECKOxygen System Control . . . . . . . . . . PULL ON SYS READYDiluter Demand System . . . CHECK OPERATION/MASKS 100%

WARNING:Oxygen duration is computed for the auto-deployedtype mask, rated at 3.7 Standard Liters per Minute -NTPD flow. Early Puritan-Bennett masks are not color

coded, new masks have an orange and black fittingend. Scott-Sierra masks have a green fitting-end. Thistable is also used for the quick-donning diluter demandcrew oxygen masks by doubling the number of crewmasks is use for computation. Crew masks are to useeither the normal or the 100% mode up to 20,000 feetpressure altitude and the 100% mode above 20,000feet pressure altitude.

OXYGEN SYSTEM CHECK

FUEL SYSTEM CHECK


18/174



2500

2000

1500

500

1000

00 25 50 75 100

PERCENT OF USABLE CAPACITY

GA

GE

PRESSURE

PSIG

60C(140F)

0C(32F)

-60C(-76F)

BOTT

LETEM

PERATU

RE

** Number of People Using1 2 3 4 5 6 7 8 9

Duration in Minutes

StatedCylinderSize

(cu ft)

22 144 72 48 36 28 24 20 18 16

50 317 158 105 79 63 52 45 39 35

77 488 244 162 122 97 81 69 61 54

115 732 366 244 183 146 122 104 91 81

** Number of People Using

10 11 12 13 14 15 **16 **17

Duration in Minutes

StatedCylinder

Size(cu ft)

22 14 13 12 11 10 * * *

50 31 28 26 24 22 21 19 18

77 48 44 40 37 34 32 30 28

115 73 66 61 56 52 48 45 43* Will not meet oxygen requirements.** For normal oxygen duration computations, count each diluter-demand crew mask in

use as 2 (e.g., with a crew of 2 and 4 passengers, enter the table at 8 people using).


19/174


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Inverter No. 1 . . . . . . . . . . . . . . . . . . . . . . . . ONVerify INVERTER annunciator extinguishes. Check that invertervoltage and frequency are within tolerances.

Inverter No. 2 . . . . . . . . . . . . . . . . . . . . . . . . ONVerify INVERTER annunciator extinguishes. Check that invertervoltage and frequency are within tolerances.

PC-17A Inverters: 115V AC +5/-7% - 400 Hz 1% PC-250 Inverters: 115V AC 5% - 400 Hz 1%

Condition Levers . . . . . . . . . . . . . . . . . . . . . HI IDLECabin Altitude Selector . . . . . . . . . . . . . . . . . . . SET

Adjust so that CABIN ALT dial indicates an altitude 1,000 feetbelow field pressure altitude. Consider Vacuum and PneumaticPressure Check, below.

Rate Control Selector Knob . . . . . SET INDEX AT 12 OCLOCKCabin Pressurization Switch . . . . . . . . . . . . HOLD IN TESTCabin Climb Indicator . . . . CHECK FOR DESCENT INDICATION

Cabin Pressurization Switch . . . . . . . . . . . RELEASE WHEN. . . . . . . . . . . . . . .PRESSURIZATION CONFIRMEDCabin Altitude Selector Knob . . . . . . . . . . . . . . ADJUST

Adjust selector knob so that inner scale (ACFT ALT) indicatesplanned cruise altitude plus 1,000 ft. If this setting does not resultin an outer scale (CABIN ALT) indication of at least 500 ft abovetakeoff field pressure altitude, adjust as required.

Left Bleed Air Valve . . . . . . . . . . . . . INSTR & ENVIR OFFL/R BLEED FAIL Annunciators . . . . . . . . . . . EXTINGUISHL BL AIR OFF Annunciator . . . . . . . . . . . . ILLUMINATEDGyro Suction Gage . . . . . . . . . . . . . . IN GREEN ARCPneumatic Pressure Gage . . . . . . . . . . . IN GREEN ARC

Right Bleed Air Valve . . . . . . . . . . . . INSTR & ENVIR OFFR BL AIR OFF Annunciator . . . . . . . . . . . . ILLUMINATEDL/R BLEED FAIL Annunciators . . . . . . . . . . ILLUMINATEDGyro Suction Gage . . . . . . . . . . . . . . . . . . . ZEROPneumatic Pressure Gage . . . . . . . . . . . . . . . . ZERO

Left Bleed Air Valve . . . . . . . . . . . . . . . . . . . . OPENL BL AIR OFF Annunciator . . . . . . . . . . . . EXTINGUISHED

Right Bleed Air Valve . . . . . . . . . . . . . . . . . . . OPEN

VACUUM AND PNEUMATIC PRESSURE CHECK

PRESSURIZATION CHECK

INVERTER CHECK



20/174


21/174

Normal Procedures


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Rudder Boost . . . . . . . . . . . . . . . . . . . . . . . . ONProp Governor Test Switch . . . . . . HOLD IN PROP GOV TESTITT/Torque Limits . . . . . . . . . . . . . . . . . . . OBSERVELeft Power Lever . . . . . . . . . . . . INCREASE UNTIL STABLE

. . . . . . . . . . . . . . . . . . . . .AT 1870 40 RPMLeft Propeller Lever . . . . . . . . . . . . RETARD TO DETENT

. . . . . . . . . . . . . . . . . . .THEN FULL FORWARDLeft Power Lever . . . . . . INCREASE UNTIL RUDDER MOVESLeft Power Lever . . . . . . . . . . . . . . . . . . . . . IDLE

Right Power Lever . . . . . . . . . . . INCREASE UNTIL STABLE. . . . . . . . . . . . . . . . . . . . .AT 1870 40 RPM

Right Propeller Lever . . . . . . . . . . . RETARD TO DETENT. . . . . . . . . . . . . . . . . . .THEN FULL FORWARD

Right Power Lever . . . . . INCREASE UNTIL RUDDER MOVESRight Power Lever . . . . . . . . . . . . . . . . . . . . IDLE

Prop Governor Test Switch . . . . . . . . . . . . . . . RELEASE

Auto Ignition Switches . . . . . . . . . . . . . . . . . . . . ON

Power Levers . . . . . . . . . . . APPROX 500 FT-LBS TORQUEAutofeather Switch . . . . . . . . . . . . . . . . HOLD TO TESTL/R AUTOFEATHER Annunciators . . . . . . . . . . ILLUMINATEDLeft Power Lever . . . . . . . . . . . . . . . . . . . . RETARD

At approximately 410 ft-lbs R AUTOFEATHER and L IGNITIONannunciators illuminate.

At approximately 260 ft-lbs L AUTOFEATHER annunciatorbegins flashing with prop feathering action.

Left Power Lever . . . . . . . . . . . . . INCREASE TO REGAIN . . . . . . . . . . . . . .AUTOFEATHER ANNUNCIATORS

Right Power Lever . . . . . . . . . . . . . . . . . . . . RETARDAt approximately 410 ft-lbs L AUTOFEATHER and R IGNITIONannunciators illuminate.

At approximately 260 ft-lbs L AUTOFEATHER annunciatorbegins flashing with prop feathering action.

Power Levers . . . . . . . . . . . . . . . . . . . RETARD BOTHAuto Ignition Switches . . . . . . . . . . . . . . . . . . . OFF

AUTOFEATHER CHECK

OVERSPEED GOVERNOR AND RUDDER BOOST CHECK

CAE SimuFlite


22/174

Normal Procedures


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Bleed Air Valves . . . . . . . . . . . . . . . . . . . . . OPENSelect ENVIR OFF for more efficient cooling on the ground.

Cabin Temp Mode . . . . . . . . . . . . . . . . . . . . AUTOCabin Temperature . . . . . . . . . . . . . . . . AS REQUIRED

Vent Blower . . . . . . . . . . . . . . . . . . . . . . . AUTOAft Blower (if installed) . . . . . . . . . . . . . . AS REQUIRED

Cabin/Cockpit Air Control . . . . . . . . . . . . . AS REQUIRED With the CABIN TEMP MODE switch in AUTO, MAN HEAT or

MAN COOL, the ventilation blower operates at low speed.For increased air circulation, turn the vent blower to HIGH.

For maximum cooling, the ventilation blower should be in theHIGH mode and the aft blower (if installed) should be selectedON.

For maximum heating, the ventilation blower should be selectedto HIGH and the aft blower should be selected OFF.

Battery Switch . . . . . . . . . . . . . . . . . . . . . . . ONDoor . . . . . . . . . . . . . . . . . . . . OPEN AND LOCKED

Verify CABIN DOOR annunciator illuminated.Cabin Door Fwd Switch . . . . . . . . . . . . . . . . . . PRESSPressing the lower forward bayonet receiver should extinguishCABIN DOOR annunciator

Cabin Door . . . . . . . . . . . . . . . . . . UNLOCK/CLOSEVerify CABIN DOOR annunciator remains illuminated.

Cabin Door . . . . . . . . . . . . . . . . . . CLOSED/LATCHEDVerify CABIN DOOR annunciator extinguishes.

NOTE: Observe the requirement for both bayonet and lockingmechanism micro-switches to be contacted before CABINDOOR annunciator will extinguish. Otherwise consult MEL.

Cabin Door . . . . . . . . . . . . . . . . . . . . . AS DESIRED

CABIN DOOR CIRCUITRY CHECK

HEATING/COOLING SYSTEM

CAE SimuFlite


23/174

Normal Procedures


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Either Generator . . . . . . . . . . . . . . . . . . . . . . OFFVoltmeter . . . . . . . . . . . . . . . ENSURE 28V INDICATIONBattery Switch . . . . . . . . . . . . OFF MOMENTARILY/NOTE

. . . . . . . . . . . . . . . . . .LOADMETER DECREASEIf decrease exceeds 2.5%:

Battery . . . . . . . . . . . . CONTINUE CHARGING/REPEAT

. . . . . . . . . . . . . . .ABOVE STEPS EVERY 90 SECSBattery Charge Annunciator . . . . . . . EXTINGUISHED WHEN

. . . . . . . . . . . .LOADMETER DECREASE BELOW 2.5%

The following checks should be completed in addition to the

normal checklist items during cold weather operations. Please referto the AFM Section 4 for complete procedures to be accomplishedduring cold weather operation.

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . CHECKPower Levers . . . . . . . . . . . . . . . . . . . . . . IDLE

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . ARML/R IGNITION ON annunciators illuminated.

Power Levers . . . . . . . ADVANCE ABOVE 360 - 460 FT-LBSL/R IGNITION ON annunciators extinguished.

Power Levers . . . . . . . . . . . . . . . . . . . . . . IDLEL/R IGNITION ON annunciators illuminated.

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . OFFL/R IGNITION ON annunciators extinguished.

Engine Anti-Ice . . . . . . . . . . . . . . . . . . . . . . CHECKBefore Takeoff:

Power Levers . . . . . . . . . . . . . . . . . . 1800 RPMEngine Ice Vane Controls . . . . . . . . . . . . EXTEND

Verify Torque drop. Monitor ICE VANE annunciators.Engine Ice Vane Controls . . . . . . . . . . . . RETRACT

Verify Torque increase. Monitor ICE VANE annunciators.Power Levers . . . . . . . . . . . . . . . REDUCE TO IDLE

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . CHECK

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . HIGHObserve increase on left and right loadmeters and magneticcompass fluctuation.

Windshield Anti-Ice . . . . . . . . . . . OFF/THEN NORMALObserve increase on left and right loadmeters and magneticcompass fluctuation.

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . OFF


BEFORE TAKEOFF (RUNUP) COLD WEATHER OPS

NI-CAD BATTERY CHECK (GROUND OPERATION ONLY)

CAE SimuFlite


24/174

Normal Procedures



Electrothermal Propeller Deice . . . . . . . . . . . . . . CHECKAutomatic Prop Deice . . . . . . . . . . . . . . . . . AUTODeice Ammeter . . . . . . . . . . . . . . . 14 TO 18 AMPS

Monitor for 90 seconds to ensure automatic timer operation.Manual Prop Deice Switch . . . HOLD IN MANUAL POSITION

Small deflection on both loadmeters indicates systemoperation. Deice ammeter should indicate zero amps.

Manual Prop Deice Switch . . . . . . . . . . . . . . RELEASE

Deice Ammeter . . . . . . . . . . . . . . . 14 TO 18 AMPSAutomatic Prop Deice . . . . . . . . . . . . . . . . . . OFF

CAUTION: Do not operate propeller deice when the propellers arestatic.

Surface Deice System . . . . . . . . . . . . . . . . . . CHECKPreflight . . . . . . . . . . . . . . . . CLEAN/UNDAMAGEDCondition Levers . . . . . . . . . . . . . . . . . . HIGH IDLEPneumatic Pressure . . . . . . . . . . . . . . . . . . CHECKSurface Deice Switch . . . . . . . . . SINGLE CYCLE/RELEASE

Pneumatic pressure decreases momentarily. Visually checkfor boot inflation then hold down. The wing boots inflate insix seconds followed by the horizontal stabilizer boots infour seconds.

Surface Deice Switch . . . . . . . . . . . . . MANUAL/HOLDPneumatic pressure decreases momentarily. Visually checkthe boots for inflation.

Surface Deice Switch . . . . . . . . . . . . . . . . . RELEASECondition Levers . . . . . . . . . . . . . . . . . . LOW IDLE

WARNING: Do not cycle the boots during takeoff.

Stall Warning and Pitot Heat . . . . . . . . . . . . . . . CHECK

CAUTION: Prolonged use of stall warning and pitot heat on theground will damage the heating elements.

Pages N-19 and N-20 have been intentionally omit-ted from this handout.

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King Air 200 (mid) Operating HandbookDeveloped for Training Jul 01 N3

PF . . . . . . Pilot Flying. The pilot responsible for controlling theaircraft. Performs tasks and responds to checklist

challenges.PNF . . . . . Pilot Not Flying. Reads checklist challenges. . . . . . . . Intermediate stop/fast turnaround.

PNF PF

Passenger Briefing (see N-12) . . . . . . . . . . COMPLETEDCabin Door/Cargo Door Circuitry Check . . . . . COMPLETED

Cabin Door/Cargo Door . . . . . . . . . . . . . . . LOCKEDElectric Toilet (if installed) . . . . . . . . . KNIFE VALVE OPEN

Load and Baggage . . . . . . . . . . . . . . . . . SECURED Weight and Center-of-Gravity . . . . . . . . . . . CHECKED Seats . . . . . . . . . . . . . . . . . . . . . . POSITIONED

Control Locks . . . . . . . . . . . . . . . . . . . REMOVED Seats/Rudder Pedals . . . . . . . . . . . . . . . ADJUSTEDSeatbelts/Shoulder Harnesses . . . . . . . . . . . FASTENEDOxygen System Ready . . . . . . . . . . . . . . . PULL ONOxygen System Preflight (page N-17) . . . . . . COMPLETEDFuel Panel Circuit Breakers . . . . . . . . . . . . . . . . . IN

Pilots Instrument Panel . . . . . . . . . . . . . . . CHECKED Compass Control . . . . . . . . . . . . . . . . . . . SLAVED

TYPE I Prop Sync Switch (if installed) . . . . . . . . . . . OFF TYPE II Prop Sync Switch (if installed) . . . . . . . . . . . ON

Pilots Clock . . . . . . . . . . . . . . . . . . CHECKED/SET Pilots Subpanel . . . . . . . . . . . . . . . . . . CHECKED Mic Selector Switch . . . . . . . . . . . . . . . . . NORMAL Parking Brake . . . . . . . . . . . . . . . . . CONFIRM SET Engine Ice Vane Switches . . . . . . . . . . . . . EXTENDED

Pilot Air Control . . . . . . . . . . . . . . . . AS REQUIRED Defrost Air Control . . . . . . . . . . . . . . . AS REQUIRED Landing Gear Control . . . . . . . . . . . . . . . . . . . DN Landing Gear Relay Circuit Breaker . . . . . . . . . . . . IN All Other Switches . . . . . . . . . . . . . . . . . . . . OFF Avionics Panel Switches . . . . . . . . . . . . AS REQUIRED

Radar . . . . . . . . . . . . . . . . . . . OFF OR STANDBY Power Console . . . . . . . . . . . . . . . . . . . CHECKED

Power Levers . . . . . . . . . . . . . . . IDLE/FRICTION SET Propeller Levers . . . . . . . . FULL FORWARD/FRICTION SET Condition Levers . . . . . . . . FUEL CUT OFF/FRICTION SET Elevator/Aileron/Rudder Trim . . . . . . . . . . . . . . SET




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PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Right Ignition and Engine Start . . . . . . . . . . . . . . . ONRight Condition Lever . . . . . . . . . LOW IDLE (12% N1 MIN)ITT and N1 . . . . . . . . . . . . . . . MONITOR/1000C MAXRight Oil Pressure . . . . . . . . . . . . . . . . . . . CHECKEDRight Condition Lever . . . . . . . . . . . . . . . . . HIGH IDLERight Ignition and Engine Start . . . . . . . . OFF (N1 50% MIN)

Right Generator . . . . . . . . . . . ON/CHARGE BATTERY/OFFGenerator OFF when loadmeter reads approximately 0.50

Left Ignition and Engine Start . . . . . . . . . . . . . . . . ONRight Generator . . . . . . . . . . . . . . ON (L N1 12% MIN)Left Condition Lever . . . . . . . . . LOW IDLE (L N1 12% MIN)ITT and N1 . . . . . . . . . . . . . . . MONITOR/1000C MAXLeft Oil Pressure . . . . . . . . . . . . . . . . . . . . CHECKEDLeft Ignition and Engine Start . . . . . . . . OFF (N1 50% MIN)DC Volts/Loadmeters . . . . . . . . . . CHECKED (27.5 TO 29V)Left Generator . . . . . . . . . . . . . . . . . RESET/THEN ONRight Condition Lever . . . . . . . . . . . . . . . . . LOW IDLE

Avionics Master Switch . . . . . . . . . . . . . . . . . . . OFFLeft/Right Generator Switches . . . . . . . . . . . . . . . . OFFBattery . . . . . . . . . . . . . . . . . . . . . . . . . . . ONExternal Power . . . . . . . . . . . . . . . . OFF/CONNECTEDExternal Power . . . . . . . . . . . . . . . . . . . . . . . ON

Voltmeter . . . . . . . . . . . . . . . . . . . . . 28 TO 28.4 VPropeller Levers . . . . . . . . . . . . . . . . . . . . FEATHERRight Ignition/Engine Start . . . . . . . . . . . . . . . . . ON

R FUEL PRESS Annunciator . . . . . . . . . . . . EXTINGUISHEDRight Condition Lever . . . . . . . . . LOW IDLE (12% N1 MIN)ITT/N1 . . . . . . . . . . . . . . . . . MONITOR/1000C MAXRight Oil Pressure . . . . . . . . . . . . . . . . . . . CHECKEDRight Ignition/Engine Start . . . . . . . . . . OFF (N1 50% MIN)Left Ignition/Engine Start . . . . . . . . . . . . . . . . . . ONL FUEL PRESS Annunciator . . . . . . . . . . . . EXTINGUISHED

Left Condition Lever . . . . . . . . . . LOW IDLE (12% N1 MIN)ITT/N1 . . . . . . . . . . . . . . . . . MONITOR/1000C MAXLeft Oil Pressure . . . . . . . . . . . . . . . . . . . . CHECKEDLeft Ignition/Engine Start . . . . . . . . . . . OFF (N1 50% MIN)External Power . . . . . . . . . . OFF/DISCONNECT/SECUREDLeft and Right Generators . . . . . . . . . . . RESET/THEN ONPropeller Levers . . . . . . . . . . . . . . . . . FULL FORWARD

ENGINE STARTING EXTERNAL POWER

ENGINE STARTING (BATTERY)


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King Air 200 (mid) Operating HandbookDeveloped for Training Jan 03N6

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Condition Lever . . . . . . . . . . . . . . . . FUEL CUT OFFIgnition/Engine Start . . . . . . STARTER ONLY/40 SEC MAXStarter Use . . . . . . . . . . . . . . DO NOT EXCEED LIMITS

Starter Limitation - 40 secs ON/60 secs OFF/40 secs ON/60 secs OFF/40 secs ON/30 mins OFF

Ignition/Engine Start . . . . . . . . . . . . . . . . . . . OFF

Inverters (page N-13) . . . . . . . . . . . . . . . CHECKED Inverters . . . . . . . . . . . . . . . SELECT No. 1 OR No. 2 Loadmeters . . . . . . . . . . . . PARALLELED WITHIN 10% Avionics Master . . . . . . . . . . . . . . . . . . . . . ON External Lights . . . . . . . . . . . . . . . . . AS REQUIRED Cabin Lights . . . . . . . . . . . . . . . . . . AS REQUIRED Bleed Air Valves . . . . . . . . . . . . OPEN OR ENVIR OFF Cabin Temp Mode . . . . . . . . . . . . . . . . . . . AUTO Cabin Temperature . . . . . . . . . . . . . . . AS REQUIRED Instruments . . . . . . . . . . . . . . . . . . . . . CHECKED

Brake Deice (if installed) . . . . . . . . . . . . . . CHECKED

Flight Controls . . . . . . . . . . CHECKED/FREE MOVEMENT Flaps . . . . . . . . . . . . . . . . . . . . . CHECKED/SET Brakes . . . . . . . . . . . . . . . . . RELEASED/CHECKED

Avionics and Radar . . . . . . . . . . . . . . . . CHECKED

Pressurization (page N-13) . . . . . . . . . . . CHECKED/SETAutopilot (page N-14) . . . . . . . . . . . . . . . CHECKEDElevator Trim (page N-14) . . . . . . . . . . . . . CHECKED

Trim Tabs . . . . . . . . . . . . . . . . . . . CONFIRM SETPrimary and Overspeed Governorsand Rudder Boost (page N-15) . . . . . . . . . . . . TESTED

Autofeather (if installed) (page N-15) . . . . . . . . CHECKED Autofeather (if installed) . . . . . . . . . . . . . . . ARMED Propeller Feathering (manual) . . . . . . . . . . . CHECKED

Vacuum and Pneumatic Pressure (page N-16) . . . . CHECKED Engine Ice Vanes . . . . . . . . . . . . . . . . . . CHECKED Systems for Icing Flight (page N-19) . . . . . . . . CHECKED Fuel Quantity . . . . . . . . . . . . . . . . . . . . CHECKED Flight Instruments . . . . . . . . . . . . . . . . . . CHECKED Engine Instruments . . . . . . . . . . . . . . . . . CHECKED

BEFORE TAKEOFF (RUNUP)

BEFORE TAXI

ENGINE CLEARING


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Normal Procedures

King Air 200 (mid) Operating HandbookDeveloped for Training Jan 03 N7

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Propeller Levers . . . . . . . . . . . . . . . . . FULL FORWARDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETBrake Deice (if installed) . . . . . . . . . . . . . . . . . . OFFLeft/Right Bleed Air . . . . . . . . . . . . . . . . . . . . OPEN

Aft Blower . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Annunciators . . . . . . . . . . . EXTINGUISHED/CONSIDEREDIce Protection . . . . . . . . . . . . . . . . . ON IF REQUIRED

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . ON . . . . . .(L and R IGNITION ON annunciators illuminated)

Engine Ice Vanes . . . . . . . . . . . . CONFIRM EXTENDED(L and R ENG ANTI-ICE annunciators illuminated)

Windshield Anti-Ice . . . . . . . . . . . . . . . NORMAL/HIProp Heat . . . . . . . . . . . . . . . . . . . . . . . AUTOLeft and Right Fuel Vent Heat . . . . . . . . . . . . . . . ONStall Warning Heat . . . . . . . . . . . . . . . . . . . . ONLeft and Right Pitot Heat . . . . . . . . . . . . . . . . . ON

Generator Load . . . . . . . . . . . . . . . . . . . . CHECKEDEngine Ice Vanes . . . . . . . . . RETRACTED IF NOT REQUIREDExternal Lights . . . . . . . . . . . . . . . . . . AS REQUIREDTransponder . . . . . . . . . . . . . . . . . . . . . . . . ON

Crew Briefing . . . . . . . . . . . . . . . . . . . . COMPLETE

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . HOLDPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Autofeather Annunciators (if installed) . . . . . . . ILLUMINATED

Brakes . . . . . . . . . . . . . . . . . . . . . . . . RELEASEDLanding Gear . . . . . . . . . . . . . . UP AT POSITIVE CLIMBFlaps . . . . . . . . . . . . . . . . . . . . . . . UP (VYSE MIN)

Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . ONClimb Power . . . . . . . . . . . . . . . . . . . . . . . . SET

ITT/Torque/N1 Limits . . . . . . . . . . . . . . . . . MONITORPropeller . . . . . . . . . . . . . . . . . . . . . . . 1900 RPMPropeller Synchrophaser . . . . . . . . . . . . . . . . . . ON

Autofeather . . . . . . . . . . . . . . . . . . . . . . . . . OFFEngine Instruments . . . . . . . . . . . . . . . . . . MONITORCabin Sign . . . . . . . . . . . . . . . . . . . . AS REQUIREDCabin Pressurization . . . . . . . . . . . . . . . . . CHECKED

Aft Blower . . . . . . . . . . . . . . . . . . . . AS REQUIREDLights . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

CLIMB

TAKEOFF

BEFORE TAKEOFF (FINAL ITEMS)

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King Air 200 (mid) Operating HandbookDeveloped for Training Mar 01 N9

WEIGHT X 1,000 LBS

12.5 12 11 10 9VYSE 121 119 117 114 111

VREF 0 FLAPS 132 130 126 122 117

VREF 100% FLAPS 103 102 99 96 93

WT(LBS)X

1000

VREFVYSE

TEMPC

LANDING DISTANCE (FT)

PRESSURE ALTITUDE (FT)

SL 2000 4000 6000

12.5 40 3150 3300 3550 390020 2950 3150 3300 3550

103 0 2750 2950 3150 3300121 -20 2550 2750 2950 3150

12 40 2950 3150 3350 365020 2750 2950 3150 3350

102 0 2550 2750 2950 3150

119 -20 2450 2550 2750 2950

11 40 2750 2950 3150 340020 2550 2750 2950 3150

99 0 2350 2550 2750 2950117 -20 2250 2350 2550 2750

10 40 2600 2800 3000 320020 2400 2600 2800 3000

96 0 2200 2400 2600 2800114 -20 2100 2200 2400 2600

9 40 2450 2650 2850 305020 2250 2450 2650 2850

93 0 2050 2250 2450 2650111 -20 1950 2050 2250 2450

The data given is estimated and is based on zero wind conditions. For exact values,refer to POH, Performance.

Wind factor for VAP is 1/2 Wind Speed Component + Gust Factor (Max. 10 kts).

For other/associated conditions, refer to pages F-34/35.

Landing 100% Flaps


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Normal Procedures

King Air 200 (mid) Operating HandbookDeveloped for Training Jul 01N10

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Approach Speed . . . . . . . . . . . . . . . . . . CONFIRMEDPressurization (see F-33) . . . . . . . . . . . . . . . CHECKEDCabin Sign . . . . . . . . . . . . . . . . . . . NO SMOKE/FSBFlaps . . . . . . . . . . . . . . . . . . . . . . . . APPROACHLanding Gear . . . . . . . . . . . . . . . . . . . . . . . . DNLights . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDProp Sync (Type I) . . . . . . . . . . . . . . . . . . . . . . OFFRadar . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDSurface Deice . . . . . . . . . . . . . . . CYCLED AS REQUIRED

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNAirspeed . . . . . . . . . . . . . . NORMAL APPROACH SPEEDYaw Damper . . . . . . . . . . . . . . . . . . . . . . . . OFFPower Levers . . . . . . . . . . . . . . . . . . . . . . . . IDLEPropeller Levers . . . . . . . . . . . . . . . . . FULL FORWARDPower Levers . . . . . . . BETA/REVERSE AFTER TOUCHDOWNBrakes . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNAirspeed . . . . . . . . . . . . . . NORMAL APPROACH SPEEDYaw Damper . . . . . . . . . . . . . . . . . . . . . . . . OFFCondition Levers . . . . . . . . . . . . . . . . . . . HIGH IDLE

Propeller Levers . . . . . . . . . . . . . . . . . . . HIGH RPMPower Levers . . . . . . . . LIFT/REVERSE AFTER TOUCHDOWNBrakes . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDCondition Levers . . . . . . . . . . . . . . . . . . . LOW IDLE

Power . . . . . . . . . . . . . . . . . MAXIMUM ALLOWABLEAirspeed . . . . . . . . . . . . . . . . . . . . . . . 100 KTSWhen clear of obstacles:Normal Climb . . . . . . . . . . . . . . . . . . ESTABLISHEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPLanding Gear . . . . . . . . . . . . . . . . . . . . . . . UP

BALKED LANDING

MAXIMUM REVERSE THRUST LANDING

NORMAL LANDING

BEFORE LANDING

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PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . . OFFEngine Ice Vanes . . . . . . . . . . . . . . . . . . . EXTENDEDLights . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDIce Protection . . . . . . . . . . . . . . . . . . . . . . . . OFFTransponder . . . . . . . . . . . . . . . . . . . . . . STANDBYRadar . . . . . . . . . . . . . . . . . . . . STANDBY OR OFFTrim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . SETFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . SET

Standby Boost Pumps/Crossfeed . . . . . . . . . . . . . . OFFAvionics Master . . . . . . . . . . . . . . . . . . . . . . . OFFInverter . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Autofeather . . . . . . . . . . . . . . . . . . . . . . . . . OFFLights . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Vent Blower . . . . . . . . . . . . . . . . . . . . . . . AUTOCabin Temp Mode . . . . . . . . . . . . . . . . . . . . . OFF

Aft Blower . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Radiant Heat . . . . . . . . . . . . . . . . . . . . . . . . OFFBattery . . . . . . . . . . . . . . . . . . . . . . . . CHARGEDITT . . . . . . . . STABILIZED AT MIN TEMP FOR ONE MINUTECondition Levers . . . . . . . . . . . . . . . . . FUEL CUT OFFPropeller Levers . . . . . . . . . . . . . . . . . . . . FEATHERDC Volts/Loadmeters . . . . . . . . . . . . . CHECK VOLTAGEOverhead Panel Switches . . . . . . . . . . . . . . . . . . OFF

Oxygen System Ready . . . . . . . . . . . . . . . . PUSH OFFBattery/Generator Switches . . . . . . . . OFF BELOW 15% N1Control Locks . . . . . . . . . . . . . . . . . . . . . INSTALLEDEmergency Exit . . . . . . . . . . . . . . . . . . . . . LOCKEDElectric Toilet . . . . . . . . . . . . . . SERVICED AS REQUIREDTiedowns/Chocks . . . . . . . . . . . . . . . . . AS REQUIREDExternal Covers . . . . . . . . . . . . . . . . . . AS REQUIREDPropeller Locks . . . . . . . . . . . . . . . . . . AS REQUIRED

Oil Quantity Check . . . . . . . . . . . . . . . . AS REQUIRED

SHUTDOWN

AFTER LANDING


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The passenger briefing should include the following items: Smoking Use of Safety Belts Seat Positions Normal and Emergency Exit Operation Fire Extinguishers Oxygen Use (if required) Survival Equipment (if required) Overwater Equipment (if required).

NOTE: This briefing is required to be given by the Pilot inCommand, crewmember, or other person designated bythe Certificate Holder before takeoff. It may be deliveredby means of an approved playback device but must be sup-plemented by printed cards appropriate to the aircraft.

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . ONL/R FUEL PRESS and L/R ICE VANE EXT annunciators illuminate.

Firewall Shutoff Valves . . . . . . . . . . . . . . . . . . CLOSEStandby Pumps . . . . . . . . . . . . . . . . . . . . . . . ONListen for operation. L/R FUEL PRESS annunciators illuminate.

Firewall Shutoff Valves . . . . . . . . . . . . . . . . . . OPENL/R FUEL PRESS annunciators extinguish.

Standby Pumps . . . . . . . . . . . . . . . . . . . . . . . OFFL/R FUEL PRESS annunciators illuminate.

Crossfeed . . . . . . . . . . . . . . . ALTERNATELY LEFT/RIGHTFUEL CROSSFEED Annunciators . . . . . . . . . . . ILLUMINATEL/R FUEL PRESSURE Annunciators . . . . . . . . . EXTINGUISHCrossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Auxiliary Tank Transfer . . . . . . . . . . . . . . . . . . AUTONo Transfer Lights . . . . . . . . . . . . . . . . PRESS TO TEST

FUEL SYSTEM CHECK

PASSENGER BRIEFING


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Normal Procedures

King Air 200 (mid) Operating HandbookDeveloped for Training Mar 01N14

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Control Wheel . . . . . . . . . . . . . . . PULL TO MID-TRAVELAutopilot . . . . . . . . . . . . . . . . . . . . . . . ENGAGEControl Wheel . . . . . . . . . . . . . PUSH FORWARD/HOLD

With the control wheel pushed forward, the trim wheel shouldmove toward nose-up.

Control Wheel . . . . . . . . . . . . . . . . . PULL AFT/HOLD

With the control wheel pushed forward, the trim wheel shouldmove toward nose-down.

Pitch Wheel . . . . . . . . . . . . . . . . . . . MOVE UP/DNThe control wheel should follow pitch wheel movement.

Turn Knob . . . . . . . . . . . . . . . . . . . . . . LEFT/RIGHTThe control wheel should follow turn knob movement.

HSI Heading Marker . . . . . . . . . . SET UNDER LUBBER LINEFlight Director . . . . . . . . . . . . . . . . SELECT HDG MODEHeading Marker . . . . . . . . . . . . . . . . . . . . . MOVE

The control wheel should follow heading marker movement.Control Wheel Disconnect Switch . . . . . . . . . . . . . PRESS

Autopilot . . . . . . . . . . . . . . . . . . . . . DISENGAGESIf AP DISC light begins flashing, press AP-YD/TRIM switch toextinguish light.

Autopilot . . . . . . . . . . . . . . . . . . . . . . . ENGAGE

Electric Trim . . . . . . . . . . . . . . . . . . . . . . . . . ONPitch Trim Switches . . . . . . . . . . . . . . . . . . . TOUCHAutopilot should disconnect but yaw damper remains engaged.

Primary Controls . . . . . . . CHECK FREEDOM OF MOVEMENT

Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . ONPilots and Copilots Switches . . . . . . . . CHECK OPERATIONTrim Quick Disconnect . . . . . . . . . . . . . . . . . . CHECKELECT TRIM OFF Annunciator . . . . . . . . . . . ILLUMINATEDElevator Trim . . . . . . . . . . . . . . . . . . . OFF THEN ONELEC TRIM OFF Annunciator . . . . . . . . . . . EXTINGUISHED

WARNING: Electric trim system operation should only occur withmovement of pairs of switches. Any elevator trim wheelmovement while depressing only one switch indicatessystem malfunction. The elevator trim control switchmust then be turned off and flight conducted using onlymanual trim wheel.

ELEVATOR TRIM CHECK

AUTOPILOT CHECK

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Normal Procedures

King Air 200 (mid) Operating HandbookDeveloped for Training Mar 01 N15

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Rudder Boost . . . . . . . . . . . . . . . . . . . . . . . . ONProp Governor Test Switch . . . . . . HOLD IN PROP GOV TESTITT/Torque Limits . . . . . . . . . . . . . . . . . . . OBSERVELeft Power Lever . . . . . . . . . . . . INCREASE UNTIL STABLE

. . . . . . . . . . . . . . . . . . .AT 1830 TO 1910 RPMLeft Propeller Lever . . . . . . . . . . . . . RETARD TO DETENT

. . . . . . . . . . . . . . . . . . .THEN FULL FORWARDLeft Power Lever . . . . . . . INCREASE UNTIL RUDDER MOVESLeft Power Lever . . . . . . . . . . . . . . . . . . . . . . IDLERight Power Lever . . . . . . . . . . . INCREASE UNTIL STABLE

. . . . . . . . . . . . . . . . . . .AT 1830 TO 1910 RPMRight Propeller Lever . . . . . . . . . . . . RETARD TO DETENT

. . . . . . . . . . . . . . . . . . .THEN FULL FORWARDRight Power Lever . . . . INCREASE UNTIL RUDDER MOVEMENTRight Power Lever . . . . . . . . . . . . . . . . . . . . . IDLEProp Governor Test Switch . . . . . . . . . . . . . . . RELEASE

Power Levers . . . . . . . . . . . APPROX 500 FT-LBS TORQUE

Autofeather Switch . . . . . . . . . . . . . . . . HOLD TO TESTL/R AUTOFEATHER Annunciators . . . . . . . . . . ILLUMINATEDLeft Power Lever . . . . . . . . . . . . . . . . . . . . RETARD

At approximately 410 ft-lbs R AUTOFEATHER annunciatorextinguishes.

At approximately 260 ft-lbs both AUTOFEATHER annunciatorsextinguish.

Right Power Lever . . . . . . . . . . . . . . . . . . . . RETARD At approximately 410 ft-lbs L AUTOFEATHER annunciator

extinguishes. At approximately 260 ft-lbs both AUTOFEATHER annunciators

extinguish.Power Levers . . . . . . . . . . . . . . . . . . . RETARD BOTH

NOTE:Autofeather annunciators will cycle on and off with torquefluctuation as propeller feathers.

AUTOFEATHER CHECK

OVERSPEED GOVERNOR AND RUDDER BOOST CHECK

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PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PFLeft Bleed Air Valve . . . . . . . . . . . . . INSTR & ENVIR OFF

L BL AIR OFF Annunciator . . . . . . . . . . . . ILLUMINATEDGyro Suction Gage . . . . . . . . . . . . . . IN GREEN ARCPneumatic Pressure Gage . . . . . . . . . . . IN GREEN ARC

Right Bleed Air Valve . . . . . . . . . . . . INSTR & ENVIR OFFR BL AIR OFF Annunciator . . . . . . . . . . . . ILLUMINATEDL/R BLEED FAIL Annunciators . . . . . . . . . . ILLUMINATEDGyro Suction Gage . . . . . . . . . . . . . . . . . . . ZEROPneumatic Pressure Gage . . . . . . . . . . . . . . . . ZERO

Left Bleed Air Valve . . . . . . . . . . . . . . . . . . . . OPENL BL AIR OFF Annunciator . . . . . . . . . . . EXTINGUISHEDL/R BLEED FAIL Annunciators . . . . . . . . . EXTINGUISHED

Right Bleed Air Valve . . . . . . . . . . . . . . . . . . . OPENR BL AIR OFF Annunciator . . . . . . . . . . . EXTINGUISHED

Bleed Air Valves . . . . . . . . . . . . . . . . . . . . . OPENSelect ENVIR OFF for more efficient cooling on the ground.

Cabin Temp Mode . . . . . . . . . . . . . . . . . . . . AUTOCabin Temperature . . . . . . . . . . . . . . . . AS REQUIRED

Vent Blower . . . . . . . . . . . . . . . . . . . . . . . AUTOAft Blower (if installed) . . . . . . . . . . . . . . AS REQUIREDCabin/Cockpit Air Control . . . . . . . . . . . . . AS REQUIRED

With the CABIN TEMP MODE switch in AUTO, MAN HEAT or MANCOOL, the ventilation blower operates at low speed. For increasedair circulation, turn the vent blower to HIGH. For maximum cooling,the ventilation blower should be in the HIGH mode and the aft blow-

er (if installed) should be selected ON. For maximum heating, theventilation blower should be selected to HIGH and the aft blowershould be selected OFF.

HEATING/COOLING SYSTEM

VACUUM AND PNEUMATIC PRESSURE CHECK

Normal Procedures



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42/174

Normal Procedures


PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDoor . . . . . . . . . . . . . . . OPEN/MECHANISM LOCKED

With door open and the mechanism locked, verify the DOORUNLOCKED annunciator illuminates.

Door . . . . . . . . . . . CLOSED AND LATCHED/NOT LOCKEDWith the door closed and latched but not locked, verify the

DOOR UNLOCKED annunciator remains illuminated.Door . . . . . . . . . . . . . . . . . . . CLOSED AND LOCKED

With the door closed and locked, the DOOR UNLOCKEDannunciator should extinguish.

Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Ensure that the door is closed and locked using the following: Ensure that the door handle will not move out of the locked

position without depressing the release button. Lift the top doorstep and ensure that the red safety arm is

around the plunger. Ensure that the green index mark on each of the four locking

bolts align with the black pointer in the observation port.

Either Generator . . . . . . . . . . . . . . . . . . . . . . OFFVoltmeter . . . . . . . . . . . . . . . ENSURE 28V INDICATIONBattery Switch . . . . . . . . . . . . OFF MOMENTARILY/NOTE

. . . . . . . . . . . . . . . . . .LOADMETER DECREASEIf decrease exceeds 2.5%Battery . . . . . . . . . . . . . CONTINUE CHARGING/REPEAT

. . . . . . . . . . . . . . .ABOVE STEPS EVERY 90 SECSBattery Charge Annunciator . . . . . . . EXTINGUISHED WHEN. . . . . . . . . . . .LOADMETER DECREASE BELOW 2.5%

NI-CAD BATTERY CHECK (GROUND OPERATION ONLY)

CABIN DOOR CIRCUITRY (B200)

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Normal Procedures


The following checks should be completed in addition to the normalchecklist items during cold weather operations. Please refer to AFMSection 4 for complete procedures to be accomplished during cold

weather operation.

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . CHECK

Power Levers . . . . . . . . . . . . . . . . . . . . . . IDLEAuto Ignition . . . . . . . . . . . . . . . . . . . . . . ARM

L/R IGNITION ON annunciators illuminated.Power Levers . . . . . . ADVANCE ABOVE 360 460 FT-LBS

L/R IGNITION ON annunciators extinguished.Power Levers . . . . . . . . . . . . . . . . . . . . . . IDLE

L/R IGNITION ON annunciators illuminated.

Auto Ignition . . . . . . . . . . . . . . . . . . . . . . . OFFL/R IGNITION ON annunciators extinguished.Engine Anti-Ice . . . . . . . . . . . . . . . . . . . . . . CHECK

Engine Ice Vanes . . . . . . . . . . . . . . . . . . RETRACTL/R ICE VANE EXT annunciators extinguished.

Engine Ice Vanes . . . . . . . . . . . . . . . . . . . EXTENDL/R ICE VANE EXT annunciators illuminated.

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . CHECK

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . HIGHObserve increase on left and right loadmeters.

Windshield Anti-Ice . . . . . . . . . . . OFF/THEN NORMALObserve increase on left and right loadmeters.

Windshield Anti-Ice . . . . . . . . . . . . . . . . . . . OFFElectrothermal Propeller Deice . . . . . . . . . . . . . . CHECK

Automatic Prop Deice . . . . . . . . . . . . . . . . . AUTODeice Ammeter . . . . . . . . . . . . . . . . . . . . CHECK

Monitor for 90 seconds to ensure automatic timer operation.Manual Prop Deice Switch . . . HOLD IN MANUAL POSITION

Small deflection on both loadmeters indicates systemoperation. Deice ammeter should indicate zero amps.

Manual Prop Deice Switch . . . . . . . . . . . . . . RELEASEDeice Ammeter . . . . . . . . . . . . . . . . . . . . CHECK

Automatic Prop Deice . . . . . . . . . . . . . . . . . . OFF

CAUTION: Do not operate propeller deice when the propellers arestatic.

Continued on next page

BEFORE TAKEOFF (RUNUP) COLD WEATHER OPS

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PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Surface Deice System . . . . . . . . . . . . . . . . . . CHECKCondition Levers . . . . . . . . . . . . . . . . . . . HIGH IDLEPneumatic Pressure . . . . . . . . . . . . . . . . . . . CHECKSurface Deice Switch . . . . . . . . . . . . . . SINGLE/RELEASE

Pneumatic pressure decreases momentarily. Visually check forboot inflation then hold down. The wing boots inflate in six sec-

onds followed by the horizontal stabilizer boots in four seconds.Surface Deice Switch . . . . . . . . . . . . . . MANUAL/HOLD

Pneumatic pressure decreases momentarily. Visually check theboots for inflation.

Surface Deice Switch . . . . . . . . . . . . . . . . . . RELEASECondition Levers . . . . . . . . . . . . . . . . . . . LOW IDLE

WARNING: Do not cycle the boots during takeoff.

Stall Warning and Pitot Heat . . . . . . . . . . . . . . . CHECK

CAUTION: Prolonged use of stall warning and pitot heat on theground will damage the heating elements.


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King Air 200 Operating HandbookDeveloped for Training Jan 03 N21

PNF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PF

Auto-Ignition . . . . . . . . . . . . . . . . . . . . . . . . OFFIce Protection . . . . . . . . . . . . . . . . . . . AS REQUIREDFlaps . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Crew Briefing . . . . . . . . . . . . . . . . . . . . COMPLETEDRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Altitude Alerter . . . . . . . . . . . . . . . . . . . . . . . SET

Flight Director . . . . . . . . . . . . . . . . . . . . . . . . SETFlaps . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTrim . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDFinal Items:

Headings . . . . . . . . . . . . . . . . . . . . . . CHECKEDAuto-Ignition . . . . . . . . . . . . . . . . . . . . . ARMEDAutofeather . . . . . . . . . . . . . . . . . . . . . . ARMEDIce Protection . . . . . . . . . . . . . . . . . . AS REQUIRED

Ignition Lights . . . . . . . . . . . . . . . . . . . . . . . . OFFAutofeather Lights . . . . . . . . . . . . . . . . . . . . . . ONPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Engine Instruments . . . . . . . . . . . . . . . . . . CHECKED

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPLanding/Taxi Lights . . . . . . . . . . . . . . . . . . . . . OFF

Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . ONPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

CLIMB

TAKEOFF

BEFORE TAKEOFF

AFTER LANDING/TAXIBACK

LOCAL TRAINING


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Normal Procedures

King Air 200 Operating HandbookDeveloped for Training Jul 01N22

Crew Briefing . . . . . . . . . . . . . . . . . . . . COMPLETEDAltimeters . . . . . . . . . . . . . . . . . . . . SET/CHECKEDAutofeather . . . . . . . . . . . . . . . . . . . . . . . ARMEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . APPROACH

Landing Gear . . . . . . . . . . . . . . . . . DOWN/3 GREENLanding/Taxi Lights . . . . . . . . . . . . . . . . . . . . . ONFinal Items:

Flaps . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . OFFProp . . . . . . . . . . . . . . FORWARD AT TOUCHDOWN

BEFORE LANDING

APPROACH

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King Air 200 (late) Operating Handbook

Developed for Training Purposes Oct 07 N-1

Normal ProceduresCAE SimuFlite

The Following Weather Conditions May Be Conducive to Severe

In-Flight Icing:

Visible rain at temperatures below 0C ambient air temperature.Droplets that splash or splatter on impact at temperatures below 0Cambient air temperature.

Procedures for Exiting the Severe Icing Environment

These procedures are applicable to all flight phases from takeoff to

landing. Monitor the ambient air temperature. While severe icing may

form at temperatures as cold as -18C, increased vigilance is warranted

at temperatures around freezing with visible moisture present. If the

visual cues specified in the Limitations Section of the AFM for identify-ing severe icing conditions are observed, accomplish the following:

Immediately request priority handling from Air Traffic Control tofacilitate a route or an altitude change to exit the severe icing condi-tions in order to avoid extended exposure to flight conditions moresevere than those for which the airplane has been certificated.Avoid abrupt and excessive maneuvering that may exacerbate con-trol difficulties.

Do not engage the autopilot.If the autopilot is engaged, hold the control wheel firmly and disen-gage the autopilot.If an unusual roll response or un-commanded roll control movementis observed, reduce the angle-of-attack.Do not extend flaps when holding in icing conditions. Operation withflaps extended can result in a reduced wing angle-of-attack, with thepossibility of ice forming on the upper surface further aft on the wingthan normal, possibly aft of the protected area.

If the flaps are extended, do not retract them until the airframe isclear of ice.Report these weather conditions to Air Traffic Control.

ICING CONDITIONS

N-10/07


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Developed for Training Purposes Oct 07 N-3

Normal ProceduresCAE SimuFlite

PF . . . . . . . . Pilot Flying. The pilot responsible for controlling the aircraft.Performs tasks and responds to checklist challenges.

PM . . . . . . . . Pilot Monitoring. Reads checklist challenges. . . . . . . . . . Intermediate stop/fast turnaround.

PM PF

Passenger Briefing (see N-12) . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETECabin Door/Cargo Door Circuitry Check . . . . . . . . . . . . . . . . . . . COMPLETE

Cabin Door/Cargo Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED

Electric Toilet (if installed) . . . . . . . . . . . . . . . . . . . . . . . KNIFE VALVE OPEN

Load and Baggage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM SECURED

Weight and Center-of-Gravity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .POSITIONED

Emergency Exit . . . . . . . . . . . . . . . . . CONFIRM SECURE AND UNLOCKED

Control Locks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .REMOVED

Seats/Rudder Pedals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTED

Seat belts/Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED

Oxygen System Ready . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PULL ON

Oxygen System Preflight (page N-17) . . . . . . . . . . . . . . . . . . . . COMPLETED

Fuel Panel Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN

Pilots Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Compass Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SLAVED

EFIS Aux Power (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Test Switch. . . . . . . . . . . . . . . . . . . . . . . HOLD IN TEST FOR 5 SECONDS

Test Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE TO OFF

Prop Sync Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Pilots Clock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK/SET

Pilots Subpanel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Mic Selector Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM SETPilot Air Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Defrost Air Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Landing Gear Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DN

Landing Gear Relay Circuit Breaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN

All Other Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Avionics Panel Switches. . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Radar. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF OR STANDBY

Power Console. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDPower Levers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IDLE/FRICTION SET

Propeller Levers . . . . . . . . . . . . . . . . . . FULL FORWARD/FRICTION SET

Condition Levers. . . . . . . . . . . . . . . . . . . .FUEL CUT OFF/FRICTION SET




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N-4 Developed for Training Purposes Oct 07

Normal Procedures CAE SimuFlite

BEFORE STARTING ENGINES CONTINUED

PM PFElevator/Aileron/Rudder Trim. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Landing Gear Alternate Extension . . . . . . . . . . . . . . . . . . . . . . . STOWED

Oxygen System Ready . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM ON

Pedestal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

EFIS Power Switches (if installed). . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

EFIS Reversionary Switches (if installed). . . . . . . . . . . . . . . . . . NORMAL

Cabin Pressure Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PRESSRudder Boost Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Elevator Trim Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Pressurization Controller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Copilots Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Compass Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SLAVED

Copilots Clock (control wheel) . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK/SET

Copilots Subpanel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Cabin Sign . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NO SMOKE/FSBVent Blower Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO

Bleed Air Valve Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENVIR OFF

Cabin Temp Mode Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Cabin/Cockpit Air Control

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King Air B200 Operating Handbook 2010 CAE Simuflite

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