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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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King Air 200 Operating Handbook
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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King Air 200 Operating Handbook
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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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Preflight Procedures CAE SimuFlite
continued from previous page
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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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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King Air 200 (early) Operating HandbookDeveloped for Training Mar 2001 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-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
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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
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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
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King Air 200 (early) Operating HandbookDeveloped for Training Mar 01 N7
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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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
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King Air 200 (early) Operating HandbookDeveloped for Training Mar 01 N9
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
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King Air 200 (early) Operating HandbookDeveloped for Training Mar 01 N11
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
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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).
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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
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King Air 200 (early) 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 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
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King Air 200 (early) Operating HandbookDeveloped for Training Mar 01N16
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
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Normal Procedures
King Air 200 (early) Operating HandbookDeveloped for Training Mar 01 N17
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
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BEFORE TAKEOFF (RUNUP) COLD WEATHER OPS
NI-CAD BATTERY CHECK (GROUND OPERATION ONLY)
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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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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
continued on next page
BEFORE STARTING ENGINES
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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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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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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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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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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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CAE SimuFliteNormal Procedures
King Air 200 (mid) Operating HandbookDeveloped for Training Jul 01N12
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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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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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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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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King Air 200 (mid) Operating HandbookDeveloped for Training Jul 01 N19
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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King Air 200 (mid) Operating HandbookDeveloped for Training Mar 01N20
continued from previous page
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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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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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
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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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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
continued on next page
BEFORE STARTING ENGINES
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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