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BEECHCRAFT
KING AIR B200 POH
Super King Air B200/B200C · PT6A-42 · POH/AFM P/N 101-590010-147C
QUICK REFERENCE — 12,500 LBS
V1 / VR TO (Flaps UP)
95
KIAS Rotation
V2 / 50-ft (Flaps UP)
121
KIAS at 50 ft
VYSE (Blue Line)
121
KIAS best ROC OEI
VXSE
115
KIAS best angle OEI
VMCA
86
KIAS min ctrl air
VMO / MMO
260 / .52
KIAS / Mach
Vy (2-Engine)
125
KIAS best ROC
Emergency Descent
181
KIAS max
📋
LIMITATIONS
Airspeed · Engine · Fuel · Weight · Icing
🚨
EMERGENCY
Engine failure · Fire · Descent · Electrical
⚡
ABNORMAL
Smoke · Fuel low · Door unlocked
✅
NORMAL PROC
Preflight · Start · Taxi · TO · Landing
📊
CRUISE PERF
TAS · Fuel flow · Torque · Climb
🛫
DECOLAGEM
V1 · VR · V2 · Ground Roll · Total Dist
🛬
POUSO
Vapp · Vth · Distância · Com/Sem reverso
⚖️
WEIGHT & BAL
Peso · CG · ZFW · TOW · Envelope
📝
CONDENSED CHECKLIST · PROLINE 21
Checklist interativo completo · Preflight → Shutdown · V-speeds · Para usar em voo
⚠️ FOR TRAINING PURPOSES ONLY This reference is derived from the Beechcraft Super King Air B200/B200C POH/AFM P/N 101-590010-147C. Not for operational use. Always refer to the current AFM for actual flight operations.

⚠️ Section II — Limitations

FAA Approved · Must be observed in all operations
Airspeed Limitations
VMO — Max Operating Speed260 KIAS / 259 KCAS
MMO — Max MachM 0.52
VA — Maneuvering Speed (12,500 lb)181 KIAS
VFE — Flaps Approach (40%)200 KIAS
VFE — Flaps Full Down (100%)157 KIAS
VLO — Gear Extension / Retraction181 KIAS
VLE — Max Gear Extended181 KIAS
VMCA — Air Min Control Speed86 KIAS
Do not make full or abrupt control movements above VA. Do not lift power levers in flight.
Powerplant Limitations — PT6A-42
Engines2 × Pratt & Whitney PT6A-42
Max Torque (T/O & Max Cont)2,230 ft-lbs
ITT — Takeoff & Max Continuous800°C
ITT — Transient (max 5 sec)850°C
ITT — Starting (max)1,000°C
N1 — Max Gas Generator RPM101.5%
Propeller RPM — Max2,000 RPM
Propeller RPM — Normal Cruise1,700 RPM
CONDITIONTORQUE (ft-lb)ITT (°C)N1 (%)
Starting—1,000 max—
Low Idle———
High Idle———
Takeoff / Max Continuous2,230800101.5
Max Reverse850800—
Transient (5 sec max)2,230850—
Starter Limits40s ON / 60s OFF / 40s ON / 60s OFF / 40s ON — then 30 min OFF
Weight Limitations
Maximum Takeoff Weight12,500 lb
Maximum Ramp Weight12,590 lb
Maximum Landing Weight12,500 lb
Maximum Zero Fuel Weight10,430 lb
Minimum Flight Crew1 Pilot
Maximum Occupancy (incl. crew)15
Altitude & Pressure Limits
Max Operating Pressure Altitude35,000 ft
Max Altitude — Yaw Damp Inoperative17,000 ft
Max Cabin Pressure Differential6.6 psi
Max Outside Air Temp (SL–25,000 ft)ISA + 37°C
Max Outside Air Temp (above 25,000 ft)ISA + 31°C
Fuel Limitations
Approved — CommercialJet A, Jet A-1, Jet B
Approved — MilitaryJP-4, JP-5, JP-8
Emergency (AvGas)100LL, 100/130, 115/145, 80
Max Fuel Imbalance200 lb
Emergency AvGas: Limited to 150 hrs between overhauls. Max FL 200 if standby pump inoperative. Avgas prohibited above FL 310.
Icing Limitations
Min Ambient Temp for Deice Boots−40°C
Min Airspeed — Sustained Icing140 KIAS
Ice Vanes EXTEND — at or below+5°C (visible moisture)
Ice Vanes RETRACT — above+15°C all ops
⚠️ WARNINGSustained flight in icing conditions with flaps extended is PROHIBITED except for approach and landing.
Systems & Equipment Limits
Landing Gear Cycle Limit6 cycles, then 15 min cool-down
Min interval per cycle5 minutes
Aft-facing seats: seatback must be fully raised for takeoff and landing.

🚨 Section III — Emergency Procedures

Bold items = immediate action · All airspeeds are IAS
EMERGENCY AIRSPEEDS (12,500 LB): VXSE = 115 kts · VYSE = 121 kts · VMCA = 86 kts · Emergency Descent = 181 kts max · Max Range Glide = 135 kts
⚠️APPLIES TO: Engine torque increase unscheduled · Engine fire in flight · Engine failure in flight
Condition Lever — AFFECTED ENGINE
FUEL CUT OFF
Propeller Lever
FEATHER
Firewall Shutoff Valve
CLOSED
Fire Extinguisher (if installed)
ACTUATE
Auto Ignition
OFF
Generator
OFF
Prop Sync
OFF
Electrical Load
MONITOR
⚠️If conditions preclude immediate landing. Bank 3°–5° into operating engine.
Power
MAX ALLOWABLE
Airspeed
Maintain takeoff speed or above
MAINTAIN
Landing Gear
UP
Propeller Lever (inop engine)
Verify FEATHER if autofeather installed
FEATHER
Airspeed — after obstacle clearance
VYSE 121 KT
Flaps
UP
Condition Lever (inop engine)
FUEL CUT OFF
Propeller Lever (inop engine)
FEATHER
Firewall Shutoff Valve
CLOSED
Auto Ignition / Autofeather
OFF
Generator (inop engine)
OFF
Electrical Load
MONITOR
Condition Lever
FUEL CUT OFF
Firewall Shutoff Valve
CLOSED
Ignition and Engine Start
STARTER ONLY
Fire Extinguisher (if installed)
ACTUATE
Power Levers
IDLE
Brakes
AS REQUIRED
Operative Engine
MAX REVERSE
⚠️If insufficient runway for stopping:
Condition Levers
FUEL CUT OFF
Firewall Shutoff Valves
CLOSED
Master Switch (gang bar down)
OFF
Oxygen — Crew required, passengers as required
Pull ON · DON masks · Mic selector OXYGEN MASK · Pull passenger lanyard
ON / DON
Power Levers
IDLE
Propeller Levers
FULL FORWARD
Flaps
APPROACH
Landing Gear
DOWN
Airspeed
181 KT MAX
Oxygen — PULL ON · DON Masks 100% · Mic → OXYGEN MASK
ON / DON
Cabin Temp Mode
OFF
Vent Blower
AUTO
Aft Blower
OFF
Avionics Master
OFF
Non-essential Electrical Equipment
OFF
⚠️If smoke persists or fire not confirmed extinguished: DUMP cabin pressure · Land nearest suitable airport immediately.
Landing Gear
UP
Flaps
UP
Propellers — after restart attempts exhausted
FEATHER
Airspeed
135 KIAS
Glide ratio: 2.0 nm per 1,000 ft altitude. Decrease 0.2 nm per 10 kts headwind.
Power
Reduce as required to maintain directional control
REDUCE
Nose
Lower to accelerate above VMCA
LOWER
Power (operative engine)
AS REQUIRED
Failed Engine
SECURE

⚡ Section IIIA — Abnormal Procedures

Non-emergency malfunctions requiring pilot action
Standby Pump (failed side)
ON
FUEL PRESS Annunciator
EXTINGUISHED?
Select other inverter
SELECT OTHER
⚠️Do NOT check door security in flight. Remain as far from door as possible. Seatbelts securely fastened.
All Occupants — seated, seatbelts securely fastened
SEATED
Cabin Sign
NO SMOKE & FSB
Cabin Differential Pressure
Descend and/or select higher cabin altitude — reduce to lowest practical (zero preferred)
REDUCE
Oxygen
AS REQUIRED
Land at nearest suitable airport
DIVERT
Oxygen — PULL ON · DON Masks · Mic → OXYGEN MASK
ON / DON
Cabin Temp Mode
OFF
Vent Blower
HIGH
Left Bleed Air Valve
ENVIR OFF
If smoke decreases — continue with L bleed off
If smoke does NOT decrease: open L, close R bleed air valve
MONITOR
Airplane Attitude — maintain using elevator control
MAINTAIN
Control Wheel Disconnect Switch
Depress fully (2nd level) — ELEC TRIM OFF annunciator illuminates
DEPRESS

✅ Section IV — Normal Procedures

• Items may be omitted at pilot's discretion after first flight of the day
Condition Levers
FUEL CUT OFF
Landing Gear Control
DN
Control Locks
REMOVE
Parking Brake
SET
Ignition and Engine Start
ENSURE OFF
Battery — ON, check minimum 23V
ON / CHECK
Fuel Quantity
CHECK
Flap Control (if desired)
APPR → DOWN
Oxygen System Preflight Inspection
COMPLETE
Walk-around (per POH flow)
Engine oil · Props · Fuel caps · Gear · Boots · Lights · Static wicks
COMPLETE
Battery
OFF
Cabin Door — locked and checked
LOCKED
Load and Baggage
SECURE
Weight and CG
CHECKED
Seats — positioned, seatbacks upright
POSITIONED
Emergency Exit
SECURE & UNLOCKED
Passenger Briefing
COMPLETE
Control Locks
REMOVED
Seatbelts and Shoulder Harnesses
FASTENED
Oxygen System Ready
PULL ON
Fuel Panel Circuit Breakers
IN
Engine Ice Vane Switches
EXTEND
Power Levers — IDLE, Friction set
IDLE
Propeller Levers — FULL FORWARD, Friction set
FULL FWD
Condition Levers — FUEL CUT OFF, Friction set
FUEL CUT OFF
Trim Controls — set for TO
SET
Battery — ON
ON
Firewall Shutoff Valves
OPEN
Annunciators
TEST
Beacon
ON
Fuel Quantity
CHECK
RIGHT Ignition and Engine Start
R FUEL PRESS annunciator extinguishes
ON
Right Condition Lever — at 12% N1 or above
LOW IDLE
ITT and N1
No ITT rise in 10 sec → CUT OFF. Wait 60 sec then ENGINE CLEARING.
MONITOR 1000°C
Right Oil Pressure
CHECK
Right Condition Lever
HIGH IDLE
Right Ignition and Engine Start — at 50% N1 or above
OFF
Right Generator — RESET (hold 1 sec) then ON
Charge battery until loadmeter reads ~50% or less
RESET → ON
Right Generator (after battery charged)
OFF
LEFT Ignition and Engine Start
L FUEL PRESS annunciator extinguishes
ON
Left Condition Lever (as L N1 thru 12%) + Right Generator ON
LOW IDLE / ON
ITT and N1
MONITOR 1000°C
Left Oil Pressure
CHECK
Left Ignition and Engine Start — at 50% N1
OFF
DC Volt/Loadmeters
Should read 27.5–29.0 volts
CHECK 27.5–29V
Left Generator — RESET (hold 1 sec) then ON
RESET → ON
Inverters — check volts/freq (105–120V / 380–420 Hz)
CHECK
Loadmeters — parallel within 10%
CHECK
Avionics Master
ON
External Lights
AS REQUIRED
Cabin Temp Mode
AUTO
Flight Controls — freedom and proper direction
CHECK
Flaps — check and set
CHECK / SET
Brakes
RELEASED & CHECKED
Propeller Levers — test and exercise
CHECK
Autofeather (if installed)
ARM / TEST
Engine Power — check at high power
CHECK
Bleed Air — both sides open, check pressurization
OPEN / CHECK
Engine Ice Vanes
CHECK
Fuel Quantity, Flight and Engine Instruments
CHECK
Propeller Levers
FULL FORWARD
Flaps
CONFIRM SET
Trim
CONFIRM SET
Left and Right Bleed Air
OPEN
Annunciators
EXTINGUISHED
Ice Protection (if required)
Auto Ignition ON · Ice Vanes extended · Windshield Anti-ice NORMAL/HI · Prop Heat AUTO · Pitot Heat ON
ON IF REQD
External Lights
AS REQUIRED
Transponder
ON
V1, VR, V2 and Min Takeoff Power
CONFIRM
Brakes
HOLD
Power — set, ensure minimum takeoff power available
SET
Autofeather Annunciators (if installed)
ILLUMINATED
Brakes
RELEASED
Landing Gear — when positive climb established
UP
Flaps — at blue line (121 kts min)
UP
Yaw Damp
ON
Climb Power
SET
Propellers
1,900 RPM
Prop Sync (if installed)
ON
Autofeather (if installed)
OFF
Engine Instruments
MONITOR
Pressurization
CHECK
⚠️Do NOT lift power levers in flight.
Cruise Power — per cruise power tables/graphs
SET
Engine Instruments
MONITOR
Auxiliary Fuel Gages — ensure transfer from aux tanks
MONITOR
Pressurization — reset if altitude changes by 1,000 ft+
MONITOR
Pressurization — set cabin alt selector for landing altitude + 500 ft
SET
Altimeter
SET
Windshield Anti-ice (if required)
NORMAL or HI well before descent into warm moist air to aid defogging
AS REQUIRED
Autofeather (if installed)
ARM
Fuel Balance
CHECK
Power
~75% N1 required to maintain pressurization schedule
AS REQUIRED
⚠️Avoid propeller RPM range of 1,750–1,850 RPM — may cause ILS interference.
Approach Speed
CONFIRM
Pressurization
CHECK
Cabin Sign
NO SMOKE & FSB
Flaps
APPROACH
Landing Gear
DN / 3 GREEN
Lights
AS REQUIRED
Prop Sync (Type I)
OFF
Radar
AS REQUIRED
Flaps
DOWN
Airspeed
NORMAL APPR SPD
Yaw Damp
OFF
Power Levers
IDLE
Propeller Levers
FULL FORWARD
After Touchdown — Power Levers
BETA / REVERSE
Brakes
AS REQUIRED
Auto Ignition
OFF
Engine Ice Vanes
EXTEND
Ice Protection
OFF
Transponder
STANDBY
Radar
STANDBY / OFF
Trim Tabs
SET
Flaps
UP
Parking Brake
SET
Standby Boost Pumps and Crossfeed
OFF
Avionics Master
OFF
Inverter
OFF
Autofeather (if installed)
OFF
Lights
OFF
Cabin Temp Mode
OFF
Condition Levers
FUEL CUT OFF
Propeller Levers
FEATHER
Battery
OFF

📊 Performance Calculator

POH Section V · 1700 RPM · Data based on 11,000 lb unless noted
V-Speeds Reference (12,500 lb)
VR — Flaps UP
95
KIAS rotation
V2 / 50-ft — Flaps UP
121
KIAS at 50 ft
VR — Flaps APPR
94
KIAS rotation
50-ft — Flaps APPR
106
KIAS at 50 ft
VYSE — Blue Line
121
KIAS best ROC OEI
VXSE
115
KIAS best angle OEI
Vy (2-engine)
125
KIAS best ROC
Cruise Climb
160
KIAS typical
V-speeds vary slightly with weight. Climb speeds: 125/124/121/118/115 kts at 12500/12000/11000/10000/9000 lb. Approach flaps climb: 115–103 kts decreasing with weight.
Cruise Performance Calculator
Normal Cruise 1700 RPM · POH Tables pp.5-46 to 5-55 · ISA day
Time · Fuel · Distance to Climb
From Sea Level · 1900 RPM · Max Continuous Power · Gear Up · ISA · 12,500 lb takeoff weight

⚖️ Weight & Balance

POH Section VI · CG in inches aft of datum (F.S.)
Enter values for your aircraft. BEW and moment from your W&B form at delivery. Fuel at 6.7 lb/gal. Arm approximations from POH — verify with aircraft W&B form.
AIRCRAFT
CREW & PASSENGERS (F.S. stations)
BAGGAGE
FUEL (6.7 lb/gal · arm approx. F.S. 177 main / F.S. 243 aux)
⚠️ Aux tanks may be used ONLY when main tanks are completely filled (POH)
CG Envelope Reference (gear down)
12,500 lb — Forward CGF.S. 185.0
12,500 lb — Aft CGF.S. 196.4
≤ 11,279 lb — Forward CGF.S. 181.0
≤ 11,279 lb — Aft CGF.S. 196.4
Max Zero Fuel Weight11,000 lb
Max Takeoff Weight12,500 lb

🛫 Decolagem

POH Sec. V — Dados de V-speeds: exatos do POH · Distâncias: aproximadas dos gráficos POH
⚠️ AVISO DE DADOS V1/VR/V2: exatos do POH (tabelas embutidas nos gráficos Sec. V). Distâncias: modelo paramétrico ancorado nos exemplos do POH (OAT=28°C, PA=5.433ft, 12.500lb, HW=9,5kt). Devem ser verificadas no gráfico do POH antes do voo operacional. Para operações FAR 135/91, use somente os gráficos oficiais do POH.
V-Speeds de Referência — Exatos do POH Sec. V
FLAPS UP (0%)
WT (lb)VRV2VYSE
12,50095121121
12,00095119119
11,50095117118
11,00095115117
10,50095113116
10,00095111114
9,50095110113
9,00095108111
FLAPS APPROACH (40%)
WT (lb)VRV2VYSE
12,50094106121
12,00094105119
11,50094104118
11,00094103117
10,50094102116
10,00094101114
9,50094100113
9,0009499111
V2 Flaps UP = também é VYSE para este peso. Flaps APPROACH: VYSE = blue line (varia com peso, independente de flap).

🛬 Pouso

POH Sec. V pp.5-120 a 5-123 — Gráficos de distância de pouso
⚠️ AVISO DE DADOS Velocidades de aproximação: exatas do POH (VYSE+10, Flaps UP/DOWN). Distâncias: modelo paramétrico baseado nos gráficos POH. Verificar no gráfico oficial para operações.
Velocidades de Aproximação e Threshold — Exatas do POH
WT (lb) VAPP
VYSE+10 · F0/40		 Vth F100%
Threshold		 Vth F0%
Flaps UP
12,500131103131
12,000129102129
11,500128101127
11,00012799125
10,50012698123
10,00012496121
9,50012395120
9,00012193118
VAPP = VYSE + 10 · Pista paved, dry, level · Braking máximo · Obstáculo 50 ft