KING AIR 200 Flashcards
Emergency Engine Shutdown
1 Condition Lever……….Fuel Cutoff
2 Prop Lever………………Feather
- Firewall Shutoff ……..Close
- Fire Extinguisher…….Actuate
Extinguisher if installed and if fire warning persists.
Engine Fire on the Ground
1 Condition Lever…………….Fuel Cutoff
2 Firewall Shutoff …………..Close
- Ignition / Engine Start….Starter Only
If Fire warning persists…
- Fire Extinguisher…….Actuate
Extinguisher if installed
Emergency Engine Shutdown
on the Ground
1 Condition Lever……….Fuel Cutoff
2 Prop Lever………………Feather
- Firewall Shutoff ……..Close
- Master Switch GB…..Off
- ESIS Power…………….Off
Engine Failure During Takeoff
At or Below V1 Takeoff Aborted
- Power Levers………………Ground Fine
- Brakes……….As required to achieve stopping distance
- Operative Engine………..Max Reverse
Engine Failure During Takeoff
At or Above V1
Takeoff Continued
- Power……………..Max allowable
- Airspeed…………Maintain Take off Speed or above
- Landing Gear when pos climb established….UP
- Prop Inop engine…………verify feather
- Airspeed after obstacle clearance…..Vyse
Engine Failure in Flight Below
Air minimumControl Speed (VMCA)
- Power…………..Reduce as required to maintain control
- Nose…………….Lover to accelerate above VMCA
Engine Flameout
(Second Engine)
- Power Lever ………………….IDLE
- Prop Lever ……………………DO NOT FEATHER
- Condition Lever ……………FUEL CUTOFF
- Conduct Air Start Procedure in ABNORMAL PROCEDURES.
Fuel Pressure Low
L Fuel Pressure or R Fuel Pressure

Standby Pump ( Failed Side) ……………ON
SMOKE and FUME Elimination
ELECTRICAL SMOKE OR FIRE
SMOKE and FUME Elimination
ELECTRICAL SMOKE OR FIRE
- Oxygen Masks…………………..DON
- Mask Selector Switch ……….EMER POSITION
- MIC Switch(es) ………………… OXY
ENVIRONMENTAL SYSTEM
SMOKE OR FUMES
ENVIRONMENTAL SYSTEM
SMOKE OR FUMES
- Oxygen Masks…………………DON
- Mask Selector Switch ……..EMER POSITION
- MIC Switch(es) ………………..OXY
AIRSTAIR DOOR/CARGO DOOR
UNLOCKED

AIRSTAIR DOOR/CARGO DOOR
UNLOCKED
If the [DOOR UNLOCKED] Illuminates, or if an Unlatched Airstair Door/Cargo Door is Suspected:
All Occupants …….
SEATED WITH SEAT BELTS SECURELY FASTENED
EMERGENCY DESCENT
EMERGENCY DESCENT
- Power Levers …………. IDLE
- Prop Levers …………. FULL FORWARD
- Flaps (200 knots maximum). APPROACH
- Landing Gear (181 knots .. DN
- Airspeed …………….. 181 KNOTS MAXIMUM
GLIDE
GLIDE
- Landing Gear ………… UP
- Flaps ………………. UP
- Propellers ………….. FEATHERED
- Airspeed ……………. 135 KNOTS
DUAL GEN FAILURE
L DC GEN R DC GEN

DUAL GEN FAILURE
L DC GEN R DC GEN
Generators ………….. RESET, THEN ON
USE OF OXYGEN
USE OF OXYGEN
- Oxygen Mask(s) ……..DON
- MIC Switch(es) ……. OXY
PRESSURIZATION LOSS
ALT WARN

PRESSURIZATION LOSS
ALT WARN
- Oxygen Mask(s) ……….DON
- MIC Switch(es) ……… OXY
- Passenger Manual Drop-Out .PULL ON [PASS OXY ON] – ILLUMINATED
- Descend ……………. AS REQUIRED
HIGH DIFFERENTIAL PRESSURE
HIGH DIFFERENTIAL PRESSURE
If Cabin Differential Pressure exceeds 6.6 PSI:
- Bleed Air Valves …………. ENVIR OFF
- Oxygen (Crew and Passengers) ..AS REQUIRED
- Descend …………………. AS REQUIRED
AUTO DEPLOYMENT
OXYGEN SYSTEM FAILURE

- Passenger Manual Dropout…..Pull On
BLEED AIR FAIL

- Bleed Air Valve effected Engin
INST & ENVIR OFF
SPINS
Intentional spins are prohibited. If an unintentional spin is encountered, perform the following procedure IMMEDIATELY–THE LONGER THE DELAY, THE MORE DIFFICULT RECOVERY WILL BECOME. Steps 1 through 3 should be done AGGRESSIVELY and SIMULTANEOUSLY.
The full forward position of the control column may be reduced slightly, if required, to prevent the airplane from exceeding a 90° nose down (inverted) attitude.
- Control Column ……..full forward Airerons Neutral
- Full Rudder……………..opposite direction of spin
- Power Levers………….idle
- Rudder…………………….Neutalize when spin stops
- Execute smooth pullout
UNSCHEDULED ELECTRIC ELEVATOR
TRIP ACTIVATION
- Airplane Attitude………………………Maintain using elevator control
- A/P/Trim Disconnect………………..Depress fully and hold
UNSCHEDULED RUDDER BOOST ACTIVATION
- Directional Control ………Maintain using Rudder Pedals
- Rudder Boost………………..OFF
- IF Condition Persists
- Rudder Boost Circuit Breaker……Pull
AUTOPILOT MISTRIM ANNUNCIATION
- Flight Controls…………………..HOLD FIRMLY
- A/P………………………………………Disengage
AUTOPILOT TRIM FAIL ANNUNCIATION
- Flight Controls………………HOLD FIRMLY
- A/P………………………………….Disengage
ENHANCED GROUND PROXIMITY
WARNING SYSTEM (EGPWS)
GPWS WARNING (RED [PULL UP] ON PFD AND CONTINUOUS “PULL UP, PULL UP” VOICE WARNING) EGPWS TERRAIN WARNING (RED [PULL UP] ON PFD AND “TERRAIN, TERRAIN, PULL UP” OR “OBSTACLE, OBSTACLE, PULL UP” VOICE WARNING)
In IMC or at Night:
- Wings …………………….. LEVEL
- Power …………………… MAX ALLOWABLE
- Pitch ……………………….INCREASE
- Promptly and smoothly increase pitch towards an initial pitch attitude of 20°–25°.
- Adjust as required to avoid continuous buffeting and/or stall warning.
- Adjust to maintain 100 KIAS.
- Gear and Flaps …………….. UP
Engine Oil Limitations
Oil Temp for Starting ……………….. ?°C (Min)
Oil Press for Idle RPM ………………. ? PSI (Min)
Oil Press Maximum Transient …….? PSI
Engine Oil Limitations
Oil Temp for Starting ……………….. –40°C (Min)
Oil Press for Idle RPM ………………. 60 PSI (Min)
Oil Press Maximum Transient ………….. 200 PSI
ENGINE LIMITS
Oil (°C/PSI)
Oil Temp Takeoff & Max Continuous Thrust ……….?° C
Oil Press Takeoff & Max Continuous Thrust ….. ? PSI
(?° C Recommended)
ENGINE LIMITS
Oil (°C/PSI)
Oil Temp Takeoff & Max Continuous Thrust ……….. 0—99° C
(55° C Recommended)
Oil Press Takeoff & Max Continuous Thrust ….. 100 - 135 PSI
PROPELLER LIMITS
Idle ……………………. ? RPM
Takeoff & Max Continuous ….. ? RPM
Transient ……………….. ? RPM
PROPELLER LIMITS
Idle ……………………. 1180 RPM
Takeoff & Max Continuous ….. 2000 RPM
Transient ……………….. 2200 RPM
EXTERNAL POWER LIMITS
Volts ……………….. ?
Amps ………………… ? (Momentarily) ? (Continuous)
EXTERNAL POWER LIMITS
Volts ……………….. 28.0 – 28.4
Amps ………………… 1000 (Momentarily) 300 (Continuous)
Maximum sustained generator
load is limited as follows:
In-Flight:
Sea Level to 31,000 Feet Altitude ……….. ?%
Above 31,000 Feet Altitude ………………. ?%
Ground Operation ……………………….. ?%
Maximum sustained generator
load is limited as follows:
In-Flight:
Sea Level to 31,000 Feet Altitude ……….. 100%
Above 31,000 Feet Altitude ………………. 88%
Ground Operation ……………………….. 85%
Starter Limitations
Duration On/Off ?
Starter Limitations
Duration On/Off …………..
40 seconds ON, 60 seconds OFF
40 seconds ON, 60 seconds OFF
40 seconds ON, 30 minutes OFF
FUEL LIMITS
Approved Engine Fuels
Commercial Grades Military Grades
FUEL LIMITS
Approved Engine Fuels
Commercial Grades Military Grades
- Jet A • Jet A-1 • Jet B
- JP-4 • JP-5 • JP-8
- Chinese Jet Fuel No. 3
FUEL LIMITS
Emergency Engine Fuels …………. 80 Red (Formerly 80/87)
100 Green (Formerly 100/130) 100LL Blue (100L Green) 91/96 115/145 Purple
FUEL LIMITS
Emergency Engine Fuels …………. 80 Red (Formerly 80/87)
100 Green (Formerly 100/130) 100LL Blue (100L Green) 91/96 115/145 Purple
FUEL LIMITS
Emergency Engine Fuels - Limitations on the Use of Aviation Gasoline:
- Operation is limited to ? hours between engine overhauls.
- Operation is limited to ? feet pressure altitude or below if either standby pump is inoperative.
- Crossfeed capability is required for climbs above ? feet pressure
- Operation above ? feet is prohibited.
FUEL LIMITS
Emergency Engine Fuels - Limitations on the Use of Aviation Gasoline:
- Operation is limited to 150 hours between engine overhauls.
- Operation is limited to 20,000 feet pressure altitude (FL 200) or below if either standby pump is inoperative.
- Crossfeed capability is required for climbs above 20,000 feet pressure
- Operation above 31,000 feet (FL 310) is prohibited.
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.7 = Pounds)
Total Usable Fuel Quantity …….. ? gallons (? lb)
- Each Main Fuel Tank System ..? gallons (? lb)
- Each Auxiliary Fuel Tank ………..? gallons (? lb)
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.7 = Pounds)
Total Usable Fuel Quantity …….. 544 gallons (3,645 lb)
- Each Main Fuel Tank System ..193 gallons (1,293 lb)
- Each Auxiliary Fuel Tank ………..79 gallons (529 lb)
FUEL MANAGEMENT
Maximum Imbalance ……….. ? LB
Fuel Crossfeed …… Permitted only ?
FUEL MANAGEMENT
Maximum Imbalance ……….. 1000 LB
Fuel Crossfeed …… Permitted only when one engine is inoperative.
FUEL MANAGEMENT
Takeoff is not allowed with:
Indication ……………. ?
Amount of Fuel ………… LESS THAN ? LB
in each main tank system
FUEL MANAGEMENT
Takeoff is not allowed with:
Indication ……………. IN THE YELLOW ARC
Amount of Fuel ………… **LESS THAN 265 LB **
in each main tank system
AUTOPILOT FAILURES
AUTOPILOT AUTOMATIC DISENGAGEMENT
- Maintain Airplane Control.
- AP/TRIM Disconnect ………..DEPRESS TO 1ST LEVEL TO CANCEL HORN
AIRSPEED LIMITATIONS
Maneuvering Speed (VA)
(KIAS at 12,500 lb)
181 Kts
Maximum Flaps Speeds (VFE)
(KIAS at 12,500 lb)
VFE/VFO Approach—40% (White “APP” Arrow) …….?
VFE/VFO Full Down—100% (White “DN” Arrow) ……?
VFE/VFO (Approach) ………….200 KIAS
VFE/VFO (Full Down) …………157 KIAS
AIRSPEED LIMITATIONS
Maximum Landing Gear Speeds (VLO/VLE)
(KIAS at 12,500 lb)
VLO (Extension) ……………?
VLO (Retraction) …………..?
VLE ………………………?
AIRSPEED LIMITATIONS
Maximum Landing Gear Speeds (VLO/VLE)
(KIAS at 12,500 lb)
VLO (Extension) ……………181 KIAS
VLO (Retraction) …………..163 KIAS
VLE ………………………181 KIAS
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
(Red Line)
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
(Red Line)
86 KIAS
AIRSPEED LIMITATIONS
Maximum Operating Speeds
VMO …………….. ?
MMO …………….. ?
AIRSPEED LIMITATIONS
Maximum Operating Speeds
VMO …………….. 259 KIAS
MMO …………….. Mach .52
AIRSPEED LIMITATIONS
Top of Low Speed Cue (LSC)
VS0 (Max weight with flaps down and idle power) ……. ?
VS1 (Max weight with flaps approach and idle power) … ?
VS1 (Max weight with flaps up and idle power) ……… ?
AIRSPEED LIMITATIONS
Top of Low Speed Cue (LSC)
VS0 (Max weight with flaps down and idle power) …..75 KIAS
VS1 (Max weight with flaps approach and idle power) 85 KIAS
VS1 (Max weight with flaps up and idle power) ……… 99 KIAS
EMERGENCY AIRSPEEDS
VXSE (One-Engine-Inoperative Best Angle-of-Climb)
?
VYSE (One-Engine-Inoperative Best Rate-of-Climb)(Blue Line)
?
One-Engine-Inoperative Enroute Climb
?
EMERGENCY AIRSPEEDS
VXSE (One-Engine-Inoperative Best Angle-of-Climb)
VXSE ** 115 KIAS**
VYSE (One-Engine-Inoperative Best Rate-of-Climb)(Blue Line)
VYSE ** 121 KIAS**
One-Engine-Inoperative Enroute Climb
121 KIAS
EMERGENCY AIRSPEEDS
Emergency Descent ………………?
Maximum Range Glide …………….?
EMERGENCY AIRSPEEDS
Emergency Descent ………………181 KIAS
Maximum Range Glide …………….135 KIAS
POWER LEVERS
Do not lift power levers in flight. Lifting the power levers in flight, or moving the power levers in flight below the flight idle position, could result in a nose-down pitch and a descent rate leading to aircraft damage or injury to personnel.
ENGINE LIMITS
Torque — Takeoff, Max Continuous ……?
Torque — Transient ………………..?
ENGINE LIMITS
Torque — Takeoff, Max Continuous ……2230 FT Lbs
Torque — Transient ………………..2750 FT lbs
ENGINE LIMITS
N1 — Takeoff, Max Continuous ………?
N1 — Transient …………………..?
ENGINE LIMITS
N1 — Takeoff, Max Continuous ………101.5 %
N1 — Transient …………………..102.6 %
ENGINE LIMITS
ITT Temp (°C)
Start ……………………….. ?
Takeoff / Max Continuous ………. ?
Cruise Climb / Normal Cruise …… ?
Transient ……………………. ?
ENGINE LIMITS
ITT Temp (°C)
Start ……………………….. 1000°C
Takeoff / Max Continuous ………. 800°C
Cruise Climb / Normal Cruise …… 770°C
Transient ……………………. 850°C
FUEL LIMITS
Approved Engine Fuels
FUEL LIMITS
Approved Engine Fuels
Commercial Grades Military Grades
Jet A • Jet A-1
JP-4 JP-5 Jet B JP-8
Chinese Jet Fuel No. 3
AUXILIARY FUEL
AUXILIARY FUEL
Do not put any fuel into the auxiliary tanks
unless the main tanks are full.
OPERATING WITH LOW FUEL PRESSURE
OR
Time until overhauling or replacement of the affected engine driven fuel pump …………………………………………………………………. ?
OPERATING WITH LOW FUEL PRESSURE
OR
Time until overhauling or replacement of the affected engine driven fuel pump ………………………….10 Hours
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 5 seconds …………?
Reverse …………………………………?
All other conditions ……………………..?
Minimum idle speed ……………………….?
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 5 seconds ………..2200 rpm
Reverse …………………………………1900 rpm
All other conditions ……………………..2000 rpm
Minimum idle speed ……………………….1180 rpm
PROPELLER ROTATIONAL OVERSPEED LIMITS
Sustained above 2000 RPM
(Primary Governor Failure):
Torque Limit ……………………….. ?
Sustained above 2120 RPM (Not Approved)
(Primary Governor & Overspeed Governor Failure):
Maximum Overspeed …………………….?
Time Limit ……………………………………….?
PROPELLER ROTATIONAL OVERSPEED LIMITS
Sustained above 2000 RPM
(Primary Governor Failure):
Torque Limit ……………………….. 1800 ft lbs
Sustained above 2120 RPM (Not Approved)
(Primary Governor & Overspeed Governor Failure):
Maximum Overspeed …………………….2200 rpms
Time Limit ……………………………………….5 seconds
PROPELLER AUTOFEATHER
PROPELLER AUTOFEATHER
The propeller autofeather system must be operable for
all flights and must be armed for takeoff, climb, approach
and landing.
WEIGHT LIMITS
Maximum Ramp Weight ……………………..?
Maximum Takeoff Weight:
All Except 14 CFR Part 135 Operations ……..?
Maximum Landing Weight …………………..?
Maximum Zero Fuel Weight …………………?
WEIGHT LIMITS
Maximum Ramp Weight ……………………..12,590 lbs
Maximum Takeoff Weight:
All Except 14 CFR Part 135 Operations ……..12,500 lbs
Maximum Landing Weight …………………..12,500 lbs
Maximum Zero Fuel Weight …………………11,000 lbs
WEIGHT LIMITS
Maximum Weight in Baggage Compartment:
When Equipped With Fold-Up Seats …………. ?
When Not Equipped With Fold-Up Seats ……… ?
WEIGHT LIMITS
Maximum Weight in Baggage Compartment:
When Equipped With Fold-Up Seats …………. 510 lbs
When Not Equipped With Fold-Up Seats ……… 550 lbs
MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS
Normal Operation ………………………. ?
Operation with Yaw Damp System Inoperative .. ?
MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS
Normal Operation ………………………. 35,000 ft
Operation with Yaw Damp System Inoperative .. 17,000 ft
MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS
Sea Level to 25,000 Feet Pressure Altitude …..?
Above 25,000 Feet Pressure Altitude …………?
MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS
Sea Level to 25,000 Feet Pressure Altitude …..ISA + 37°C
Above 25,000 Feet Pressure Altitude …………ISA + 31°C
CABIN PRESSURIZATION LIMIT
Maximum Cabin Pressure Differential ……….?
CABIN PRESSURIZATION LIMIT
Maximum Cabin Pressure Differential ……….6.6 psi
Landing Gear Cycle Limits
Landing Gear Cycle Limits
Landing gear cycles (1 up–1 down) are limited to one every 5 minutes for a total of 6 cycles followed by a 15 minute cool-down period.
Aft-Facing Seats
Aft-Facing Seats
The seat back of each occupied aft-facing seat must be
in the upright position and the headrest fully extended for
takeoff and landing.
SYSTEMS AND EQUIPMENT LIMITS
Brake Deice (If Installed)
Brake Deice system is not to be operated above ?°C.
SYSTEMS AND EQUIPMENT LIMITS
Brake Deice (If Installed)
Brake Deice system is not to be operated above 15°C.
ICING LIMITATIONS
Min Ambient Temperature for Operation of Deicing Boots
?
Min Airspeed for Sustained Icing Flight ………? KIAS
ICING LIMITATIONS
Min Ambient Temperature for Operation of Deicing Boots
–40°C
Min Airspeed for Sustained Icing Flight ………140 KIAS
ICING LIMITATIONS - Flight with Flaps Extended
ICING LIMITATIONS - Flight with Flaps Extended
Sustained flight in icing conditions with flaps extended is prohibited except for approach and landings.
ICING LIMITATIONS - Engine Anti-Ice
When flight free of visible moisture cannot be assured:
ON …………………………?°C or below
Takeoff and Flight Operations:
OFF ………………………..Above ?°C
ICING LIMITATIONS - Engine Anti-Ice
When flight free of visible moisture cannot be assured:
ON …………………………+5°C or below
Takeoff and Flight Operations:
OFF ………………………..Above +15°C
AVIONICS LIMITS - General
- ?
- ?
- ?
- ?
- ?
- Operating in the composite mode is limited to training and display failure conditions.
- The pilot’s and copilot’s Air Data Computers must be operative for takeoff.
- AHRS 1 and 2 must be operative for takeoff.
- The pilots PFD and MFD and copilot PFD must be installed and operational in the normal mode for takeoff.
- The MFD must be operational prior to engine start.
AUTOPILOT - Pre Flight Check
- ?
AUTOPILOT - Pre Flight Check
- An autopilot preflight check must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.
AUTOPILOT
The autopilot minimum engage height after takeoff is ? feet AGL.
AUTOPILOT
The autopilot minimum engage height after takeoff is 400 feet AGL.
AUTOPILOT
The autopilot minimum use height during cruise is ? feet AGL.
AUTOPILOT
The autopilot minimum use height during cruise is 1000 feet AGL.
AUTOPILOT
The autopilot minimum use height during approach is ? feet AGL.
AUTOPILOT
The autopilot minimum use height during approach is 79 feet AGL.
AUTOPILOT
The maximum coupled intercept angles are:
- Nav and Localizer — Less than ?°
- Back Course — ?°
AUTOPILOT
The maximum coupled intercept angles are:
- Nav and Localizer — Less than 90°
- Back Course — 70°
VNAV - Limitations
- ?
- ?
VNAV - Limitations
- VNAV altitudes must be displayed on the MFD map page or CDU legs page when utilizing VNAV for flight guidance.
- VNAV approach guidance to a DA is not authorized if the reported surface temperature is below the Baro-VNAV minimum temperature limitation specified on the applicable RNAV approach procedure chart.
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)
Terrain Inhibit (TERR INHIBIT) must be used when ……..?
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)
- Within 15 NM of an airport not listed in the database during:
a. Takeoff
b. Approach
c. Landing - FMS is operating in the DR mode.