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King Air 200 Memory Items > KING AIR 200 Flashcards > Flashcards

KING AIR 200 Flashcards

1
Q

Emergency Engine Shutdown

A

1 Condition Lever……….Fuel Cutoff

2 Prop Lever………………Feather

  1. Firewall Shutoff ……..Close
  2. Fire Extinguisher…….Actuate

Extinguisher if installed and if fire warning persists.

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2
Q

Engine Fire on the Ground

A

1 Condition Lever…………….Fuel Cutoff

2 Firewall Shutoff …………..Close

  1. Ignition / Engine Start….Starter Only

If Fire warning persists…

  1. Fire Extinguisher…….Actuate

Extinguisher if installed

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3
Q

Emergency Engine Shutdown

on the Ground

A

1 Condition Lever……….Fuel Cutoff

2 Prop Lever………………Feather

  1. Firewall Shutoff ……..Close
  2. Master Switch GB…..Off
  3. ESIS Power…………….Off
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4
Q

Engine Failure During Takeoff

At or Below V1 Takeoff Aborted

A
  1. Power Levers………………Ground Fine
  2. Brakes……….As required to achieve stopping distance
  3. Operative Engine………..Max Reverse
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5
Q

Engine Failure During Takeoff

At or Above V1

Takeoff Continued

A
  1. Power……………..Max allowable
  2. Airspeed…………Maintain Take off Speed or above
  3. Landing Gear when pos climb established….UP
  4. Prop Inop engine…………verify feather
  5. Airspeed after obstacle clearance…..Vyse
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6
Q

Engine Failure in Flight Below

Air minimumControl Speed (VMCA)

A
  1. Power…………..Reduce as required to maintain control
  2. Nose…………….Lover to accelerate above VMCA
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7
Q

Engine Flameout

(Second Engine)

A
  1. Power Lever ………………….IDLE
  2. Prop Lever ……………………DO NOT FEATHER
  3. Condition Lever ……………FUEL CUTOFF
  4. Conduct Air Start Procedure in ABNORMAL PROCEDURES.
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8
Q

Fuel Pressure Low

L Fuel Pressure or R Fuel Pressure

A

Standby Pump ( Failed Side) ……………ON

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9
Q

SMOKE and FUME Elimination

ELECTRICAL SMOKE OR FIRE

A

SMOKE and FUME Elimination

ELECTRICAL SMOKE OR FIRE

  1. Oxygen Masks…………………..DON
  2. Mask Selector Switch ……….EMER POSITION
  3. MIC Switch(es) ………………… OXY
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10
Q

ENVIRONMENTAL SYSTEM

SMOKE OR FUMES

A

ENVIRONMENTAL SYSTEM
SMOKE OR FUMES

  1. Oxygen Masks…………………DON
  2. Mask Selector Switch ……..EMER POSITION
  3. MIC Switch(es) ………………..OXY
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11
Q

AIRSTAIR DOOR/CARGO DOOR
UNLOCKED

A

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

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12
Q

EMERGENCY DESCENT

A

EMERGENCY DESCENT

  1. Power Levers …………. IDLE
  2. Prop Levers …………. FULL FORWARD
  3. Flaps (200 knots maximum). APPROACH
  4. Landing Gear (181 knots .. DN
  5. Airspeed …………….. 181 KNOTS MAXIMUM
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13
Q

GLIDE

A

GLIDE

  1. Landing Gear ………… UP
  2. Flaps ………………. UP
  3. Propellers ………….. FEATHERED
  4. Airspeed ……………. 135 KNOTS
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14
Q

DUAL GEN FAILURE

L DC GEN R DC GEN

A

DUAL GEN FAILURE

L DC GEN R DC GEN

Generators ………….. RESET, THEN ON

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15
Q

USE OF OXYGEN

A

USE OF OXYGEN

  1. Oxygen Mask(s) ……..DON
  2. MIC Switch(es) ……. OXY
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16
Q

PRESSURIZATION LOSS

ALT WARN

A

PRESSURIZATION LOSS

ALT WARN

  1. Oxygen Mask(s) ……….DON
  2. MIC Switch(es) ……… OXY
  3. Passenger Manual Drop-Out .PULL ON [PASS OXY ON] – ILLUMINATED
  4. Descend ……………. AS REQUIRED
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17
Q

HIGH DIFFERENTIAL PRESSURE

A

HIGH DIFFERENTIAL PRESSURE

If Cabin Differential Pressure exceeds 6.6 PSI:

  1. Bleed Air Valves …………. ENVIR OFF
  2. Oxygen (Crew and Passengers) ..AS REQUIRED
  3. Descend …………………. AS REQUIRED
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18
Q

AUTO DEPLOYMENT

OXYGEN SYSTEM FAILURE

A
  1. Passenger Manual Dropout…..Pull On
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19
Q

BLEED AIR FAIL

A
  1. Bleed Air Valve effected Engin

INST & ENVIR OFF

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20
Q

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.

A
  1. Control Column ……..full forward Airerons Neutral
  2. Full Rudder……………..opposite direction of spin
  3. Power Levers………….idle
  4. Rudder…………………….Neutalize when spin stops
  5. Execute smooth pullout
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21
Q

UNSCHEDULED ELECTRIC ELEVATOR

TRIP ACTIVATION

A
  1. Airplane Attitude………………………Maintain using elevator control
  2. A/P/Trim Disconnect………………..Depress fully and hold
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22
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. Directional Control ………Maintain using Rudder Pedals
  2. Rudder Boost………………..OFF
  3. IF Condition Persists
  4. Rudder Boost Circuit Breaker……Pull
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23
Q

AUTOPILOT MISTRIM ANNUNCIATION

A
  1. Flight Controls…………………..HOLD FIRMLY
  2. A/P………………………………………Disengage
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24
Q

AUTOPILOT TRIM FAIL ANNUNCIATION

A
  1. Flight Controls………………HOLD FIRMLY
  2. A/P………………………………….Disengage
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25
Q

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)

A

In IMC or at Night:

  1. Wings …………………….. LEVEL
  2. Power …………………… MAX ALLOWABLE
  3. 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.

  1. Gear and Flaps …………….. UP
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26
Q

Engine Oil Limitations

Oil Temp for Starting ……………….. ?°C (Min)

Oil Press for Idle RPM ………………. ? PSI (Min)

Oil Press Maximum Transient …….? PSI

A

Engine Oil Limitations

Oil Temp for Starting ……………….. –40°C (Min)

Oil Press for Idle RPM ………………. 60 PSI (Min)

Oil Press Maximum Transient ………….. 200 PSI

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27
Q

ENGINE LIMITS

Oil (°C/PSI)

Oil Temp Takeoff & Max Continuous Thrust ……….?° C

Oil Press Takeoff & Max Continuous Thrust ….. ? PSI

(?° C Recommended)

A

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

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28
Q

PROPELLER LIMITS

Idle ……………………. ? RPM

Takeoff & Max Continuous ….. ? RPM

Transient ……………….. ? RPM

A

PROPELLER LIMITS

Idle ……………………. 1180 RPM

Takeoff & Max Continuous ….. 2000 RPM

Transient ……………….. 2200 RPM

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29
Q

EXTERNAL POWER LIMITS

Volts ……………….. ?

Amps ………………… ? (Momentarily) ? (Continuous)

A

EXTERNAL POWER LIMITS

Volts ……………….. 28.0 – 28.4

Amps ………………… 1000 (Momentarily) 300 (Continuous)

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30
Q

Maximum sustained generator
load is limited as follows:

In-Flight:

Sea Level to 31,000 Feet Altitude ……….. ?%

Above 31,000 Feet Altitude ………………. ?%

Ground Operation ……………………….. ?%

A

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%

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31
Q

Starter Limitations

Duration On/Off ?

A

Starter Limitations

Duration On/Off …………..

40 seconds ON, 60 seconds OFF
40 seconds ON, 60 seconds OFF

40 seconds ON, 30 minutes OFF

32
Q

FUEL LIMITS

Approved Engine Fuels

Commercial Grades Military Grades

A

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
33
Q

FUEL LIMITS

Emergency Engine Fuels …………. 80 Red (Formerly 80/87)

                                            100 Green (Formerly 100/130)

                                            100LL Blue (100L Green)

                                            91/96

                                             115/145 Purple
A

FUEL LIMITS

Emergency Engine Fuels …………. 80 Red (Formerly 80/87)

                                            100 Green (Formerly 100/130)

                                            100LL Blue (100L Green)

                                            91/96

                                             115/145 Purple
34
Q

FUEL LIMITS

Emergency Engine Fuels - Limitations on the Use of Aviation Gasoline:

  1. Operation is limited to ? hours between engine overhauls.
  2. Operation is limited to ? feet pressure altitude or below if either standby pump is inoperative.
  3. Crossfeed capability is required for climbs above ? feet pressure
  4. Operation above ? feet is prohibited.
A

FUEL LIMITS

Emergency Engine Fuels - Limitations on the Use of Aviation Gasoline:

  1. Operation is limited to 150 hours between engine overhauls.
  2. Operation is limited to 20,000 feet pressure altitude (FL 200) or below if either standby pump is inoperative.
  3. Crossfeed capability is required for climbs above 20,000 feet pressure
  4. Operation above 31,000 feet (FL 310) is prohibited.
35
Q

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)
A

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)
36
Q

FUEL MANAGEMENT

Maximum Imbalance ……….. ? LB

Fuel Crossfeed …… Permitted only ?

A

FUEL MANAGEMENT

Maximum Imbalance ……….. 1000 LB

Fuel Crossfeed …… Permitted only when one engine is inoperative.

37
Q

FUEL MANAGEMENT

Takeoff is not allowed with:

Indication ……………. ?

Amount of Fuel ………… LESS THAN ? LB

in each main tank system

A

FUEL MANAGEMENT

Takeoff is not allowed with:

Indication ……………. IN THE YELLOW ARC

Amount of Fuel ………… **LESS THAN 265 LB **
in each main tank system

38
Q

AUTOPILOT FAILURES

AUTOPILOT AUTOMATIC DISENGAGEMENT

A
  1. Maintain Airplane Control.
  2. AP/TRIM Disconnect ………..DEPRESS TO 1ST LEVEL TO CANCEL HORN
39
Q

AIRSPEED LIMITATIONS

Maneuvering Speed (VA)

(KIAS at 12,500 lb)

A

181 Kts

40
Q

Maximum Flaps Speeds (VFE)

(KIAS at 12,500 lb)

VFE/VFO Approach—40% (White “APP” Arrow) …….?

VFE/VFO Full Down—100% (White “DN” Arrow) ……?

A

VFE/VFO (Approach) ………….200 KIAS

VFE/VFO (Full Down) …………157 KIAS

41
Q

AIRSPEED LIMITATIONS

Maximum Landing Gear Speeds (VLO/VLE)

(KIAS at 12,500 lb)

VLO (Extension) ……………?

VLO (Retraction) …………..?

VLE ………………………?

A

AIRSPEED LIMITATIONS

Maximum Landing Gear Speeds (VLO/VLE)

(KIAS at 12,500 lb)

VLO (Extension) ……………181 KIAS

VLO (Retraction) …………..163 KIAS

VLE ………………………181 KIAS

42
Q

AIRSPEED LIMITATIONS

Air Minimum Control Speed (VMCA)

(Red Line)

A

AIRSPEED LIMITATIONS

Air Minimum Control Speed (VMCA)

(Red Line)

86 KIAS

43
Q

AIRSPEED LIMITATIONS

Maximum Operating Speeds

VMO …………….. ?

MMO …………….. ?

A

AIRSPEED LIMITATIONS

Maximum Operating Speeds

VMO …………….. 259 KIAS

MMO …………….. Mach .52

44
Q

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) ……… ?

A

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

45
Q

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
?

A

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

46
Q

EMERGENCY AIRSPEEDS

Emergency Descent ………………?

Maximum Range Glide …………….?

A

EMERGENCY AIRSPEEDS

Emergency Descent ………………181 KIAS

Maximum Range Glide …………….135 KIAS

47
Q

POWER LEVERS

A

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.

48
Q

ENGINE LIMITS

Torque — Takeoff, Max Continuous ……?

Torque — Transient ………………..?

A

ENGINE LIMITS

Torque — Takeoff, Max Continuous ……2230 FT Lbs

Torque — Transient ………………..2750 FT lbs

49
Q

ENGINE LIMITS

N1 — Takeoff, Max Continuous ………?

N1 — Transient …………………..?

A

ENGINE LIMITS

N1 — Takeoff, Max Continuous ………101.5 %

N1 — Transient …………………..102.6 %

50
Q

ENGINE LIMITS

ITT Temp (°C)

Start ……………………….. ?

Takeoff / Max Continuous ………. ?

Cruise Climb / Normal Cruise …… ?

Transient ……………………. ?

A

ENGINE LIMITS

ITT Temp (°C)

Start ……………………….. 1000°C

Takeoff / Max Continuous ………. 800°C

Cruise Climb / Normal Cruise …… 770°C

Transient ……………………. 850°C

51
Q

FUEL LIMITS

Approved Engine Fuels

A

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

52
Q

AUXILIARY FUEL

A

AUXILIARY FUEL

Do not put any fuel into the auxiliary tanks

unless the main tanks are full.

53
Q

OPERATING WITH LOW FUEL PRESSURE

OR

Time until overhauling or replacement of the affected engine driven fuel pump …………………………………………………………………. ?

A

OPERATING WITH LOW FUEL PRESSURE

OR

Time until overhauling or replacement of the affected engine driven fuel pump ………………………….10 Hours

54
Q

PROPELLER ROTATIONAL SPEED LIMITS

Transients not exceeding 5 seconds …………?

Reverse …………………………………?

All other conditions ……………………..?

Minimum idle speed ……………………….?

A

PROPELLER ROTATIONAL SPEED LIMITS

Transients not exceeding 5 seconds ………..2200 rpm

Reverse …………………………………1900 rpm

All other conditions ……………………..2000 rpm

Minimum idle speed ……………………….1180 rpm

55
Q

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 ……………………………………….?

A

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

56
Q

PROPELLER AUTOFEATHER

A

PROPELLER AUTOFEATHER

The propeller autofeather system must be operable for

all flights and must be armed for takeoff, climb, approach

and landing.

57
Q

WEIGHT LIMITS

Maximum Ramp Weight ……………………..?

Maximum Takeoff Weight:

All Except 14 CFR Part 135 Operations ……..?

Maximum Landing Weight …………………..?

Maximum Zero Fuel Weight …………………?

A

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

58
Q

WEIGHT LIMITS

Maximum Weight in Baggage Compartment:

When Equipped With Fold-Up Seats …………. ?

When Not Equipped With Fold-Up Seats ……… ?

A

WEIGHT LIMITS

Maximum Weight in Baggage Compartment:

When Equipped With Fold-Up Seats …………. 510 lbs

When Not Equipped With Fold-Up Seats ……… 550 lbs

59
Q

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation ………………………. ?

Operation with Yaw Damp System Inoperative .. ?

A

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation ………………………. 35,000 ft

Operation with Yaw Damp System Inoperative .. 17,000 ft

60
Q

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level to 25,000 Feet Pressure Altitude …..?

Above 25,000 Feet Pressure Altitude …………?

A

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

61
Q

CABIN PRESSURIZATION LIMIT

Maximum Cabin Pressure Differential ……….?

A

CABIN PRESSURIZATION LIMIT

Maximum Cabin Pressure Differential ……….6.6 psi

62
Q

Landing Gear Cycle Limits

A

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.

63
Q

Aft-Facing Seats

A

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.

64
Q

SYSTEMS AND EQUIPMENT LIMITS

Brake Deice (If Installed)

Brake Deice system is not to be operated above ?°C.

A

SYSTEMS AND EQUIPMENT LIMITS

Brake Deice (If Installed)

Brake Deice system is not to be operated above 15°C.

65
Q

ICING LIMITATIONS

Min Ambient Temperature for Operation of Deicing Boots
?

Min Airspeed for Sustained Icing Flight ………? KIAS

A

ICING LIMITATIONS

Min Ambient Temperature for Operation of Deicing Boots
–40°C

Min Airspeed for Sustained Icing Flight ………140 KIAS

66
Q

ICING LIMITATIONS - Flight with Flaps Extended

A

ICING LIMITATIONS - Flight with Flaps Extended

Sustained flight in icing conditions with flaps extended is prohibited except for approach and landings.

67
Q

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

A

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

68
Q

AVIONICS LIMITS - General

  1. ?
  2. ?
  3. ?
  4. ?
  5. ?
A
  1. Operating in the composite mode is limited to training and display failure conditions.
  2. The pilot’s and copilot’s Air Data Computers must be operative for takeoff.
  3. AHRS 1 and 2 must be operative for takeoff.
  4. The pilots PFD and MFD and copilot PFD must be installed and operational in the normal mode for takeoff.
  5. The MFD must be operational prior to engine start.
69
Q

AUTOPILOT - Pre Flight Check

  1. ?
A

AUTOPILOT - Pre Flight Check

  1. An autopilot preflight check must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.
70
Q

AUTOPILOT

The autopilot minimum engage height after takeoff is ? feet AGL.

A

AUTOPILOT

The autopilot minimum engage height after takeoff is 400 feet AGL.

71
Q

AUTOPILOT

The autopilot minimum use height during cruise is ? feet AGL.

A

AUTOPILOT

The autopilot minimum use height during cruise is 1000 feet AGL.

72
Q

AUTOPILOT

The autopilot minimum use height during approach is ? feet AGL.

A

AUTOPILOT

The autopilot minimum use height during approach is 79 feet AGL.

73
Q

AUTOPILOT

The maximum coupled intercept angles are:

  • Nav and Localizer — Less than ?°
  • Back Course — ?°
A

AUTOPILOT

The maximum coupled intercept angles are:

  • Nav and Localizer — Less than 90°
  • Back Course — 70°
74
Q

VNAV - Limitations

  1. ?
  2. ?
A

VNAV - Limitations

  1. VNAV altitudes must be displayed on the MFD map page or CDU legs page when utilizing VNAV for flight guidance.
  2. 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.
75
Q

ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)

Terrain Inhibit (TERR INHIBIT) must be used when ……..?

A

ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)

  1. Within 15 NM of an airport not listed in the database during:
    a. Takeoff
    b. Approach
    c. Landing
  2. FMS is operating in the DR mode.

King Air 200 Memory Items (12 decks)

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