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King Air 200/B200 > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

Cabin Door Unlocked (CABIN DOOR annunciation)

A

*All occupants - seated with seat belts on

Cabin sign - no smoke/fsb

Cabin differential pressure - reduce to lowest value practical (0 preferred) by descending/selecting higher cabin altitude setting

Oxygen - as required

Land at nearest airport

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2
Q

Emergency Exit

A

Emergency exit handle - PULL (plug type and opens into the cabin)

Before flight, always ensure door is unlocked

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3
Q

Spins

A
  • Control Column - full forward
  • Full rudder - Opposite direction of spin
  • Power levers - idle
  • Controls - Neutralize when rotation stops
  • Execute smooth pullout

NO spin tests have been conducted

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4
Q

Cabin door annunciation circuitry check

A

Battery - On

With door open & mechanism in locked position, ensure CABIN DOOR annunciation is illuminated

With door closed & latched, but not locked, ensure CABIN DOOR annunciation remains illuminated

With door closed & locked, ensure CABIN DOOR annunciation is EXTINGUISHED

Battery - Off

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5
Q

Electrical smoke or fire

A
  • Oxygen
  • Oxygen system ready: Pull on (verify)
  • Crew: Don masks (100% position)
  • Mic selector: Oxygen Mask
  • Audio speaker: On
Cabin temp mode - off
Vent blower - auto
Aft blower (if installed) - off
Avionics - off
Nonessential electrical equipment - off

if smoke or fire ceases
Individually restore avionics and equipment previously turned off

Isolate defective equipment

if smoke persists or fire extinguishing not confirmed
Cabin pressure - dump
Land ASAP

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6
Q

Generator inoperative

A

Load meter - verify Gen is off (0% load)
Generator- reset, then on

If generator will not reset:
Generator - off
Load meter - don’t exceed 100% (88% above 31,000)

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7
Q

Excessive load meter indication

A

Battery - off (monitor load meter)

If loadmeter still indicates above 100%:
Nonessential electrical equipment - off

If loadmeter indicates 100% or below:
Battery - on

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8
Q

Circuit breaker tripped

A

Nonessential circuit - Do not reset
Essential circuit:
- Breaker - push to reset
- if it trips again - do not reset

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9
Q

Hot battery bus check

A

Fuel firewall valves - closed
Standby boost pumps - on (listen for operation)
Battery switch - on: FUEL PRESS light illuminates immediately
Fuel firewall valves - OPEN: fuel press light extinguishes
Standby boost pumps - off: fuel press light illuminates

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10
Q

Current limiter check

A

One generator - turn off either L or R
L & R Volt/Loadmeters - normal
28 Volts on both load meters - normal
Less than 28 volts on any load meter - failed current limiter

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11
Q

Fuel pressure low (L FUEL PRESS or R FUEL PRESS)

A

*Standby pump (failed side) - On

[FUEL PRESS] - Extinguished

Oil temperature and oil pressure gages (failed side) - Monitor

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12
Q

Crossfeed (one engine inop)

A

Crossfeed - L or R (FUEL CROSSFEED) - Illuminated

Standby pumps - off

Aux tank transfer - auto

Fuel balance - monitor

if fuel is required from the inop engines aux tank and reason for shutdown is not engine fire or fuel leak:

Firewall shutoff valve - Open (FUEL PRESS) Extinguished

No transfer light (inop engine) - extinguished in 30-50 seconds

to discontinue crossfeed
Crossfeed flow switch - off (centered)

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13
Q

Aux fuel transfer failure (no transfer annunciation)

A

Aux tank transfer - override

No transfer light - extinguished (if not, aux fuel may not be available)

Aux fuel - monitor

Aux tank transfer - auto (when aux tank is empty)

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14
Q

Fuel system check - with battery on

A

Firewall shutoff valve - Close

Standby pumps - on (listen for operation, both FUEL PRESS lights illuminate)

Firewall shutoff valves - open (both FUEL PRESS lights extinguished)

Standby pumps - off (both FUEL PRESS lights illuminated)

Crossfeed - L then R while verifying FUEL CROSSFEED light illuminates & FUEL PRESS light extinguishes

Crossfeed- Off

Aux tank transfer - auto

No transfer light - press to test

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15
Q

Engine Failure - Emergency engine shutdown

*Proceed with this checklist for:
Engine torque increase - unscheduled
Engine fire in flight
Engine failure in flight

A 
*Affected engine
Condition lever - fuel cutoff
Prop lever - feather
Firewall shutoff valve - closed
Fire extinguisher (if installed) - actuate
Auto ignition - off
Generator - off
Prop sync - off 
Electrical load - monitor
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16
Q

Engine fire on ground

A 
*affected engine
Condition lever - fuel cutoff
Firewall shutoff valve - closed
Ignition and engine start - starter only
Fire extinguisher (if installed) - actuate (if required)
17
Q

Engine failure during ground roll

A

Power levers - idle
Brakes - as required
Operative engine - max reverse

*If insufficient runway remains for stopping
Condition levers - fuel cutoff
Firewall shutoff valve - closed
Master switch - off (gang bar down)

18
Q

Engine failure after lift off

A

Maintain directional control, pitch attitude, airspeed (121 Kts)
Power - max allowable
Landing gear - up

*if autofeather installed & being used, do not retard power lever of failed engine until the autofeather system has completely stopped prop rotation
Propeller - feather manually or autofeather
Flaps - up

*Inop engine side*
Condition lever - fuel cutoff
Propeller lever - feather
Firewall shutoff valve - closed 
Auto ignition - off
Autofeather- off 
Generator- off
Electrical load - monitor
19
Q

Engine failure in flight below Vmc

A

Power - reduce as required to maintain directional control
Nose - lower to accelerate above Vmc
Power - as required
Failed engine - secure (see emergency engine shutdown)

20
Q

Engine flameout (2nd engine aka both engine fails & this is the 2nd one to fail)

A

Power lever - idle
Propeller lever - do not feather
Condition lever - fuel cutoff
Conduct air start procedures

21
Q

Engine out glide

A

Landing gear - up
Flaps - up
Propellers - feathered
Airspeed - 135 knots

Glide ratio is 2nm per 1,000 feet of altitude

22
Q

Air start procedures (Starter assist)

  • do not attempt air starts if N1 indicates zero
  • above 20,000 feet, starts get a lot hotter. It may be necessary to move condition lever into cutoff in order to avoid an over temperature condition
A 
Cabin temp mode - off
Vent blower - auto
Aft blower (if installed) - off
Radar - standby or off
Windshield heat - off
Power lever - idle
Prop lever (inoperative engine) - Low rpm
Condition lever - fuel cutoff
Firewall shutoff valve - open
Generator (inop engine) - off

*If conditions permit, retard operative engine ITT to 700 degrees or less to reduce the possibility of exceeding ITT limit - reduce electrical load to minimum consistent with flight conditions

Ignition and engine start - ON (Ignition On annunciation illuminates)
Condition lever - low idle
ITT and N1 - Monitor (1,000 maximum)
Ignition and engine start - Off (N1 above 50%)
Prop lever - as required
Generator - on
Auto ignition - arm
Prop sync - on
Cabin temp mode - auto
23
Q

Air start Procedure (No starter assist) - Windmilling prop

A 
Power lever - idle
Prop lever - forward
Condition lever - fuel cutoff
Engine ice vane (inop engine) - retracted
Firewall shutoff valve - open
Generator (inop engine) - Off
Airspeed - 140kts minimum 
Altitude - below 20,000’
Auto ignition - arm (ignition on annunciation- illuminated)
Condition lever - Low idle
ITT and N1 - monitor (1000 maximum)
Power - as required (after ITT peaks)
Generator - On
Prop Sync - On
24
Q

What oil pressure values are undesirable and should on be tolerated for the completion of the flight?

How should the engine be operated in this case?

What limits requires the engine to be shut down or a landing made at the nearest airport?

A

60-85PSI

Reduced power setting to not exceed 1,100 lbs of torque

Oil pressure values below 60PSI

25
Q

If the CHIP DETECTOR annunciation illuminates what should you do?

A

Monitor the engine, if it’s performing normal just continue at discretion.

If the engine parameters become abnormal, shutdown is at pilot discretion and land ASAP.

26
Q

Overspeed Governor/Rudder Boost Test

A 
Rudder boost - on
Prop levers - full forward
Prop test switch - Hold to TEST
Left power lever - 1,800rpm
Left overspeed governor/rudder boost check - 1,870 +- 40 RPM
Left power lever - idle
Right power lever - 1,800rpm
Right overspeed governor/rudder boost check - 1,870 +- 40 RPM
Right power lever - idle
Prop test switch - Released
27
Q

Autofeather test

A

Power levers - 500 ft-lb torque
Autofeather switch - Hold to TEST
Power levers - Retard individually
- 400 ft-lb - opposite annunciator extinguished
- 200 ft-lb - Autofeather light cycle on & off
Power levers - both idle
Autofeather switch - ARM

28
Q

Loss of pressurization

A 
Oxygen
 - oxygen system - ready
 - crew - don mask
 - mic selector - oxygen mask
 - audio speaker - on
 - passenger manual drop out - pull on 
 - passengers - pull lanyard pin, don mask
Descend as required
Range - determine for final cruise altitude 
Oxygen duration - confirm
29
Q

Emergency Descent

A 
Oxygen - Crew Required
 - oxygen system - pull on
 - crew - don mask
 - mic selector - oxygen mask
 - audio speaker - on
 - passenger manual dropout - pull on
Power lever - idle
Prop levers - full forward
Flaps - approach 
Landing gear - down
Airspeed - 181 kts max
30
Q

Bleed air line failure (L or R BL AIR FAIL Annunciation)

A

Bleed air valve - applicable one to INSTR & ENVIR off position
-*Bleed air warning annunciation will not extinguish after closing the switches

Engine instruments - monitor for increase in torque, decrease in ITT (indicates the leak was isolated)

31
Q

Unscheduled Electric Elevator Trim

A

Airplane attitude - maintain

Control wheel disconnect - Depress fully (2nd level, ELEC TRIM OFF annunciator illuminated)

Elevator trim - off

32
Q

Unscheduled rudder boost activation

A

Directional control - maintain using rudder pedals

Rudder boost - off

*if condition persists:
Rudder boost circuit breaker - pull

Either bleed air valve - INST & ENVIR OFF

Rudder trim - as required

Perform normal landing

King Air 200/B200 (10 decks)

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