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B1900 > Emergency Drill > Flashcards

Emergency Drill Flashcards

1
Q

Engine Fire or Failure in Flight

A

Condition Level…………..Fuel Cut Off

Prop Lever………………….Feather

Firewall Fuel Valve……….Pull Closed

Fire Extinguisher………….Actuate

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2
Q

Engine Fire on Ground

A

Condition Lever………………………………Fuel Cut off

Firewall Fuel Valve…………………………..Pull Closed

Ignition and Engine Start Switch……….Starter Only

Fire Extinguisher(if required)……………..Actuate

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3
Q

Engine Failure in Flight Below Air Minimum Control Speed (Vmca)

A
  1. Reduce power on operative engine as required to maintain control
  2. Lower nose to accelerate above Vmca
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4
Q

Oil Pressure Low (L or R OIL PRES LO Annunciator)

A
  1. Oil Pressure gage……….confirm below 60 PSI
  2. If confirmed………………secure engine or land at nearest suitable airport using the minimum power required to sustain flight
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5
Q

Prop Collisions During Ground Operation

A
  1. Power Levers………Ground Fine or Idle
  2. Condition Levers…..Fuel Cutoff
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6
Q

Fuel Pressure Low

A

Standby Pump(failed side)…………..ON

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7
Q

Electrical Smoke or Fire

A
  1. Oxygen
    a. Oxygen control………………..confirm on
    b. Crew……..Don masks,and goggles

Mark Selector Switch……..emergency

Purge Valve……………open

c. Headsets…………..DON
d. MIC selector switches……..OXYGEN MASK

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8
Q

Environmental System Smoke or Fumes

A
  1. Oxygen
    a. Oxygen control………………..confirm on
    b. Crew……..Don masks, and goggles

Mask Selector Switch……..emergency

Purge Valve……………open

c. Headsets…………..DON
d. MIC selector switches……..OXYGEN MASK

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9
Q

Cabin or Cargo Door Unlocked (Cabin door or cargo door annunciator)

A
  1. All Occupants…….Seated with seat belts securely fastened
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10
Q

Emergency Descent

A
  1. Power Levers……………………IDLE
  2. Propeller Levers………………..Full Forward
  3. Flaps……………………………….17Deg
  4. Landing Gear…………………….Down
  5. Airspeed…………………………..180 kts
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11
Q

GLIDE

A

Landing Gear Control……………….UP

Flaps………………………………………UP

Propellers……………………………….Feathered

Airspeed…………………………………140 kts

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12
Q

Single Inverter or AC Bus Failure (L or R AC BUS Annunciator)

A
  1. Ac Bus Switch(failed side)…………off then on
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13
Q

Single Inverter Failure followed by a second inverter or AC bus failure(L and R AC BUS failure)

A
  1. Attiude/Heading Control…………..Use Standby Attitude Indicator and Compass
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14
Q

Dual inverter Failure (L and R AC Bus Annunciators)

A

Attitude/Heading Control…………Use Standby Attitude Indicator and Compass

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15
Q

Dual Generator Failure (L and R DC Gen Annunciators)

A
  1. Instrument emergency lights………………ON
  2. Generators…………….RESET,

Then ON If either Generator will reset

  1. Do not Exceed 100%load on Operating generator If Neither Generator Will Reset:
  2. Non-Essential Equipment……………….OFF
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16
Q

Unscheduled Electric Elevator Trim

A
  1. Airplane Attitude…………………Maintain(Using Elevator Control)
  2. Control Wheel Disconnect Switch……………Depress Fully (Pitch Trim OFF Annunciator - Illuminated)
17
Q

Unscheduled Rudder Boost Activation

A
  1. Control Wheel Disconnect Switch…………Depress and Hold

Rudder Boost/Yaw Control Test Switch…….off if condition persists: Rudder Boost CCT Breaker…………..PULL

18
Q

Use of Oxygen

A
  1. Oxygen Control……………Confirm On
  2. Cabin Oxygen Control………..Pull On
  3. Crew…………………………..Don Masks
  4. Mask Selector Switch……………..SET

Inflatable type harness……….SET

Strap Type Harness…………NORMAL (100% at cabin altitudes above 20,000)

  1. Headsets…………………………..DON
  2. MIC Selector Switches…..OXYGEN MASK
19
Q

Cabin Decompression

A
  1. Oxygen Control……………Confirm On
  2. Cabin Oxygen Control………..Pull On
  3. Crew…………………………..Don Masks
  4. Mask Selector Switch……………..SET

Inflatable type harness……….SET

Strap Type Harness…………NORMAL (100% at cabin altitudes above 20,000)

  1. Headsets…………………………..DON
  2. MIC Selector Switches…..OXYGEN MASK
20
Q

High Differential Pressure(CAB DIFF HI Annunciator)

A
  1. Bleed Air Valves………………..Environmental OFF
21
Q

Bleed Air Line Failure (L or R BL AIR Fail Annunciator)

A

Bleed Air Valve (affected Engine)…………..INST ENVIR OFF

22
Q

Environmental Failure (L or R ENVIR FAIL Annunciator)

A
  1. Bleed Air Valve (affected side)……….CYCLE to Environmental off and back to open

if ENVIR FAIL Annunciator Extingishes, Continue operation

If Annunciator Remains Illuminated:

  1. Bleed Air valves (affected side)………..Environment OFF
23
Q

In Flight Activation of GPWS Warning

A

In IMC or at Night

  1. Wings………………………….Level
  2. Airspeed………………………122KIAS
  3. Power…………………………..Max Allowable
  4. Gear and Flaps………………Retract
  5. Continue Climb at 122 KIAS Until Visual and Aural Warnings Cease

In Day VMC

  1. Evaluate Flight Path With Respect to Terrain
  2. Take Action As Necessary to Recover Safe Terrain Clearance
24
Q

SPIN

A
  1. Control Column……….Full FWD,

Ailerons Neutral

  1. Full Rudder……………Opposite the direction of spin
  2. Power Levers…………IDLE
  3. Rudder…………..Neutralize when Rotation Stops 5. Execute a smooth pull out

B1900 (9 decks)

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