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King Air 350 > Emergency Procedures Memory Actions > Flashcards

Emergency Procedures Memory Actions Flashcards

1
Q

ENGINE FIRE OR FAILURE IN FLIGHT

A

Affected Engine
1. Condition Lever…………………………………………….Fuel Cut Off
2. Prop Lever…………………………………………………………..Feather
3 Firewall Fuel Valve……………………………………………………Close
(Extinguisher push) & (Closed) Illuminated
4. Fire Extinguisher (if fire persists)………………………….Actuate
(Discharged) Illuminated

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2
Q

ENGINE FIRE ON GROUND

A

Affected Engine
1. Condition Lever…………………………………………….Fuel Cut Off
2. Firewall Fuel Valve…………………………………………………..Close
(Extinguisher Push) & (Closed) - Illuminated
3. Starter Switch……………………………………………….Starter Only
4. Fire Extinguisher.(if fire persists)………………………….Actuate
(Discharged) - Illuminated

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3
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A
  1. Condition Levers……………………………………….FUEL CUT OFF
  2. Prop Levers……………………………………………………….FEATHER
  3. Firewall Fuel Valves……………………………………………..CLOSED
    (EXTINGUISHER PUSH) & (CLOSED) - ILLUMINATED
  4. Master Switch (gang bar)…………………………………………..OFF
  5. Battery Bus…………………………………………………..EMERG 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……………………MAXIMUM (or as required to achieve
    stopping distance)
    WARNING: Do not use reverse with one engine inoperative. Care must be exercised when using single-engine ground fine on surfaces with reduced traction.
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5
Q

ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1)- TAKEOFF CONTINUED

A
  1. Vr Speed………………………………………………………. ROTATE TO
    APPROXIMATELY 10° PITCH ATTITUDE
  2. Landing Gear (when positive climb established) …………Up
  3. Airspeed…………………………………Maintain V2 to 400 FT AGL
  4. Propeller (inoperative engine)………………..Verify Feathered
    WARNING: Do not retard failed engine power lever until autofeather system has completely stopped propeller rotation.
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6
Q

ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (Vmca)

A
  1. Power……………………………………..REDUCE AS REQUIRED TO
    MAINTAIN CONTROL
  2. Nose…………………………………………..LOWER TO ACCELERATE
    ABOVE Vmca
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7
Q

GLIDE

A
  1. Landing Gear………………………………………………………………UP
  2. Flaps…………………………………………………………………………..UP
    WARNING: Do not feather second engine propeller if a No Start Assist Air Start is to be conducted. Air starts with a windmilling propeller will result in lower starting tempuratures. Refer too Abnormal Procedures for Air Start procedures.
  3. Prop Levers……………………………………………………..Feathered
  4. Airspeed……………………………………………………………..135 KTS
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7
Q

DUAL GENERATOR FAILURE
L DC GEN (light ON)
AND
R DC GEN (light ON)

A
  1. Instrument Emergency Lights (if required)………………….ON
  2. Generators…………………………………………….RESET, THEN ON
    If Either Generator Will Reset:
  3. Operating Generator Loadmeter……………………..MONITOR
    If Neither Generator Will Reset:
  4. Non- essential Equipment…………………………………………OFF
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8
Q

SINGLE INVERTER FAILURE
#1 AC BUS (light ON)
OR
#2 AC BUS (light ON)

A
  1. AC Bus Circuit Breakers…………………………………………CHECK
    If Circuit Breaker is Not Tripped:
  2. Failed Inverter………………………………………………………SELECT
    BUS TRANSFER
    If Circuit Breaker is Tripped:
    3.Circuit Breaker………………………………………………………..RESET
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9
Q

DUAL INVERTER FAILURE
#1 AC BUS (light ON)
AND
#2 AC BUS (light ON)

A
  1. Attitude/Heading Control…………………………….USE BACKUP
    INSTRUMENTS
  2. AC Bus Circuit Breakers (if tripped)…………………………RESET
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10
Q

UNSCHEDULED ELECTRICAL PITCH TRIM ACTIVATION

A
  1. Aircraft Attitude……………………………………MAINTAIN USING
    ELEVATOR CONTROL
  2. AP/Trim Disconnect……………………………….. DEPRESS FULLY
    [PITCH TRIM OFF]- ILLUMINATED
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11
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. AP/Trim Disconnect……………………..DEPRESS TO 1ST LEVEL
    AND HOLD
  2. Rudder Boost…………………………………………………………….OFF
    If Condition Persists:
  3. Rudder Boost Circuit Breaker…………………………………..PULL
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12
Q

SPINS

A

If a Spin is Entered Inadvertently:
NOTE: Steps 1 through 3 should be done AGGRESSIVELY and SIMULTANEOUSLY.
1. Control Column……………………………………..FULL FORWARD,
AILERONS NEUTRAL
2. Full Rudder……………….OPPOSITE THE DIRECTION OF SPIN
3. Power Levers……………………………………………………………IDLE
4. Rudder………………………………………………NEUTRALIZE WHEN
ROTATION STOPS
5. Execute smooth pullout

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13
Q

WINDSHIELD ELECTRICAL FAULT

A
  1. WSHLD ANTI-ICE switches………………………………………….OFF
    If Smoke and/or Fire Does Not Cease:
  2. ELECTRICAL SMOKE OR FIRE Procedure…………..CONDUCT
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14
Q

ELECTRICAL SMOKE OR FIRE

A

WARNING: Dissipation of smoke is not sufficient evidence that a fire has been extinguished. If it cannot be visually confirmed that no fire exists, land at the nearest suitable airport.
1. Oxygen Mask(s)……………………………………………………….DON
2. Mask Selector Switch………………………………EMERG Position
3. Headset(s)……………………………………………..DON, OR AUDIO
SPEAKER(S)- ON
4. Mic Switch(es)…………………………………………OXYGEN MASK

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15
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A

Oxygen:
1. Oxygen Mask(s)……………………………………………………….DON
2. Mask Selector Switch………………………………EMERG Position
3. Headset(s)……………………………………………..DON, OR AUDIO
SPEAKER(S)- ON
4. Mic Switch(es)…………………………………………..OXYGEN MASK

16
Q

AIRSTAIR DOOR/CARGO DOOR UNLOCKED
DOOR UNLOCKED (light ON)

A

WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seatbelts securely fastened.

If the [DOOR UNLOCKED] illuminates, Or If An Unlatched Airstair Door/Cargo Door Is Suspected:
1. All Occupants……………………………………………..SEATED WITH
SEAT BELTS SECURELY FASTENED

17
Q

EMERGENCY DESCENT

A
  1. Power Levers……………………………………………………………IDLE
  2. Prop Levers…………………………………………….FULL FORWARD
  3. Flaps (202 knots maximum)……………………………APPROACH
  4. Landing gear (184 knots maximum)………………………DOWN
  5. Airspeed………………………………………..184KNOTS MAXIMUM
18
Q

USE OF OXYGEN

A

Crew:
1. Oxygen Mask(s)……………………………………………………….DON
2. Headset(s)……………………………………………..DON, OR AUDIO
SPEAKER(S) ON
3. Mic Switch(es)…………………………………………..OXYGEN MASK

19
Q

PRESSURIZATION LOSS
CABIN ALT HI (light ON)

A
  1. Oxygen Mask(s)……………………………………………………….DON
  2. Headset(s)……………………………………………..DON, OR AUDIO
    SPEAKER(S) ON
  3. Mic Switch(es)…………………………………………..OXYGEN MASK
  4. Passenger Manual Drop-Out……………………………..PULL ON
    [PASS OXYGEN ON]- ILLUMINATED
  5. Descend……………………………………………………..AS REQUIRED
    WARNING: The highest recommended cabin altitude for sustained flight is 25,000 ft.
20
Q

HIGH DIFFERENTIAL PRESSURE
CABIN DIFF HI (light ON)

A
  1. Bleed Air Valves………………………………………………ENVIR OFF
  2. Oxygen (crew and passengers)…………………..AS REQUIRED
  3. Descend……………………………………………………..AS REQUIRED
21
Q

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE
CABIN ALT HI (light ON)
PASS OXYGEN ON (light OFF)

A
  1. Passenger Manual Drop-Out……………………………..PULL ON
22
Q

BLEED AIR FAILURE
L BLEED FAIL (light ON)
OR
R BLEED FAIL (light ON)

A

If Illuminated During Flight
1. Bleed Air Valve (affected engine)………..PNEU & ENVIR OFF
[L BLEED OFF] or [R BLEED OFF] -ILLUMINATED

23
Q

ENHANCHED GROUND PROXIMITY WARNING SYSTEM (EGPWS) (IF INSTALLED)

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° to 25°
·Adjust as required to avoid continuous buffeting
and/or stall warning
·Adjust to maintain 125 KIAS (B300/B300C)
4. Gear and Flaps……………………………………………………………UP

King Air 350 (14 decks)

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