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King Air 350 CAE > 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
  6. 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……………………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

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. ECS MODE …………OFF
  5. Cockpit Cabin Blower………….OFF
  6. Non- essential Equipment…………………………………………OFF
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8
Q

UNSCHEDULED ELECTRICAL PITCH TRIM ACTIVATION

A
  1. Aircraft Attitude……………………………………MAINTAIN USING
    ELEVATOR CONTROL
  2. AP/Trim Disconnect……………………………….. DEPRESS FULLY & HOLD
    [TRIM OFF]- ILLUMINATED
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9
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. AP/Trim Disconnect……………………..DEPRESS TO 1ST LEVEL
    AND HOLD
  2. Rudder Boost…………………………………………………………….OFF
    If Condition Persists:
  3. YD/AP DISC (on Flight Guidance Panel)………..PULL DOWN
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10
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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11
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. Mic Switch(es)…………………………………………OXYGEN MASK

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12
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A

Oxygen:
1. Oxygen Mask(s)……………………………………………………….DON
2. Mask Selector Switch………………………………EMERG Position
3. Mic Switch(es)…………………………………………..OXYGEN MASK

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13
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

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14
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
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15
Q

USE OF OXYGEN

A

Crew:
1. Oxygen Mask(s)……………………………………………………….DON
2. Mic Switch(es)…………………………………………..OXYGEN MASK

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16
Q

PRESSURIZATION LOSS
CABIN ALT HI (light ON)

A
  1. Oxygen Mask(s)……………………………………………………….DON
  2. Mic Switch(es)…………………………………………..OXYGEN MASK
  3. Passenger Manual Drop-Out……………………………..PULL ON
    [PASS OXYGEN ON]- ILLUMINATED
  4. Descend……………………………………………………..AS REQUIRED
17
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
18
Q

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

A
  1. Passenger Manual Drop-Out……………………………..PULL ON
19
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

20
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
21
Q

AUTOPILOT MISTRIM

A
  1. Flight Controls…………..HOLD FIRMLY
  2. AP……………………………..DISENGAGE
22
Q

AUTOPILOT TRIM FAIL

A
  1. Flight Controls…….HOLD FIRMLY
  2. AP……………………….DISENGAGE
23
Q

AUTOMATIC AUTOPILOT DISENGAGEMENT

A
  1. Maintain Airplane Control
  2. AP/TRIM Disconnect…………..DEPRESS TO 1ST LEVEL TO CANCEL HORN
24
Q

EGPWS

A
  1. Wings level
  2. Power…… MAX ALLOWABLE
  3. Pitch ….. INCREASE
    • promptly and smoothly to 20-25*
    • adjust as required to avoid stall/buffeting
    • adjust to maintain 125
      4.Gear & Flaps……UP

King Air 350 CAE (14 decks)

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