Emergency Memory Items Flashcards

1
Q

One-Engine Inoperative Best
Angle-of-Climb (VXSE)

A

115KIAS

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2
Q

One-Engine Inoperative Best
Rate-of-Climb (VYSE)

A

121KIAS

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3
Q

Air Minimum Control (VMCA)

A

86KIAS

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4
Q

One-Engine Inoperative
Enroute Climb

A

121KIAS

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5
Q

Emergency Descent

A

181KIAS

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6
Q

One-engine-inoperative Landing —
Final Approach

A

103KIAS

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7
Q

Intentional One-Engine-
Inoperative (VSSE)

A

104KIAS

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8
Q

Maximum Range Glide

A

135KIAS

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9
Q

ENGINE FIRE ON GROUND

A
  1. Condition Lever ……………………….. FUEL CUTOFF
  2. Fuel Firewall Valve ………………………………. CLOSE
  3. Starter Switch ……………………….. STARTER ONLY
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10
Q

NACELLE FIRE ON GROUND

A
  1. Both Condition Levers ……………… FUEL CUTOFF
  2. Both Propeller Levers ……………………….FEATHER
  3. Both Fuel Firewall Valves ……………………. CLOSE
  4. Fire Extinguisher (if installed) ………………….PUSH
    (for affected engine)
  5. Master Switch …………………OFF (Gang bar down)
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11
Q

INTENTIONAL ENGINE SHUTDOWN IN FLIGHT
UNSCHEDULED TORQUE INCREASE
CONFIRMED ENGINE FIRE OR EXPLOSION IN FLIGHT

A

Affected Engine:
1. ACTUATE (if required)
Condition Lever………………………..FUEL CUTOFF
2. Propeller Lever…………………………………FEATHER Fuel Firewall Valve……………………………… CLOSE
Fire Extinguisher (if installed)…………………………..ACTUATE (if required)

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12
Q

SUSPECTED POWER LOSS IN FLIGHT

A
  1. Both Power Levers ………………………….. INCREASE AS REQUIRED
  2. Both Propeller Levers…………….. FULL FORWARD
  3. Flaps……………………….CONSIDER (UP, if in doubt)
  4. Gear ………………………..CONSIDER (UP, if in doubt)
  5. Identify & Verify Inoperative Engine.
    For Affected Engine:
  6. Propeller Lever………………………………..FEATHER
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13
Q

ENGINE FAILURE DURING TAKEOFF — TAKEOFF ABORTED

A
  1. Power Levers ………………………………….. REVERSE
  2. Brakes…………………. MAXIMUM (or as required to achieve stopping distance)
    If insufficient runway remains for stopping:
  3. Both Condition Levers ……………… FUEL CUTOFF
  4. Both Fuel Firewall Valves …………………….. CLOSE
  5. Master Switch …………………OFF (Gang bar down)
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14
Q

ENGINE FAILURE DURING TAKEOFF — TAKEOFF CONTINUED

A
  1. Power……………….CHECK (increase if necessary)
    (Propeller Levers — VERIFY FULL FORWARD)
  2. Landing Gear ………………………………………………UP (when positive climb is established)
  3. Airspeed ………………………………..MAINTAIN AT V2
  4. Identify & Verify Inoperative Engine.
  5. Propeller Lever (inop engine)…………….FEATHER
  6. Airspeed ………………ACCELERATE TO 121 Knots
    (at 400 feet AGL minimum)
  7. Flaps …………………………………………………………..UP
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15
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 pitch attitude to accelerate above Vmca.
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16
Q

ENGINE FLAMEOUT (2nd Engine)

A
  1. Propeller ……………………………. DO NOT FEATHER
  2. Engine Auto-Ignition ………………. VERIFY ARMED
  3. Condition Lever ……………………………… HIGH IDLE
  4. Fuel Panel……………………………..VERIFY NORMAL
17
Q

FUEL PRESSURE LOW
(L or R FUEL PRESS Annunciator)

A
  1. Standby Pump (affected side) …………………….. ON
18
Q

ELECTRICAL SMOKE OR FIRE

A
  1. Oxygen
    a. Oxygen Supply Control Handles (2) …………… PULL BOTH
    b. Crew ……………………….. REMOVE HEADSETS, DON MASKS (100% POSITION) (Use purge button as required, if installed)
    c. Audio Speaker(s) …………………………………. ON
    d. Mic Selector Sw………………… OXYGEN MASK
    e. Passengers………………. PULL LANYARD PIN, DON MASKS
  2. Cabin Temp Mode Selector ………………………. OFF
  3. Vent Blower, Aft Blower,
    Radiant Heat Switches……………AUTO, OFF, OFF
  4. Windshield Anti-Ice Switches …………………… OFF
19
Q

ENVIRONMENTAL SMOKE OR FUMES

A
  1. Oxygen
    a. Oxygen Supply Control Handles (2) …………… PULL BOTH
    b. Crew ……………………….. REMOVE HEADSETS, DON MASKS (100% POSITION) (Use purge button as required, if installed)
    c. Audio Speaker(s) …………………………………. ON
    d. Mic Selector Sw………………… OXYGEN MASK
    e. Passengers………………. PULL LANYARD PIN, DON MASKS
  2. Cabin Temp Mode Selector ………………………. OFF
  3. Vent Blower Switch ………………………………….HIGH
  4. Left Bleed Air Valve Switch ……………. ENVIR OFF
20
Q

EMERGENCY DESCENT

A
  1. Power Levers ………………………………………….. IDLE
  2. Propeller Levers …………………… FULL FORWARD
  3. Flaps ……………… APPROACH (200 kts maximum)
  4. Landing Gear …………..DOWN (181 kts maximum)
  5. Airspeed ………………………. 181 KNOTS MAXIMUM
21
Q

GLIDE

A
  1. Both Propeller Levers ……………………….FEATHER
  2. Flaps …………………………………………………………..UP
  3. Landing Gear ………………………………………………UP
  4. Airspeed ……………………………………….. 135 KNOTS
22
Q

INVERTER FAILURE (INVERTER Annunciator
or torque gauges inoperative)

A
  1. Inverter Switch ……………………………. SELECT THE OTHER INVERTER (Flight Director/Autopilot modes will likely need to be re-selected.
23
Q

DUAL GENERATOR FAILURE
(L DC GEN and R DC GEN Annunciators)

A

DUAL GENERATOR FAILURE
(L DC GEN and R DC GEN Annunciators)
1. Gen. Switches ……………….. OFF, RESET, then ON
If either generator will reset:
2. Do not exceed 1.0 (100%) load on the operating generator.
If neither generator will reset:
2. Remaining unnecessary equipment ………….. OFF
3. Land at the nearest suitable airport.

24
Q

UNSCHEDULED ELECTRIC TRIM ACTIVATION

A
  1. Airplane Attitude………………………………MAINTAIN
    (using elevator control)
  2. Control Wheel Disconnect Switch ……………………. DEPRESS FULLY AND RELEASE
  3. Manually retrim the airplane.
  4. ELEV TAB Switch (if installed)………………….. OFF
25
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A

Rudder Boost Switch ………………………………………. OFF

26
Q

USE OF OXYGEN

A
  1. Oxygen
    a. Oxygen Supply Control Handles (2) …………… PULL BOTH
    b. Crew ……………………….. REMOVE HEADSETS, DON MASKS (100% POSITION) (Use purge button as required, if installed)
    c. Audio Speaker(s) …………………………………. ON
    d. Mic Selector Sw………………… OXYGEN MASK
    e. Passengers………………. PULL LANYARD PIN,
    DON MASKS
27
Q

PRESSURIZATION LOSS (ALT WARN Annunciator)

A
  1. Oxygen ……………….AS REQUIRED (See Page E8)
  2. Descent……………………………………. AS REQUIRED
28
Q

BLEED AIR FAIL
(L or R BL AIR FAIL Annunciator)

A
  1. Bleed Air Valve Switch (affected engine)………….. INST & ENVIR OFF
29
Q

EMERGENCY EXIT

A

Escape Hatch Handle …………………………………….. PULL

30
Q

PROPELLER OVERSPEED

A
  1. If the propeller speed stabilizes at approximately 2080 RPM, do not exceed 1800 ft-lbs of torque.