EPs Flashcards

1
Q

Engine Failure after Takeoff

A

*1. Power — Maximum allowable.
*2. Gear — UP.
3. Airspeed — Accelerate to Vxse or Vyse.
4. Propeller (inoperative engine) — Confirm auto feather or FEATHER (PM).
*5. Flaps — UP.
*6. Emergency Shutdown Checklist — Perform.

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2
Q

(N/W/C) Engine Failure after Takeoff

A

• Maximum climb performance can be achieved by raising the failed engine 3
to 5° up and displacing the slip skid indicator one-half to three-quarters of a ball width toward the good engine.
• If the auto feather system is being used, retarding the POWER lever below
approximately 90 percent N1 before the feathering sequence is complete will deactivate the auto feather circuit and prevent automatic feathering.

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3
Q

Aborted Takeoff

A

*1. POWER levers — IDLE/REVERSE as required.
*2. Brakes — As required.

Prior to departing the prepared surface:
*3. CONDITION levers — FUEL CUTOFF (PM).
*4. PROP levers — FEATHER (PM).

After aircraft stops:
*5. Firewall valves — CLOSED.
*6. Engine fire extinguisher — As required (PM).
*7. AUX BATT switch — OFF.
*8. Gangbar — Off.

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4
Q

(N/W/C) Aborted Takeoff

A

In the event of a malfunction affecting the ability to control engine power,
bringing the POWER levers to IDLE prior to cutting off fuel may accentuate
yaw and result in departure from the runway. In this case, consideration
should be given to moving both CONDITION levers to FUEL CUTOFF
prior to reducing POWER levers.

Single-engine reversing must be applied cautiously or loss of directional
control may result. Use extreme caution if takeoff surface is not hard and dry.

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5
Q

Abnormal Start

A

*1. CONDITION lever — FUEL CUTOFF (note ITT decrease).
*2. ENGINE START switch — OFF.

In the event of a hot start or a hung start:
*3. ENGINE START switch — STARTER ONLY (for the remainder of the 40 seconds).

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6
Q

Emergency Shutdown on Deck

A

*1. Aircraft — Stop.
*2. Parking brake — Set.
*3. CONDITION lever(s) — FUEL CUTOFF (PM).

In case of fire, fuel leak, or at TPC discretion
*4. PROP levers — FEATHER (PM).
*5. Firewall valves — CLOSED.
*6. Engine fire extinguisher — As required (PM).

*8. AUX BATT switch — OFF.
*9. Gangbar — Off.

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7
Q

Emergency Shutdown Checklist

A

1. CONDITION lever — FUEL CUTOFF (PM).
2. PROP lever — FEATHER (PM).
3. Firewall valve — CLOSED (LS).
4. Engine fire extinguisher — As required (PM).

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8
Q

Engine Fire

A

*1. Confirm fire.
If fire exists:
*2. Emergency Shutdown Checklist — Perform.

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9
Q

Fire/Smoke/Fumes (Electrical Source Suspected)

A

*1. Oxygen masks — Don/deploy (crew 100 percent) (both/TA).

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10
Q

Fire/Smoke/Fumes (Environmental Source Suspected)

A

*1. Oxygen masks — Don/deploy (crew 100 percent) (both/TA).

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11
Q

Fuselage Fire

A

*1. Oxygen masks — Don/deploy (crew 100 percent) (both/TA).

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12
Q

Primary Governor Failure/Malfunction

A

*1. PROP lever – Attempt to adjust to normal operating range.

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13
Q

Explosive Decompression

A

*1. Oxygen masks — Don/deploy (crew 100 percent) (both/TA) (if above 10,000 feet).
*2. Descend — As required.

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14
Q

Emergency Descent

A

*1. POWER levers — IDLE.
*2. PROP levers — Full forward.
*3. FLAPS — As required.
*4. Landing gear — As required.
*5. Airspeed — As required.

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15
Q

Spin Recovery

A

*1. POWER levers — IDLE.
*2. Ailerons — Neutralize.
*3. Control Wheel — Rapidly move forward.
*4. Rudder — Full deflection opposite the direction of the spin.
*5. Rudder — Neutralize once rotation has stopped.
*6. Execute a smooth pullout.

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16
Q

Windshear Escape Procedure/Terrain Warning

A

*1. Autopilot — Disengage.
*2. Power — Maximum.
*3. Wings — Level.
*4. PROP Levers — Full Forward.
*5. Pitch — Rotate toward 15 degrees up.
*6. Configuration — Do not change.

17
Q

Single-Engine Waveoff/Missed Approach

A

*1. Power — Maximum allowable.
*2. PROP lever – Full Forward.
*3. Pitch — Establish positive rate of climb (7 to 10° up).
*4. Airspeed — VXSE or VYSE.
*5. Gear — UP.
*6. Flaps — UP.

18
Q

NAC LOW L/R

A

*1. Land as soon as possible.

19
Q

Prohibited Maneuvers

A
  1. Abrupt control movement.
  2. Unusual g loading.
  3. Bank angle greater than 60° (normal category).
  4. Bank angle greater than 35° (restricted category).
  5. Pitch attitude more than 30° above or below the horizon.
  6. Intentional spins.
20
Q

BL AIR FAIL L/R (n/w/c)

A

The first indication of a ruptured
bleed air line in the engine
compartment will be a reduction of
engine power possibly followed by
fire. This cannot be remedied by
securing the BLEED AIR VALVES
switch. Consideration should be
given to reducing engine power or
securing the engine if it cannot be
determined that the bleed air valve
closed. This type of failure will
not cause the BL AIR FAIL light to
illuminate.