3. Emergency Procedures - AI Cards Flashcards

1
Q

How should a pilot respond to an ENGINE OUT/low rotor RPM warning?

A

The pilot should respond immediately by adjusting collective to maintain rotor RPM within limits and then check engine instruments and other indications to confirm engine trouble.

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2
Q

What actions should a pilot take if experiencing engine failure while cruising at 500 feet AGL or above?

A

The pilot should adjust collective pitch to maintain rotor speed, apply pedal pressure to control yaw, and adjust cyclic control to manage airspeed and flight path.

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3
Q

Explain the relationship between torque and yaw during an engine failure.

A

The amount of yaw during an engine failure is dependent on the amount of torque at the moment of power loss; high torque causes a large yaw, while low torque results in a smaller yaw.

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4
Q

What is the minimum rate of descent with power off in a helicopter?

A

The minimum rate of descent with power off will be attained at 60 KIAS and 410 NR.

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5
Q

How can a pilot extend glide distance during an engine out situation?

A

A pilot can extend glide distance by operating at 80 KIAS and maintaining 410 NR.

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6
Q

What should a pilot do after confirming a complete loss of power?

A

The pilot should place the twistgrip in cutoff, close the fuel shutoff valve, select a landing area, and maneuver as required.

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7
Q

Describe the procedure for restoring rotor RPM during an autorotation.

A

To restore rotor RPM during an autorotation, the pilot should lower collective prior to flare out.

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8
Q

Describe the procedure for landing after an engine failure above 12 feet AGL.

A

Flare as required to reduce forward speed and rate of descent, level the aircraft before ground contact, and touch down in a level attitude while increasing collective pitch to cushion landing. Avoid aft cyclic or rapid lowering of collective pitch during initial ground contact.

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9
Q

How should a pilot respond to a power failure during takeoff or low-level flight?

A

The collective pitch must be initially lowered to maintain rotor speed. The amount and duration of collective reduction depend on the airspeed and height above the ground at which the power loss occurs.

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10
Q

What actions should be taken during an engine failure while hovering below 12 feet AGL?

A

Do not reduce collective pitch, apply right pedal to prevent yawing, and increase collective pitch as necessary to cushion landing.

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11
Q

Define the indications of partial power loss in the engine.

A

Under partial power conditions, the engine may operate smoothly with reduced power or erratically with intermittent surges of power.

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12
Q

What should a pilot do if the engine operates erratically during partial power loss?

A

Turning the start pump ON may smooth out the erratic operation and/or restore power, enabling the pilot to fly to a favorable landing area. However, the need to land should not be disregarded.

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13
Q

Describe the conditions under which a pilot should not attempt an engine restart.

A

Do not attempt a restart if a malfunction is suspected, at low altitude, or when time is critical.

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14
Q

Explain the procedure for attempting an engine restart when altitude and time permit.

A

Close the twist grip to cutoff position, press the start/ignition button immediately, and if N1 is 18 percent or above, open the twist grip to ground idle. Maintain safe autorotational airspeed.

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15
Q

What is the recommended N1 speed range for the coolest and fastest engine restarts?

A

N1 speeds of 25 to 40 percent are preferred for the coolest and fastest restarts.

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16
Q

Describe the indications of low rotor speed in a helicopter.

A

The indications of low rotor speed include the red ENGINE OUT warning indicator being ON, an audible warning in the headset, a drop in rotor RPM, and a change in noise level.

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17
Q

Explain the conditions that can lead to low rotor RPM.

A

Low rotor RPM can be associated with engine failure, transient rotor droop during large, rapid increases in power, or governor failure producing an underspeed.

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18
Q

How should a pilot respond to a low rotor RPM warning?

A

Adjusting the collective to maintain rotor RPM within limits and check other caution/warning indicators and engine instruments for engine trouble.

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19
Q

What actions should be taken if a fire occurs on the ground or after landing?

A

The engine should be shut down, crew and passengers evacuated, and firefighting should begin immediately. A ‘MAYDAY’ call should be made if possible.

20
Q

Describe the steps to ventilate the cabin during a smoke or fume incident.

A

Open cabin heat if the source of smoke is the cabin heat duct, open fresh air vent, and pilot/cabin door vents. If necessary, open the pilot’s door (airspeed below 130 KIAS) to expedite smoke and fume evacuation.

21
Q

How should a pilot respond to a cabin fire while still airborne?

A

The use of a fire extinguisher on a cabin fire while airborne is not recommended and should only be considered after all other means to extinguish and control the fire have been tried. The pilot’s first responsibility is to fly the helicopter and land immediately.

22
Q

Define the procedure for handling an engine fire during starting.

A

To extinguish an engine fire during start, twist the grip to shut off fuel, cut off the motor until the temperature is below 150°C, and pull to close the fuel shut-off valve.

23
Q

What actions should be taken if an engine fire occurs during flight at low altitude?

A

Land immediately, twist the fuel shutoff valve, cut off the battery/external power switch, and evacuate passengers and crew as soon as the helicopter is on the ground.

24
Q

How should a pilot handle an engine fire during flight at high altitude?

A

Consider prevailing circumstances such as altitude, available landing areas, and confirmation of engine fire to determine whether to execute a power-on approach or a power-off autorotational descent.

25
How should a pilot respond to a malfunctioning fuel control or power turbine governor producing an overspeed?
Indications include instrument needle fluctuation and sudden increases in engine torque, TOT, N1, and N2/NR. Increase collective to load the main rotor and roll the twist grip toward ground idle until control of N2 speed is obtained.
26
Define the actions to take if an engine fuel control system malfunctions and produces an overspeed.
Close the twistgrip to CUTOFF and make an autorotational landing. Immediate pilot action is necessary due to potential increases in engine torque, TOT, N2, and rotor RPM.
27
What should a pilot do if experiencing an underspeed condition?
Lower collective to maintain rotor RPM in the green (410-523) and attempt level flight at 60 knots IAS. If power is insufficient, make an autorotational landing.
28
Explain the procedure for handling a power turbine governor surge.
N2 fluctuating indicates the governor is not maintaining pre-set speed. Turning the start pump ON may allow the engine to operate smoothly. Control N2 manually with the twistgrip (102% to 103% N2).
29
Describe the effect of power application on the nose of the aircraft during an anti-torque emergency.
The nose of the aircraft will turn right with power application.
30
Explain the procedure for a complete loss of thrust during forward flight.
Reduce power by lowering collective, adjust airspeed between 50 to 60 knots, and use left lateral cyclic in combination with collective pitch to limit left sideslip.
31
Describe the procedure for anti-torque failure with a fixed tail rotor pitch setting.
Adjust power to maintain 50 to 60 knots airspeed and perform a shallow approach and running landing into wind.
32
What is the indication of a one-way lock failure in the cyclic control system?
Aft feedback in the cyclic at high airspeed or higher than normal forces required to move the cyclic longitudinally.
33
Explain the procedure to follow if the one-way lock has a push rod shaft or check valve seizure.
Reduce airspeed to 100 KIAS or less and limit cyclic movement to those required to safely fly the helicopter.
34
What should a pilot do if they experience cyclic trim failure?
The pilot should land the helicopter immediately if their physical condition or strength is compromised.
35
How can directional control be maintained during an anti-torque failure?
Directional control may be accomplished by small adjustments in throttle and/or collective control.
36
What is the recommended landing speed during an anti-torque failure?
Touch down at a speed between effective translational lift and 30 knots.
37
Describe the procedure to follow when the trim motor fails to respond to the cyclic trim switch.
Establish a safe flight condition that produces the least cyclic control force, typically straight and level at the last trimmed airspeed. Actuate the trim switch through all positions to attempt to restore trim capability. If restored, trim to a near neutral position and land as soon as practical.
38
Explain the actions to take if trim failure is determined in all directions.
If trim failure is in all directions and control of the helicopter can be maintained safely, check/reset the TRIM circuit breaker. Land as soon as practical if unable to re-establish full cyclic trim control.
39
How can cyclic stick forces be managed during a forward longitudinal runaway trim failure?
Cyclic stick forces may be reduced by maintaining higher airspeeds during a forward longitudinal runaway trim failure.
40
What should be done if an aft longitudinal runaway trim failure is experienced?
To reduce cyclic stick forces during an aft longitudinal runaway trim failure, maintain slower airspeeds.
41
What is the first action to take when the yellow FUEL FILTER indicator is on?
Turn on the start pump and continue flight.
42
What should be avoided when landing with a trim runaway to the full forward position?
When landing with a trim runaway to the full forward position, accomplish landing into the wind and do not hover downwind in winds exceeding 15 knots.
43
Describe the indications of a generator malfunction.
The yellow GEN OUT indicator is ON, and the ammeter indicates zero.
44
What steps should be taken if the GEN OUT indicator remains ON after resetting the generator switch?
Pull the generator circuit breaker OUT and ensure the generator switch is in the ON position for the remainder of the flight.
45
Explain the importance of the generator switch position during flight.
The generator switch must be in the ON position to enable the Engine Out/Low Rotor audio warning to function as required.