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AEL Recurrent > Bell 206L4 Emergency Procedures > Flashcards

Bell 206L4 Emergency Procedures Flashcards

1
Q

B206
What failure is indicated by the following:
1 - Left Yaw
2 - ENG OUT light illuminated
3 - Engine instruments indicate power loss
4 - Engine out audio
5 - NR decreasing
6 - ROTOR LOW RPM light and audio activated

A

Engine Failure

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2
Q

B206
What are the 6 possible indications of an engine failure?

A

1 - Left Yaw
2 - ENG OUT light illuminated
3 - Engine instruments indicate power loss
4 - Engine out audio
5 - NR decreasing
6 - ROTOR LOW RPM light and audio activated

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3
Q

B206
What is the max autorotational airspeed?

A

100 KIAS

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4
Q

B206
What is the minimum rate of descent autorotational airspeed?

A

52 KIAS

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5
Q

B206
What is the maximum glide distance airspeed?

A

69 KIAS

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6
Q

B206
What is the nominal autorotative airspeed?

A

61 KIAS

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7
Q

B206
During an autorotational landing, touchdown should be made prior to passing through what rotor RPM?
During the touchdown what should be avoided?

A

70%
On ground contact, smoothly reduce collective pitch with neutral cyclic.
Avoid holding collective up during ground run or floating for long distances.

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8
Q

B206
~~~
What failure is indicated by the following:
1 - Decrease in N1
2 - Subsequent decrease in N2
3 - Possible decrease in Nr
4 - Decrease in TORQUE
~~~

A

Engine Underspeed

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9
Q

B206
What are the 4 indications of an Engine Underspeed?

A

1 - Decrease in N1
2 - Subsequent decrease in N2
3 - Possible decrease in Nr
4 - Decrease in TORQUE

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10
Q

B206
Engine Underspeed Procedure?

A

1 - Collective - Adjust for 90-107% Nr
2 - Throttle - confirm full open
3 - If unable to maintain Nr, establish autorotative glide
4 - Prepare for power off landing

NOTE: If engine underspeeds but continues to operate, do not shutdown engine. This will help maintain tail rotor effectiveness and assist to cushion the landing.

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11
Q 
What failure is indicated by the following:
1 - Increase in Nr
2 - Increase in N2
3 - Increase in N1
4 - Increase in TORQUE
A

Engine Overspeed

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12
Q

B206
What are the 4 indications of an Engine Overspeed?

A

1 - Increase in Nr
2 - Increase in N2
3 - Increase in N1
4 - Increase in TORQUE

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13
Q

B206
Procedure for Engine Overspeed?

A

1 - Throttle - Retard
2 - N1 or N2/Nr - Attempt to stabilize with throttle and collective
3 - TOT - monitor for normal operation
4 - Nr - Maintain 90 - 107% with throttle/collective

If pilots elects to shutdown engine:
5 - Enter autorotation
6 - Throttle - closed
7 - FUEL VALVE switch - OFF
8 - Accomplish auto descent & landing

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14
Q 
What failure is indicated by the following:
1 - Engine pops
2 - High or erratic TOT
3 - Decreasing or erratic N1 or N2
4 - TORQUE oscillations
A

Engine Compressor Stall / Surge

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15
Q

B206
What are the 4 indications of an Engine Compressor Stall / Surge?

A

1 - Engine pops
2 - High or erratic TOT
3 - Decreasing or erratic N1 or N2
4 - TORQUE oscillations

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16
Q

B206
Engine Compressor Stall / Surge Procedure?

A

1 - Collective - Reduce power, maintain slow cruise flight
2 - TOT & N1 - Check for normal indications
3 - ENGINE ANTI-ICING switch - ON
4 - PARTICLE SEP PRG switch - ON (if installed)
5 - HEATER switch - ON (if installed)

If pilot elects to continue flight:
6 - Collective - increase slowly to desired power
7 - TOT & N1 - monitor for normal response
8 - Land as soon as practical

If pilot elects to shut down engine:
9 - Enter autorotation
10 - Throttle - Closed
11 - Fuel Valve switch - OFF
12 - Accomplish Auto

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17
Q

Engine Hot Start / Shutdown Procedures?

A

1 - Throttle - Closed
2 - FUEL VALVE switch - OFF
3 - STARTER button - Press to motor engine until TOT stabilizes at normal temperature
4 - Complete helicopter shutdown

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18
Q

Engine oil pressure below minimum procedure?

A

1 - Monitor engine oil pressure and temperature

2 - Land as soon as possible

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19
Q

B206
Engine oil pressure above max or fluctuating abnormally procedure?

A

1 - Monitor engine oil pressure and temperature

2 - Land as soon as practical

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20
Q

B206
Engine oil temp increasing above normal OR temp above maximum procedure?

A

Land as soon as practical

21
Q 
What failure is indicated by the following:
1 - Left yaw
2 - Rapid decrease in Nr
3 - Rapid increase in N2
4 - ROTOR LOW RPM audio horn
5 - Illumination of ROTOR LOW RPM light
6 - Possible increase in noise level
A

Driveshaft Failure

22
Q

B206
What are the 6 possible indications of a driveshaft failure?

A 
1 - Left yaw
2 - Rapid decrease in Nr
3 - Rapid increase in N2
4 - ROTOR LOW RPM audio horn
5 - Illumination of ROTOR LOW RPM light
6 - Possible increase in noise level due to overspeeding engine and driveshaft breakage
23
Q

B206
Driveshaft Failure Procedures?

A

1 - Accomplish autorotative descent & landing
2 - Complete helicopter shutdown

NOTE - To maintain tail rotor effectiveness, do not shutdown engine.

24
Q

B206
Engine Fire on the Ground Procedure?

A 
1 - Throttle - Closed
2 - FUEL VALVE switch - OFF
3 - BAT switch - OFF
4 - Rotor Brake - Engage
5 - Exit helicopter
25
Q

B206
Engine Fire in Flight Procedures?

A

1 - Immediately enter autorotation
2 - Throttle - Closed
3 - FUEL VALVE switch - OFF
4 - If time permits, LEFT/RIGHT BOOST circtuit breakers - Pull out
5 - Accomplish auto descent and landing
6 - BAT switch - OFF

26
Q

B206 Cabin Smoke Procedures?

A

1 - In flight - Start descent
2 - HEATER switch - OFF
3 - All vents - Open
4 - Side windows - Open
If time and altitude permits:
5 - Source - Attempt to identify and secure
6 - If source is ID’ed and smoke persists - Land as soon as possible
7 - If source is ID’ed and smoke is cleared - Land as soon as practical

27
Q

What failure is indicated by the following:
1 - Uncontrollable yawing to the right (left sideslip)
2 - Nose down tucking
3 - Possible roll of fuselage

A

Complete Loss of Tail Rotor Thrust

28
Q

What are the 3 indications of a Complete Loss of Tail Rotor Thrust

A

1 - Uncontrollable yawing to the right (left sideslip)
2 - Nose down tucking
3 - Possible roll of fuselage

NOTE - Severity of initial reaction of helicopter will be affected by AIRSPEED, CG, power being used, and Density Altitude

29
Q

Complete Loss of Tail Rotor Thrust Procedure?

A

Reduce throttle to idle
Immediately enter autorotation
Maintain minimum Airspeed of 52 KIAS during descent

30
Q

In the event of a Complete Loss of Tail Rotor Thrust, if a landing area is not immediately available, what do you do (NOTE from EP)?

A

NOTE
When a suitable landing site is not available, vertical fin may permit controlled flight at low power levels and sufficient airspeed. During final stages of approach, a mild flare should be executed, making sure all power to rotor is off. Maintain helicopter in a slight flare and smoothly use collective to execute a soft, slightly nose-high landing. Landing on aft portion of skids will tend to correct side drift. This technique will, in most cases, result in a run-on type landing.

31
Q

What failure is indicated by the following:
1 - Lack of directional response
2 - Locked pedals

A

Fixed Pitch Failure

32
Q

What are the 2 indications of a Fixed Pitch Failure?

A

1 - Lack of directional response

2 - Locked pedals

33
Q

Fixed Pitch Failure at a Hover procedure and considerations?

A

Do not close throttle unless a severe right yaw occurs. If pedals lock in any position at a hover, landing from a hover can be accomplished with greater safety under power-controlled flight rather than by closing throttle and entering autorotation.

34
Q

B206
Fixed Pitch Failure in flight - Left Pedal Applied procedures and considerations?

A

Helicopter will yaw left when power is reduced.
Adjust airspeed for comfortable yaw.
At higher airspeeds, vertical fin may increase left yaw
Establish power-on approach with sufficiently low airspeed.
Attain rate of descent with comfortable sideslip.
A decrease in N2 will decrease tail rotor thrust.
As collective is increased just before touchdown, left yaw will be reduced.

35
Q

B206
Fixed Pitch Failure in flight - Right Pedal Applied procedures and considerations?

A

Helicopter will yaw right when power is increased.
Low power run-on type landing will be necessary.
For touchdown, gradually reduce throttle for heading while adding collective for cushion. If right yaw becomes excessive, close throttle.

36
Q

B206
What failure is indicated by the following:
1 - Grinding or howling noise from pump
2 - Increase in force required to move flight controls
3 - Feedback forces may be evident during flight control movement
4 - Cyclic and collective movements are rate limited

A

Loss of Hydraulic Pressure

37
Q

B206
What are the 4 indications of a Loss of Hydraulic Pressure?

A

1 - Grinding or howling noise from pump
2 - Increase in force required to move flight controls
3 - Feedback forces may be evident during flight control movement
4 - Cyclic and collective movements are rate limited

38
Q

B206
Loss of Hydraulic Pressure Procedure?

A

1 - Airspeed - Reduce to 60-80 KIAS
2 - HYDR SYSTEM CB - Out. If hydraulics not restored - In
3 - HYDRAULIC SYSTEM switch - ON; OFF is hydraulic power is not restored
4 - Land as soon as practical
5 - A run-on landing at appx 9 KIAS is recommended

39
Q

What failure is indicated by the following:
1 - Uncommanded flight control inputs
2 - High flight control forces to oppose movement in one axis
3 - Feedback forces only in affected flight control axis
4 - Flight control forces normal in unaffected axis.

A

Flight Control Actuator Malfunction

40
Q

What are the 4 indications of a Flight Control Actuator Malfunction?

A

1 - Uncommanded flight control inputs
2 - High flight control forces to oppose movement in one axis
3 - Feedback forces only in affected flight control axis
4 - Flight control forces normal in unaffected axis.

41
Q

B206
Flight Control Actuator Malfunction Procedure?

A

1 - Attitude - Maintain
2 - HYDRAULIC SYSTEM switch - OFF
3 - AIRSPEED - 60 to 80 KIAS
4 - Land as soon as Possible using Loss of Hydraulic Pressure Procedure.

42
Q

B206
What failure is indicated by the following:
1 - GEN FAIL light illuminated
2 - DC loadmeter indicates 0% LOAD

A

GENERATOR FAILURE

43
Q

What are the 2 indications of a Generator Failure?

A

1 - GEN FAIL light illuminated

2 - DC loadmeter indicates 0% LOAD

44
Q

Generator Failure Procedure?

A

1 - GEN FIELD and GEN REST CBs - Check In
2 - GEN switch - RESET; then GEN
3 - If power is not restored, place GEN switch to OFF
4 - Land as soon as practical

45
Q

B206
With all electrical equipment off, how long will an 80% charged battery operate the left fuel boost pump?

A

3 hours.

For night operations, appx 1 hour of battery power will be available.

46
Q

What failure is indicated by the following:
1 - DC loadmeter indicates excessive load
2 - Smoke or fumes

A

Excessive Electrical Load

47
Q

What are the 2 indications of an Excessive Electrical Load?

A

1 - DC loadmeter indicates excessive load

2 - Smoke or fumes

48
Q

Excessive Electrical Load Procedure?

A

1 - GEN switch - OFF
2 - BAT switch - OFF
3 - LEFT FUEL BOOST CB - Check in
4 - Land as soon as practical

49
Q

B206
In the event of an electrical failure, what are your considerations if the battery depletes and is no longer operating the LEFT BOOST PUMP?

A

Prior to battery depletion, altitude SHALL be reduced to below 6000 ft. PA. Once battery is depleted, unusable fuel may be as high as 86.3 pounds.

AEL Recurrent (9 decks)

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