SFAR 73 Flashcards

You may prefer our related Brainscape-certified flashcards:
1
Q

SFAR 73 Awareness Training applies to the following helicopters

A
  • Robinson R22
  • Robinson R44

  1. Applicability “SFAR applies to all persons who seek to manipulate the controls or act as pilot in command of a Robinson model R-22 or R-44 helicopter.”
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2
Q

True or False

SFAR 73 Awareness Training is required prior to anyone manipulating R22 or R44 flight controls, UNLESS it is just a quick ‘demo flight’ (with only a few minutes of the prospective student touching the controls) and so not a ‘proper’ flight lesson.

A

False

  1. Awareness Training
    “ no person may manipulate the controls of a Robinson model R-22 or R-44 helicopter . . . for the purpose of flight unless the awareness training . . . is completed”
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3
Q

True or False

SFAR 73 Awareness Training requires an endorsement.

A

True

  1. (a)(1) “and the person’s logbook has been endorsed by a certified flight instructor”
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4
Q

You can find the full SFAR 73 regulation

A

At the start of Part 61 of the FAR/AIM

SFAR 71 is found at the start of Part 61 of the FAR/AIM or on the Federal Regulations website under
Title 14 → Chapter I → Subchapter D → Part 61 → Appendix

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5
Q

True or False

Anyone can give SFAR 73 Awareness Training, as long all the areas listed in SFAR 73 2. (a)(3) are covered and an endorsement is given.

A

False

  1. (a)(3)
    “Awareness training must be conducted by a certified flight instructor who has been endorsed under paragraph (b)(5) of this section”
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6
Q

True or False

SFAR 73 Awareness Training is good for both R22 and R44 and is not required to have an expiration date.

A

True

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7
Q

What are the subject areas to be covered by SFAR 73 Awareness Training?

A
  • Energy Management
  • Low G leading to Mast Bumping
  • Low Rotor RPM leading to Blade (Rotor) Stall

  1. (a)(3)
    Awareness training . . . consists of instruction in the following general subject areas:

(i) Energy management;
(ii) Mast bumping;
(iii) Low rotor RPM (blade stall); [*rotor stall]
(iv) Low G hazards; and
(v) Rotor RPM decay.

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8
Q

What is Low G?

A

When the rotor disk is temporarily unloaded, causing the pilot to feel light or weightless

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9
Q

What situations could cause a hazardous Low G situation?

A
  • Pilot abruptly pushing cyclic forward to level after a climb
  • Moderate or greater turbulence
  • Pilot rapidly pushing cyclic forward to follow falling terrain
  • Pilot suddenly pushing the cyclic forward to avoid a bird or other aircraft
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10
Q

Low G Pushovers or turbulence can lead to a rapid (100+ degrees a second) roll to the

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11
Q

To recover from an un-commanded, rapid (100+ degrees a second) roll caused by a Low G Pushover or turbulence, the pilot must immediately

A

Gradually apply aft cyclic

In hazardous Low G, the pilot must immediately apply gradual aft cyclic to restore positive G forces before applying any lateral cyclic to fix the roll.
See the R44 POH for more information and Robinson Helicopters Safety Notice 11 (SN-11) - Low-G Pushovers - Extremely Dangerous

12 / 30

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12
Q

True or False

Experienced airplane pilots are especially at danger from Low G Pushovers when flying the R22 and R44. They are more likely to instinctively push the cyclic forward to avoid a collision because that would be a ‘normal’ response in an airplane.

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13
Q

True or False

Low G can be demonstrated if done carefully.

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14
Q

When encountering turbulence, what can a pilot do to reduce the chance of hazardous Low G?

A
  • Reduce airspeed to 60 to 70 KIAS
  • Rest cyclic arm on thigh to avoid over-controlling

  • Mast bumping is less likely at lower airspeeds - slow to below normal cruise speed and if turbulence is significant slow to 60 to 70 KIAS
  • Do not over control, rest your arm on your thigh and allow the aircraft to go with the turbulence
  • Depart the area of turbulence if possible, else land as soon as practical.
    See more in Robinson Helicopter Safety Notice 32 (SN-32) - High Winds or Turbulence
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15
Q

True or False

Turbulence will likely be most severe on the downwind side of hills, ridges and tall buildings.

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16
Q

The helicopter is more susceptible to turbulence when the aircraft is

17
Q

In November 2016 Robinson Helicopters issued a Service Bulletin for both the R44 and R66 to add a yellow arc on the speed indicator from 110 to 130 or a placard for older aircraft. What is the yellow arc telling the pilot?

A

Only fly in the yellow arc in smooth air

  • 110 KIAS should only be exceeded in smooth air
  • Doors off limit is 100 KIAS (red and white barber pole)
  • 5 min takeoff power limit is 100 KIAS (red and white barber pole)
18
Q

In an R22, with the engine running, Low RPM is considered as soon as

A

RPM drops below the bottom of the green arc (below 101%)

19
Q

True or False

Low RPM Rotor Stall can happen at any airspeed.

20
Q

True or False

If the main rotor stalls due to low RPM, a pilot can easily recover by pushing forward with the cyclic, just like in an airplane.

A

False

If the main rotor stalls, there is a dramatic loss of lift and increase in drag. The increase in drag decreases the rotor RPM further. The loss of lift causes the helicopter to start to fall out of the sky, causing an uprush of airflow that increases the rotor stall further. At this point the situation is unrecoverable and often fatal. We MUST maintain rotor RPM!

Robinson Helicopters Safety Notice 24 (SN-24) - Low Rotor RPM Can Be Fatal

21
Q

Catastrophic (unrecoverable) rotor stall at 5,000’ MSL can happen if rotor RPM drops below

A

85%

Catastrophic (unrecoverable) rotor stall can happen if rotor RPM drops below 80%, plus 1% per 1,000 feet of altitude.
So 5,000 feet = 85% (80 %+ 5%)

See Section 4 of the R44 POH

22
Q

What can often cause Low Rotor RPM?

A
  • Incorrect RPM control in an autorotation
  • Rolling the throttle the wrong way (down instead of up)
  • ‘Over Pitching’ - pulling up too much collective
  • ‘Death Grip’ of the throttle
  • Slow or malfunctioning governor
  • Engine or transmission failure
23
Q

What are good indications of Low RPM?

A
  • Reduced engine/rotor noise
  • Increased descent rate
  • Increased vibration
  • Low RPM light and horn
24
Q

On recognizing Low RPM, the pilot should immediately

A

Simultaneously lower collective slightly while rolling throttle on

Section 3 of the R44 POH

25
Q

To recover from Low RPM in forward flight, in addition to the normal recovery procedure, the pilot can increase RPM by

A

Applying aft cyclic

Section 3 of the R44 POH

26
Q

True or False

If you have Low RPM and only lower collective, you may reduce the RPM further due to the correlator. You must roll throttle on at the same time.

A

True

27
Q

To maintain good power-on (engine running) energy management

A
  • Have a good grasp of current wind conditions that might affect performance
  • Use preflight planning to know IGE/OGE hover and power limits for the flight
28
Q

During an autorotation, does the air flow up or down through the main rotor system?

A

Up

29
Q

What are the 3 types of energy reserves we use in the event of an engine failure?

A
  • Airspeed
  • Rotor Inertia
  • Altitude

3 Forms of energy keep the rotor blades turning:

  • Altitude - potential energy - descent converts altitude to rotor RPMs \
  • Airspeed - potential energy - flare converts airspeed to rotor RPM
  • Rotor System Inertia* - maintains rotor RPM for a very short while…
    *(Inertia = something wants to keep moving until friction or other force…)
30
Q

Which of the following are examples of good energy management?

A
  • When possible, fly at least 60 KIAS
  • Keep the rotor RPM in the green
  • When possible, fly at least 500 feet above ground