Autorotations/Simulated Engine Failure Procedures Flashcards

1
Q

When should SNA wave-off by when executing a simulated EP while away from suitable outlying fields (channel work/on the way to outlying fields…)?

A

By 300’ AGL and no slower than 50KIAS

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2
Q

When are simulated engine failures at altitude prohibited?

A
  • At gross weights above 2900 lbs
  • When dry DA exceeds 1800’
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3
Q

What are the limitations on cut-guns?

A
  • Should only be executed when aircraft HDG is within 45° of the windline
  • Shall not be conducted when gross weight exceeds 2900 lbs
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4
Q

What are the limits for practice autorotations?

A
  • Winds must not be less than 5kts
  • Dry DA cannot exceed 2500’
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5
Q

Required build-up maneuvers prior to a power-recovery autorotation:

A
  1. Sliding landing
  2. Hover cut-gun
  3. Taxi cut-gun
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6
Q

Required build-up maneuvers prior to a full (power-off recovery) autorotation:

A
  1. Power recovery autorotation
  2. Power recovery autorotation followed by a simulated engine failure in a hover taxi
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7
Q

Practice Autorotation Entry Parameters (Altitude)

A

For a 90° Auto:
* 600’ AGL

For a 180° Auto:
* 700’ AGL

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8
Q

Fuel requirements for practice full autorotation:

A

Fuel load shall be 45gal or less (for a TH-57B)

Fuel load shall be 40gal or less (for a TH-57C)

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9
Q

Required wave-off criteria for practice autorotations:

A
  1. Airpseed falls below 55 KIAS prior to the 100’ gate
  2. Either crewmember misses a required callout below 200’ AGL
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10
Q

Practice Autorotation Set-Up Parameters

A

“Lane”
* Ensure that 90 or 180 auto lane is clear of obstacles

“Lock”
* Lock the shoulder harness

“Sock”
* Check the windsock to ensure that there is no tailwind component

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11
Q

Practice Autorotation Entry Parameter Procedure

A
  • “600’ & 70KIAS”
  • “VSI at or below zero”
  • “Aircraft in trim”
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12
Q

Practice Autorotation/Simulated Engine Failure Entry Procedure

A

“Down”
* Smoothly lower collective to full down in no less than two seconds

“Right”
* Anticipate the need for right pedal

“Transition”
* Use cyclic to establish a 50-72 KIAS descending attitude

“Turn”
* Initiate a turn to courseline
* For a 180° auto, include “Over 1, Back 1” (for cyclic) and “Up 1” (for collective)

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13
Q

What are the desired airspeed and Nr ranges?

A
  • 50-60 KIAS (We want 60KIAS)
  • 94-95% Nr is optimal but maintain between 90-107% Nr
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14
Q

Autorotation/Simulated Engine Failure Scan Procedure

A

Attitude
* Trim to maintain 50-60 KIAS (We want 60 KIAS)

Nr
* Use collective to maintain Nr between 90-107% Nr

Ball
* Keep the ball centered

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15
Q

What are the required callout gates?

A

Three: 200’ AGL, 150’ AGL, 100’ AGL

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16
Q

200’ AGL Callout Procedure

A

“200’ on course-line”

Ensure that you’re wings level (or you have the proper crosswind input) and on course-line

17
Q

150’ AGL Callout Procedure

A

“150’ collective full down”

Ensure that the collective is full down

18
Q

100’ AGL Callout Procedure

A

“100’ flare”

At 75-100’ AGL, apply aft cyclic to flare to reduce the rate of descent, reduce groundspeed, and increase Nr

19
Q

What do you do after the 100’ AGL callout gate?

A

Confirm the position of the twist grip

20
Q

Power Recovery Twist Grip Confirmation Procedure

A

“Twist grip full open.”

  • The PNAC will confirm the position w/ “Roger, twist grip full open”
21
Q

Power-Off Twist Grip Confirmation Procedure

A

“Twist grip flight idle.”

  • The PNAC will confirm the position w/ “Roger, twist grip flight idle.”
22
Q

Practice Autorotation Landing Procedure

A

“10-15’, pull”
* Increase collective to arrest rate of descent

“Pause”
* Pause momentarily to slow groundspeed to 0 10 10kts

“Level”
* Apply forward cyclic to achieve a 5ft. level skid attiude w/ nose aligned in the direction of travel

Power-On Recovery:
“Taxi, Taxi, Taxi”

Power-Off Recovery:
“Cushion, Cushion, Cushion”

23
Q

For a simulated engine failure, what do you call for after entry into the maneuver?

A

“Lock”
Lock shoulder harness

“Talk”
PNAC simulates mayday call

“Squawk”
PNAC simulates sqauwking 7700

“Restart”
PNAC simulates excuting engine restart in flight procedure