Autorotations/Simulated Engine Failure Procedures Flashcards
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…)?
By 300’ AGL and no slower than 50KIAS
When are simulated engine failures at altitude prohibited?
- At gross weights above 2900 lbs
- When dry DA exceeds 1800’
What are the limitations on cut-guns?
- Should only be executed when aircraft HDG is within 45° of the windline
- Shall not be conducted when gross weight exceeds 2900 lbs
What are the limits for practice autorotations?
- Winds must not be less than 5kts
- Dry DA cannot exceed 2500’
Required build-up maneuvers prior to a power-recovery autorotation:
- Sliding landing
- Hover cut-gun
- Taxi cut-gun
Required build-up maneuvers prior to a full (power-off recovery) autorotation:
- Power recovery autorotation
- Power recovery autorotation followed by a simulated engine failure in a hover taxi
Practice Autorotation Entry Parameters (Altitude)
For a 90° Auto:
* 600’ AGL
For a 180° Auto:
* 700’ AGL
Fuel requirements for practice full autorotation:
Fuel load shall be 45gal or less (for a TH-57B)
Fuel load shall be 40gal or less (for a TH-57C)
Required wave-off criteria for practice autorotations:
- Airpseed falls below 55 KIAS prior to the 100’ gate
- Either crewmember misses a required callout below 200’ AGL
Practice Autorotation Set-Up Parameters
“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
Practice Autorotation Entry Parameter Procedure
- “600’ & 70KIAS”
- “VSI at or below zero”
- “Aircraft in trim”
Practice Autorotation/Simulated Engine Failure Entry Procedure
“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)
What are the desired airspeed and Nr ranges?
- 50-60 KIAS (We want 60KIAS)
- 94-95% Nr is optimal but maintain between 90-107% Nr
Autorotation/Simulated Engine Failure Scan Procedure
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
What are the required callout gates?
Three: 200’ AGL, 150’ AGL, 100’ AGL