Sport Flight Instructor - Helicopter, Simplified Flight ControlsFAA-S-ACS-31
Area of Operation XI
Emergency Operations
11 Tasks
Task A Powerplant Failure in a Hover in a Single-Engine Helicopter-Simplified Flight Controls
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands power failure in a ground effect hover, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
See Appendix 2: Safety of Flight.
Knowledge
Elements related to powerplant failure in a hover, including energy management concepts.
Effects of wind, weight, temperature, and density altitude.
High and low inertia of rotor systems, as applicable.
Aerodynamics associated with powerplant failure in a hover.
Proper orientation, division of attention, and proper planning.
Common errors related to this Task.
Risk Management
Powerplant failure in a hover.
Flight control inputs.
Aircraft movement.
Dynamic rollover.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Skills
Complete the appropriate checklist(s).
Make radio calls as appropriate.
Clear the area.
Select a suitable landing area.
Establish a stationary or forward hover into the wind.
Simulate powerplant failure.
Maintain a heading, ±10°, throughout the maneuver.
Touchdown with minimum sideward movement and no rearward movement.
Use appropriate simplified flight control inputs to cushion the touchdown.
After touchdown, lower collective or neutralize simplified flight controls, as applicable.
Analyze and correct common errors related to this Task.
Task B Powerplant Failure at Altitude in a Single-Engine Helicopter-Simplified Flight Controls
References
AC 61-140; FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands power failure at altitude, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
See Appendix 2: Safety of Flight and Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations for information related to this Task.
Knowledge
Elements of a powerplant failure at altitude.
Effects of wind, weight, temperature, and density altitude.
Main rotor (Nr) speed.
Energy management.
Causes and effects of high descent rates.
Effect of varying bank angles, airspeeds, and rotor rpm.
Common errors related to this Task.
Risk Management
Low entry altitudes.
Selection of landing area.
Flight control inputs.
Turbulence, including wake turbulence.
Windshear.
Low rotor rpm or rotor stall, as applicable.
Powerplant failure during the maneuver.
Collision hazards.
Autorotation power-off never-exceed speed (VNE) limitation, as applicable.
Helicopter-Simplified Flight Controls trim, as applicable.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Skills
Establish an autorotation.
Establish power-off glide with the helicopter-simplified flight controls trimmed and autorotation airspeed, ±10 knots.
Maintain main rotor(s) (Nr) within normal limits.
Select a suitable landing area considering altitude, wind, terrain, and obstructions.
Compensate for wind speed and direction as necessary to avoid undershooting or overshooting the selected landing area.
Make radio calls as appropriate.
Terminate approach with a power recovery at a safe altitude as directed by the evaluator.
Analyze and correct common errors related to this Task.
Task C Approach and Landing with an Engine Inoperative (Simulated) (Multiengine Helicopter-Simplified Flight Controls Only)
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands approach and landing with an engine inoperative (simulated), can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
See Appendix 2: Safety of Flight and Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations for information related to this Task.
Knowledge
Elements of approach and landing with an engine inoperative.
Effects of atmospheric conditions on emergency approach and landing.
Stabilized approach.
Approach and landing profiles and aircraft configuration.
Common errors related to this Task.
Risk Management
Consideration of altitude, wind, terrain, obstructions, and available landing area.
Planning and following a flightpath to the selected landing area.
Collision hazards.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Skills
Maintain the operating powerplant within limits.
Maintain, prior to beginning the final approach segment, the recommended flight profile with altitude ±200 feet, airspeed, ±20 knots, heading ±10°, and maintain track.
Make radio calls as appropriate.
Plan and follow a flightpath to the selected landing area considering altitude, wind, terrain, and obstructions.
Complete the appropriate checklist(s).
Maintain directional control and appropriate crosswind correction throughout the approach and landing.
Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.
Analyze and correct common errors related to this Task.
Task D Vortex Ring State (VRS)
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands Vortex Ring State (VRS), can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
See Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations for information related to this Task.
Knowledge
Elements of vortex ring state.
Effects of wind, weight, temperature, and density altitude.
Requirements for the formation of VRS.
Aerodynamics and indications of VRS.
Flight scenarios under which VRS can occur.
Effective recovery techniques.
Common errors related to this Task.
Risk Management
Pilot recognition and response to VRS.
Entering the maneuver at a lower altitude than planned.
Collision hazards.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Application of power or exceeding powerplant limitations.
Loss of tail rotor effectiveness (LTE), as applicable.
Skills
Complete the appropriate checklist(s).
Clear the area.
Select an altitude that allows recovery to be completed no lower than 1,000 feet AGL or as recommended by the manufacturer, whichever is higher.
Establish conditions leading to VRS entry.
Promptly recognize, announce, and recover at the first indication of VRS.
Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.
Analyze and correct common errors related to this Task.
Task E Low Rotor Revolutions Per Minute (RPM) Recognition and Recovery
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands low rotor rpm recognition and recovery, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
See Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations for information related to this Task.
Knowledge
Elements related to low rotor rpm recovery energy management, including the combination of conditions that may lead to this situation, as applicable.
Effects of wind, weight, temperature, and density altitude.
Aerodynamics that affect low rotor rpm conditions.
Powerplant performance.
Main rotor(s) (Nr) limitations.
Difference between low rotor rpm and blade stall.
Common errors related to this Task.
Risk Management
Powerplant limitations.
Powerplant governor operation, as applicable.
Collision hazards.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Low inertia rotor systems, as applicable.
Skills
Complete the appropriate checklist(s).
Clear the area.
Detect the development of low rotor rpm and initiate prompt corrective action.
Execute the recovery procedure to return rotor rpm to normal limits.
Analyze and correct common errors related to this Task.
Task F Systems and Equipment Malfunctions
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands system and equipment malfunctions appropriate to the aircraft provided for the practical test, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Knowledge
Causes of partial or complete power loss related to the specific type of powerplant(s).
System and equipment malfunctions specific to the helicopter-simplified flight controls, including:
a. Electrical malfunction
b. Flight instrument malfunctions
c. Pitot-static system malfunction
d. Electronic flight instrument display malfunction
e. Landing gear malfunctions, as applicable
f. Inoperative simplified flight controls/trim, as applicable
g. Hydraulic failure, if applicable
Various frequency vibrations and the possible components that may be affected.
Causes and remedies for smoke or fire onboard the aircraft.
Any other system malfunction specific to the helicopter-simplified flight controls flown.
Common errors related to this Task.
Risk Management
Startle response.
Checklist usage for a system or equipment malfunction.
Distractions, task prioritization, loss of situational awareness, or disorientation.
Undesired aircraft state.
Skills
Determine appropriate action for simulated emergencies specified by the evaluator, from at least four of the elements or sub-elements listed in K1 through K5.
Complete the appropriate checklist(s).
Analyze and correct common errors related to this Task.
Task G Dynamic Rollover
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM; SAFO 16016
Objective
To determine the applicant understands dynamic rollover, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
Evaluator assesses this Task orally only.
Knowledge
Elements related to dynamic rollover.
Interactions between thrust, crosswind, slope, lateral CG, aircraft weight, and flight controls that contribute to dynamic rollover.
Preventive flight technique and recovery during flight operations, including slope operations.
Common errors related to this Task.
Risk Management
Surface conditions conducive to dynamic rollover.
Landing gear proximity to obstructions on the ground during low altitude hover.
Flight control inputs during takeoff or landing.
Sideward hover.
Aircraft slope limitations.
Critical rollover angle and rolling moment.
Translating tendency, as applicable.
Skills
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Task H Ground Resonance
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands ground resonance, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
Evaluator assesses this Task orally only.
Knowledge
Exhibits knowledge of the elements related to ground resonance by describing:
a. Conditions that contribute to ground resonance
b. Preventive flight technique during takeoffs and landings
c. Landing surface
Inspection of items that may contribute to ground resonance.
Corrective actions during low and normal rotor rpm speeds.
Common errors related to this Task.
Risk Management
Factors that may contribute to the onset of ground resonance.
Recognition of the onset of ground resonance.
Recovery procedure selection.
Skills
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Task I Low Gravity (G) Recognition and Recovery
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands low G recognition and recovery, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
Evaluator assesses this Task orally only.
Knowledge
Exhibits knowledge of the elements related to low G conditions by describing:
a. Aerodynamic factors related to low G conditions
b. Situations that contribute to low G conditions
c. Avoidance, recognition, and appropriate recovery procedures
Effects of low G conditions on various rotor systems.
Pilot responses that lead to mast bumping in a low G condition, as applicable.
Common errors related to this Task.
Risk Management
Control inputs that cause low G conditions.
Turbulence/gusty wind conditions.
Control inputs that cause mast bumping, as applicable.
Skills
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Task J Emergency Equipment and Survival Gear
References
AC 61-65; FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands emergency equipment and survival gear, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Knowledge
Emergency Locator Transmitter (ELT) operations, limitations, and testing requirements, as applicable.
Fire extinguisher operations and limitations.
Emergency equipment and survival gear needed for:
a. Climate extremes (hot/cold)
b. Mountainous terrain
c. Overwater operations
Common errors related to this Task.
Risk Management
Survival gear (water, clothing, shelter) for 48 to 72 hours.
Skills
Identify appropriate equipment and personal gear.
Brief passengers on proper use of on-board emergency equipment and survival gear.
Analyze and correct common errors related to this Task.
Task K Antitorque System Failure
References
FAA-H-8083-2, FAA-H-8083-4, FAA-H-8083-9, FAA-H-8083-21, FAA-H-8083-25; POH/RFM
Objective
To determine the applicant understands antitorque system failure, can apply that knowledge, manage associated risks, demonstrate appropriate skills, and provide effective instruction.
Note
Evaluator assesses this Task orally only.
Knowledge
Elements related to antitorque system failure by describing:
a. Indications of an antitorque system failure(s)
b. Differences between complete loss of antitorque and mechanical flight control failures
c. RFM procedures for antitorque system(s) failure, as applicable
Wind conditions that favor a landing with an antitorque failure.
Common errors related to this Task.
Risk Management
Preflight inspection of the antitorque system, as applicable.
Antitorque failure(s) for the aircraft supplied for the practical test, as applicable.
Use of antitorque failure procedures, as applicable.
Skills
[Intentionally left blank].