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HI.18.F both lesson 45–60 minutes

Operational Requirements – X. Performance Maneuvers, Task B: Straight-In Autorotation in a Single-Engine Helicopter

Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations · Task Operational Requirements – X. Performance Maneuvers, Task B: Straight-In Autorotation in a Single-Engine Helicopter

Completion Standards

CFI candidate demonstrates knowledge of all HI.18.F items and ability to teach the concept effectively. All skill elements demonstrated to ACS standards.

Objective

Upon completion of this lesson, the CFI candidate will demonstrate the ability to teach the operational requirements for straight-in autorotations in single-engine helicopters per ACS task HI.XVIII.F, including minimum entry altitudes, go-around criteria, safety prioritization, and landing area assessment procedures.

Content

Entry Altitude Requirements (HI.XVIII.F.K1, HI.XVIII.F.R1)

The minimum entry altitude for straight-in autorotations is 500 feet AGL. This altitude provides sufficient time for:

In strong wind conditions, higher entry altitudes are required because:

Think of autorotation altitude like insurance - 500 feet is the minimum policy, but you buy more coverage when conditions are challenging.

Go-Around Decision Making (HI.XVIII.F.K2, HI.XVIII.F.K3)

Two distinct go-around scenarios exist:

Unsatisfactory Performance (HI.XVIII.F.K2):

Safety-Related Go-Around (HI.XVIII.F.K3):

The key distinction: performance-based go-arounds indicate skill deficiency, while safety-based go-arounds demonstrate good judgment.

Safety Prioritization (HI.XVIII.F.K4, HI.XVIII.F.R2)

Safety of flight always takes precedence over task completion. Never force a landing when:

This principle reflects real-world emergency procedures where pilots must continuously assess changing conditions and abort approaches when necessary.

Straight-In Autorotation Technique

The straight-in autorotation differs from 180-degree autorotations by:

Key phases include:

  1. Entry: Immediate collective lowering, aft cyclic application
  2. Glide: Maintain best glide airspeed, monitor glide path
  3. Flare: Aggressive aft cyclic at appropriate altitude/airspeed
  4. Touchdown: Collective application to cushion landing

Teaching Considerations

When instructing straight-in autorotations:

Schedule

TimeActivityFocus
0:00-0:05Introduction and Objective ReviewACS requirements overview
0:05-0:15Entry Altitude RequirementsMinimum altitudes, wind considerations
0:15-0:25Go-Around CriteriaPerformance vs. safety decisions
0:25-0:35Safety PrioritizationRisk management principles
0:35-0:45Technique DemonstrationChair flying exercise
0:45-0:55Teaching PracticeCFI candidate instruction
0:55-1:00Review and QuestionsCompletion standards verification

Equipment

Instructor Actions

The CFI candidate will:

  1. Explain entry altitude requirements by demonstrating calculation of minimum altitudes for various wind conditions and relating altitude to available reaction time

  2. Differentiate go-around scenarios by presenting specific examples of performance-based versus safety-based go-around situations and their evaluation implications

  3. Demonstrate safety prioritization by walking through decision-making scenarios where task completion conflicts with flight safety

  4. Chair fly the straight-in autorotation while providing continuous narration of control inputs, altitude callouts, and decision points per HI.XVIII.F.S1

  5. Explain go-around procedures by demonstrating the transition from autorotation to powered flight when landing area safety concerns arise per HI.XVIII.F.S2

  6. Teach landing area assessment by explaining factors that determine landing area suitability and when safety concerns necessitate a go-around

  7. Address common student errors including premature flare, inadequate airspeed control, and reluctance to execute go-arounds

Student Actions

The student (evaluator) will:

  1. Ask questions about minimum entry altitude calculations and wind condition adjustments
  2. Present scenarios requiring go-around decision making
  3. Challenge the CFI candidate’s understanding of safety prioritization
  4. Observe the chair flying demonstration for accuracy and teaching effectiveness
  5. Evaluate the clarity of explanations regarding operational requirements
  6. Assess the CFI candidate’s ability to relate ACS standards to practical application

Completion Standards

The CFI candidate demonstrates satisfactory performance when they can teach a student to meet ACS standards for HI.XVIII.F by:

  1. Explaining entry altitude requirements including the 500-foot AGL minimum and adjustments for wind conditions per HI.XVIII.F.K1 and HI.XVIII.F.R1

  2. Clearly distinguishing between performance-based go-arounds (unsatisfactory per HI.XVIII.F.K2) and safety-based go-arounds (not unsatisfactory per HI.XVIII.F.K3)

  3. Emphasizing safety prioritization per HI.XVIII.F.K4 and HI.XVIII.F.R2 with specific examples of when not to force a landing

  4. Demonstrating proper technique for initiating straight-in autorotation at minimum 500 feet AGL per HI.XVIII.F.S1

  5. Teaching go-around procedures for landing area safety concerns per HI.XVIII.F.S2

  6. Presenting information clearly and accurately using appropriate teaching methods and maintaining student engagement throughout the lesson

Performance meets ACS task HI.XVIII.F standards when the CFI candidate can effectively teach operational requirements while maintaining focus on safety and regulatory compliance.

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