Objective
The student will demonstrate knowledge of normal and crosswind approach procedures and perform normal and crosswind approaches to a safe landing or hover within ACS standards. Upon completion of this lesson, the student will be able to:
- Explain the effects of wind, weight, altitude, and temperature on helicopter approach performance (Knowledge - FAA-S-ACS-15 PH.V.B)
- Demonstrate proper wind correction techniques during approach and landing (Knowledge/Skill - FAA-S-ACS-15 PH.V.B)
- Select appropriate landing surfaces and touchdown points considering obstructions and hazards (Knowledge/Skill - FAA-S-ACS-15 PH.V.B)
- Explain factors affecting the height/velocity diagram profile during approaches (Knowledge - FAA-S-ACS-15 PH.V.B)
- Execute normal and crosswind approaches maintaining airspeed ±10 knots, arriving at termination point ±4 feet (Skill - FAA-S-ACS-15 PH.V.B)
- Identify and mitigate risks associated with various wind conditions, surface conditions, and approach hazards (Risk Management - FAA-S-ACS-15 PH.V.B)
Content
Wind Effects on Approach Performance
Effects of Wind, Weight, Altitude, and Temperature:
- Headwind increases effective translational lift (ETL), allowing steeper approach angles with same power settings
- Tailwind reduces ETL effectiveness, requiring shallower approaches and increased power
- Crosswind creates asymmetric lift on the rotor disc, requiring cyclic correction and anti-torque adjustment
- Higher density altitude (high altitude/temperature, low pressure) reduces available power and rotor efficiency
- Increased gross weight requires higher power settings and affects autorotational glide distance
- Temperature affects power available - hot days reduce engine and rotor performance significantly
Wind Correction Techniques:
- Establish wind correction angle early in approach to maintain ground track
- Use crab method: point helicopter nose into wind to maintain desired ground track
- Transition to sideslip method before touchdown: lower upwind skid first, maintain longitudinal alignment with landing direction
- Monitor drift continuously - small corrections are more effective than large late corrections
- In gusty conditions, carry extra airspeed (5-10 knots) for control responsiveness
Landing Surface Selection and Touchdown Points
Landing Surface Considerations (14 CFR 91.119):
- Firm, level surface free of loose debris that could be blown up by rotor wash
- Adequate size for safe approach and departure considering helicopter dimensions
- Clear of obstacles in approach and departure paths
- Consider surface material: concrete/asphalt ideal, grass acceptable if firm, avoid soft dirt or sand
- Evaluate slope - maximum safe slope varies by helicopter type (typically 5-15 degrees)
Touchdown Point Selection:
- Choose point allowing normal approach angle (typically 6-10 degrees)
- Ensure adequate clearance from obstacles in approach path
- Consider go-around options - clear departure paths available
- Account for wind direction relative to obstacles and surface conditions
Height/Velocity Diagram Factors
The H/V diagram (dead man’s curve) represents combinations of height and airspeed to avoid during normal operations:
Factors Affecting H/V Profile:
- Gross weight: heavier aircraft has larger avoid area due to higher sink rates in autorotation
- Density altitude: reduces autorotational glide performance, expanding avoid area
- Center of gravity: aft CG reduces autorotational flare capability
- Aircraft configuration: external loads or equipment affect autorotational characteristics
- During approaches, minimize time spent in avoid area by maintaining appropriate airspeed for height
Risk Management
Wind-Related Risks:
- Crosswind: Causes drift, requires constant correction, affects LTE susceptibility at low speeds
- Windshear: Sudden wind changes can cause rapid altitude or airspeed variations requiring immediate pilot response
- Tailwind: Reduces ETL effectiveness, increases groundspeed, complicates distance judgment
- Turbulence/Wake Turbulence: Can cause uncommanded attitude changes, loss of control authority; avoid approaches behind large aircraft
Vortex Ring State (VRS) Prevention:
- Occurs with high rates of descent (>300 fpm) at low forward airspeeds (<30 knots)
- Avoid by maintaining forward airspeed throughout approach
- If encountered: lower collective, apply forward cyclic, increase airspeed before attempting recovery
Surface and Approach Path Risks:
- Touchdown Surface: Evaluate firmness, slope, contamination; soft surfaces can cause dynamic rollover
- Obstructions: Power lines, towers, trees in approach path; maintain safe clearance margins
- Go-around Planning: Always have escape route planned; brief go-around procedures before approach
Operational Risks:
- Loss of Tail Rotor Effectiveness (LTE): Critical azimuth awareness (210-330 degrees), weathercock stability regions
- Collision Hazards: Other aircraft, ground vehicles, personnel in landing area
- Distractions: Maintain scan pattern, prioritize flight path control over secondary tasks
- Loss of Situational Awareness: Brief approach plan, maintain orientation with visual references
Schedule
| Time | Phase | Activity |
|---|---|---|
| 0:00-0:10 | Preflight | Review objective, discuss wind conditions, brief approach procedures |
| 0:10-0:25 | Ground | Demonstrate wind effects using model, review H/V considerations |
| 0:25-0:35 | Taxi/Departure | Radio procedures, departure with wind analysis |
| 0:35-0:50 | Practice Area | Normal approaches to different surfaces, various wind conditions |
| 0:50-1:05 | Pattern Work | Crosswind approach practice, go-around procedures |
| 1:05-1:15 | Return/Shutdown | Debrief approaches, discuss performance standards |
Equipment
Required References:
- FAA-H-8083-21B Rotorcraft Flying Handbook Chapter 8
- FAA-S-ACS-15 Private Pilot Helicopter ACS Area V Task B
- Aircraft Pilot’s Operating Handbook/Flight Manual
- Sectional chart for local area
- 14 CFR Part 91 regulations
Materials:
- Helicopter model for wind effect demonstrations
- Wind correction angle calculator or E6B
- Approach angle demonstration aid
- H/V diagram for aircraft type
- Local area hazard map showing approach considerations
Visual Aids:
- Height/velocity diagram poster
- Wind triangle diagram
- LTE critical azimuth diagram
- Crosswind approach technique illustrations
Instructor Actions
- Preflight Briefing: Explain lesson objectives, review current wind conditions using AWOS/ATIS, brief approach procedures and emergency actions
- Demonstrate Wind Effects: Use helicopter model to show crosswind effects on approach path, explain correction techniques
- Brief H/V Considerations: Show aircraft-specific H/V diagram, explain how approach profile affects time in avoid area
- Review Risk Factors: Discuss VRS, LTE, windshear recognition, go-around decision criteria
- Demonstrate Normal Approach: Execute stabilized approach showing proper sight picture, control inputs, and wind corrections
- Coach Crosswind Approach: Guide student through wind correction angle establishment and sideslip transition technique
- Demonstrate Go-Around: Show proper go-around technique from various points in approach
- Monitor Student Performance: Observe control smoothness, wind correction effectiveness, altitude/airspeed control
- Provide Corrective Feedback: Address common errors like excessive control inputs, poor wind drift correction, unstabilized approaches
- Evaluate Decision Making: Assess student’s surface selection, hazard identification, and risk mitigation strategies
Student Actions
- Preflight Planning: Determine wind conditions, calculate crosswind components, brief approach procedures
- Radio Communications: Make appropriate traffic pattern calls, coordinate with tower if applicable
- Wind Assessment: Determine wind direction using visual indicators (flags, smoke, water patterns)
- Approach Execution: Establish normal approach angle, maintain airspeed within ±10 knots of target
- Wind Correction: Apply appropriate crab angle to maintain ground track, transition to sideslip for landing
- Hazard Scanning: Continuously scan approach path and landing area for traffic and obstacles
- Performance Monitoring: Maintain rotor RPM and engine parameters within normal limits
- Precision Flying: Arrive at termination point within ±4 feet horizontally
- Go-Around Execution: Recognize unstabilized approach conditions and execute go-around when appropriate
- Risk Assessment: Identify and communicate potential hazards throughout approach phase
Completion Standards
The student demonstrates satisfactory knowledge and skill in normal and crosswind approaches when they:
Knowledge Standards (FAA-S-ACS-15 PH.V.B):
- Explains how wind, weight, altitude, and temperature affect approach performance
- Describes proper wind correction techniques for approach and landing
- Identifies appropriate landing surfaces and touchdown points considering obstacles
- Explains factors affecting H/V diagram profile during approaches
Risk Management Standards (FAA-S-ACS-15 PH.V.B):
- Selects appropriate approach path based on wind conditions and aircraft limitations
- Identifies hazards associated with crosswind, windshear, tailwind, and turbulence
- Recognizes VRS conditions and demonstrates avoidance techniques
- Evaluates touchdown surface conditions and selects appropriate landing technique
- Demonstrates understanding of go-around procedures and decision criteria
Skill Standards (FAA-S-ACS-15 PH.V.B):
- Completes appropriate checklists for approach phase
- Makes proper radio calls for traffic pattern or approach procedures
- Determines wind direction using available indicators
- Aligns helicopter with correct runway or touchdown point
- Maintains effective scan for traffic and obstructions
- Establishes and maintains proper ground track with wind correction
- Maintains normal approach angle and rate of closure
- Keeps powerplant and main rotor RPM within normal operating limits
- Arrives at termination point (surface or stabilized hover) within ±4 feet
- Uses appropriate runway incursion avoidance procedures when applicable