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PH.V.H both lesson 90–120 minutes

Shallow Approach and Running/Roll-On Landing

Takeoffs, Landings, and Go-Arounds · Task Task H. Shallow Approach and Running/Roll-On Landing

Completion Standards

Student demonstrates knowledge of all PH.V.H items to ACS standards without reference to materials. Risk management items correctly identified. All skill elements performed to ACS standards.

Objective

Upon completion of this lesson, the student will demonstrate the knowledge, risk management, and skill to perform a shallow approach and running/roll-on landing in accordance with FAA-S-ACS-15 PH.V.H. The student will explain when to use this maneuver, identify associated risks including wind effects and surface conditions, and execute the approach while maintaining effective translational lift through touchdown with ±5 knots airspeed, ±100 feet altitude, and proper ground track alignment.

Content

Shallow Approach and Running/Roll-On Landing Elements (PH.V.H.K1)

A shallow approach and running/roll-on landing is executed at a reduced approach angle (typically 3-6 degrees) compared to a normal approach (6-12 degrees), allowing the helicopter to maintain effective translational lift throughout surface contact. This technique is primarily used when:

Aircraft Limitations: The shallow approach requires adequate landing area length (minimum 200 feet for most training helicopters). Maximum demonstrated crosswind component per RFM must be observed. The technique is unsuitable for confined areas or obstacles on approach path.

Landing Surface Texture Effects: Hard surfaces (concrete, asphalt) provide optimal conditions for roll-on landing due to minimal friction during initial contact. Grass surfaces increase friction and may cause more abrupt deceleration. Soft or uneven surfaces can cause dynamic rollover if lateral forces develop during ground contact.

Performance Factors (PH.V.H.K2)

Wind Effects: Headwinds reduce groundspeed during approach while maintaining appropriate indicated airspeed, shortening ground roll distance. Tailwinds increase groundspeed and extend ground roll requirements. Crosswinds require drift correction during approach and careful control inputs during surface contact to prevent sideways sliding or dynamic rollover.

Weight Effects: Increased gross weight requires higher approach speeds to maintain effective translational lift, resulting in longer ground roll distances and higher power requirements during approach.

Temperature and Density Altitude: High density altitude reduces rotor efficiency, requiring higher approach speeds and longer ground roll distances. Engine power available decreases with increased density altitude, potentially limiting go-around capability.

Risk Management

Approach Path and Landing Site Selection (PH.V.H.R1): Evaluate aircraft performance charts for current weight, altitude, and temperature. Ensure landing area length exceeds required ground roll distance by minimum 50%. Select approach path clear of obstacles with 8:1 glide ratio clearance minimum.

Wind Assessment (PH.V.H.R2a): Monitor ATIS/AWOS for current winds. Observe surface wind indicators (windsocks, flags, smoke, water surface). Maximum demonstrated crosswind component typically 17 knots for most training helicopters per 14 CFR 27.233.

Windshear Recognition (PH.V.H.R2b): Monitor for sudden airspeed changes, unexpected control inputs required, or rapid altitude deviations. Windshear typically occurs near frontal boundaries, thunderstorms, or significant temperature inversions. Execute immediate go-around if windshear encountered.

Turbulence Management (PH.V.H.R2c): Light turbulence may be acceptable for shallow approaches. Moderate or greater turbulence should prompt consideration of delayed landing or alternate approach technique. Wake turbulence from preceding aircraft requires minimum 3-minute separation for light aircraft, 2 minutes for helicopters.

Engine Failure During Approach (PH.V.H.R3a): Shallow approach provides improved autorotation entry compared to steep approaches. Maintain 65 knots minimum airspeed for optimal autorotation glide ratio. Be prepared to lower collective immediately and enter autorotation if engine failure occurs.

Collision Hazards (PH.V.H.R4): Maintain visual scanning during approach. Monitor radio for traffic advisories. Use landing lights during day operations. Follow 14 CFR 91.113 right-of-way rules - helicopters give way to airplanes on final approach.

Landing Surface Assessment (PH.V.H.R5): Verify surface suitability during reconnaissance. Hard, level surfaces preferred. Avoid wet surfaces when possible due to reduced braking effectiveness. Check for debris, potholes, or surface irregularities that could cause dynamic rollover.

Dynamic Rollover Prevention (PH.V.H.R6): Maintain forward motion during ground contact. Avoid lateral control inputs that could catch skid gear. If rollover tendency develops, immediately return to flight by adding collective pitch. Critical angle typically 8-10 degrees for most skid-equipped helicopters.

Ground Resonance Awareness (PH.V.H.R7): Ensure proper rotor RPM before touchdown per RFM. Be prepared to add collective and return to flight if ground resonance develops. Ground resonance occurs when main rotor frequency matches landing gear natural frequency, typically between 90-100% rotor RPM.

Aircraft Limitations (PH.V.H.R8): Observe maximum gross weight per 14 CFR 27.25. Monitor engine and transmission parameters within normal limits per RFM. Respect center of gravity limits per weight and balance calculations.

Situational Awareness (PH.V.H.R9): Prioritize aircraft control over radio calls or checklist items during approach phase. Maintain awareness of approach angle, airspeed, and ground track. If distracted or disoriented, execute go-around and reestablish situational awareness.

Regulatory References

Schedule

TimeActivityDescription
0:00-0:10Ground DiscussionShallow approach theory, when to use, limitations
0:10-0:20Risk Management ReviewWind assessment, surface evaluation, emergency procedures
0:20-0:25Equipment CheckAircraft inspection, checklist review
0:25-0:45DemonstrationCFI demonstrates 2-3 shallow approaches
0:45-1:15Student PracticeStudent performs 3-5 approaches with coaching
1:15-1:25DebriefPerformance review, areas for improvement
1:25-1:30DocumentationLogbook entries, grade sheets

Equipment

Instructor Actions

  1. Brief student on shallow approach theory emphasizing 3-6 degree approach angle compared to normal 6-12 degree approach
  2. Explain when to use shallow approach technique using analogy of airplane approach versus normal helicopter approach
  3. Demonstrate wind assessment techniques using windsock and surface indicators
  4. Show approach path planning using 8:1 obstacle clearance rule and landing distance calculations
  5. Explain effective translational lift requirements during surface contact - “keep the helicopter flying until the skids touch”
  6. Demonstrate first approach with detailed narration of control inputs and visual references
  7. Point out approach angle visual references and airspeed control during demonstration
  8. Show proper flare technique to reduce vertical velocity while maintaining forward momentum
  9. Demonstrate surface contact with skids parallel to ground track and continued forward motion
  10. Coach student through first practice approach with emphasis on angle and airspeed control
  11. Provide immediate feedback on approach angle deviations and control input timing
  12. Guide student through crosswind correction techniques during subsequent approaches
  13. Emphasize go-around decision points if approach becomes unstabilized
  14. Monitor student for proper checklist completion and radio communications
  15. Debrief each approach highlighting successful elements and areas needing improvement

Student Actions

Completion Standards

The student demonstrates satisfactory performance when able to perform shallow approach and running/roll-on landing per FAA-S-ACS-15 PH.V.H within the following standards:

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