REJECTED LANDING

Objective

The student will demonstrate proficiency in executing a rejected landing (go-around) in a turbine helicopter to ATP standards, making timely decisions to discontinue an approach, applying proper power and pitch control, managing helicopter configuration changes, and maintaining precise directional and airspeed control throughout the maneuver. The student will apply professional judgment and crew resource management principles consistent with single-pilot turbine operations. Upon completion, the student will meet or exceed the standards specified in FAA-S-ACS-ATP Task AT.VIII.C.

Content

Rejected Landing Overview and Decision-Making

A rejected landing (go-around) is a fundamental safety procedure executed when continuing an approach to landing becomes unsafe or inadvisable. At the ATP level, this maneuver requires immediate recognition, decisive action, and precise aircraft control while managing configuration changes and power applications in turbine helicopters.

The rejected landing is not a failure—it’s a professional decision that prioritizes safety over completion. ATP pilots must develop a “go-around mindset” that eliminates hesitation when conditions warrant discontinuing the approach.

Conditions Dictating a Rejected Landing

ATP helicopter pilots must recognize numerous situations requiring immediate rejection of the landing:

Environmental Conditions:

• Sudden wind shifts, gusts, or loss of effective translational lift (ETL) causing unacceptable control margins
• Deteriorating visibility below approach minima
• Developing whiteout or brownout conditions during final approach
• Windshear or microburst encounter
• Unexpected turbulence exceeding safe operating limits
• Foreign object debris (FOD) on landing area

Aircraft Performance and Configuration:

• Excessive approach speed or descent rate that cannot be corrected
• Unstabilized approach parameters (outside ATP tolerances)
• Loss of effective tail rotor authority
• Abnormal engine indications or caution/warning lights
• Hydraulic system degradation
• Configuration anomaly (landing gear malfunction, door ajar)

Operational Factors:

• Landing area obstruction (vehicle, personnel, wildlife, other aircraft)
• Loss of landing area visual reference
• ATC instructions to go around
• Traffic conflict
• Approach clearance canceled or changed
• Landing area conditions unsuitable (wet helipad, snow-covered surface beyond limits)

Professional Judgment:

• Pilot discomfort or uncertainty about approach continuation
• Any doubt about safe completion of landing
• Multiple minor deviations accumulating

The ATP standard demands recognition of these conditions earlier than commercial operations. The decision trigger is “when in doubt, go around”—not attempting to salvage a deteriorating approach.

Importance of Timely Decision-Making

Delayed go-around decisions create compounding problems:

1. Energy Management: Low altitude and low airspeed with insufficient power margin for recovery
2. Height-Velocity Diagram: Descending into the avoid areas without adequate energy for recovery
3. Terrain/Obstacle Clearance: Insufficient altitude to clear obstacles during climb-out
4. Psychological Pressure: Increasing stress reduces decision quality and coordination
5. Configuration Management: Less time to properly sequence gear retraction and power application

ATP pilots must make the go-around decision immediately when approach parameters are not met or conditions change. The decision point is typically when any approach tolerance is exceeded, not after attempting correction fails. In turbine helicopters, the decision may occur anywhere from approach initiation to 10 feet AGL.

Think of it like this: Commercial pilots go around when they must. ATP pilots go around when they should.

Recommended Airspeeds and V-speeds

Go-around airspeeds vary by helicopter type and are published in the RFM/AFM. ATP candidates must know and apply their specific aircraft’s speeds.

Typical Turbine Helicopter Go-Around Speeds:

• Initial climb speed: VY (best rate of climb) or manufacturer-specified speed
• Acceleration altitude: Per aircraft limitations, typically 200-500 feet AGL
• Cruise climb speed: Often VY to pattern altitude, then transition to cruise climb

Examples by Aircraft Type:

• Bell 206: VY approximately 60 KIAS (verify RFM)
• Bell 407: VY approximately 60 KIAS, cruise climb 80 KIAS
• AS350: VY approximately 65 KIAS (varies by series)
• EC130: VY approximately 60 KIAS

V-Speed Application:

• During initial go-around: establish VY ±5 knots (ATP standard)
• Maintain VY until clearing obstacles and reaching safe altitude
• Accelerate to cruise climb speed after clearing pattern conflicts
• Retractable gear aircraft: accelerate through VLE (landing gear extended speed) considerations

Airspeeds must account for density altitude effects. At high density altitudes, actual VY may differ from sea-level values, and climb performance is degraded.

Power Application and Energy Management

Turbine helicopter go-arounds require aggressive yet smooth power application:

Power Setting Sequence:

1. Immediate: Increase collective to maximum continuous power or takeoff power (within limits)
2. Monitor: Torque, TGT/MGT, rotor RPM within operational limits
3. Adjust: Coordinate pedal input for torque change (right pedal for increased power in American helicopters)
4. Sustain: Maintain power setting until achieving positive rate of climb and VY

ATP Considerations:

• Know your aircraft’s power limitations: maximum continuous, takeoff, one-engine-inoperative (if multi-engine)
• Account for density altitude—power available decreases with altitude and temperature
• In hot/high conditions, go-around may require all available power
• If approaching power limits during approach, earlier go-around decision is critical
• Single-pilot resource management: vocalize power application (“Full power applied, torque 95%”)

Energy State Management:

• Low-energy go-around (low speed, descending): requires maximum power, level pitch initially, then climb as speed increases
• High-energy go-around (normal approach speed): power increases climb while maintaining VY
• Never sacrifice rotor RPM for climb—maintain within green arc first

Think of turbine power like a credit card—you can use it immediately, but there are limits. Know those limits before the approach begins.

Clean-Up Procedure

Configuration management during go-around must follow precise sequencing for safety:

Standard Configuration Sequence:

1. Power: Maximum continuous/takeoff power applied
2. Pitch: Adjust to achieve VY (initially level or slight climb if low energy state)
3. Positive Rate: Verify climb on VSI/altimeter—verbalize “Positive rate”
4. Landing Gear (if retractable): Retract only after positive rate and safe altitude
5. Flaps/Other Devices: Retract per manufacturer sequence (rare in helicopters)
6. Trim: Adjust cyclic and pedal trim as needed for coordination

Landing Gear Considerations:

• Most helicopter training occurs in fixed-gear aircraft (Bell 206, AS350, R44)
• Retractable gear helicopters (S-76, AW139, some EMS configurations): gear up only with positive rate and above minimum safe altitude
• Never retract gear below manufacturer-specified minimum altitude
• Verify “gear up” indication before confirming retraction complete

ATP Precision Standards:

• Sequence must be automatic, flowing naturally from practice
• Configuration changes made smoothly without disrupting flight path
• Trim adjustments minimize control forces for sustained climb
• All actions coordinated with navigation and communication requirements

Ground Track Maintenance

During go-around, maintaining proper ground track demonstrates professional control:

ATP Standard: Maintain ground track within ±5° of intended path

Factors Affecting Ground Track:

• Torque change requires pedal correction (right pedal for increased power)
• Wind drift during climb transition
• Remaining aligned with runway/approach path for traffic separation
• Clearing obstacles along departure corridor

Technique:

• Select visual reference aligned with intended track (runway centerline, approach path)
• Anticipate right yaw from power application—lead with pedal
• Small cyclic corrections maintain lateral position
• Avoid aggressive maneuvering at low altitude and low airspeed

Communication Integration:

• Announce go-around to ATC: “Helicopter [callsign], going around”
• Follow ATC vectors or published missed approach as appropriate
• Single-pilot IFR: balance configuration management with navigation and communication

Checklist Procedures

ATP operations require timely and appropriate checklist usage:

Go-Around/Balked Landing Checklist:

• Most turbine helicopters have published go-around or balked landing checklists
• Items typically include: power setting verification, configuration changes, trim, system checks
• Execute checklist when workload permits—do not delay power application or flight control

Checklist Philosophy:

• Memory items first (power, pitch, positive rate, gear)
• Printed checklist when stabilized in climb and workload permits
• Single-pilot operations: brief before approach when go-around is anticipated
• Do not let checklist distract from aircraft control at low altitude

After Go-Around:

• Complete landing or approach checklist reset
• Brief approach for second attempt
• Consider fuel state and alternate plans if multiple go-arounds occur

Risk Management Elements

Timely Decision-Making:

• Establish personal minimums for go-around triggers before approach
• Brief specific go-around criteria before each approach
• Use callouts at decision points (“100 feet, on speed, on glide path, continuing”)
• Eliminate “get-home-itis” or external pressure to land
• If second approach shows same issues, consider diversion

Appropriate Power Setting:

• Know aircraft power limitations before beginning approach
• Confirm power available exceeds power required for go-around at current density altitude
• Do not hesitate to use maximum power when needed
• Monitor engine instruments during power application—respect limitations
• If power limits are reached during go-around, manage climb performance accordingly

Pitch Attitude Control:

• Establish pitch attitude that achieves VY without excessive nose-up (avoid tail rotor strike potential)
• Coordinate pitch and power for desired performance
• Avoid over-pitching in low-energy situations (rotor RPM decay)
• Use outside visual references and flight instruments together

Height-Velocity Awareness:

• During go-around from low hover or approach, transitioning through H/V avoid areas is unavoidable
• Minimize time in avoid areas by aggressive power application and proper airspeed
• Plan go-around to exit avoid areas on safe side (altitude or airspeed)

Single-Pilot Resource Management:

• Verbalize actions to maintain situational awareness
• Prioritize: aviate, navigate, communicate
• Minimize heads-down time during initial climb
• Use autopilot if available and appropriate to reduce workload

Common Errors and ATP-Level Corrections

• Delayed decision: ATP pilots decide immediately when tolerances are exceeded—set hard triggers
• Inadequate power: Use full authorized power without hesitation—turbine engines respond quickly
• Poor pitch control: Focus on achieving VY smoothly—excessive pitch causes rotor decay
• Premature gear retraction: Wait for positive rate and safe altitude—verify climb before configuration change
• Directional control loss: Anticipate right pedal requirement as power increases
• Fixation on landing area: Transition eyes to flight path ahead—clear obstacles first
• Checklist distraction: Fly the helicopter first—checklist when stabilized

Schedule

Equipment

Required References

• FAA-S-ACS-ATP (Airline Transport Pilot—Helicopter ACS), current edition, Area of Operation VIII, Task C
• Helicopter Flying Handbook (FAA-H-8083-21B), Chapter 11 (Helicopter Emergencies and Hazards)
• Rotorcraft Flight Manual/Approved Flight Manual for training aircraft
• Pilot Operating Handbook (POH) or Aircraft Flight Manual Supplement
• 14 CFR Part 91 (General Operating and Flight Rules)
• 14 CFR Part 61 (Certification: Pilots, Flight Instructors, and Ground Instructors)

Training Aircraft

• Turbine helicopter (Bell 206, Bell 407, AS350, EC130, or similar) appropriate for ATP training
• Aircraft must be airworthy with current inspections and suitable performance for rejected landing maneuvers
• Aircraft equipped with functioning engine instruments (torque meter, TGT/MGT, fuel flow, rotor RPM)
• Retractable landing gear (if applicable to training aircraft type) functioning properly

Materials and Visual Aids

• Whiteboard or tablet for diagramming rejected landing scenario profiles
• Aircraft-specific V-speed reference card (VY, VLE if applicable, cruise climb speeds)
• Height-velocity diagram for training aircraft
• Approach profile diagram showing decision points for rejected landing
• Power available vs. power required chart for density altitude considerations
• Go-around/balked landing checklist (aircraft-specific)

Flight Equipment

• Current aeronautical charts for training area
• Pilot checklist for training aircraft
• Knee board and flight notepad
• Fuel calculator or EFB for weight and balance, density altitude computation
• Stopwatch or timer for tracking maneuver segments

Instructor Actions

1. Pre-Flight Briefing: Explain rejected landing scenarios, emphasizing ATP-level decision-making differs from commercial training—immediate action when approach tolerances are exceeded, not salvage attempts. State: “At ATP level, you’re not trying to save a bad approach. You recognize early and go around decisively.”

2. Review Decision Criteria: Brief specific triggers for rejected landing in today’s scenarios: approach speed deviation exceeding ±5 knots, descent rate exceeding planned profile, loss of visual reference, simulated obstacle appearance, unstable approach parameters. State: “We’ll train you to call ‘go-around’ the moment parameters exceed limits, not after attempting correction.”

3. Discuss V-Speeds: Review training aircraft’s VY, power limitations, and configuration procedures. Use whiteboard to show power-pitch-configuration sequence. State: “In the [aircraft type], VY is [XX] knots. When you call go-around, you’ll apply maximum continuous power, establish pitch for VY, confirm positive rate, then retract gear if applicable.”

4. Risk Management Emphasis: Discuss density altitude effects on go-around performance, height-velocity considerations during transition, and single-pilot resource management. State: “Today’s density altitude is [XXXX] feet. That means our power available is reduced. If we delay the decision, we may not have enough power to execute safely. Decide early.”

5. Ground Discussion: Cover timely decision-making with real-world scenarios—EMS approach finding unexpected wires, corporate approach encountering sudden wind shift, offshore approach with deck movement. State: “Professional helicopter pilots go around routinely. It’s a normal procedure, not an emergency. Your job is to recognize and act.”

6. Demonstration Setup: Position aircraft on approach to suitable landing area (elevated platform, runway, clear area). Establish normal approach profile at appropriate airspeed and descent rate. Narrate throughout demonstration.

7. Demonstrate Decision Point: At approximately 100 feet AGL, announce: “Simulated unstable approach—excessive sink rate, going around.” Immediately apply maximum continuous power smoothly while coordinating right pedal.

8. Demonstrate Pitch Control: Adjust cyclic to establish nose attitude for VY. State: “Pitch for [VY] knots. Not too aggressive—we need to maintain rotor RPM. Watch the VSI—positive rate developing.”

9. Demonstrate Positive Rate: As VSI shows climb and altimeter increases, state: “Positive rate of climb confirmed. Airspeed approaching VY.” If aircraft has retractable gear, continue: “Gear up,” and retract landing gear.

10. Demonstrate Track Control: Maintain alignment with approach path using visual references. State: “Maintaining runway centerline. Small cyclic corrections for lateral position. Anticipating right pedal as power settles.”

11. Demonstrate Configuration Management: Trim aircraft for hands-off climb if equipped with trim. State: “Adjusting pedal trim for coordinated flight. Cyclic trim reducing control forces. This lets me manage navigation and communication while sustaining climb.”

12. Demonstrate Second Scenario: Execute rejected landing from low hover taxi (simulating obstacle appearance). State: “From hover taxi at 10 feet, simulated vehicle enters path—going around. Power smoothly to maximum continuous, cyclic forward for translational lift, climbing out.”

13. Debrief Demonstration: Emphasize decision immediacy, power application coordination, maintaining VY ±5 knots, directional control with pedal input, configuration sequencing. State: “Notice I didn’t try to fix the approach. When I saw the deviation, I immediately went around. That’s ATP decision-making.”

14. Coach First Student Practice: Have student establish approach. Call simulated condition requiring go-around. Observe student’s decision timing—coach if delayed. State: “That’s your trigger—call it now. Go around.”

15. Monitor Power Application: Observe student’s power application and pedal coordination. Provide immediate feedback: “More right pedal—anticipate the yaw. Smooth on the collective, don’t spike the torque.”

16. Monitor Pitch and Airspeed: Watch pitch attitude and airspeed. Guide student to VY: “Ease nose down slightly—you’re 10 knots slow. We want [VY] knots for best climb performance.”

17. Monitor Track Control: Observe lateral position relative to approach path. Provide corrections: “Drifting left—small cyclic right to hold centerline. You’re 7 degrees off—tighten it up within 5.”

18. Evaluate Configuration Management: If aircraft has retractable gear, ensure student verifies positive rate before calling for gear retraction. State: “Confirm positive rate verbally before gear up. Good—‘positive rate, gear up.’”

19. Coach Second Scenario: Set up unstable approach with multiple small deviations (airspeed +8 knots, slightly right of centerline). Test student’s decision-making. State: “You’re 8 knots fast and right of centerline. What’s your decision?”

20. Evaluate Decision Timing: Assess whether student recognizes cumulative deviations and makes timely go-around decision. Provide immediate feedback: “You waited too long. When airspeed exceeded +5 and you were off centerline, that was your trigger. Let’s run it again.”

21. Coach Third Scenario: Set up rejected landing from hover taxi or low approach. Announce simulated condition: “Vehicle crossing your path—go.” Observe power application and climb technique.

22. Emphasize Single-Pilot Resource Management: During practice, have student verbalize actions: “Going around, full power, pitch for VY, positive rate, gear up.” State: “Vocalizing keeps you ahead of the aircraft and helps with crew resource management in multi-pilot operations later.”

23. Evaluate to ATP Standards: During final evaluation scenarios, assess decision timing (immediate when tolerances exceeded), airspeed control (VY ±5 knots), track maintenance (±5°), configuration sequencing (proper and safe), and checklist usage (appropriate and timely).

24. Provide Scenario Variety: Introduce different rejected landing triggers: simulated wind shear, brownout conditions developing, approach lights out (simulated night), traffic conflict, ATC go-around instruction.

25. Debrief Performance: Post-flight, review each scenario, decision quality, control precision, and ATP standard achievement. State: “Your decision-making improved throughout the lesson. On the final scenario, you recognized the deviation immediately and executed precisely. That’s ATP-level performance.”

Student Actions

1. Pre-Flight Preparation: Reviews AT.VIII.C ACS standards, training aircraft V-speeds, power limitations, go-around procedures from RFM/AFM, and height-velocity diagram.

2. Briefing Participation: Asks questions about rejected landing decision criteria, aircraft-specific procedures, and ATP performance standards. Confirms understanding of scenario triggers and completion standards.

3. Ground Discussion: Discusses density altitude effects on go-around performance for planned training flight. Calculates expected power available at current conditions. Reviews decision-making process for timely go-around execution.

4. Pre-Flight Inspection: Conducts thorough pre-flight inspection with emphasis on control systems, engine condition, landing gear operation (if retractable), and instrument function critical for approach monitoring.

5. Observation During Demonstration: Closely observes CFI demonstration, noting decision point timing, power application technique, pitch control for VY, pedal coordination, configuration sequencing, and track maintenance. Takes mental notes of control inputs and verbal callouts.

6. First Practice Setup: Establishes stabilized approach at correct airspeed, descent rate, and approach path. Monitors approach parameters using outside references and flight instruments.

7. Decision Execution: When CFI calls simulated condition or deviation is observed, immediately announces “Going around” and begins maneuver execution without hesitation.

8. Power Application: Smoothly increases collective to maximum continuous or takeoff power (within limitations), coordinating right pedal input to counteract torque effect. Monitors torque meter, TGT/MGT, and rotor RPM.

9. Pitch Control: Adjusts cyclic to establish pitch attitude that achieves VY. References airspeed indicator and adjusts pitch to achieve VY ±5 knots (ATP standard). Maintains pitch attitude while airspeed stabilizes.

10. Positive Rate Confirmation: Verifies positive rate of climb on VSI and altimeter. Verbalizes “Positive rate” when climb is confirmed. Maintains VY during initial climb segment.

11. Configuration Management: If aircraft equipped with retractable landing gear, selects gear up only after confirming positive rate and safe altitude. Follows manufacturer-recommended sequence for configuration changes.

12. Track Control: Maintains ground track within ±5° of intended path (approach centerline or runway heading) using visual references and coordinated flight control inputs. Makes small cyclic corrections to prevent drift.

13. Trim Adjustment: Adjusts cyclic and pedal trim to reduce control forces during sustained climb. Establishes hands-off coordinated flight when workload permits.

14. Checklist Usage: Completes go-around or balked landing checklist when aircraft is stabilized in climb and workload permits. Does not delay critical flight control for checklist completion.

15. Second Scenario Practice: Establishes approach and monitors for approach parameter deviations (airspeed, track, descent rate). Makes timely decision to reject landing when parameters exceed ATP tolerances (+5 knots airspeed, ±5° track).

16. Self-Critique: Evaluates own decision timing and execution precision. Asks CFI for feedback on areas needing improvement: “Did I hesitate on that decision?” or “Was my track control within limits?”

17. Third Scenario Practice: Executes rejected landing from low hover taxi or low approach when simulated obstacle or condition change occurs. Applies immediate power and proper climb technique to clear simulated obstacle.

18. Verbalization: Verbalizes actions during maneuver execution to demonstrate single-pilot resource management: “Going around, full power applied, pitch for VY, positive rate, gear up, tracking centerline.”

19. Multiple Repetitions: Practices rejected landings from various approach phases (normal approach, unstable approach, low hover) until execution is immediate, precise, and consistent with ATP standards.

20. Scenario Adaptation: Responds appropriately to different rejected landing triggers introduced by CFI: simulated wind shear, visibility loss, traffic conflict, obstacle appearance, ATC instruction.

21. Performance Self-Assessment: Monitors own performance against ATP standards throughout practice: airspeed within ±5 knots VY, track within ±5°, timely configuration changes, proper power management.

22. Post-Flight Debrief Participation: Reviews performance with CFI, identifies areas of strong performance and areas needing additional practice. Asks specific questions about decision-making quality and control precision.

23. Standards Comprehension: Confirms understanding of AT.VIII.C completion standards and ability to consistently meet those standards before progressing to evaluation scenarios.

24. Final Evaluation Performance: Demonstrates consistent, precise rejected landing execution across multiple scenarios with immediate decision-making, accurate VY ±5 knots, track maintenance ±5°, proper configuration sequencing, and appropriate checklist usage.

Completion Standards

The lesson is complete when the student demonstrates consistent proficiency in executing rejected landings to ATP helicopter standards as specified in FAA-S-ACS-ATP Task AT.VIII.C. The student must meet all of the following performance criteria:

Knowledge Standards

1. Exhibits adequate knowledge of rejected landing procedures by correctly explaining conditions requiring go-around, decision-making process, aircraft-specific V-speeds (VY and applicable speeds), power limitations, configuration sequencing, and checklist procedures during briefing and post-flight debrief.

2. Articulates conditions dictating rejected landing including environmental factors (wind shear, visibility loss, whiteout/brownout), aircraft performance deviations (excessive speed/sink rate, unstable approach), operational factors (obstacle appearance, traffic conflict, ATC instruction), and professional judgment triggers.

3. Demonstrates understanding of timely decision-making importance by explaining consequences of delayed go-around decisions, describing decision triggers based on ATP approach tolerances, and correctly identifying decision points for various scenario types.

4. Correctly identifies recommended airspeeds/V-speeds for training aircraft, including VY (best rate of climb), cruise climb speed, and VLE if applicable. States these speeds accurately and applies them within ±5 knots during maneuver execution.

5. Explains appropriate clean-up procedure including power-pitch-positive rate-gear sequence, configuration change timing and safety considerations, trim adjustment requirements, and checklist integration without compromising aircraft control.

Risk Management Standards

6. Makes timely decision to reject landing by recognizing approach deviations or changing conditions immediately (within 2-3 seconds) and announcing “Going around” without hesitation when ATP approach tolerances are exceeded or simulated conditions warrant discontinuation.

7. Applies appropriate power setting for flight condition by smoothly increasing collective to maximum continuous or takeoff power (within aircraft limitations), coordinating pedal input for torque change, and maintaining rotor RPM within green arc throughout maneuver.

8. Establishes pitch attitude necessary to obtain desired performance by adjusting cyclic to achieve VY, balancing climb performance with rotor RPM management, and avoiding excessive pitch attitudes that could lead to tail strike or rotor decay.

Skill Standards (ATP ACS Tolerances)

9. Adjusts helicopter configuration in correct sequence by executing power-pitch-positive rate-gear sequence properly, retracting landing gear (if applicable) only after confirming positive rate of climb and safe altitude, and managing configuration changes without disrupting flight path.

10. Establishes positive rate of climb verified on both VSI and altimeter, verbalizes “Positive rate” when climb is confirmed, and maintains climb throughout maneuver without altitude loss after go-around initiation.

11. Establishes and maintains appropriate airspeed within ±5 knots by achieving VY ±5 knots during initial climb segment, making smooth pitch adjustments to correct airspeed deviations, and transitioning to cruise climb speed (if appropriate) within ±5 knots after clearing pattern conflicts.

12. Maintains proper ground track within ±5° of intended path (approach centerline or runway heading) throughout rejected landing procedure by making small coordinated cyclic corrections, anticipating wind drift, and using visual references effectively.

13. Accomplishes appropriate checklist items in timely manner by completing memory items (power, pitch, positive rate, gear) immediately, executing printed go-around/balked landing checklist when aircraft is stabilized and workload permits, and not allowing checklist to distract from aircraft control at low altitude.

14. Demonstrates consistent performance across multiple scenarios by successfully executing rejected landings from normal approach, unstable approach, and low hover/taxi situations with equal precision and decision quality.

15. Maintains single-pilot resource management throughout maneuver by verbalizing actions, prioritizing aviate-navigate-communicate, managing workload effectively, and demonstrating professional control discipline consistent with turbine helicopter operations.

Overall ATP Performance Standard

The student performs rejected landing maneuvers with precision, consistency, and professionalism expected of an ATP helicopter pilot. Decision-making is immediate when approach tolerances are exceeded. Power application is smooth and coordinated. Airspeed control is precise (VY ±5 knots). Track maintenance is accurate (±5°). Configuration changes are properly sequenced and executed at safe altitudes. Checklist procedures are followed appropriately without compromising aircraft control. The student demonstrates the judgment, skill, and risk management required for professional single-pilot turbine helicopter operations and meets or exceeds all standards specified in ACS Task AT.VIII.C.