PH.VIII.B — Powerplant Failure at Altitude in a Single-Engine Helicopter
PH.VIII.B for the Private Pilot Rotorcraft ACS: official objective, references, and 24 exact knowledge, risk-management, and skill descriptions.
FAA-S-ACS-15, November 2023. This study page does not replace the current FAA publication or an examiner's plan of action.
Official task context
| Certificate or rating | Private Pilot |
|---|---|
| Aircraft category | Rotorcraft |
| Area of operation | Area of Operation VIII. Emergency Operations |
| Task | Task B. Powerplant Failure at Altitude in a Single-Engine Helicopter |
| Task code prefix | PH.VIII.B |
| Official references | AC 61-140; FAA-H-8083-2, FAA-H-8083-21, FAA-H-8083-25; POH/RFM |
| FAA document | FAA-S-ACS-15 — Private Pilot for Rotorcraft Category Helicopter Rating Airman Certification Standards |
| FAA source library | Open the official ACS library |
Official task objective
To determine the applicant exhibits satisfactory knowledge, risk management, and skills associated with a simulated powerplant failure at altitude.
What the ACS code means
- PH identifies the ACS standard family used for this Private Pilot Rotorcraft document.
- VIII identifies Emergency Operations, the Area of Operation.
- B identifies Powerplant Failure at Altitude in a Single-Engine Helicopter, the Task within that Area.
- K, R, and S identify knowledge, risk-management, and skill elements. The number selects the item; a trailing lowercase letter identifies a listed sub-element.
Knowledge elements
| ACS code | Official description | How a mock oral can probe it |
|---|---|---|
| PH.VIII.B.K1 | Elements of a powerplant failure at altitude. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
| PH.VIII.B.K2 | Effects of wind, weight, temperature, and density altitude. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
| PH.VIII.B.K3 | Main rotor (Nr) speed. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
| PH.VIII.B.K4 | Energy management. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
| PH.VIII.B.K5 | Causes and effects of high descent rates. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
| PH.VIII.B.K6 | Effect of varying bank angles, airspeeds, and rotor rpm. | Explain the element, apply it to a scenario, and connect the answer to current references or aircraft information when relevant. |
Risk management elements
| ACS code | Official description | How a mock oral can probe it |
|---|---|---|
| PH.VIII.B.R1 | Low entry altitudes. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R2 | Selection of landing area. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R3 | Flight control inputs. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R4 | Turbulence, including wake turbulence. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R5 | Low rotor rpm or rotor stall. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R6 | Windshear. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R7 | Powerplant failure during the maneuver. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R8 | Collision hazards. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R9 | Autorotation power-off never-exceed speed (VNE) limitation. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R10 | Helicopter trim. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
| PH.VIII.B.R11 | Distractions, task prioritization, loss of situational awareness, or disorientation. | Work through a scenario by identifying the hazard, evaluating the risk, and explaining a practical mitigation or decision. |
Skills elements
| ACS code | Official description | How a mock oral can probe it |
|---|---|---|
| PH.VIII.B.S1 | Establish an autorotation. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S2 | Establish power-off glide with the helicopter trimmed and autorotation airspeed, ±10 knots. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S3 | Maintain main rotor (Nr) within normal limits. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S4 | Select a suitable landing area considering altitude, wind, terrain, and obstructions. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S5 | Maneuver to avoid undershooting or overshooting the selected landing area. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S6 | Make radio calls as appropriate. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
| PH.VIII.B.S7 | Terminate approach with a power recovery at a safe altitude as directed by the evaluator. | Describe the procedure, interpretation, or decision process that can be discussed during an oral. Physical aircraft performance remains part of the practical test. |
Difficulty data
Difficulty calibration is ongoing for this Task. A difficulty estimate is published only with a sufficiently large, privacy-preserving first directly recorded assessment sample. Any observed difficulty comes from Checkride AI mock-oral practice assessments and is a practice-data proxy, not an FAA practical-test pass or fail rate.
Difficulty calibration remains ongoing until an item clears the private reporting threshold. Percentages, when available, describe the share who needed review on their first directly recorded assessment. Underlying sample sizes are never published, and historical final states are not backfilled into this measure.
Official task notes
- Note: See Appendix 2: Safety of Flight and Appendix 3: Aircraft, Equipment, and Operational Requirements & Limitations for information related to this Task.
How to use this in a mock oral
A mock examiner can ask you to explain the published elements, apply them to the configured aircraft and airport scenario, identify risks, and defend a decision. The prompts are practice scenarios; they are not claimed to be actual FAA examiner scripts or a prediction of the questions you will receive.
Related ACS tasks
- All Private Pilot Rotorcraft ACS tasks
49 task-level resources from FAA-S-ACS-15.
- PH.VIII.A — Powerplant Failure in a Hover in a Single-Engine Helicopter
Area of Operation VIII. Emergency Operations
- PH.VIII.C — Approach and Landing with One Engine Inoperative (OEI) (Simulated) (Multiengine Helicopter Only)
Area of Operation VIII. Emergency Operations
- PH.VIII.D — Systems and Equipment Malfunctions
Area of Operation VIII. Emergency Operations
- PH.VIII.E — Vortex Ring State (VRS)
Area of Operation VIII. Emergency Operations