UA.I.E.K16: Impact kinetic energy.
ACS Area I — Regulations Task E: Operations Over People References: 14 CFR parts 89 and 107; AC 107-2; FAA-H-8083-25; FAA-G-8082-22
Key Concepts
Understanding Impact Kinetic Energy in Operations Over People
Impact kinetic energy is a core safety and regulatory concept for operations over people under 14 CFR Part 107. Knowing how to evaluate and apply impact energy thresholds is essential for determining what operations are permitted and for ensuring compliance with Category 2 and 3 requirements. The FAA uses limits on impact kinetic energy as a key method to reduce the risk and severity of injuries in the event of a small unmanned aircraft (sUA) falling onto a person. As such, understanding how kinetic energy is calculated—and how it applies to practical operations—is a major exam topic and an operational requirement for remote pilots.
Calculating Impact Kinetic Energy
Kinetic energy (KE) is a measure of the energy carried by an object due to its motion. For sUAS, kinetic energy upon impact is determined by both the aircraft's weight and its speed at impact, and is calculated using this formula:
KEimpact = 0.0155 × w × v²
where:
- w = weight in pounds (lbs) of the sUA (including all onboard or attached components during operation)
- v = maximum impact speed in feet per second (ft/s)
For example, a 1.0 lb sUAS with a maximum impact speed of 26 ft/s would have an impact kinetic energy calculated as KEimpact = 0.0155 × 1.0 × (26)² = 10.5 ft-lbs. If the speed is increased to 40 ft/s for the same weight, the kinetic energy jumps to 24.8 ft-lbs[4]. This demonstrates the critical importance of both mass and velocity: even a relatively light aircraft can exceed energy thresholds quickly at higher speeds.
Practical Application for Remote Pilots
Part 107 divides operations over people into Categories 1 through 4, with Categories 2 and 3 relying directly on kinetic energy limits as ‘performance-based safety requirements’. This means the aircraft must not exceed a specified maximum impact kinetic energy in the event of a failure or loss of control. Manufacturers and remote pilots must assess the worst-case scenario speeds that could result from system malfunctions, equipment failures, or pilot error, and use the above formula to ensure the sUA remains within allowable limits[4].
Remote pilots are responsible for:
- Knowing the weight of the UAS throughout flight (including temporary payloads or after-market attachments),
- Understanding the potential speed the UAS could reach during uncontrolled descent,
- Verifying that the aircraft is authorized, labeled, and listed as eligible for operations over people in the relevant category,
- Consulting the FAA-accepted Declaration of Compliance (DOC) and manufacturer instructions to stay within permissible impact energy limits[8].
Operational Implications
- Pre-Flight: Always consider the effect of adding or removing payloads, or making modifications that could change the operational weight or falling speed—a heavier or faster aircraft may exceed category limits.
- Category Compliance: Ensure your sUA's impact kinetic energy is below the maximum permitted for the Category of operation (exact thresholds are determined by FAA testing and compliance procedures; do not estimate or invent values).
- Risk Mitigation: The calculation assumes full energy transfer (without accounting for energy-absorbing materials), so a conservative approach is required.
- Documentation: Maintain and review all required documentation, including remote pilot operating instructions and the DOC, prior to operations over people[8].
By mastering the concept of impact kinetic energy and knowing how to monitor and comply with its thresholds, remote pilots can operate safely, responsibly, and in compliance with the law when flying over people.
Test Yourself
UA.I.E.K16No practice questions are currently available for this specific knowledge element.
