ANAC RBAC 100 Remote Pilot flashcards
ANAC RBAC 100 Remote Pilot · Build recall with a focused review session.
32 cards. Read the term and the definition here. The deck at the top of this page is optional.
- RBAC 100
- Brazilian regulation for civil remotely piloted aircraft, defining operational classes by maximum takeoff mass and the registration, licensing, and authorization requirements for UAS operations in Brazil.
- RPA registration threshold
- RPA with maximum takeoff mass above 250 g must be registered with ANAC through SISANT, and the registration number must be displayed on the aircraft and available during operations.
- Remote pilot license
- ANAC-issued license required for pilots of RPA above 25 kg, or operating BVLOS, or above 400 ft AGL; it requires a medical certificate and a recognized competency assessment.
- ICAO Annex 2
- Annex containing the rules of the air, including right-of-way rules; RPA must give way to manned aircraft, and an aircraft in distress has priority over all others.
- Class G airspace
- Uncontrolled airspace where no ATC clearance is required; see-and-avoid and right-of-way rules apply, and RPA operations still require compliance with RBAC 100 limits.
- 400 ft AGL limit
- Standard maximum altitude for RPA operations under RBAC 100; operations above this limit require specific ANAC authorization and coordination with the responsible ATS unit.
- ATZ coordination
- Operations within the aerodrome traffic zone or control zone require prior coordination with the aerodrome operator and ATC; the typical protected radius is 9 km (5 NM).
- VLOS default
- The remote pilot must maintain direct unaided visual contact with the RPA; beyond visual line of sight operations require specific authorization and, where applicable, detect-and-avoid capability.
- Density altitude
- Pressure altitude corrected for temperature and humidity; higher density altitude reduces air density, propeller thrust, and lift, degrading RPA performance during takeoff and climb.
- Wind limit rule
- Small multirotor RPA typically have a maximum safe wind limit of about 8–10 m/s (15–20 kt); operations should be suspended when gusts exceed the manufacturer's demonstrated limit.
- Thunderstorm avoidance
- A 20 km (10 NM) avoidance margin from cumulonimbus clouds is a common operational rule; operations should be suspended when lightning is within 10 km of the operating area.
- Lithium-polymer cold effect
- Battery capacity drops significantly below 0 °C and above 40 °C; battery temperature should be checked before flight to avoid voltage sag and sudden power loss.
- Maximum takeoff mass
- The maximum mass at which the RPA is approved for takeoff, including airframe, batteries, payload, and installed equipment; it must never be exceeded in any configuration.
- Center of gravity envelope
- The manufacturer-specified range of CG positions within which the RPA is controllable; loading must keep CG inside this envelope, and any configuration change requires verification.
- Battery reserve rule
- A common planning rule is to reserve at least 20% of battery capacity for contingencies and landing, accounting for wind, temperature, and unexpected delays.
- Load factor limit
- The maximum g-load the RPA structure is designed to withstand, typically 2–3 g for small RPA; abrupt maneuvers and gusts can exceed this and cause structural failure.
- GNSS signal quality
- Satellite availability and HDOP/VDOP must be verified before flight; poor geometry degrades position accuracy, and the pilot must have a contingency for GNSS loss.
- Return-to-home altitude
- The pre-set altitude the RPA climbs to before returning to the launch point; it must be set above the tallest obstacle in the operating area to avoid collisions.
- Geofence
- A software-defined boundary that limits where the RPA can fly; it must match the authorized operating area and is a key barrier against airspace violations.
- Coordinate formats
- Latitude and longitude can be expressed in decimal degrees or degrees-minutes-seconds; the pilot must know the format used by the navigation system and ATS unit.
- Risk matrix
- A tool combining likelihood and severity to assess risk; the operation is acceptable only if residual risk after mitigations is tolerable, and the assessment must be documented.
- Lost link procedure
- The RPA executes a predefined action, typically return-to-home or hover and land; the pilot monitors the RPA and coordinates with ATC if operating in controlled airspace.
- Fly-away response
- The pilot should not chase the RPA; instead, notify ATC, record the last known position, and follow the operator's emergency plan, including reporting to ANAC and CENIPA.
- Accident reporting
- Accidents involving injury or damage must be reported to CENIPA and ANAC; the operator must preserve evidence and cooperate with the investigation.
- Situational awareness
- The perception and understanding of the operational environment; its loss is a leading factor in UAS accidents, especially in BVLOS and high-workload phases.
- DECIDE model
- A structured decision-making model: Detect, Estimate, Choose, Identify, Do, Evaluate; it helps pilots make systematic in-flight decisions under time pressure.
- Just culture
- A safety culture that encourages reporting of errors and near misses without fear of punishment, improving safety data and prevention of future accidents.
- Read-back requirement
- Clearances and instructions that affect safety must be read back to the issuing controller to confirm correct understanding and reduce communication errors.
- MAYDAY and PAN-PAN
- MAYDAY is the distress call for grave and imminent danger; PAN-PAN is the urgency call for a serious but non-immediate situation; both require position and intentions.
- C2 link
- The command and control data link between the control station and the RPA; it must be monitored for signal strength and latency, with a procedure for degradation.
- Propeller thrust relation
- Thrust is proportional to propeller speed squared and to air density; high density altitude reduces available thrust, limiting payload and climb performance.
- Flight controller modes
- Manual, attitude, GPS, and autonomous modes offer different automation levels and failure responses; the pilot must be proficient in switching between them.