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Prior to flight, the remote pilot in command must: (a) Assess the operating environment, considering risks to persons and property in the immediate vicinity both on the surface and in the air. This assessment must include: (1) Local weather conditions; (2) Local airspace and any flight restrictions; (3) The location of persons and property on the surface; and (4) Other ground hazards. (b) Ensure that all persons directly participating in the small unmanned aircraft operation are informed about the operating conditions, emergency procedures, contingency procedures, roles and responsibilities, and potential hazards; (c) Ensure that all control links between ground control station and the small unmanned aircraft are working properly; (d) If the small unmanned aircraft is powered, ensure that there is enough available power for the small unmanned aircraft system to operate for the intended operational time; (e) Ensure that any object attached or carried by the small unmanned aircraft is secure and does not adversely affect the flight characteristics or controllability of the aircraft; and (f) If the operation will be conducted over human beings under subpart D of this part, ensure that the aircraft meets the requirements of § 107.110, § 107.120(a), § 107.130(a), or § 107.140, as applicable. My Commentary on Section 107.49 Preflight familiarization, inspection, and actions for aircraft operation.I would create a checklist using this regulation. Integrate it with the PAVE and IMSAFE checklists. Advisory Circular 107-2A on Section 107.49 Preflight familiarization, inspection, and actions for aircraft operation.
2. Ensure all persons directly participating in the small UAS operation are informed about the following: • Operating conditions; • Emergency procedures; • Contingency procedures, including those for persons or moving vehicles not directly participating in the operation that enter the operational area; • Roles and responsibilities of each person participating in the operation; and • Potential hazards. 3. Ensure all control links between the CS and the small unmanned aircraft are working properly. Before each flight, the remote PIC must determine the small unmanned aircraft flight control surfaces necessary for the safety of flight are moving correctly through the manipulation of the small unmanned aircraft CS. If the remote PIC observes that one or more of the control surfaces are not responding correctly to CS inputs, then the remote PIC may not conduct flight operations until correct movement of all flight control surface(s) is established. 4. Ensure sufficient power exists to continue controlled flight operations to a normal landing. This can be accomplished by following the small UAS manufacturer’s operating manual power consumption tables. Another method would be to include a system on the small UAS that detects power levels and alerts the remote pilot when remaining aircraft power is diminishing to a level that is inadequate for continued flight operation. 5. Ensure the small unmanned aircraft anti-collision light(s) function(s) properly prior to any flight that will occur during civil twilight or at night. The remote PIC must also consider, during his or her preflight check, whether the anti-collision light(s) could reduce the amount of power available to the small unmanned aircraft. The remote PIC may need to reduce the planned duration of the small unmanned aircraft operation to ensure sufficient power exists to maintain the illuminated anti-collision light(s) and to ensure sufficient power exists for the small unmanned aircraft to proceed to a normal landing. 6. Ensure any object attached or carried by the small unmanned aircraft is secure and does not adversely affect the flight characteristics or controllability of the aircraft. 7. Ensure all necessary documentation is available for inspection, including the remote PIC’s Remote Pilot Certificate, identification, aircraft registration, and CoW, if applicable (§ 107.7). 5.11.2 Safety Risk Assessment. These preflight familiarizations, inspections, and actions can be accomplished as part of an overall safety risk assessment. The FAA encourages the remote PIC to conduct the overall safety risk assessment as a method of compliance with the restriction on operating over any person who is not directly involved in the operation, unless the small unmanned aircraft is eligible for an operation over people in accordance with part 107 subpart D. The safety risk assessment also assists with ensuring the small unmanned aircraft will remain clear of other aircraft. Appendix A provides additional guidance on how to conduct an overall safety risk assessment. ………………………. 7.2.2 Unscheduled Maintenance. During the course of a preflight inspection, the remote PIC may discover a small UAS component is in need of servicing (such as lubrication), repair, modification, overhaul, or replacement outside of the scheduled maintenance period as a result of normal flight operations or resulting from a mishap. In addition, the small UAS manufacturer or component manufacturer may require an unscheduled system software update to correct a problem. In the event such a condition is found, flight operations should not occur until the issue is corrected. ……………………….. 7.3 Preflight Inspection. Pursuant to the requirements of § 107.49, in addition to assessing the intended area of operation and planning the operation as described above in paragraph 5.10, the remote PIC must inspect the small UAS to ensure that it is in a condition for safe operation prior to each flight. This inspection includes examining the small UAS for equipment damage or malfunction(s). This preflight inspection should be conducted in accordance with the small UAS manufacturer’s inspection procedures when available (usually found in the manufacturer’s owner or maintenance manual) and/or an inspection procedure developed by the small UAS owner or operator. 7.3.1 Creating an Inspection Program. As an option, small UAS owners or operators may wish to create an inspection program for their small UAS. The person creating such an inspection program may find sufficient details to assist in the development of a suitable inspection program tailored to a specific small UAS in a variety of industry programs. 7.3.2 Scalable Preflight Inspection. The preflight check as part of the inspection program should include an appropriate small UAS preflight inspection that is scalable to the small UAS, program, and operation that the remote PIC performs prior to each flight. An appropriate preflight inspection should encompass the entire system in order to determine a continued condition for safe operation prior to flight. 7.3.3 Title 14 CFR Part 43 Appendix D Guidelines. Another option and best practice may include opting to comply with the portions of part 43 appendix D. Although part 43 appendix D is technically a maintenance inspection checklist and not a preflight inspection checklist, it provides a logical and systematic approach to performing an inspection by dividing the aircraft into subgroups. It details inspection of the airframe, then the flight controls, then the batteries, then the engine, etc. Unlike manned aircraft that require significant disassembly, most small UAS inspection items are visible without necessitating the need for disassembly. In the absence of a manufacturer’s instructions, an operator may use part 43 appendix D as a guide to develop their own inspection program, but it is not comprehensive, as it does not address unique UAS features like datalinks or support equipment. An operator would need to identify those items not covered and include them in their inspection program. 7.3.4 Preflight Inspection Items. Even if the small UAS manufacturer has a written preflight inspection procedure, the FAA recommends the remote PIC ensure the following inspection items be incorporated into the remote PIC’s preflight inspection procedure. Such a practice will ensure the remote PIC accurately determines that the small UAS is in a condition for safe operation. The preflight inspection should include a visual or functional check of the following items. 1. Visual condition inspection of the small UAS components; 2. Airframe structure (including undercarriage), all flight control surfaces, and linkages; 3. Registration markings, for proper display and legibility (part 48, § 48.205); 4. Moveable control surface(s), including airframe attachment point(s); 5. Servo motor(s), including attachment point(s); 6. Propulsion system, including powerplant(s), propeller(s), rotor(s), ducted fan(s), etc.; 7. Check fuel for correct type and quantity; 8. Check that any equipment, such as a camera, is securely attached; 9. Check that control link connectivity is established between the aircraft and the CS; 10. Verify communication with small unmanned aircraft and that the small UAS has acquired GPS location from the minimum number of satellites specified by the manufacturer; 11. Verify all systems (e.g., aircraft and control unit) have an adequate power supply for the intended operation and are functioning properly; 12. Verify correct indications from avionics, including control link transceiver, communication/navigation equipment, and antenna(s); 13. Display panel, if used, is functioning properly; 14. Check ground support equipment, including takeoff and landing systems, for proper operation; 15. Verify adequate communication between CS and small unmanned aircraft exists; check to ensure the small UAS has acquired GPS location from the minimum number of satellites specified by the manufacturer; 16. Check for correct movement of control surfaces using the CS; 17. Check flight termination system, if applicable; 18. Check that the anti-collision light is functioning (if operating during civil twilight and night); 19. Calibrate small UAS compass prior to any flight; 20. Verify controller operation for heading and altitude; 21. Start the small UAS propellers to inspect for any imbalance or irregular operation; 22. At a controlled low altitude, fly within range of any interference and recheck all controls and stability; and23. Check battery levels for the aircraft and CS. 7.3.5 Benefits of Recordkeeping. Small UAS owners and operators may find recordkeeping to be beneficial. This may be done by documenting any repair, modification, overhaul, or replacement of a system component resulting from normal flight operations, and recording the time-in-service for that component at the time of the maintenance procedure. The operator would then be able to establish a reliable maintenance schedule for the small UAS and its components. The use of hardcopy and/or electronic logbook format for recordkeeping, inclusive of all periodic inspections, maintenance, preventative maintenance, repairs, and alterations performed on the small UAS, is useful in documenting the history of the small UAS. Recordkeeping would include all components of the small UAS, including: small unmanned aircraft, CS, launch and recovery equipment, Command and Control (C2) link equipment, payload, and any other components required to safely operate the small UAS. Recordkeeping of documented maintenance and inspection events reinforces owner/operator responsibility through a systematic means to determine that the small UAS is in a condition for safe flight. Maintenance and inspection recordkeeping provides retrievable evidence of vital safety assessment data defining the condition of safety-critical systems and components supporting the decision to launch. For operators that rapidly accumulate flight operational hours/cycles, recordkeeping of a small UAS may provide an essential safety support. Methodical maintenance and inspection data collection can prove to be very helpful in the tracking of small UAS component service life, as well as systemic component, equipage, and structural failure events. 2020 Over People Regulation Amending the 2016 Rule
2016 Final Small Unmanned Aircraft Rule Discussion on Section 107.49 Preflight familiarization, inspection, and actions for aircraft operation
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