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Regulatory Requirements for Heavy-Lift Drones:
Weight and Classification: The Unmanned Aerial System (UAS) for agricultural purposes weighs at least 55 lbs (including the weight of the substance being displaced). It falls under the regulations specified in 14 CFR Part 47, which governs Aircraft Registration.
Part 107 Pilot License: To operate the agricultural UAS, you must obtain or already hold a Part 107 Pilot License. This license is issued by the FAA and confirms that you possess the necessary knowledge and skills for safe operation.
Important Updates:
Expiration of Section 44807: The FAA Exemption granted by Section 44807 expired on September 30, 2023. As a result, compliance with all regulations is now mandatory, and previous exemptions are no longer valid.
Remote ID Compliance: Drone pilots have been expected to comply with Remote ID requirements since September 16, 2023. However, the FAA will consider relevant factors to determine enforcement through March 16, 2024.
Additional Information:
For detailed information on the registration process for a UAS under 14 CFR Part 47, obtaining the Part 107 Pilot License, and the steps to become a drone pilot, please refer to the official FAA website. The FAA website provides comprehensive and up-to-date information on UAS operations, regulations, and the necessary procedures.
Note: It is crucial to regularly monitor the official FAA website for any updates or changes in regulations to ensure ongoing compliance with the requirements for operating agricultural drones.
Price
Please contact us for a quote. The total cost is the base price plus tariffs, transportation costs, and taxes. Additionally, actual quotations can be customized according to your needs.
Configuration
Parameters
Body Material
High strength carbon fiber + 7075 aluminum alloy
Diagonal Wheelbase
2,650 mm
Folded Size
980 (L) x 980 (W) x 820 mm (H)
Expanded Size
? (L) x ? (W) x ? mm (H)
Operational Power
51.8V~58.8V
Machine Weight
125 kg (including engine, generator, water cooling system, and 30 L of fuel)
Battery Weight
7 kg
Maximum Payload Capacity
60 kg
Economic Payload Capacity
50 kg
Maximum Takeoff Weight
195 kg
Flight Endurance
100 minutes
50 kg Load Flight Endurance
60 minutes
Total Engine Output Power
30,000 W
Engine Maintenace Time
≥ 300 hours
Standard Load Fuel Consumption
30 L/hour
Flight Control System
Antiseismic dual-core IMU (dual backup)
GNSS, RTK, broken propellor protection, etc.
Flight Hover Accuracy
0.1 m
Wind Resistance
Level 6
Level 8 instantaneous
Flight Speed
0-12 m/s
Flight Altitude
≤ 1200 m (higher altitude will decrease oxygen intake to engine, reducing power)
Climb & Descent Rate
3-5 m/s
Video Remote Control Distance
30,000 m (visible distance)
Flight Mode
Manual, GPS, and autonomous flight
Status information display
APP Intelligient Ground Station
Operating Temperature
-30°C to 65°C
Extended Functions Supported
Transporation, firefighting, communications, rescue, etc
