Light, single-engine utility helicopter optimized for simple operations and flexible mission equipment.
The Airbus AS 350BA (AStar) is an earlier variant of the AS350 family, positioned as a straightforward, work-oriented single-engine helicopter with a broad operating envelope for day-to-day utility flying. Buyers typically consider it when they want a proven airframe that can be configured for passenger transport, aerial work, or public-service-style missions, and when they value a simpler single-engine operating model over twin-engine redundancy.
Currently for saleIn service use, the AS 350BA tends to fit missions that prioritize access, hovering and low-speed maneuvering, and the ability to switch between passenger and work configurations. It is commonly selected for operations that benefit from a practical cabin, good external visibility, and compatibility with common role equipment. It is less aligned with missions that are dominated by cruise speed, long legs without refueling, or requirements that effectively drive operators to twin-engine types.
Cabin experience is functional rather than luxury-oriented: the aircraft is generally configured to move a small group plus pilot, with easy loading and good visibility. Comfort, noise levels, and finish vary significantly by interior package and the aircraft’s utility history. Door configuration and seating choices can materially affect how quickly you can reconfigure between passenger and work missions.
The AS 350BA reflects a practical, analog-first design typical of its era, often updated over time with targeted avionics and mission equipment rather than a fully integrated, factory-modern flight deck. Many aircraft in the fleet have been modified to match local regulatory needs (e.g., radios, navigation, transponder/ADS-B solutions) and operator preferences, so the specific aircraft’s equipment list matters more than the type’s baseline.
11,100 nm from New York
Airbus AS 350BA (AStar) — 11,100 nm range
Operationally, a light single like the AS 350BA is usually optimized for frequent short sectors, hovering/low-speed work, and operations from constrained or unimproved sites within performance planning limits. Real-world endurance and range depend heavily on fuel configuration, payload, temperature/altitude, and how much time is spent hovering versus cruising. If your missions involve high-altitude/high-temperature conditions, confirm performance margins for your expected loads and procedures.
Maintenance planning is driven by airframe and dynamic-component life limits, engine condition, and the depth/quality of historical records. As an older variant, individual aircraft condition and modification status can vary widely. A thorough records review and inspection focus on the dynamic system, corrosion/hard-use indicators, and compliance with applicable service bulletins and airworthiness directives for the specific serial number and installed equipment.