Specifications
Broker
EUROTECH S R L
AI Description
- Fresh 12Y inspection extension completed in May 2022 at 600 hours.
- Main rotor blade and spindle assembly with an expiration of September 2028, total time since new (TSN) of 495 hours.
- Main gearbox (MGB) time since overhaul (TSO) of 1133 hours.
- Clutch assembly TSO of 65 hours.
- Tail rotor blades TSN of 65 hours, expiration in May 2036.
- Avionics include two 8.33 Garmin COM radios (GTR225A and GTR225B), radar altimeter, artificial horizon, turn indicator DG, Garmin Mode S transponder, and Kannad 406 compact ELT.
- Additional equipment: air conditioning, emergency floats, special corrosion factory prevention treatment, wind/water deflectors, four yacht tiedown rings, extended high gear (Clipper II), leather interior, and factory-installed Icom marine radio (IC-M422).
- Operating under VFR flight rules.
- Airworthy condition confirmed.
About this Model
Overview
The Robinson R44 Clipper II is a light, single-engine piston helicopter in the R44 family, aimed at owner-operators, flight schools, and commercial operators needing a straightforward four-seat platform. It emphasizes practical payload-and-range capability for regional trips, aerial work support, and frequent-cycle utilization, with operating economics typically associated with piston rotorcraft rather than turbine models.
Mission Fit
The Clipper II tends to fit missions where simplicity, predictable handling, and moderate trip lengths matter more than all-weather capability or turbine-class performance. Typical use cases include day VFR travel, repeated training sorties, and visual aerial work where the aircraft’s size and operating costs are central to the mission.
Cabin
The R44 cabin is a compact four-seat layout with two front seats and a rear bench. Entry is via side doors, and the cabin is oriented toward visibility and accessibility rather than executive comfort. Cabin loading is sensitive to fuel quantity and occupant weights, so real-world comfort and baggage capacity depend heavily on the planned fuel load and density altitude conditions.