The 350B helicopter is part of the Ecureuil/Astar family, manufactured by Airbus Helicopters. The history of this versatile rotorcraft traces back to Aérospatiale, which introduced the initial AS350 models. The second prototype, designated AS350B, successfully completed its maiden flight on February 14, 1975. This model was distinctively powered by a Turbomeca Arriel 1A engine, setting the stage for its global market success outside of North America. The aircraft family is renowned for its reliability and multi-mission capability.
A range of access platforms and solutions are used for comprehensive maintenance across this aircraft. These solutions provide access to critical areas for thorough service.
Access needs are addressed for the: Nose Section, covering the radome, antenna, avionics, cockpit, and bulkhead.
Forward Fuselage, including the main entry door, cargo/baggage area, lighting, cabin access, environmental control systems, and forward wheel well access.
Landing Gear (NLG + MLG), focusing on both the nose and main landing gear.
Middle Fuselage / Wing Box Area, supporting maintenance for the wing box, fuel tanks, oil maintenance points, cabin interior, Wi-Fi systems, and emergency exits.
Wing & Engine Pylon, covering the pylon structure, anti-ice systems, engine (inlet/exhaust), engine body, flaps, fan, compressor, turbine, FADEC/EEC, hydraulics, fuel tanks/pumps, and undercowl access.
AFT Fuselage, including the rear bulkhead, cargo, cabin doors, auxiliary fuel, environmental ducting, rear avionics, and APU compartments.
Tail Section (Empennage), providing access to the APU intake, generator, compressor, exhaust port, vertical stabilizer, horizontal stabilizer, and rudder.
