LATEST GENERATION CAPABILITIES

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1 Offshore AW189

2

3 LATEST GENERATION CAPABILITIES 2

4 DELIVERING PRODUCTIVITY Belonging to the AWFamily of products the AW189 is designed for long range, all-weather, day and night, deep water missions typical of Offshore operations, maximising operational capability and minimising cost. The AW189 features a bright spacious constant section cabin and exceeds the airworthiness requirements of the most recent EASA/FAA amendments in the transport category (Part 29), qualifying the aircraft for the most stringent guidelines of the major OGP companies. The AW189 also benefits from an industry-leading 50 minutes dry-run capability on the main gearbox. Our Customer Support & Training Global Network provides AW189 operators a range of Service Plans and a state-of-the-art training capability, maximizing operational safety and availability. LEADING FEATURES Fully articulated main and tail rotors Fully integrated avionics system, with four 8 x 10 color active matrix liquid crysal displays (AMLCD) HTWAS and TCAS II Weather Radar Landing and taxing lights Emergency Floats (up to Sea State 6 ditching capability) AW189: SAFETY BY DESIGN Structural crashworthiness integral to the design of the airframe, fuel system and seats, a reinforced windscreen and optimum position of critical controls, which mitigates the consequences of a birdstrike. The cockpit design incorporates latest generation, advanced situational awareness technologies (HTAWS, TCAS II, ADS-B Out, Fight Data Monitoring) which reduce crew workload. Advanced Helicopter Usage and Monitoring System (HUMS) diagnostic tools continuously monitor systems, further enhancing safety and reducing time on the ground. High main rotor clearance ensures a safe environment for ground operations and maintenance crew. Seats aligned to large push-out windows (Exceeding Type IV) to maximise egress speed. Flotation system is certified for ditching up to Sea State 6 and life rafts are positioned for access directly from the cabin or from outside.

5 Two GE engines 2000 shp per engine Dedicated 60 kw Auxiliary Power Unit (APU) ADELT Wide sliding doors External Life Rafts READY FOR MISSION Typical Offshore Passenger Configuration comprises: 16 individual crashworthy seats with separate four point safety belts External life rafts (2 x 21) with emergency JTSO 126 beacon ADELT JTSO 126 Emergency floats (up to Sea State 6 ditching capability) Helicopter Emergency Exit Light System (HEELS) HUMS and Flight Data Monitoring (FDM) as standard VHF/FM radio Satcom with Flight Following Environmental Control System TCAS II Weather radar Optional Equipment includes: Full Ice Protection System (FIPS) or Limited Ice Protection System (LIPS) for operations in icing conditions, pressure refuelling, single/dual hoist, search light, mission console, nose-mounted FLIR and cargo hook for Limited SAR operations. 4

6 SPACE AND ACCESSIBILITY The AW189 benefits from the largest cabin in its class (11.2 m 3 / ft 3 ), featuring: Large, flat floor space, with accommodation for up to 19 passengers disposed on 4 rows Seat rows aligned with emergency exit windows Different internal layouts with easy and fast conversion for maximum flexibility Low vibration and noise levels Capability to rapidly install equipment for Limited SAR (Lim. SAR) operations Large sliding doors for simultaneous and quick passenger entry and egress from all 4 seat rows Large baggage compartment (2.4 m 3 / 85 ft 3 ), accessible from both helicopter s sides.

7 AW189 CHARACTERISTICS Weights Max Gross Weight 8,300 / 8,600 kg 18,298 / 18,960 lb Propulsion Powerplant 2 x General Electric CT7-2E1 Turboshafts with FADEC (2,000 shp class each) and 1 x APU (60kW) Engine Ratings Take off power (5 min) 2 x 1,479 kw 2 x 1,983 shp Maximum Continuous Power 2 x 1,395 kw 2 x 1,870 shp Seating Crew 1-2 Passengers Up to 19 (16 for OGP standard) External Dimensions Overall length (1) m 57 ft 9 in Overall height (1) 5.06 m 16 ft 7 in Rotor diameter m 47 ft 11 in Performance (ISA, S.L., MTOW) VNE (IAS) 313 km/h 169 kt Max cruise speed 287 km/h 155 kt Hovering OGE 2,673 m 8,770 ft Maximum range (2) 889 km 480 nm Maximum endurance (2) 4 h 30 min (1) Rotors turning (2) No reserve, with under floor and transversal auxiliary fuel tanks 6

8 Leonardo - Società per azioni Registered Head Office: Piazza Monte Grappa, Rome - Italy Tel Fax Leonardo Helicopters Head Office: Via Giovanni Agusta, Cascina Costa di Samarate - Italy Tel Leonardo - Società per azioni This document contains information that is proprietary to Leonardo - Società per azioni and is supplied on the express condition that it may not be reproduced in whole or in part, or used for manufacture, or used for any purpose other than for which it is supplied. leonardocompany.com

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