Technical Data DAUPHIN. (Civil Version) AS365 N3+ PANTHER. (Military Version) AS565 MBe

Transcription

1 2016

2 DAUPHIN (Civil Version) AS365 N3+ PANTHER (Military Version) AS565 MBe

3 Contents 1 Foreword General Characteristics Cockpit and Cabin Layouts Weight Power Ratings Fuel Capacities External Dimensions Internal Dimensions High Performance ARRIEL 2C Engine STARFLEX Main Rotor: reliability and simplicity FENESTRON Tail Rotor: safety and discretion Instruments Automatic Flight Control System Baseline Aircraft Definition Mission Configurations Oil & Gas Favorite VIP Favorite Executive Favorite Public Services Favorite SAR Favorite Main Performance Service and Support Information Assets Inspection Programs Main Components TBO/ SLL Technical Support HCare Material Management Engine Maintenance Program Training Technical Publications Technical Information Publication on Internet (T.I.P.I.) Customer Flight Operations Support & Services Abbreviations N E 1

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5 1 Foreword The AS365 N3+ belongs to the famous DAUPHIN family. It is a medium twin engine helicopter of 4,300 kg Maximum Take-Off Weight based on the type certificate of AS365 N3. The AS365 N3+ is a powerful and fast helicopter that provides outstanding performance and long range capabilities. Its two Turbomeca ARRIEL 2C turbine engines fitted with Full Authority Digital Engine Control System (FADEC), makes it a helicopter particularly well adapted for operations in high altitude and hot countries. In order to ease the crew workload, the AS365 N3+ has been fitted with the unique Airbus Helicopters dual digital 4-axis Autopilot, APM 2010, also implemented on EC145 T2, EC155, EC175, EC225 & EC725. This state of the art AFCS is the 1st Autopilot ever designed specifically for helicopters. As a fly-through system, it offers no resistance to pilot initiated override maneuvres and maximizes safety and mission efficiency. For more practicality, the main instrument panel is equipped with a 10.4 inches mission display touch screen that relays the information brought by the various dedicated mission equipment such as the DMAP, EOS, Radar, TCAS, EGPWS, DF... Thanks to its versatile cabin, the AS365 N3+ can operate different missions like Offshore, VIP, Executive, Public Services, EMS, Surveillance and Full SAR (Day & Night) operations. Its useful volume can be fitted with various seating arrangements to accommodate up to 12 passengers plus 2 crew members. A wide range of optional equipment contributing to increase safety and mission efficiency, such as Flight Management System or SAR modes are proposed. 365 N E 3

6 The AS365 N3+ also incorporates the new generation, all composite FENESTRON tail rotor that provides high maneuvrability, exceptional efficiency at all speeds, and unparalleled ground & in flight crew safety, with a low sound level making it the quietest in its category. Over 1050 units of the DAUPHIN family have been delivered to date, cumulating more than 5,996,200 flight hours. The AS365 N3+ complies to the latest offshore regulations. In case of ditching, the helicopter is notably certified for water landing in the harshest conditions (up to sea state 6). Technical advancements developed by Airbus Helicopters on the AS365 N3+ include modular design of the mechanical assemblies, use of composite materials (STARFLEX rotor head, blades, airframe...) which has led to significant maintenance reduction. Airbus Helicopters is deeply aware that the majority of the cost of ownership is incurred over the operational life of the helicopter. Indeed, as much as 60 % of the life cycle costs occurs during the in-service phase. For this reason, reliability, maintainability and supportability are the cornerstones of the design of all Airbus Helicopters products. The basic AS365 N3+ vehicle design is based on the concept of Reliability Centered Maintenance and, as such, embodies a modern concept of dynamic assemblies and systems, use of composite materials, redundant systems and unlimited service life of main components. The AS365 N3+ possesses designed-in maintainability with numerous interchangeable parts that can be replaced quickly to ease maintenance and reduce down time. The main components (engines, main rotor head, main gearbox) have a modular design and are directly accessible, with minimum requirements to remove other components of the helicopter N E

7 2 General Characteristics 2.1 Cockpit and Cabin Layouts Minimum crew VFR : IFR : Transport Passengers VIP Executive Medevac single/ dual pilot single/ dual pilot up to 12 passengers with comfort seats up to 7 passengers with VIP layout up to 8 passengers with Executive layout up to 2 medical stretchers 1 and 4 seats 2.2 Weight kg lb Empty weight, Baseline Aircraft Definition 2 2,374 5,234 Maximum Take-Off Weight (MTOW) 4,300 9,480 Maximum Take-Off Weight with external load 4,250 9,370 Maximum cargo-sling load 1,600 3,527 Note : Empty weight accuracy: within 2 %. 2.3 Power Ratings 2 x Turbomeca ARRIEL 2C turboshaft engines All Engine Operative (AEO) kw shp Take-Off Power (TOP) Maximum Continuous Power (MCP) One Engine Inoperative (OEI) kw shp OEI 30s OEI 2 min OEI continuous Note : Thermodynamic values per engine, in standard atmosphere, at sea level 2.4 Fuel Capacities Usable Fuel liters US gal kg lb Standard fuel tanks 1, ,977 Auxiliary fuel tanks (option) Medical installation, including Stretcher(s) can be purchased separately on request, and certified under STC. Baseline aircraft empty weight includes oil and unusable fuel. 365 N E 5

8 2.5 External Dimensions (*) Height at MTOW Dimensions with blades folded N E

9 2.6 Internal Dimensions Cabin main dimensions: CABIN Surface 4.20 m² sq ft Volume 5.10 m cu.ft HOLD Surface 2.25 m² sq ft Volume 1.10 m cu.ft Cockpit and cargo doors: The luggage hold is accessible from the RH side of the helicopter. The cockpit is accessible through two jettisonable hinged doors. 365 N E 7

10 2.7 High Performance ARRIEL 2C Engine... with : modular design, for an easier maintenance, blade shedding and FADEC, for an increased safety. 1 axial compressor (1) 1 single-stage free turbine (6) 1 one-stage centrifugal compressor (2) 1 outlet diffuser (7) 1 through-flow annular combustion (3) chamber 1 reduction gearbox (8) with centrifugal fuel injection system 1 shielding rings for the turbines (9) 1 single-stage monocristal blade (4) 1 coupling shaft (10) generator turbine 1 accessory gearbox (11) 1 rear bearing (5) The ARRIEL 2C is controlled by a Full Authority Digital Engine Control (FADEC), which controls the power turbine constant speed, whatever the power drawn from the engine by continuous accurate adjustment of the gas generator speed. In addition, the FADEC controls some automatic functions (Automatic engine starts / shut-down sequences, acceleration / deceleration control of the engine preventing surge / flame out, in-flight automatic restart and engine maintenance aid), offering the latest safety standards in engine technology N E

11 2.8 STARFLEX Main Rotor: reliability and simplicity With a diameter of m (39.17 ft), the main rotor includes a STARFLEX type rotor head and four fibreglass blades rotating clockwise (as viewed from above) at a nominal speed of r.p.m. for an engine output speed of 5,990.4 r.p.m. This speed varies between 347 and 365 r.p.m. in flight (except in autorotation flight). The STARFLEX rotor head combines simplicity and reliability: very few parts among which the main elements are fibreglass / carbon fiber composite (fail safe design) no bearing no lubrication Main Rotor Blades: The main rotor blades take benefit of a 30 year-experience in composite material blades. Immune to scratches and notches, corrosion free and impact resistant they are individually interchangeable and manually foldable. 1 - Blade tip cap 2 - Balancing weights 3 - Stainless steel strip 4 - Glass carbon fibre cloth 5 - Bushings 6 - Tab 7 - Fibreglass-roving spar 8 - Moltoprene filler 9 - Integrated weight 10 - Balancing weight support 11 - Bonding strip 365 N E 9

12 2.9 FENESTRON Tail Rotor: safety and discretion The FENESTRON tail rotor provides outstanding characteristics compared to classical tail rotors: safety on ground: with nearly 30 years in operation, no injury to ground personnel was reported, discretion: the 10 blades are unevenly distributed around the rotor hub to reduce the sound level, safety in flight: tail fin asymmetrical profile design provides anti-torque thrust. Tail Rotor Blades: The 10 rotor carbon fibre composite blades take advantage from Resin Transfer Molding advanced technology and are individually-interchangeable N E

13 2.10 Instruments (*) Optional equipment, included in all mission favorite configuration Note: Depending on the optional equipment to be installed, the instrument panel here above may be customized and some equipment relocated. Instrument-panel equipment: 2 Collins MFD-255 Primary Flight Displays (PFD) 2 Collins MFD-255 Navigation Displays (ND) 1 stand-by gyro-horizon 1 stand-by altimeter 1 stand-by airspeed indicator 1 dual torquemeter 2 engine T4 indicators 2 engine oil temperature indicators 2 engine oil pressure indicators 2 fuel pressure indicators 2 hydraulic circuit 1 and 2 pressure indicators 1 MGB oil pressure indicator 1 MGB oil temperature indicator 1 voltmeter 1 ammeter 1 dual fuel gauge 2 stopwatches 1 triple tachometer (rotor and engine 1 and 2 free wheel r.p.m) 1 rotor r.p.m tachometer 2 engine 1 and 2 Ng indicators 1 electric and hydraulic power generation control panel 1 landing gear monitoring and control panel 1 warning panel 2 master alarm warning lights 2 manoeuvring limit (or torque limit, or gas generator r.p.m deviation limit) warning lights 1 "landing gear not extended" warning light 1 stand-by magnetic compass Console equipment: 1 Auto Pilot Mode Selector (APMS) control box 1 Attitude and Heading Reference Sensor (AHRS) control box 1 fuel circuit control and monitoring panel 1 landing light selector 1 landing gear brake control handle 1 nose wheel caster lock handle 3 breaker panels Main overhead panel standard equipment: 1 engine control panel with 2 fire warning lights and 2 dual fire extinguisher controls for engine bays lighting controls ventilation / heating system controls AFCS collective trim switch AFCS cyclic trim switch mission selector (winch or cargo) 365 N E 11

14 2.11 Automatic Flight Control System Through the years, Airbus Helicopters has developed unique competencies in AFCS software design. With the APM2010 computer, it has developed the most advanced autopilot specifically designed for helicopters. Airbus Helicopters Automatic Flight Control System is a sophisticated digital 4-axis autopilot that offers no resistance to pilot initiated override manoeuvres and provides an utmost safety thus making flying a child s play. Taking into account the parameters supplied by the Air Data Computers, the AFCS determines the helicopter Flight envelope with VNE (Velocity Never to Exceed) and Vy (Optimum Rate-of-Climb) to prevent the helicopter from exceeding the flight envelope. This AFCS provides unique functionalities : Unrivalled mission effectiveness: Supports pilot task when all engines operative: 4-axis collective management optimized for cruise flight, using the Upper modes, such as: ALT, HDG, IAS, ALT.A, V/S, Go-Around, VOR, NAV, LOC, G/S, Cruise Height. Thanks to the "4-axis" mechanization, multiple combinations of these modes are available, No more speed limitation for Automatic ILS approach, No more up and down variations during speed reduction in automatic ILS procedures, No more trimming of cyclic for pilots below 30 kts thanks to effort detection and Automatic Trim follow-up, No altitude limitation for 4-axis use. Supports pilot task for SAR operation (SAR modes to be ordered separately): Fully automatic transitions to hover Unrivalled precision and stability of automatic hover leading to faster rescue and safer hoisting procedures Automatic hover possible over ships and over land Unrivalled safety, supports the pilot should one engine fail: Automatic management of 1 engine failure with priority to maintain altitude Automatic Emergency go-around procedure in case of engine failure during hoisting The AFCS is controlled through one Autopilot Mode Selector (APMS), installed on the central console in the sight area of both pilots, the cyclic and collective grips pushbuttons and the overhead panel controls. The Autopilot Module (APM) provides fully coupled Autopilot function in pitch, roll, yaw and collective axis, providing the basic stabilization and the upper modes functions in the same unit. The AFCS receives the information acquired and consolidated by the MFD's (data centralizer), such as, glide/localizer deviations, VOR bearing, selected course, roll steering command, radio height. It receives also engine information such as Free Turbine speed, torque, NG and T4. Note: A Stability Augmentation Sub-mode (SAS) function (Back-up mode) allows the pilot to take over; when the auto-trim function is disabled, the basic AFCS provides stabilit augmentation on pitch, roll and yaw axis using the series actuators N E

15 In SAR mission configuration, the AFCS is completed with the SAR modes option to better support pilots tasks during SAR operations. The unrivalled precision and stability of automatic hover it provides enable faster rescues and safer hoisting procedures. The SAR modes include : GSPD : Ground speed acquisition and hold HT/HOV : Autonomous transition down or hover height acquisition and hold F/TDN : Automatic transition down to hover (Trans-Down) TUP : Automatic transition from the hover to acquisition and hold of a predefined radar height and airspeed (Trans-Up) Note: Taking into account the parameters supplied by the Air Data Computers the AFCS determines the helicopter flight envelope with VNE (Velocity Never to Exceed) and Vy (Optimum Rate-of-Climb) to prevent the helicopter from exceeding the flight envelope (flight envelope protection). Moreover the AFCS provides the crew with an on-ground adjustable safety speed (Vtoss) through pitch beep in order to manage an engine failure from the hover (GA mode). 365 N E 13

16 3 Baseline Aircraft Definition N E

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18 4 Mission Configurations Airbus Helicopters proposes different mission configurations for the AS365 N3+. The benefits for the customer are a state of the art helicopter that complies with current operational and regulation requirements. According to this standardisation approach, the helicopter configurations are built the following manner: A standard mission configuration An interior layout (to be selected in the Mandatory Equipment List) Mission Equipment to be chosen from the Further Available Equipement List Two core avionics suites are proposed. The first one includes the Garmin GNS 430W suite, and is dedicated to missions which cover Offshore, VIP, Executive and Public Services roles. The second one, including the Collins Proline 21 suite coupled with the FMS CMA 9000, is dedicated to SAR role. These two core avionics suites are completed with optional equipment complying with the specific mission. The standard mission cannot be modified and must be completed with one interior layout to be chosen from the Mandatory Equipment List. Finally, Further Equipment Available may be added, for further customisation depending on mission s needs. The AS365 N3+ standard mission configurations are: Oil & Gas Offshore passenger transport Executive passenger transport Public Services SAR mission In the same philosophy a recommended configuration is proposed for VIP transport: VIP passenger transport Any modification and/or complement of the proposed mission configuration must be done in with assistance of an Airbus Helicopters sales representative N E

19 4.1 Oil & Gas Favorite The AS365 N3+ Oil & Gas standard configuration is basically fitted with all the mission equipment necessary for transport missions over seas (emergency floatation gears, heels, ADELT) as set by the EASA-OPS regulations. In addition to these equipment, Airbus Helicopters has endowed the AS365 N3+ with the highest level of safety : it is now certified for water landing up to sea state 6, its SSCVFDR is ED-112 compliant, and a cockpit camera has been added in all configurations thus answering the latest safety and certification requirements. Up to 12 passengers in cabin. Lowest maintenance level in its category. Eased maintenance & monitoring thanks to the UMS, HUMS & QAR systems. Proven and mature aircraft which benefits from a continuous improvement product policy : it has for example recently been certified to stand water landings up to sea state N E 17

20 4.1.1 Oil & Gas Standard Configuration Document reference Commercial reference Description kg lb A CI Standard Utility and Transport Configuration A CI AS365 N3+ Baseline Aircraft as per 365 N E A CI Enhanced offshore anti-corrosion protection A CI Windshield washer A CI Fuel flowmeter, displayed on GPS Garmin GNS 430W A FP Goodrich Category 1 electrical Hoist (272 kg - 88 m) - Fixed Parts A FP Rappelling installation (ropes excluded) - Fixed Parts A CI Under fuselage anti-collision strobe light A CI Lightweight Aircraft Recording System - Appareo Alerts Vision A CI Emergency Locator Transmitter KANNAD - Integra 406 AP- (ER) with GPS connection A CI Digital Audio Communication System NAT with 2 control panels A CI Third control panel for NAT Digital Audio Communication System A CI Passengers address NAT AA with 4 loudspeakers A CI Passenger interphone linked to DACS for 12 passengers A CI David Clark H10-13 H headset (Qty 2) A CI Two additional ICS jacks in cockpit for Bose Aviation headsets (headsets excluded) A CI Transponder (Mode S) - Garmin GTX 330 ES - ADS-B_OUT- NRA A CI ADF - Collins ADF-4000 (displayed on MFD255) A CI DME Collins DME (displayed on MFD-255) A CI Marker beacon receiver - Honeywell KR A CI Weather/search radar Telephonics RDR-1600C (displayed on MFD 255 and 10.4" screen) A CI TCAS Goodrich / L3 Com SKYWATCH HP (displayed on 10.4" screen) A CI VHF/VOR/LOC/GS/GPS n 1 Garmin GNS 430W A CI VHF/VOR/LOC/GS/GPS n 2 Garmin GNS 430W A CI Moving map EUROAVIONICS EURONAV VII, linked to GPS (displayed on 10.4" screen) A CI Mission display 10,4" A CI Solid State Cockpit Voice & Flight Data Recorder - L3COM SSCVFDR with MFDAU A CI UMS - complement of SSCVFDR (usage functions) with MFDAU++ Ground station excluded N E

21 4.1.2 Mandatory Equipment Document reference General Package Commercial reference Description kg lb A CI Oil & Gas Package A CI First aid kit - EASA Ops compatible A CI 2nd fire extinguisher A FP Emergency floatation gear with automatic percussion Fixed parts A RP Emergency floatation gear with automatic percussion Removable parts A FP External Aerazur life rafts inst. (2 x 10 pax) with ELT compart (ELT not included) - Fixed Parts A RP External Aerazur life rafts inst. (2 x 10 pax) with ELT compart (ELT not included) - Removable Parts A CI Helicopter Emergency Egress Lighting (HEEL) A CI Automatic deployable Emergency Locator Transmitter (ADELT) HR SMITH series 503 with GPS connection A CI Personal Locator Beacon HR Smith PLB 500 series (Qty:2) A CI EGPWS Honeywell MK XXII (displayed on 10.4" screen) A CI HUMS - complement of UMS (health functions) with MFDAU A CI QAR (Quick Access Recorder) for HOMP - with MFDAU Interior Layout A CI 12-seat layout with 4-point harnesses A CI 8-seat layout with 4-point harnesses A CI 11-seat layout with 4-point harnesses Further Available Equipment Document reference General Equipment Commercial reference Description kg lb A CI Customized external paint A CI High visibility markings of the main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Sand prevention filters, dynamic type - Fixed parts A RP Sand prevention filters, dynamic type - Removable parts A CI Re-inforced sand erosion protection strip on main rotor blades A CI Air conditioning system (split) A CI Icing detector (Rosemount) A FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Fixed Parts A RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Removable Parts Specific Mission Equipment A RP Goodrich Category 1 electrical Hoist (272 kg - 88 m) with electrostatic discharge protection - Removable Parts A RP Rappelling installation (ropes excluded) - Removable Parts A FP Cargo sling with dynamometer & ext mirrors (1,600kg), ext liferaft compatible - Fixed Parts A RP Cargo sling with dynamometer & ext mirrors (1,600kg), ext liferaft compatible - Removable Parts A CI Under Water Acoustic Beacon DUKANE DK 120 / N E 19

22 Further Available Equipment (Continued) Interior Layout A CI Complement for 12-seat layout with 4-point harnesses Requires CI A CI Complement for 11-seat layout with 4-point harnesses Requires CI A CI Headrest (Qty 8) Avionics A CI David Clark H10-13 H headset (qty 1) Quantity to be defined, following the number of passengers or crews A CI Active noise cancelling headsets Bose A20 (qty 1) Quantity to be defined, following the number of passengers or crews A CI Weather radar RDR 2000 Honeywell (displayed on MFD 255 and 10.4" screen) A CI Weather/search radar Telephonics RDR-1600C removed from the Standard Utility and Transport Configuration A CI Automatic hover & ground speed modes A CI Hoist operator joystick for automatic hover & ground speed modes Avionics equipment choice : Only one on three equipment can be selected in additoin to the above installations A CI HF/SSB Collins HF A CI VHF/FM NAT NPX A CI Satcom IRIDIUM Skyconnect (voice and A/C position) control in cockpit only N E

23 4.1.4 Performance Data Mission Profile Take-off at MTOW (Cat. A Clear Area) Outbound flight: climb + cruise at 5000ft at VBr Fuel allowance for operation on platform Inbound flight climb + cruise at 5000ft at VBr Reserve: 10% of the mission fuel + 30 min at VBe, 1500ft (EASA-OPS) Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, standard Oil & Gas Offshore Configuration 2,801 6,175 with 8-seat layout (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg, EASA-OPS PART CAT) Maximum Take-Off Weight 4,300 9,480 Useful load 1,345 2,900 Fuel tanks capacity Standard fuel tanks 897 1,977 Passengers vs. Radius of Action in standard Oil & Gas Offshore configurations at ISA. 365 N E 21

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25 4.2 VIP Favorite In its VIP version, the AS365 N3+ has been designed to offer the maximum level of comfort to the passengers during their flight: the cabin is fitted with a specific enhanced sound proofing system and two hinged doors replace the standard sliding doors thus providing spacious storage compartments. No partition separates the cabin from the cockpit which allows direct communication with the pilots and visibility of the instrument panel and through the windshield. Three-seat-divan Easy deck landing thanks to the small foot print of the AS365 N3+. Interior layouts proposing various divan and seat-bench combinations are available. Touch screen for a rapid and easy intercommunication management. Two-seat-bench Cabin customisable at customer s preferences: seat designs, materials and fabrics, colors and finishings are selectable among a wide list of choices. 365 N E 23

26 4.2.1 VIP Recommended Configuration Document reference Commercial reference Description kg lb A CI Recommended VIP Transport Configuration A CI AS365 N3+ Baseline Aircraft as per 365 N E A CI Limousine window panes in the cabin (for hinged cabin door configuration) A CI Windshield washer A CI Air conditioning system (split) A CI Fuel flowmeter, displayed on GPS Garmin GNS 430W A CI Under fuselage anti-collision strobe light A CI Lightweight Aircraft Recording System - Appareo Alerts Vision A CI Emergency locator transmitter KANNAD 406 AP with GPS connection A CI 2 hinged passengers doors with 2 rear doors extensions (instead of the standard sliding doors) A CI Digital Audio Communication System NAT with 2 control panels A CI Passengers address NAT AA with 4 loudspeakers A CI Passenger interphone linked to DACS for VIP handset A CI VIP cabin and intercommunication management system A CI David Clark H10-13 H headset (qty 2) A CI Two additional ICS jacks in cockpit for Bose Aviation headsets (headsets excluded) A CI Transponder (Mode S) - Garmin GTX 330 ES - ADS-B_OUT- NRA A CI ADF - Collins ADF-4000 (displayed on MFD255) A CI DME Collins DME (displayed on MFD-255) A CI Marker beacon receiver - Honeywell KR A CI Weather radar RDR 2000 Honeywell (displayed on MFD 255 and 10.4" screen) A CI TCAS Goodrich / L3 Com SKYWATCH HP (displayed on 10.4" screen) A CI VHF/VOR/LOC/GS/GPS n 1 Garmin GNS 430W A CI VHF/VOR/LOC/GS/GPS n 2 Garmin GNS 430W A CI Moving map EUROAVIONICS EURONAV VII, linked to GPS (displayed on 10.4" screen) A CI Mission display 10,4" A CI Solid State Cockpit Voice & Flight Data Recorder - L3COM SSCVFDR with MFDAU A CI UMS - complement of SSCVFDR (usage functions) with MFDAU++ Ground station excluded N E

27 4.2.2 Mandatory Equipment Mandatory Equipment Document reference Interior Layout Commercial reference Description kg lb A CI 7-seat VIP installation (4+3) - without partition A CI 6-seat VIP installation (3+3) - without partition Further Available Equipment Document reference General Equipment Commercial reference Description kg lb A CI Customized external paint A CI High visibility markings of the main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Sand prevention filters, dynamic type - Fixed parts A RP Sand prevention filters, dynamic type - Removable parts A CI Re-inforced sand erosion protection strip on main rotor blades A CI 2nd fire extinguisher A CI Icing detector (Rosemount) A FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Fixed Parts A RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Removable Parts Specific Mission Equipment A FP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Fixed Parts A RP Cargo sling with dynamometer & external mirrors 10-A (1,600 kg - 3,527 lb) - Removable Parts A FP Emergency floatation gear with automatic percussion Fixed parts A RP Emergency floatation gear with automatic percussion Removable parts Interior Layout A CI Additional hand tufted carpet for VIP cabin (spare) A CI Gold plated finishing of the visible cabin metallized parts Avionics A CI Active noise cancelling headsets Bose A20 (qty 1) Quantity to be defined, following the number of passengers or crews A CI EGPWS Honeywell MK XXII (displayed on 10.4" screen) A CI Automatic hover & ground speed modes Avionic equipment choice : only one on two equipment can be selected in addition to the above installations A CI HF/SSB Collins HF A CI Satcom IRIDIUM Skyconnect (voice and A/C position) control in cockpit and cabin 365 N E 25

28 4.2.4 Performance Data 6-seat VIP installation (3+3) Mission Profile Take-off at MTOW (Cat. A Clear Area) Climb + cruise at 5000ft at VBr Reserve: 30 min at VBe, 1500ft Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, Standard VIP Configuration with 6-seat (3+3) 2,900 6,393 (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,235 2,723 Fuel tanks capacity Standard fuel tanks 897 1,977 Passengers vs. Range in VIP 6-seat configuration at ISA N E

29 7-seat VIP installation (4+3) Mission Profile Take-off at MTOW (Cat. A Clear Area) Climb + cruise at 5000ft at VBr Reserve: 30 min at VBe, 1500ft Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, Standard VIP Configuration with 7-seat (4+3) 2,862 6,309 (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,273 2,807 Fuel tanks capacity Standard fuel tanks 897 1,977 Passengers vs. Range in VIP 7-seat configuration at ISA 365 N E 27

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31 4.3 Executive Favorite The AS365 N3+ Executive configuration is fitted with a comfortable and unobstructed cabin easily accessible thanks to the two large rear sliding doors. On the front cabin, hinged doors of the same size provide wide storage compartments. The cabin directly extends to the cockpit which allows direct communication with the pilots and opens the view on the instrument panel and through the windshield. Unobstructed cabin 2-place bench seats The Executive configuration can accommodate up to 8 passengers in great comfort conditions. Two interior layouts proposing different combinations of divan and seat-bench are available. The cabin is customisable at customer s preferences: seat designs, materials and fabrics are selectable among a list of available choices. 365 N E 29

32 4.3.1 Executive Standard Configuration Document reference Commercial reference Description kg lb A CI Standard Utility and Transport Configuration A CI AS365 N3+ Baseline Aircraft as per 365 N E A CI Enhanced offshore anti-corrosion protection A CI Windshield washer A CI Fuel flowmeter, displayed on GPS Garmin GNS 430W A FP Goodrich Category 1 electrical Hoist (272 kg - 88 m) with electrostatic discharge protection - Fixed Parts A FP Rappelling installation (ropes excluded) - Fixed Parts A CI Under fuselage anti-collision strobe light A CI Lightweight Aircraft Recording System - Appareo Alerts Vision A CI Emergency Locator Transmitter KANNAD - Integra 406 AP-(ER) with GPS connection A CI Digital Audio Communication System NAT with 2 control panels A CI Third control panel for NAT Digital Audio Communication System A CI Passengers address NAT AA with 4 loudspeakers A CI Passenger interphone linked to DACS for 12 passengers A CI David Clark H10-13 H headset (qty 2) A CI Two additional ICS jacks in cockpit for Bose Aviation headsets (headsets excluded) A CI Transponder ( Mode S) - Garmin GTX 330 ES - ADS-B_OUT- NRA A CI ADF - Collins ADF-4000 (displayed on MFD255) A CI DME Collins DME (displayed on MFD-255) A CI Marker beacon receiver - Honeywell KR A CI Weather/search radar Telephonics RDR-1600C (displayed on MFD 255 and 10.4" screen) A CI TCAS Goodrich / L3 Com SKYWATCH HP (displayed on 10.4" screen) A CI VHF/VOR/LOC/GS/GPS n 1 Garmin GNS 430W A CI VHF/VOR/LOC/GS/GPS n 2 Garmin GNS 430W A CI Moving map EUROAVIONICS EURONAV VII, linked to GPS (displayed on 10.4" screen) A CI Mission display 10,4" A CI Solid State Cockpit Voice & Flight Data Recorder L3COM SSCVFDR with MFDAU A CI UMS - complement of SSCVFDR (usage functions) with MFDAU++ Ground station excluded N E

33 4.3.2 Mandatory Equipment Document reference Interior Layout Commercial reference Description kg lb A CI 8-seat layout with 4-point harnesses A CI 7-seat Executive installation (4+3) - for sliding doors Further Available Equipment Document reference General Equipment Commercial reference Description kg lb A CI Customized external paint A CI High visibility markings of the main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Sand prevention filters, dynamic type - Fixed parts A RP Sand prevention filters, dynamic type - Removable parts A A CI Re-inforced sand erosion protection strip on main rotor blades A CI 2nd fire extinguisher A CI Limousine window panes in the cabin (for sliding cabin door configuration) A CI Air conditioning system (split) A CI Icing detector (Rosemount) A FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Fixed Parts A RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Removable Parts Specific Mission Equipment A FP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Fixed Parts A RP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Removable Parts A FP Emergency floatation gear with automatic percussion Fixed parts A RP Emergency floatation gear with automatic percussion Removable parts Interior Layout A CI Executive 'Plus' cabin trimming A CI VIP treatment of the cockpit Avionics A CI HF/SSB Collins HF A CI Satcom IRIDIUM Skyconnect (voice and A/C position) control in cockpit only A CI David Clark H10-13 H headset (qty 1) Quantity to be defined, following the number of passengers or crews A CI Active noise cancelling headsets Bose A20 (qty 1) Quantity to be defined, following the number of passengers or crews A CI Weather radar RDR 2000 Honeywell (displayed on MFD 255 and 10.4" screen) A CI Weather/search radar Telephonics RDR-1600C removed from the Standard Utility and Transport Configuration A CI EGPWS Honeywell MK XXII (displayed on 10.4" screen) A CI Automatic hover & ground speed modes N E 31

34 4.3.4 Performance Data 7-seat Executive installation (4+3) Mission Profile Take-off at MTOW (Cat. A Clear Area) Climb + cruise at 5000ft at VBr Reserve: 30 min at VBe, 1500ft Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, Standard Executive Configuration with 7-seat (4+3) 2,721 5,999 (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,378 3,039 Fuel tanks capacity Standard fuel tanks 897 1,977 Passengers vs. Range in Executive 7-seat configuration at ISA N E

35 8-seat Executive installation (4+4) Mission Profile Take-off at MTOW (Cat. A Clear Area) Climb + cruise at 5000ft at VBr Reserve: 30 min at VBe, 1500ft Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, Standard Executive Configuration 8-seat (4+4) 2,709 5,972 (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,391 3,066 Fuel tanks capacity Standard fuel tanks 897 1,977 Passengers vs. Range in Executive 8-seat configuration at ISA 365 N E 33

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37 4.4 Public Services Favorite The AS365 N3+ is designed for operations in the most severe environmental conditions. Pilots and crew appreciate its exceptional endurance and maneuvrability while on-ground maintenance staff appreciate its low and easy maintenance. The AS365 N3+ indeed benefits the lowest maintenance and operational costs of its category. Thanks to the wide range of mission equipment proposed such as hoist, sling, search light, EOS, etc. the Public Services configuration can perform multi-role missions from surveillance and monitoring operations to aerial work and ground support missions. The ideal partner for anti-disaster mission Bambi bucket operations Hot & High Performance. Versatility : quick and easy mission reconfiguration without any special tools required for any type of operation (Police, Medical Services, Fire-fighting, Surveillance and Monitoring, Freight, etc.). With the Automatic Hover and Ground Speed modes, the Public Services Favorite can be configured for light SAR missions. 365 N E 35

38 4.4.1 Public Services Standard Configuration Document reference Commercial reference Description kg lb A CI Standard Utility and Transport Configuration A CI AS365 N3+ Baseline Aircraft as per 365 N E A CI Enhanced offshore anti-corrosion protection A CI Windshield washer A CI Fuel flowmeter, displayed on GPS Garmin GNS 430W A FP Goodrich Category 1 electrical Hoist (272 kg - 88 m) - Fixed Parts A FP Rappelling installation (ropes excluded) - Fixed Parts A CI Under fuselage anti-collision strobe light A CI Lightweight Aircraft Recording System - Appareo Alerts Vision A CI Emergency Locator Transmitter KANNAD - Integra 406 AP-(ER) with GPS connection A CI Digital Audio Communication System NAT with 2 control panels A CI Third control panel for NAT Digital Audio Communication System A CI Passengers address NAT AA with 4 loudspeakers A CI Passenger interphone linked to DACS for 12 passengers A CI David Clark H10-13 H headset (qty 2) A CI Two additional ICS jacks in cockpit for Bose Aviation headsets (headsets excluded) A CI Transponder ( Mode S) - Garmin GTX 330 ES - ADS-B_OUT- NRA A CI ADF - Collins ADF-4000 (displayed on MFD255) A CI DME Collins DME (displayed on MFD-255) A CI Marker beacon receiver - Honeywell KR A CI Weather/search radar Telephonics RDR-1600C (displayed on MFD 255 and 10.4" screen) A CI TCAS Goodrich / L3 Com SKYWATCH HP (displayed on 10.4" screen) A CI VHF/VOR/LOC/GS/GPS n 1 Garmin GNS 430W A CI VHF/VOR/LOC/GS/GPS n 2 Garmin GNS 430W A CI Moving map EUROAVIONICS EURONAV VII, linked to GPS (displayed on 10.4" screen) A CI Mission display 10,4" A CI Solid State Cockpit Voice & Flight Data Recorder L3COM SSCVFDR with MFDAU A CI UMS - complement of SSCVFDR (usage functions) with MFDAU++ Ground station excluded N E

39 4.4.2 Mandatory Equipment Document reference Interior Layout Commercial reference Description kg lb A CI 12-seat layout with 4-point harnesses A CI 8-seat layout with 4-point harnesses A CI 11-seat layout with 4-point harnesses A CI Aircraft delivered without cabin layout Further Available Equipment Document reference General Equipment Commercial reference Description kg lb A CI Customized external paint A CI First aid kit - EASA Ops compatible A CI Wire strike protection system (upper cutter) A CI High visibility markings of the main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Sand prevention filters, dynamic type - Fixed parts A RP Sand prevention filters, dynamic type - Removable parts A CI Re-inforced sand erosion protection strip on main rotor blades A CI 2nd fire extinguisher A CI Sliding window on the enlarged and bubble sliding door RH Side A CI Sliding window on the enlarged and bubble sliding door LH Side A CI Air conditioning system (split) A CI Icing detector (Rosemount) A FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Fixed Parts A RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Removable Parts Specific Mission Equipment A RP Goodrich Category 1 electrical Hoist (272 kg - 88 m) with electrostatic discharge protection - Removable Parts A RP Rappelling installation (ropes excluded) - Removable Parts A FP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Fixed Parts A RP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Removable Parts A FP Electrical hailer with siren for Passenger Address system Fixed Parts A RP Electrical hailer with siren for Passenger Address system Removable Parts A FP Spectrolab SX-16 search light - Fixed parts A RP Spectrolab SX-16 search light - Removable parts A CI EOS / Searchlight Spectrolink Slaving Unit A CI Infrared filter for SPECTROLAB SX-16 search light N E 37

40 Specific Mission Equipment (Continued) A FP Pod mounted EOS Ultraforce 350 EP - Fixed Parts A RP Pod mounted EOS Ultraforce 350 EP - Removable Parts Including : Color TV camera / IR camera / Autotracker. Requires French export license. Note that this product can be updated by the vendor and may have an impact on the configuration A CI Video camera on hoist beam A FP Emergency floatation gear with automatic percussion Fixed parts A RP Emergency floatation gear with automatic percussion Removable parts A CI Life raft Aerazur A CI Automatic deployable Emergency Locator Transmitter (ADELT) HR SMITH series 503 with GPS connection A CI Personal Locator Beacon HR Smith PLB 500 series (Qty:1) A CI Under Water Acoustic Beacon DUKANE DK 120 / A CI Special cockpit lighting with dedicated control boxes and external lighting A FP Fire-fighting "Bambi Bucket" (910 litres) - Fixed parts A RP Fire-fighting "Bambi Bucket" (910 litres) - Removable parts Interior Layout A CI Complement for 12-seat layout with 4-point harnesses Requires CI A CI Complement for 11-seat layout with 4-point harnesses Requires CI A CI Transaco hoistable Stretcher A CI Headrest (Qty 8) Avionics A CI David Clark H10-13 H headset (qty 1) Quantity to be defined, following the number of passengers or crews A CI Active noise cancelling headsets Bose A20 (qty 1) Quantity to be defined, following the number of passengers or crews A CI Weather radar RDR 2000 Honeywell (displayed on MFD 255 and 10.4" screen) A CI Weather/search radar Telephonics RDR-1600C removed from the Standard Utility and Transport Configuration A CI EGPWS Honeywell MK XXII (displayed on 10.4" screen) A CI Automatic hover & ground speed modes A CI Hoist operator joystick for automatic hover & ground speed modes A CI HUMS - complement of UMS (health functions) with MFDAU Avionic equipment choice : only one on five equipment can be selected in addition to the above installations A CI HF/SSB Collins HF A CI VHF/FM NAT NPX A CI V/UHF/AM/FM Chelton-Wulfsberg - RT A CI Satcom IRIDIUM Skyconnect (voice and A/C position) control in cockpit only A CI Airborne Video / Data Digital Recorder - AVALEX AVR N E

41 4.4.4 Performance Data Mission Profile Take-off at MTOW (Cat. A Clear Area) Climb + cruise at 5000ft at Best Range Speed Reserve: 30 min at Best Endurance Speed, 1500ft Fuel tanks capacity: Standard fuel tanks Weight kg lb Empty weight, Standard Public Services configuration with 8-seat 2,627 5,792 (including engine oil, unusable fuel and 2% margin) Pilots (2 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,508 3,326 Fuel tanks capacity Standard fuel tanks 897 1,977 Payload vs. Range in standard Public Services configuration at ISA 365 N E 39

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43 4.5 SAR Favorite The SAR configuration has been studied to provide its operators the best conditions to operate day & night in all weather conditions. The configuration is fitted with an FMS/ GPS installation coupled to a digital 4-axis autopilot integrating full SAR modes (includes automatic transitions, search patterns and hover mode), one sliding window on each each bubble sliding door to easier the search phase, a maritime transponder allows dynamic exchanges with ships and helicopters (AIS subscribers). In addition, the SAR configuration is capable of a wide range of equipment such as hoist, floatation gear, searchlight, rappelling, hailer, etc. to enlarge the mission scopes. Full SAR modes maximize the level of safety and minimize pilot s workload. Ship borne capabilities : moorings for bad weather conditions, blade folding for an easy parking in the confined areas, small foot print to allow landing on small platforms. Beacons fully comply with the latests regulations standards and all include their own GPS sensors. The hoist installation now includes a static discharger for an improved operational safety. The transponder is ADSB-out compatible. Extended squitter function available on request. 365 N E 41

44 4.5.1 SAR Standard Configuration Document reference Commercial reference Description kg lb A CI Standard SAR Configuration A CI AS365 N3+ Baseline Aircraft as per 365 N E A CI Enhanced offshore anti-corrosion protection A CI Sliding window on the enlarged and bubble sliding door - RH Side A CI Sliding window on the enlarged and bubble sliding door - LH Side A CI Windshield washer A FP Goodrich Category 1 electrical Hoist (272 kg - 88 m) with electrostatic discharge protection - Fixed Parts A FP Rappelling installation (ropes excluded) - Fixed Parts A CI Under fuselage anti-collision strobe light A CI Lightweight Aircraft Recording System - Appareo Alerts Vision A FP Emergency floatation gear with automatic percussion Fixed parts A RP Emergency floatation gear with automatic percussion Removable parts A CI Emergency locator transmitter KANNAD 406 AP with GPS connection A CI Automatic deployable Emergency Locator Transmitter (ADELT) HR SMITH series 503 with GPS connection A CI VHF/AM Rockwell-Collins VHF-4000 n (including 8.33 khz channel spacing) A CI VHF/AM Rockwell-Collins VHF-4000 n (including 8.33 khz channel spacing) A CI Digital Audio Communication System NAT with 2 control panels A CI Third control panel for NAT Digital Audio Communication System A CI Passengers address NAT AA with 4 loudspeakers A CI Passenger interphone linked to DACS for 12 passengers A CI David Clark H10-13 H headset (qty 2) A CI Two additional ICS jacks in cockpit for Bose Aviation headsets (headsets excluded) A CI Complement SAR Modes Navigation Package A CI Long interseat console A CI Thales AHV 16 second radio altimeter A CI SAR mode of CMA A CI Automatic transition & hover modes A CI Mode S Transponder COLLINS TDR 94 D with flight ident function A CI R4 AIS transponder displayed on mission display 10.4" A CI DME Collins DME (displayed on MFD-255) A CI VOR/ILS/MKR - Collins NAV-4500 n (displayed on MFD-255) A CI VOR/ILS/MKR/ADF - Collins NAV-4000 n (displayed on MFD-255) A CI Search radar TELEPHONICS RDR 1500 B (displayed on 10.4" screen) A CI GPS receiver - Canadian Marconi CMA A CI Flight Management System - Canadian Marconi CMA (including fuel management, search pattern & DTM ) A CI Moving map EUROAVIONICS EURONAV VII, linked to GPS (displayed on 10.4" screen) A CI Mission display 10,4" A CI Solid State Cockpit Voice & Flight Data Recorder - L3COM SSCVFDR with MFDAU A CI UMS - complement of SSCVFDR (usage functions) with MFDAU++ Ground station excluded N E

45 4.5.2 Mandatory Equipment Document reference Interior Layout Commercial reference Description kg lb A CI 8-seat layout with 4-point harnesses A CI Aircraft delivered without cabin layout A CI Headrest (Qty 8) Further Available Equipment Document reference General Equipment Commercial reference Description kg lb A CI Customized external paint A CI First aid kit - EASA Ops compatible A CI Wire strike protection system (upper cutter) A CI High visibility markings of the main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Sand prevention filters, dynamic type - Fixed parts A RP Sand prevention filters, dynamic type - Removable parts A CI Re-inforced sand erosion protection strip on main rotor blades A CI 2nd fire extinguisher A CI Air conditioning system (split) A CI Icing detector (Rosemount) A FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Fixed Parts A RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) Removable Parts Specific Mission Equipment A RP Goodrich Category 1 electrical Hoist (272 kg - 88 m) with electrostatic discharge protection - Removable Parts A RP Rappelling installation (ropes excluded) - Removable Parts A FP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Fixed Parts A RP Cargo sling with dynamometer & external mirrors (1,600 kg - 3,527 lb) - Removable Parts A FP Electrical hailer with siren for Passenger Address system Fixed Parts A RP Electrical hailer with siren for Passenger Address system Removable Parts A FP Spectrolab SX-16 search light - Fixed parts A RP Spectrolab SX-16 search light - Removable parts A CI EOS / Searchlight Spectrolink Slaving Unit A CI Infrared filter for SPECTROLAB SX-16 search light A FP Pod mounted EOS Ultraforce 350 EP - Fixed Parts A RP Pod mounted EOS Ultraforce 350 EP - Removable Parts Including : Color TV camera / IR camera / Autotracker. Requires French export license. Note that this product can be updated by the vendor and may have an impact on the configuration A CI Video camera on hoist beam A CI Life raft Aerazur N E 43

46 Specific Mission Equipment (Continued) A CI Personal Locator Beacon HR Smith PLB 500 series (Qty:1) A CI Under Water Acoustic Beacon DUKANE DK 120 / A CI Special cockpit lighting with dedicated control boxes and external lighting A FP Fire-fighting "Bambi Bucket" (910 litres) - Fixed parts A RP Fire-fighting "Bambi Bucket" (910 litres) - Removable parts Interior Layout A CI Transaco hoistable Stretcher Avionics A CI HF/SSB Collins HF A CI VHF/FM NAT NPX A CI Satcom IRIDIUM Skyconnect (voice and A/C position) control in cockpit only A CI David Clark H10-13 H headset (qty 1) Quantity to be defined, following the number of passengers or crews A CI Active noise cancelling headsets Bose A20 (qty 1) Quantity to be defined, following the number of passengers or crews A CI Direction finder / homing Cobham DF (displayed on MFD-255) A CI TCAS Goodrich / L3 Com SKYWATCH HP (displayed on 10.4" screen) A CI EGPWS Honeywell MK XXII (displayed on 10.4" screen) A CI Airborne Video / Data Digital Recorder - AVALEX AVR N E

47 4.5.4 Performance Data Mission Profile Take-off at MTOW (Cat. A Clear Area) Outbound flight : climb + cruise at 5000ft at VBr Loiter at 5000ft, Vy Rescue operation : hover 5min for 1 rescue at 85 kg (HOGE with AEO) Inbound flight : climb + cruise at 5000ft at VBr Reserve : 30min at VBe, 1500ft Fuel tanks capacity: Standard fuel tanks Weight Empty weight, Standard SAR configuration with 1 bench of 2 seats. Removable Part of Hoist, SX16, EOS, and SAR equipment (including engine oil, unusable fuel and 2% margin) kg lb 2,853 6,290 Pilots (2 x 85 kg) Crews (1 x 85 kg) Maximum Take-Off Weight 4,300 9,480 Useful load 1,192 2,629 Fuel tanks capacity Standard fuel tanks 897 1,977 Rescuee vs. Radius of Action (RoA) in standard SAR configuration at ISA 365 N E 45

48 5 Main Performance The following performance values and figures refer to an AS365 N3+, equipped with new engines. Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind conditions. Performance on 2 engines (AEO) Gross Weight kg lb 3,750 8,267 4,000 8,818 4,300 9,480 Max. speed, VNE km/h kts Fast cruise speed km/h kts Fast cruise speed (5000ft) km/h kts Recommended cruise speed km/h kts Recommended cruise speed (5000ft) km/h kts Fuel consumption at recommended cruise speed (5000ft) kg/h lb/h Rate-of-climb at TAS=75 kts m/s ft/min 9 1, , ,328 Rate-of-climb at TAS=75 kts (ISA+20 C) m/s ft/min 9 1, , ,299 Hover ceiling I.G.E. at Take-Off Power (6 ft) ISA m 3, ft 12, ISA + 20 C m 3, ft 10, Hover ceiling O.G.E. at Take-Off Power ISA m ft ISA + 20 C m ft Service ceiling (Vz= 0.5m/s-100ft/mn,TAS=75kts) ISA m ft ISA m ft Maximum range (without fuel reserve, at recommended cruise speed) with standard tanks km NM with optional auxiliary tank km NM Maximum endurance [without reserve at 140 km/h (75 kts)] with standard tanks h with optional auxiliary tank h N E

49 Performance with external load (drag: 1m²) Gross Weight kg lb 4,250 9,370 Rate-of-climb (conditions :speed, power) m/s 6.3 ft/min 1,232 Performance on 1 engine (OEI) Gross Weight kg lb 3,750 8,267 4,000 8,818 4,300 9,480 Rate-of-climb at TAS=75kts, continuous OEI power m/s ft/min Service ceiling (0.5 m/sec ft/min.) TAS=75kts m 2,923 2,295 1,594 continuous OEI power ft 9,590 7,530 5,230 Operating limitations The helicopter is cleared to be operated within the following altitude and temperature limitations (according to the Flight Manual). For complementary information, refer to the Flight Manual: Maximum altitude (ISA) Flight Take-off and landing 6,096 m 20,000 ft (Density Altitude) 4,575 m 15,000 ft (Pressure Altitude) Temperature Maximum ISA + 35 C limited to + 50 C Minimum temperature - 40 C Units NM nautical miles h:min hours:minutes kts knots kg kilograms ft/min feet/minute lb pounds m/s meters per seconds km kilometres C degrees Celsius Km/h Kilometers per hour 365 N E 47

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51 Performance charts The performance charts presented hereafter apply to a clean helicopter as per the standard definition. Page Take-off Weight in hover IGE (6 ft) on 2 engines at Maximum take-off power Take-off Weight in hover OGE on 2 engines at Maximum take-off power Maximum Permissible Gross Weight on Take-off from clear heliport Category A Maximum Permissible Gross Weight on Take-off from clear helipad Category A Fast Cruise Speed on 2 engines at maximum continuous power, ISA Fast Cruise Speed on 2 engines at maximum continuous power, ISA +20 C Rate of climb in oblique flight on 2 engines at maximum continuous power, ISA; T.A.S. = 75 kts Rate of climb in oblique flight on 2 engines at maximum continuous power, ISA+ 20 C; T.A.S. = 75 kts Rate of climb in oblique flight on 1 engine OEI unlimited, ISA; T.A.S. = 75 kts Rate of climb in oblique flight on 1 engine OEI unlimited, ISA+ 20 C; T.A.S. = 75 kts Hourly fuel consumption in level flight Pressure-altitude = 0 ft, ISA (temperature = 15 C) Hourly fuel consumption in level flight Pressure-altitude = 5000 ft, ISA (temperature = 5.1 C) Hourly fuel consumption in level flight Pressure-altitude = ft, ISA (temperature = -4.8 C) Hourly fuel consumption in level flight Pressure-altitude = 0 ft, ISA+20 C (temperature = 35 C) 63 Hourly fuel consumption in level flight Pressure-altitude = 5000 ft, ISA+20 C (temperature = 25 C) Hourly fuel consumption in level flight Pressure-altitude = ft, ISA+20 C (temperature = 15.2 C) N E 49

52 Take-off Weight in hover I.G.E. (Height 6 ft) On 2 engines at maximum take-off power Pressure altitude (ft) ISO-Weight (kg) (m) 6000 ISA ISA+ 20 ISA+ 35 Density altitude max 15000ft Temperature ( C) N E

53 Take-off Weight in hover ceiling O.G.E. On 2 engines at maximum take-off power Pressure altitude (ft) ISO-Weight (kg) (m) ISA+ 20 ISA+ 35 Density altitude max 15000ft 4000 ISA Temperature ( C) 365 N E 51

54 Maximum permissible gross weight on take-off from clear heliport Category A Vtoss: 65 / 75 kts Vy: 75 kts Pressure altitude (ft) ISO-Weight (kg) (m) ISA ISA+ 20 ISA Temperature ( C) N E

55 Maximum permissible gross weight on take-off from clear helipad Category A 365 N E 53

56 Fast cruise Speed ISA Pressure altitude (ft) ISO-Weight (kg) True Air Speed (kt) N E

57 Fast cruise Speed ISA +20 C Pressure altitude (ft) ISO-Weight (kg) True Air Speed (kt) 365 N E 55

58 Rate of climb in oblique flight On 2 engines at maximum continuous power ISA, T.A.S. = 75kts N E

59 Rate of climb in oblique flight On 2 engines at maximum continuous power ISA+20 C, T.A.S. = 75kts 365 N E 57

60 Rate of climb in oblique flight On 1 engine OEI unlimited ISA, T.A.S. = 75kts N E

61 Rate of climb in oblique flight On 1 engine OEI unlimited ISA+20 C, T.A.S. = 75kts 365 N E 59

62 Hourly fuel consumption in level flight Pressure altitude = 0ft, ISA (Temperature = 15 C) N E

63 Hourly fuel consumption in level flight Pressure altitude = 5000ft, ISA (Temperature = 5.1 C) 365 N E 61

64 Hourly fuel consumption in level flight Pressure altitude = 10000ft, ISA (Temperature = -4.8 C) N E

65 Hourly fuel consumption in level flight Pressure altitude = 0ft, ISA+20 C (Temperature = 35 C) 365 N E 63

66 Hourly fuel consumption in level flight Pressure altitude = 5000ft, ISA+20 C (Temperature = 25 C) N E

67 Hourly fuel consumption in level flight Pressure altitude = 10000ft, ISA+20 C (Temperature = 15.2 C) 365 N E 65