- Page 4 and 5: Table of Content 5 Further Product
- Page 6 and 7: Blank Technical Data Page 4 of 168
- Page 8 and 9: Compared to other helicopters in it
- Page 10 and 11: 1.1 News, Highlights and Main Impro
- Page 12 and 13: Blank Technical Data Page 10 of 168
- Page 14 and 15: 2.2 Interior Dimensions 2.3 Possibl
- Page 16 and 17: 2.6 Engines 2 Pratt & Whitney turbi
- Page 18 and 19: TRANSMISSION SYSTEM • Flat-shaped
- Page 20 and 21: Technical Data Performance calculat
- Page 22 and 23: 4.1.1 EMS - Glass Cockpit (Air Ambu
- Page 24 and 25: Interior layout Technical Data Qty
- Page 26 and 27: Mission equipment Technical Data Qt
- Page 28 and 29: 1 06-21017-D L8512-001-20 External
- Page 30 and 31: 4.1.1.4 Performance Data Maximum ra
- Page 32 and 33: 4.1.2 EMS - Glass Cockpit (Aerolite
- Page 34 and 35: 1 Stretcher "Combi" with stretcher
- Page 36 and 37: Mission equipment Technical Data Qt
- Page 38 and 39: 1 06-21017-D L8512-001-20 External
- Page 40 and 41: 4.1.2.4 Performance Data Maximum ra
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- Page 44 and 45: 4.2.1 Disaster Management (Air Ambu
- Page 46 and 47: Mission equipment Interior layout T
- Page 48 and 49: Interior layout Avionics Technical
- Page 50 and 51: Mission equipment Interior layout A
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4.2.1.4 Performance Data 4.2.1.4.1E
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Mission profile • Take-off at SL
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Payload [kg] 800 600 400 200 0 5 In
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Search and rescue Intervention 4.2.
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Avionics 4.2.2.2.2Recommended Items
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4.2.2.3 Further Available Equipment
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Technical Data Qty DocRef ComRef Ti
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Planned TOW [kg] 2900 2800 2700 260
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4.2.2.4.3Intervention Mission Radiu
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4.3.1 Mission Parameter • Flight
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Avionics 4.3.2.2 Recommended Items
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Mission equipment Interior layout A
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4.3.4 Material and Color Definition
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Payload [kg] 800 600 400 200 0 Figu
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4.4.1 Mission Parameter • Flight
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Avionics 4.4.2.2 Recommended Items
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Mission equipment Interior layout A
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4.4.4 Material and Color Definition
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Payload [kg] 800 600 400 200 0 Figu
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4.5.1 Mission Parameter • Flight
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1 Rear cabinet HERMES 1 Separation
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a.Recommended 1 per customer if CVF
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4.6.1 Mission Parameter • Flight
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Avionics 4.6.2.2 Recommended Items
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Mission equipment Technical Data Qt
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Technical Data Headsets and adapter
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Figure 4.22: Payload versus range d
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4.7.1 Mission Parameter • Flight
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Avionics 4.7.2.2 Recommended Items
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4.7.3 Further Available Equipment G
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Avionics Technical Data Qty DocRef
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Mission profile • Take-off at SL
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Dual Pilot / Single Dual Pilot Tran
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Dual Pilot / Single Dual Pilot Dual
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5.2 Antenna Layouts 5.2.1 Typical V
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Technical Data Title Weight [kg] We
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Technical Data Title Weight [kg] We
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5.4 Police Technical Data Whatever
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• Ergonomic design adjustable to
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Figure 5.11: Typical cockpit layout
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Gross weight kg lb • Maximum endu
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Performance on 1 engine (OEI) Turbo
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Hover in Ground Effect (HIGE, TOP,
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Hover Out of Ground Effect (HOGE, T
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Hover Out of Ground Effect (HOGE, 2
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Hover Out of Ground Effect (HOGE, 2
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Maximum cruising speed with two ARR
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Maximum rate of climb, TOP with two
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Payload / Range with two ARRIUS 2B2
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Technical Data Scheduled airframe i
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7.4 Eurocopter Maintenance Support
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• Required product support improv
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Technical Data ficient and timely f
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Technical Data The range covered by
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7.8 Technical Support Technical Dat
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Abbreviation Meaning ELT Emergency
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Abbreviation Meaning VDC Volt Direc