AS365N2 Data

azz DAUPHIN AS 365 N2Technical Data

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This document is the property of EUROCOPTER; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. EUROCOPTER

MAIN DIMENSIONS (at the M.G.W. of 4,250 kg/9,369 lb and an average C.G. location)

DIMENSIONS WITH BLADES FOLDED


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DIMENSIONS OF COMPARTMENTS AND ACCESSES

CABIN

Area 4.20 m2

45.20 sq.ft

Volume 5.00 m3

176.57 cu.ft

LUGGAGE HOLD

Area 2.25 m2

24.21 sq.ft

Volume 1.10 m3

38.84 cu.ft


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GENERAL CHARACTERISTICS

LAY-OUT

n Passenger transport : 1 or 2 pilots + 8 passengers with comfort seats1 or 2 pilots + 11 passengers with comfort seats

n Casualty transport : 1 or 2 pilots + 4 stretcher-patients + 1 seat for medical attendant(or 2 stretcher-patients and 4 seats)

WEIGHTS

kg lb

n Empty weight, standard aircraft :(including engine oil and non usable fuel)

2,271 5,007

n Useful load : 1,979 4,362

______ ______

n Maximum all-up weight : 4,250 9,369

n Maximum load on cargo sling : 1,600 3,527

n Maximum all-up weight in external load configuration : 4,250 9,369

Note : Empty weight is correct to 2 %.

POWER PLANT : 2 TURBOMECA ARRIEL 1C2 free turbine engines

Available engine power (in standard atmosphere, at sea level with new engines)

kW ch shp

n Maximum emergency power 569 774 763

n Intermediate emergency power 550 749 737

n Take-off power 550 749 737

n Maximum continuous power 471 640 632

USABLE FUEL CAPACITIES

litres US gal. kg lb

n Standard fuel tanks (2 groups) 1,135 300 897 1,977

n Additional fuel tanks (option)

l Auxiliary fuel tank 180 47 142 313

l Ferrying fuel tank 460 121 375 826


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AS 365 N2 DAUPHIN - DEFINITION OF THE STANDARD AIRCRAFT


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OPTIONAL EQUIPMENT

Weight supplementThe equipment weight included in this chapter are probableaverage values, subject to change without notice.

Completeinstallation

Includingfixed parts

kg lb kg lb

GENERAL ITEMS OF EQUIPMENT

05-010 CAA Certification kit 24.4 53.8

05-015 43 Amp/hr cadmium battery 8.6 18.9 - -

05-016 FAA Certification Kit - - - -

05-020 Retractable second landing light 4.1 9.0 - -

05-030 Instrument lighting for storm condition flight 0.3 0.7 - -

05-040 Front panes in glass instead of plexiglass 10.9 24.0 - -

05-045 Windshield washer 2.3 5.0 - -

05-050 Icing detector (Rosemount) 1.1 2.4 - -

05-060 De-icing of panes in front of the crew 1.3 2.9 - -

05-070 Fuel anti-icing system 4.0 8.8

05-096 Air conditioning system - (R 134 A freon type) 56.0 123.4 - -

05-100 10-kVA A.C. alternator 27.8 61.3 - -

05-112 Tinted plexiglass (cabin only) 0.0 0.0 - -

05-120 Hourmeter 0.1 0.2 - -

05-131 Pilot and and copilot seats adjustable in height 14.4 31.7 - -

05-133 Pilot and Copilot energy absorbing seats 30.4 66.9 - -

05-140 Nose wheel caster- lock 1.2 2.6 - -

05-170 Sliding window(s) on the enlarged bubble slid. door(s) *1.0 *2.2 - -

05-180 Customized outside paint - - - -

05-240 High visibility main rotor blades 0.3 0.7 - -

(*) Weight supplement per door


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INSTRUMENTS AND FLYING AIDS

06-010 Remaining fuel flowmeter 3.2 7.0 - -

SPECIFIC MISSION EQUIPMENT

07-015 NG limiter for O.E.I training 0.1 0.2 - -

07-020 Emergency floatation gear 57.8 127.4 13.5 29.8

07-030 AERAZUR life raft installation (fitted on cabin ceiling). 61.9 136.5 -1.7 -3.7

07-051 Sand prevention filters, dynamic type 13.8 30.4 2.8 6.2

07-070 Skis 71.3 157.2 6.1 13.4

07-080 Ferrying tank (475 litres - 121 US gal.) 5.3 11.7 - -

07-090 Auxiliary fuel tank in the hold (180 litres - 47 US gal.) 27.6 60.8 3.9 8.6

07-100 Fuel jettison system 6.6 14.6 - -

07-140 Cargo sling, dynamometer, mirror (1,600 kg - 3,527 lb) 26.9 59.3 7.9 17.4

07-155 Fire-fighting "BAMBI BUCKET" (910 litre) (1) 51.0 112.3 1.0 2.2

07-161 Enlarged and bubbled rear sliding door(s) (2) 6.0 (2) 13.2 - -

07-170 AIR EQUIPEMENT electrical hoist (272 kg - 600 lb)with 90 m - 295 ft cable

71.9 158.5 3.8 8.6

07-200 Casualty-carrying installation (excluding stretchers) 12.3 27.1 1.8 4.0

07-210 Stretchers (4) (3) 8.3 18.2 - -

(1) Equipment to be proposed with cargo sling(2) Weight supplement per door(3) Not certified equipment


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kg lb kg lb

SPECIFIC MISSION EQUIPMENT (continued)

07-235 SPECTROLAB SX-16 searchlight 30.1 66.4 2.0 4.4

07-255 Under fuselage anti-collision strobe light TBD TBD - -

07-261 Hailer with siren system 30.2 66.5 10.0 22.0

07-310 Rappelling installation (Ropes are not included) 5.9 13.0 3.3 7.3

07-350 Anti-corrosion protection for S.A.R. mission 5.0 11.0 - -

INTERIOR CABIN ARRANGEMENTS

09-010 11 standard seat lay-out complement 14.3 31.5 - -

09-030 Comfort upholstery with improved sound-proofing andcarpeting

57.0 125.6 - -

09-035 8-seat EXECUTIVE installation with improved sound-proofing and carpeting

63.0 139.0 - -

09-040 5-seat VIP installation with enhanced sound-proofingand carpeting

237.0 522.5 - -

09-110 Headrests 4.0 8.8 - -

09-160 Storage unit in pilot and copilot doors 1.0 2.2 - -

GROUND HANDLING & PICKETING

10-011 Blade folding kit *30.0 *67.4 - -

(*)Tooling weight


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CUSTOMIZED & VENDOR SUPPLIED EQUIPMENT*

Weight supplement* The vendor is in charge for the conformity, performances andcertification of this installation regarding the final customer.



kg lb kg lb

VENDOR SPECIFIC MISSION EQUIPMENT

AERAZUR Separate life raft (6 person) 17.3 38.1 - -

TRANSACO Hoistable stretcher for land operations 14.0 30.8 - -

TRANSACO Hoistable stretcher for land & sea operations 28.0 61.7 - -

SIMPLEX Fire Fighting Installation System (STC certification) 136.0 300.0 5.0 11.0

VENDOR E. M. S. INSTALLATIONS

A. A. T. "Basic" EMS kit (1)

(1 stretcher)37.4 82.4 - -

A. A. T. "Rescue" EMS kit (1)

(1 stretcher with medical equipment carrier)56.4 124.0 - -

A. A. T. "Disaster" EMS kit (1)

(2 stretchers with medical equipment carrier)96.5 356.0 - -

A. A. T. AAT medical equipment kit (2) TBD TBD - -

(1) Helicopter shall be equipped with last raw of the 11 seat layout.

(2) Helicopter shall be equipped with "Rescue" or "Disaster" EMS kit.

Note : All optional equipement weight figures are probable average values.


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RADIO COMMUNICATION AND RADIO NAVIGATION EQUIPMENT

The radio/com/nav. equipment weight figures included in this chapter are average values. As theinstallation of those equipment may vary from one a/c to an other, the weight of a completeconfiguration with multiple items may not be the simple sum of all individual weights.

1. MINIMUM ITEMS OF EQUIPMENT - I F R CERTIFICATION (single pilot and / or two pilots)

Designation Solution 1 Solution 2

VHF/AM n1 HONEYWELL KTR 908 COLLINS VHF 22A

VHF/AM n2 HONEYWELL KTR 908 COLLINS VHF 22A

VOR/ILS n1 HONEYWELL KNR 634 A COLLINS VIR 32

VOR/ILS n2 HONEYWELL KNR 634 A COLLINS VIR 32

D.M.E. HONEYWELL KDM 706 A COLLINS DME 42

A.D.F. HONEYWELL KDF 806 COLLINS ADF 60

Transponder HONEYWELL KXP 756 COLLINS TDR 90

Altitude encoder SHADIN 8800 T SHADIN 8800 T

Radar altimeter (with 2indicators)

THALES AHV 16 THALES AHV 16

GPS (1) TRIMBLE TNL 2101 I/OApproach +

TRIMBLE TNL 2101 I/OApproach +

I.C.S. with 2 control boxes TEAM TB 31 TEAM TB 31

I.C.S. third control box TEAM TB 31 TEAM TB 31

Passenfer interphone(for 8 passengers)

TEAM BA 1920 TEAM BA 1920

Emergency Locator Transmitter JOLLIET JE 2 NG JOLLIET JE 2 NG

Flight Director Coupler SFIM CDV 85 D3 SFIM CDV 85 D3

Weather radar TELEPHONICS RDR 1400 C

Weight supplement 66.9 kg /147.71 lb 88.1 kg / 194.5 lb

(1) The customer must take out a subscription to the data base in order to use the GPS after having taken deliveryof the helicopter.


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2. EQUIPMENT THAT CAN BE ADDED DEPENDING ON THE OPERATIONAL NEEDS ORTHE REQUIREMENTS OF THE AUTHORITIES IN CERTAIN COUNTRIES

Designation Solution 1 kg lb Solution 2 kg lb

VHF/FM Maritime NAT NPX 138 7.6 16.8 NAT NPX 138 7.6 16.8SAR Homer CHELTON SYSTEM 7 4.5 9.9 CHELTON SYSTEM 7 4.5 9.9HF/SSB COLLINS HF 9100 21.5 47.4 COLLINS HF 9100 21.5 47.4Passenger address NAT AA 20-431 4.5 9.9 NAT AA 20-431 4.5 9.9Automatic DeployableEmergency Locator Transmitter(ADELT)

CALEDONIANCPT 606

6.9 15.2 CALEDONIANCPT 606

6.9 15.2

Flight Director Coupler (4-axis)(instead of 3-axis FDC)

SFIM CDV 155 (with2nd radar altimeter)

41.4 91.3

3. HEADSETS AND HELMETS

Designation kg lb

SILEC 4449-1 0.5 1.1HEADSETS

ELNO 247 SP 442 0.6 1.3

HELMETS GUENEAU-SILEC 459 1.3 2.8


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MAIN PERFORMANCE

The following performance figures and charts are probable average values obtained with newengines. Unless otherwise specified, they are for the aircraft in "clean" configuration in zero wind, sealevel, standard atmosphere conditions.

1. PERFORMANCE ON 2 ENGINESAll-up weight kg 3,750 4,000 4,250

lb 8,267 8,818 9,369

n Max. speed, VNE km/hr 306 296 287kts 165 160 155

n Fast cruise speed km/hr 286 281 275kts 154 152 148

n Recommended cruise speed km/hr 261 258 254kts 141 139 137

n Fuel consumption at recommended cruise speed kg/hrlb/h

270595

273602

275606

n Rate-of-climb m/sec. 9.0 7.8 6.8ft/min. 1,772 1,535 1,339

n Maximum range (without fuel reserve,at recommended cruise speed)l with standard tanks km 895 880 860

n.m 483 475 464

l with optional auxiliary tank km 1,040 1,027 1,004n.m 561 554 542

n Maximum endurance [without reserveat 140 km/hr (87 mph - 75 kts)]l with standard tanks hr 4.5 4.4 4.3l with optional auxiliary tank hr 5.2 5.1 5.0

n Hover ceiling I.G.E. at Take-Off Power (6 ft)l ISA m 3,150 2,440 1,900

ft 10,332 8,000 6,233

l ISA + 20C m 2,450 1,750 1,100ft 8,036 5,740 3,608

n Hover ceiling O.G.E. at Take-Off Powerl ISA m 2,400 1,800 1,200

ft 7,872 5,904 3,936

l ISA + 20 C m 1,600 850 150ft 5,248 2,788 492

n Service ceiling (Vz = 0,5 m /sec. - 100 ft/min.)l ISA m >4,575 4,300 3,700

ft >15,000 14,104 12,136

l ISA + 20C m 4,100 3,400 2,750ft 13,451 11,155 9,022


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2. PERFORMANCE ON 1 ENGINE

All-up weight kg 3,750 4,000 4,250lb 8,267 8,818 9,369

n Rate-of-climb at intermediate emergency power m / sec.ft / min.

2.8551

2.0394

1.3256

n Service ceiling (0,5 m /sec. - 100 ft / min.) atintermediate emergency power

mft

2,4508,036

1,8005,904

1,2003,936

3. OPERATING LIMITATIONS

The aircraft is cleared to operate within the following altitude and temperature limitations :(Refer to Flight Manual for complementary information)

n Maximum pressure altitude (Standard Atmosphere Conditions)

l Take-off and landing 4,575 m - 15,000 ft

l Flight 6,100 m- 20,000 ft

n Maximum temperature ISA + 35 C limited at + 50 C

n Minimum temperature - 40 C


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TAKE-OFF WEIGHT IN HOVER I.G.E. (6 ft)

on 2 engines at Maximum Take-Off Power


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TAKE-OFF WEIGHT IN HOVER O.G.E.

on 2 engines at Maximum Take-Off Power


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FAST CRUISE SPEED

On 2 engines at maximum continuous power

(ISA)


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operational empty weight with one pilot : 2,445 Kg/5,390 lb (without auxiliary fuel tank)


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AS365N2 Data

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