Spec EC - 130 B4

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PT. NATIONAL UTILITY HELICOPTERS

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AIRCRAFT SPECIFICATIONEC-130B4

1. Model : EC-130B4

2. Registration : PK - URR

3. Serial Number : 4060

4. Flight Rules : VFR

5. Year of Manufacture : 2006

6. Aircraft Conf iguration : Onshore / Offshore Operations

7. Passenger Capacity : 1 Pilot + 6 Pax

8. Power Plant : 1 Turbomeca ARRIEL 2B1 Turbine Engine

The EC-130B4 is the new 6-7 seat single engine helicopter in the Eurocopter product rangeoffering particular qualities of silence, comfort and spaciousness.

It features a low external noise emission, 8.5dB under the ICAO requirement. This is achievedby the low noise "Fenestron" and the automatic control of the rotor RPM,a function whichautomatically optimizes the overflight noise signature without operational limitations.

The very roomy and modular cabin (width 2.03m compared to 1.87m for the Ecureuil), has a lowinternal noise level, and all seats comply with FAA regulations in terms of energy absorbtion.

The EC-130B4 is powered by a Turbomeca ARRIEL 2B1 turbine engine, complete with dualchannel digital engine control system (FADEC), and a back-up control box that automaticallycontrols the engine in case of total failure of both digital channels of the FADEC.

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TECHNICAL DATA

LAY-OUT

Passenger transport1 pilot + 6 passengers in standard version

1 pilot + 7 passengers in "medium density" version

Casualty-evacuation1 pilot + 1 or 2 stretcher patients + 2 medical attendants or

2 pilots + 1 stretcher patient + 2 medical attendants

Cargo carrying 1 pilot + 3.7 m3(130.7 cu.ft) load in cabin

Equipment Complete 7 seats interior + trims + carpets icluded in standard.Ready to operate radio package included in standard:-2 VHF-2 VOR / LOC / GLIDE-1 GPS-1 XPD mode C-1 ICS capable of 8 outlets-1 ADI-1 HSI

WEIGHTS

Note : Empty weight accuracy : within 2% kg lb

Empty weight, standard aircraft(including engine oil and unusable fuel)

1.370 3,020

Useful load 1.030 2.271

Maximum take-off weight 2.400 5.291

Maximum cargo sling load 1.160 2.557Maximum operational weight in external load configuration 2.800 6.172

ENGINE RATINGS

Thermic Power in ISA, at sea level:

kW ch shp

Take-off power 632 860 847

Maximum cont inuous power 543 739 728

USABLE FUEL CAPACITIES

litres US gal. kg lb

Standard total tanks 540 143 426 939

EXTERNAL NOISE

Average ICAO annex 16, chapter 8 86.8EPNdB

(-7.0 dB / ICAO limit)

Overflight 84.3EPNdB (-8.5 dB / ICAO limit)(-0.5 dB / GCNP (1) noise rule 6 PAX)(-1.2 dB / GCNP noise rule 7 PAX)

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DIMENSIONS

MAIN DIMENSIONS

CABIN DIMENSIONS

CABIN

SurfaceA

3.00 m232.3 ft2

Volume3.7 m3

130.7 ft3

RH HOLD

Surface0.43 m24.63 ft2

Volume

0.245 m3

8.65 ft3

LH HOLD


Volume0.285 m310.06 ft3

REAR HOLD


Volume0.565 m319.95 ft3

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PERFORMANCE

Unless otherwise specified, the following performance figures and charts are values obtainedwith new production engine and are given for a clean standard aircraft, in zero wind at sea level,standard atmosphere conditions.

kg 1,800 2,000 2,200 2,300 2,400TAKE-OFF WEIGHTlb 3,968 4,409 4,850 4,960 5,291

km/hr 287 287 287 287 287 VNE

kts 155 155 155 155 155km/hr 259 255 248 242 235

Fast cru ise speedkts 140 138 134 131 127

kg/hr 151 151 151 151 151 Fuel consumption at recommended cruise speed

lb/hr 333 333 333 333 333m/sec 11.6 10.9 10.1 9.65 9.1

Rate-of-climbft/min 2,290 2,150 1,990 1,900 1,800

Hover ceiling I.G.E. at take-off powerm 5875 4950 4080 3670 3265

ISAft 19,275 16,235 13,395 12,040 10,720m 5180 4220 3330 2895 2450

ISA + 20 Cft 17,000 13,850 10,930 9,495 8,055

Hover ceiling O.G.E. at take-off powerm 5320 4380 3490 3070 2660

ISAft 17,450 14,370 11,440 10,075 8,740m 4610 3630 2700 2240 1780

ISA + 20 Cft 15,120 11,910 8,855 7,340 5,850m > 7,010 6,705 5,791 5,395 5,029

Service Ceiling (0.5 m/sec., 100 ft/min.)ft > 23,000 22,000 19,000 17,700 16,500

HOVER CEILING

Hover Ceiling IGE Hover Ceiling OGE

FUEL CONSUMPTION RATE OF CLIMB

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EQUIPMENT

VEMD ( Vehicle & Engine Multi function Display Case Description )

VEMD : In Normal Ground and Start Operations

UPPER SCREEN T4 (Turbine gas temperature) with startingtemperature

Delta NG (Engine power margin versus limitations inpresent altitude/temperature conditions) TQ (Torque) Fuel quantity Numeric value of Outside Air Temperature (OAT) Free turbine speed Flag Bleed Valve openLOWER SCREEN Engine oil temperature Engine oil pressure Bus voltage and starter current

Equipped with V.E.M.D whichprovide HOGE, HIGE performancecalculation and automatic enginehealth control.

Modern Instrument Panel

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MISSIONS

ONSHORE / OFFSHORE OPERATION

MEDICAL EVACUATION OPERATION

The wide unobstructed cabin of the EC-130B4 and its large doorsallow easy loading of patients and rapid access for medicalpersonnel. Doctors and paramedics have plenty of space to takecare of the patient during the flight. The extremely low internalnoise level and the flat cabin floor offer a suitable environment toinstall fragile and bulky medical equipment.The fuel tank being independent form the cabin, that allows morespace to accommodate 1 or 2 stretchers and 2 medical attendants

on adjustable energy absorbing seats.

EXTERNAL LOAD OPERATION

Spec EC - 130 B4

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