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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
Surface0.52 m25.60 ft2
Volume0.285 m310.06 ft3
REAR HOLD
Surface0.55 m25.92 ft2
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
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