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Mil Mi-8MSB |
[VERKOCHT]
US$ 12.300.000 |
Overview
| Base data | | Type: | Helikopter (Turbine) | | Producent: | Mil | | Model: | Mi-8MSB | | Bouwjaar: | 2018 | | Attributes: | IFR certified
IFR equipped
Always hangared
Commercially registered
EU-OPS 1 registered | | Location: | Rusland, Moscow, ZIA | | Total Time (TTAF): | 1 h | | Prijs: | US$ 12.300.000
(~ € 11.813.292)[VERKOCHT] | | Full details |
| Aanbieder |
Aircraft Tools Consulting Ltd.
Presnensky Val st., 27
123557 Moscow
Rusland
Tel: +7 (495) 769 4242
Mobile: +7 (916) 650 4707 |
| Contact seller |
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Full Details
| Base data | | Type: | Helikopter (Turbine) | | Producent: | Mil | | Model: | Mi-8MSB | | Bouwjaar: | 2018 | | Attributes: | IFR certified
IFR equipped
Always hangared
Commercially registered
EU-OPS 1 registered | | Location: | Rusland, Moscow, ZIA | | Total Time (TTAF): | 1 h | | Prijs: | US$ 12.300.000
(~ € 11.813.292)[VERKOCHT] | | No. of passengers: | 2-24 |
| Engine(s) | | Number of engines: | 2 | | Make/Model: | TV3-117VMA-SBM1V, series 4E | TV3-117VMA-SBM1V, series 4E | | Power: | 2,200 PS | 2,200 PS | | Total Time: | 1 h | 1 h |
| Description/Details of engines | The turboshaft engine with one-shaft gas-generator and free turbine maintains power flat rated to high values of ambient air temperature, deployment and flight altitudes comparing with existing TV2-117 helicopter engines.
2.5-min OEI power rating,
Continuous OEI 1 power rating – 60 minute (Cont 1)
(Í=0, Ìfl=0, ISA +20°C):
Power, hp (kW).................................................................... 1,700 (1,251)
Continuous OEI 2 power rating – 60 minute (Cont 2)
Take-off power rating
Continuous take-off power rating (30 min)
(Í=0, Ìfl=0, ISA):
Power, hp (kW).................................................................... 1,500 (1,104)
flat rated up to tamb, °C...................................................................... +55
Specific fuel consumption, kg/hp·h................................................. .0.251
Maximum continuous power rating
(Í=0, Ìfl=0, ISA):
Power, hp (kW)....................................................................... 1,200 (883)
flat rated to tamb, °C........................................................................... +60
Specific fuel consumption, kg/hp·h.................................................. 0.266
Cruise power rating
(Í=0, Ìfl=0, ISA):
Power, hp (kW)....................................................................... 1,000 (736)
flat rated up to tamb, °C...................................................................... +60
Specific fuel consumption, kg/hp·h.................................................. 0.280
Engine dry weight, kg......................................................................... 295 |
| Avionics | The Supplementary Type Certificates (STC) were obtained for all equipment of the Mi-8MSB helicopter
GTN650 - Multifunctional navigation and communication equipment;
SN3500 - Horizontal situation indicator;
KN63 - Radio distance measurement equipment with indicator;
ADF3502 - Automatic radio compass;
MKR3300 - Marker beacon receiver;
RDR2100 - Meteo-navigation radar station;
KVG-350 - Vertical gyro;
EX600 - Multifunctional radar indicator;
GTX33H - ATC transponder;
RN-7 - Navigation and tactical graphic processor with function HTAWS;
MDU-268 - Multifunctional displays;
AD32 - System for air data measurement, indication and warning of deviations from selected altitude;
LUN1241 - Gyro horizon;
Almaz-UP - Airborne equipment for voice warning system;
Aerox - Oxygen equipment;
Artex C406-1HM - Emergency radio beacon;
DK140 - Hydroacoustic beacon;
CAS67A - Traffic collision avoidance system;
BAS-V - Centralized warning system;
DVCS6100 - Digital voice communication system;
ISAT200A - Satellite communication and position monitoring system;
IC-F8100 - Communication radio;
DF-935 - Radio equipment for orientation. |
| Equipment | AIRCRAFT EQUIPMENT COMPLEX
The complex electronic hardware provides an opportunity for making day and night flights under ordinary and difficult meteorological conditions according to the instrument flight rules (IFR) taking into account the effective ICAO requirements.
Resolved issues:
- navigation by ground beacons VOR, DME, NDB;
- landing according to the 1-st category using systems NDB, ILS, VOR, DME and marker beacon.
- non-precision approach according to satellite navigation data GPS;
- making flights under area navigation conditions B-RNAV (RNP-5);
- making flights in vertical separation system with warning indication of deviations from selected altitude;
- preprogramming of flight plan;
- making flights according to search-and-rescue operations;
- making low-altitude day and night flights in unknown unmarked areas, including mountainous areas, under ordinary and difficult meteorological conditions using the information received from HTAWS;
- automatic flight data transmission to AT controller;
- automatic flight data transmission to air traffic participants to take joint measures for prevention of collisions;
- providing external communication in the VHF range with frequency spectrum of 8.33/25 kHz, internal communication between crew members, public address and talks between passengers and crew members;
- providing external communication in the HF range;
- providing monitoring of helicopter position and satellite communication. |
| Modifications/Conversions | | This helicopter can also be used as a passenger helicopter, for extinguishing fires, for conducting search and rescue operations, etc. The cabin of the helicopter is designed as a LEGO constructor, which allows it to be quickly (about 2 hours) converted for various purposes. |
| Opmerkingen | In August 2013, Mi-8MSB helicopter powered by TV3-117VMA-SBM1V Series 4Å new generation engines established a set of world records (per FAI classification) at Kirovskoye airfield, Autonomous Republic of Crimea, city of Feodosiya:
1. Absolute world record in E-1 class (helicopters):
•• maximum altitude at level flight – 9,150 m;
2. Records in E-1g subclass of E-1 class (weight from 6,000 kg to 10,000 kg):
•• maximum altitude reached without cargo – 9,150 m;
•• maximum flight altitude with a payload of 100 kg – 9,150 m;
•• maximum flight altitude with a payload of 200 kg – 8,420 m;
•• maximum flight altitude with a payload of 1,000 kg – 8,420 m;
•• maximum flight altitude with a payload of 2,000 kg – 7,525 m;
•• maximum flight cargo lifted to an altitude of 2,000 m – 3,019 kg.
3. Records in E-1h subclass of E-1 class (weight from 10,000 kg to 20,000 kg):
•• maximum flight cargo lifted to an altitude of 2,000 m – 5,566 kg;
•• maximum flight altitude with a payload of 5,000 kg – 5,440 m. |
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