Mi-8MSB

Mi-8MSB Medium class transport helicopter

In August 2013, Mi-8MSB helicopter powered by TV3-117VMA-SBM1V Series 4Е new generation engines established a set of world records (per FAI classification)

Цена: $ 7 600 000

In 2011, the State Aviation Administration of Ukraine issued to Motor Sich JSC Certificate CP No. 0009 for designer of aviation equipment and Additional type certificate No. ДТВ-0003 for the Mi-8MSB helicopter.

Helicopters Motor Sich Ltd was founded for promotion of own aviation products and mastering of new business activity. The main function of this specialized subdivision consists in organization of production of own high-performance helicopter. In 2012 the helicopters production was certified by the State Aviation Administration of Ukraine.

MAIN CHARACTERISTICS OF TV3-117VMA-SBM1V,
SERIES 4E, ENGINE

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) (H=0, Mf|=0, ISA +20C):
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) (H=0, Mf|=0, ISA):
Power, hp (kW)................................................... 1,500 (1,104)
flat rated up to t_amb, °C....................................... +55
Specific fuel consumption, kg/hp-h......................0.251

Maximum continuous power rating (H=0, Mf|=0, ISA):
Power, hp (kW).................................................. 1,200 (883)
flat rated to t_amb, °C........................................... +60
amb
Specific fuel consumption, kg/hp-h..................0.266

Cruise power rating (H=0, Mf|=0, ISA):
Power, hp (kW)................................................ 1,000 (736)
flat rated up to t_amb., °C.................................. +60
amb
Specific fuel consumption, kg/hp-h 0.280
Engine dry weight, kg.................................... 295

OUTLINE DRAWING AND PRINCIPAL DIMENSIONS

COMPARATIVE CHARACTERISTICS OF ENGINES

Environmental conditions at which engine takeoff power is flat-rated

COMPARATIVE CHARACTERISTICS OF ENGINES

COMPARISON OF OPERATIONAL PARAMETERS OF HELICOPTERS

In August 2013, Mi-8MSB helicopter powered by TV3-117VMA-SBM1V Series 4E 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.

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.

COMPLEX COMPOSITION

The Supplementary Type Certificates (STC) were obtained for all equipment of the Mi-8MSB helicopter

Download presentation Mi-8MSB.pdf

Ткаченко Анатолий Владимирович
Anatoliy V. Tkachenko
( +38067 9583148
     www.An-26.com
* An-26@meta.ua
* clef@An-26.com