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MBB Bölkow Bo-105

November 29, 2008 by R.Vogelaar 

Bölkow Bo-105CB-4 B-70 Royal Netherlands Army

Bölkow Bo-105CB-4 B-70 Royal Netherlands Army

The Bo-105CBS-5 Army or Navy is a lightweight twin-engine multi-role military helicopter. It is built by the Eurocopter Group (since July 10th 2000 member of EADS), owned 70% by Aérospatiale France and 30% by Daimler Aerospace (DASA) of Germany. The military version of the Bo-105 include the antitank version with weapon-carrying outriggers and the scout version which has a mast-mounted sight above the main rotor. Missions include: direct air support, antitank, reconnaissance, search and rescue, and transport. In addition to reconnaissance, observation and surveillance missions. Many civil operators use the Bo-105 for medical assistance by accidents. Also for police operations is the Bo-105 perfect.

The Bo-105 was developed initially by Messerschmitt-Bölkow-Blohm in Germany. Others are built in Chile, the Philippines, Indonesia (NBo-105), and Spain (CASA Bo-105/ATH).

  • Bo-105CB: The standard production variant.
  • Bo-105CBS: VIP version with a slightly longer fuselage to accommodate 6 passengers, some used in a SAR role.
  • Bo-105LS: Upgraded to 2x 550-shp Allison 250-C28 turbo shafts engines for extended capabilities in high altitudes and temperatures. Produced only in Canada.
  • Bo-105M/VBH: Standard reconnaissance version.
  • Bo-105P/PAH1: Standard antitank version.
  • The Bo-105P has a roof-mounted direct-view, daylight-only sight to allow firing of HOT ATGMs. Options exist to fit a thermal imaging system for night operations, and a laser designator.
  • Available avionics include weather radar, Doppler and GPS navigation, and an autopilot. It is capable of operation in day, night, and instrument meteorological conditions.

 

 

Developing Nation:

Germany.

Manufacturer/Designer: 

Eurocopter.

Task:

Light utility helicopter .

First Flight:

February 16, 1967.

First Delivery:

1979.

First Operational:

1980.

Crew:

1 or 2.

Troops/passengers:

4 or 5

Maine rotor diameter:

9,84 m.

Maine rotor disc area:

76,05 m².

Tail rotor diameter:

1,90 m.

Tail rotor disc area:

2,835 m².

Length overall, rotors turning:

11,86 m.

Length fuselage:

8,56 m.

Height overall:

3,00 m.

Engine (s):

Two Allison 250-C-20B each rated at 313 kW for take-off and 298 kW for continuous running.

Weight:

- Empty: 1.276 Kg.

- Internal fuel: 456 Kg.

- Max. payload: 691 Kg.

Max. Take off weight:

2.500 Kg.

Cruise Speed:

242 km/h.

Max. Speed:

270 km/h at m.

Service ceiling:

5.180 m.

Hovering ceiling:

- in ground effect 2.560 m.

- out of ground effect 1.615 m.

Max. Range:

1.112 km.

Performance:

Max. endurance 2 hours 10 minutes.

Rate of climb:

480 m per minute.

Weapons:

- Rheinmetall Rh 202 20mm cannon.

- AIM-92A Stinger.

- AS-12 ASM pods

- 2.75-in rocket pods.

- 68-mm SNEB rocket pods.

- 50-mm SNIA rockets.

- TOW I air-to-ground missile.

- TOW II air-to-ground missile.

- Hot II air-to-ground missile.

Military Bölkow Bo-105 operators :

Bahrain.

- 3 Bo-105C

Brunei.

- 5 Bo-105CB

- 1 Bo-105CBS

Chile.

- 7 Bo-105C

- 10 Bo-105S

- 1 Bo-105LS-A1

- 2 Bo-105CBS

- 5 Bo-105CB

Ciskei.

- 1 Bo-105

Colombia. 

- 2 Bo-105CB

Dubai.

- 6 Bo-105S

Germany.

- 208 Bo-105P

-   96 Bo-105M

Indonesia.

- 12 NBo-105C

- 4 NBo-105SC

- 18 NBo-105C/CB

Iraq.

- 75 Bo-105C

Jordan.

- 3 NBo-105C

Kenya.

- 1 Bo-105S

Lesotho.

- 2 Bo-105CBS

Mexico.

- 6 Bo-105C

- 5 Bo-105CB

Netherlands.*

- 31 Bo-105CB-4

Peru.

- 18 Bo-105C

- 6 Bo-105L

Philippines.

- 4 Bo-105C

- 10 Bo-105SC

Sierra Leone.

- 1 Bo-105C

Spain.

- 28 Bo-105ATH (HA.15)

- 18 Bo-105GSH (HR.15)

- 14 Bo-105LOH (HR.15)

Sweden.

- 20 Bo-105CB (Hkp 9B)

Trinidad and Tobago.

- 1 Bo-105CBS

 

*number 32 is a civilian Bo-105D, G-AZTI is an instruction aircraft at LETS (Air Force School)

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