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BO-105 German Light Utility Helicopter

BO-105

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Basic Information
Name
BO-105 German Light Utility Helicopter
Designation
BO-105
Alternate Designation
B0-105, MBB BO 105, Messerschmitt-Bölkow-Blohm Bo 105
Equipment Type
Manufacturer
Messerschmitt-Bölkow-Blohm (MBB)
Date of Introduction
1970
Description

The Messerschmitt-Bölkow-Blohm Bo 105 is a light, twin-engine, multi-purpose helicopter developed by Bölkow of Ottobrunn, West Germany. It was the first light twin-engine helicopter in the world, and the first rotorcraft that could perform aerobatic maneuvers such as inverted loops.[5][6] The Bo 105 features a revolutionary hingeless rotor system, at that time a pioneering innovation in helicopters when it was introduced into service in 1970. Production of the Bo 105 began at the then-recently merged Messerschmitt-Bölkow-Blohm (MBB). The BO105 is considered a rugged, time-proven design. It is easily maintained in the field and is highly maneuverable in flight due to a unique hingeless main rotor system. The compact cabin has a flat floor, rear clamshell doors and provides excellent visibility for the pilot. The main production facilities for producing the Bo 105 were located in Germany and Canada; due to the level of export sales encountered, additional manufacturing lines were set up in Spain, Indonesia, and the Philippines.[7] MBB became a part of Eurocopter in 1991, who continued production of the type until 2001. The Bo 105 was formally replaced in Eurocopter's product range by the newer Eurocopter EC135, which was itself a development of the Bo 105.

Air & Air Defense Specifications
Crew 1
Engine Gas Turbine (400 hp)
Endurance 3.00 hrs
Rotor Diameter 9.84 m
Variants
Bo 105A First production model primarily for civil use and equipped with two Allison 250-C18 turbine engines.
Bo 105ATH Anti-tank version for the Spanish Army.
Bo 105C Initial version. Developed in 1972 and equipped with two Allison 250-C20 turbines engines.
Bo 105CB Light observation, utility transport version. Developed in 1976 and equipped with two Allison 250-C20B turbine engines of which 30 were delivered to The Royal Netherlands Air Force.[
Bo 105CBS Utility transport version, with the fuselage stretched by 10 inches and an extra window for emergency medical service duties
EC-Super Five High performance version of the Bo 105CBS.
Bo 105CBS-5 Also known as Superfive, with increased lifting capabilities similar to the LS A3 Superlifter
Bo 105D UK certified offshore version.
Bo 105GSH Armed scout version for the Spanish Army.
Bo 105HGH A high speed research variant wint aerodynamic refinements, such as a rotor head fairing, rear fuselage fairing, small individual skids and 6 m (20 ft) long fixed auxiliary wings.
Bo 105 KLH license-produced combat version of CBS-5 custom-fitted with Korean mission equipment package including communication, navigation, electronic warfare and target acquisition system, to meet Republic of Korea Army's operational requirements. KLH also has greatly improved rotor blade and transmission system. 12 are in service.
Bo 105LOH Observation version for the Spanish Army.
Bo 105LS A1 Developed in 1984 with stretched fuselage and two Allison 250-C28C turbine engines.
Bo 105LS A3 Developed in 1986 with maximum take-off weight increased to 2,600 kg.
Bo 105LS A3 "Superlifter" Developed in 1995 with maximum mission weight increased to 2,850 kg.
Bo 105M With its army designation "VBH" (Verbindungshubschrauber; 'liaison chopper'), is a light transport and surveillance helicopter
Bo 105MSS Maritime version, fitted a search radar.
Bo 105P/BSH Proposed escort version for the German Army, armed with Stinger air-to-air missiles.
Bo 105P/PAH-1 With its army designation "PAH-1" and "PAH-1A1" for the upgraded version (PAH=Panzerabwehrhubschrauber; 'Tank-defence helicopter'), is an anti-tank helicopter armed with wire-guided HOT ATGMs (HOT2 for the upgraded A1 version).
Bo 105P/PAH-1A1 Improved anti-tank version for the German Army, fitted with six HOT missile tubes.[
Bo 105P/PAH-1 Phase 2 Proposed night attack version for the German Army
Bo 105S Search and rescue version.
Bo 105/Ophelia Test and trials aircraft fitted with a mast-mounted sight.
NBO-105 Were Manufactured by IPTN under license from MBB (now Airbus Helicopters) 1976–2011; only rotors and transmission now supplied by Germany; originally NBO-105 CB, but stretched NBO-105 CBS available from 101st aircraft onwards. 122 were produced, Dirgantara Indonesia stopped production in 2008.
Bo 105 Executaire Boeing Vertol and Carson Helicopters manufactured a 24.5 cm stretched version of the Bo 105 under license as the Executaire in an attempt to break into the U.S. light helicopter market, but sales were dismal.
Bo 105E-4 12 German Army Bo 105P upgraded and overhauled for a 10 million euro contract and donated to Albania first batch delivered in 2006, the helicopters have better performance and avionics. The conversion of other Bo 105 helicopters from the German Armed Forces is also under consideration with a view to future sales.
Bo 106 Widened cabin to seat 7 instead of 5. First flight was on 26 September 1973. A single helicopter of that variant has been made (registration D-HDCI, serial no. 84). The Bo 106 was also equipped with more powerful Allison 250 C 20B engines. In 1981, the German air rescue organization Deutsche Rettungsflugwacht/DRF Luftrettung bought that prototype and had it rebuilt into a 105 CB-2 with a standard cabin. It flew for DRF until November 1993 under the registration D-HCCC, but in 1994 it was put aside to gain spare parts for another DRF helicopter (Bo 105 CBS-S, registration D-HNNN, serial number 662).
PADC Hummingbird An unlicensed development of the Bo 105C with revised cockpit structure.
System
Alternative Designation B0-105, MBB BO 105, Messerschmitt-Bölkow-Blohm Bo 105
Primary Function light, twin-engine, multi-purpose helicopter
Manufacturer Messerschmitt-Bölkow-Blohm (MBB)
In Service 1970-Present
Crew 1 or 2 ea
Passengers 4-5 ea
Blades, Main Rotor 4
Blades, Tail Rotor 2 ea
Number of Engines 2 ea
Day/Night Capable Yes
All Weather Capable Yes
Takeoff or Landing Limitations INA
Number of Hard Points INA
Skids The main body rests on a pair of skids (with optional flotation skids for seagoing helicopters).
Note The rotor system is entirely hingeless, the rotor head consisting of a solid titanium block to which the four blades are bolted;
Dimensions
Length 11.6 m
Width 2.53 m
Height 3.00 m
Rotor Diameter 9.84 m
Tailrotor Diameter 1.90 m
Weight, Empty 1,433 kg kg
Weight, Takeoff 2,500 kg kg
Weight, Sling Load 1,200 kg kg
Automotive
Engine Name 2 x Allison 250-C 20B Turbine
Engine Type Turbine
Engine Power 400 hp
RPM 424
Cruising Range 528 km
Speed, Maximum 243 km/h
Speed, Cruise 204 km/h
Ceiling 5,180 m
Fuel Capacity 570 liters
Hover Ceiling IGE 1,829 m
Hover Ceiling OGE 1,158 m
Climb Rate 7.4 m/sec
Endurance 3 hr 30 min (standard fuel, maximum payload)
Airfoil NACA 23012
Communications
Radio Various depending on country and mission
Wing Mounted Weapons
Missile System
Name HOT (missile)
Type High Subsonic, Optical, Remote-Guided, Tube-Launched ATGM Missile
Manufacturer Euromissile (now MBDA)
In Service 1977-Present
Variants HOT 1, HOT 2, HOT 3
Length 1.30 m
Diameter 0.15 m
Weight 24.5 kg
Wingspan 0.31 m
Basic Load 6 ea
Warhead Type Tandem charge HEAT
Engine Two-stage solid fuel rocket
Operational Range 75-4,300 m
Speed 864 km/h
Guidance System SACLOS
Fire Control
Fire Control System Type INA
Fire Control Radar INA
Digital or Analog Cockpit Analog
Direct Fire Control INA
Laser Designator INA
Automated Helmet INA
Sensor Suite(s) Available Yes
Position Location System Yes
Protection
Stealth Properties No
Heat Signature Reduction INA
Add on Armor Available
NBC Protection Yes
EW INA
Counter Measures (Chaff/Flares) INA
Details
Country of Origin Germany
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
11.6 m
Width
2.53 m
Height
3 m
Weight
2500 kg
Operators (10)
Spain
Albania
Bahrain
Brunei
Chile
Colombia
Indonesia
Mexico
Peru
Uruguay
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