Samiksha Jaiswal (Editor)

Bell 206

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Top speed
  
222 km/h

Weight
  
718 kg

Wingspan
  
10 m

Engine type
  
Allison Model 250

Range
  
702 km

Length
  
12 m

Unit cost
  
900,000–1,200,000 USD

Bell 206 Bell 206 JetRanger Bank of aircraft

Bell 206l 4 longranger landing full stop


The Bell 206 is a family of two-bladed, single- or twin-engined helicopters, manufactured by Bell Helicopter at its Mirabel, Quebec plant. Originally developed as the Bell YOH-4 for the United States Army's Light Observation Helicopter program, it was not selected by the Army. Bell redesigned the airframe and successfully marketed the aircraft commercially as the five-place Bell 206A JetRanger. The new design was eventually selected by the Army as the OH-58 Kiowa. Bell also developed a seven-place LongRanger, which was later offered with a twin-engined option as the TwinRanger, while Tridair Helicopters offers a similar conversion of the LongRanger called the Gemini ST. The ICAO-assigned model designation "B06" is used on flight plans for the JetRanger and LongRanger, and the designation "B06T" is used for the twin-engined TwinRangers.

Contents

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Bell 206l 4 longranger full start takeoff


Origins and JetRanger

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On October 14, 1960, the United States Navy solicited response from 25 aircraft manufacturers to a request for proposals (RFP) on behalf of the Army for the Light Observation Helicopter (LOH). Bell entered the competition along with 12 other manufacturers, including Hiller Aircraft and Hughes Tool Co., Aircraft Division. Bell submitted the D-250 design, which would be designated as the YHO-4. On May 19, 1961, Bell and Hiller were announced as winners of the design competition.

Bell 206 Bell 206 Wikipedia

Bell developed the D-250 design into the Bell 206 aircraft, redesignated as YOH-4A in 1962, and produced five prototype aircraft for the Army's test and evaluation phase. The first prototype flew on December 8, 1962. The YOH-4A also became known as the Ugly Duckling in comparison to the other contending aircraft. Following a flyoff of the Bell, Hughes and Fairchild-Hiller prototypes, the Hughes OH-6 was selected in May 1965.

Bell 206 Used Bell 206 Jet Ranger Sales Archives Robinson Helicopters

When the YOH-4A was eliminated by the Army, Bell went about solving the problem of marketing the aircraft. In addition to the image problem, the helicopter lacked cargo space and only provided cramped quarters for the planned three passengers. The solution was a redesigned fuselage, sleeker and aesthetically appealing, adding 16 ft3 (0.45 m3) of cargo space in the process. A Bell executive contributed to this redesign by drawing on a sketch two lines extending the fuselage to where it meets the tail. The redesign was designated Bell 206A, and Bell President Edwin J. Ducayet named it the JetRanger, denoting an evolution from the popular Model 47J Ranger.

LongRanger

Bell 206 Bell 206 JetRanger YouTube

The 206L LongRanger is a stretched variant with seating for seven. The fuselage, stretched a total of 30 inches (760 mm), adds two rear-facing seats between the front and rear seats. Since 1975, Bell has produced more than 1,700 LongRangers across all variant types. In 1981, a military version was released, the 206L TexasRanger. The original 206L used an Allison 250-C20B engine, and a series of model upgrades replaced this engine with more powerful versions; the 206L-1 used a 250-C28, and the 206L-3 and 206L-4 used the 250-C30P. In both applications, the 250-C30P is derated from 650 hp for takeoff and 501 hp continuous. The 206L-3 is transmission–limited to 435 hp for take-off, and the 206L-4 is transmission-limited to 495 hp. The derating of the C30P produces an advantage in hot-day and high-altitude operations as it can produce the rated horsepower at higher altitudes and temperatures where applications that use the maximum rating of the engine at sea level suffer accelerated performance deterioration with increases in temperature and altitude. The 206L-3 and L-4 have not been offered in a twin configuration under those model designations.

Bell 206 Bell 206 Wikipedia

In 2007, Bell announced an upgrade program for the 206L-1 and 206L-3 which is designed to modify the aircraft to the 206L-4 configuration; modified aircraft are designated 206L-1+ and 206L-3+. Modifications include strengthened airframe structural components (including a new tailboom), improved transmission, upgraded engine for the L-1, all of which result in a maximum gross weight increase of 300 pounds and increased performance.

Bell 206 Private Air Charter Bell 206 Jetranger with Execflyer

On January 24, 2008, Bell Helicopter announced plans to end production of the Bell 206B-3 version after current order commitments were fulfilled in 2010. In 2011, used 206B-3s sold for around $1.4 million depending upon the equipment and configuration. However, production of the 206L-4 is ongoing as of 2016.

Gemini ST and TwinRanger

The TwinRanger name dates from the mid-1980s when Bell developed the Bell 400 TwinRanger, but it never entered production.

In 1989, Tridair Helicopters began developing a twin–engine conversion of the LongRanger, the Gemini ST. The prototype's first flight was on January 16, 1991, while full FAA certification was awarded in November. Certification covers the conversion of LongRanger 206L-1s, L-3s and L-4s to Gemini ST configuration. In mid-1994 the Gemini ST was certificated as the first Single/Twin aircraft, allowing it to operate either as a single or twin engine aircraft throughout all phases of flight.

The Bell 206LT TwinRanger was a new-build production model equivalent to Tridair's Gemini ST, and was based on the 206L-4. Thirteen 206LTs were built, the first being delivered in January 1994, and the last in 1997. The TwinRanger was replaced in Bell's lineup by the mostly-new Bell 427, whereas Bell intends for the Bell 505 Jet Ranger X to replace the 206 single-engine versions from around 2015 and compete with the Robinson R66.

Operational history

The first Bell 206A flew on January 10, 1966, and the aircraft was revealed later that month at the Helicopter Association of America (HAA) convention. On October 20, 1966, the JetRanger received FAA certification. Delivery of the JetRanger to customers began on January 13, 1967, with the first aircraft being purchased by Harry Holly, CEO of the Hollymatic Corporation and previous owner of a Bell Ranger. In 1968, the United States Navy selected the 206A as its primary trainer, the TH-57 Sea Ranger. The Army also eventually selected the 206A for a light observation helicopter as the OH-58 Kiowa.

The basic shape and design of the JetRanger remained unchanged since 1967, but Bell introduced the 206B JetRanger II in 1971. In 1977, the 206B-3 JetRanger III was introduced with its modified tail rotor and more powerful engine. The JetRanger is popular with news media for traffic and news reporting. The LongRanger is commonly used as an air ambulance and as a corporate transport. On September 1, 1982, pilots H. Ross Perot, Jr. and Jay Coburn departed Dallas, Texas in the "Spirit of Texas", a Bell 206L-2 (N3911Z). They returned on 30 September, 29 days and 3 hours later, completing the first around–the–world helicopter flight, making them Earthrounders. In 1983, Australian Businessman Dick Smith became the first helicopter pilot to complete a solo trip around the world in 260 flight hours. During the trip, he landed his 206B-3 (S/N 3653; VH-DIK) on prepositioned container ships to refuel between Japan and the Aleutian Islands.

In 1993, the U.S. Army chose the Bell 206B-3 as the winner of the New Training Helicopter competition, to serve as its primary training helicopter, the TH-67 Creek. The number of TH-67s being divested by the Army is too small to impact civilian markets.

On July 22, 1994, Ron Bower landed his 206B-3 (N206AJ) at Hurst, Texas, setting a new record for around-the-world flight by a helicopter. Bower had departed on June 24 and returned 24 days, 4 hours, 36 minutes and 24 seconds later, averaging 35.62 knots (40.99 mph, 65.97 km/h). Bower had added a 91-gallon auxiliary fuel tank, which doubled the JetRanger III's range.

In September 1995 in southwestern Washington State, a low–flying LongRanger was downed by a metal arrow launched by an irate deer hunter. The arrow pierced a rotor blade, bending the blade. The arrow shaft tore the tailfin and boom as it was being chopped up by the spinning rotor. The helicopter was still flyable, but the pilot made a precautionary landing to assess the damage.

On 20 August 2014, Guatemala's Chief of Army Staff was killed when his Bell 206 crashed.

Civilian

Bell 206
Five (5) YOH-4A prototypes, for flight evaluation in the Army's LOH program (1963).
Bell 206A
Initial production version, powered by an Allison 250-C18 turboshaft engine. FAA-certified in 1966. Selected as the OH-58A Kiowa in 1968.
Agusta-Bell 206A
License-built in Italy.
Bell 206A-1
OH-58A aircraft that are modified for FAA civil certification.
Agusta-Bell 206A-1
License-built in Italy.
Bell 206B
Upgraded Allison 250-C20 engine.
Agusta-Bell 206B
License-built in Italy.
Bell 206B-2
Bell 206B models upgraded with Bell 206B-3 improvements.
Bell 206B-3
Upgraded Allison 250-C20J engine and added 2 inches (51 mm) to tail rotor diameter for yaw control.
Bell 206L LongRanger
Stretched, seven-seat configuration, powered by an Allison 250-C20B turboshaft engine.
Bell 206L-1 LongRanger II
Higher-powered version, powered by an Allison 250-C28 turboshaft engine.
Bell 206L-1+ LongRanger
Bell modifications, including 250-C30P engine, to upgrade aircraft to 206L-4 configuration.
Bell 206L-3 LongRanger III
Powered by an Allison 250-C30P turboshaft engine.
Bell 206L-3+ LongRanger
Bell modifications to upgrade aircraft to 206L-4 configuration.
Bell 206L-4 LongRanger IV
Improved version, 250-C30P engine and transmission upgrade.
Bell 206LT TwinRanger
Twin-engined conversions and new-builds of the 206L; replaced by the Bell 427.
Bell 407
based on the 206L with four-blade rotor system.
Bell 417
upgraded 407 with larger engine; project canceled.
HESA Shahed 278
An Iranian re-hash of Bell 206 components.
Aurora Flight Sciences Tactical Autonomous Aerial Logistics System test platform

Military

Bell 206AS
Export version for the Chilean Navy.
Bell CH-139 JetRanger
Canadian military designation for the Bell 206B-3.
OH-58 Kiowa
Light observation helicopter that replaced the OH-6A Cayuse.
TH-57A Sea Ranger
40 commercial Bell 206A aircraft purchased as the primary U.S. Navy helicopter trainer in January 1968 for training prospective U.S. Navy, U.S. Marine Corps, U.S. Coast Guard and select NATO/Allied helicopter pilots.
206L TexasRanger
proposed export military version. One demonstrator was built (1981).
TH-57B
45 commercial Bell 206B-3 helicopters purchased by the US Navy in 1989 as replacements for the TH-57A for primary training under visual flight rules.
TH-57C
71 commercial Bell 206B-3 helicopters purchased by the US Navy beginning prior to 1985 with cockpits configured for advanced training under instrument flight rules.
TH-57D
Planned upgrade program to convert US Navy TH-57B and TH-57C aircraft to a single standard digital cockpit.
TH-67 Creek
137 commercial Bell 206B-3 purchased in 1993 as the primary and instrument helicopter trainer for the US Army at Fort Rucker, Alabama. 35 in VFR configuration and 102 in IFR configuration. The US Army currently has 181 units, of which 121 are in VFR configuration and 60 are in IFR configuration. All TH-67 display US registrations ("N" numbers) and are operated as public use aircraft.
Zafar 300
an Iranian modification to tandem–seat gunship, probably for propaganda purposes only.

Operators

The Bell 206 has been popular for all types of uses both commercial and private.

Military and government

 Albania
  • Albanian Air Force
  •  Argentina
  • Argentine Army Aviation
  •  Australia
  • Australian Army
  • Queensland Police Service
  •  Bangladesh
  • Bangladesh Air Force
  • Bangladesh Army
  •  Brazil
  • Brazilian Air Force
  • Brazilian Navy
  •  Bulgaria
  • Bulgarian Air Force
  •  Chile
  • Chilean Air Force
  • Chilean Navy
  •  Colombia
  • Colombian Air Force
  •  Croatia
  • Croatian Air Force
  •  Ecuador
  • Ecuadorian Air Force
  • Ecuadorian Navy
  •  Finland
  • Finnish Border Guard
  •  Guatemala
  • Guatemalan Air Force
  •  Guyana
  • Guyana Defence Force
  •  Iran
  • Islamic Republic of Iran Air Force
  • Islamic Republic of Iran Army
  •  Iraq
  • Iraqi Air Force
  •  Israel
  • Israeli Air Force
  •  Italy
  • Italian Army
  •  Jamaica
  • Jamaica Defence Force
  •  Japan
  • Japan Coast Guard
  •  Latvia
  • Latvian State Border Guard
  •  Lesotho
  • Lesotho Defence Force
  •  Macedonia
  • Macedonian Air Force
  • Macedonian police (as of 2005)
  •  Mexico
  • Mexican Air Force
  •  Morocco
  • Royal Moroccan Air Force
  •  Pakistan
  • Pakistan Army
  • Pakistan Coast Guards Air Wing
  •  Peru
  • Peruvian Navy
  •  Serbia
  • Serbian Ministry of the Interior
  •  Slovenia
  • Slovenian Air Force and Air Defence
  •  Sri Lanka
  • Sri Lanka Air Force
  •  Republic of China (Taiwan)
  • Republic of China Army
  •  Thailand
  • Royal Thai Army
  • Royal Thai Police
  •  Turkey
  • Turkish Army
  •  Uganda
  • Ugandan Air Force
  •  United States
  • San Juan County, New Mexico Sheriff's Office
  • Los Angeles Police Department
  • United States Army
  • United States Navy
  •  Venezuela
  • Venezuelan Army
  • Venezuelan Navy
  •  Yemen
  • Yemeni Air Force
  • Former operators

     Australia
  • Royal Australian Navy
  •  Canada
  • Canadian Forces
  •  Chile
  • Chilean Army
  •  Jamaica
  • Jamaica Defence Force
  •  Malta
  • Armed Forces of Malta
  •  Sweden
  • Swedish Air Force
  • Swedish Navy
  • Specifications (206B-L4)

    Data from Bell 206B-L4 specifications

    General characteristics

  • Crew: one pilot
  • Capacity: four passengers
  • Length: 39 ft 8 in (12.11 m)
  • Rotor diameter: 33 ft 4 in (10.16 m)
  • Height: 9 ft 4 in (2.83 m)
  • Disc area: 872 ft² (81.1 m²)
  • Empty weight: 2,331 lb (1,057 kg)
  • Max. takeoff weight: 3,200 lb (1,451 kg)
  • Powerplant: 1 × Allison 250-C30P turboshaft, 420 shp; derated to 317 shp due to drivetrain limitations (310 kW)
  • Performance

  • Never exceed speed: 130 knots (241 km/h, 150 mph)
  • Maximum speed: 120 knots (222 km/h, 138 mph)
  • Range: 374 nmi (430 mi, 693 km)
  • Service ceiling: 13,500 ft (4,115 m)
  • Rate of climb: 1,350 ft/min (6.9 m/s)
  • Disc loading: 4 lb/ft² (177 N/m²)
  • Power/mass: 0.26 hp/lb (430 W/kg)
  • References

    Bell 206 Wikipedia


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